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 |
2017-09-22 (8 years ago)
|
| Days in orbit | 3286 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| WWW | Here |
| Perigee | 19292 km |
| Apogee | 19856 km |
| Orbit slope (inclination) | 63.96° |
| Laps per day | 2 |
| Height FREGAT R/B | 19584.1 km |
Additional information FREGAT R/B
FREGAT R/B, 42940 is space debris in MEO originally from a launch on Fri, 22 Sep 2017 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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 22.09.2017y. Average height of ISS FREGAT R/B hundred 19584.1 km. Average velocity FREGAT R/B is 14108.09 km/h. Inclination FREGAT R/B satellite 63.96°.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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