INMARSAT 2-F2 R/B(PAM-D)
Satellite information INMARSAT 2-F2 R/B(PAM-D) - INMARSAT 2-F2 R/B(PAM-
| Spacetrack Directory Name | INMARSAT 2-F2 R/B(PAM-D) |
| Alternative name | INMARSAT 2-F2 R/B(PAM- |
| Follow INMARSAT 2-F2 R/B(PAM-D) | INMARSAT 2-F2 R/B(PAM-D) Tracker |
| Pass predictions INMARSAT 2-F2 R/B(PAM-D) | Pass predictions INMARSAT 2-F2 R/B(PAM-D) |
| Orbit launches |
1991-03-08 (35 years ago)
|
| Days in orbit | 12968 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 287 km |
| Apogee | 10023 km |
| Orbit slope (inclination) | 23.2° |
| Laps per day | 8 |
| Height INMARSAT 2-F2 R/B(PAM-D) | 5322.74 km |
Additional information INMARSAT 2-F2 R/B(PAM-D)
INMARSAT 2-F2 R/B(PAM-D), 21151 is space debris originally from a launch on Fri, 08 Mar 1991 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 INMARSAT 2-F2 R/B(PAM-D) Date of exalting 08.03.1991y. Average height of ISS INMARSAT 2-F2 R/B(PAM-D) hundred 5322.74 km. Average velocity INMARSAT 2-F2 R/B(PAM-D) is 20939.96 km/h. Inclination INMARSAT 2-F2 R/B(PAM-D) satellite 23.21°.TLE
Average orbit height INMARSAT 2-F2 R/B(PAM-D)
Average velocity INMARSAT 2-F2 R/B(PAM-D)
Average inclination INMARSAT 2-F2 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) INMARSAT 2-F2 R/B(PAM-D)
Mean argument of perigee INMARSAT 2-F2 R/B(PAM-D)
Mean semi-major axis of the orbit INMARSAT 2-F2 R/B(PAM-D)
Mean orbital eccentricity INMARSAT 2-F2 R/B(PAM-D)
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