EUTE 2-F2
Satellite information EUTE 2-F2 - EUTELSAT 2-F2
| Spacetrack Directory Name | EUTE 2-F2 |
| Alternative name | EUTELSAT 2-F2 |
| Follow EUTE 2-F2 | EUTE 2-F2 Tracker |
| Pass predictions EUTE 2-F2 | Pass predictions EUTE 2-F2 |
| Orbit launches |
1991-01-15 (35 years ago)
|
| Days in orbit | 13032 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36151 km |
| Apogee | 36176 km |
| Orbit slope (inclination) | 14.92° |
| Laps per day | 1 |
| Height EUTE 2-F2 | 36163.78 km |
Additional information EUTE 2-F2
EUTE 2-F2, 21056 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Tue, 15 Jan 1991 UTC via an ARIANE 44L 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-F2 Date of exalting 15.01.1991y. Average height of ISS EUTE 2-F2 hundred 36163.78 km. Average velocity EUTE 2-F2 is 11019.82 km/h. Inclination EUTE 2-F2 satellite 14.91°.TLE
Average velocity EUTE 2-F2
Average inclination EUTE 2-F2
Mean right ascension of the ascending node (RAAN) EUTE 2-F2
Mean argument of perigee EUTE 2-F2
Mean semi-major axis of the orbit EUTE 2-F2
Mean orbital eccentricity EUTE 2-F2
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