ARABSAT 1D (ANIK D2)
Satellite information ARABSAT 1D (ANIK D2)
| Spacetrack Directory Name | ARABSAT 1D (ANIK D2) |
| Follow ARABSAT 1D (ANIK D2) | ARABSAT 1D (ANIK D2) Tracker |
| Pass predictions ARABSAT 1D (ANIK D2) | Pass predictions ARABSAT 1D (ANIK D2) |
| Orbit launches |
1984-11-08 (41 years ago)
|
| Days in orbit | 15279 |
| Country/organisation of origin | Arab Satellite Communications Organization (AB) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 36049 km |
| Apogee | 36300 km |
| Orbit slope (inclination) | 13.53° |
| Laps per day | 1 |
| Height ARABSAT 1D (ANIK D2) | 36173.15 km |
Additional information ARABSAT 1D (ANIK D2)
ARABSAT 1D (ANIK D2), 15383 is a payload satellite owned by Telesat (SA) in GEO that was launched on Thu, 08 Nov 1984 UTC via an SPACE SHUTTLE 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 ARABSAT 1D (ANIK D2) Date of exalting 08.11.1984y. Average height of ISS ARABSAT 1D (ANIK D2) hundred 36173.15 km. Average velocity ARABSAT 1D (ANIK D2) is 11018.66 km/h. Inclination ARABSAT 1D (ANIK D2) satellite 13.54°.TLE
Average velocity ARABSAT 1D (ANIK D2)
Average inclination ARABSAT 1D (ANIK D2)
Mean right ascension of the ascending node (RAAN) ARABSAT 1D (ANIK D2)
Mean argument of perigee ARABSAT 1D (ANIK D2)
Mean semi-major axis of the orbit ARABSAT 1D (ANIK D2)
Mean orbital eccentricity ARABSAT 1D (ANIK D2)
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