ANIK A3 (TELESAT-3)
Satellite information ANIK A3 (TELESAT-3)
| Spacetrack Directory Name | ANIK A3 (TELESAT-3) |
| Follow ANIK A3 (TELESAT-3) | ANIK A3 (TELESAT-3) Tracker |
| Pass predictions ANIK A3 (TELESAT-3) | Pass predictions ANIK A3 (TELESAT-3) |
| Orbit launches |
1975-05-07 (51 years ago)
|
| Days in orbit | 18753 |
| Country/organisation of origin | Kanada (CA) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35831 km |
| Apogee | 35857 km |
| Orbit slope (inclination) | 7.52° |
| Laps per day | 1 |
| Height ANIK A3 (TELESAT-3) | 35849.45 km |
Additional information ANIK A3 (TELESAT-3)
ANIK A3 (TELESAT-3), 7790 is a payload satellite owned by Telesat (CA) in GEO that was launched on Wed, 07 May 1975 UTC via a DELTA 2914 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 ANIK A3 (TELESAT-3) Date of exalting 07.05.1975y. Average height of ISS ANIK A3 (TELESAT-3) hundred 35849.45 km. Average velocity ANIK A3 (TELESAT-3) is 11060.69 km/h. Inclination ANIK A3 (TELESAT-3) satellite 7.55°.TLE
Average velocity ANIK A3 (TELESAT-3)
Average inclination ANIK A3 (TELESAT-3)
Mean right ascension of the ascending node (RAAN) ANIK A3 (TELESAT-3)
Mean argument of perigee ANIK A3 (TELESAT-3)
Mean semi-major axis of the orbit ANIK A3 (TELESAT-3)
Mean orbital eccentricity ANIK A3 (TELESAT-3)
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