2.2.2 spase://VMO/NumericalData/ISEE1/MAG/PT1M ISEE 1 magnetometer 1-min data at CDAWeb 2011-06-09T00:00:00 This data set contains magnetic field component and magnitude averages every minute, with components given in spacecraft, GSE and GSM coordinates. Standard deviations in the averages are given, as are differences between the averages and model field vectors. Geocentric (GSE and GSM) spacecraft position information is given, as is ISEE1-ISEE2 separation vector information. ISEE 1 spin vector direction and ISEE 1 velocity vector information, relative to the Earth and to ISEE 2, are given. Miscellaneous other parameters are also given. Data are accessible as plots, lists and files from CDAWeb, and as CDF files from CDAWeb's ftp area. ISEE Magnetometer Team at UCLA/IGPP and the CDAWeb team at NASA/GSFC spase://SMWG/Person/Robert.J.Strangeway DataProducer UCLA-IGPP ISEE Magnetometer Interactive Data Server http://www-ssc.igpp.ucla.edu/forms/isee Data at 60-s and 4-s resolution are available for the entire ISEE mission (October 22, 1977 through September 25, 1987) and can be displayed either as a plot or an ASCII listing. The ISEE-1 and -2 magnetometer data server is provided by the Institute of Geophysics and Planetary Physics (IGPP) at UCLA, through a grant to Robert J. Strangeway from the NASA Space Physics Data System (SPDS). spase://SMWG/Repository/NASA/GSFC/SPDF Open FTP access to files at SPDF ftp://spdf.gsfc.nasa.gov/pub/data/isee/isee1/isee1_cdaweb/60sec_mfi/ ftp access to CDF files HTTP access to files at SPDF http://spdf.gsfc.nasa.gov/pub/data/isee/isee1/isee1_cdaweb/60sec_mfi/ In CDF via HTTP from SPDF CDF UCLA ISEE Magnetometer and GSFC CDAWeb teams spase://SMWG/Repository/NASA/GSFC/SPDF Open CDAWeb http://cdaweb.gsfc.nasa.gov/cdaweb/sp_phys ISEE1_60SEC_MFI Plots, lists and files from CDAWeb Text UCLA ISEE Magnetometer and GSFC CDAWeb teams spase://SMWG/Repository/UCLA/IGPP.ISEE.Magnetometer.Interactive.Data.Server Open ftp area at UCLA-IGPP ftp://igpp.ucla.edu/pub/data/isee/isee1.60s The folder contains 60-sec ISEE-1 magnetometter data in the IGPP flat file format. Detailed description of the IGPP flat file format can be found at http://www-ssc.igpp.ucla.edu/flatfile.txt. These files contain a subset of the parameters described below and available via CDAWeb. Specifcally, this subset is the Cartesian components of the magnetic field vector, in spacecraft coordinates. Binary UCLA-IGPP ISEE Magnetometer Interactive Data Server Calibrated spase://SMWG/Instrument/ISEE1/MAG MagneticField 1977-10-22T21:04:19 1987-09-25T16:10:30 PT1M Earth.Magnetosphere Earth.Magnetosheath Heliosphere.NearEarth Universal Time Epoch DD-MON-YY HH:MM:SS.SSS Temporal Magnetic Field Vector, SC Coordinates BX, BY, BZ Triaxial magnetic field vector in spacecraft coordinates (SC) PT1M nT 1.0E-9>T Cartesian SC 3 The three elements are BX, BY, BZ Vector Magnetic Magnetic Field Magnitude BTOT Magnetic field magnitude PT1M nT 1.0E-9>T Magnitude Magnetic Magnetic Field Vector, GSM Coordinates BX_GSM, BY_GSM, BZ_GSM Triaxial magnetic field vector in GSM coordinates PT1M nT 1.0E-9>T Cartesian GSM 3 The three elements are BX, BY, BZ Vector Magnetic Magnetic Field Vector, GSE Coordinates BX_GSE, BY_GSE, BZ_GSE Triaxial magnetic field vector in GSM coordinates PT1M nT 1.0E-9>T Cartesian GSE 3 The three elements are BX, BY, BZ Vector Magnetic Standard Deviations in field component averages SDX, SDY, SDZ Standard deviations in the field component averages in SC coordinates PT1M nT 1.0E-9>T Cartesian SC 3 The three elements are the standard deviations in BX, BY, BZ (SC coordinates) averages StandardDeviation Vector Magnetic Standard Deviations in field magnitude averages SDT Standard deviations in the field magnitude averages PT1M nT 1.0E-9>T StandardDeviation Magnitude Magnetic Composite Standard Deviations in field average SDC Difference between magnitudes of model internal field and observed field PT1M nT 1.0E-9>T StandardDeviation Magnetic Model internal field minus observed field, magnitudes BINT Difference between magnitudes of model internal field and observed field PT1M nT 1.0E-9>T Deviation Magnitude Magnetic Model internal field