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    <ResourceHeader>
      <ResourceName>Geotail Spacecraft Definitive Positions</ResourceName>
      <ReleaseDate>2021-04-27T17:52:35Z</ReleaseDate>
      <Description>Definitive Geotail spacecraft positions in various coordinate systems</Description>
      <Contact>
        <PersonID>spase://SMWG/Person/Gerald.Blackwell</PersonID>
        <Role>DataProducer</Role>
      </Contact>
      <Contact>
        <PersonID>spase://SMWG/Person/Jan.Merka</PersonID>
        <Role>MetadataContact</Role>
      </Contact>
      <PriorID>spase://VMO/NumericalData/Geotail/Ephemeris/PT10M</PriorID>
      <PriorID>spase://VSPO/NumericalData/Geotail/Ephemeris/PT10M</PriorID>
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      <RepositoryID>spase://SMWG/Repository/NASA/GSFC/SPDF/CDAWeb</RepositoryID>
      <Availability>Online</Availability>
      <AccessRights>Open</AccessRights>
      <AccessURL>
        <Name>FTPS from SPDF (not with most browsers)</Name>
        <URL>ftps://spdf.gsfc.nasa.gov/pub/data/geotail/orbit/def_or/</URL>
        <Description>NASA/GSFC CDAWeb ftp access to the data.</Description>
      </AccessURL>
      <AccessURL>
        <Name>HTTPS from SPDF</Name>
        <URL>https://spdf.gsfc.nasa.gov/pub/data/geotail/orbit/def_or/</URL>
        <Description>In CDF via HTTP from SPDF</Description>
      </AccessURL>
      <AccessURL>
        <Name>CDAWeb</Name>
        <URL>https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=GE_OR_DEF&amp;index=sp_phys</URL>
        <ProductKey>GE_OR_DEF</ProductKey>
      </AccessURL>
      <AccessURL>
        <Name>SSCWeb</Name>
        <URL>https://sscweb.gsfc.nasa.gov/cgi-bin/Locator.cgi</URL>
        <ProductKey>geotail</ProductKey>
      </AccessURL>
      <Format>CDF</Format>
      <Encoding>None</Encoding>
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      <Availability>Online</Availability>
      <AccessRights>Open</AccessRights>
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        <Style>HAPI</Style>
        <ProductKey>GE_OR_DEF</ProductKey>
        <Description>Web Service to this product using the HAPI interface.</Description>
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      <Format>CSV</Format>
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    <InstrumentID>spase://SMWG/Instrument/Geotail/Ephemeris</InstrumentID>
    <MeasurementType>Ephemeris</MeasurementType>
    <TemporalDescription>
      <TimeSpan>
        <StartDate>1992-07-27T16:00:00</StartDate>
        <RelativeStopDate>-P7D</RelativeStopDate>
      </TimeSpan>
      <Cadence>PT10M</Cadence>
    </TemporalDescription>
    <Parameter>
      <Name>Orbit Epoch Time</Name>
      <ParameterKey>Epoch</ParameterKey>
      <Description>Number of milliseconds since the CDF epoch</Description>
      <Units>ms</Units>
      <UnitsConversion>1e-3&gt;s</UnitsConversion>
      <ValidMin>01-Jul-1992 00:00:00.000</ValidMin>
      <ValidMax>31-Dec-2020 23:59:59.000</ValidMax>
      <FillValue>-1.0E31</FillValue>
      <Support>
        <SupportQuantity>Temporal</SupportQuantity>
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    </Parameter>
    <Parameter>
      <Name>Orbit PB5 Time</Name>
      <ParameterKey>Time_PB5</ParameterKey>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>Year</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>1</Index>
          <Units>year</Units>
          <ValidMin>1992</ValidMin>
          <ValidMax>2020</ValidMax>
          <FillValue>-2147483648</FillValue>
        </Element>
        <Element>
          <Name>Day of Year (Jan 1 = day 1)</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>2</Index>
          <Units>day</Units>
          <ValidMin>1</ValidMin>
          <ValidMax>366</ValidMax>
          <FillValue>-2147483648</FillValue>
        </Element>
        <Element>
          <Name>Elapsed ms of day</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>3</Index>
          <Units>ms</Units>
          <UnitsConversion>1e-3&gt;s</UnitsConversion>
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          <ValidMax>86399000</ValidMax>
          <FillValue>-2147483648</FillValue>
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      <Support>
        <SupportQuantity>Temporal</SupportQuantity>
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    </Parameter>
    <Parameter>
      <Name>GCI Cartesian Position</Name>
      <ParameterKey>GCI_POS</ParameterKey>
      <Description>Spacecraft position vector in GCI coordinates</Description>
      <Units>km</Units>
      <UnitsConversion>1e3&gt;m</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GEI</CoordinateSystemName>
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          <Name>X GCI</Name>
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          <ValidMax>1800000.0</ValidMax>
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          <Index>2</Index>
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          <ValidMax>1800000.0</ValidMax>
