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://www.spase-group.org/data/schema/spase-2.4.1.xsd">
<Version>2.4.1</Version>
<NumericalData>
<ResourceID>spase://CNES/NumericalData/CDPP-AMDA/INTERBALL-Tail/Ephemeris/intt-orb-all</ResourceID>
<ResourceHeader>
<ResourceName>orbit</ResourceName>
<ReleaseDate>2013-05-24T12:42:32Z</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>
<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>CDPP/AMDA HAPI Server</Name>
<URL>https://amda.irap.omp.eu/service/hapi</URL>
<Style>HAPI</Style>
<ProductKey>intt-orb-all</ProductKey>
<Description>Web Service to this product using the HAPI interface.</Description>
</AccessURL>
<Format>CSV</Format>
<Acknowledgement>Thank you for acknowledging the use of AMDA in publications with wording like "Data analysis was performed with the AMDA science analysis system provided by the Centre de Données de la Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and Université Paul Sabatier, Toulouse". See the Rules of the road at https://amda.cdpp.eu/help/policy.html . Please acknowledge the Data Providers.</Acknowledgement>
</AccessInformation>
<AccessInformation>
<RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
<Availability>Online</Availability>
<AccessRights>Open</AccessRights>
<AccessURL>
<Name>CDPP/AMDA Web application</Name>
<URL>https://amda.cdpp.eu</URL>
<Description>Access to Data via CDPP/AMDA Web application.</Description>
</AccessURL>
<Format>CSV</Format>
<Format>VOTable</Format>
<Format>CDF</Format>
<Format>PNG</Format>
<Acknowledgement>Thank you for acknowledging the use of AMDA in publications with wording like "Data analysis was performed with the AMDA science analysis system provided by the Centre de Données de la Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and Université Paul Sabatier, Toulouse". See the Rules of the road at https://amda.cdpp.eu/help/policy.html . Please acknowledge the Data Providers.</Acknowledgement>
</AccessInformation>
<ProviderName>CDAWeb</ProviderName>
<InstrumentID>spase://CNES/Instrument/CDPP-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.ephem;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.ephem;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>