minus observed field, GSM components BXIM_GSM, BYIM_GSM, BZIM_GSM Difference between GSM components of model internal field and observed field PT1M nT 1.0E-9>T Cartesian GSM 3 GSM X,Y,Z components of model internal field vector minus observed field vector Deviation Component Magnetic Model internal plus external field minus observed field, magnitudes BINTEXT Difference between magnitudes of model internal plus external field and observed field PT1M nT 1.0E-9>T Deviation Magnitude Magnetic Model internal plus external field minus observed field, GSM components BXIE_GSM, BYIE_GSM, BZIE_GSM Difference between GSM components of model internal plus external field and observed field PT1M nT 1.0E-9>T Cartesian GSM 3 GSM X,Y,Z components of model internal plus external field vector minus observed field vector Deviation Component Magnetic Geocentric distance of spacecraft R Geocentric distance of spacecraft, in Earth radii PT1M Re Positional Spacecraft position vector, GSM X_GSM, Y_GSM, Z_GSM Spacecraft position vector, GSM Cartesian components, in Earth radii PT1M Re Cartesian GSM 3 GSM X,Y,Z components of spacecraft position vector Positional Spacecraft position vector, GSE X_GSE, Y_GSE, Z_GSE Spacecraft position vector, GSE Cartesian components, in Earth radii PT1M Re Cartesian GSE 3 GSE X,Y,Z components of spacecraft position vector Positional Z position of nominal Russell Brody neutral sheet, GSM ZNS_GSM Positional Dipole tilt angle TILT Positional L Shell parameter L Positional Local time Local_time Positional Magnetic latitude MLAT Positional Sun-Earth-Satellite angle SES Positional Clock angle PHI Clock angle from Y GSM axis, positive toward +Z GSM Positional Spacecraft spin period SPIN Positional GSM longitude of spin axis SLNG_GSM Positional GSM latitude of spin axis SLT_GSM Positional GSE longitude of spin axis SLNG_GSE Positional GSE latitude of spin axis SLT_GSE Positional GSM X component of spacecraft velocity VX_GSM Positional GSM Y component of spacecraft velocity VY_GSM Positional GSM Z component of spacecraft velocity VZ_GSM Positional Spacecraft speed V Positional GSM X component of ISEE 1 velocity relative to ISEE 2 DVX_GSM Positional GSM Y component of ISEE 1 velocity relative to ISEE 2 DVY_GSM Positional GSM Z component of ISEE 1 velocity relative to ISEE 2 DVZ_GSM Positional ISEE 1 speed relative to ISEE 2 DV Positional GSM X separation of ISEE 2 to ISEE 1 DX_GSM Positional GSM Y separation of ISEE 2 to ISEE 1 DY_GSM Positional GSM Z separation of ISEE 2 to ISEE 1 DZ_GSM Positional GSE X separation of ISEE 2 to ISEE 1 DX_GSE Positional GSE Y separation of ISEE 2 to ISEE 1 DY_GSE Positional GSE Z separation of ISEE 2 to ISEE 1 DZ_GSE Positional Distance between ISEE 2 to ISEE 1 DR Positional GSE X component of vector to magnetopause NMPX_GSE GSE X component of the vector that starts at the spacecraft and intersects the model magnetopause perpendicularly Positional GSE Y component of vector to magnetopause NMPY_GSE GSE Y component of the vector that starts at the spacecraft and intersects the model magnetopause perpendicularly Positional GSE Z component of vector to magnetopause NMPZ_GSE GSE Z component of the vector that starts at the spacecraft and intersects the model magnetopause perpendicularly Positional Component of ISEE_1-ISEE_2 vector, MP MPS Component of the ISEE_1-ISEE_2 separation vector along the vector that starts at the spacecraft and intersects the model magnetopause perpendicularly Positional GSE X component of vector to bow shock NSX_GSE GSE X component of the vector that starts at the spacecraft and intersects the model bow shock perpendicularly Positional GSE Y component of vector to bow shock NSY_GSE GSE Y component of the vector that starts at the spacecraft and intersects the model bow shock perpendicularly Positional GSE Z component of vector to bow shock NSZ_GSE GSE Z component of the vector that starts at the spacecraft and intersects the model bow shock perpendicularly Positional Component of ISEE_1-ISEE_2 vector, BS MPS Component of the ISEE_1-ISEE_2 separation vector along the vector that starts at the spacecraft and intersects the model bow shock perpendicularly Positional