THORAD DELTA 1 R/B(2)
Satellite information THORAD DELTA 1 R/B(2)
| Spacetrack Directory Name | THORAD DELTA 1 R/B(2) |
| Follow THORAD DELTA 1 R/B(2) | THORAD DELTA 1 R/B(2) Tracker |
| Pass predictions THORAD DELTA 1 R/B(2) | Pass predictions THORAD DELTA 1 R/B(2) |
| Orbit launches |
1974-12-19 (51 years ago)
|
| Days in orbit | 18892 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 399 km |
| Apogee | 35495 km |
| Orbit slope (inclination) | 13.03° |
| Laps per day | 2 |
| Height THORAD DELTA 1 R/B(2) | 24008.42 km |
Additional information THORAD DELTA 1 R/B(2)
THORAD DELTA 1 R/B(2), 9330 is space debris in HEO originally from a launch on Thu, 19 Dec 1974 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 THORAD DELTA 1 R/B(2) Date of exalting 19.12.1974y. Average height of ISS THORAD DELTA 1 R/B(2) hundred 24008.42 km. Average velocity THORAD DELTA 1 R/B(2) is 12498.4 km/h. Inclination THORAD DELTA 1 R/B(2) satellite 13.08°.TLE
Average velocity THORAD DELTA 1 R/B(2)
Average inclination THORAD DELTA 1 R/B(2)
Mean right ascension of the ascending node (RAAN) THORAD DELTA 1 R/B(2)
Mean argument of perigee THORAD DELTA 1 R/B(2)
Mean semi-major axis of the orbit THORAD DELTA 1 R/B(2)
Mean orbital eccentricity THORAD DELTA 1 R/B(2)
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