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 |
1970-12-02 (55 years ago)
|
| Days in orbit | 20411 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 1588 km |
| Apogee | 5083 km |
| Orbit slope (inclination) | 51.59° |
| Laps per day | 9 |
| Height SL-12 R/B(AUX MOTOR) | 3499.16 km |
Additional information SL-12 R/B(AUX MOTOR)
SL-12 R/B(AUX MOTOR), 4789 is space debris in LEO originally from a launch on Wed, 02 Dec 1970 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 02.12.1970y. Average height of ISS SL-12 R/B(AUX MOTOR) hundred 3499.16 km. Average velocity SL-12 R/B(AUX MOTOR) is 22874.33 km/h. Inclination SL-12 R/B(AUX MOTOR) satellite 51.6°.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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