2.0.1 spase://VMO/NumericalData/GOES/9/MAG/PT1M GOES 9 Magnetometer 1-Minute Data 2011-07-19T21:41:00Z 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: * (1) Spacecraft P,E,N * (2) GSM x,y,z and * (3) GSE x,y,z. Spacecraft magnetic field is defined as: * P - perpendicular to the spacecraft orbital plane or parallel to the Earth's spin axis in the case of a zero degree inclination orbit; * E - perpendicular to P and directed earhtwards; and * N - perpendicular to both P and E and directed eastwards. Users should acknowledge the CDAWeb for providing access to the data as well as the PI H. Singer and originating institution NOAA Space Environment Center spase://SMWG/Person/Howard.J.Singer PrincipalInvestigator Geostationary Satellite Server http://www.goes.noaa.gov/ A web site hosted by NOAA with information and links to the GOES spacecraft and data spase://VMO/NumericalData/GOES9/MAG/PT1M spase://SMWG/Repository/NASA/GSFC/SPDF/CDAWeb Online Open 1-minute GOES 9 MAG data at CDAWeb ftp://cdaweb.gsfc.nasa.gov/pub/data/goes/goes09/mag_k0 An ftp repository hosting 1-minute GOES 9 MAG data CDF None GOES_9 Level 2 4 spase://SMWG/Instrument/GOES/9/MAG spase://SMWG/Instrument/GOES/9/Ephemeris MagneticField Ephemeris 1995-12-01T00:00:30 1998-07-27T23:59:30 PT1M Earth.Magnetosphere Magnetic field Epoch Epoch Epoch of the data point PT1M Milliseconds 01-Jan-1977 00:00:00.000 31-Dec-2010 00:00:00.000 -1.0e+31 Temporal Time PB5 Time_PB5 Time array in the form [year, day of year, millisecond] PT1M 01-Jan-1977 00:00:00.000 31-Dec-2010 00:00:00.000 -2147483648 Temporal Magnetic Field Vector GSE B_GSE_c Magnetic Field vector in GSE coordinates PT1M nT Cartesian GSE Xgse Component.I 1 Ygse Component.J 2 Zgse Component.K 3 -600.00 600.00 -1.0e+31 Vector Magnetic Magnetic Field vector GSM B_GSM_c Magnetic Field vector in GSM coordinates PT1M nT Cartesian GSM Xgsm Component.I 1 Ygsm Component.J 2 Zgsm Component.K 3 -600.0 600.0 -1.0e+31 Vector Magnetic Magnetic Field vector spacecraft coordinates B_lcl_c 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 Earth's spin axis in the case of a zero degree inclination orbit; * E - perpendicular to P and directed earhtwards; and * N - perpendicular to both P and E and directed eastwards. PT1M nT Cartesian SpacecraftOrbitPlane P Component.I 1 E Component.J 2 N Component.K 3 -600.0 600.0 -1.0e+31 Vector Magnetic Spacecraft Position Geographic SC_pos_ll Spacecraft position in Geographic coordinates PT1M [degrees,degrees,km] Spherical GEO Latitude DirectionAngle.ElevationAngle 1 degrees -90 90 Longitude DirectionAngle.AzimuthAngle 2 degrees 0 360 Radius Magnitude 3 km 50 50000 -1.0e+31 Positional Spacecraft position GEO SC_pos_eo Spacecraft position in GEO coordinates PT1M km Cartesian GEO X GEO Component.I 1 Y GEO Component.J 2 Z GEO Component.K 3 -5000.0 5000.0 -1.0e+31 Positional Spacecraft Position GSE SC_pos_se Spacecraft position in GSE coordinates PT1M km Cartesian GSE GSE X 1 GSE Y 2 GSE Z 3 -5000.0 5000.0 -1.0e+31 Positional Spacecraft position GSM SC_pos_sm Spacecraft position in GSM coordinates PT1M km Cartesian GSM X GSM 1 Y GSM 2 Z GSM Component.K 3 -5000.0 5000.0 -1.0e+31 Positional MGF Instrument Status MGF_stat Status of the magnetic field instrument: * 0 = ok, * 1 = minor problem, * 2 = major problem, * 3 = missing data. PT1M Other Mag post-gap flag B_flag Magnetic field data flag: * 0 = no gap, * 1 = data not available PT1M Other Spacecraft post-gap flag SC_flag Spacecraft location data flag: * 0 = no gap, * 1 = data not available PT1M Other