TITAN 3 R/B(2)
Satellite information TITAN 3 R/B(2)
| Spacetrack Directory Name | TITAN 3 R/B(2) |
| Follow TITAN 3 R/B(2) | TITAN 3 R/B(2) Tracker |
| Pass predictions TITAN 3 R/B(2) | Pass predictions TITAN 3 R/B(2) |
| Orbit launches |
1990-06-23 (36 years ago)
|
| Days in orbit | 13226 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 267 km |
| Apogee | 32784 km |
| Orbit slope (inclination) | 24.27° |
| Laps per day | 3 |
| Height TITAN 3 R/B(2) | 21282.94 km |
Additional information TITAN 3 R/B(2)
TITAN 3 R/B(2), 20669 is space debris in HEO originally from a launch on Sat, 23 Jun 1990 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 TITAN 3 R/B(2) Date of exalting 23.06.1990y. Average height of ISS TITAN 3 R/B(2) hundred 21282.94 km. Average velocity TITAN 3 R/B(2) is 13180.42 km/h. Inclination TITAN 3 R/B(2) satellite 24.22°.TLE
Average velocity TITAN 3 R/B(2)
Average inclination TITAN 3 R/B(2)
Mean right ascension of the ascending node (RAAN) TITAN 3 R/B(2)
Mean argument of perigee TITAN 3 R/B(2)
Mean semi-major axis of the orbit TITAN 3 R/B(2)
Mean orbital eccentricity TITAN 3 R/B(2)
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