AURORA 2 R/B(PAM-D)
Satellite information AURORA 2 R/B(PAM-D) - AURORA 2 R/B [PAM-D]
| Spacetrack Directory Name | AURORA 2 R/B(PAM-D) |
| Alternative name | AURORA 2 R/B [PAM-D] |
| Follow AURORA 2 R/B(PAM-D) | AURORA 2 R/B(PAM-D) Tracker |
| Pass predictions AURORA 2 R/B(PAM-D) | Pass predictions AURORA 2 R/B(PAM-D) |
| Orbit launches |
1991-05-29 (35 years ago)
|
| Days in orbit | 12886 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 1389 km |
| Apogee | 35496 km |
| Orbit slope (inclination) | 24.18° |
| Laps per day | 2 |
| Height AURORA 2 R/B(PAM-D) | 24257 km |
Additional information AURORA 2 R/B(PAM-D)
AURORA 2 R/B(PAM-D), 21394 is space debris in HEO originally from a launch on Wed, 29 May 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 AURORA 2 R/B(PAM-D) Date of exalting 29.05.1991y. Average height of ISS AURORA 2 R/B(PAM-D) hundred 24257 km. Average velocity AURORA 2 R/B(PAM-D) is 12548.17 km/h. Inclination AURORA 2 R/B(PAM-D) satellite 24.16°.TLE
Average velocity AURORA 2 R/B(PAM-D)
Average inclination AURORA 2 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) AURORA 2 R/B(PAM-D)
Mean argument of perigee AURORA 2 R/B(PAM-D)
Mean semi-major axis of the orbit AURORA 2 R/B(PAM-D)
Mean orbital eccentricity AURORA 2 R/B(PAM-D)
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