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 |
2005-12-28 (20 years ago)
|
| Days in orbit | 7554 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 23394 km |
| Apogee | 23478 km |
| Orbit slope (inclination) | 59.02° |
| Laps per day | 2 |
| Height FREGAT R/B | 23443.65 km |
Additional information FREGAT R/B
FREGAT R/B, 28923 is space debris originally from a launch on Wed, 28 Dec 2005 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 28.12.2005y. Average height of ISS FREGAT R/B hundred 23443.65 km. Average velocity FREGAT R/B is 13163.15 km/h. Inclination FREGAT R/B satellite 59.02°.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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