ANIK A2 (TELESAT 2)
Satellite information ANIK A2 (TELESAT 2)
| Spacetrack Directory Name | ANIK A2 (TELESAT 2) |
| Follow ANIK A2 (TELESAT 2) | ANIK A2 (TELESAT 2) Tracker |
| Pass predictions ANIK A2 (TELESAT 2) | Pass predictions ANIK A2 (TELESAT 2) |
| Orbit launches |
1973-04-20 (53 years ago)
|
| Days in orbit | 19500 |
| Country/organisation of origin | Kanada (CA) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35862 km |
| Apogee | 35974 km |
| Orbit slope (inclination) | 6.74° |
| Laps per day | 1 |
| Height ANIK A2 (TELESAT 2) | 35921.19 km |
Additional information ANIK A2 (TELESAT 2)
ANIK A2 (TELESAT 2), 6437 is a payload satellite owned by Telesat (CA) in GEO that was launched on Fri, 20 Apr 1973 UTC via a DELTA 1914 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 A2 (TELESAT 2) Date of exalting 20.04.1973y. Average height of ISS ANIK A2 (TELESAT 2) hundred 35921.19 km. Average velocity ANIK A2 (TELESAT 2) is 11051.31 km/h. Inclination ANIK A2 (TELESAT 2) satellite 6.77°.TLE
Average velocity ANIK A2 (TELESAT 2)
Average inclination ANIK A2 (TELESAT 2)
Mean right ascension of the ascending node (RAAN) ANIK A2 (TELESAT 2)
Mean argument of perigee ANIK A2 (TELESAT 2)
Mean semi-major axis of the orbit ANIK A2 (TELESAT 2)
Mean orbital eccentricity ANIK A2 (TELESAT 2)
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