SL-16 DEB
Satellite information SL-16 DEB - Satelita
| Spacetrack Directory Name | SL-16 DEB |
| Alternative name | Satelita |
| Follow SL-16 DEB | SL-16 DEB Tracker |
| Pass predictions SL-16 DEB | Pass predictions SL-16 DEB |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | |
| Perigee | 833 km |
| Apogee | 841 km |
| Orbit slope (inclination) | 71.02° |
| Laps per day | 14 |
| Height SL-16 DEB | 847.53 km |
Additional information SL-16 DEB
SL-16 DEB, 54753 is space debris originally from a Commonwealth of Independent States-origin launch on Fri, 25 Dec 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.
Average height of ISS SL-16 DEB hundred 847.53 km. Average velocity SL-16 DEB is 26750.17 km/h. Inclination SL-16 DEB satellite 71.02°.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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