INSAT 2R (ARABSAT 1C)
Satellite information INSAT 2R (ARABSAT 1C)
| Spacetrack Directory Name | INSAT 2R (ARABSAT 1C) |
| Alternative name | INSAT-2DT (ARABSAT-1C) |
| Follow INSAT 2R (ARABSAT 1C) | INSAT 2R (ARABSAT 1C) Tracker |
| Pass predictions INSAT 2R (ARABSAT 1C) | Pass predictions INSAT 2R (ARABSAT 1C) |
| Orbit launches |
1992-02-26 (34 years ago)
|
| Days in orbit | 12625 |
| Country/organisation of origin | Indie (IND) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36121 km |
| Apogee | 36353 km |
| Orbit slope (inclination) | 14.42° |
| Laps per day | 1 |
| Height INSAT 2R (ARABSAT 1C) | 36237.09 km |
Additional information INSAT 2R (ARABSAT 1C)
INSAT 2R (ARABSAT 1C), 21894 is a payload satellite owned by Arabsat (IN) in GEO that was launched on Wed, 26 Feb 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 INSAT 2R (ARABSAT 1C) Date of exalting 26.02.1992y. Average height of ISS INSAT 2R (ARABSAT 1C) hundred 36237.09 km. Average velocity INSAT 2R (ARABSAT 1C) is 11010.44 km/h. Inclination INSAT 2R (ARABSAT 1C) satellite 14.41°.TLE
Average velocity INSAT 2R (ARABSAT 1C)
Average inclination INSAT 2R (ARABSAT 1C)
Mean right ascension of the ascending node (RAAN) INSAT 2R (ARABSAT 1C)
Mean argument of perigee INSAT 2R (ARABSAT 1C)
Mean semi-major axis of the orbit INSAT 2R (ARABSAT 1C)
Mean orbital eccentricity INSAT 2R (ARABSAT 1C)
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