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 |
2017-05-18 (9 years ago)
|
| Days in orbit | 3413 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| WWW | Here |
| Perigee | 2344 km |
| Apogee | 31331 km |
| Orbit slope (inclination) | 6.63° |
| Laps per day | 2 |
| Height FREGAT R/B | 21331.74 km |
Additional information FREGAT R/B
FREGAT R/B, 42710 is space debris in HEO originally from a launch on Thu, 18 May 2017 UTC launched from the French Guiana (FRGUI). 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 18.05.2017y. Average height of ISS FREGAT R/B hundred 21331.74 km. Average velocity FREGAT R/B is 13356.85 km/h. Inclination FREGAT R/B satellite 6.68°.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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