ATLAS 28E R/B
Satellite information ATLAS 28E R/B
| Spacetrack Directory Name | ATLAS 28E R/B |
| Follow ATLAS 28E R/B | ATLAS 28E R/B Tracker |
| Pass predictions ATLAS 28E R/B | Pass predictions ATLAS 28E R/B |
| Orbit launches |
1990-04-11 (36 years ago)
|
| Days in orbit | 13288 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 600 km |
| Apogee | 694 km |
| Orbit slope (inclination) | 89.87° |
| Laps per day | 15 |
| Height ATLAS 28E R/B | 640.2 km |
Additional information ATLAS 28E R/B
ATLAS 28E R/B, 20563 is space debris in LEO originally from a launch on Wed, 11 Apr 1990 UTC launched 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 28E R/B Date of exalting 11.04.1990y. Average height of ISS ATLAS 28E R/B hundred 640.2 km. Average velocity ATLAS 28E R/B is 27141.88 km/h. Inclination ATLAS 28E R/B satellite 89.87°.TLE
Average velocity ATLAS 28E R/B
Average inclination ATLAS 28E R/B
Mean right ascension of the ascending node (RAAN) ATLAS 28E R/B
Mean argument of perigee ATLAS 28E R/B
Mean semi-major axis of the orbit ATLAS 28E R/B
Mean orbital eccentricity ATLAS 28E R/B
ISS
Buy us a coffee!
