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NumericalData/AMDA/INTERBALL-Tail/Ephemeris/intt-orb-all.xml 6.99 KB
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<?xml version="1.0" encoding="UTF-8"?>
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<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">
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    <Version>2.2.6</Version>
    <NumericalData>
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        <ResourceID>spase://CDPP/NumericalData/AMDA/INTERBALL-Tail/Ephemeris/intt-orb-all</ResourceID>
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        <ResourceHeader>
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            <ResourceName>orbit</ResourceName>
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            <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>
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            </Contact>
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            <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>
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        <InstrumentID>spase://CDPP/Instrument/AMDA/Interball-1/Ephemeris</InstrumentID>
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        <MeasurementType>Ephemeris</MeasurementType>
        <TemporalDescription>
            <TimeSpan>
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                <StartDate>1995-08-04T00:01:00Z</StartDate>
                <StopDate>2000-10-16T13:55:00Z</StopDate>
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            </TimeSpan>
            <Cadence>PT2M</Cadence>
        </TemporalDescription>
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        <ObservedRegion>Earth.Magnetosphere</ObservedRegion>       
        <ObservedRegion>Earth.Magnetosheath</ObservedRegion>
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        <ObservedRegion>Earth.Magnetosphere.Main</ObservedRegion>
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        <ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
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        <Caveats>The data cadence varies</Caveats>
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        <Parameter>
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            <Name>xyz_gse</Name>
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            <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&gt;m</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
                <ValueFormat>F7.3</ValueFormat>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Element>
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                    <Name>x</Name>
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                    <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>
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                    <Name>y</Name>
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                    <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>
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                    <Name>z</Name>
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                    <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>
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            <Name>xyz_gsm</Name>
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            <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&gt;m</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSM</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
                <ValueFormat>F7.3</ValueFormat>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Element>
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                    <Name>x</Name>
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                    <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>
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                    <Name>y</Name>
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                    <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>
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                    <Name>z</Name>
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                    <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>