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 |
2026-08-24 (27 days ago)
|
| Days in orbit | 27 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PKMTR |
| Perigee | 19217 km |
| Apogee | 19342 km |
| Orbit slope (inclination) | 64.79° |
| Laps per day | 2 |
| Height FREGAT R/B | 19283.96 km |
Additional information FREGAT R/B
FREGAT R/B, 100461 is space debris in MEO originally from a launch on Mon, 24 Aug 2026 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 24.08.2026y. Average height of ISS FREGAT R/B hundred 19283.96 km. Average velocity FREGAT R/B is 14190.25 km/h. Inclination FREGAT R/B satellite 64.8°.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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