IUS R/B(2)
Satellite information IUS R/B(2)
| Spacetrack Directory Name | IUS R/B(2) |
| Orbit launches |
1991-08-02 |
| Deorbitation |
|
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35639 km |
| Apogee | 35945 km |
| Height IUS R/B(2) | 35773.26 km |
Additional information IUS R/B(2)
IUS R/B(2), 21641 is space debris in GEO originally from a launch on Fri, 02 Aug 1991 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 IUS R/B(2) Date of exalting 02.08.1991y. Average height of ISS IUS R/B(2) hundred 35773.26 km. Average velocity IUS R/B(2) is 11070.76 km/h. Inclination IUS R/B(2) satellite 13.71°.Average velocity IUS R/B(2)
Average inclination IUS R/B(2)
Mean right ascension of the ascending node (RAAN) IUS R/B(2)
Mean argument of perigee IUS R/B(2)
Mean semi-major axis of the orbit IUS R/B(2)
Mean orbital eccentricity IUS R/B(2)
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