CS 3A
Satellite information CS 3A - SAKURA-3A (CS-3A)
| Spacetrack Directory Name | CS 3A |
| Alternative name | SAKURA-3A (CS-3A) |
| Follow CS 3A | CS 3A Tracker |
| Pass predictions CS 3A | Pass predictions CS 3A |
| Orbit launches |
1988-02-19 (38 years ago)
|
| Days in orbit | 14077 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 36355 km |
| Apogee | 36438 km |
| Orbit slope (inclination) | 15.21° |
| Laps per day | 1 |
| Height CS 3A | 36396.26 km |
Additional information CS 3A
CS 3A, 18877 is a Japanese payload satellite in GEO that was launched on Fri, 19 Feb 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 3A Date of exalting 19.02.1988y. Average height of ISS CS 3A hundred 36396.26 km. Average velocity CS 3A is 10989.84 km/h. Inclination CS 3A satellite 15.21°.TLE
Average velocity CS 3A
Average inclination CS 3A
Mean right ascension of the ascending node (RAAN) CS 3A
Mean argument of perigee CS 3A
Mean semi-major axis of the orbit CS 3A
Mean orbital eccentricity CS 3A
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