IABS R/B
Satellite information IABS R/B
| Spacetrack Directory Name | IABS R/B |
| Follow IABS R/B | IABS R/B Tracker |
| Pass predictions IABS R/B | Pass predictions IABS R/B |
| Orbit launches |
1993-11-28 (32 years ago)
|
| Days in orbit | 11971 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35603 km |
| Apogee | 36135 km |
| Orbit slope (inclination) | 13.73° |
| Laps per day | 1 |
| Height IABS R/B | 35864.73 km |
Additional information IABS R/B
IABS R/B, 22916 is space debris in GEO originally from a launch on Sun, 28 Nov 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 IABS R/B Date of exalting 28.11.1993y. Average height of ISS IABS R/B hundred 35864.73 km. Average velocity IABS R/B is 11058.73 km/h. Inclination IABS R/B satellite 13.74°.TLE
Average velocity IABS R/B
Average inclination IABS R/B
Mean right ascension of the ascending node (RAAN) IABS R/B
Mean argument of perigee IABS R/B
Mean semi-major axis of the orbit IABS R/B
Mean orbital eccentricity IABS R/B
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