TANSEI 3 DEB
Satellite information TANSEI 3 DEB
| Spacetrack Directory Name | TANSEI 3 DEB |
| Follow TANSEI 3 DEB | TANSEI 3 DEB Tracker |
| Pass predictions TANSEI 3 DEB | Pass predictions TANSEI 3 DEB |
| Orbit launches |
1977-02-19 (49 years ago)
|
| Days in orbit | 18126 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | KSCUT (Uchinoura Space Center, Japan) |
| Perigee | 804 km |
| Apogee | 3766 km |
| Orbit slope (inclination) | 65.74° |
| Laps per day | 11 |
| Height TANSEI 3 DEB | 2420.93 km |
Additional information TANSEI 3 DEB
TANSEI 3 DEB, 14512 is space debris in LEO originally from a launch on Sat, 19 Feb 1977 UTC launched from the Kagoshima Space Center University Of Tokyo (KSCUT). 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 TANSEI 3 DEB Date of exalting 19.02.1977y. Average height of ISS TANSEI 3 DEB hundred 2420.93 km. Average velocity TANSEI 3 DEB is 24237.06 km/h. Inclination TANSEI 3 DEB satellite 65.75°.TLE
Average velocity TANSEI 3 DEB
Average inclination TANSEI 3 DEB
Mean right ascension of the ascending node (RAAN) TANSEI 3 DEB
Mean argument of perigee TANSEI 3 DEB
Mean semi-major axis of the orbit TANSEI 3 DEB
Mean orbital eccentricity TANSEI 3 DEB
ISS
Buy us a coffee!
