INMARSAT 2-F3
Satellite information INMARSAT 2-F3
| Spacetrack Directory Name | INMARSAT 2-F3 |
| Follow INMARSAT 2-F3 | INMARSAT 2-F3 Tracker |
| Pass predictions INMARSAT 2-F3 | Pass predictions INMARSAT 2-F3 |
| Orbit launches |
1991-12-16 (34 years ago)
|
| Days in orbit | 12697 |
| Country/organisation of origin | International Mobile Satellite Organization (INMARSAT) (IM) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36942 km |
| Apogee | 37077 km |
| Orbit slope (inclination) | 14.21° |
| Laps per day | 1 |
| Height INMARSAT 2-F3 | 37010.44 km |
Additional information INMARSAT 2-F3
INMARSAT 2-F3, 21814 is a payload satellite owned by INMARSAT (UK) in GEO that was launched on Mon, 16 Dec 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 INMARSAT 2-F3 Date of exalting 16.12.1991y. Average height of ISS INMARSAT 2-F3 hundred 37010.44 km. Average velocity INMARSAT 2-F3 is 10911.68 km/h. Inclination INMARSAT 2-F3 satellite 14.2°.TLE
Average velocity INMARSAT 2-F3
Average inclination INMARSAT 2-F3
Mean right ascension of the ascending node (RAAN) INMARSAT 2-F3
Mean argument of perigee INMARSAT 2-F3
Mean semi-major axis of the orbit INMARSAT 2-F3
Mean orbital eccentricity INMARSAT 2-F3
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