DELTA 4 R/B
Satellite information DELTA 4 R/B
| Spacetrack Directory Name | DELTA 4 R/B |
| Orbit launches |
2020-12-11 |
| Deorbitation |
|
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36189 km |
| Apogee | 38429 km |
| Height DELTA 4 R/B | 37273.11 km |
Additional information DELTA 4 R/B
DELTA 4 R/B, 47238 is space debris in GEO originally from a launch on Fri, 11 Dec 2020 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 DELTA 4 R/B Date of exalting 11.12.2020y. Average height of ISS DELTA 4 R/B hundred 37273.11 km. Average velocity DELTA 4 R/B is 10884.98 km/h. Inclination DELTA 4 R/B satellite 2.95°.Average velocity DELTA 4 R/B
Average inclination DELTA 4 R/B
Mean right ascension of the ascending node (RAAN) DELTA 4 R/B
Mean argument of perigee DELTA 4 R/B
Mean semi-major axis of the orbit DELTA 4 R/B
Mean orbital eccentricity DELTA 4 R/B
ISS
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