SBS 3 R/B(PAM-D)
Satellite information SBS 3 R/B(PAM-D) - SBS 3 R/B [PAM-D]
| Spacetrack Directory Name | SBS 3 R/B(PAM-D) |
| Alternative name | SBS 3 R/B [PAM-D] |
| Follow SBS 3 R/B(PAM-D) | SBS 3 R/B(PAM-D) Tracker |
| Pass predictions SBS 3 R/B(PAM-D) | Pass predictions SBS 3 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 | 341 km |
| Apogee | 33289 km |
| Orbit slope (inclination) | 23.57° |
| Laps per day | 3 |
| Height SBS 3 R/B(PAM-D) | 22186.03 km |
Additional information SBS 3 R/B(PAM-D)
SBS 3 R/B(PAM-D), 13658 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 SBS 3 R/B(PAM-D) Date of exalting 11.11.1982y. Average height of ISS SBS 3 R/B(PAM-D) hundred 22186.03 km. Average velocity SBS 3 R/B(PAM-D) is 12951.51 km/h. Inclination SBS 3 R/B(PAM-D) satellite 23.58°.TLE
Average velocity SBS 3 R/B(PAM-D)
Average inclination SBS 3 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) SBS 3 R/B(PAM-D)
Mean argument of perigee SBS 3 R/B(PAM-D)
Mean semi-major axis of the orbit SBS 3 R/B(PAM-D)
Mean orbital eccentricity SBS 3 R/B(PAM-D)
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