<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_0_1.xsd">
    <Version>2.2.2</Version>
    <NumericalData>
        <ResourceID>spase://VMO/NumericalData/Cluster/Ephemeris/SummaryParameter/PT1M</ResourceID>
        <ResourceHeader>
            <ResourceName>Cluster Auxiliary Data</ResourceName>
            <ReleaseDate>2011-02-04T15:51:43Z</ReleaseDate>
            <Description>Cluster Auxiliary Parameters are produced by the Cluster Hungarian Data Center in Budapest.  These data are the primary orbit product supplied to users by the Cluster Active Archive.  The data contain Position, Velocity and Attitude of four Cluster spacecraft.

            For additional details on the methodology behind these data see:

            Robert P., et al., "Tetrahedron Geometric Factors", p. 328, Analysis Methods of Multi-Spacecraft Data, ed. G. Paschmann and P. Daly, 1998, ESA and the International Space Institute, Bern.</Description>
            <Contact>
                <PersonID>spase://SMWG/Person/M.Tatrallyay</PersonID>
                <Role>DataProducer</Role>
            </Contact>
            <PriorID>spase://VMO/NumericalData/Cluster2/Ephemeris/PT1M</PriorID>
            <PriorID>spase://VMO/NumericalData/Cluster2/Ephemeris/SummaryParameter/PT1M</PriorID>
        </ResourceHeader>
        <AccessInformation>
            <RepositoryID>spase://SMWG/Repository/NASA/GSFC/SPDF/CDAWeb</RepositoryID>
            <AccessURL>
                <Name>FTP access to files at SPDF</Name>
                <URL>ftp://spdf.gsfc.nasa.gov/pub/data/cluster/cl/sp/aux</URL>
            </AccessURL>
            <AccessURL>
                <Name>HTTP access to files at SPDF</Name>
                <URL>http://spdf.gsfc.nasa.gov/pub/data/cluster/cl/sp/aux</URL>
                <Description>In CDF via HTTP from SPDF</Description>
            </AccessURL>
            <AccessURL>
                <Name>CDAWeb</Name>
                <URL>http://cdaweb.gsfc.nasa.gov/</URL>
                <ProductKey>CL_SP_AUX</ProductKey>
            </AccessURL>
            <Format>CDF</Format>
        </AccessInformation>
        <InstrumentID>spase://SMWG/Instrument/Cluster-Rumba/Ephemeris</InstrumentID>
        <InstrumentID>spase://SMWG/Instrument/Cluster-Salsa/Ephemeris</InstrumentID>
        <InstrumentID>spase://SMWG/Instrument/Cluster-Samba/Ephemeris</InstrumentID>
        <InstrumentID>spase://SMWG/Instrument/Cluster-Tango/Ephemeris</InstrumentID>
        <MeasurementType>Ephemeris</MeasurementType>
        <TemporalDescription>
            <TimeSpan>
                <StartDate>2000-08-22T00:00:30</StartDate>
                <RelativeStopDate>-P3M</RelativeStopDate>
            </TimeSpan>
            <Cadence>PT1M</Cadence>
        </TemporalDescription>
        <ObservedRegion>Earth.Magnetosheath</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere.Magnetotail</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere.Main</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere.Polar</ObservedRegion>
        <ObservedRegion>Earth.Magnetosphere.RadiationBelt</ObservedRegion>
        <ObservedRegion>Earth.NearSurface.AuroralRegion</ObservedRegion>
        <ObservedRegion>Earth.NearSurface.Ionosphere</ObservedRegion>
        <ObservedRegion>Earth.NearSurface.Plasmasphere</ObservedRegion>
        <ObservedRegion>Earth.NearSurface.PolarCap</ObservedRegion>
        <ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
        <Parameter>
            <Name>Epoch</Name>
            <ParameterKey>Epoch__CL_SP_AUX</ParameterKey>
            <Description>Interval centered time tag rounded to the nearest millisecond</Description>
            <Units>ms</Units>
            <UnitsConversion>1.0e-3&gt;s</UnitsConversion>
            <ValidMin>6.2924602e13</ValidMin>
            <ValidMax>6.34295223e13</ValidMax>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft Status</Name>
            <ParameterKey>sc_status__CL_SP_AUX</ParameterKey>
            <Description>Spacecraft Status, 0 = Bad Value, 1 = Use with caution, 2 = OK, 255 = Not Supplied</Description>
            <Cadence>PT1M</Cadence>
            <Structure>
                <Size>5</Size>
            </Structure>
            <ValidMin>0</ValidMin>
