MORELOS 2 R/B(PAM-D)
Satellite information MORELOS 2 R/B(PAM-D) - MORELOS 2 R/B [PAM-D]
| Spacetrack Directory Name | MORELOS 2 R/B(PAM-D) |
| Alternative name | MORELOS 2 R/B [PAM-D] |
| Follow MORELOS 2 R/B(PAM-D) | MORELOS 2 R/B(PAM-D) Tracker |
| Pass predictions MORELOS 2 R/B(PAM-D) | Pass predictions MORELOS 2 R/B(PAM-D) |
| Orbit launches |
1985-11-27 (40 years ago)
|
| Days in orbit | 14895 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 351 km |
| Apogee | 34729 km |
| Orbit slope (inclination) | 25.34° |
| Laps per day | 2 |
| Height MORELOS 2 R/B(PAM-D) | 23432.46 km |
Additional information MORELOS 2 R/B(PAM-D)
MORELOS 2 R/B(PAM-D), 16293 is space debris in HEO originally from a launch on Wed, 27 Nov 1985 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 MORELOS 2 R/B(PAM-D) Date of exalting 27.11.1985y. Average height of ISS MORELOS 2 R/B(PAM-D) hundred 23432.46 km. Average velocity MORELOS 2 R/B(PAM-D) is 12600.46 km/h. Inclination MORELOS 2 R/B(PAM-D) satellite 25.32°.TLE
Average velocity MORELOS 2 R/B(PAM-D)
Average inclination MORELOS 2 R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) MORELOS 2 R/B(PAM-D)
Mean argument of perigee MORELOS 2 R/B(PAM-D)
Mean semi-major axis of the orbit MORELOS 2 R/B(PAM-D)
Mean orbital eccentricity MORELOS 2 R/B(PAM-D)
ISS
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