TOS R/B
Satellite information TOS R/B
| Spacetrack Directory Name | TOS R/B |
| Follow TOS R/B | TOS R/B Tracker |
| Pass predictions TOS R/B | Pass predictions TOS R/B |
| Orbit launches |
1993-09-12 (32 years ago)
|
| Days in orbit | 12048 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 328 km |
| Apogee | 38296 km |
| Orbit slope (inclination) | 15.32° |
| Laps per day | 2 |
| Height TOS R/B | 25934.39 km |
Additional information TOS R/B
TOS R/B, 22797 is space debris in HEO originally from an American launch on Sun, 12 Sep 1993 UTC launched from the Air Force Eastern Test Range (AFETR). 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 TOS R/B Date of exalting 12.09.1993y. Average height of ISS TOS R/B hundred 25934.39 km. Average velocity TOS R/B is 12098.54 km/h. Inclination TOS R/B satellite 15.29°.TLE
Average velocity TOS R/B
Average inclination TOS R/B
Mean right ascension of the ascending node (RAAN) TOS R/B
Mean argument of perigee TOS R/B
Mean semi-major axis of the orbit TOS R/B
Mean orbital eccentricity TOS R/B
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