SL-16 R/B
Satellite information SL-16 R/B
| Spacetrack Directory Name | SL-16 R/B |
| Follow SL-16 R/B | SL-16 R/B Tracker |
| Pass predictions SL-16 R/B | Pass predictions SL-16 R/B |
| 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) |
| Categories | |
| Perigee | 829 km |
| Apogee | 845 km |
| Orbit slope (inclination) | 71° |
| Laps per day | 14 |
| Height SL-16 R/B | 846.55 km |
Additional information SL-16 R/B
SL-16 R/B, 22220 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 R/B Date of exalting 17.11.1992y. Average height of ISS SL-16 R/B hundred 846.55 km. Average velocity SL-16 R/B is 26752 km/h. Inclination SL-16 R/B satellite 71°.TLE
Average velocity SL-16 R/B
Average inclination SL-16 R/B
Mean right ascension of the ascending node (RAAN) SL-16 R/B
Mean argument of perigee SL-16 R/B
Mean semi-major axis of the orbit SL-16 R/B
Mean orbital eccentricity SL-16 R/B
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