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  <front>
    <journal-meta><journal-id journal-id-type="publisher">AMT</journal-id><journal-title-group>
    <journal-title>Atmospheric Measurement Techniques</journal-title>
    <abbrev-journal-title abbrev-type="publisher">AMT</abbrev-journal-title><abbrev-journal-title abbrev-type="nlm-ta">Atmos. Meas. Tech.</abbrev-journal-title>
  </journal-title-group><issn pub-type="epub">1867-8548</issn><publisher>
    <publisher-name>Copernicus Publications</publisher-name>
    <publisher-loc>Göttingen, Germany</publisher-loc>
  </publisher></journal-meta>
    <article-meta>
      <article-id pub-id-type="doi">10.5194/amt-19-2763-2026</article-id><title-group><article-title>Studying anomalous propagation over marine areas using an experimental AIS receiver set-up</article-title><alt-title>Studying anomalous propagation over marine areas</alt-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1">
          <name><surname>Rautiainen</surname><given-names>Laura</given-names></name>
          <email>laura.rautiainen@fmi.fi</email>
        <ext-link>https://orcid.org/0000-0002-2363-2647</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Johansson</surname><given-names>Milla M.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-9566-5149</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Lensu</surname><given-names>Mikko</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-3932-4139</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Tyynelä</surname><given-names>Jani</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-4360-3800</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Jalkanen</surname><given-names>Jukka-Pekka</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-8454-4109</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Hasu</surname><given-names>Mikael</given-names></name>
          
        <ext-link>https://orcid.org/0009-0004-9838-7764</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Stenbäck</surname><given-names>Ken</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Lonka</surname><given-names>Harry</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff2">
          <name><surname>Laakso</surname><given-names>Lauri</given-names></name>
          
        </contrib>
        <aff id="aff1"><label>1</label><institution>Finnish Meteorological Institute, Erik Palménin Aukio 1, Helsinki, Finland</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>Atmospheric Chemistry Research Group, Chemical Resource Beneficiation, North-West University, Potchefstroom, South Africa</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Laura Rautiainen (laura.rautiainen@fmi.fi)</corresp></author-notes><pub-date><day>23</day><month>April</month><year>2026</year></pub-date>
      
      <volume>19</volume>
      <issue>8</issue>
      <fpage>2763</fpage><lpage>2785</lpage>
      <history>
        <date date-type="received"><day>15</day><month>April</month><year>2025</year></date>
           <date date-type="rev-request"><day>11</day><month>August</month><year>2025</year></date>
           <date date-type="rev-recd"><day>16</day><month>January</month><year>2026</year></date>
           <date date-type="accepted"><day>19</day><month>January</month><year>2026</year></date>
      </history>
      <permissions>
        <copyright-statement>Copyright: © 2026 Laura Rautiainen et al.</copyright-statement>
        <copyright-year>2026</copyright-year>
      <license license-type="open-access"><license-p>This work is licensed under the Creative Commons Attribution 4.0 International License. To view a copy of this licence, visit <ext-link ext-link-type="uri" xlink:href="https://creativecommons.org/licenses/by/4.0/">https://creativecommons.org/licenses/by/4.0/</ext-link></license-p></license></permissions><self-uri xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026.html">This article is available from https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026.html</self-uri><self-uri xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026.pdf">The full text article is available as a PDF file from https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026.pdf</self-uri>
      <abstract><title>Abstract</title>

      <p id="d2e161">Automatic Identification System (AIS) is a wireless communication system used by vessels to exchange real-time information with each other and with coastal authorities, enhancing situational awareness and maritime safety. Consequently, safety at sea depends on reliable signal transmission, which can be disrupted by anomalous signal propagation. In particular, tropospheric ducting can extend the AIS antenna horizon, allowing messages to be received over greater distances than under standard conditions. To study the behaviour of the AIS signal under standard and anomalous propagation conditions, 1-year of AIS-observations were collected from two antennae at 7 and 30 m heights above the mean sea level on the Utö Island in the Baltic Sea. The AIS antennae were co-located with mast-mounted measurements of temperature and humidity. This allows for studying the AIS signal propagation alongside observed refractivity profiles. The AIS over-the-horizon observations occurred 34 % of the time for the 7 m antenna and 59 % of the time for the 30 m antenna, mainly during the spring and summer months. A strong diurnal cycle was observed in the Archipelago Sea, north of Utö, while no diurnal cycle was observed in the open sea region south of Utö. During periods of anomalous signal propagation, the AIS messages were received from farther away, from up to 600 km from Utö and the observed received signal strength decayed slower with distance, indicating reductions in propagation losses due to ducting. Anomalous AIS observations were also associated with stronger and higher ducts; when the duct height was 59 m, the occurrence rates were 90 % and 95 % for the 7 and 30 m antenna, respectively.</p>
  </abstract>
    
