<?xml version="1.0" encoding="UTF-8"?>
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  <Version>2.3.0</Version>
  <NumericalData>
    <ResourceID>spase://NOAA/NumericalData/GOES/9/MAG/PT1M</ResourceID>
    <ResourceHeader>
      <ResourceName>GOES 9 Space Environment Monitor (SEM) Triaxial Fluxgate Magnetometer (FGM), Magnetic Field and Ephemeris, Multiple Coordinate Systems, 1.0 min Data</ResourceName>
      <ReleaseDate>2021-04-27T17:52:57Z</ReleaseDate>
      <Description>The NOAA Geostationary Operational Environment Satellite (GOES) key parameters.  This data is a subset of the data available from the GOES Space Environment Monitor (SEM) instruments.  It contains vector magnetic field in three coordinate systems:

* Spacecraft P,E,N
* GSM X,Y,Z
* GSE X,Y,Z

Spacecraft magnetic field is defined as:

* P perpendicular to the spacecraft orbital plane or parallel to the spin axis of the Earth in the case of a 0° inclination orbit
* E perpendicular to P and directed earthward
* N perpendicular to both P and E and directed eastward</Description>
      <Acknowledgement>Users should acknowledge the CDAWeb for providing access to the data as well as the P.I. H. Singer and originating institution NOAA Space Environment Center</Acknowledgement>
      <Contact>
        <PersonID>spase://SMWG/Person/Howard.J.Singer</PersonID>
        <Role>PrincipalInvestigator</Role>
      </Contact>
      <InformationURL>
        <Name>Geostationary Satellite Server</Name>
        <URL>https://www.goes.noaa.gov/</URL>
        <Description>A web site hosted by NOAA with information and links to the GOES spacecraft and data</Description>
      </InformationURL>
      <PriorID>spase://VMO/NumericalData/GOES9/MAG/PT1M</PriorID>
      <PriorID>spase://VMO/NumericalData/GOES/9/MAG/PT1M</PriorID>
      <PriorID>spase://VSPO/NumericalData/GOES/9/MAG/PT60S</PriorID>
      <PriorID>spase://VSPO/NumericalData/GOES/9/MAG/PT1M</PriorID>
    </ResourceHeader>
    <AccessInformation>
      <RepositoryID>spase://SMWG/Repository/NASA/GSFC/SPDF</RepositoryID>
      <Availability>Online</Availability>
      <AccessRights>Open</AccessRights>
      <AccessURL>
        <Name>FTPS from SPDF (not with most browsers)</Name>
        <URL>ftps://spdf.gsfc.nasa.gov/pub/data/goes/goes09/mag_k0/</URL>
      </AccessURL>
      <AccessURL>
        <Name>HTTPS from SPDF</Name>
        <URL>https://spdf.gsfc.nasa.gov/pub/data/goes/goes09/mag_k0/</URL>
        <Description>In CDF via HTTP from CDAWeb</Description>
      </AccessURL>
      <AccessURL>
        <Name>CDAWeb</Name>
        <URL>https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=G9_K0_MAG&amp;index=sp_phys</URL>
        <ProductKey>G9_K0_MAG</ProductKey>
      </AccessURL>
      <Format>CDF</Format>
    </AccessInformation>
    <AccessInformation>
      <RepositoryID>spase://SMWG/Repository/NASA/GSFC/SPDF</RepositoryID>
      <Availability>Online</Availability>
      <AccessRights>Open</AccessRights>
      <AccessURL>
        <Name>CDAWeb HAPI Server</Name>
        <URL>https://cdaweb.gsfc.nasa.gov/hapi</URL>
        <Style>HAPI</Style>
        <ProductKey>G9_K0_MAG</ProductKey>
        <Description>Web Service to this product using the HAPI interface.</Description>
      </AccessURL>
      <Format>CSV</Format>
    </AccessInformation>
    <ProviderResourceName>NOAA GOES 9</ProviderResourceName>
    <ProviderProcessingLevel>Level-2</ProviderProcessingLevel>
    <ProviderVersion>4</ProviderVersion>
