irm-orb-all.xml
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<?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://www.spase-group.org/data/schema/spase-2_3_0.xsd">
<Version>2.3.0</Version>
<NumericalData>
<ResourceID>spase://CNES/NumericalData/CDPP-AMDA/IRM/ORBIT/irm-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/IRM team in any publication resulting from the use of these data.
</Acknowledgement>
</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></ProviderName>
<ProviderResourceName></ProviderResourceName>
<ProviderAcknowlegment> </ProviderAcknowlegment>
<InstrumentID>spase://CNES/Instrument/CDPP-AMDA/IRM/Ephemeris</InstrumentID>
<MeasurementType>Ephemeris</MeasurementType>
<TemporalDescription>
<TimeSpan>
<StartDate>1984-08-25T07:31:00</StartDate>
<StopDate>1986-04-09T04:20:10</StopDate>
</TimeSpan>
<Cadence>PT60S</Cadence>
</TemporalDescription>
<ObservedRegion>Earth.Magnetosheath</ObservedRegion>
<ObservedRegion>Earth.Magnetosphere</ObservedRegion>
<ObservedRegion>Earth.Magnetosphere.Magnetotail</ObservedRegion>
<ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
<Parameter>
<Name>xyz_gse</Name>
<ParameterKey>irm_orb_xyz</ParameterKey>
<Description>
Spacecraft position in GSE Cartesian coordinates
</Description>
<Units>Re</Units>
<UnitsConversion>6.378e6;km</UnitsConversion>
<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>irm_orb_xyz(0)</ParameterKey>
</Element>
<Element>
<Name>y</Name>
<Qualifier>Component.J</Qualifier>
<Index>2</Index>
<ParameterKey>irm_orb_xyz(1)</ParameterKey>
</Element>
<Element>
<Name>z</Name>
<Qualifier>Component.K</Qualifier>
<Index>3</Index>
<ParameterKey>irm_orb_xyz(2)</ParameterKey>
</Element>
</Structure>
</Parameter>
<Parameter>
<Name>distance irm-earth</Name>
<ParameterKey>irm_orb_mag</ParameterKey>
<Description>
Spacecraft distance to earth center
</Description>
<Units>Re</Units>
<UnitsConversion></UnitsConversion>
<CoordinateSystem>
<CoordinateRepresentation>Cartesian</CoordinateRepresentation>
<CoordinateSystemName>GSE</CoordinateSystemName>
</CoordinateSystem>
<RenderingHints>
<DisplayType>TimeSeries</DisplayType>
</RenderingHints>
</Parameter>
</NumericalData>
</Spase>