INMARSAT 2-F1
Satellite information INMARSAT 2-F1
| Spacetrack Directory Name | INMARSAT 2-F1 |
| Follow INMARSAT 2-F1 | INMARSAT 2-F1 Tracker |
| Pass predictions INMARSAT 2-F1 | Pass predictions INMARSAT 2-F1 |
| Orbit launches |
1990-10-30 (36 years ago)
|
| Days in orbit | 13158 |
| Country/organisation of origin | International Mobile Satellite Organization (INMARSAT) (IM) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36135 km |
| Apogee | 36230 km |
| Orbit slope (inclination) | 13.11° |
| Laps per day | 1 |
| Height INMARSAT 2-F1 | 36182.28 km |
Additional information INMARSAT 2-F1
INMARSAT 2-F1, 20918 is a payload satellite owned by INMARSAT (UK) in GEO that was launched on Tue, 30 Oct 1990 UTC via a DELTA 6925 launch vehicle from the Air Force Eastern Test Range (AFETR). 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-F1 Date of exalting 30.10.1990y. Average height of ISS INMARSAT 2-F1 hundred 36182.28 km. Average velocity INMARSAT 2-F1 is 11017.39 km/h. Inclination INMARSAT 2-F1 satellite 13.08°.TLE
Average velocity INMARSAT 2-F1
Average inclination INMARSAT 2-F1
Mean right ascension of the ascending node (RAAN) INMARSAT 2-F1
Mean argument of perigee INMARSAT 2-F1
Mean semi-major axis of the orbit INMARSAT 2-F1
Mean orbital eccentricity INMARSAT 2-F1
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