ARABSAT 1B R/B(PAM-D)
Satellite information ARABSAT 1B R/B(PAM-D) - ARABSAT-1B R/B [PAM-D]
| Spacetrack Directory Name | ARABSAT 1B R/B(PAM-D) |
| Alternative name | ARABSAT-1B R/B [PAM-D] |
| Follow ARABSAT 1B R/B(PAM-D) | ARABSAT 1B R/B(PAM-D) Tracker |
| Pass predictions ARABSAT 1B R/B(PAM-D) | Pass predictions ARABSAT 1B R/B(PAM-D) |
| Orbit launches |
1985-06-17 (41 years ago)
|
| Days in orbit | 15058 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 369 km |
| Apogee | 33998 km |
| Orbit slope (inclination) | 27.12° |
| Laps per day | 2 |
| Height ARABSAT 1B R/B(PAM-D) | 22968.09 km |
Additional information ARABSAT 1B R/B(PAM-D)
ARABSAT 1B R/B(PAM-D), 15836 is space debris in HEO originally from a launch on Mon, 17 Jun 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 ARABSAT 1B R/B(PAM-D) Date of exalting 17.06.1985y. Average height of ISS ARABSAT 1B R/B(PAM-D) hundred 22968.09 km. Average velocity ARABSAT 1B R/B(PAM-D) is 12709.14 km/h. Inclination ARABSAT 1B R/B(PAM-D) satellite 27.12°.TLE
Average velocity ARABSAT 1B R/B(PAM-D)
Average inclination ARABSAT 1B R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) ARABSAT 1B R/B(PAM-D)
Mean argument of perigee ARABSAT 1B R/B(PAM-D)
Mean semi-major axis of the orbit ARABSAT 1B R/B(PAM-D)
Mean orbital eccentricity ARABSAT 1B R/B(PAM-D)
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