SL-4 R/B
Satellite information SL-4 R/B
| Spacetrack Directory Name | SL-4 R/B |
| Orbit launches |
2026-09-16 |
| Deorbitation |
|
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TTMTR |
| Perigee | 171 km |
| Apogee | 194 km |
| Height SL-4 R/B | 88.6 km |
Additional information SL-4 R/B
SL-4 R/B, 100713 is space debris in LEO originally from a launch on Wed, 16 Sep 2026 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 SL-4 R/B Date of exalting 16.09.2026y. Average height of ISS SL-4 R/B hundred 88.6 km. Average velocity SL-4 R/B is 28280.83 km/h. Inclination SL-4 R/B satellite 51.66°.Average velocity SL-4 R/B
Average inclination SL-4 R/B
Mean right ascension of the ascending node (RAAN) SL-4 R/B
Mean argument of perigee SL-4 R/B
Mean semi-major axis of the orbit SL-4 R/B
Mean orbital eccentricity SL-4 R/B
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