ASC 1 R/B(PAM-D)
Satellite information ASC 1 R/B(PAM-D) - ASC 1 R/B [PAM-D]
| Spacetrack Directory Name | ASC 1 R/B(PAM-D) |
| Alternative name | ASC 1 R/B [PAM-D] |
| Follow ASC 1 R/B(PAM-D) | ASC 1 R/B(PAM-D) Tracker |
| Pass predictions ASC 1 R/B(PAM-D) | Pass predictions ASC 1 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 | 388 km |
| Apogee | 34558 km |
| Orbit slope (inclination) | 26.33° |
| Laps per day | 2 |
| Height ASC 1 R/B(PAM-D) | 23304.85 km |
Additional information ASC 1 R/B(PAM-D)
ASC 1 R/B(PAM-D), 16007 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 ASC 1 R/B(PAM-D) Date of exalting 27.08.1985y. Average height of ISS ASC 1 R/B(PAM-D) hundred 23304.85 km. Average velocity ASC 1 R/B(PAM-D) is 12701.67 km/h. Inclination ASC 1 R/B(PAM-D) satellite 26.37°.TLE
Average velocity ASC 1 R/B(PAM-D)
Average inclination ASC 1 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) ASC 1 R/B(PAM-D)
Mean argument of perigee ASC 1 R/B(PAM-D)
Mean semi-major axis of the orbit ASC 1 R/B(PAM-D)
Mean orbital eccentricity ASC 1 R/B(PAM-D)
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