OPTUS A1 R/B(PAM-D)
Satellite information OPTUS A1 R/B(PAM-D) - OPTUS A1 R/B [PAM-D]
| Spacetrack Directory Name | OPTUS A1 R/B(PAM-D) |
| Alternative name | OPTUS A1 R/B [PAM-D] |
| Follow OPTUS A1 R/B(PAM-D) | OPTUS A1 R/B(PAM-D) Tracker |
| Pass predictions OPTUS A1 R/B(PAM-D) | Pass predictions OPTUS A1 R/B(PAM-D) |
| Orbit launches |
1985-08-27 (41 years ago)
|
| Days in orbit | 14987 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 421 km |
| Apogee | 34436 km |
| Orbit slope (inclination) | 25.82° |
| Laps per day | 2 |
| Height OPTUS A1 R/B(PAM-D) | 23161.81 km |
Additional information OPTUS A1 R/B(PAM-D)
OPTUS A1 R/B(PAM-D), 15996 is space debris in HEO originally from a launch on Tue, 27 Aug 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 A1 R/B(PAM-D) Date of exalting 27.08.1985y. Average height of ISS OPTUS A1 R/B(PAM-D) hundred 23161.81 km. Average velocity OPTUS A1 R/B(PAM-D) is 12760.61 km/h. Inclination OPTUS A1 R/B(PAM-D) satellite 25.83°.TLE
Average velocity OPTUS A1 R/B(PAM-D)
Average inclination OPTUS A1 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) OPTUS A1 R/B(PAM-D)
Mean argument of perigee OPTUS A1 R/B(PAM-D)
Mean semi-major axis of the orbit OPTUS A1 R/B(PAM-D)
Mean orbital eccentricity OPTUS A1 R/B(PAM-D)
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