SL-23 R/B
Satellite information SL-23 R/B - FREGAT R/B
| Spacetrack Directory Name | SL-23 R/B |
| Alternative name | FREGAT R/B |
| Follow SL-23 R/B | SL-23 R/B Tracker |
| Pass predictions SL-23 R/B | Pass predictions SL-23 R/B |
| Orbit launches |
2008-04-27 (18 years ago)
|
| Days in orbit | 6700 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| WWW | Here |
| Perigee | 23428 km |
| Apogee | 23607 km |
| Orbit slope (inclination) | 59.06° |
| Laps per day | 2 |
| Height SL-23 R/B | 23526 km |
Additional information SL-23 R/B
SL-23 R/B, 32782 is space debris originally from a launch on Sun, 27 Apr 2008 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-23 R/B Date of exalting 27.04.2008y. Average height of ISS SL-23 R/B hundred 23526 km. Average velocity SL-23 R/B is 13145 km/h. Inclination SL-23 R/B satellite 59.06°.TLE
Average velocity SL-23 R/B
Average inclination SL-23 R/B
Mean right ascension of the ascending node (RAAN) SL-23 R/B
Mean argument of perigee SL-23 R/B
Mean semi-major axis of the orbit SL-23 R/B
Mean orbital eccentricity SL-23 R/B
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