SATCOM K2 R/B(PAM-D2)
Satellite information SATCOM K2 R/B(PAM-D2) - SATCOM K2 R/B [PAM-D2]
| Spacetrack Directory Name | SATCOM K2 R/B(PAM-D2) |
| Alternative name | SATCOM K2 R/B [PAM-D2] |
| Follow SATCOM K2 R/B(PAM-D2) | SATCOM K2 R/B(PAM-D2) Tracker |
| Pass predictions SATCOM K2 R/B(PAM-D2) | Pass predictions SATCOM K2 R/B(PAM-D2) |
| Orbit launches |
1985-11-27 (40 years ago)
|
| Days in orbit | 14895 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 370 km |
| Apogee | 33969 km |
| Orbit slope (inclination) | 26.69° |
| Laps per day | 2 |
| Height SATCOM K2 R/B(PAM-D2) | 22976.49 km |
Additional information SATCOM K2 R/B(PAM-D2)
SATCOM K2 R/B(PAM-D2), 16295 is space debris in HEO originally from a launch on Wed, 27 Nov 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 SATCOM K2 R/B(PAM-D2) Date of exalting 27.11.1985y. Average height of ISS SATCOM K2 R/B(PAM-D2) hundred 22976.49 km. Average velocity SATCOM K2 R/B(PAM-D2) is 12717.6 km/h. Inclination SATCOM K2 R/B(PAM-D2) satellite 26.71°.TLE
Average velocity SATCOM K2 R/B(PAM-D2)
Average inclination SATCOM K2 R/B(PAM-D2)
Mean right ascension of the ascending node (RAAN) SATCOM K2 R/B(PAM-D2)
Mean argument of perigee SATCOM K2 R/B(PAM-D2)
Mean semi-major axis of the orbit SATCOM K2 R/B(PAM-D2)
Mean orbital eccentricity SATCOM K2 R/B(PAM-D2)
ISS
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