ANIK C3 (TELESAT-5)
Satellite information ANIK C3 (TELESAT-5)
| Spacetrack Directory Name | ANIK C3 (TELESAT-5) |
| Follow ANIK C3 (TELESAT-5) | ANIK C3 (TELESAT-5) Tracker |
| Pass predictions ANIK C3 (TELESAT-5) | Pass predictions ANIK C3 (TELESAT-5) |
| Orbit launches |
1982-11-11 (43 years ago)
|
| Days in orbit | 16007 |
| Country/organisation of origin | Kanada (CA) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35875 km |
| Apogee | 35910 km |
| Orbit slope (inclination) | 12.39° |
| Laps per day | 1 |
| Height ANIK C3 (TELESAT-5) | 35891.01 km |
Additional information ANIK C3 (TELESAT-5)
ANIK C3 (TELESAT-5), 13652 is a payload satellite owned by Telesat (CA) in GEO that was launched on Thu, 11 Nov 1982 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 ANIK C3 (TELESAT-5) Date of exalting 11.11.1982y. Average height of ISS ANIK C3 (TELESAT-5) hundred 35891.01 km. Average velocity ANIK C3 (TELESAT-5) is 11055.28 km/h. Inclination ANIK C3 (TELESAT-5) satellite 12.41°.TLE
Average velocity ANIK C3 (TELESAT-5)
Average inclination ANIK C3 (TELESAT-5)
Mean right ascension of the ascending node (RAAN) ANIK C3 (TELESAT-5)
Mean argument of perigee ANIK C3 (TELESAT-5)
Mean semi-major axis of the orbit ANIK C3 (TELESAT-5)
Mean orbital eccentricity ANIK C3 (TELESAT-5)
ISS
Buy us a coffee!
