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1) CRRES Ephemeris Information maxmize
Resource ID:spase://VMO/NumericalData/CRRES/Ephemeris/PT5M
Start:1990-10-11 00:00:00 Observatory:CRRES Cadence:5 minutes
Stop:1991-10-13 00:00:00 Instrument:CRRES Spacecraft Position Resource:NumericalData
This data set contains orbital information from the CRRES spacecraft. The ephemeris data is at 5 min resolution. The files include the magnetic coordinates, spacecraft radial locaton, the L shell information, the spacecraft position in ECI coordinates, and the northern and southern hemisphere foot print location in geographic latitutde and longitude coordinates at 100 km in altitude.
2) Cluster Auxiliary Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster/Ephemeris/SummaryParameter/PT1M
Start:2000-08-22 00:00:30 Observatory:Cluster FM5 (Rumba) Cadence:1 minute
Stop:2013-05-22 01:01:12 Instrument:Cluster-Rumba Positions Resource:NumericalData
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.
3) Double Star 1 Spacecraft Auxiliary Summary Parameters Data maxmize
Resource ID:spase://VMO/NumericalData/DoubleStar1/Ephemeris/SummaryParameters/60S
Start:2004-01-05 00:00:30 Observatory:Double Star 1 Cadence:60 seconds
Stop:2007-09-19 23:59:30 Instrument:Double Star 1 Spacecraft Position Resource:NumericalData
The Double Star 1 auxiliary summary parameter data set contains various parameters in GSE coordinates at 60 s resolution. These parameters include universal time, orbit number, GSE position, GSE spacecraft velocity vector, longitude, and dipole tilt. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.
4) Double Star 2 Spacecraft Auxiliary Summary Parameters Data maxmize
Resource ID:spase://VMO/NumericalData/DoubleStar2/Ephemeris/SummaryParameters/60S
Start:2004-07-27 00:00:30 Observatory:Double Star 2 Cadence:60 seconds
Stop:2008-06-30 23:59:30 Instrument:Double Star 2 Spacecraft Position Resource:NumericalData
The Double Star 2 auxiliary summary parameter data set contains various parameters in GSE coordinates at 60 s resolution. These parameters include universal time, orbit number, GSE position, GSE spacecraft velocity vector, longitude, and dipole tilt. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.
5) FAST Positions maxmize
Resource ID:spase://VMO/NumericalData/FAST/Ephemeris/PT1M
Start:1996-01-26 00:00:00 Observatory:FAST Cadence:1 minute
Stop:2011-12-31 00:00:00 Instrument:FAST Position Resource:NumericalData
FAST Positions
6) All GOES Longitudinal Locations at 1 Day Resolution as West Geographic longitude. maxmize
Resource ID:spase://VMO/NumericalData/GOES/Ephemeris/PD1
Start:1986-01-01 00:00:00 Observatory:GOES 2 Cadence:31 days
Stop:2010-02-28 00:00:00 Instrument:GOES 2 Positions Resource:NumericalData
The GOES longitudinal location information consists of the west geographic longitude in degrees. The data are separated into spacecraft (GOES 2-12), year, and month. The location is given for each day of the month is in units of degrees and the geographic latitude is assumed to be zero degrees.
7) Geotail Spacecraft Definitive Positions maxmize
Resource ID:spase://VMO/NumericalData/Geotail/Ephemeris/PT10M
Start:1992-07-27 16:00:00 Observatory:Geotail Cadence:10 minutes
Stop:2013-05-22 01:01:35 Instrument:Geotail Spacecraft Position Resource:NumericalData
Definitive Geotail spacecraft positions in various coordinate systems
8) IMP 8 Spacecraft Positions maxmize
Resource ID:spase://VMO/NumericalData/IMP8/Ephemeris/PT12M
Start:1973-10-30 00:00:00 Observatory:IMP 8 Cadence:12 minutes
Stop:2013-05-22 01:01:36 Instrument:IMP 8 Spacecraft Position Resource:NumericalData
IMP-8 spacecraft positions in various coordinate systems
9) ISEE 3 12-min Trajectory Data maxmize
Resource ID:spase://VEPO/NumericalData/ISEE3/Ephemeris/PT12M
Start:1978-08-16 00:00:00 Observatory:ISEE 3 Cadence:12 minutes
Stop:1984-02-01 00:00:00 Instrument:ISEE 3 Position Resource:NumericalData
ISEE 3 positions.
