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 |
2026-07-19 (2 months ago)
|
| Days in orbit | 63 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PKMTR |
| Perigee | 287 km |
| Apogee | 319 km |
| Orbit slope (inclination) | 82.28° |
| Laps per day | 16 |
| Height FREGAT R/B | 282.88 km |
Additional information FREGAT R/B
FREGAT R/B, 100142 is space debris in LEO originally from a launch on Sun, 19 Jul 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 19.07.2026y. Average height of ISS FREGAT R/B hundred 282.88 km. Average velocity FREGAT R/B is 27860.67 km/h. Inclination FREGAT R/B satellite 82.28°.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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