SPACENET 4 R/B(PAM-D)
Satellite information SPACENET 4 R/B(PAM-D) - SPACENET 4 R/B [PAM-D]
| Spacetrack Directory Name | SPACENET 4 R/B(PAM-D) |
| Alternative name | SPACENET 4 R/B [PAM-D] |
| Follow SPACENET 4 R/B(PAM-D) | SPACENET 4 R/B(PAM-D) Tracker |
| Pass predictions SPACENET 4 R/B(PAM-D) | Pass predictions SPACENET 4 R/B(PAM-D) |
| Orbit launches |
1991-04-13 (35 years ago)
|
| Days in orbit | 12932 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 1291 km |
| Apogee | 35942 km |
| Orbit slope (inclination) | 21.98° |
| Laps per day | 2 |
| Height SPACENET 4 R/B(PAM-D) | 24503.63 km |
Additional information SPACENET 4 R/B(PAM-D)
SPACENET 4 R/B(PAM-D), 21229 is space debris in HEO originally from a launch on Sat, 13 Apr 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 SPACENET 4 R/B(PAM-D) Date of exalting 13.04.1991y. Average height of ISS SPACENET 4 R/B(PAM-D) hundred 24503.63 km. Average velocity SPACENET 4 R/B(PAM-D) is 12524.48 km/h. Inclination SPACENET 4 R/B(PAM-D) satellite 21.98°.TLE
Average velocity SPACENET 4 R/B(PAM-D)
Average inclination SPACENET 4 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) SPACENET 4 R/B(PAM-D)
Mean argument of perigee SPACENET 4 R/B(PAM-D)
Mean semi-major axis of the orbit SPACENET 4 R/B(PAM-D)
Mean orbital eccentricity SPACENET 4 R/B(PAM-D)
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