<?xml version="1.0" encoding="UTF-8"?>
<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://cdpp1.cesr.fr/AMDA-NG/public/schemas/spase-amda-1_2_0.xsd">
    <Version>2.2.6</Version>
    <NumericalData>
        <ResourceID>spase://CDPP/NumericalData/AMDA/ISEE/ISEE2/Ephemeris/isee2-orb-all</ResourceID>
        <ResourceHeader>

            <ResourceName>orbit</ResourceName>

            <ReleaseDate>2015-10-16T14:30:00</ReleaseDate>
            <Description/>
            <Contact>
                <PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
                <Role>TechnicalContact</Role>
            </Contact>
            <InformationURL>
                <Name>UCLA-IGPP ISEE Magnetometer Interactive Data Server</Name>
                <URL>http://www-ssc.igpp.ucla.edu/forms/isee</URL>
                <Description>Data at 60-s and 4-s resolution are available for the entire ISEE mission (October 22, 1977 through  September 25, 1987) and can be displayed either as a plot or an ASCII listing. The ISEE-1 and -2 magnetometer data server is provided by the Institute of Geophysics and Planetary Physics (IGPP) at UCLA, through a grant to Robert J. Strangeway from the NASA Space Physics Data System (SPDS).</Description>
            </InformationURL>
        </ResourceHeader>
        <AccessInformation>
            <RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
            <AccessRights>Open</AccessRights>
            <AccessURL>
                <Name>AMDA at CDPP</Name>
                <URL>http://amda.cdpp.eu</URL>
            </AccessURL>
            <Format>NetCDF</Format>
        </AccessInformation>
        <ProviderName>NSSDC</ProviderName>
        <ProcessingLevel>Calibrated</ProcessingLevel>

        <InstrumentID>spase://CDPP/Instrument/AMDA/ISEE2/Ephemeris</InstrumentID>

        <MeasurementType>Ephemeris</MeasurementType>
        <TemporalDescription>
            <TimeSpan>

                <StartDate>1977-10-22T14:49:00Z</StartDate>
                <StopDate>1987-09-26T05:59:00Z</StopDate>

            </TimeSpan>
            <Cadence>PT1M</Cadence>
        </TemporalDescription>
        <ObservedRegion>Earth.Magnetosphere</ObservedRegion>
        <ObservedRegion>Earth.Magnetosheath</ObservedRegion>
        <ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
        <Parameter>

            <Name>xyz_gse</Name>

            <ParameterKey>isee2_xyz</ParameterKey>
            <Description>
                Spacecraft position vector, GSE Cartesian components, in Earth radii
            </Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Cadence>PT1M</Cadence>
            <Units>Re</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Description>
                    GSE X,Y,Z components of spacecraft position vector
                </Description>
                <Element>
                    <Name>x</Name>
                    <Index>1</Index>
                    <ParameterKey>isee2_xyz(0)</ParameterKey>
                </Element>
                <Element>
                    <Name>y</Name>
                    <Index>2</Index>
                    <ParameterKey>isee2_xyz(1)</ParameterKey>
                </Element>
                <Element>
                    <Name>z</Name>
                    <Index>3</Index>
                    <ParameterKey>isee2_xyz(2)</ParameterKey>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>

            <Name>xyz_gsm</Name>

            <ParameterKey>isee2_xyz_gsm</ParameterKey>
            <Description>
                Spacecraft position vector, GSM Cartesian components, in Earth radii
            </Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Cadence>PT1M</Cadence>
            <Units>Re</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSM</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Description>GSM X,Y,Z components of spacecraft position vector
                </Description>
                <Element>

                    <Name>x</Name>

                    <Index>1</Index>
                    <ParameterKey>isee2_xyz_gsm(0)</ParameterKey>
                </Element>
                <Element>

                    <Name>y</Name>

                    <Index>2</Index>
                    <ParameterKey>isee2_xyz_gsm(1)</ParameterKey>
                </Element>
                <Element>

                    <Name>z</Name>

                    <Index>3</Index>
                    <ParameterKey>isee2_xyz_gsm(2)</ParameterKey>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
    </NumericalData>
</Spase>