ace-orb-all.xml 10 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://amda.irap.omp.eu/public/schemas/spase-2_3_1.xsd">
    <Version>2.3.1</Version>
    <NumericalData>
        <ResourceID>spase://CNES/NumericalData/CDPP-AMDA/ACE/Ephemeris/ace-orb-all</ResourceID>
        <ResourceHeader>
            <ResourceName>orbit L1</ResourceName>
            <AlternateName>orbit L1 libration point</AlternateName>
            <ReleaseDate>2015-10-12T10:46:00</ReleaseDate>
            <Description>ACE orbits the L1 libration point which is a point of Earth-Sun gravitational equilibrium about 1.5 million km from 
                Earth and 148.5 million km from the Sun</Description>                      
        </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.ASCII</Format>
        </AccessInformation>
        <ProviderName>CDAWeb/SSCWeb</ProviderName>
        <InstrumentID>spase://CNES/Instrument/CDPP-AMDA/ACE/Ephemeris</InstrumentID>
        <MeasurementType>Ephemeris</MeasurementType>
        <TemporalDescription>
            <TimeSpan>
                <StartDate>1997-08-26T00:00:00Z</StartDate>
                <StopDate>2018-12-31T23:59:00Z</StopDate>
            </TimeSpan>
            <Cadence>PT12M</Cadence>
         </TemporalDescription>            
        <Parameter>
            <Name>xyz_gse</Name>
            <ParameterKey>ace_xyz_gse</ParameterKey>
            <Description>Spacecraft position in GSE</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</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ParameterKey>ace_xyz_gse(0)</ParameterKey>
                    <ValidMin>-1594535.0</ValidMin>
                    <ValidMax>1594535.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>y</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>ace_xyz_gse(1)</ParameterKey>
                    <ValidMin>-1594535.0</ValidMin>
                    <ValidMax>1594535.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>z</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>ace_xyz_gse(2)</ParameterKey>
                    <ValidMin>-1594535.0</ValidMin>
                    <ValidMax>1594535.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>xyz_gsm</Name>
            <ParameterKey>ace_xyz_gsm</ParameterKey>
            <Description>Spacecraft position in GSM</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</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ParameterKey>ace_xyz_gsm(0)</ParameterKey>
                    <ValidMin>-1594535.0</ValidMin>
                    <ValidMax>1594535.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>y</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>ace_xyz_gsm(1)</ParameterKey>
                    <ValidMin>-1594535.0</ValidMin>
                    <ValidMax>1594535.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>z</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>ace_xyz_gsm(2)</ParameterKey>
                    <ValidMin>-1594535.0</ValidMin>
                    <ValidMax>1594535.0</ValidMax>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
       <Parameter>
            <Name>xyz_hci</Name>
            <ParameterKey>ace_xyz_hci</ParameterKey>
            <Description>Spacecraft position in HCI</Description>
            <Ucd/>
            <Units>AU</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>HCI</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>x</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ParameterKey>ace_xyz_hci(0)</ParameterKey>
                    <ValidMin/>
                    <ValidMax/>
                    <FillValue/>
                 </Element>   
                <Element>
                    <Name>y</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>ace_xyz_hci(1)</ParameterKey>
                    <ValidMin/>
                    <ValidMax/>
                    <FillValue/>
                </Element>
                <Element>
                    <Name>z</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>ace_xyz_hci(2)</ParameterKey>
                    <ValidMin/>
                    <ValidMax/>
                    <FillValue/>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
    </Parameter>
    <Parameter>
            <Name>xyz_hee</Name>
            <ParameterKey>ace_xyz_hee</ParameterKey>
            <Description>Spacecraft position in HEE</Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Units>AU</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>HEE</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>x</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ParameterKey>ace_xyz_hee(0)</ParameterKey>
                </Element>
                <Element>
                    <Name>y</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>ace_xyz_hee(1)</ParameterKey>
                </Element>
                <Element>
                    <Name>z</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>ace_xyz_hee(2)</ParameterKey>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
	 <Parameter>
            <Name>distance ace-earth</Name>
            <ParameterKey>ace_r</ParameterKey>
            <Units>Re</Units>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
         <Parameter>
            <Name>distance ace-sun</Name>
            <ParameterKey>ace_r_sun</ParameterKey>
            <Units>AU</Units>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
    	 <Parameter>
            <Name>lon hee</Name>
            <ParameterKey>ace_lon_hee</ParameterKey>
            <Units>deg</Units>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter> 
         <Parameter>
            <Name>lat hee</Name>
            <ParameterKey>ace_lat_hee</ParameterKey>
            <Units>deg</Units>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>  
    </NumericalData>
</Spase>