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        <Element>
          <Name>Z GCI</Name>
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          <ValidMax>1800000.0</ValidMax>
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        </Element>
      </Structure>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>GCI Cartesian Velocity</Name>
      <ParameterKey>GCI_VEL</ParameterKey>
      <Description>Spacecraft orbital velocity vector in GCI coordinates</Description>
      <Units>km/s</Units>
      <UnitsConversion>1e3&gt;m/s</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GEI</CoordinateSystemName>
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      <Structure>
        <Size>3</Size>
        <Element>
          <Name>vx GCI</Name>
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      </Structure>
      <Support>
        <SupportQuantity>Velocity</SupportQuantity>
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    </Parameter>
    <Parameter>
      <Name>GSE Cartesian Position</Name>
      <ParameterKey>GSE_POS</ParameterKey>
      <Description>Spacecraft position vector in GSE coordinates</Description>
      <Units>km</Units>
      <UnitsConversion>1e3&gt;m</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
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          <FillValue>-1.0E31</FillValue>
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      </Structure>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>GSE Cartesian Velocity</Name>
      <ParameterKey>GSE_VEL</ParameterKey>
      <Description>Spacecraft orbital velocity vector in GSE coordinates</Description>
      <Units>km/s</Units>
      <UnitsConversion>1e3&gt;m/s</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GSE</CoordinateSystemName>
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          <Name>vz GSE</Name>
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      </Structure>
      <Support>
        <SupportQuantity>Velocity</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>GSM Cartesian Position</Name>
      <ParameterKey>GSM_POS</ParameterKey>
      <Description>Spacecraft position vector in GSM coordinates</Description>
      <Units>km</Units>
      <UnitsConversion>1e3&gt;m</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GSM</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
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          <Name>X GSM</Name>
          <Qualifier>Component.I</Qualifier>
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          <ValidMax>1800000.0</ValidMax>
          <FillValue>-1.0E31</FillValue>
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          <Name>Y GSM</Name>
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          <ValidMax>1800000.0</ValidMax>
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          <FillValue>-1.0E31</FillValue>
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    </Parameter>
    <Parameter>
      <Name>GSM Cartesian Velocity</Name>
      <ParameterKey>GSM_VEL</ParameterKey>
      <Description>Spacecraft orbital velocity vector in GSM coordinates</Description>
      <Units>km/s</Units>
      <UnitsConversion>1e3&gt;m/s</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GSM</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>vx GSM</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>1</Index>
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          <ValidMax>12.0</ValidMax>
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          <ValidMax>12.0</ValidMax>
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          <ValidMax>12.0</ValidMax>
          <FillValue>-1.0E31</FillValue>
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      </Structure>
      <Support>
        <SupportQuantity>Velocity</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>GCI Sun Postion Vector</Name>
      <ParameterKey>SUN_VECTOR</ParameterKey>
      <Description>Sun position vector in GCI coordinates</Description>
      <Units>km</Units>
      <UnitsConversion>1e3&gt;m</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GEI</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>Sun X GCI</Name>
          <Qualifier>Component.I</Qualifier>
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          <ValidMax>1.6E8</ValidMax>
          <FillValue>-1.0E31</FillValue>
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          <Name>Sun Y GCI</Name>
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          <ValidMax>1.6E8</ValidMax>
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          <Name>Sun Z GCI</Name>
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          <ValidMax>1.6E8</ValidMax>
          <FillValue>-1.0E31</FillValue>
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        <SupportQuantity>Positional</SupportQuantity>
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    <Parameter>
      <Name>HEC Cartesian Position</Name>
