ANIK C3 R/B(PAM-D)
Satellite information ANIK C3 R/B(PAM-D) - ANIK C3 R/B [PAM-D]
| Spacetrack Directory Name | ANIK C3 R/B(PAM-D) |
| Alternative name | ANIK C3 R/B [PAM-D] |
| Follow ANIK C3 R/B(PAM-D) | ANIK C3 R/B(PAM-D) Tracker |
| Pass predictions ANIK C3 R/B(PAM-D) | Pass predictions ANIK C3 R/B(PAM-D) |
| Orbit launches |
1982-11-11 (43 years ago)
|
| Days in orbit | 16008 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 351 km |
| Apogee | 33184 km |
| Orbit slope (inclination) | 23.11° |
| Laps per day | 3 |
| Height ANIK C3 R/B(PAM-D) | 22097.6 km |
Additional information ANIK C3 R/B(PAM-D)
ANIK C3 R/B(PAM-D), 13666 is space debris in HEO originally from a launch on Thu, 11 Nov 1982 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 C3 R/B(PAM-D) Date of exalting 11.11.1982y. Average height of ISS ANIK C3 R/B(PAM-D) hundred 22097.6 km. Average velocity ANIK C3 R/B(PAM-D) is 12900.7 km/h. Inclination ANIK C3 R/B(PAM-D) satellite 23.16°.TLE
Average velocity ANIK C3 R/B(PAM-D)
Average inclination ANIK C3 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) ANIK C3 R/B(PAM-D)
Mean argument of perigee ANIK C3 R/B(PAM-D)
Mean semi-major axis of the orbit ANIK C3 R/B(PAM-D)
Mean orbital eccentricity ANIK C3 R/B(PAM-D)
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