    <InstrumentID>spase://SMWG/Instrument/GOES/9/MAG</InstrumentID>
    <InstrumentID>spase://SMWG/Instrument/GOES/9/Ephemeris</InstrumentID>
    <MeasurementType>MagneticField</MeasurementType>
    <MeasurementType>Ephemeris</MeasurementType>
    <TemporalDescription>
      <TimeSpan>
        <StartDate>1995-12-01T00:00:30</StartDate>
        <StopDate>1998-07-27T23:59:30</StopDate>
      </TimeSpan>
      <Cadence>PT1M</Cadence>
    </TemporalDescription>
    <ObservedRegion>Earth.Magnetosphere</ObservedRegion>
    <Keyword>Magnetic field</Keyword>
    <Parameter>
      <Name>Epoch</Name>
      <ParameterKey>Epoch</ParameterKey>
      <Description>Epoch of the data point</Description>
      <Cadence>PT1M</Cadence>
      <Units>ms</Units>
      <ValidMin>1977-01-01T00:00:00</ValidMin>
      <ValidMax>2010-12-31T23:59:59</ValidMax>
      <FillValue>-1.0e+31</FillValue>
      <Support>
        <SupportQuantity>Temporal</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Time PB5</Name>
      <ParameterKey>Time_PB5</ParameterKey>
      <Description>Time array in the form: year, day of year, ms</Description>
      <Cadence>PT1M</Cadence>
      <ValidMin>1977-01-01T00:00:00</ValidMin>
      <ValidMax>2010-12-31T23:59:59</ValidMax>
      <FillValue>-2147483648</FillValue>
      <Support>
        <SupportQuantity>Temporal</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Magnetic Field Vector GSE</Name>
      <ParameterKey>B_GSE_c</ParameterKey>
      <Description>Magnetic Field vector in GSE coordinates</Description>
      <Cadence>PT1M</Cadence>
      <Units>nT</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GSE</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>X, GSE</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>1</Index>
        </Element>
        <Element>
          <Name>Y, GSE</Name>
          <Qualifier>Component.J</Qualifier>
          <Index>2</Index>
        </Element>
        <Element>
          <Name>Z, GSE</Name>
          <Qualifier>Component.K</Qualifier>
          <Index>3</Index>
        </Element>
      </Structure>
      <ValidMin>-600.0</ValidMin>
      <ValidMax>600.0</ValidMax>
      <FillValue>-1.0e+31</FillValue>
      <Field>
        <Qualifier>Vector</Qualifier>
        <FieldQuantity>Magnetic</FieldQuantity>
      </Field>
    </Parameter>
    <Parameter>
      <Name>Magnetic Field vector GSM</Name>
      <ParameterKey>B_GSM_c</ParameterKey>
      <Description>Magnetic Field vector in GSM coordinates</Description>
      <Cadence>PT1M</Cadence>
      <Units>nT</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GSM</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>X, GSM</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>1</Index>
        </Element>
        <Element>
          <Name>Y, GSM</Name>
          <Qualifier>Component.J</Qualifier>
          <Index>2</Index>
        </Element>
        <Element>
          <Name>Z, GSM</Name>
          <Qualifier>Component.K</Qualifier>
          <Index>3</Index>
        </Element>
      </Structure>
      <ValidMin>-600.0</ValidMin>
      <ValidMax>600.0</ValidMax>
      <FillValue>-1.0e+31</FillValue>
      <Field>
        <Qualifier>Vector</Qualifier>
        <FieldQuantity>Magnetic</FieldQuantity>
      </Field>
    </Parameter>
    <Parameter>
      <Name>Magnetic Field vector spacecraft coordinates</Name>
      <ParameterKey>B_lcl_c</ParameterKey>
      <Description>Magnetic Field vector in spacecraft coordinates. Spacecraft magnetic field (P,E,N) is defined as:

