ANIK D2 R/B(PAM-D)
Satellite information ANIK D2 R/B(PAM-D) - PAM-D
| Spacetrack Directory Name | ANIK D2 R/B(PAM-D) |
| Alternative name | PAM-D |
| Follow ANIK D2 R/B(PAM-D) | ANIK D2 R/B(PAM-D) Tracker |
| Pass predictions ANIK D2 R/B(PAM-D) | Pass predictions ANIK D2 R/B(PAM-D) |
| Orbit launches |
1984-11-08 (41 years ago)
|
| Days in orbit | 15279 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Rocket body |
| WWW | Here |
| Perigee | 366 km |
| Apogee | 33050 km |
| Orbit slope (inclination) | 25.14° |
| Laps per day | 3 |
| Height ANIK D2 R/B(PAM-D) | 22100.37 km |
Additional information ANIK D2 R/B(PAM-D)
ANIK D2 R/B(PAM-D), 15387 is space debris in HEO originally from a launch on Thu, 08 Nov 1984 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 ANIK D2 R/B(PAM-D) Date of exalting 08.11.1984y. Average height of ISS ANIK D2 R/B(PAM-D) hundred 22100.37 km. Average velocity ANIK D2 R/B(PAM-D) is 12948.17 km/h. Inclination ANIK D2 R/B(PAM-D) satellite 25.17°.TLE
Average velocity ANIK D2 R/B(PAM-D)
Average inclination ANIK D2 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) ANIK D2 R/B(PAM-D)
Mean argument of perigee ANIK D2 R/B(PAM-D)
Mean semi-major axis of the orbit ANIK D2 R/B(PAM-D)
Mean orbital eccentricity ANIK D2 R/B(PAM-D)
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