NATO 4A R/B(PAM-D)
Satellite information NATO 4A R/B(PAM-D) - NATO 4A R/B [PAM-D]
| Spacetrack Directory Name | NATO 4A R/B(PAM-D) |
| Alternative name | NATO 4A R/B [PAM-D] |
| Follow NATO 4A R/B(PAM-D) | NATO 4A R/B(PAM-D) Tracker |
| Pass predictions NATO 4A R/B(PAM-D) | Pass predictions NATO 4A R/B(PAM-D) |
| Orbit launches |
1991-01-08 (35 years ago)
|
| Days in orbit | 13027 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 765 km |
| Apogee | 35455 km |
| Orbit slope (inclination) | 25.98° |
| Laps per day | 2 |
| Height NATO 4A R/B(PAM-D) | 24230.71 km |
Additional information NATO 4A R/B(PAM-D)
NATO 4A R/B(PAM-D), 21049 is space debris in HEO originally from a launch on Tue, 08 Jan 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 NATO 4A R/B(PAM-D) Date of exalting 08.01.1991y. Average height of ISS NATO 4A R/B(PAM-D) hundred 24230.71 km. Average velocity NATO 4A R/B(PAM-D) is 12486.65 km/h. Inclination NATO 4A R/B(PAM-D) satellite 25.99°.TLE
Average velocity NATO 4A R/B(PAM-D)
Average inclination NATO 4A R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) NATO 4A R/B(PAM-D)
Mean argument of perigee NATO 4A R/B(PAM-D)
Mean semi-major axis of the orbit NATO 4A R/B(PAM-D)
Mean orbital eccentricity NATO 4A R/B(PAM-D)
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