<Spase xmlns="http://www.spase-group.org/data/schema" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.spase-group.org/data/schema http://www.spase-group.org/data/schema/spase-2_2_2.xsd">
    <Version>2.2.2</Version>
    <NumericalData>
        <ResourceID>spase://VMO/NumericalData/Geotail/Ephemeris/PT10M</ResourceID>
        <ResourceHeader>
            <ResourceName>Geotail Spacecraft Definitive Positions</ResourceName>
            <ReleaseDate>2010-04-05T22:16:33Z</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>
        </ResourceHeader>
        <AccessInformation>
            <RepositoryID>spase://SMWG/Repository/NASA/GSFC/SPDF/CDAWeb</RepositoryID>
            <Availability>Online</Availability>
            <AccessRights>Open</AccessRights>
            <AccessURL>
                <Name>FTP access to files at SPDF</Name>
                <URL>ftp://spdf.gsfc.nasa.gov/pub/data/geotail/def_or</URL>
                <Description>NASA/GSFC CDAWeb ftp access to the data.</Description>
            </AccessURL>
            <AccessURL>
                <Name>HTTP access to files at SPDF</Name>
                <URL>http://spdf.gsfc.nasa.gov/pub/data/geotail/def_or</URL>
                <Description>In CDF via HTTP from SPDF</Description>
            </AccessURL>
            <AccessURL>
                <Name>CDAWeb</Name>
                <URL>http://cdaweb.gsfc.nasa.gov/</URL>
                <ProductKey>GE_OR_DEF</ProductKey>
            </AccessURL>
            <AccessURL>
                <Name>SSCWeb</Name>
                <URL>http://sscweb.gsfc.nasa.gov/cgi-bin/Locator.cgi</URL>
                <ProductKey>geotail</ProductKey>
            </AccessURL>
            <Format>CDF</Format>
            <Encoding>None</Encoding>
        </AccessInformation>
        <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>
            </Support>
        </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>
                    <ValidMin>0</ValidMin>
                    <ValidMax>86399000</ValidMax>
                    <FillValue>-2147483648</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </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>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>X GCI</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ValidMin>-1800000.0</ValidMin>
                    <ValidMax>1800000.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Y GCI</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-1800000.0</ValidMin>
                    <ValidMax>1800000.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Z GCI</Name>
                    <Qualifier>Component.K</Qualifier>
                    <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>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>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>vx GCI</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>vy GCI</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>vz GCI</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Velocity</SupportQuantity>
            </Support>
        </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>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>X GSE</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ValidMin>-1800000.0</ValidMin>
                    <ValidMax>1800000.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Y GSE</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-1800000.0</ValidMin>
                    <ValidMax>1800000.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Z GSE</Name>
                    <Qualifier>Component.K</Qualifier>
                    <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>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>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>vx GSE</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>vy GSE</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>vz GSE</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </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>
                <Element>
                    <Name>X GSM</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ValidMin>-1800000.0</ValidMin>
                    <ValidMax>1800000.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Y GSM</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-1800000.0</ValidMin>
                    <ValidMax>1800000.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Z GSM</Name>
                    <Qualifier>Component.K</Qualifier>
                    <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>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>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>vy GSM</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>vz GSM</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </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>
                    <Index>1</Index>
                    <ValidMin>-1.6E8</ValidMin>
                    <ValidMax>1.6E8</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Sun Y GCI</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-1.6E8</ValidMin>
                    <ValidMax>1.6E8</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Sun Z GCI</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ValidMin>-1.6E8</ValidMin>
                    <ValidMax>1.6E8</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <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>
                <Size>3</Size>
                <Element>
                    <Name>X HEC</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ValidMin>-1800000.0</ValidMin>
                    <ValidMax>1800000.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Y HEC</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-1800000.0</ValidMin>
                    <ValidMax>1800000.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Z HEC</Name>
                    <Qualifier>Component.K</Qualifier>
                    <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>
            <Structure>
                <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>
                </Element>
                <Element>
                    <Name>vy HEC</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>vz HEC</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ValidMin>-12.0</ValidMin>
                    <ValidMax>12.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </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>
            </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 Craft</Name>
            <ParameterKey>LAT_SPACE</ParameterKey>
            <Description>Heliographic latitude of the spacecraft</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>
    </NumericalData>
</Spase>