10) Interball Tail definitive orbital data maxmize
Resource ID:spase://VMO/NumericalData/Interball-Tail/Ephemeris/PT2M
Start:1995-08-07 00:00:00 Observatory:Interball-1 Cadence:2 minutes
Stop:2000-10-16 13:55:00 Instrument:Interball-1 Orbit Resource:NumericalData
Definitive Interball Tail satellite and subsatellite (Interball-1 and Magion-4) orbital data: Spacecraft position, velocity, and status flags.
11) POLAR Predicted Orbit maxmize
Resource ID:spase://VMO/NumericalData/POLAR/Ephemeris/PT01M
Start:1996-02-27 00:00:00 Observatory:POLAR Cadence:01 minutes
Stop:2013-05-22 01:02:06 Instrument:POLAR Orbit Resource:NumericalData
Polar predicted orbit data
12) Pioneer10 Positions maxmize
Resource ID:spase://VEPO/NumericalData/Pioneer10/Ephemeris/P1D
Start:1972-01-01 00:00:00 Observatory:Pioneer 10 Cadence:1 day
Stop:2013-05-21 01:00:43 Instrument:Pioneer10 Positions Resource:NumericalData
Pioneer10 satellite positions.
13) Pioneer11 Positions maxmize
Resource ID:spase://VEPO/NumericalData/Pioneer11/Ephemeris/P1D
Start:1972-01-01 00:00:00 Observatory:Pioneer 11 Cadence:1 day
Stop:2013-05-21 01:00:43 Instrument:Pioneer11 Positions Resource:NumericalData
Pioneer11 satellite positions.
14) SCATHA Positions maxmize
Resource ID:spase://VMO/NumericalData/SCATHA/Ephemeris/PT1M
Start:1979-02-06 00:00:00 Observatory:SCATHA Cadence:1 minute
Stop:1986-12-31 23:59:00 Instrument:SCATHA Positions Resource:NumericalData
SCATHA satellite positions.
15) THEMIS-A Level 1 Probe State Data maxmize
Resource ID:spase://VMO/NumericalData/THEMIS/A/Ephemeris/PT01M
Start:2007-02-17 23:35:58 Observatory:THEMIS-A Cadence:01 minutes
Stop:2013-05-22 01:01:32 Instrument:THEMIS-A Probe Status Resource:NumericalData
The L1 STATE files contain the following data, sampled at one-minute intervals: * probe position and velocity in GEI, GSE, and GSM coordinates; * flags to indicate regions of interest and maneuver status; * RA and declination of spin axis; * spin period and spin phase; * spin model parameters for high-precision interpolation of spin phase between one-minute data points. Version number indicates data source as follows: * V00: predicted ephemeris and attitude, no spin period or spin phase; * V01: predicted ephemeris and attitude, spin period and spin phase derived from probe telemetry; * V02: predicted attitude, definitive ephemeris from magnetometer and Doppler tracking data; * V03: corrected attitude and spin phase derived from fully calibrated magnetometer data (added science attitude determination using perigee data post-processing). Produced by Mission Ops, Science Ops and Science Team.
16) THEMIS-B Level 1 Probe State Data maxmize
Resource ID:spase://VMO/NumericalData/THEMIS/B/Ephemeris/PT01M
Start:2007-02-17 23:35:58 Observatory:THEMIS-B Cadence:01 minutes
Stop:2013-05-22 01:01:29 Instrument:THEMIS-B Probe Status Resource:NumericalData
The L1 STATE files contain the following data, sampled at one-minute intervals: * probe position and velocity in GEI, GSE, and GSM coordinates; * flags to indicate regions of interest and maneuver status; * RA and declination of spin axis; * spin period and spin phase; * spin model parameters for high-precision interpolation of spin phase between one-minute data points. Version number indicates data source as follows: * V00: predicted ephemeris and attitude, no spin period or spin phase; * V01: predicted ephemeris and attitude, spin period and spin phase derived from probe telemetry; * V02: predicted attitude, definitive ephemeris from magnetometer and Doppler tracking data; * V03: corrected attitude and spin phase derived from fully calibrated magnetometer data. (added science attitude determination using perigee data post-processing). Produced by Mission Ops, Science Ops and Science Team.