      <ParameterKey>HEC_POS</ParameterKey>
      <Description>Spacecraft position vector in HEC coordinates</Description>
      <Units>km</Units>
      <UnitsConversion>1e3&gt;m</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>HEE</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
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          <Index>1</Index>
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          <ValidMax>1800000.0</ValidMax>
          <FillValue>-1.0E31</FillValue>
        </Element>
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          <Name>Y HEC</Name>
          <Qualifier>Component.J</Qualifier>
          <Index>2</Index>
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          <ValidMax>1800000.0</ValidMax>
          <FillValue>-1.0E31</FillValue>
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        <Element>
          <Name>Z HEC</Name>
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          <Index>3</Index>
          <ValidMin>-1800000.0</ValidMin>
          <ValidMax>1800000.0</ValidMax>
          <FillValue>-1.0E31</FillValue>
        </Element>
      </Structure>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>HEC Cartesian Velocity</Name>
      <ParameterKey>HEC_VEL</ParameterKey>
      <Description>Spacecraft orbital velocity vector in HEC coordinates</Description>
      <Units>km/s</Units>
      <UnitsConversion>1e3&gt;m/s</UnitsConversion>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>HEE</CoordinateSystemName>
      </CoordinateSystem>
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        <Size>3</Size>
        <Element>
          <Name>vx HEC</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>1</Index>
          <ValidMin>-12.0</ValidMin>
          <ValidMax>12.0</ValidMax>
          <FillValue>-1.0E31</FillValue>
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          <ValidMax>12.0</ValidMax>
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          <ValidMax>12.0</ValidMax>
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      </Structure>
      <Support>
        <SupportQuantity>Velocity</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Carrington Rotation Number</Name>
      <ParameterKey>CRN_EARTH</ParameterKey>
      <Description>Carrington rotation number of the Earth</Description>
      <ValidMin>1857</ValidMin>
      <ValidMax>2239</ValidMax>
      <FillValue>-2147483648</FillValue>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Heliographic Long of the Earth</Name>
      <ParameterKey>LONG_EARTH</ParameterKey>
      <Description>Heliographic longitude of the Earth</Description>
      <Units>rad</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Spherical</CoordinateRepresentation>
        <CoordinateSystemName>HG</CoordinateSystemName>
      </CoordinateSystem>
      <ValidMin>0.0</ValidMin>
      <ValidMax>6.283185307</ValidMax>
      <FillValue>-1.0E31</FillValue>
      <Support>
        <Qualifier>DirectionAngle.AzimuthAngle</Qualifier>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Heliographic Lat of the Earth</Name>
      <ParameterKey>LAT_EARTH</ParameterKey>
      <Description>Heliographic latitude of the Earth</Description>
      <Units>rad</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Spherical</CoordinateRepresentation>
        <CoordinateSystemName>HG</CoordinateSystemName>
      </CoordinateSystem>
      <ValidMin>-1.570796327</ValidMin>
      <ValidMax>1.570796327</ValidMax>
      <FillValue>-1.0E31</FillValue>
      <Support>
        <Qualifier>DirectionAngle.ElevationAngle</Qualifier>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Heliographic Long of Craft</Name>
      <ParameterKey>LONG_SPACE</ParameterKey>
      <Description>Heliographic longitude of the spacecraft</Description>
      <Units>rad</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Spherical</CoordinateRepresentation>
        <CoordinateSystemName>HG</CoordinateSystemName>
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      <ValidMin>0.0</ValidMin>
      <ValidMax>6.283185307</ValidMax>
      <FillValue>-1.0E31</FillValue>
      <Support>
        <Qualifier>DirectionAngle.AzimuthAngle</Qualifier>
        <SupportQuantity>Positional</SupportQuantity>
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    </Parameter>
    <Parameter>
      <Name>Heliographic Lat of the Craft</Name>
      <ParameterKey>LAT_SPACE</ParameterKey>
      <Description>Heliographic latitude of the spacecraft</Description>
      <Units>rad</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Spherical</CoordinateRepresentation>
        <CoordinateSystemName>HG</CoordinateSystemName>
      </CoordinateSystem>
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      <ValidMax>1.570796327</ValidMax>
      <FillValue>-1.0E31</FillValue>
      <Support>
        <Qualifier>DirectionAngle.ElevationAngle</Qualifier>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
  </NumericalData>
</Spase>