            <ValidMax>255</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft Orbit Number</Name>
            <ParameterKey>sc_orbit_num__CL_SP_AUX</ParameterKey>
            <Description>Spacecraft orbit number including phase. Values are of the form orbit.phase</Description>
            <Cadence>PT1M</Cadence>
            <ValidMin>0</ValidMin>
            <ValidMax>1000</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Reference Spacecraft Position GSE</Name>
            <ParameterKey>sc_r_xyz_gse__CL_SP_AUX</ParameterKey>
            <Description>Position, in GSE, of the Reference Spacecraft. Cluster 3 is used as the reference spacecraft</Description>
            <Cadence>PT1M</Cadence>
            <Units>km</Units>
            <UnitsConversion>1.0e3&gt;m</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>GSE X</Name>
                    <Index>0</Index>
                    <ValidMin>-140000</ValidMin>
                    <ValidMax>140000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Y</Name>
                    <Index>1</Index>
                    <ValidMin>-140000</ValidMin>
                    <ValidMax>140000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Z</Name>
                    <Index>2</Index>
                    <ValidMin>-140000</ValidMin>
                    <ValidMax>140000</ValidMax>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Reference Spacecraft Velocity GSE</Name>
            <ParameterKey>sc_v_xyz_gse__CL_SP_AUX</ParameterKey>
            <Description>Velocity, in GSE, of the Reference Spacecraft. Cluster 3 is used as the reference spacecraft</Description>
            <Cadence>PT1M</Cadence>
            <Units>km/s</Units>
            <UnitsConversion>1.0e3&gt;m s^-1</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>GSE X</Name>
                    <Index>0</Index>
                    <ValidMin>-10</ValidMin>
                    <ValidMax>10</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Y</Name>
                    <Index>1</Index>
                    <ValidMin>-10</ValidMin>
                    <ValidMax>10</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Z</Name>
                    <Index>2</Index>
                    <ValidMin>-10</ValidMin>
                    <ValidMax>10</ValidMax>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Velocity</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 1 Position Relative to Reference Spacecraft</Name>
            <ParameterKey>sc_dr1_xyz_gse__CL_SP_AUX</ParameterKey>
            <Description>Offset, in GSE, of Spacecraft 1 from the reference spacecraft. Cluster 3 is used as the reference spacecraft</Description>
            <Cadence>PT1M</Cadence>
            <Units>km</Units>
            <UnitsConversion>1.0e3&gt;m</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>GSE X</Name>
                    <Index>0</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Y</Name>
                    <Index>1</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Z</Name>
                    <Index>2</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 2 Position Relative to Reference Spacecraft</Name>
            <ParameterKey>sc_dr2_xyz_gse__CL_SP_AUX</ParameterKey>
            <Description>Offset, in GSE, of Spacecraft 2 from the reference spacecraft. Cluster 3 is used as the reference spacecraft</Description>
            <Cadence>PT1M</Cadence>
            <Units>km</Units>
            <UnitsConversion>1.0e3&gt;m</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>GSE X</Name>
                    <Index>0</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Y</Name>
                    <Index>1</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Z</Name>
                    <Index>2</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 3 Position Relative to Reference Spacecraft</Name>
            <ParameterKey>sc_dr3_xyz_gse__CL_SP_AUX</ParameterKey>
            <Description>Offset, in GSE, of Spacecraft 3 from the reference spacecraft. Cluster 3 is used as the reference spacecraft</Description>
            <Cadence>PT1M</Cadence>
            <Units>km</Units>
            <UnitsConversion>1.0e3&gt;m</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>GSE X</Name>
