SAKURA (CS) - Norad Identifikationsnummer: 10516
| Name im Katalog Spacetrack | SAKURA 1A (CS-1A) |
| Alternative Bezeichnung | SAKURA (CS) |
| Folge SAKURA 1A (CS-1A) | SAKURA 1A (CS-1A) Tracker |
| Flugzeiten SAKURA 1A (CS-1A) | Flugzeiten SAKURA 1A (CS-1A) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 17800 |
| Herkunftsland/-organisation | Japonia (JPN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perygeum | 36158 km |
| Apogäum | 36186 km |
| Neigung der Umlaufbahn (Inklination) | 7.19° |
| Runden pro Tag | 1 |
| Höhe SAKURA 1A (CS-1A) | 36171.23 km |
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.
der Satellit SAKURA 1A (CS-1A) hinausgetragen 15.12.1977r. Durchschnittshöhe SAKURA 1A (CS-1A) Text Nummer 1: das. 36171.23 km. Durchschnittsgeschwindigkeit SAKURA 1A (CS-1A) beträgt 11018.79 km/h. Neigung SAKURA 1A (CS-1A) Satelliten 7.22°.