Mission type | Lunar orbiter |
---|---|
Operator | NASA |
COSPAR ID | 1998-001A |
SATCAT no. | 25131 |
Mission duration | 570 days |
Spacecraft properties | |
Bus | LM-100 |
Manufacturer | Lockheed Martin |
Launch mass | 295 kilograms (650 lb) |
Dry mass | 126 kilograms (278 lb) |
Power | 202.0 W |
Start of mission | |
Launch date | January 7, 1998, 02:28:44 UTC |
Rocket | Athena II |
Launch site | Cape Canaveral SLC-46 |
Contractor | Lockheed Martin Space Systems |
End of mission | |
Decay date | July 31, 1999, 09:52:02 UTC |
Orbital parameters | |
Reference system | Selenocentric |
Eccentricity | 0.00046 |
Periselene altitude | 99.45 kilometers (61.80 mi) |
Aposelene altitude | 101.2 kilometers (62.9 mi) |
Inclination | 90.55 degrees |
Period | 117.9 minutes |
Epoch | January 16, 1998[1] |
Lunar orbiter | |
Orbital insertion | January 11, 1998, 10:28 UTC |
Impact site | 87.7°S 42.1°E |
Orbits | ~7060 |
Instruments | |
Gamma ray spectrometer (GRS) Lunar Prospector neutron spectrometer (NS) Alpha particle spectrometer (APS) Doppler gravity experiment (DGE) Magnetometer (MAG) Electron reflectometer (ER) | |
Official insignia of the Lunar Prospector mission |
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