THEMIS-A (P5) Orbit (Ephemeris)

공공데이터포털

THEMIS-A Orbital Information provided via the Satellite Situation Center, SSCWeb, System and Services, Space Physics Data Facility, SPDF, GSFC, NASA

THEMIS-E (P4) Orbit (Ephemeris)

공공데이터포털

THEMIS-E Orbital Information provided via the Satellite Situation Center, SSCWeb, System and Services, Space Physics Data Facility, SPDF, GSFC, NASA

THEMIS-C (P2/ARTEMIS-P2) Orbit (Ephemeris)

공공데이터포털

THEMIS-C Orbital Information provided via the Satellite Situation Center, SSCWeb, System and Services, Space Physics Data Facility, SPDF, GSFC, NASA

THEMIS-B (P1/ARTEMIS-P1) Orbit (Ephemeris)

공공데이터포털

THEMIS-B Orbital Information provided via the Satellite Situation Center, SSCWeb, System and Services, Space Physics Data Facility, SPDF, GSFC, NASA

IMAGE Predicted Orbital Data

공공데이터포털

IMAGE Predicted Orbit Data, GSE and GSM Coordinates

Spacecraft ephemeris

공공데이터포털

Spacecraft ephemeris

Horizons

공공데이터포털

The JPL HORIZONS on-line solar system data and ephemeris computation service provides access to key solar system data and flexible production of highly accurate ephemerides for solar system objects ( 561485 asteroids, 3099 comets, 171 planetary satellites, 8 planets, the Sun, L1, L2, select spacecraft, and system barycenters ). HORIZONS is provided by the Solar System Dynamics Group of the Jet Propulsion Laboratory.

THEMIS-D (P3), Electric Field Instrument (EFI) Spacecraft measured Electric Field

공공데이터포털

THEMIS-D: Electric Field Instrument, EFI, Electric Field Measurements. The L2 Product is a 3D Estimate of the perpnedicular Electric Field, Eperp, derived from the Spin Plane E-Field Measurements assuming E ⋅ B = 0, using relevant Flux-Gate Magnetometer, FGM, Data. This Data Product includes Spin-Averaged, and Fast Survey Field Data. The Spin-Averaged Data, EFS_DOT0, has approximately 3 s Time Resolution. Fast Survey, EFF_DOT0, Data has 0.125 s Time Resolution.

LP MOON SPACECRAFT EPHEMERIS V1.0

공공데이터포털

The Lunar Prospector ephemeris data set consists of spacecraft position and velocity determinations as a function of time in Moon-centered, Earth equator, mean of J2000 coordinates. Tracking data collected by ground stations are used by the Goddard Flight Dynamics Analysis Branch (FDAB) to compute the Lunar Prospector orbit ephemeris. The Level 0 Data archive contains the ephemeris type known as the 'definitive ephemeris', which is based on an updated lunar gravity model [FDAB1997].

MODIS/Aqua 24-hour Spacecraft ephemeris/orbit data files to be read via SDP Toolkit Binary Format - NRT

공공데이터포털

PM1EPHND is the Aqua Near Real Time (NRT) daily spacecraft definitive ephemeris data file in native format. This is MODIS Ancillary Data. The data collection consists of PM1 Platform Attitude Data that has been preprocessed by ECS to an internal standard supported by the ECS SDP Toolkit. This data is typically used in determining the geolocation of earth remote sensing observations.The file name format is the following:PM1EPHND_NRT.Ayyyyddd.hhmm.vvv where from left to right:PM1 = PM1 (Aqua);EPH = Spacecraft Ephemeris; N = Native format; D = Definitive; A = Acquisition; yyyy = data year, ddd = Julian data day, hh = data hour, mm = data minute; vvv = Version ID.