<funding-group>
<award-group id="gs1">
<funding-source>Research Council of Finland</funding-source>
<award-id>338150</award-id>
</award-group>
</funding-group>
</article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <label>1</label><title>Introduction</title>
      <p id="d2e173">The maritime situational awareness and safety depend on effective radio communications. The Automatic Identification System (AIS) is a maritime communication system that was developed to prevent maritime collisions and improve vessel tracking <xref ref-type="bibr" rid="bib1.bibx25" id="paren.1"/>. It is used for communication between vessels, and between vessels and vessel traffic services, via 162 MHz channel belonging to the marine VHF range (156–162 MHz). VHF signals propagate via line-of-sight (LoS) and interact with the troposphere and physical objects and surfaces via refraction, reflection, diffraction and scattering. As AIS plays an important role in maritime safety and situational awareness, it is important to assess its functioning under different signal propagation conditions, in particular under tropospheric ducting.</p>
      <p id="d2e179">Tropospheric ducting is a phenomenon where due to the vertical gradients of air temperature, humidity and pressure, radio waves get strongly bent towards the Earth's surface, causing them to be trapped in a quasi-horizontal layer known as a duct. Within the duct, the radio waves can travel to further distances than outside of the duct <xref ref-type="bibr" rid="bib1.bibx44" id="paren.2"/>. Due to its impacts on the reliability of signal transmission, ducting has been the subject of study in the field of radio communications for decades <xref ref-type="bibr" rid="bib1.bibx29" id="paren.3"/>. Ducts can be observed in vertical profiles of refractivity which in turn can be derived from vertical profile measurements of air temperature, humidity and pressure from radiosondes <xref ref-type="bibr" rid="bib1.bibx4 bib1.bibx39 bib1.bibx5 bib1.bibx36 bib1.bibx35 bib1.bibx21 bib1.bibx45" id="paren.4"><named-content content-type="pre">e.g.</named-content></xref> and mast-mounted measurements <xref ref-type="bibr" rid="bib1.bibx13 bib1.bibx12 bib1.bibx1 bib1.bibx54 bib1.bibx22 bib1.bibx46 bib1.bibx47" id="paren.5"><named-content content-type="pre">e.g.</named-content></xref>. In the near surface applications it is common to use modified refractivity (<inline-formula><mml:math id="M1" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>, see Sect. 2.5). Based on the vertical <inline-formula><mml:math id="M2" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-gradient (<inline-formula><mml:math id="M3" display="inline"><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>M</mml:mi><mml:mo>/</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M4" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula> units km<sup>−1</sup>), signal propagation can be divided into four categories: standard refraction (<inline-formula><mml:math id="M6" display="inline"><mml:mrow><mml:mn mathvariant="normal">78</mml:mn><mml:mo>&lt;</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>M</mml:mi><mml:mo>/</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">157</mml:mn></mml:mrow></mml:math></inline-formula>), sub-refraction (<inline-formula><mml:math id="M7" display="inline"><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>M</mml:mi><mml:mo>/</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi><mml:mo>&gt;</mml:mo><mml:mn mathvariant="normal">157</mml:mn></mml:mrow></mml:math></inline-formula>), super-refraction (<inline-formula><mml:math id="M8" display="inline"><mml:mrow><mml:mn mathvariant="normal">0</mml:mn><mml:mo>&lt;</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>M</mml:mi><mml:mo>/</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">78</mml:mn></mml:mrow></mml:math></inline-formula>) and ducting (<inline-formula><mml:math id="M9" display="inline"><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>M</mml:mi><mml:mo>/</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>) <xref ref-type="bibr" rid="bib1.bibx52" id="paren.6"/>. The impacts of ducting on the AIS include increased range, interference and signal degradation, and other data anomalies <xref ref-type="bibr" rid="bib1.bibx26" id="paren.7"/>. Due to the potential impact on operational coverage <xref ref-type="bibr" rid="bib1.bibx42" id="paren.8"><named-content content-type="pre">e.g.</named-content></xref>, developing operative ducting monitoring and forecasting is important to ensure maritime safety and situational awareness.</p>
      <p id="d2e348">Besides ducting, there are other causes of anomalous propagation for the VHF channel <xref ref-type="bibr" rid="bib1.bibx49 bib1.bibx14 bib1.bibx7 bib1.bibx50 bib1.bibx33" id="paren.9"/>. However, troposcatter and ducting are the most relevant factors resulting in anomalous signal propagation at distances of less than 1000 km. Although troposcatter, i.e. irregularities in the refractive index, can also cause the AIS range to be extended,  ducting has been found to cause a significantly greater reduction in propagation losses <xref ref-type="bibr" rid="bib1.bibx50" id="paren.10"/>. In the northern Baltic Sea region ducting can persist for days <xref ref-type="bibr" rid="bib1.bibx47" id="paren.11"/> and is a common phenomenon particularly during spring and summer months <xref ref-type="bibr" rid="bib1.bibx41 bib1.bibx47" id="paren.12"/>.</p>
      <p id="d2e363">Due to the scarcity of continuous measurements of vertical refractivity over sea areas, there is a growing need for observations that can be used to validate both waveguide propagation models and ducting forecasts based on  numerical weather models.  As the propagation of AIS signal is affected by the  atmosphere, its propagation characteristics inversely tell us about the properties of the atmosphere it propagated trough. Thus AIS can be a valuable tool for filling the observation gaps over marine areas, particularly as inversion methods improve <xref ref-type="bibr" rid="bib1.bibx51 bib1.bibx16 bib1.bibx23" id="paren.13"/>. While the effects of ducting are well-documented across different radio wave frequencies, its potential impact on AIS signals has garnered limited attention due to AIS being a relatively new system. Prior observation-based research focuses mainly on case studies or point-to-point connections for AIS <xref ref-type="bibr" rid="bib1.bibx6 bib1.bibx53 bib1.bibx7" id="paren.14"><named-content content-type="pre">e.g.</named-content></xref>, other systems using the VHF frequency <xref ref-type="bibr" rid="bib1.bibx3 bib1.bibx8" id="paren.15"><named-content content-type="pre">e.g.</named-content></xref> and UHF frequency <xref ref-type="bibr" rid="bib1.bibx15" id="paren.16"/>. Longer time series are needed to establish the occurrence  of anomalous propagation and its diurnal and seasonal cycles. For the northern Baltic Sea region diurnal and seasonal cycles have been previously established based on C-band weather radar ground clutter <xref ref-type="bibr" rid="bib1.bibx41" id="paren.17"/> and X-band surveillance radar over-the-horizon observations <xref ref-type="bibr" rid="bib1.bibx47" id="paren.18"/>. Particularly if AIS is to be used for validating propagation models, it is important to assess how similar the effects of ducting are across different frequencies and systems. Propagation modelling has been used to study AIS signal propagation under ducting <xref ref-type="bibr" rid="bib1.bibx6 bib1.bibx50" id="paren.19"><named-content content-type="pre">e.g.</named-content></xref>.</p>
      <p id="d2e395">Applying AIS data for real-time ducting analyses is complicated. The quantity of messages received  can be overwhelming, particularly in busy shipping areas. The data itself lacks the information of the transmitting antenna which affects the application of the data unless the information is acquired from the operator of each transmitter, as has been done in <xref ref-type="bibr" rid="bib1.bibx6" id="text.20"/>. The data can also include user errors which cause the data to behave in unexpected ways, e.g. the frequency of broadcasted messages does not correspond to the speed of the vessel. Furthermore, the reliability of the data can be questioned as received messages can be unintentionally incorrect or intentionally falsified or spoofed <xref ref-type="bibr" rid="bib1.bibx17 bib1.bibx48" id="paren.21"/>. AIS transponder can also be turned off for illicit operations <xref ref-type="bibr" rid="bib1.bibx38" id="paren.22"/>. Efforts have been put into identifying the false messages in real-time <xref ref-type="bibr" rid="bib1.bibx48 bib1.bibx28 bib1.bibx55" id="paren.23"><named-content content-type="pre">e.g.</named-content></xref>. Most of the methods involve excluding messages with clearly erroneous data, e.g. invalid Maritime Mobile Service Identity (MMSI), positions over land or unavailable coordinates. More sophisticated methods include e.g. expected-motion prediction and triangularization methods based on the time differences observed between different AIS receivers and multisensor data combining e.g. simultaneous radar and AIS observations.</p>
      <p id="d2e412">In this study, an experimental AIS receiver set-up at Utö island in the Baltic Sea is introduced. The set-up includes two receivers installed at different heights, 7 and 30 m above mean sea level (a.m.s.l.), that correspond to heights of mast measurements of temperature and humidity (4, 7, 12, 22, 32 and 59 m a.m.s.l.). This allows for studying the AIS signal propagation alongside observed refractivity profiles. The aim of the study is to (a) introduce the experimental AIS set-up for ducting research and monitoring, (b) explore methods to identify periods of anomalous signal propagation from the AIS data, (c) study how the AIS range and signal strength behave during normal and anomalous conditions, and (d) compare the AIS range with modified refractivity profiles derived from the measurements of temperature and humidity.</p>
</sec>
<sec id="Ch1.S2">
  <label>2</label><title>Materials and Methods</title>
<sec id="Ch1.S2.SS1">
  <label>2.1</label><title>Automatic Identification System (AIS)</title>
      <p id="d2e430">Automatic Identification System (AIS) is a maritime technology where ships broadcast real-time information to other ships and coastal authorities. AIS was introduced already in the late 1990s but since 2002, the International Maritime Organisation (IMO) has set AIS as mandatory for vessels over 300 gross tonnage (GT) on international voyages, cargo ships over 500 GT, and all passenger ships, as part of the SOLAS (Safety of Life At Sea) agreement which required these vessels to fit a Class A AIS transceiver <xref ref-type="bibr" rid="bib1.bibx25" id="paren.24"/>. Later in 2006, simpler and cheaper Class B AIS transceivers were introduced that can be used on recreational boats. AIS operates by broadcasting real-time data as short binary messages using the 162 MHz VHF frequency reserved for the purpose. The messages do not target specific recipients, but the transceivers process messages from all other transceivers within reach. Terrestrial receivers are set up by authorities or by anyone interested in monitoring the ship traffic. As the range of AIS signal is limited to <inline-formula><mml:math id="M10" display="inline"><mml:mo>&lt;</mml:mo></mml:math></inline-formula>100 km under normal propagation conditions, monitoring the marine traffic further away from coast relies on AIS satellites owned by governmental institutions or commercial enterprises.</p>
</sec>
<sec id="Ch1.S2.SS2">
  <label>2.2</label><title>The Experimental AIS Set-up</title>
      <p id="d2e451">This study presents the experimental AIS set-up at the Utö Atmospheric and Marine Research Station, located on the island of Utö, in the Archipelago Sea of the Baltic Sea (59°46<sup>′</sup>50 N, 21°22<sup>′</sup>23 E). The research station has a long history of atmospheric and marine observations dating back to 1881 <xref ref-type="bibr" rid="bib1.bibx2 bib1.bibx32 bib1.bibx24 bib1.bibx31 bib1.bibx30 bib1.bibx19 bib1.bibx46 bib1.bibx47 bib1.bibx20" id="paren.25"/>. The region has a lot of potential for AIS based ducting research and monitoring with many busy sea routes near the island and in the study area. The study area is shown in Fig. <xref ref-type="fig" rid="F1"/>a. The complex archipelago is shown in panel c based on the European digital elevation model (v. 1.1) from the Copernicus Land Monitoring Service <xref ref-type="bibr" rid="bib1.bibx9" id="paren.26"/>.</p>

      <fig id="F1" specific-use="star"><label>Figure 1</label><caption><p id="d2e482"><bold>(a)</bold> The study area encompasses nine Baltic Sea basins. Utö Atmospheric and Marine Research Station is located on the island of Utö in the Archipelago Sea and is denoted by the red diamond. <bold>(b)</bold> The VHF antennae, indicated by the two white arrows, are mounted at 30 m and 7 m a.m.s.l. on the profiling mast, with two GPS antennae next to the VHF antenna at 7 m a.m.s.l. The T-RH sensors at heights 4, 7, 12, 22 and 32 m a.m.s.l. can also be seen on the mast image. Photo by M. Johansson. <bold>(c)</bold> Azimuthal presentation (360°) of elevation [m] from Utö given at 100 m spatial resolution.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f01.png"/>

        </fig>

      <p id="d2e499">In July 2023, two AIS receiver systems were installed at Utö. Each AIS receiver system consists of VHF and GPS antennae, receiver, and data logger (Fig. <xref ref-type="fig" rid="F2"/>). The VHF antennae are Comrod AV7 antennae with vertical polarization and an antenna gain of 2 dBi. The installation heights were set by technical considerations such as location of other close-by radio transmitters and protection against the sea spray. Both antenna cables were set at the same length of 120 m, which introduces approximately 7 dB loss. Although this reduces the sensitivity, it ensures that the set-ups are comparable. The mast set-up is shown in Fig. <xref ref-type="fig" rid="F1"/>b.</p>
      <p id="d2e507">Kongsberg AIS RX610 receivers are used for receiving all incoming AIS messages from Channels 1 (161.975 MHz) and 2 (162.025 MHz). The Received Signal Strength Indicator (RSSI) of each message is logged, with the sensitivity of the receiver being <inline-formula><mml:math id="M13" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">115</mml:mn></mml:mrow></mml:math></inline-formula> dBm which is more sensitive than the typical <inline-formula><mml:math id="M14" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">109</mml:mn></mml:mrow></mml:math></inline-formula> dBm <xref ref-type="bibr" rid="bib1.bibx26" id="paren.27"/>. The incoming messages are pre-processed and saved into hourly data files. The messages are decoded in near-real-time using the freely available Python library Pyais for binary AIS message decoding (<uri>https://pypi.org/project/pyais/</uri>, last access: 8 May 2024). After decoding, further preprocessing includes discarding messages that have virtual<inline-formula><mml:math id="M15" display="inline"><mml:mi mathvariant="italic">_</mml:mi></mml:math></inline-formula>aid parameter that is non-zero or lack location information. The virtual aid parameter is used to exclude virtual Aid-to-Navigation (AtoN) messages that are simulated by nearby AIS stations rather than broadcasted by the real AtoN (e.g. a buoy). The data used for analysis includes time, message type, MMSI, RSSI and location. Based on the location, transmitter distance and the azimuth from the receiver are calculated for each message.</p>

      <fig id="F2" specific-use="star"><label>Figure 2</label><caption><p id="d2e545">An overview of the setup of the AIS receiver and data logger.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f02.png"/>

        </fig>

</sec>
<sec id="Ch1.S2.SS3">
  <label>2.3</label><title>Global AIS data</title>
      <p id="d2e562">The global AIS data used in this study was provided by ORBCOMM Ltd. The global AIS data is a combination of terrestrial and satellite AIS data. ORBCOMM has a commercial satellite network with 18 AIS-enabled satellites. This results in up to 135 satellite passes and overhead coverage up to 90 %. In total 8.9 billion messages were received in 2023. The ORBCOMM global AIS data is independent from the AIS data used in this study and therefore was used as a background “truth” to establish the areal coverage of the experimental AIS set-up over two months, September–October 2023. As the global AIS combines satellite and terrestrial AIS data, it is used as the background truth in the analysis, assuming it shows all vessels present in the study area. However, the global dataset can also be affected by anomalous propagation which can introduce error in the analysis.</p>
</sec>
<sec id="Ch1.S2.SS4">
  <label>2.4</label><title>The maximum AIS range</title>
      <p id="d2e585">The line-of-sight distance (<inline-formula><mml:math id="M16" display="inline"><mml:mi>R</mml:mi></mml:math></inline-formula>) is the maximum distance at which a radio signal can be transmitted and received due to the curvature of the Earth under standard refractivity conditions. It depends on the heights of the receiving (<inline-formula><mml:math id="M17" display="inline"><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mi mathvariant="normal">R</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) and transmitting antennae (<inline-formula><mml:math id="M18" display="inline"><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) and can be calculated:

