TOPEX/POSEIDON
Satellite information TOPEX/POSEIDON
| Spacetrack Directory Name | TOPEX/POSEIDON |
| Follow TOPEX/POSEIDON | TOPEX/POSEIDON Tracker |
| Pass predictions TOPEX/POSEIDON | Pass predictions TOPEX/POSEIDON |
| Orbit launches |
1992-08-10 (34 years ago)
|
| Days in orbit | 12459 |
| Country/organisation of origin | USA (US) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 1331 km |
| Apogee | 1343 km |
| Orbit slope (inclination) | 66.04° |
| Laps per day | 13 |
| Height TOPEX/POSEIDON | 1346.73 km |
Additional information TOPEX/POSEIDON
TOPEX/POSEIDON, 22076 is an American payload satellite in LEO that was launched on Mon, 10 Aug 1992 UTC via an ARIANE 42P launch vehicle from the French Guiana (FRGUI). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite TOPEX/POSEIDON Date of exalting 10.08.1992y. Average height of ISS TOPEX/POSEIDON hundred 1346.73 km. Average velocity TOPEX/POSEIDON is 25871.2 km/h. Inclination TOPEX/POSEIDON satellite 66.04°.TLE
Average velocity TOPEX/POSEIDON
Average inclination TOPEX/POSEIDON
Mean right ascension of the ascending node (RAAN) TOPEX/POSEIDON
Mean argument of perigee TOPEX/POSEIDON
Mean semi-major axis of the orbit TOPEX/POSEIDON
Mean orbital eccentricity TOPEX/POSEIDON
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