DELTA 2 R/B(2)
Satellite information DELTA 2 R/B(2)
| Spacetrack Directory Name | DELTA 2 R/B(2) |
| Follow DELTA 2 R/B(2) | DELTA 2 R/B(2) Tracker |
| Pass predictions DELTA 2 R/B(2) | Pass predictions DELTA 2 R/B(2) |
| Orbit launches |
1993-12-08 (32 years ago)
|
| Days in orbit | 11961 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 835 km |
| Apogee | 35741 km |
| Orbit slope (inclination) | 22.93° |
| Laps per day | 2 |
| Height DELTA 2 R/B(2) | 24525.73 km |
Additional information DELTA 2 R/B(2)
DELTA 2 R/B(2), 22923 is space debris in HEO originally from a launch on Wed, 08 Dec 1993 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 2 R/B(2) Date of exalting 08.12.1993y. Average height of ISS DELTA 2 R/B(2) hundred 24525.73 km. Average velocity DELTA 2 R/B(2) is 12409.28 km/h. Inclination DELTA 2 R/B(2) satellite 22.93°.TLE
Average velocity DELTA 2 R/B(2)
Average inclination DELTA 2 R/B(2)
Mean right ascension of the ascending node (RAAN) DELTA 2 R/B(2)
Mean argument of perigee DELTA 2 R/B(2)
Mean semi-major axis of the orbit DELTA 2 R/B(2)
Mean orbital eccentricity DELTA 2 R/B(2)
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