TELSTAR 3C R/B(PAM-D)
Satellite information TELSTAR 3C R/B(PAM-D) - TELSTAR 302 R/B [PAM-D
| Spacetrack Directory Name | TELSTAR 3C R/B(PAM-D) |
| Alternative name | TELSTAR 302 R/B [PAM-D |
| Follow TELSTAR 3C R/B(PAM-D) | TELSTAR 3C R/B(PAM-D) Tracker |
| Pass predictions TELSTAR 3C R/B(PAM-D) | Pass predictions TELSTAR 3C R/B(PAM-D) |
| Orbit launches |
1984-08-30 (42 years ago)
|
| Days in orbit | 15349 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 326 km |
| Apogee | 33471 km |
| Orbit slope (inclination) | 24.72° |
| Laps per day | 3 |
| Height TELSTAR 3C R/B(PAM-D) | 22111.85 km |
Additional information TELSTAR 3C R/B(PAM-D)
TELSTAR 3C R/B(PAM-D), 15246 is space debris in HEO originally from a launch on Thu, 30 Aug 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 TELSTAR 3C R/B(PAM-D) Date of exalting 30.08.1984y. Average height of ISS TELSTAR 3C R/B(PAM-D) hundred 22111.85 km. Average velocity TELSTAR 3C R/B(PAM-D) is 12961.36 km/h. Inclination TELSTAR 3C R/B(PAM-D) satellite 24.74°.TLE
Average velocity TELSTAR 3C R/B(PAM-D)
Average inclination TELSTAR 3C R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) TELSTAR 3C R/B(PAM-D)
Mean argument of perigee TELSTAR 3C R/B(PAM-D)
Mean semi-major axis of the orbit TELSTAR 3C R/B(PAM-D)
Mean orbital eccentricity TELSTAR 3C R/B(PAM-D)
ISS
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