SL-12 R/B(AUX MOTOR)
Satellite information SL-12 R/B(AUX MOTOR)
| Spacetrack Directory Name | SL-12 R/B(AUX MOTOR) |
| Follow SL-12 R/B(AUX MOTOR) | SL-12 R/B(AUX MOTOR) Tracker |
| Pass predictions SL-12 R/B(AUX MOTOR) | Pass predictions SL-12 R/B(AUX MOTOR) |
| Orbit launches |
1984-09-28 (41 years ago)
|
| Days in orbit | 15338 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| WWW | Here |
| Perigee | 809 km |
| Apogee | 827 km |
| Orbit slope (inclination) | 66.55° |
| Laps per day | 14 |
| Height SL-12 R/B(AUX MOTOR) | 824.5 km |
Additional information SL-12 R/B(AUX MOTOR)
SL-12 R/B(AUX MOTOR), 15335 is space debris in LEO originally from a launch on Fri, 28 Sep 1984 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(AUX MOTOR) Date of exalting 28.09.1984y. Average height of ISS SL-12 R/B(AUX MOTOR) hundred 824.5 km. Average velocity SL-12 R/B(AUX MOTOR) is 26793.24 km/h. Inclination SL-12 R/B(AUX MOTOR) satellite 66.55°.TLE
Average velocity SL-12 R/B(AUX MOTOR)
Average inclination SL-12 R/B(AUX MOTOR)
Mean right ascension of the ascending node (RAAN) SL-12 R/B(AUX MOTOR)
Mean argument of perigee SL-12 R/B(AUX MOTOR)
Mean semi-major axis of the orbit SL-12 R/B(AUX MOTOR)
Mean orbital eccentricity SL-12 R/B(AUX MOTOR)
ISS
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