DELTA 2 R/B(1)
Satellite information DELTA 2 R/B(1)
| Spacetrack Directory Name | DELTA 2 R/B(1) |
| Follow DELTA 2 R/B(1) | DELTA 2 R/B(1) Tracker |
| Pass predictions DELTA 2 R/B(1) | Pass predictions DELTA 2 R/B(1) |
| Orbit launches |
1998-10-24 (27 years ago)
|
| Days in orbit | 10180 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 533 km |
| Apogee | 1000 km |
| Orbit slope (inclination) | 31.43° |
| Laps per day | 14 |
| Height DELTA 2 R/B(1) | 749.72 km |
Additional information DELTA 2 R/B(1)
DELTA 2 R/B(1), 25510 is space debris in LEO originally from a launch on Sat, 24 Oct 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 R/B(1) Date of exalting 24.10.1998y. Average height of ISS DELTA 2 R/B(1) hundred 749.72 km. Average velocity DELTA 2 R/B(1) is 26936.29 km/h. Inclination DELTA 2 R/B(1) satellite 31.43°.TLE
Average velocity DELTA 2 R/B(1)
Average inclination DELTA 2 R/B(1)
Mean right ascension of the ascending node (RAAN) DELTA 2 R/B(1)
Mean argument of perigee DELTA 2 R/B(1)
Mean semi-major axis of the orbit DELTA 2 R/B(1)
Mean orbital eccentricity DELTA 2 R/B(1)
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