ANIK C2 R/B(PAM-D)
Satellite information ANIK C2 R/B(PAM-D) - ANIK C2 R/B [PAM-D]
| Spacetrack Directory Name | ANIK C2 R/B(PAM-D) |
| Alternative name | ANIK C2 R/B [PAM-D] |
| Follow ANIK C2 R/B(PAM-D) | ANIK C2 R/B(PAM-D) Tracker |
| Pass predictions ANIK C2 R/B(PAM-D) | Pass predictions ANIK C2 R/B(PAM-D) |
| Orbit launches |
1983-06-18 (43 years ago)
|
| Days in orbit | 15788 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 333 km |
| Apogee | 31148 km |
| Orbit slope (inclination) | 23.02° |
| Laps per day | 3 |
| Height ANIK C2 R/B(PAM-D) | 20459.33 km |
Additional information ANIK C2 R/B(PAM-D)
ANIK C2 R/B(PAM-D), 14135 is space debris in HEO originally from a launch on Sat, 18 Jun 1983 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 C2 R/B(PAM-D) Date of exalting 18.06.1983y. Average height of ISS ANIK C2 R/B(PAM-D) hundred 20459.33 km. Average velocity ANIK C2 R/B(PAM-D) is 13410.48 km/h. Inclination ANIK C2 R/B(PAM-D) satellite 22.99°.TLE
Average velocity ANIK C2 R/B(PAM-D)
Average inclination ANIK C2 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) ANIK C2 R/B(PAM-D)
Mean argument of perigee ANIK C2 R/B(PAM-D)
Mean semi-major axis of the orbit ANIK C2 R/B(PAM-D)
Mean orbital eccentricity ANIK C2 R/B(PAM-D)
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