SATCOM K1 R/B(PAM-D2)
Satellite information SATCOM K1 R/B(PAM-D2) - SATCOM K1 R/B [PAM-D2]
| Spacetrack Directory Name | SATCOM K1 R/B(PAM-D2) |
| Alternative name | SATCOM K1 R/B [PAM-D2] |
| Follow SATCOM K1 R/B(PAM-D2) | SATCOM K1 R/B(PAM-D2) Tracker |
| Pass predictions SATCOM K1 R/B(PAM-D2) | Pass predictions SATCOM K1 R/B(PAM-D2) |
| Orbit launches |
1986-01-12 (40 years ago)
|
| Days in orbit | 14849 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 308 km |
| Apogee | 33331 km |
| Orbit slope (inclination) | 26.83° |
| Laps per day | 3 |
| Height SATCOM K1 R/B(PAM-D2) | 22234.83 km |
Additional information SATCOM K1 R/B(PAM-D2)
SATCOM K1 R/B(PAM-D2), 16483 is space debris in HEO originally from a launch on Sun, 12 Jan 1986 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 K1 R/B(PAM-D2) Date of exalting 12.01.1986y. Average height of ISS SATCOM K1 R/B(PAM-D2) hundred 22234.83 km. Average velocity SATCOM K1 R/B(PAM-D2) is 12945.62 km/h. Inclination SATCOM K1 R/B(PAM-D2) satellite 26.8°.TLE
Average velocity SATCOM K1 R/B(PAM-D2)
Average inclination SATCOM K1 R/B(PAM-D2)
Mean right ascension of the ascending node (RAAN) SATCOM K1 R/B(PAM-D2)
Mean argument of perigee SATCOM K1 R/B(PAM-D2)
Mean semi-major axis of the orbit SATCOM K1 R/B(PAM-D2)
Mean orbital eccentricity SATCOM K1 R/B(PAM-D2)
ISS
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