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   <Version>2.3.0</Version>
   <NumericalData>

      <ResourceID>spase://CNES/NumericalData/CDPP-AMDA/CCE/ORBIT/cce-orb-all</ResourceID>

      <ResourceHeader>

          <ResourceName>orbit</ResourceName>

          <AlternateName>Ephemeris</AlternateName>      
          <ReleaseDate>2019-05-05T12:34:56Z</ReleaseDate>
         <Description>           
         </Description>
          <Acknowledgement>User will acknowledge the AMPTE/CCE team in any publication resulting from the use of these data.
         </Acknowledgement>
         <Contact>
           <PersonID>spase://SMWG/Person/Brian.J.Anderson</PersonID>
           <Role>PrincipalInvestigator</Role>
         </Contact>
         <InformationURL>
           <Name>AMPTE-CCE Magnetic Field Experiment Home Page</Name>
             <URL>http://sd-www.jhuapl.edu/AMPTE/MAG/</URL>
           <Description>
               Website hosting AMPTE/CCE magnetic experiment instrument information as well as spin-averaged data.
           </Description>
         </InformationURL>
      </ResourceHeader>
      <AccessInformation>
         <RepositoryID>spase://SMWG/Repository/CNES/CDPP-AMDA</RepositoryID>
         <Availability>Online</Availability>
         <AccessRights>Open</AccessRights>
         <AccessURL>
            <Name>AMDA at CDPP</Name>
            <URL>
                http://amda.cdpp.eu
            </URL>
         </AccessURL>
         <Format>Text</Format>
         <Acknowledgement>
                AMDA is a science analysis system provided by the Centre de Donnees de la 
                Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and 
                Universite Paul Sabatier, Toulouse
         </Acknowledgement>
      </AccessInformation>
      <ProviderName>JHUAPL</ProviderName> 
       <ProviderResourceName>AMPTE/MAG/SA_Data/</ProviderResourceName>
      <ProviderAcknowlegment> </ProviderAcknowlegment>

      <InstrumentID>spase://CNES/Instrument/CDPP-AMDA/CCE/Ephemeris</InstrumentID>

      <MeasurementType>Ephemeris</MeasurementType>
      <TemporalDescription>
         <TimeSpan>
            <StartDate>1984-08-21T00:00:12Z</StartDate>
             <StopDate>1989-01-09T23:59:55Z</StopDate>
         </TimeSpan>

          <CadenceMin>PT60S</CadenceMin>

      </TemporalDescription>
       <ObservedRegion>Earth.Magnetosheath</ObservedRegion>
       <ObservedRegion>Earth.Magnetosphere</ObservedRegion>
       <ObservedRegion>Earth.Magnetosphere.Magnetotail</ObservedRegion>   
       <ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
      <Parameter>

         <Name>xyz_gse</Name>

         <ParameterKey>cce_orb_xyz</ParameterKey>
         <Description>
             Position in GSE Cartesian coordinates
         </Description>
         <Units>Re</Units>
         <CoordinateSystem>
            <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
            <CoordinateSystemName>GSE</CoordinateSystemName>
         </CoordinateSystem>
         <RenderingHints>
              <DisplayType>TimeSeries</DisplayType>
         </RenderingHints>
         <Structure>
            <Size>3</Size>
            <Element>
                <Name>x</Name>
                <Qualifier>Component.I</Qualifier>
                <Index>1</Index>
                <ParameterKey>cce_orb_xyz(0)</ParameterKey>                           
            </Element>
            <Element>
                <Name>y</Name>
                <Qualifier>Component.J</Qualifier>
                <Index>2</Index>
                <ParameterKey>cce_orb_xyz(1)</ParameterKey>      
            </Element>
            <Element>
                <Name>z</Name>
                <Qualifier>Component.K</Qualifier>
                <Index>3</Index>
                <ParameterKey>cce_orb_xyz(2)</ParameterKey> 
            </Element>
         </Structure>
      </Parameter>

       <Parameter>
           <Name>xyz_gsm</Name>
           <ParameterKey>cce_orb_gsm</ParameterKey>
           <Description>
               Position in GSM Cartesian coordinates
           </Description>
           <Units>Re</Units>
           <CoordinateSystem>
               <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
               <CoordinateSystemName>GSM</CoordinateSystemName>
           </CoordinateSystem>
           <RenderingHints>
               <DisplayType>TimeSeries</DisplayType>
           </RenderingHints>
           <Structure>
               <Size>3</Size>
               <Element>
                   <Name>x</Name>
                   <Qualifier>Component.I</Qualifier>
                   <Index>1</Index>
                   <ParameterKey>cce_orb_gsm(0)</ParameterKey>                           
               </Element>
               <Element>
                   <Name>y</Name>
                   <Qualifier>Component.J</Qualifier>
                   <Index>2</Index>
                   <ParameterKey>cce_orb_gsm(1)</ParameterKey>      
               </Element>
               <Element>
                   <Name>z</Name>
                   <Qualifier>Component.K</Qualifier>
                   <Index>3</Index>
                   <ParameterKey>cce_orb_gsm(2)</ParameterKey> 
               </Element>
           </Structure>
       </Parameter>

       <Parameter>
           <Name>distance cce-earth</Name>
           <ParameterKey>cce_orb_mag</ParameterKey>
           <Description>
               Spacecraft distance to earth center
           </Description>
           <Units>Re</Units>
           <RenderingHints>
               <DisplayType>TimeSeries</DisplayType>
           </RenderingHints>
       </Parameter>

</NumericalData>
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