            <disp-formula id="Ch1.E1" content-type="numbered"><label>1</label><mml:math id="M19" display="block"><mml:mrow><mml:mi>R</mml:mi><mml:mo>=</mml:mo><mml:msqrt><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:mi>a</mml:mi><mml:mi>k</mml:mi></mml:mrow></mml:msqrt><mml:mo>×</mml:mo><mml:mo>(</mml:mo><mml:msqrt><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mi mathvariant="normal">R</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:mo>+</mml:mo><mml:msqrt><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:mo>)</mml:mo><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>

          where <inline-formula><mml:math id="M20" display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula> is the earth radius and <inline-formula><mml:math id="M21" display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> is the earth factor that is <inline-formula><mml:math id="M22" display="inline"><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> for standard atmosphere <xref ref-type="bibr" rid="bib1.bibx43" id="paren.28"/>. The line-of-sight distances for both 7 and 30 m antenna are shown in Fig. <xref ref-type="fig" rid="F3"/>.</p>

      <fig id="F3" specific-use="star"><label>Figure 3</label><caption><p id="d2e693">Estimations of received power [dBm] for the two receiving antennae at 7 m (green) and 30 m (pink) when the transmitting antennae are at heights 10 m (dashed) and 60 m (dotted). The line-of-sight distances for the two antenna heights are shown for transmitting antenna heights of 10 m (square markers) and 60 m (circle markers). The receiver sensitivity is <inline-formula><mml:math id="M23" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">115</mml:mn></mml:mrow></mml:math></inline-formula> dBm (solid line).</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f03.png"/>

        </fig>

      <p id="d2e712">The role of diffraction is greater at lower frequencies. Hence, the maximum range of terrestrial AIS is governed by line-of-sight and diffraction propagation <xref ref-type="bibr" rid="bib1.bibx26" id="paren.29"/>. The smooth earth diffraction propagation loss at 162 MHz can be described:

            <disp-formula id="Ch1.E2" content-type="numbered"><label>2</label><mml:math id="M24" display="block"><mml:mtable rowspacing="0.2ex" class="split" displaystyle="true" columnalign="right left"><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">diff</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">FS</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:mi>F</mml:mi><mml:mo>(</mml:mo><mml:mi>X</mml:mi><mml:mo>)</mml:mo><mml:mo>+</mml:mo><mml:mi>G</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi>Y</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:mo>)</mml:mo><mml:mo>+</mml:mo><mml:mi>G</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi>Y</mml:mi><mml:mi mathvariant="normal">R</mml:mi></mml:msub><mml:mo>)</mml:mo><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">FS</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">20</mml:mn><mml:mi>log⁡</mml:mi><mml:mo>(</mml:mo><mml:mi>D</mml:mi><mml:mo>)</mml:mo><mml:mo>+</mml:mo><mml:mn mathvariant="normal">20</mml:mn><mml:mi>log⁡</mml:mi><mml:mo>(</mml:mo><mml:mi>f</mml:mi><mml:mo>)</mml:mo><mml:mo>+</mml:mo><mml:mn mathvariant="normal">20</mml:mn><mml:mi>log⁡</mml:mi><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mi mathvariant="italic">π</mml:mi></mml:mrow><mml:mi>c</mml:mi></mml:mfrac></mml:mstyle></mml:mfenced><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mi>F</mml:mi><mml:mo>(</mml:mo><mml:mi>X</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mn mathvariant="normal">11</mml:mn><mml:mo>+</mml:mo><mml:mn mathvariant="normal">10</mml:mn><mml:mi>log⁡</mml:mi><mml:mo>(</mml:mo><mml:mi>X</mml:mi><mml:mo>)</mml:mo><mml:mi mathvariant="normal">−</mml:mi><mml:mn mathvariant="normal">17.6</mml:mn><mml:mo>×</mml:mo><mml:mi>X</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mi>X</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.029</mml:mn><mml:mi>D</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mi>G</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi>Y</mml:mi><mml:mrow><mml:mi mathvariant="normal">T</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">R</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mn mathvariant="normal">20</mml:mn><mml:mi>log⁡</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi>Y</mml:mi><mml:mrow><mml:mi mathvariant="normal">T</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">R</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mn mathvariant="normal">0.1</mml:mn><mml:mo>×</mml:mo><mml:msubsup><mml:mi>Y</mml:mi><mml:mrow><mml:mi mathvariant="normal">T</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">R</mml:mi></mml:mrow><mml:mn mathvariant="normal">3</mml:mn></mml:msubsup><mml:mo>)</mml:mo><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mrow><mml:mi mathvariant="normal">T</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">R</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.014</mml:mn><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi mathvariant="normal">T</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>

          where <inline-formula><mml:math id="M25" display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">FS</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the free space propagation loss (dB), <inline-formula><mml:math id="M26" display="inline"><mml:mi>f</mml:mi></mml:math></inline-formula> is the frequency (Hz), <inline-formula><mml:math id="M27" display="inline"><mml:mi>c</mml:mi></mml:math></inline-formula> is speed of light (m s<sup>−1</sup>), <inline-formula><mml:math id="M29" display="inline"><mml:mrow><mml:mi>F</mml:mi><mml:mo>(</mml:mo><mml:mi>X</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is the distance factor (dB), <inline-formula><mml:math id="M30" display="inline"><mml:mi>D</mml:mi></mml:math></inline-formula> is the distance separator, <inline-formula><mml:math id="M31" display="inline"><mml:mrow><mml:mi>G</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi>Y</mml:mi><mml:mrow><mml:mi mathvariant="normal">T</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">R</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> are the height gain factors (dB) and <inline-formula><mml:math id="M32" display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula> is the transmitter and receiver antenna heights (m) <xref ref-type="bibr" rid="bib1.bibx26 bib1.bibx27" id="paren.30"/>. Received power (dBm) can be estimated:

            <disp-formula id="Ch1.E3" content-type="numbered"><label>3</label><mml:math id="M33" display="block"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="normal">EIRP</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">diff</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>G</mml:mi><mml:mi mathvariant="normal">R</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>G</mml:mi><mml:mi mathvariant="normal">Corr</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">misc</mml:mi></mml:msub><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>

          where EIRP is the ship-borne AIS equivalent isotropic radiated power (dBm) typically 41 dBm for Class A vessels, <inline-formula><mml:math id="M34" display="inline"><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi mathvariant="normal">R</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the receiver antenna gain (dBi), <inline-formula><mml:math id="M35" display="inline"><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi mathvariant="normal">Corr</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the receiver correlation gain (dB) (assumed as 5 dB here) and <inline-formula><mml:math id="M36" display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">misc</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the miscellaneous cable losses (assumed to be 7 dB here) <xref ref-type="bibr" rid="bib1.bibx26" id="paren.31"/>. The estimated received power (dBm) as a function of distance for the two Utö antennae can be seen in Fig. <xref ref-type="fig" rid="F3"/>. The maximum AIS range, based on the receiver sensitivity, can be estimated to be 42–67 km for the 7 m antenna and 64–89 km for the 30 m antenna. The range increases with the height of the transmitting antenna.</p>
      <p id="d2e1152">Information about AIS antenna heights is not readily available and varies between ships as there are no IMO regulations for AIS antenna height or placement on the ship, although it is typically in the mast superstructure above the bridge. For the Baltic ferries this can be up to 50 m. Thus in Utö AIS data, a ship exceeding a certain distance suggested by the range formulas could be either a tall ferry or a small boat observed due to anomalous propagation conditions. AIS data from individual ships with known transceiver specifications could be used to validate the range formulas and study how they can be used to detect anomalous propagation and the associated atmospheric conditions. However, the objective of the present study is to use the AIS data en masse to identify propagation conditions and their seasonal and diurnal variations in the study area extending to nine Baltic basins. Hence, empirical  and statistical methods are experimented in order to establish over-the-horizon (OH) propagation criteria and to identify periods of OH observations. The selected basic descriptor for each antenna is the 95th percentile of  maximum distance, that is, the radius of a circular boundary such that for 95 % of the ships the maximum distance detected during a time period is within the boundary. The 95th percentile was chosen as it was more descriptive of OH observations than the median and less sensitive to individual ships than the 99th percentile. Furthermore, the AIS data was gridded into <inline-formula><mml:math id="M37" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="italic">°</mml:mi><mml:mo>×</mml:mo><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="italic">°</mml:mi></mml:mrow></mml:math></inline-formula> grid and hourly visibility was calculated for each grid and visualised as percentages. This allows for identifying the horizon based on the global AIS product. Hourly visibility is the percentage of hours during which at least one message was received from the grid, and therefore 100 % visibility is reached if at least one signal was received every hour during the 1-year period, August 2023–July 2024.</p>
</sec>
<sec id="Ch1.S2.SS5">
  <label>2.5</label><title>Modified refractivity and duct characteristics</title>
      <p id="d2e1180">In this study, profiles of the modified refractivity (<inline-formula><mml:math id="M38" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-profiles) were calculated based on measurements of air temperature and relative humidity at heights 4, 7, 12, 22, 32 and 59 m a.m.s.l. similarly to <xref ref-type="bibr" rid="bib1.bibx46 bib1.bibx47" id="text.32"/>. From the <inline-formula><mml:math id="M39" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-profiles, vertical gradients of <inline-formula><mml:math id="M40" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula> (<inline-formula><mml:math id="M41" display="inline"><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>M</mml:mi><mml:mo>/</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:math></inline-formula>) were calculated. The vertical layer in the <inline-formula><mml:math id="M42" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-profile where <inline-formula><mml:math id="M43" display="inline"><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>M</mml:mi><mml:mo>/</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula> is the trapping layer of the duct. The top height of the trapping layer is the duct height. Duct strength (intensity) (<inline-formula><mml:math id="M44" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>M</mml:mi></mml:mrow></mml:math></inline-formula>) is defined as the absolute change in <inline-formula><mml:math id="M45" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula> in M-Units (MU) in the trapping layer.</p>
</sec>
</sec>
<sec id="Ch1.S3">
  <label>3</label><title>Results</title>
<sec id="Ch1.S3.SS1">
  <label>3.1</label><title>Number of received messages</title>
      <p id="d2e1284">The AIS receivers record a large number of messages per day (Fig. <xref ref-type="fig" rid="F4"/>). On average, after preprocessing, the receiver at 7 m received 198 116 valid messages per day and the 30 m receiver 477 462 messages per day over the study period. The number of received and preprocessed messages are strongly correlated (<inline-formula><mml:math id="M46" display="inline"><mml:mrow><mml:mi>r</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.98</mml:mn></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M47" display="inline"><mml:mrow><mml:mi>p</mml:mi><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">0.05</mml:mn></mml:mrow></mml:math></inline-formula>). During the preprocess, on average 34 % of the daily received messages are discarded from the 7 m AIS antenna data and 29 % of the 30 m antenna data. The number of discarded messages increases during winter and peaks in early spring, where nearly 50 % is discarded during preprocess. This is due to the increase in virtual AtoNs over winter due to sea ice in the Baltic Sea (Fig. <xref ref-type="fig" rid="F4"/>).</p>

