SAKURA 2A (CS-2A)
Satellite information SAKURA 2A (CS-2A)
| Spacetrack Directory Name | SAKURA 2A (CS-2A) |
| Follow SAKURA 2A (CS-2A) | SAKURA 2A (CS-2A) Tracker |
| Pass predictions SAKURA 2A (CS-2A) | Pass predictions SAKURA 2A (CS-2A) |
| Orbit launches |
1983-02-04 (43 years ago)
|
| Days in orbit | 15918 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 35989 km |
| Apogee | 36075 km |
| Orbit slope (inclination) | 10.16° |
| Laps per day | 1 |
| Height SAKURA 2A (CS-2A) | 36030.29 km |
Additional information SAKURA 2A (CS-2A)
SAKURA 2A (CS-2A), 13782 is a payload satellite owned by NASDA (JP) in GEO that was launched on Fri, 04 Feb 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 2A (CS-2A) Date of exalting 04.02.1983y. Average height of ISS SAKURA 2A (CS-2A) hundred 36030.29 km. Average velocity SAKURA 2A (CS-2A) is 11037.12 km/h. Inclination SAKURA 2A (CS-2A) satellite 10.18°.TLE
Average velocity SAKURA 2A (CS-2A)
Average inclination SAKURA 2A (CS-2A)
Mean right ascension of the ascending node (RAAN) SAKURA 2A (CS-2A)
Mean argument of perigee SAKURA 2A (CS-2A)
Mean semi-major axis of the orbit SAKURA 2A (CS-2A)
Mean orbital eccentricity SAKURA 2A (CS-2A)
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