EUTE 2-F4
Satellite information EUTE 2-F4 - EUTELSAT 2-F4
| Spacetrack Directory Name | EUTE 2-F4 |
| Alternative name | EUTELSAT 2-F4 |
| Follow EUTE 2-F4 | EUTE 2-F4 Tracker |
| Pass predictions EUTE 2-F4 | Pass predictions EUTE 2-F4 |
| Orbit launches |
1992-07-09 (34 years ago)
|
| Days in orbit | 12491 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36105 km |
| Apogee | 36146 km |
| Orbit slope (inclination) | 14.78° |
| Laps per day | 1 |
| Height EUTE 2-F4 | 36124.64 km |
Additional information EUTE 2-F4
EUTE 2-F4, 22028 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Thu, 09 Jul 1992 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-F4 Date of exalting 09.07.1992y. Average height of ISS EUTE 2-F4 hundred 36124.64 km. Average velocity EUTE 2-F4 is 11024.9 km/h. Inclination EUTE 2-F4 satellite 14.77°.TLE
Average velocity EUTE 2-F4
Average inclination EUTE 2-F4
Mean right ascension of the ascending node (RAAN) EUTE 2-F4
Mean argument of perigee EUTE 2-F4
Mean semi-major axis of the orbit EUTE 2-F4
Mean orbital eccentricity EUTE 2-F4
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