      <fig id="F4" specific-use="star"><label>Figure 4</label><caption><p id="d2e1317">Daily number received, received minus virtual aid messages and preprocessed messages for the <bold>(a)</bold> 7 m AIS antenna <bold>(b)</bold> 30 m AIS antenna.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f04.png"/>

        </fig>

      <p id="d2e1332">The number of messages is relatively stable from October 2023 to February 2024 and unstable from August to September 2023 and March to July 2024 (Fig. <xref ref-type="fig" rid="F4"/>). The number of valid received messages depends on multiple factors; characteristics of the receiving antenna (e.g. height and sensitivity), characteristics of the transmitting antenna (e.g. height and power), any filtering performed in post-processing, the amount of ships within reach, surrounding topography (shadowing) and atmospheric conditions. Majority of these aforementioned factors are stable and any variance in the number of messages is caused by the number of ships within reach, potential shadowing of antennae by other ships and atmospheric propagation conditions. The differences in the number of received messages between the two antennae are most likely due to the lower antenna having a lower range and it being more susceptible to shadowing.</p>
</sec>
<sec id="Ch1.S3.SS2">
  <label>3.2</label><title>Directional distribution of AIS messages</title>
      <p id="d2e1345">The directional distribution of Class A and Class B position reports, their RSSI and distance from Utö, in a circular plot (wind rose) divided into eight segments (cardinal and ordinal directions) for two months (September and October 2023) can be seen in Fig. <xref ref-type="fig" rid="F5"/>. The percentages correspond to the proportion of the messages that are received from each direction during a month long period. It appears that for October when the daily number of messages was mostly stable, most messages are received from east and northwest, within 0–50 km for the 7 m antenna and 0–100 km for the 30 m antenna. As expected, the share of messages received further away is greater for the 30 m antenna.</p>

      <fig id="F5" specific-use="star"><label>Figure 5</label><caption><p id="d2e1352">Directional distribution of AIS messages and the RSSI [dBi] (two left columns) and distance from Utö [km] (two right columns) of messages received by the two antennae (columns) for two months September and October 2023 (rows) presented as circular plots divided into eight segments. The percentages correspond to the proportion of the messages that are received from that direction during the month.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f05.png"/>

        </fig>

      <p id="d2e1361">Directly to the east is the guest port of Utö, where most of the strongest messages (RSSI <inline-formula><mml:math id="M48" display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mo>-</mml:mo><mml:mn mathvariant="normal">71</mml:mn></mml:mrow></mml:math></inline-formula>) are transmitted from. The guest port is especially strongly represented in the 7 m antenna data, as 30 % of the messages are received from within 1 km to the east in October. For September, when the daily number of messages was unstable with some peaks, the share of messages received from south, and from within the sea sector of the mast (roughly from northwest to southeast) is increased. This decreases the relative share of east in the charts. The share of weaker messages received further away also increases beyond 100 km. This indicates that while the number of messages is increased, some of the messages are also transmitted from further away. The roses for all months during the study period (August 2023–July 2024) can be seen in Figs. <xref ref-type="fig" rid="FA1"/> and <xref ref-type="fig" rid="FA2"/> (Appendix <xref ref-type="sec" rid="App1.Ch1.S1"/>).</p>
</sec>
<sec id="Ch1.S3.SS3">
  <label>3.3</label><title>Anomalies in the AIS range</title>
      <p id="d2e1390">In order to identify anomalies in the AIS range and study their occurrence, the hourly maximum distance of each vessel from Utö was calculated based on Class A and Class B position reports. Based on these maximum distances, daily 5th, 50th (median), and 95th percentiles of distance were then computed (Fig. <xref ref-type="fig" rid="F6"/>). The nearest 1 km from Utö is disproportionally represented in the data (up to 30 %) (Fig. <xref ref-type="fig" rid="F5"/>) and hence excluded before calculating the maximum distances.</p>

      <fig id="F6" specific-use="star"><label>Figure 6</label><caption><p id="d2e1399">Time series of the daily 5th, 50th and 95th percentiles of maximum distance, for the two antennae at the heights of <bold>(a)</bold> 7 m and <bold>(b)</bold> 30 m.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f06.png"/>

        </fig>

      <p id="d2e1414">The 95th percentile is more reactive to changes in the AIS range than the median. The time series suggest the presence of a horizon within which the messages are received under standard propagation conditions (within horizon, WH), and periods of anomalous conditions with over-the-horizon (OH) observations. However, the distance to the horizon cannot be expected to be sharply defined as it varies with the characteristics of the shipboard transmitters (e.g. height of the transmitting antenna).</p>
      <p id="d2e1418">Instead, the  horizon was studied in terms of a statistical distribution model for the 95th percentile of hourly maximum distance understood as a random variable exp(<inline-formula><mml:math id="M49" display="inline"><mml:mi>X</mml:mi></mml:math></inline-formula>). The data north of Utö was excluded to limit the effects of the archipelago which obstructs signal propagation and restrains the traffic to few fixed routes. This leaves the spatially more scattered traffic in the open sea for the analysis. The model is defined in terms of the logarithm <inline-formula><mml:math id="M50" display="inline"><mml:mi>X</mml:mi></mml:math></inline-formula> of the percentile distance. The histogram for <inline-formula><mml:math id="M51" display="inline"><mml:mi>X</mml:mi></mml:math></inline-formula> was bimodal for both antenna heights, indicating an overlapping superposition <inline-formula><mml:math id="M52" display="inline"><mml:mrow><mml:mi>X</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> resulting from  standard (<inline-formula><mml:math id="M53" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>) and anomalous (<inline-formula><mml:math id="M54" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>) propagation. The superposition was resolved by fitting to both components the generalised normal distribution (Subbotin distribution):

            <disp-formula id="Ch1.E4" content-type="numbered"><label>4</label><mml:math id="M55" display="block"><mml:mrow><mml:mi>f</mml:mi><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mi>K</mml:mi><mml:mi>exp⁡</mml:mi><mml:mfenced open="(" close=")"><mml:mrow><mml:mo>-</mml:mo><mml:mo>|</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi>x</mml:mi><mml:mo>-</mml:mo><mml:mi mathvariant="italic">μ</mml:mi></mml:mrow><mml:mrow><mml:msqrt><mml:mn mathvariant="normal">2</mml:mn></mml:msqrt><mml:mi mathvariant="italic">σ</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:msup><mml:mo>|</mml:mo><mml:mi>s</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:mo>,</mml:mo><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mi>K</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mi>s</mml:mi><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:msqrt><mml:mn mathvariant="normal">2</mml:mn></mml:msqrt><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi>s</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>

          The fitting was done in terms of half-distributions from zero to mode for <inline-formula><mml:math id="M56" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and from mode to infinity for <inline-formula><mml:math id="M57" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> as described in <xref ref-type="bibr" rid="bib1.bibx47" id="text.33"/> where a similar model was used to separate WH and OH components of X-band radar clutter. The result is shown in Fig. <xref ref-type="fig" rid="F7"/>. The component distributions for the 95th percentile distance, exp(<inline-formula><mml:math id="M58" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>) and exp(<inline-formula><mml:math id="M59" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>), are thus of generalised lognormal type <xref ref-type="bibr" rid="bib1.bibx40" id="paren.34"/>. The general argument for the applicability of this distribution family is that the decrease of signal power is expected to be a multiplicative result of several factors of different origin.</p>

      <fig id="F7" specific-use="star"><label>Figure 7</label><caption><p id="d2e1623">The normalized histograms of the 95th percentile distance logarithm for the <bold>(a)</bold> 7 m antenna and <bold>(b)</bold> 30 m antenna based on a year of data. The superposition model (<inline-formula><mml:math id="M60" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>) and horizon (vertical dashed line) are also shown.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f07.png"/>

        </fig>

      <p id="d2e1670">The superposition weight for <inline-formula><mml:math id="M61" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> is 0.49 and 0.68 for 7 and 30 m antenna respectively. The parameter <inline-formula><mml:math id="M62" display="inline"><mml:mi>s</mml:mi></mml:math></inline-formula> controls the shape of the Subbotin distribution and for (<inline-formula><mml:math id="M63" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>,<inline-formula><mml:math id="M64" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>) has values (1.19,1.68) for the 7 m antenna and (1.08,1.67) for the 30 m antenna. This indicates that especially for <inline-formula><mml:math id="M65" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> the statistical variation is a result of the same process for both antenna heights. The superposition is also apparent in other data types although the bimodality of the statistics is not as clear. For instance, the number of unique ships observed per hour combines the effects traffic density and propagation variations making the separation of standard and anomalous propagation more complicated. From the number of ships, exp(<inline-formula><mml:math id="M66" display="inline"><mml:mi>Y</mml:mi></mml:math></inline-formula>), the anomalous propagation component <inline-formula><mml:math id="M67" display="inline"><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> of ship number logarithm for 30 m antenna was separated using quantile-quantile (QQ) plotting for the pair <inline-formula><mml:math id="M68" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M69" display="inline"><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>. The QQ plot was linear for the quantiles corresponding to the half-distribution <inline-formula><mml:math id="M70" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> from mode to infinity. This indicates that the values of parameter <inline-formula><mml:math id="M71" display="inline"><mml:mi>s</mml:mi></mml:math></inline-formula> are close to each other and are assumed equal, 1.68. The remaining two parameters of <inline-formula><mml:math id="M72" display="inline"><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>  are obtained from a linear fit to the quantile plot. The results can be seen in Fig. <xref ref-type="fig" rid="F8"/>. For the separated standard propagation part <inline-formula><mml:math id="M73" display="inline"><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> the Subbotin fit was less perfect, indicating that the statistics is dominated by traffic density variations. For the 7 m antenna the superposition was barely discernible in the ship number statistics.</p>

