SAKURA 1A (CS-1A)
Satellite information SAKURA 1A (CS-1A) - SAKURA (CS)
| Spacetrack Directory Name | SAKURA 1A (CS-1A) |
| Alternative name | SAKURA (CS) |
| Follow SAKURA 1A (CS-1A) | SAKURA 1A (CS-1A) Tracker |
| Pass predictions SAKURA 1A (CS-1A) | Pass predictions SAKURA 1A (CS-1A) |
| Orbit launches |
1977-12-15 (48 years ago)
|
| Days in orbit | 17800 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36158 km |
| Apogee | 36186 km |
| Orbit slope (inclination) | 7.19° |
| Laps per day | 1 |
| Height SAKURA 1A (CS-1A) | 36171.23 km |
Additional information SAKURA 1A (CS-1A)
SAKURA 1A (CS-1A), 10516 is a payload satellite owned by NASDA (JP) in GEO that was launched on Thu, 15 Dec 1977 UTC via a DELTA 2914 launch vehicle from the Air Force Eastern Test Range (AFETR). 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 1A (CS-1A) Date of exalting 15.12.1977y. Average height of ISS SAKURA 1A (CS-1A) hundred 36171.23 km. Average velocity SAKURA 1A (CS-1A) is 11018.79 km/h. Inclination SAKURA 1A (CS-1A) satellite 7.22°.TLE
Average velocity SAKURA 1A (CS-1A)
Average inclination SAKURA 1A (CS-1A)
Mean right ascension of the ascending node (RAAN) SAKURA 1A (CS-1A)
Mean argument of perigee SAKURA 1A (CS-1A)
Mean semi-major axis of the orbit SAKURA 1A (CS-1A)
Mean orbital eccentricity SAKURA 1A (CS-1A)
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