Data Set Information
DATA_SET_NAME GALILEO ORBITER EARTH POS EARTH2 FLYBY TRAJ V1.0
DATA_SET_ID GO-E-POS-6-EARTH2-FLYBY-TRAJ-V1.0
NSSDC_DATA_SET_ID
DATA_SET_TERSE_DESCRIPTION
DATA_SET_DESCRIPTION Data Set Overview ================= This dataset contains the Galileo spacecraft trajectory during the Earth-2 flyby. The data have been derived from SPICE kernels at a 1 minute sample rate. The data are provided in both Geocentric Solar Ecliptic (GSE) and Geocentric Solar Magnetic (GSM) coordinates and are given in units of earth radii (Re) where 1 Re = 6378 km. Data ==== ------------------------------------------------------------------ Table 1. Data record structure, ------------------------------------------------------------------ Column Units Description ------------------------------------------------------------------ time seconds S/C event time (UT) in the PDS format (yyyy-mm-ddThh:mm:ss.sss ) X Re S/C position X component in GSE or GSM coords. Y_gse Re S/C position Y component in GSE coords. Z_gse Re S/C position Z component in GSE coords. Y_gsm Re S/C position Y component in GSM coords. Z_gsm Re S/C position Z component in GSM coords. Coordinate Systems ================== The Galileo trajectory data are being archived in 2 coordinate systems. Geocentric Solar Ecliptic (GSE) and Geocentric Solar Magnetic (GSM) are related earth centered coordinate systems. Both the GSE and GSM X directions are taken along the Earth - Sun line, positive towards the Sun. The GSE Z direction is parallel to the ecliptic normal, positive northward, and Y completes the right-handed set (towards dusk). For GSM, the X-Z plane contains the Earth's dipole moment vector, positive northward, and Y completes the right-handed set. GSE coordinates are commonly used for analyzing the solar wind near the Earth and GSM coordinates are used when analyzing data inside the Earth's bow shock. Data Processing =============== The trajectory has been derived from the Galileo SPK kernel: 'S970311A.BSP' This kernel was obtained by the PDS-PPI node from the PDS-NAIF node. The code which produced the trajectory data was developed and executed at PDS-PPI. This code utilized SPICE routines which were developed at and distributed by PDS-NAIF. Both SPICE kernels and code may be available through PDS-NAIF.
DATA_SET_RELEASE_DATE 2003-03-01T00:00:00.000Z
START_TIME 1992-11-03T12:00:00.000Z
STOP_TIME 1992-12-20T12:00:00.000Z
MISSION_NAME GALILEO
MISSION_START_DATE 1977-10-01T12:00:00.000Z
MISSION_STOP_DATE 2003-09-21T12:00:00.000Z
TARGET_NAME EARTH
TARGET_TYPE PLANET
INSTRUMENT_HOST_ID GO
INSTRUMENT_NAME N/A
INSTRUMENT_ID POS
INSTRUMENT_TYPE N/A
NODE_NAME planetary plasma interactions
ARCHIVE_STATUS ARCHIVED
CONFIDENCE_LEVEL_NOTE Confidence Level Overview ========================= The data have been derived from the Galileo SPICE kernels using well tested software from the SPICELIB and GLLSPICE subroutine libraries. Each data point is computed using S/C and planetary ephemerides computed at the time of the dataset sample (not interpolated).
CITATION_DESCRIPTION Joy, S.P., Mafi, J.N., GALILEO ORBITER EARTH POS EARTH2 FLYBY TRAJ V1.0, GO-E-POS-6-EARTH2-FLYBY-TRAJ-V1.0, NASA Planetary Data System, 2003
ABSTRACT_TEXT Galileo Orbiter 60 second sampled trajectory data from the Earth-2 flyby in GSE and GSM coordinates. These data cover the interval 1992-11-03 to 1992-12-20.
PRODUCER_FULL_NAME MARGARET G. KIVELSON
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