SL-16 DEB
Satellite information SL-16 DEB
| Spacetrack Directory Name | SL-16 DEB |
| Follow SL-16 DEB | SL-16 DEB Tracker |
| Pass predictions SL-16 DEB | Pass predictions SL-16 DEB |
| Orbit launches |
1996-09-04 (30 years ago)
|
| Days in orbit | 10967 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 844 km |
| Apogee | 1152 km |
| Orbit slope (inclination) | 70.99° |
| Laps per day | 14 |
| Height SL-16 DEB | 1007.58 km |
Additional information SL-16 DEB
SL-16 DEB, 24302 is space debris in LEO originally from a launch on Wed, 04 Sep 1996 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 04.09.1996y. Average height of ISS SL-16 DEB hundred 1007.58 km. Average velocity SL-16 DEB is 26458.47 km/h. Inclination SL-16 DEB satellite 70.98°.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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