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 |
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) |
| Categories | |
| Perigee | 841 km |
| Apogee | 860 km |
| Orbit slope (inclination) | 70.77° |
| Laps per day | 14 |
| Height SL-16 R/B | 861.5 km |
Additional information SL-16 R/B
SL-16 R/B, 24298 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 R/B Date of exalting 04.09.1996y. Average height of ISS SL-16 R/B hundred 861.5 km. Average velocity SL-16 R/B is 26724.35 km/h. Inclination SL-16 R/B satellite 70.77°.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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