ANIK C1 R/B(PAM-D)
Satellite information ANIK C1 R/B(PAM-D) - ANIK C1 R/B [PAM-D]
| Spacetrack Directory Name | ANIK C1 R/B(PAM-D) |
| Alternative name | ANIK C1 R/B [PAM-D] |
| Follow ANIK C1 R/B(PAM-D) | ANIK C1 R/B(PAM-D) Tracker |
| Pass predictions ANIK C1 R/B(PAM-D) | Pass predictions ANIK C1 R/B(PAM-D) |
| Orbit launches |
1985-04-12 (41 years ago)
|
| Days in orbit | 15124 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 316 km |
| Apogee | 30268 km |
| Orbit slope (inclination) | 23.07° |
| Laps per day | 3 |
| Height ANIK C1 R/B(PAM-D) | 19751.14 km |
Additional information ANIK C1 R/B(PAM-D)
ANIK C1 R/B(PAM-D), 15644 is space debris in HEO originally from a launch on Fri, 12 Apr 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 ANIK C1 R/B(PAM-D) Date of exalting 12.04.1985y. Average height of ISS ANIK C1 R/B(PAM-D) hundred 19751.14 km. Average velocity ANIK C1 R/B(PAM-D) is 13580.01 km/h. Inclination ANIK C1 R/B(PAM-D) satellite 23.06°.TLE
Average velocity ANIK C1 R/B(PAM-D)
Average inclination ANIK C1 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) ANIK C1 R/B(PAM-D)
Mean argument of perigee ANIK C1 R/B(PAM-D)
Mean semi-major axis of the orbit ANIK C1 R/B(PAM-D)
Mean orbital eccentricity ANIK C1 R/B(PAM-D)
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