                    <Index>0</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Y</Name>
                    <Index>1</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Z</Name>
                    <Index>2</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 4 Position Relative to Reference Spacecraft</Name>
            <ParameterKey>sc_dr4_xyz_gse__CL_SP_AUX</ParameterKey>
            <Description>Offset, in GSE, of Spacecraft 4 from the reference spacecraft. Cluster 3 is used as the reference spacecraft</Description>
            <Cadence>PT1M</Cadence>
            <Units>km</Units>
            <UnitsConversion>1.0e3&gt;m</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>GSE X</Name>
                    <Index>0</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Y</Name>
                    <Index>1</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
                <Element>
                    <Name>GSE Z</Name>
                    <Index>2</Index>
                    <ValidMin>-100000</ValidMin>
                    <ValidMax>100000</ValidMax>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 1 Axis Latitude GSE</Name>
            <ParameterKey>sc_at1_lat__CL_SP_AUX</ParameterKey>
            <Description>GSE latitude of spacecraft 1 axis, angle from Ecliptic Plane</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1.0&gt;degrees</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <ValidMin>-90</ValidMin>
            <ValidMax>90</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 1 Axis Longitude GSE</Name>
            <ParameterKey>sc_at1_long__CL_SP_AUX</ParameterKey>
            <Description>GSE longitude of spacecraft 1 axis, angle from x in x-y GSE plane</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1.0&gt;degrees</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <ValidMin>0</ValidMin>
            <ValidMax>360</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 2 Axis Latitude GSE</Name>
            <ParameterKey>sc_at2_lat__CL_SP_AUX</ParameterKey>
            <Description>GSE latitude of spacecraft 2 axis, angle from Ecliptic Plane</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1.0&gt;degrees</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <ValidMin>-90</ValidMin>
            <ValidMax>90</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 2 Axis Longitude GSE</Name>
            <ParameterKey>sc_at2_long__CL_SP_AUX</ParameterKey>
            <Description>GSE longitude of spacecraft 2 axis, angle from x in x-y GSE plane</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1.0&gt;degrees</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <ValidMin>0</ValidMin>
            <ValidMax>360</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 3 Axis Latitude GSE</Name>
            <ParameterKey>sc_at3_lat__CL_SP_AUX</ParameterKey>
            <Description>GSE latitude of spacecraft 3 axis, angle from Ecliptic Plane</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1.0&gt;degrees</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <ValidMin>-90</ValidMin>
            <ValidMax>90</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 3 Axis Longitude GSE</Name>
            <ParameterKey>sc_at3_long__CL_SP_AUX</ParameterKey>
            <Description>GSE longitude of spacecraft 3 axis, angle from x in x-y GSE plane</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1.0&gt;degrees</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <ValidMin>0</ValidMin>
            <ValidMax>360</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 4 Axis Latitude GSE</Name>
            <ParameterKey>sc_at4_lat__CL_SP_AUX</ParameterKey>
            <Description>GSE latitude of spacecraft 4 axis, angle from Ecliptic Plane</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1.0&gt;degrees</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <ValidMin>-90</ValidMin>
            <ValidMax>90</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft 4 Axis Longitude GSE</Name>
            <ParameterKey>sc_at4_long__CL_SP_AUX</ParameterKey>
            <Description>GSE longitude of spacecraft 4 axis, angle from x in x-y GSE plane</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1.0&gt;degrees</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <ValidMin>0</ValidMin>
