EQUATOR S
Satellite information EQUATOR S
| Spacetrack Directory Name | EQUATOR S |
| Follow EQUATOR S | EQUATOR S Tracker |
| Pass predictions EQUATOR S | Pass predictions EQUATOR S |
| Orbit launches |
1997-12-02 (28 years ago)
|
| Days in orbit | 10566 |
| Country/organisation of origin | Niemcy (GER) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 468 km |
| Apogee | 67161 km |
| Orbit slope (inclination) | 2.06° |
| Laps per day | 1 |
| Height EQUATOR S | 47638.68 km |
Additional information EQUATOR S
EQUATOR S, 25068 is a payload satellite owned by MPE (DE) in HEO that was launched on Tue, 02 Dec 1997 UTC via an ARIANE 44P 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 EQUATOR S Date of exalting 02.12.1997y. Average height of ISS EQUATOR S hundred 47638.68 km. Average velocity EQUATOR S is 9003.07 km/h. Inclination EQUATOR S satellite 2.6°.TLE
Average velocity EQUATOR S
Average inclination EQUATOR S
Mean right ascension of the ascending node (RAAN) EQUATOR S
Mean argument of perigee EQUATOR S
Mean semi-major axis of the orbit EQUATOR S
Mean orbital eccentricity EQUATOR S
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