TIROS 2 DEB
Satellite information TIROS 2 DEB
| Spacetrack Directory Name | TIROS 2 DEB |
| Follow TIROS 2 DEB | TIROS 2 DEB Tracker |
| Pass predictions TIROS 2 DEB | Pass predictions TIROS 2 DEB |
| Orbit launches |
1960-11-23 (65 years ago)
|
| Days in orbit | 24011 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 971 km |
| Apogee | 1030 km |
| Orbit slope (inclination) | 47.03° |
| Laps per day | 14 |
| Height TIROS 2 DEB | 1004.38 km |
Additional information TIROS 2 DEB
TIROS 2 DEB *, 5922 is space debris in LEO originally from a launch on Wed, 23 Nov 1960 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 TIROS 2 DEB Date of exalting 23.11.1960y. Average height of ISS TIROS 2 DEB hundred 1004.38 km. Average velocity TIROS 2 DEB is 26466.35 km/h. Inclination TIROS 2 DEB satellite 47.03°.TLE
Average velocity TIROS 2 DEB
Average inclination TIROS 2 DEB
Mean right ascension of the ascending node (RAAN) TIROS 2 DEB
Mean argument of perigee TIROS 2 DEB
Mean semi-major axis of the orbit TIROS 2 DEB
Mean orbital eccentricity TIROS 2 DEB
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