intt-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://cdpp.irap.omp.eu/AMDA-NG/public/schemas/spase-amda-1_2_0.xsd">
<Version>2.2.6</Version>
<NumericalData>
<ResourceID>spase://CDPP/NumericalData/AMDA/INTERBALL-Tail/Ephemeris/intt-orb-all</ResourceID>
<ResourceHeader>
<ResourceName>orbit</ResourceName>
<ReleaseDate>2015-10-16T18:00:00.000</ReleaseDate>
<Description>Definitive Interball Tail satellite and subsatellite (Interball-1 and Magion-4) orbital data: Spacecraft position, velocity, and status flags.</Description>
<Acknowledgement>The Interball project, Russian Space Research Institute (IKI) and Dr. Prokhorenko</Acknowledgement>
<Contact>
<PersonID>spase://SMWG/Person/Victoria.I.Prokhorenko</PersonID>
<Role>PrincipalInvestigator</Role>
</Contact>
<Contact>
<PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
<Role>TechnicalContact</Role>
</Contact>
<InformationURL>
<Name>IKI Satellite Situation Center</Name>
<URL>http://www.iki.rssi.ru/vprokhor</URL>
<Description>This page maintains the Situation Analysis for the IKI International Space Missions and its coordination with the Inter-Agency multimission campaigns.</Description>
</InformationURL>
<InformationURL>
<Name>Interball Tail Probe Situation Analysis</Name>
<URL>http://www.iki.rssi.ru/vprokhor/tail.htm</URL>
</InformationURL>
</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/Interball-1/Ephemeris</InstrumentID>
<MeasurementType>Ephemeris</MeasurementType>
<TemporalDescription>
<TimeSpan>
<StartDate>1995-08-04T00:01:00Z</StartDate>
<StopDate>2000-10-16T13:55:00Z</StopDate>
</TimeSpan>
<Cadence>PT2M</Cadence>
</TemporalDescription>
<ObservedRegion>Earth.Magnetosphere</ObservedRegion>
<ObservedRegion>Earth.Magnetosheath</ObservedRegion>
<ObservedRegion>Earth.Magnetosphere.Main</ObservedRegion>
<ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
<Caveats>The data cadence varies.</Caveats>
<Parameter>
<Name>xyz_gse</Name>
<ParameterKey>it_xyz</ParameterKey>
<Description>Interball-1 spacecraft position in GSE frame, 3 components in RE (6370km)</Description>
<Ucd>pos.earth;instr.obsty</Ucd>
<Units>Re</Units>
<UnitsConversion>6.37e6>m</UnitsConversion>
<CoordinateSystem>
<CoordinateRepresentation>Cartesian</CoordinateRepresentation>
<CoordinateSystemName>GSE</CoordinateSystemName>
</CoordinateSystem>
<RenderingHints>
<DisplayType>TimeSeries</DisplayType>
<ValueFormat>F7.3</ValueFormat>
</RenderingHints>
<Structure>
<Size>3</Size>
<Element>
<Name>x</Name>
<Qualifier>Component.I</Qualifier>
<Index>1</Index>
<ParameterKey>it_xyz(0)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
<Element>
<Name>y</Name>
<Qualifier>Component.J</Qualifier>
<Index>2</Index>
<ParameterKey>it_xyz(1)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
<Element>
<Name>z</Name>
<Qualifier>Component.K</Qualifier>
<Index>3</Index>
<ParameterKey>it_xyz(2)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
</Structure>
<Support>
<Qualifier>Vector</Qualifier>
<SupportQuantity>Positional</SupportQuantity>
</Support>
</Parameter>
<Parameter>
<Name>xyz_gsm</Name>
<ParameterKey>it_xyz_gsm</ParameterKey>
<Description>Interball-1 spacecraft position in GSM frame, 3 components in RE (6370km)</Description>
<Ucd>pos.earth;instr.obsty</Ucd>
<Units>Re</Units>
<UnitsConversion>6.37e6>m</UnitsConversion>
<CoordinateSystem>
<CoordinateRepresentation>Cartesian</CoordinateRepresentation>
<CoordinateSystemName>GSM</CoordinateSystemName>
</CoordinateSystem>
<RenderingHints>
<DisplayType>TimeSeries</DisplayType>
<ValueFormat>F7.3</ValueFormat>
</RenderingHints>
<Structure>
<Size>3</Size>
<Element>
<Name>x</Name>
<Qualifier>Component.I</Qualifier>
<Index>1</Index>
<ParameterKey>it_xyz_gsm(0)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
<Element>
<Name>y</Name>
<Qualifier>Component.J</Qualifier>
<Index>2</Index>
<ParameterKey>it_xyz_gsm(1)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
<Element>
<Name>z</Name>
<Qualifier>Component.K</Qualifier>
<Index>3</Index>
<ParameterKey>it_xyz_gsm(2)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
</Structure>
<Support>
<Qualifier>Vector</Qualifier>
<SupportQuantity>Positional</SupportQuantity>
</Support>
</Parameter>
</NumericalData>
</Spase>