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 |
1985-10-03 (40 years ago)
|
| Days in orbit | 14950 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35316 km |
| Apogee | 35806 km |
| Orbit slope (inclination) | 9.91° |
| Laps per day | 1 |
| Height IUS R/B(2) | 35559.99 km |
Additional information IUS R/B(2)
IUS R/B(2), 16119 is space debris in GEO originally from a launch on Thu, 03 Oct 1985 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 03.10.1985y. Average height of ISS IUS R/B(2) hundred 35559.99 km. Average velocity IUS R/B(2) is 11098.94 km/h. Inclination IUS R/B(2) satellite 9.93°.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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