DELTA 2 DEB
Satellite information DELTA 2 DEB
| Spacetrack Directory Name | DELTA 2 DEB |
| Follow DELTA 2 DEB | DELTA 2 DEB Tracker |
| Pass predictions DELTA 2 DEB | Pass predictions DELTA 2 DEB |
| Orbit launches |
1998-01-10 (28 years ago)
|
| Days in orbit | 10467 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 758 km |
| Apogee | 1248 km |
| Orbit slope (inclination) | 26.88° |
| Laps per day | 14 |
| Height DELTA 2 DEB | 994.65 km |
Additional information DELTA 2 DEB
DELTA 2 DEB, 25138 is space debris in LEO originally from a launch on Sat, 10 Jan 1998 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 DEB Date of exalting 10.01.1998y. Average height of ISS DELTA 2 DEB hundred 994.65 km. Average velocity DELTA 2 DEB is 26485.17 km/h. Inclination DELTA 2 DEB satellite 26.88°.TLE
Average velocity DELTA 2 DEB
Average inclination DELTA 2 DEB
Mean right ascension of the ascending node (RAAN) DELTA 2 DEB
Mean argument of perigee DELTA 2 DEB
Mean semi-major axis of the orbit DELTA 2 DEB
Mean orbital eccentricity DELTA 2 DEB
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