OSCAR 30 DEB
Satellite information OSCAR 30 DEB
| Spacetrack Directory Name | OSCAR 30 DEB |
| Follow OSCAR 30 DEB | OSCAR 30 DEB Tracker |
| Pass predictions OSCAR 30 DEB | Pass predictions OSCAR 30 DEB |
| Orbit launches |
1985-08-03 (41 years ago)
|
| Days in orbit | 15000 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 967 km |
| Apogee | 1195 km |
| Orbit slope (inclination) | 90.17° |
| Laps per day | 14 |
| Height OSCAR 30 DEB | 1078.1 km |
Additional information OSCAR 30 DEB
OSCAR 30 DEB, 21878 is space debris in LEO originally from a launch on Sat, 03 Aug 1985 UTC launched from the Air Force Western Test Range (AFWTR). 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 OSCAR 30 DEB Date of exalting 03.08.1985y. Average height of ISS OSCAR 30 DEB hundred 1078.1 km. Average velocity OSCAR 30 DEB is 26332.24 km/h. Inclination OSCAR 30 DEB satellite 90.17°.TLE
Average velocity OSCAR 30 DEB
Average inclination OSCAR 30 DEB
Mean right ascension of the ascending node (RAAN) OSCAR 30 DEB
Mean argument of perigee OSCAR 30 DEB
Mean semi-major axis of the orbit OSCAR 30 DEB
Mean orbital eccentricity OSCAR 30 DEB
ISS
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