17) THEMIS-C Level 1 Probe State Data maxmize
Resource ID:spase://VMO/NumericalData/THEMIS/C/Ephemeris/PT01M
Start:2007-02-17 23:35:58 Observatory:THEMIS-C Cadence:01 minutes
Stop:2013-05-22 01:01:26 Instrument:THEMIS-C Probe Status Resource:NumericalData
The L1 STATE files contain the following data, sampled at one-minute intervals: * probe position and velocity in GEI, GSE, and GSM coordinates; * flags to indicate regions of interest and maneuver status; * RA and declination of spin axis; * spin period and spin phase; * spin model parameters for high-precision interpolation of spin phase between one-minute data points. Version number indicates data source as follows: * V00: predicted ephemeris and attitude, no spin period or spin phase; * V01: predicted ephemeris and attitude, spin period and spin phase derived from probe telemetry; * V02: predicted attitude, definitive ephemeris from magnetometer and Doppler tracking data; * V03: corrected attitude and spin phase derived from fully calibrated magnetometer data. (added science attitude determination using perigee data post-processing). Produced by Mission Ops, Science Ops and Science Team.
18) THEMIS-D Level 1 Probe State Data maxmize
Resource ID:spase://VMO/NumericalData/THEMIS/D/Ephemeris/PT01M
Start:2007-02-17 23:35:58 Observatory:THEMIS-D Cadence:01 minutes
Stop:2013-05-22 01:01:18 Instrument:THEMIS-D Probe Status Resource:NumericalData
The L1 STATE files contain the following data, sampled at one-minute intervals: * probe position and velocity in GEI, GSE, and GSM coordinates; * flags to indicate regions of interest and maneuver status; * RA and declination of spin axis; * spin period and spin phase; * spin model parameters for high-precision interpolation of spin phase between one-minute data points. Version number indicates data source as follows: * V00: predicted ephemeris and attitude, no spin period or spin phase; * V01: predicted ephemeris and attitude, spin period and spin phase derived from probe telemetry; * V02: predicted attitude, definitive ephemeris from magnetometer and Doppler tracking data; * V03: corrected attitude and spin phase derived from fully calibrated magnetometer data. (added science attitude determination using perigee data post-processing). Produced by Mission Ops, Science Ops and Science Team.
19) THEMIS-E Level 1 Probe State Data maxmize
Resource ID:spase://VMO/NumericalData/THEMIS/E/Ephemeris/PT01M
Start:2007-02-17 23:35:58 Observatory:THEMIS-E Cadence:01 minutes
Stop:2013-05-22 01:01:15 Instrument:THEMIS-E Probe Status Resource:NumericalData
The L1 STATE files contain the following data, sampled at one-minute intervals: * probe position and velocity in GEI, GSE, and GSM coordinates; * flags to indicate regions of interest and maneuver status; * RA and declination of spin axis; * spin period and spin phase; * spin model parameters for high-precision interpolation of spin phase between one-minute data points. Version number indicates data source as follows: * V00: predicted ephemeris and attitude, no spin period or spin phase; * V01: predicted ephemeris and attitude, spin period and spin phase derived from probe telemetry; * V02: predicted attitude, definitive ephemeris from magnetometer and Doppler tracking data; * V03: corrected attitude and spin phase derived from fully calibrated magnetometer data. (added science attitude determination using perigee data post-processing). Produced by Mission Ops, Science Ops and Science Team.
20) TWINS 1 - Spacecraft Ephemeris maxmize
Resource ID:spase://VMO/NumericalData/TWINS1/Ephemeris/PT1M45S
Start:2001-04-01 00:01:03 Observatory:TWINS 1 Cadence:1 minute; 45 seconds
Stop:2013-05-22 01:01:11 Instrument:TWINS 1 Positions Resource:NumericalData
Definitive orbit data
21) TWINS 2 - Spacecraft Ephemeris maxmize
Resource ID:spase://VMO/NumericalData/TWINS2/Ephemeris/PT1M45S
Start:2001-04-11 00:03:22 Observatory:TWINS 2 Cadence:1 minute; 45 seconds
Stop:2013-05-22 01:01:45 Instrument:TWINS 2 Positions Resource:NumericalData
Definitive orbit data
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