      <fig id="F8" specific-use="star"><label>Figure 8</label><caption><p id="d2e1810">The normalized histogram of the number of observed ships per hour logarithm <inline-formula><mml:math id="M74" display="inline"><mml:mrow><mml:mi>Y</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> (green) for the 30 m antenna based on a year of data. The anomalous propagation model <inline-formula><mml:math id="M75" display="inline"><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> (blue) is shown with standard propagation residual histogram <inline-formula><mml:math id="M76" display="inline"><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> (orange).</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f08.png"/>

        </fig>

      <p id="d2e1863">To limit the over-forecasting of anomalous propagation, the statistical definition of the horizon in terms of the distribution model for <inline-formula><mml:math id="M77" display="inline"><mml:mi>X</mml:mi></mml:math></inline-formula> was chosen to be the 98th percentile of <inline-formula><mml:math id="M78" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>. For the hourly 95th percentile distance this is 82 km for the 7 m antenna and 94 km for the 30 m antenna (dashed line in Fig. <xref ref-type="fig" rid="F7"/>). This roughly corresponds to the estimations with a 60 m high transmitting antenna in Fig. <xref ref-type="fig" rid="F3"/>. It is worth noting that for the 7 m antenna, the 98 percent cumulation of <inline-formula><mml:math id="M79" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> results in a greater overlap of <inline-formula><mml:math id="M80" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M81" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> (Fig. <xref ref-type="fig" rid="F7"/>) which means that the chosen horizon will likely under-forecast anomalous propagation when compared to the 30 m antenna.</p>
</sec>
<sec id="Ch1.S3.SS4">
  <label>3.4</label><title>The occurrence of AIS OH observations</title>
      <p id="d2e1932">For the hourly 95th percentile maximum distance over the 1-year study period, the frequency of OH observations was 34 % and 59 % for the 7 and 30 m receiver, respectively, while the corresponding numbers for the data south of Utö were 33 % and 62 %. From the superposition weights of <inline-formula><mml:math id="M82" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>, the selected horizon detects south of Utö  67 % and 91 % of the anomalous propagation instances for the 7 and 30 m receivers, respectively. For the 30 m antenna hourly ship number exp(<inline-formula><mml:math id="M83" display="inline"><mml:mi>Y</mml:mi></mml:math></inline-formula>) the values exceeding 37, or the value corresponding to the mode of <inline-formula><mml:math id="M84" display="inline"><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>, are a clear indication of anomalous propagation in similar annual traffic conditions, detecting 50 % of the instances. This can be used as a simple indicator of anomalous conditions and occurs 23 % of the time.</p>

      <fig id="F9" specific-use="star"><label>Figure 9</label><caption><p id="d2e1966">Hourly occurrence [%] of OH observations by season for <bold>(a)</bold> 7 m antenna and <bold>(b)</bold> 30 m antenna. Solid line is based on all data, dashed line based on the data north of Utö (archipelago), and dotted line based on the data south of Utö (open sea). DJF <inline-formula><mml:math id="M85" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> December, January and February corresponding to winter, MAM <inline-formula><mml:math id="M86" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> March, April and May corresponding to spring, JJA <inline-formula><mml:math id="M87" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> June, July and August corresponding to summer and SON <inline-formula><mml:math id="M88" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> September, October and November corresponding to autumn.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f09.png"/>

        </fig>

      <p id="d2e2010">The seasonal hourly occurrence of OH observations based on the hourly 95th percentile distance is shown in Fig. <xref ref-type="fig" rid="F9"/>. The OH observations occur more frequently in spring and summer, where the hourly occurrence is up to 65 % for the 7 m antenna and up to 90 % for the 30 m antenna. During autumn and winter, the occurrence is lower, around 0 %–25 % for the 7 m antenna and 25 %–50 % for the 30 m antenna. A diurnal cycle where the OH observations occur more frequently in the evening and at night, and less frequently during the day, is also visible during summer. When the data is separated to the archipelago (north of Utö) and open sea (south of Utö), it is apparent that the diurnal occurrence of ducting is from the archipelago. In the archipelago sector, ducting occurrence increases 35 % from daytime to evening and night. Similar observations were made for the X-band coastal radar in Utö where the strong diurnal cycle was found to result from the archipelago sector where the marine boundary layer is influenced by the boundary layer over land <xref ref-type="bibr" rid="bib1.bibx47" id="paren.35"/>.</p>
</sec>
<sec id="Ch1.S3.SS5">
  <label>3.5</label><title>Received Signal Strength Indicator</title>
      <p id="d2e2027">The median RSSI over the study period is <inline-formula><mml:math id="M89" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">110</mml:mn></mml:mrow></mml:math></inline-formula> dBi for the 7 m antenna and <inline-formula><mml:math id="M90" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">109</mml:mn></mml:mrow></mml:math></inline-formula> dBi for the 30 m antenna (Table <xref ref-type="table" rid="T1"/>). The hourly median RSSI varies between <inline-formula><mml:math id="M91" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">120</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M92" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">60</mml:mn></mml:mrow></mml:math></inline-formula> dBi within-horizon, while over-the-horizon, it varies from <inline-formula><mml:math id="M93" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">120</mml:mn></mml:mrow></mml:math></inline-formula> to <inline-formula><mml:math id="M94" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">100</mml:mn></mml:mrow></mml:math></inline-formula> dBi. This is explained by the increased reception of weaker messages over-the-horizon. As such, RSSI alone is not a good indicator for AIS OH observations.</p>

<table-wrap id="T1"><label>Table 1</label><caption><p id="d2e2096">The 5th, 50th and 95th percentiles of RSSI [dBi] over the one year study period.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="4">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="center"/>
     <oasis:colspec colnum="3" colname="col3" align="center"/>
     <oasis:colspec colnum="4" colname="col4" align="center"/>
     <oasis:thead>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Antenna</oasis:entry>
         <oasis:entry colname="col2">5th</oasis:entry>
         <oasis:entry colname="col3">50th</oasis:entry>
         <oasis:entry colname="col4">95th</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1">7 m</oasis:entry>
         <oasis:entry colname="col2"><inline-formula><mml:math id="M95" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">116</mml:mn></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3"><inline-formula><mml:math id="M96" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">110</mml:mn></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col4"><inline-formula><mml:math id="M97" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">87</mml:mn></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">30 m</oasis:entry>
         <oasis:entry colname="col2"><inline-formula><mml:math id="M98" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">117</mml:mn></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3"><inline-formula><mml:math id="M99" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">109</mml:mn></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col4"><inline-formula><mml:math id="M100" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">85</mml:mn></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <p id="d2e2212">To examine the variability in received signal strength with respect to the distance from the antenna under standard and anomalous conditions, the RSSI over two months, September and October 2023, were plotted against distance, with the number of points illustrated in a 2-dimensional count histogram (Fig. <xref ref-type="fig" rid="F10"/>). October was chosen because it was identified as the month that had the least OH observations based on the 95th percentile time series (Fig. <xref ref-type="fig" rid="F6"/>) and a relatively stable number of daily messages (Fig. <xref ref-type="fig" rid="F4"/>), while September was identified to have frequent increased OH observations and variable number of daily messages. Only Class A and Class B position reports were included.</p>

      <fig id="F10" specific-use="star"><label>Figure 10</label><caption><p id="d2e2224">Hexagonal binned plot of RSSI [dBi] and the corresponding distance from Utö (km) for the two antennae: 7 m height (left column) and 30 m height (right column). Panels <bold>(a)</bold> and <bold>(b)</bold> show data for September 2023. Only message types 1–3 and 18–19 were included. Panels <bold>(c)</bold> and <bold>(d)</bold> show the same for October 2023. <inline-formula><mml:math id="M101" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> curve is fitted to represent the received power under standard conditions over a smooth terrain.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f10.png"/>

        </fig>

      <p id="d2e2256">Although October was identified to have the least anomalous signal propagation, it is clear that there are still periods of anomalous signal propagation, although not particularly strong (c and d panels in Fig. <xref ref-type="fig" rid="F10"/>). To further assess this, received power (<inline-formula><mml:math id="M102" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) curve (Eq. <xref ref-type="disp-formula" rid="Ch1.E3"/>) was fitted to the October data with time periods of anomalous 95th percentile excluded and the data limited to the open sea (see Appendix <xref ref-type="sec" rid="App1.Ch1.S3"/> for more details). The fitted <inline-formula><mml:math id="M103" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> curve shows the received signal strength indicator (dBi) with distance under standard conditions.</p>
      <p id="d2e2287">The <inline-formula><mml:math id="M104" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> curve fits well until the horizon (82 km for 7 m antenna and 94 km for 30 m antenna). When signal is received over-the-horizon, there is no straight-forward relationship between distance and signal strength. This is pronounced when comparing to September (a and b panels in Fig. <xref ref-type="fig" rid="F10"/>) when increased AIS range was frequently observed. It appears that over the horizon, the signal can travel to further distances without degradation, even up to hundreds of kilometers.</p>
</sec>
<sec id="Ch1.S3.SS6">
  <label>3.6</label><title>Comparison with the global AIS data</title>
      <p id="d2e2311">The AIS data from Utö antennae was compared with the ORBCOMM global AIS data to establish normal spatial coverage for the antennae. All data were limited to messages received from within the study area (see Fig. <xref ref-type="fig" rid="F1"/>) and to vessels with MID starting with numbers 2–7 (regional identifier for individual ships, e.g. first digit 2 stands for Europe). MID was used as the ORBCOMM dataset was very large and provided as separate files for each MMSI.</p>

