DODECAPOLE 2 DEB
Satellite information DODECAPOLE 2 DEB
| Spacetrack Directory Name | DODECAPOLE 2 DEB |
| Follow DODECAPOLE 2 DEB | DODECAPOLE 2 DEB Tracker |
| Pass predictions DODECAPOLE 2 DEB | Pass predictions DODECAPOLE 2 DEB |
| Orbit launches |
1965-08-13 (61 years ago)
|
| Days in orbit | 22301 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 874 km |
| Apogee | 932 km |
| Orbit slope (inclination) | 90.05° |
| Laps per day | 14 |
| Height DODECAPOLE 2 DEB | 829.87 km |
Additional information DODECAPOLE 2 DEB
DODECAPOLE 2 DEB, 41734 is space debris in LEO originally from a launch on Fri, 13 Aug 1965 UTC launched from the Air Force Western Test Range (AFWTR). 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 DODECAPOLE 2 DEB Date of exalting 13.08.1965y. Average height of ISS DODECAPOLE 2 DEB hundred 829.87 km. Average velocity DODECAPOLE 2 DEB is 26782.32 km/h. Inclination DODECAPOLE 2 DEB satellite 90.05°.TLE
Average velocity DODECAPOLE 2 DEB
Average inclination DODECAPOLE 2 DEB
Mean right ascension of the ascending node (RAAN) DODECAPOLE 2 DEB
Mean argument of perigee DODECAPOLE 2 DEB
Mean semi-major axis of the orbit DODECAPOLE 2 DEB
Mean orbital eccentricity DODECAPOLE 2 DEB
ISS
Buy us a coffee!
