OPTUS A2 R/B(PAM-D)
Satellite information OPTUS A2 R/B(PAM-D) - OPTUS A2 R/B [PAM-D]
| Spacetrack Directory Name | OPTUS A2 R/B(PAM-D) |
| Alternative name | OPTUS A2 R/B [PAM-D] |
| Follow OPTUS A2 R/B(PAM-D) | OPTUS A2 R/B(PAM-D) Tracker |
| Pass predictions OPTUS A2 R/B(PAM-D) | Pass predictions OPTUS A2 R/B(PAM-D) |
| Orbit launches |
1985-11-27 (40 years ago)
|
| Days in orbit | 14895 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 400 km |
| Apogee | 34494 km |
| Orbit slope (inclination) | 25.79° |
| Laps per day | 2 |
| Height OPTUS A2 R/B(PAM-D) | 23208.39 km |
Additional information OPTUS A2 R/B(PAM-D)
OPTUS A2 R/B(PAM-D), 16294 is space debris in HEO originally from a launch on Wed, 27 Nov 1985 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite OPTUS A2 R/B(PAM-D) Date of exalting 27.11.1985y. Average height of ISS OPTUS A2 R/B(PAM-D) hundred 23208.39 km. Average velocity OPTUS A2 R/B(PAM-D) is 12728.04 km/h. Inclination OPTUS A2 R/B(PAM-D) satellite 25.78°.TLE
Average velocity OPTUS A2 R/B(PAM-D)
Average inclination OPTUS A2 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) OPTUS A2 R/B(PAM-D)
Mean argument of perigee OPTUS A2 R/B(PAM-D)
Mean semi-major axis of the orbit OPTUS A2 R/B(PAM-D)
Mean orbital eccentricity OPTUS A2 R/B(PAM-D)
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