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   <NumericalData>
      <ResourceID>spase://NOAA/NumericalData/DSCOVR/Ephemeris/Orbit/Preliminary/PT1M</ResourceID>
      <ResourceHeader>
         <ResourceName>DSCOVR Orbital Ephemeris Predicted Spacecraft Position and Velocity</ResourceName>
         <ReleaseDate>2024-06-20T12:34:56.789</ReleaseDate>
         <RevisionHistory>
            <RevisionEvent>
               <ReleaseDate>2021-04-27T17:52:57</ReleaseDate>
               <Note>Only known prior ReleaseDate of the metadata</Note>
            </RevisionEvent>
            <RevisionEvent>
               <ReleaseDate>2024-06-20T12:34:56.789</ReleaseDate>
               <Note>Replaced StopDate with a RelativeStopDate equal to P1M, SPASE versioned up to 2.6.0, LFB 20240620</Note>
            </RevisionEvent>
         </RevisionHistory>
         <Description>DSCOVR Predicted Orbit Data File</Description>
         <Acknowledgement>A. Szabo</Acknowledgement>
         <Contact>
            <PersonID>spase://SMWG/Person/Adam.Szabo</PersonID>
            <Role>PrincipalInvestigator</Role>
         </Contact>
         <Contact>
            <PersonID>spase://SMWG/Person/Robert.E.McGuire</PersonID>
            <Role>MetadataContact</Role>
         </Contact>
         <Contact>
            <PersonID>spase://SMWG/Person/Lee.Frost.Bargatze</PersonID>
            <Role>MetadataContact</Role>
         </Contact>
         <InformationURL>
            <Name>Deep Space Climate Observatory, DSCOVR, Web Page, NESDIS, NOAA</Name>
            <URL>https://www.nesdis.noaa.gov/content/dscovr-deep-space-climate-observatory</URL>
            <Description>Deep Space Climate Observatory, DSCOVR, Web Page hosted by the National Environmental Satellite, Data, and Information Service, NESDIS, National Oceanic and Atmospheric Administration, NOAA</Description>
         </InformationURL>
         <PriorID>spase://VSPO/NumericalData/DSCOVR/Ephemeris/Orbit/PT1M</PriorID>
         <PriorID>spase://VSPO/NumericalData/DSCOVR/Ephemeris/Orbit/Preliminary/PT1M</PriorID>
      </ResourceHeader>
      <AccessInformation>
         <RepositoryID>spase://SMWG/Repository/NASA/GSFC/SPDF</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/dscovr/orbit/pre_or/</URL>
            <Description>In CDF via ftp from SPDF.</Description>
         </AccessURL>
         <AccessURL>
            <Name>HTTPS from SPDF</Name>
            <URL>https://spdf.gsfc.nasa.gov/pub/data/dscovr/orbit/pre_or/</URL>
            <Description>In CDF via http from SPDF.</Description>
         </AccessURL>
         <AccessURL>
            <Name>CDAWeb</Name>
            <URL>https://cdaweb.gsfc.nasa.gov/index.html/</URL>
            <ProductKey>DSCOVR_ORBIT_PRE</ProductKey>
            <Description>Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb</Description>
         </AccessURL>
         <Format>CDF</Format>
         <Encoding>None</Encoding>
         <Acknowledgement>A. Szabo. Please acknowledge the data providers and CDAWeb when using these data.</Acknowledgement>
      </AccessInformation>
      <AccessInformation>
         <RepositoryID>spase://SMWG/Repository/NASA/GSFC/SPDF</RepositoryID>
         <Availability>Online</Availability>
         <AccessRights>Open</AccessRights>
         <AccessURL>
            <Name>CDAWeb HAPI Server</Name>
            <URL>https://cdaweb.gsfc.nasa.gov/hapi</URL>
            <Style>HAPI</Style>
            <ProductKey>DSCOVR_ORBIT_PRE</ProductKey>
            <Description>Web Service to this product using the HAPI interface.</Description>
         </AccessURL>
         <Format>CSV</Format>
         <Acknowledgement>A. Szabo. Please acknowledge the data providers and CDAWeb when using these data.</Acknowledgement>
      </AccessInformation>
      <ProcessingLevel>Calibrated</ProcessingLevel>
      <InstrumentID>spase://SMWG/Instrument/DSCOVR/Ephemeris</InstrumentID>
      <InstrumentID>spase://SMWG/Instrument/DSCOVR/PlasMag/FaradayCup</InstrumentID>
      <InstrumentID>spase://SMWG/Instrument/DSCOVR/PlasMag/FluxgateMagnetometer</InstrumentID>
      <MeasurementType>Ephemeris</MeasurementType>
      <TemporalDescription>
         <TimeSpan>
            <StartDate>2015-02-11T00:00:00.000</StartDate>
            <RelativeStopDate>P1M</RelativeStopDate>
         </TimeSpan>
         <Cadence>PT10S</Cadence>
