INSAT 1B R/B(PAM-D)
Satellite information INSAT 1B R/B(PAM-D) - INSAT-1B R/B [PAM-D]
| Spacetrack Directory Name | INSAT 1B R/B(PAM-D) |
| Alternative name | INSAT-1B R/B [PAM-D] |
| Follow INSAT 1B R/B(PAM-D) | INSAT 1B R/B(PAM-D) Tracker |
| Pass predictions INSAT 1B R/B(PAM-D) | Pass predictions INSAT 1B R/B(PAM-D) |
| Orbit launches |
1983-08-30 (43 years ago)
|
| Days in orbit | 15715 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 252 km |
| Apogee | 20718 km |
| Orbit slope (inclination) | 24.4° |
| Laps per day | 4 |
| Height INSAT 1B R/B(PAM-D) | 12625.65 km |
Additional information INSAT 1B R/B(PAM-D)
INSAT 1B R/B(PAM-D), 14524 is space debris in HEO originally from a launch on Tue, 30 Aug 1983 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 INSAT 1B R/B(PAM-D) Date of exalting 30.08.1983y. Average height of ISS INSAT 1B R/B(PAM-D) hundred 12625.65 km. Average velocity INSAT 1B R/B(PAM-D) is 16197.77 km/h. Inclination INSAT 1B R/B(PAM-D) satellite 24.41°.TLE
Average velocity INSAT 1B R/B(PAM-D)
Average inclination INSAT 1B R/B(PAM-D)
Mean right ascension of the ascending node (RAAN) INSAT 1B R/B(PAM-D)
Mean argument of perigee INSAT 1B R/B(PAM-D)
Mean semi-major axis of the orbit INSAT 1B R/B(PAM-D)
Mean orbital eccentricity INSAT 1B R/B(PAM-D)
ISS
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