      <fig id="F11" specific-use="star"><label>Figure 11</label><caption><p id="d2e2326"><inline-formula><mml:math id="M105" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="italic">°</mml:mi><mml:mo>×</mml:mo><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="italic">°</mml:mi></mml:mrow></mml:math></inline-formula> gridded monthly visibility [%] over two months September and October 2023 for 7 m antenna (first column from the left), 30 m antenna (second column), global AIS data (middle column) and the ratio between antenna visibility and global data visibility (two right columns). Visibility for a grid is 100 % if at least one AIS message is received from within the grid every hour of the month.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f11.png"/>

        </fig>

      <p id="d2e2350">The AIS data from the two antennae was gridded into <inline-formula><mml:math id="M106" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="italic">°</mml:mi><mml:mo>×</mml:mo><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="italic">°</mml:mi></mml:mrow></mml:math></inline-formula> grid and the hourly visibility of each grid for September and October 2023 was calculated (Fig. <xref ref-type="fig" rid="F11"/>). Visibility for a grid is 100 % if at least one AIS message is received from within the grid every hour of the month. The extent of visibility increases with height and both antennae achieve great visibility along the busy ship routes. The visibility in September is much greater than in October. To address if the regions of low visibility are due to there simply being no vessels to receive messages from, or if the regions are out of range for the AIS antennae, the ORBCOMM global AIS data was also gridded into the <inline-formula><mml:math id="M107" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="italic">°</mml:mi><mml:mo>×</mml:mo><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="italic">°</mml:mi></mml:mrow></mml:math></inline-formula> grid and the visibility of each grid was presented for the two months (middle column in Fig. <xref ref-type="fig" rid="F11"/>). The global AIS data was then used as the “background” to estimate the Utö antenna's coverage area, and the antenna visibility was divided by the global AIS visibility for each grid. The ratios are shown as percentages (right columns in Fig. <xref ref-type="fig" rid="F11"/>).</p>
      <p id="d2e2397">Using the ORBCOMM global AIS as background is beneficial as it shows areas that can be expected to have constant coverage with the Utö AIS antennae (100 % visibility) and regions where coverage is occasionally achieved due to anomalous propagation (<inline-formula><mml:math id="M108" display="inline"><mml:mrow><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">100</mml:mn><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="italic">%</mml:mi></mml:mrow></mml:math></inline-formula> visibility). However, near Utö visibility in some grids exceeded 100 %.  The global data has a varying sampling frequency, depending whether the data is collected from the AIS base stations or from satellites. In addition, the probability of a successful reception of a single sentence message is higher than that of a multi-part message. If <inline-formula><mml:math id="M109" display="inline"><mml:mi>P</mml:mi></mml:math></inline-formula> is the probability, then for multi-part message <inline-formula><mml:math id="M110" display="inline"><mml:mrow><mml:msup><mml:mi>P</mml:mi><mml:mi>n</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> applies, where <inline-formula><mml:math id="M111" display="inline"><mml:mi>P</mml:mi></mml:math></inline-formula> is the probability of receiving a single message and <inline-formula><mml:math id="M112" display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula> is the number of sentences in a multi-part message. For this reason, multi-part message reception probability is lower, especially in satellite reception of AIS data. As a result, vessels that appear in a grid cell for a short amount of time can occasionally be missing in the global dataset for that grid. This means that the visibility is likely biased higher and that the bias would likely increase if the grid size was decreased.</p>
      <p id="d2e2450">As October had the least amount of ducting, the grids with visibility <inline-formula><mml:math id="M113" display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mn mathvariant="normal">95</mml:mn><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="italic">%</mml:mi></mml:mrow></mml:math></inline-formula> for October was then used to mask out the grids within the horizons of the AIS antennae. Each hour of the data was gridded and the number of grids with at least one ship during that hour was calculated over the study area for each hour (panel a in Fig. <xref ref-type="fig" rid="F12"/> and Appendix <xref ref-type="sec" rid="App1.Ch1.S4"/> Fig. <xref ref-type="fig" rid="FD1"/>).</p>

      <fig id="F12" specific-use="star"><label>Figure 12</label><caption><p id="d2e2474">Based on the 30 m antenna data: <bold>(a)</bold> hourly time series of the number of grids with at least one ship outside of the horizon, <bold>(b)</bold> hourly 95th percentile of distance and <bold>(c)</bold> relationship between the two when 95th percentile is over-the-horizon.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f12.png"/>

        </fig>

      <p id="d2e2492">The time series of number of grids over the horizon and 95th percentile of distance were compared. The correlation was high for both antenna heights, <inline-formula><mml:math id="M114" display="inline"><mml:mrow><mml:mi>r</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.8</mml:mn></mml:mrow></mml:math></inline-formula> for 30 m antenna and <inline-formula><mml:math id="M115" display="inline"><mml:mrow><mml:mi>r</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.74</mml:mn></mml:mrow></mml:math></inline-formula> for 7 m antenna (panel c in Fig. <xref ref-type="fig" rid="F12"/> and Appendix <xref ref-type="sec" rid="App1.Ch1.S4"/> Fig. <xref ref-type="fig" rid="FD1"/>). The 95th percentile of distances is more sensitive to the number of ships in the study area and their respective locations, e.g. a small number of ships during an hour could cause a spike in the hourly 95th percentile of distance, indicating a duct in a specific area.</p>
</sec>
<sec id="Ch1.S3.SS7">
  <label>3.7</label><title>Can the vertical profiles of modified refractivity predict AIS OH observations?</title>
      <p id="d2e2533">In this study we have shown AIS OH observations. However, it has not yet been demonstrated in this study, that the OH observations result from ducting. Hence, the 95th percentile distance for the two antennae were compared to observed vertical modified refractivity gradients (<inline-formula><mml:math id="M116" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-gradients) calculated from the temperature and humidity profiles at Utö and to duct strengths calculated from the <inline-formula><mml:math id="M117" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-gradients (Fig. <xref ref-type="fig" rid="F13"/>). It is important to note that the maximum measurement height of 59 m a.m.s.l. limits the detection of elevated ducts. In addition, the mast is representative of local conditions, while ducts that could influence the signal propagation can exist within the horizon of the antennae, undetected by the mast measurements.</p>

      <fig id="F13" specific-use="star"><label>Figure 13</label><caption><p id="d2e2554"><bold>(a)</bold> Time series of the hourly 95th percentile distance, i.e. the distances outside of which 5 % of the received messages originate, for the antenna at the height of 7 m, <bold>(b)</bold> same as <bold>(a)</bold> but for the 30 m antenna, <bold>(c)</bold> vertical modified refractivity gradient over time, for heights 4–7, 7–12, 12–22, 22–32 and 32–59 m and <bold>(d)</bold> duct heights (height of a bar), trapping layer thickness (vertical range of the bar) and duct strengths (colour) calculated from the vertical modified refractivity gradients.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f13.png"/>

        </fig>

      <p id="d2e2577">The time series show that when the 95th percentile distance was at its greatest during summer and autumn, a strong duct was also observed in the vertical <inline-formula><mml:math id="M118" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-profiles (Fig. <xref ref-type="fig" rid="F13"/>). However, it appears that the 95th percentile distance indicated OH observations more often, particularly over winter and spring, than a duct was observed in the vertical <inline-formula><mml:math id="M119" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-profiles.</p>
      <p id="d2e2597">To examine this more closely, the 95th percentile of distance was binned into 10 km interval bins and plotted against how often a duct was observed for each bin (Fig. <xref ref-type="fig" rid="F14"/>). It appears when 95th percentile is at the horizon (70–80 km for the 7 m antenna and 90–100 km for the 30 m antenna), a shallow duct (7–12 m) occurs 20 % of the time. When looking at the bins beyond the standard, the share of shallow ducts is smaller and the share of higher ducts (32–59 m) increases, and overall a duct occurs 20 %–40 % of the time. In addition, when the 95th percentile of distance is very low for the 7 m antenna, around 1–10 km, a shallow duct occurs 50 % of the time. Note that the 95th percentile can sometimes fall significantly below the defined statistical horizon for the 7 m antenna, which could result from e.g. the signal being physically blocked by the terrain.</p>

      <fig id="F14" specific-use="star"><label>Figure 14</label><caption><p id="d2e2604">The occurrence of duct [%] when 95th percentile distance for <bold>(a)</bold> 7 m antenna and <bold>(b)</bold> 30 m antenna are observed at certain intervals. Colors indicate the portions of duct heights.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f14.png"/>

        </fig>

      <fig id="F15" specific-use="star"><label>Figure 15</label><caption><p id="d2e2621">The occurrence of AIS OH observations [%] when duct height is at a certain height for <bold>(a)</bold> 7 m antenna and <bold>(b)</bold> 30 m antenna. Colors indicate the portions of duct strengths.</p></caption>
          <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f15.png"/>

