MARCOPOLO 2 R/B(PAM-D)
Satellite information MARCOPOLO 2 R/B(PAM-D) - MARCOPOLO 2 R/B [PAM-D
| Spacetrack Directory Name | MARCOPOLO 2 R/B(PAM-D) |
| Alternative name | MARCOPOLO 2 R/B [PAM-D |
| Follow MARCOPOLO 2 R/B(PAM-D) | MARCOPOLO 2 R/B(PAM-D) Tracker |
| Pass predictions MARCOPOLO 2 R/B(PAM-D) | Pass predictions MARCOPOLO 2 R/B(PAM-D) |
| Orbit launches |
1990-08-18 (36 years ago)
|
| Days in orbit | 13170 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 449 km |
| Apogee | 37084 km |
| Orbit slope (inclination) | 20.79° |
| Laps per day | 2 |
| Height MARCOPOLO 2 R/B(PAM-D) | 25288.82 km |
Additional information MARCOPOLO 2 R/B(PAM-D)
MARCOPOLO 2 R/B(PAM-D), 20764 is space debris in HEO originally from a launch on Sat, 18 Aug 1990 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 MARCOPOLO 2 R/B(PAM-D) Date of exalting 18.08.1990y. Average height of ISS MARCOPOLO 2 R/B(PAM-D) hundred 25288.82 km. Average velocity MARCOPOLO 2 R/B(PAM-D) is 12252.32 km/h. Inclination MARCOPOLO 2 R/B(PAM-D) satellite 20.79°.TLE
Average orbit height MARCOPOLO 2 R/B(PAM-D)
Average velocity MARCOPOLO 2 R/B(PAM-D)
Average inclination MARCOPOLO 2 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) MARCOPOLO 2 R/B(PAM-D)
Mean argument of perigee MARCOPOLO 2 R/B(PAM-D)
Mean semi-major axis of the orbit MARCOPOLO 2 R/B(PAM-D)
Mean orbital eccentricity MARCOPOLO 2 R/B(PAM-D)
ISS
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