      </TemporalDescription>
      <ObservedRegion>Heliosphere</ObservedRegion>
      <ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
      <ObservedRegion>Heliosphere.Inner</ObservedRegion>
      <Parameter>
         <Name>Epoch Time, since 0 A.D.</Name>
         <ParameterKey>Epoch</ParameterKey>
         <Description>Epoch Time, Milliseconds since 0 A.D.</Description>
         <Caveats>This parameter exhibits an increasing monotonic progression.</Caveats>
         <Cadence>PT10S</Cadence>
         <Units>ms</Units>
         <UnitsConversion>1e-3&gt;s</UnitsConversion>
         <RenderingHints>
            <AxisLabel>Epoch</AxisLabel>
            <ValueFormat>E14.8</ValueFormat>
         </RenderingHints>
         <ValidMin>11-Feb-2015 00:00:00.000</ValidMin>
         <ValidMax>11-Feb-2065 00:00:00.000</ValidMax>
         <FillValue>31-Dec-9999 23:59:59.999</FillValue>
         <Support>
            <SupportQuantity>Temporal</SupportQuantity>
         </Support>
      </Parameter>
      <Parameter>
         <Name>Time PB5</Name>
         <Set>Time series defined by using: EPOCH</Set>
         <ParameterKey>Time_PB5</ParameterKey>
         <Description>Time in PB5 Format: Year, Day, Milliseconds, Observation Time</Description>
         <Cadence>PT10S</Cadence>
         <Structure>
            <Size>3</Size>
            <Element>
               <Name>Year</Name>
               <Index>1</Index>
               <Units>year</Units>
               <ValidMin>2015</ValidMin>
               <ValidMax>2065</ValidMax>
            </Element>
            <Element>
               <Name>Day of Year</Name>
               <Index>2</Index>
               <Units>d</Units>
               <ValidMin>0</ValidMin>
               <ValidMax>366</ValidMax>
            </Element>
            <Element>
               <Name>Elapsed milliseconds of day</Name>
               <Index>3</Index>
               <Units>ms</Units>
               <ValidMin>0</ValidMin>
               <ValidMax>86400000</ValidMax>
            </Element>
         </Structure>
         <FillValue>-2147483647</FillValue>
         <Support>
            <SupportQuantity>Temporal</SupportQuantity>
         </Support>
      </Parameter>
      <Parameter>
         <Name>Sun-Earth Radial Distance</Name>
         <Set>Time series defined by using: EPOCH</Set>
         <ParameterKey>SUN_R</ParameterKey>
         <Description>Sun-Earth Radial Distance</Description>
         <Cadence>PT10S</Cadence>
         <Units>km</Units>
         <UnitsConversion>1e3&gt;m</UnitsConversion>
         <RenderingHints>
            <DisplayType>TimeSeries</DisplayType>
            <AxisLabel>Earth Distance from Sun</AxisLabel>
            <ValueFormat>F17.5</ValueFormat>
            <ScaleMin>1.45e+08</ScaleMin>
            <ScaleMax>1.55e+08</ScaleMax>
         </RenderingHints>
         <ValidMin>0.0</ValidMin>
         <ValidMax>1.8e+08</ValidMax>
         <FillValue>-1.0e+31</FillValue>
         <Support>
            <Qualifier>Magnitude</Qualifier>
            <SupportQuantity>Positional</SupportQuantity>
         </Support>
      </Parameter>
      <Parameter>
         <Name>Spacecraft Position, J2000 GCI</Name>
         <Set>Time series defined by using: EPOCH</Set>
         <ParameterKey>GCI_POS</ParameterKey>
         <Description>Spacecraft Position Vector, Geocentric Inertial, J2000 GCI, Cartesian Coordinates</Description>
         <Cadence>PT10S</Cadence>
         <Units>km</Units>
         <UnitsConversion>1e3&gt;m</UnitsConversion>
         <CoordinateSystem>
            <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
            <CoordinateSystemName>GEI</CoordinateSystemName>
         </CoordinateSystem>
         <RenderingHints>
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            <ScaleMin>-1.8e+06</ScaleMin>
            <ScaleMax>1.8e+06</ScaleMax>
         </RenderingHints>
         <Structure>
            <Size>3</Size>
            <Element>
               <Name>X GCI</Name>
               <Index>1</Index>
            </Element>
            <Element>
               <Name>Y GCI</Name>
               <Index>2</Index>
            </Element>
            <Element>
               <Name>Z GCI</Name>
               <Index>3</Index>
            </Element>
         </Structure>
         <ValidMin>-1.8e+06</ValidMin>
