EUTE 2-F1
Satellite information EUTE 2-F1 - EUTELSAT 2-F1
| Spacetrack Directory Name | EUTE 2-F1 |
| Alternative name | EUTELSAT 2-F1 |
| Follow EUTE 2-F1 | EUTE 2-F1 Tracker |
| Pass predictions EUTE 2-F1 | Pass predictions EUTE 2-F1 |
| Orbit launches |
1990-08-30 (36 years ago)
|
| Days in orbit | 13170 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36037 km |
| Apogee | 36058 km |
| Orbit slope (inclination) | 14.9° |
| Laps per day | 1 |
| Height EUTE 2-F1 | 36048.56 km |
Additional information EUTE 2-F1
EUTE 2-F1, 20777 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Thu, 30 Aug 1990 UTC via an ARIANE 44LP 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 EUTE 2-F1 Date of exalting 30.08.1990y. Average height of ISS EUTE 2-F1 hundred 36048.56 km. Average velocity EUTE 2-F1 is 11034.76 km/h. Inclination EUTE 2-F1 satellite 14.9°.TLE
Average velocity EUTE 2-F1
Average inclination EUTE 2-F1
Mean right ascension of the ascending node (RAAN) EUTE 2-F1
Mean argument of perigee EUTE 2-F1
Mean semi-major axis of the orbit EUTE 2-F1
Mean orbital eccentricity EUTE 2-F1
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