* P perpendicular to the spacecraft orbital plane or parallel to the spin axis of the Earth in the case of a 0° inclination orbit
* E perpendicular to P and directed earthward
* N perpendicular to both P and E and directed eastward</Description>
      <Cadence>PT1M</Cadence>
      <Units>nT</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>SpacecraftOrbitPlane</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>P</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>1</Index>
        </Element>
        <Element>
          <Name>E</Name>
          <Qualifier>Component.J</Qualifier>
          <Index>2</Index>
        </Element>
        <Element>
          <Name>N</Name>
          <Qualifier>Component.K</Qualifier>
          <Index>3</Index>
        </Element>
      </Structure>
      <ValidMin>-600.0</ValidMin>
      <ValidMax>600.0</ValidMax>
      <FillValue>-1.0e+31</FillValue>
      <Field>
        <Qualifier>Vector</Qualifier>
        <FieldQuantity>Magnetic</FieldQuantity>
      </Field>
    </Parameter>
    <Parameter>
      <Name>Spacecraft Position Geographic</Name>
      <ParameterKey>SC_pos_ll</ParameterKey>
      <Description>Spacecraft position in Geographic coordinates</Description>
      <Cadence>PT1M</Cadence>
      <CoordinateSystem>
        <CoordinateRepresentation>Spherical</CoordinateRepresentation>
        <CoordinateSystemName>GEO</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>Latitude</Name>
          <Qualifier>DirectionAngle.ElevationAngle</Qualifier>
          <Index>1</Index>
          <Units>°</Units>
          <ValidMin>-90</ValidMin>
          <ValidMax>90</ValidMax>
        </Element>
        <Element>
          <Name>Longitude</Name>
          <Qualifier>DirectionAngle.AzimuthAngle</Qualifier>
          <Index>2</Index>
          <Units>°</Units>
          <ValidMin>0</ValidMin>
          <ValidMax>360</ValidMax>
        </Element>
        <Element>
          <Name>Radius</Name>
          <Qualifier>Magnitude</Qualifier>
          <Index>3</Index>
          <Units>km</Units>
          <ValidMin>50</ValidMin>
          <ValidMax>50000</ValidMax>
        </Element>
      </Structure>
      <FillValue>-1.0e+31</FillValue>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Spacecraft position GEO</Name>
      <ParameterKey>SC_pos_eo</ParameterKey>
      <Description>Spacecraft position in GEO coordinates</Description>
      <Cadence>PT1M</Cadence>
      <Units>km</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GEO</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>X, GEO</Name>
          <Qualifier>Component.I</Qualifier>
          <Index>1</Index>
        </Element>
        <Element>
          <Name>Y, GEO</Name>
          <Qualifier>Component.J</Qualifier>
          <Index>2</Index>
        </Element>
        <Element>
          <Name>Z, GEO</Name>
          <Qualifier>Component.K</Qualifier>
          <Index>3</Index>
        </Element>
      </Structure>
      <ValidMin>-5000.0</ValidMin>
      <ValidMax>5000.0</ValidMax>
      <FillValue>-1.0e+31</FillValue>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Spacecraft Position GSE</Name>
      <ParameterKey>SC_pos_se</ParameterKey>
      <Description>Spacecraft position in GSE coordinates</Description>
      <Cadence>PT1M</Cadence>
      <Units>km</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GSE</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>GSE X</Name>
          <Index>1</Index>
        </Element>
        <Element>
          <Name>GSE Y</Name>
          <Index>2</Index>
        </Element>
        <Element>
          <Name>GSE Z</Name>
          <Index>3</Index>
        </Element>
      </Structure>
      <ValidMin>-5000.0</ValidMin>
      <ValidMax>5000.0</ValidMax>
      <FillValue>-1.0e+31</FillValue>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Spacecraft position GSM</Name>
      <ParameterKey>SC_pos_sm</ParameterKey>
      <Description>Spacecraft position in GSM coordinates</Description>
      <Cadence>PT1M</Cadence>
      <Units>km</Units>
      <CoordinateSystem>
        <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
        <CoordinateSystemName>GSM</CoordinateSystemName>
      </CoordinateSystem>
      <Structure>
        <Size>3</Size>
        <Element>
          <Name>X, GSM</Name>
          <Index>1</Index>
        </Element>
        <Element>
          <Name>Y, GSM</Name>
          <Index>2</Index>
        </Element>
        <Element>
          <Name>Z, GSM</Name>
          <Qualifier>Component.K</Qualifier>
          <Index>3</Index>
        </Element>
      </Structure>
      <ValidMin>-5000.0</ValidMin>
      <ValidMax>5000.0</ValidMax>
      <FillValue>-1.0e+31</FillValue>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>MGF Instrument Status</Name>
      <ParameterKey>MGF_stat</ParameterKey>
      <Description>Status of the magnetic field instrument:

* 0 OK
* 1 minor problem
* 2 major problem
* 3 missing data</Description>
      <Cadence>PT1M</Cadence>
      <Support>
        <SupportQuantity>Other</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Magnetic field post-gap flag</Name>
      <ParameterKey>B_flag</ParameterKey>
      <Description>Magnetic field data flag:

* 0 no gap
* 1 data not available</Description>
      <Cadence>PT1M</Cadence>
      <Support>
        <SupportQuantity>Other</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>Spacecraft post-gap flag</Name>
      <ParameterKey>SC_flag</ParameterKey>
      <Description>Spacecraft location data flag:

* 0 no gap
* 1 data not available</Description>
      <Cadence>PT1M</Cadence>
      <Support>
        <SupportQuantity>Other</SupportQuantity>
      </Support>
    </Parameter>
  </NumericalData>
</Spase>
