TANSEI 3 (MS-T3)
Satellite information TANSEI 3 (MS-T3)
| Spacetrack Directory Name | TANSEI 3 (MS-T3) |
| Follow TANSEI 3 (MS-T3) | TANSEI 3 (MS-T3) Tracker |
| Pass predictions TANSEI 3 (MS-T3) | Pass predictions TANSEI 3 (MS-T3) |
| 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 | 806 km |
| Apogee | 3795 km |
| Orbit slope (inclination) | 65.76° |
| Laps per day | 11 |
| Height TANSEI 3 (MS-T3) | 2440.24 km |
Additional information TANSEI 3 (MS-T3)
TANSEI 3 (MS-T3), 9841 is a payload satellite owned by ISAS (JP) in LEO that was launched on Sat, 19 Feb 1977 UTC via a MU-3H launch vehicle from the Kagoshima Space Center University Of Tokyo (KSCUT). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite TANSEI 3 (MS-T3) Date of exalting 19.02.1977y. Average height of ISS TANSEI 3 (MS-T3) hundred 2440.24 km. Average velocity TANSEI 3 (MS-T3) is 24208 km/h. Inclination TANSEI 3 (MS-T3) satellite 65.76°.TLE
Average velocity TANSEI 3 (MS-T3)
Average inclination TANSEI 3 (MS-T3)
Mean right ascension of the ascending node (RAAN) TANSEI 3 (MS-T3)
Mean argument of perigee TANSEI 3 (MS-T3)
Mean semi-major axis of the orbit TANSEI 3 (MS-T3)
Mean orbital eccentricity TANSEI 3 (MS-T3)
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