ATLAS H R/B
Satellite information ATLAS H R/B
| Spacetrack Directory Name | ATLAS H R/B |
| Follow ATLAS H R/B | ATLAS H R/B Tracker |
| Pass predictions ATLAS H R/B | Pass predictions ATLAS H R/B |
| Orbit launches |
1987-05-15 (39 years ago)
|
| Days in orbit | 14350 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 513 km |
| Apogee | 1682 km |
| Orbit slope (inclination) | 63.32° |
| Laps per day | 14 |
| Height ATLAS H R/B | 1093.89 km |
Additional information ATLAS H R/B
ATLAS H R/B, 17998 is space debris in LEO originally from a launch on Fri, 15 May 1987 UTC via an ATLAS H launch vehicle from the Air Force Western Test Range (AFWTR). 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 ATLAS H R/B Date of exalting 15.05.1987y. Average height of ISS ATLAS H R/B hundred 1093.89 km. Average velocity ATLAS H R/B is 26306.83 km/h. Inclination ATLAS H R/B satellite 63.32°.TLE
Average velocity ATLAS H R/B
Average inclination ATLAS H R/B
Mean right ascension of the ascending node (RAAN) ATLAS H R/B
Mean argument of perigee ATLAS H R/B
Mean semi-major axis of the orbit ATLAS H R/B
Mean orbital eccentricity ATLAS H R/B
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