        </fig>

      <p id="d2e2636">Particularly, the highest 95th percentile distances seem to co-occur with the stronger and higher observed ducts. To examine this more closely, the occurrence of AIS OH observations were studied against the duct height and duct strength (Fig. <xref ref-type="fig" rid="F15"/>). When the duct height is observed at 59 m, the 95th percentile of distance is increased 90 % of the time for the 7 m antenna and 95 % of the time for the 30 m antenna while the share of stronger ducts also increases with the height of the duct. It appears that when the observed duct height is 32 or 59 m, AIS OH observations can be expected. Furthermore, the 7 m antenna observes less ducts than the 30 m antenna at all heights. However, the greatest difference occurs when the duct height is small. There are more obstacles to the 7 m antenna which can cause there to be less OH observations for the 7 m antenna when the duct height is low.</p>
      <p id="d2e2641">Although the occurrence of a duct with the height of 32 or 59 m seems to be a good indicator for AIS OH observations, the OH observations still often occur without an observed duct in the vertical <inline-formula><mml:math id="M120" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-profile. In other words, the measured <inline-formula><mml:math id="M121" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-profile under-predicts AIS OH observations. This is likely because the highest measurement height of 59 m might not be high enough for this purpose, and ducts affecting the AIS signal could have occurred above the highest measurement height. Furthermore, ducts within the AIS horizon, not captured by the measurement mast, could influence the AIS signal propagation.</p>
</sec>
</sec>
<sec id="Ch1.S4">
  <label>4</label><title>Discussion</title>
      <p id="d2e2667">In this study, an experimental AIS set-up for atmospheric ducting research and monitoring was introduced and approaches for identifying ducting from the AIS data were explored. The approaches ranged from “quick and easy” to more complicated approaches. First, an approach where simply the hourly number of messages were counted was tested, assuming that ducting would increase the area of reception and therefore the number of messages received. This approach allows to identify peaks in the data without even decoding the received messages. However, the baseline is not stable over time as the number of ships in the Baltic Sea also has diurnal and seasonal cycles, and on longer timescales are affected by the state of economy, e.g. recession <xref ref-type="bibr" rid="bib1.bibx37" id="paren.36"><named-content content-type="pre">see e.g.</named-content></xref>. Furthermore, the distribution analysis showed that the distributions are superimposed for the number of messages and the number of ships and therefore further analysis (e.g. calculating occurrence) based on the number of messages or ships would be complicated and the rate of over- or under-prediction, depending on the chosen threshold, would likely be high.</p>
      <p id="d2e2675">Secondly, a statistical approach (mean, median and percentiles) based on distance from transmitters to the receiver was tested. The 95th percentile of distance is sensitive to the number of messages and hence the data had to be resampled before analysis. Using the 95th percentile of distance allows for numerically defining the horizon as the WH and OH distributions could be identified and separated. This approach benefits from being comparable to the horizon of the receiver but is not applicable to all directions, particularly to the archipelago sector. In addition, knowledge of the shipping routes within the study area is crucial when interpreting the results, as the 95th percentile of distance will be sensitive to shipping routes, particularly if the route is curved, causing the distance to receiver remaining the same while the vessel is moving.</p>
      <p id="d2e2678">Lastly, using a global AIS product as a background truth to establish the horizon was tested. Although this approach takes into account the environment and provides a better result spatially, it is likely that the global data is also influenced by the anomalous propagation conditions, especially when data is collected from the base stations. Further issues might arise from the sampling frequency. Improving the background truth by including SAR-data <xref ref-type="bibr" rid="bib1.bibx34" id="paren.37"><named-content content-type="pre">see e.g.</named-content></xref> and fine-tuning grid size, could improve this analysis.</p>
      <p id="d2e2686">The experimental AIS set-up could provide a cost-effective way to describe ducting conditions over sea areas. While the vertical profiles of refractivity can provide a good estimate of overall ducting conditions, they are not descriptive beyond the local environment, as shown in <xref ref-type="bibr" rid="bib1.bibx46" id="text.38"/> where the refractivity profile was found to be descriptive of ducting conditions with the X-band radar over open sea but not in the archipelago. Similarly, in this study the vertical <inline-formula><mml:math id="M122" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-profiles were found to underestimate the OH AIS observations.</p>
      <p id="d2e2700">Recently AIS has been studied as a signal source for atmospheric duct parameter inversions <xref ref-type="bibr" rid="bib1.bibx16 bib1.bibx23" id="paren.39"><named-content content-type="pre">e.g.,</named-content></xref>. These atmospheric duct parameters often include duct height, strength, thickness, and slope. The relationship between AIS signal power and atmospheric duct parameters is complicated and non-linear, thus intelligent optimization algorithms where the atmospheric duct profiles are matched with monitoring data have been utilized <xref ref-type="bibr" rid="bib1.bibx23" id="paren.40"/>. As these methods keep improving, the potential of AIS for duct monitoring and model validation cost-effectively increases.</p>
      <p id="d2e2711">Particularly, if the methodology is expanded from experimental set-ups to the operative AIS network, it could, in theory, be used to create a network that describes the signal propagation circumstances for the VHF channel over marine areas in real-time. Based on this network, forecasts of ducting and other signal propagation anomalies could be created. As such, it would be of great value to assess the duct characteristics that influence AIS signal, alongside other frequencies, to assess if the AIS system based forecast could also be applied to other systems, e.g. surveillance and navigational radars, and radio communications.</p>
      <p id="d2e2714">Comparing the results of this study with previous studies suggests that OH observations occur more frequently for AIS, 34 % and 59 % of the time, while for an X-band surveillance radar OH observations occurred 19 % of the time <xref ref-type="bibr" rid="bib1.bibx47" id="paren.41"/> and C-band weather radars' ground clutter in the Baltic Sea region occurred <inline-formula><mml:math id="M123" display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 10 %–25 % of the time <xref ref-type="bibr" rid="bib1.bibx41" id="paren.42"/>. The X- and C-band are more affected by the surface ducts (<inline-formula><mml:math id="M124" display="inline"><mml:mo lspace="0mm">∼</mml:mo></mml:math></inline-formula> 10s of meters), while the VHF-band is affected by the elevated ducts (<inline-formula><mml:math id="M125" display="inline"><mml:mo lspace="0mm">∼</mml:mo></mml:math></inline-formula> 100s of meters). Unfortunately, the set-up at Utö is limited to the height of 59 m which omits the assessment of elevated ducts. For future analyses, including weather soundings or drone measurements to account for the heights above 60 m is needed. In addition, in future studies, examining favourable weather conditions (e.g. temperature and humidity profiles and high-pressure systems) to AIS ducting would deepen our understanding of the phenomenon.</p>
      <p id="d2e2744">Similarly to findings by <xref ref-type="bibr" rid="bib1.bibx41" id="text.43"/> and <xref ref-type="bibr" rid="bib1.bibx47" id="text.44"/>, the AIS OH observations have diurnal and seasonal cycles. The diurnal cycle is found to result from the archipelago sector where the occurrence increases 35 % from daytime to evening and night. This reflects the radiative cooling over land that creates a stable stratification over land at night, allowing for the ducts to form more readily at night. The sea surface temperature is more stable overnight and prevents the development of a similar diurnal cycle.</p>
</sec>
<sec id="Ch1.S5" sec-type="conclusions">
  <label>5</label><title>Conclusions</title>
      <p id="d2e2762">In this study, an experimental AIS set-up for atmospheric ducting research and monitoring was introduced. The set up includes two antennae set at different heights (7 and 30 m) co-located with measurements of air temperature and humidity. This allows for assessing if the near-surface atmospheric stratification affects signal propagation at the AIS frequency.</p>
      <p id="d2e2765">A statistical approach, 95th percentile distance, was found to be a good indicator for over-the-horizon (OH) observations with the AIS antennae. The hourly occurrence of OH observations with the antennae was found to be 59 % for the 30 m antenna and 34 % for the 7 m antenna. The occurrence was more frequent during the spring and summer months. A diurnal cycle where ducting occurred more frequently during evening and night was found in the Archipelago Sea area (north of Utö) while over the open sea area (south of Utö) ducting was not dependent on the time of the day.</p>
      <p id="d2e2768">Furthermore, when OH observations occurred, the received signal strength showed less degradation with distance and messages were received from further distances, up to 600 km away. The OH observations were also found to co-occur with the stronger and higher observed ducts. However, the occurrence of locally observed ducts underestimated the AIS OH observations.</p>
</sec>

      
      </body>
    <back><app-group>

<app id="App1.Ch1.S1">
  <label>Appendix A</label><title/>
      <p id="d2e2782">The monthly RSSI and distance of received AIS message types 1–3 (Class A position reports) and 18–19 (Class B position reports) for each compass direction over the study period August 2023–July 2024.</p>

      <fig id="FA1"><label>Figure A1</label><caption><p id="d2e2787">Directional presentation of RSSI (three left columns) and distance (three right columns) from Utö (km) of messages received by the 30 m antenna for 12 months.</p></caption>
        
        <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f16.png"/>

      </fig>

<fig id="FA2"><label>Figure A2</label><caption><p id="d2e2802">Directional presentation of RSSI (three left columns) and distance (three right columns) from Utö (km) of messages received by the 7 m antenna for 12 months.</p></caption>
        
        <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f17.png"/>

      </fig>


</app>

<app id="App1.Ch1.S2">
  <label>Appendix B</label><title/>
      <p id="d2e2822">For the message number logarithm, the probability distributions are skewed to the right and especially the 30 m case has an atypical tail (Fig. <xref ref-type="fig" rid="FB1"/>). Comparison with Fig. <xref ref-type="fig" rid="F7"/> for 95th percentile distances together with the associated analysis, strongly suggests that the distribution shape is a result of a superposition of two symmetric distributions for normal and anomalous conditions, respectively. Unlike for the percentile distance, for which the modes of both component distributions are discernible, the separation of the superposition is not attempted. However, for example the 30 m received message number logarithm clearly indicates anomalous conditions if the value exceeds mode by 0.3 or so. As the message numbers are easily obtained, this can serve as a threshold for commencing other activities during operative monitoring and atmospheric campaigns.</p>

      <fig id="FB1"><label>Figure B1</label><caption><p id="d2e2831">The distributions of number of messages logarithm <bold>(a)</bold> before preprocessing for the 7 m antenna, <bold>(b)</bold> before preprocessing for the 30 m antenna, <bold>(c)</bold> after preprocessing for the 7 m antenna and <bold>(d)</bold> after preprocessing for the 30 m antenna.</p></caption>
        
        <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f18.png"/>

      </fig>


</app>

<app id="App1.Ch1.S3">
  <label>Appendix C</label><title/>
      <p id="d2e2863">In order to establish the received power (<inline-formula><mml:math id="M126" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) with distance for the two AIS antennae, the received power (<inline-formula><mml:math id="M127" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) curve was fitted to the October AIS data. To exclude anomalous signal propagation, time periods where the 95th percentile of distance exceeded 94 km for 30 m antenna data and 82 km for 7 m antenna were excluded. In addition, to limit the influence of the archipelago, the data was limited to the open sea region, south of Utö (Fig. <xref ref-type="fig" rid="FC1"/>a). As received power is the absolute power in dBm while RSSI is the gain in dBi, a fitting parameter <inline-formula><mml:math id="M128" display="inline"><mml:mi>C</mml:mi></mml:math></inline-formula> was added to Eq. (<xref ref-type="disp-formula" rid="Ch1.E3"/>):

