OPTUS A2 (AUSSAT 2)
Satellite information OPTUS A2 (AUSSAT 2)
| Spacetrack Directory Name | OPTUS A2 (AUSSAT 2) |
| Follow OPTUS A2 (AUSSAT 2) | OPTUS A2 (AUSSAT 2) Tracker |
| Pass predictions OPTUS A2 (AUSSAT 2) | Pass predictions OPTUS A2 (AUSSAT 2) |
| Orbit launches |
1985-11-27 (40 years ago)
|
| Days in orbit | 14895 |
| Country/organisation of origin | Australia (AUS) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35859 km |
| Apogee | 35900 km |
| Orbit slope (inclination) | 13.3° |
| Laps per day | 1 |
| Height OPTUS A2 (AUSSAT 2) | 35876.49 km |
Additional information OPTUS A2 (AUSSAT 2)
OPTUS A2 (AUSSAT 2), 16275 is a payload satellite owned by Aussat (AU) in GEO that was launched on Wed, 27 Nov 1985 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 OPTUS A2 (AUSSAT 2) Date of exalting 27.11.1985y. Average height of ISS OPTUS A2 (AUSSAT 2) hundred 35876.49 km. Average velocity OPTUS A2 (AUSSAT 2) is 11057.19 km/h. Inclination OPTUS A2 (AUSSAT 2) satellite 13.31°.TLE
Average velocity OPTUS A2 (AUSSAT 2)
Average inclination OPTUS A2 (AUSSAT 2)
Mean right ascension of the ascending node (RAAN) OPTUS A2 (AUSSAT 2)
Mean argument of perigee OPTUS A2 (AUSSAT 2)
Mean semi-major axis of the orbit OPTUS A2 (AUSSAT 2)
Mean orbital eccentricity OPTUS A2 (AUSSAT 2)
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