            <ValidMax>360</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Tetrahedron Quality G</Name>
            <ParameterKey>sc_config_QG__CL_SP_AUX</ParameterKey>
            <Description>Spacecraft Quality Shape, (vol/ideal) + (surf/ideal) + 1</Description>
            <Cadence>PT1M</Cadence>
            <ValidMin>1</ValidMin>
            <ValidMax>3</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Tetrahedron Quality R</Name>
            <ParameterKey>sc_config_QR__CL_SP_AUX</ParameterKey>
            <Description>Spacecraft Quality Shape, norm*(vol/sphere vol)^(1/3)</Description>
            <Cadence>PT1M</Cadence>
            <ValidMin>0</ValidMin>
            <ValidMax>1</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Minimum Distance Between Spacecraft</Name>
            <ParameterKey>sc_dr_min__CL_SP_AUX</ParameterKey>
            <Description>Minimum distance between spacecraft</Description>
            <Cadence>PT1M</Cadence>
            <Units>km</Units>
            <UnitsConversion>1e3&gt;m</UnitsConversion>
            <ValidMin>0</ValidMin>
            <ValidMax>1e7</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Maximum Distance Between Spacecraft</Name>
            <ParameterKey>sc_dr_max__CL_SP_AUX</ParameterKey>
            <Description>Maximum distance between spacecraft</Description>
            <Cadence>PT1M</Cadence>
            <Units>km</Units>
            <UnitsConversion>1e3&gt;m</UnitsConversion>
            <ValidMin>0</ValidMin>
            <ValidMax>1e7</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Rotation angle GSE to GSM</Name>
            <ParameterKey>gse_gsm__CL_SP_AUX</ParameterKey>
            <Description>Rotation angle GSE to GSM, positive from +z towards +y</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1&gt;degrees</UnitsConversion>
            <ValidMin>-90</ValidMin>
            <ValidMax>90</ValidMax>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Dipole tilt</Name>
            <ParameterKey>dipole_tilt__CL_SP_AUX</ParameterKey>
            <Description>Dipole tilt in GSM z-x plane, positive from +z towards +x</Description>
            <Cadence>PT1M</Cadence>
            <Units>degrees</Units>
            <UnitsConversion>1&gt;degrees</UnitsConversion>
            <ValidMin>-90</ValidMin>
            <ValidMax>90</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Tetrahedron size L</Name>
            <ParameterKey>sc_geom_size__CL_SP_AUX</ParameterKey>
            <Description>Tetrahedron size</Description>
            <Cadence>PT1M</Cadence>
            <Units>km</Units>
            <UnitsConversion>1e3&gt;m</UnitsConversion>
            <ValidMin>0</ValidMin>
            <ValidMax>1e7</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Tetrahedron Elongation</Name>
            <ParameterKey>sc_geom_elong__CL_SP_AUX</ParameterKey>
            <Description>Tetrahedron elongation</Description>
            <Cadence>PT1M</Cadence>
            <ValidMin>0</ValidMin>
            <ValidMax>1</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Tetrahedron Planarity</Name>
            <ParameterKey>sc_geom_planarity__CL_SP_AUX</ParameterKey>
            <Description>Tetrahedron planarity</Description>
            <Cadence>PT1M</Cadence>
            <ValidMin>0</ValidMin>
            <ValidMax>1</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Direction of elongation</Name>
            <ParameterKey>sc_geom_E_dir_gse__CL_SP_AUX</ParameterKey>
            <Description>direction of elongation, direction cosines</Description>
            <Cadence>PT1M</Cadence>
            <Structure>
                <Size>3</Size>
            </Structure>
            <ValidMin>-1</ValidMin>
            <ValidMax>1</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Normal of Planarity</Name>
            <ParameterKey>sc_geom_P_nor_gse__CL_SP_AUX</ParameterKey>
            <Description>normal of planarity, direction cosines</Description>
            <Cadence>PT1M</Cadence>
            <Structure>
                <Size>3</Size>
            </Structure>
            <ValidMin>-1</ValidMin>
            <ValidMax>1</ValidMax>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
    </NumericalData>
</Spase>