          <disp-formula id="App1.Ch1.S3.E5" content-type="numbered"><label>C1</label><mml:math id="M129" display="block"><mml:mtable class="split" rowspacing="0.2ex" displaystyle="true" columnalign="right left"><mml:mtr><mml:mtd><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub></mml:mrow></mml:mtd><mml:mtd><mml:mrow><mml:mo>=</mml:mo><mml:mi mathvariant="normal">EIRP</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">diff</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>G</mml:mi><mml:mi mathvariant="normal">Corr</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">misc</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:mi>C</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mo>-</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">diff</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msup><mml:mi>C</mml:mi><mml:mo>′</mml:mo></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>

        where all the constant terms in the equation have been combined to <inline-formula><mml:math id="M130" display="inline"><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>′</mml:mo></mml:msup><mml:mo>=</mml:mo><mml:mi mathvariant="normal">EIRP</mml:mi><mml:mo>+</mml:mo><mml:msub><mml:mi>G</mml:mi><mml:mi mathvariant="normal">R</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>G</mml:mi><mml:mi mathvariant="normal">Corr</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">misc</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:mi>C</mml:mi></mml:mrow></mml:math></inline-formula>. The fitted curves can be seen in Fig. <xref ref-type="fig" rid="FC1"/>.</p>

      <fig id="FC1"><label>Figure C1</label><caption><p id="d2e3026"><bold>(a)</bold> The rectangle shows the area that was used for the curve fitting, <bold>(b)</bold> fitted received power (<inline-formula><mml:math id="M131" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">Rec</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) curve for the 30 m and <bold>(c)</bold> 7 m antenna data.</p></caption>
        
        <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f19.png"/>

      </fig>


</app>

<app id="App1.Ch1.S4">
  <label>Appendix D</label><title/>

      <fig id="FD1"><label>Figure D1</label><caption><p id="d2e3067">Based on the 7 m antenna data: <bold>(a)</bold> hourly time series of the number of grids with at least one ship outside of the horizon, <bold>(b)</bold> hourly 95th percentile of distance and <bold>(c)</bold> relationship between the two when 95th percentile is over-the-horizon.</p></caption>
        
        <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f20.png"/>

      </fig>

</app>

<app id="App1.Ch1.S5">
  <label>Appendix E</label><title/>
      <p id="d2e3094">The ERA5 reanalysis dataset <xref ref-type="bibr" rid="bib1.bibx18" id="paren.45"/>, produced by the European Centre for Medium-Range Weather Forecasts (ECMWF), was used to characterize atmospheric ducting conditions at Utö. ERA5 is the fifth-generation global reanalysis from ECMWF and provides a physically consistent reconstruction of the atmospheric state from 1940 onward. Unlike operational forecasting systems, reanalysis products are not used for real-time prediction. Instead, they combine a numerical weather model with a wide range of historical in situ and remotely sensed observations through data assimilation. This allows delayed and reprocessed observations to be included, resulting in a dynamically more coherent representation of the atmospheric state.</p>
      <p id="d2e3100">ERA5 provides hourly data for a large number of atmospheric, land-surface, and ocean-wave variables at a horizontal resolution of 0.25<inline-formula><mml:math id="M132" display="inline"><mml:mi mathvariant="italic">°</mml:mi></mml:math></inline-formula>. The atmospheric model uses 137 vertical levels extending from the surface to the lower stratosphere. The vertical resolution is highest near the surface and gradually decreases with height, which limits the ability to resolve thin ducting layers, particularly at higher altitudes.</p>
      <p id="d2e3110">In this study, ERA5 data were processed on the model's native terrain-following hybrid sigma-pressure coordinate system to preserve the maximum available vertical resolution. The extracted variables include temperature and specific humidity on each model level, as well as pressure and geopotential height at the surface level. These variables were used to calculate radio refractivity (<inline-formula><mml:math id="M133" display="inline"><mml:mi>N</mml:mi></mml:math></inline-formula>) and modified refractivity (<inline-formula><mml:math id="M134" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>) in a 3D field for the selected area. From this data, atmospheric ducting was identified using the vertical gradient of modified refractivity between adjacent model levels (<inline-formula><mml:math id="M135" display="inline"><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>M</mml:mi><mml:mo>/</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>z</mml:mi></mml:mrow></mml:math></inline-formula>). A threshold value of <inline-formula><mml:math id="M136" display="inline"><mml:mo>&lt;</mml:mo></mml:math></inline-formula> 0 <inline-formula><mml:math id="M137" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>-units m<sup>−1</sup> was applied to indicate ducting conditions, enabling the detection of ducting layers and the estimation of their height and strength. Given the hourly temporal resolution of ERA5, each identi-fied ducting event represents atmospheric conditions for a one-hour period.</p>
      <p id="d2e3174">Figure <xref ref-type="fig" rid="FE1"/> presents (a) the vertical gradient of modified refractivity between adjacent model levels and (b) the corresponding duct strength, thickness, and height from August 2023 to July 2024 at the Utö site. Ducting conditions, indicated by negative modified refractivity gradients, occur mainly during the summer period and are confined to the lowest model levels.</p>
      <p id="d2e3180">A comparison with Fig. <xref ref-type="fig" rid="F13"/>, which shows measured ducting conditions at five height intervals between 4 and 59 m, indicates that ERA5 reproduces similar temporal patterns between approximately 12 and 59 m as observed on the mast. However, since the lowest ERA5 model level is located at about 10 m, ducts observed between 4–7 and 7–12 m are not represented. In addition, duct strengths derived from ERA5 are consistently weaker than those observed, which is likely related to limitations in both vertical and horizontal resolution that smooth and weaken small-scale ducting features. As a result, the weakest observed ducts are not captured in ERA5, while stronger ducts are present but with reduced intensity.</p>
      <p id="d2e3185">The horizontal resolution of ERA5 is approximately 27 km in the study area, meaning that each ERA5 grid cell represents atmospheric conditions averaged over a much larger area than the point measurements shown in Fig. <xref ref-type="fig" rid="F13"/>. This spatial averaging can reduce variability and further weaken ducting signals in the reanalysis. Nevertheless, the overall similarity between ducting patterns in ERA5 and the observations suggests that the Utö measurements provide a reasonable representation of ducting conditions also over a broader area of the outer Finnish archipelago.</p>

      <fig id="FE1"><label>Figure E1</label><caption><p id="d2e3192">Time series of <bold>(a)</bold> the vertical modified refractivity gradient [<inline-formula><mml:math id="M139" display="inline"><mml:mi>M</mml:mi></mml:math></inline-formula>/m] between adjacent model levels and <bold>(b)</bold> the corresponding duct strength, thickness, and height calculated for the ERA5 nearest grid to Utö. The heights of the model levels (shown as grey dashed lines) vary over time because they depend on the atmospheric conditions.</p></caption>
        
        <graphic xlink:href="https://amt.copernicus.org/articles/19/2763/2026/amt-19-2763-2026-f21.png"/>

      </fig>


</app>
  </app-group><notes notes-type="dataavailability"><title>Data availability</title>

      <p id="d2e3222">Due to the proprietary nature of the data, the collected raw data set cannot be provided on open access bases. The data used in the intermediate level analyses available upon request from the corresponding author. The ERA5 reanalysis data are freely available from the Copernicus Climate Data Store portal <xref ref-type="bibr" rid="bib1.bibx18" id="paren.46"/>.</p>
  </notes><notes notes-type="authorcontribution"><title>Author contributions</title>

      <p id="d2e3231">All authors contributed to the study through discussions. LL and KS planned and designed the experimental AIS set-up. KS and HL are responsible for the measurement installations and maintenance. MJ decoded and preprocessed the AIS data and provided the description of the set-up and the diagram showing the set-up. ML performed the fitting of the statistical distribution model to the probability density distributions, provided the distribution figures and wrote the descriptions. JJ provided the global AIS dataset. LR performed majority of the data analysis, produced majority of the visualisations and wrote majority of the manuscript with guidance and feedback from ML, JT, MJ, JJ and LL. All authors provided feedback on the manuscript. MH joined during the revision phase and provided the ERA5 analysis and comparison included in the Appendix <xref ref-type="sec" rid="App1.Ch1.S5"/>.</p>
  </notes><notes notes-type="competinginterests"><title>Competing interests</title>

      <p id="d2e3239">The contact author has declared that none of the authors has any competing interests.</p>
  </notes><notes notes-type="disclaimer"><title>Disclaimer</title>

      <p id="d2e3245">Publisher's note: Copernicus Publications remains neutral with regard to jurisdictional claims made in the text, published maps, institutional affiliations, or any other geographical representation in this paper. The authors bear the ultimate responsibil-ity for providing appropriate place names. Views expressed in the text are those of the authors and do not necessarily reflect the views of the publisher.</p>
  </notes><ack><title>Acknowledgements</title><p id="d2e3255">The following projects provided additional  technical, experimental or personnel support: International Cooperative Engagement Program For Polar Research (ICE-PPR), European Union: FESPAN project (project number 101167641); H2020 project JERICOS3 (grant agreement No. 871153). Views and opinions pressed are those of the author(s) and do not necessarily reflect those of the European Union or the European Commission. Neither the European Union nor the granting authority can be held responsible for them. The Research Council  of Finland: Finnish Marine Research Infrastructure (FINMARI); Integrated Carbon Observing System (ICOS); 335943 ANTGRAD; Marine waterways as a sustainable source of well-being, security, and safety (Decision number: 365647). The scientific color maps “batlow”, “turku”, “bamako” and “vik” by <xref ref-type="bibr" rid="bib1.bibx10" id="text.47"/> were chosen to avoid exclusion of readers with colour-vision deficiencies <xref ref-type="bibr" rid="bib1.bibx11" id="paren.48"/>.</p></ack><notes notes-type="financialsupport"><title>Financial support</title>

      <p id="d2e3266">This research has been supported by the Research Council of Finland project “Enabling forecasts on radar performance in marine environment” (grant no. 338150).</p>
  </notes><notes notes-type="reviewstatement"><title>Review statement</title>

      <p id="d2e3272">This paper was edited by Jorge Luis Chau and reviewed by three anonymous referees.</p>
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