SL-16 DEB
Satellite information SL-16 DEB - Sep Motor Cover
| Spacetrack Directory Name | SL-16 DEB |
| Alternative name | Sep Motor Cover |
| Follow SL-16 DEB | SL-16 DEB Tracker |
| Pass predictions SL-16 DEB | Pass predictions SL-16 DEB |
| Orbit launches |
1992-11-17 (33 years ago)
|
| Days in orbit | 12359 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Type | Debris |
| Perigee | 838 km |
| Apogee | 1129 km |
| Orbit slope (inclination) | 70.99° |
| Laps per day | 14 |
| Height SL-16 DEB | 993.49 km |
Additional information SL-16 DEB
SL-16 DEB, 22224 is space debris in LEO originally from a launch on Tue, 17 Nov 1992 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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 SL-16 DEB Date of exalting 17.11.1992y. Average height of ISS SL-16 DEB hundred 993.49 km. Average velocity SL-16 DEB is 26484.16 km/h. Inclination SL-16 DEB satellite 70.99°.TLE
Average velocity SL-16 DEB
Average inclination SL-16 DEB
Mean right ascension of the ascending node (RAAN) SL-16 DEB
Mean argument of perigee SL-16 DEB
Mean semi-major axis of the orbit SL-16 DEB
Mean orbital eccentricity SL-16 DEB
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