OPS 5960 DEB
Satellite information OPS 5960 DEB
| Spacetrack Directory Name | OPS 5960 DEB |
| Follow OPS 5960 DEB | OPS 5960 DEB Tracker |
| Pass predictions OPS 5960 DEB | Pass predictions OPS 5960 DEB |
| Orbit launches |
1970-11-06 (55 years ago)
|
| Days in orbit | 20396 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 25555 km |
| Apogee | 36286 km |
| Orbit slope (inclination) | 15.33° |
| Laps per day | 1 |
| Height OPS 5960 DEB | 31145.79 km |
Additional information OPS 5960 DEB
OPS 5960 DEB, 43000 is space debris originally from a launch on Fri, 06 Nov 1970 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 OPS 5960 DEB Date of exalting 06.11.1970y. Average height of ISS OPS 5960 DEB hundred 31145.79 km. Average velocity OPS 5960 DEB is 11735.68 km/h. Inclination OPS 5960 DEB satellite 15.31°.TLE
Average velocity OPS 5960 DEB
Average inclination OPS 5960 DEB
Mean right ascension of the ascending node (RAAN) OPS 5960 DEB
Mean argument of perigee OPS 5960 DEB
Mean semi-major axis of the orbit OPS 5960 DEB
Mean orbital eccentricity OPS 5960 DEB
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