CS 3B
Satellite information CS 3B - SAKURA-3B (CS-3B)
| Spacetrack Directory Name | CS 3B |
| Alternative name | SAKURA-3B (CS-3B) |
| Follow CS 3B | CS 3B Tracker |
| Pass predictions CS 3B | Pass predictions CS 3B |
| Orbit launches |
1988-09-16 (37 years ago)
|
| Days in orbit | 13867 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 36054 km |
| Apogee | 36113 km |
| Orbit slope (inclination) | 14.88° |
| Laps per day | 1 |
| Height CS 3B | 36082.73 km |
Additional information CS 3B
CS 3B, 19508 is a Japanese payload satellite in GEO that was launched on Fri, 16 Sep 1988 UTC via an H-1 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 CS 3B Date of exalting 16.09.1988y. Average height of ISS CS 3B hundred 36082.73 km. Average velocity CS 3B is 11030.3 km/h. Inclination CS 3B satellite 14.88°.TLE
Average velocity CS 3B
Average inclination CS 3B
Mean right ascension of the ascending node (RAAN) CS 3B
Mean argument of perigee CS 3B
Mean semi-major axis of the orbit CS 3B
Mean orbital eccentricity CS 3B
ISS
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