SL-12 R/B(2)
Satellite information SL-12 R/B(2)
| Spacetrack Directory Name | SL-12 R/B(2) |
| Follow SL-12 R/B(2) | SL-12 R/B(2) Tracker |
| Pass predictions SL-12 R/B(2) | Pass predictions SL-12 R/B(2) |
| Orbit launches |
1990-11-03 (35 years ago)
|
| Days in orbit | 13105 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35472 km |
| Apogee | 35771 km |
| Orbit slope (inclination) | 12.4° |
| Laps per day | 1 |
| Height SL-12 R/B(2) | 35622.47 km |
Additional information SL-12 R/B(2)
SL-12 R/B(2), 20926 is space debris in GEO originally from a launch on Sat, 03 Nov 1990 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-12 R/B(2) Date of exalting 03.11.1990y. Average height of ISS SL-12 R/B(2) hundred 35622.47 km. Average velocity SL-12 R/B(2) is 11090.6 km/h. Inclination SL-12 R/B(2) satellite 12.42°.TLE
Average velocity SL-12 R/B(2)
Average inclination SL-12 R/B(2)
Mean right ascension of the ascending node (RAAN) SL-12 R/B(2)
Mean argument of perigee SL-12 R/B(2)
Mean semi-major axis of the orbit SL-12 R/B(2)
Mean orbital eccentricity SL-12 R/B(2)
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