DELTA 4H R/B
Satellite information DELTA 4H R/B
| Spacetrack Directory Name | DELTA 4H R/B |
| Follow DELTA 4H R/B | DELTA 4H R/B Tracker |
| Pass predictions DELTA 4H R/B | Pass predictions DELTA 4H R/B |
| Orbit launches |
2009-01-18 (17 years ago)
|
| Days in orbit | 6434 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 35846 km |
| Apogee | 38175 km |
| Orbit slope (inclination) | 9.8° |
| Laps per day | 1 |
| Height DELTA 4H R/B | 37033.57 km |
Additional information DELTA 4H R/B
DELTA 4H R/B, 33491 is space debris in GEO originally from a launch on Sun, 18 Jan 2009 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 4H R/B Date of exalting 18.01.2009y. Average height of ISS DELTA 4H R/B hundred 37033.57 km. Average velocity DELTA 4H R/B is 10907.75 km/h. Inclination DELTA 4H R/B satellite 9.79°.TLE
Average velocity DELTA 4H R/B
Average inclination DELTA 4H R/B
Mean right ascension of the ascending node (RAAN) DELTA 4H R/B
Mean argument of perigee DELTA 4H R/B
Mean semi-major axis of the orbit DELTA 4H R/B
Mean orbital eccentricity DELTA 4H R/B
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