gtl-orb-all.xml 5.82 KB
<?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/Geotail/Ephemeris/gtl-orb-all</ResourceID>
        <ResourceHeader>
            <ResourceName>Geotail Spacecraft Definitive Positions</ResourceName>
            <ReleaseDate>2015-10-16T17:16:33Z</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/Elena.Budnik</PersonID>
                <Role>TechnicalContact</Role>
            </Contact>
        </ResourceHeader>
        <AccessInformation>
            <RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
            <Availability>Online</Availability>
            <AccessRights>Open</AccessRights>
            <AccessURL>
                <Name>AMDA at CDPP</Name>
                <URL>http://amda.cdpp.eu</URL>
            </AccessURL>
            <Format>NetCDF</Format>
            <Encoding>None</Encoding>
        </AccessInformation>
        <ProviderName>CDAWeb</ProviderName>
        <InstrumentID>spase://CDPP/Instrument/AMDA/Geotail/Ephemeris</InstrumentID>
        <MeasurementType>Ephemeris</MeasurementType>
        <TemporalDescription>
            <TimeSpan>
                <StartDate>1992-07-27T16:00:00</StartDate>
                <StopDate>2014-07-06T00:00:00</StopDate>
            </TimeSpan>
            <Cadence>PT10M</Cadence>
        </TemporalDescription>
        <Parameter>
            <Name>GSE Cartesian Position</Name>
            <ParameterKey>gtl_xyz</ParameterKey>
            <Description>Spacecraft position vector in GSE coordinates</Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Units>Re</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>X GSE</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ParameterKey>gtl_xyz(0)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Y GSE</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>gtl_xyz(1)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Z GSE</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>gtl_xyz(2)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>GSM Cartesian Position</Name>
            <ParameterKey>gtl_xyz_gsm</ParameterKey>
            <Description>Spacecraft position vector in GSM coordinates</Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Units>Re</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSM</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>X GSM</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ParameterKey>gtl_xyz_gsm(0)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Y GSM</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>gtl_xyz_gsm(1)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>Z GSM</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>gtl_xyz_gsm(2)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Carrington Rotation Number</Name>
            <ParameterKey>gtl_r</ParameterKey>
            <Description>Carrington rotation number of the Earth</Description>
            <Ucd>pos.distance;instr.obsty</Ucd>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <ValidMin>1857</ValidMin>
            <ValidMax>2239</ValidMax>
            <FillValue>-2147483648</FillValue>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
     </NumericalData>
</Spase>