IUS R/B(2)
Satellite information IUS R/B(2)
| Spacetrack Directory Name | IUS R/B(2) |
| Follow IUS R/B(2) | IUS R/B(2) Tracker |
| Pass predictions IUS R/B(2) | Pass predictions IUS R/B(2) |
| Orbit launches |
1983-04-04 (43 years ago)
|
| Days in orbit | 15863 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 22315 km |
| Apogee | 35081 km |
| Orbit slope (inclination) | 4.68° |
| Laps per day | 1 |
| Height IUS R/B(2) | 29351.56 km |
Additional information IUS R/B(2)
IUS R/B(2), 13970 is space debris originally from a launch on Mon, 04 Apr 1983 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 04.04.1983y. Average height of ISS IUS R/B(2) hundred 29351.56 km. Average velocity IUS R/B(2) is 12020.27 km/h. Inclination IUS R/B(2) satellite 4.66°.TLE
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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