FREGAT R/B
Satellite information FREGAT R/B
| Spacetrack Directory Name | FREGAT R/B |
| Follow FREGAT R/B | FREGAT R/B Tracker |
| Pass predictions FREGAT R/B | Pass predictions FREGAT R/B |
| Orbit launches |
2015-12-11 (10 years ago)
|
| Days in orbit | 3982 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| WWW | Here |
| Perigee | 34295 km |
| Apogee | 35839 km |
| Orbit slope (inclination) | 8.45° |
| Laps per day | 1 |
| Height FREGAT R/B | 35074.7 km |
Additional information FREGAT R/B
FREGAT R/B, 41106 is space debris in GEO originally from a launch on Fri, 11 Dec 2015 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 FREGAT R/B Date of exalting 11.12.2015y. Average height of ISS FREGAT R/B hundred 35074.7 km. Average velocity FREGAT R/B is 11163.63 km/h. Inclination FREGAT R/B satellite 8.35°.TLE
Average velocity FREGAT R/B
Average inclination FREGAT R/B
Mean right ascension of the ascending node (RAAN) FREGAT R/B
Mean argument of perigee FREGAT R/B
Mean semi-major axis of the orbit FREGAT R/B
Mean orbital eccentricity FREGAT R/B
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