SAKURA 2B (CS-2B)
Satellite information SAKURA 2B (CS-2B)
| Spacetrack Directory Name | SAKURA 2B (CS-2B) |
| Follow SAKURA 2B (CS-2B) | SAKURA 2B (CS-2B) Tracker |
| Pass predictions SAKURA 2B (CS-2B) | Pass predictions SAKURA 2B (CS-2B) |
| Orbit launches |
1983-08-05 (43 years ago)
|
| Days in orbit | 15736 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 36174 km |
| Apogee | 36227 km |
| Orbit slope (inclination) | 10.98° |
| Laps per day | 1 |
| Height SAKURA 2B (CS-2B) | 36200.95 km |
Additional information SAKURA 2B (CS-2B)
SAKURA 2B (CS-2B), 14248 is a payload satellite owned by NASDA (JP) in GEO that was launched on Fri, 05 Aug 1983 UTC via an N-2 launch vehicle from the Tanegashima Space Center (TNSTA). 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 SAKURA 2B (CS-2B) Date of exalting 05.08.1983y. Average height of ISS SAKURA 2B (CS-2B) hundred 36200.95 km. Average velocity SAKURA 2B (CS-2B) is 11014.95 km/h. Inclination SAKURA 2B (CS-2B) satellite 11°.TLE
Average velocity SAKURA 2B (CS-2B)
Average inclination SAKURA 2B (CS-2B)
Mean right ascension of the ascending node (RAAN) SAKURA 2B (CS-2B)
Mean argument of perigee SAKURA 2B (CS-2B)
Mean semi-major axis of the orbit SAKURA 2B (CS-2B)
Mean orbital eccentricity SAKURA 2B (CS-2B)
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