         <ValidMax>1.8e+06</ValidMax>
         <FillValue>-1.0e+31</FillValue>
         <Support>
            <Qualifier>Vector</Qualifier>
            <SupportQuantity>Positional</SupportQuantity>
         </Support>
      </Parameter>
      <Parameter>
         <Name>Spacecraft Velocity, J2000 GCI</Name>
         <Set>Time series defined by using: EPOCH</Set>
         <ParameterKey>GCI_VEL</ParameterKey>
         <Description>Spacecraft Velocity Vector, Geocentric Inertial, J2000 GCI, Cartesian Coordinates</Description>
         <Cadence>PT10S</Cadence>
         <Units>km/s</Units>
         <UnitsConversion>1e3&gt;m/s</UnitsConversion>
         <CoordinateSystem>
            <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
            <CoordinateSystemName>GEO</CoordinateSystemName>
         </CoordinateSystem>
         <RenderingHints>
            <DisplayType>TimeSeries</DisplayType>
            <ValueFormat>F12.7</ValueFormat>
            <ScaleMin>-12.0</ScaleMin>
            <ScaleMax>12.0</ScaleMax>
         </RenderingHints>
         <Structure>
            <Size>3</Size>
            <Element>
               <Name>Vx GCI</Name>
               <Index>1</Index>
            </Element>
            <Element>
               <Name>Vy GCI</Name>
               <Index>2</Index>
            </Element>
            <Element>
               <Name>Vz GCI</Name>
               <Index>3</Index>
            </Element>
         </Structure>
         <ValidMin>-12.0</ValidMin>
         <ValidMax>12.0</ValidMax>
         <FillValue>-1.0e+31</FillValue>
         <Support>
            <Qualifier>Vector</Qualifier>
            <SupportQuantity>Positional</SupportQuantity>
         </Support>
      </Parameter>
      <Parameter>
         <Name>Spacecraft Position, GSE</Name>
         <Set>Time series defined by using: EPOCH</Set>
         <ParameterKey>GSE_POS</ParameterKey>
         <Description>Spacecraft Position Vector, Geocentric Solar Ecliptic, GSE Cartesian Coordinates</Description>
         <Cadence>PT10S</Cadence>
         <Units>km</Units>
         <UnitsConversion>1e3&gt;m</UnitsConversion>
         <CoordinateSystem>
            <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
            <CoordinateSystemName>GSE</CoordinateSystemName>
         </CoordinateSystem>
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            <Size>3</Size>
            <Element>
               <Name>X GSE</Name>
               <Index>1</Index>
            </Element>
            <Element>
               <Name>Y GSE</Name>
               <Index>2</Index>
            </Element>
            <Element>
               <Name>Z GSE</Name>
               <Index>3</Index>
            </Element>
         </Structure>
         <ValidMin>-1.8e+06</ValidMin>
         <ValidMax>1.8e+06</ValidMax>
         <FillValue>-1.0e+31</FillValue>
         <Support>
            <Qualifier>Vector</Qualifier>
            <SupportQuantity>Positional</SupportQuantity>
         </Support>
      </Parameter>
      <Parameter>
         <Name>Moon Position, GSE</Name>
         <Set>Time series defined by using: EPOCH</Set>
         <ParameterKey>MOON_GSE_POS</ParameterKey>
         <Description>Moon Position Vector, Geocentric Solar Ecliptic, GSE Cartesian Coordinates</Description>
         <Cadence>PT10S</Cadence>
         <Units>km</Units>
         <UnitsConversion>1e3&gt;m</UnitsConversion>
         <CoordinateSystem>
            <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
            <CoordinateSystemName>GSE</CoordinateSystemName>
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            <Size>3</Size>
            <Element>
               <Name>Moon X GSE</Name>
               <Index>1</Index>
            </Element>
            <Element>
               <Name>Moon Y GSE</Name>
               <Index>2</Index>
            </Element>
            <Element>
               <Name>Moon Z GSE</Name>
               <Index>3</Index>
            </Element>
         </Structure>
         <ValidMin>-1.8e+06</ValidMin>
         <ValidMax>1.8e+06</ValidMax>
         <FillValue>-1.0e+31</FillValue>
         <Support>
            <Qualifier>Vector</Qualifier>
            <SupportQuantity>Positional</SupportQuantity>
         </Support>
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