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    <Version>2.2.6</Version>
    <NumericalData>
        <ResourceID>spase://CDPP/NumericalData/AMDA/DoubleStar1/Ephemeris/dstar1-orb-all</ResourceID>
        <ResourceHeader>

            <ResourceName>orbit</ResourceName>

            <AlternateName>Double Star 1 Auxiliary Summary Parameters Data</AlternateName>
            <ReleaseDate>2015-10-16T16:34:56.789</ReleaseDate>
            <Description>The Double Star 1 auxiliary summary parameter data set contains various parameters in GSE coordinates at 60 s resolution. These parameters include universal time, orbit number, GSE position, GSE spacecraft velocity vector, longitude, and dipole tilt. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.</Description>
            <Acknowledgement>European Space Agency/International</Acknowledgement>
            <Contact>
                <PersonID>spase://SMWG/Person/James.M.Weygand</PersonID>
                <Role>MetadataContact</Role>
            </Contact>
            <InformationURL>
                <Name>Double Star 1 Orbital Parameters</Name>
                <URL>http://nssdc.gsfc.nasa.gov/nmc/spacecraftOrbit.do?id=2003-061A</URL>
                <Description>Introduction to the Double Star 1 Orbit.</Description>
            </InformationURL>

        </ResourceHeader>
        <AccessInformation>
            <RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
            <Availability>Online</Availability>
            <AccessRights>Restricted</AccessRights>
            <AccessURL>
                <Name>AMDA at CDPP</Name>
                <URL>http://amda.cdpp.eu</URL>
            </AccessURL>
            <Format>NetCDF</Format>
            <Acknowledgement>European Space Agency/International</Acknowledgement>
        </AccessInformation>
        <ProviderName>CSDS-CNES</ProviderName>
        <ProcessingLevel>Calibrated</ProcessingLevel>
        <ProviderResourceName>Double Star 1 Auxiliary Summary Parameters Data</ProviderResourceName>
        <ProviderProcessingLevel>Calibrated</ProviderProcessingLevel>
        <ProviderVersion>1</ProviderVersion>
        <InstrumentID>spase://CDPP/Instrument/AMDA/DoubleStar1/Ephemeris</InstrumentID>
        <MeasurementType>Ephemeris</MeasurementType>
        <TemporalDescription>
            <TimeSpan>

                <StartDate>2004-02-01T00:00:00Z</StartDate>
                <StopDate>2007-10-10T12:38:00Z</StopDate>

            </TimeSpan>
            <Cadence>PT60S</Cadence>
        </TemporalDescription>
        <ObservedRegion>Earth.Magnetosheath</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere.Magnetotail</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere.Main</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere.RadiationBelt</ObservedRegion>
        <ObservedRegion>Earth.NearSurface.Ionosphere</ObservedRegion>
        <ObservedRegion>Earth.NearSurface.Plasmasphere</ObservedRegion>
        <Keyword>Double Star</Keyword>
        <Keyword>Tan Ce 1</Keyword>
        <Keyword>TC 1</Keyword>
        <Keyword>Ephemeris</Keyword>
        <Keyword>60 second</Keyword>
        <Keyword>lobe</Keyword>
        <Keyword>magnetosphere</Keyword>
        <Keyword>magnetotail</Keyword>
        <Parameter>

            <Name>xyz_gse</Name>

            <ParameterKey>ds1_xyz</ParameterKey>
            <Description>Double Star 1 spacecraft position at 60 s resolution in GSE Coordinates in units of km.</Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Cadence>PT60S</Cadence>
            <Units>Re</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
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                <Size>3</Size>
                <Element>

                    <Name>x</Name>

                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ParameterKey>ds1_xyz(0)</ParameterKey>
                </Element>
                <Element>

                    <Name>y</Name>

                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>ds1_xyz(1)</ParameterKey>
                </Element>
                <Element>

                    <Name>z</Name>

                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>ds1_xyz(2)</ParameterKey>
                </Element>
            </Structure>
            <FillValue>-1.0e31</FillValue>
            <Support>
                <Qualifier>Vector</Qualifier>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>

            <Name>xyz_gsm</Name>

            <ParameterKey>ds1_xyz_gsm</ParameterKey>
            <Description>Double Star 1 spacecraft position at 60 s resolution in GSM Coordinates in units of km.</Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Cadence>PT60S</Cadence>
            <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>ds1_xyz_gsm(0)</ParameterKey>
                </Element>
                <Element>

                    <Name>y</Name>

                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>ds1_xyz_gsm(1)</ParameterKey>
                </Element>
                <Element>

                    <Name>z</Name>

                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>ds1_xyz_gsm(2)</ParameterKey>
                </Element>
            </Structure>
            <FillValue>-1.0e31</FillValue>
            <Support>
                <Qualifier>Vector</Qualifier>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
     </NumericalData>
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