APEX R/B
Satellite information APEX R/B
| Spacetrack Directory Name | APEX R/B |
| Follow APEX R/B | APEX R/B Tracker |
| Pass predictions APEX R/B | Pass predictions APEX R/B |
| Orbit launches |
1994-08-03 (32 years ago)
|
| Days in orbit | 11711 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 350 km |
| Apogee | 1650 km |
| Orbit slope (inclination) | 69.92° |
| Laps per day | 14 |
| Height APEX R/B | 802.52 km |
Additional information APEX R/B
APEX R/B, 23198 is space debris in LEO originally from a launch on Wed, 03 Aug 1994 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 APEX R/B Date of exalting 03.08.1994y. Average height of ISS APEX R/B hundred 802.52 km. Average velocity APEX R/B is 26835.78 km/h. Inclination APEX R/B satellite 69.92°.TLE
Average velocity APEX R/B
Average inclination APEX R/B
Mean right ascension of the ascending node (RAAN) APEX R/B
Mean argument of perigee APEX R/B
Mean semi-major axis of the orbit APEX R/B
Mean orbital eccentricity APEX R/B
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