ABS 3 (AGILA 2)
Informationen über den Satelliten. ABS 3 (AGILA 2) - AGILA 2
| Name im Katalog Spacetrack | ABS 3 (AGILA 2) |
| Alternative Bezeichnung | AGILA 2 |
| Folge ABS 3 (AGILA 2) | ABS 3 (AGILA 2) Tracker |
| Flugzeiten ABS 3 (AGILA 2) | Flugzeiten ABS 3 (AGILA 2) |
| In die Umlaufbahn bringen |
1997-08-19 (29 vor Jahren)
|
| Tage im Orbit | 10670 |
| Herkunftsland/-organisation | Chiny (PRC) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | XICLF (Xichang Launch Facility, China) |
| Perygeum | 36053 km |
| Apogäum | 36094 km |
| Neigung der Umlaufbahn (Inklination) | 11.47° |
| Runden pro Tag | 1 |
| Höhe ABS 3 (AGILA 2) | 36072.39 km |
Informationen über ABS 3 (AGILA 2)
ABS 3 (AGILA 2), 24901 is a payload satellite owned by MPSC (CN) in GEO that was launched on Tue, 19 Aug 1997 UTC via a CHANG ZHENG 3B launch vehicle from the Xichang Space Center, China (XSC). 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 ABS 3 (AGILA 2) hinausgetragen 19.08.1997r. Durchschnittshöhe ABS 3 (AGILA 2) Text Nummer 1: das. 36072.39 km. Durchschnittsgeschwindigkeit ABS 3 (AGILA 2) beträgt 11031.63 km/h. Neigung ABS 3 (AGILA 2) Satelliten 11.39°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ABS 3 (AGILA 2)
Durchschnittsgeschwindigkeit ABS 3 (AGILA 2)
Durchschnitt ABS 3 (AGILA 2)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) ABS 3 (AGILA 2)
Mittleres Argument des Perigäums ABS 3 (AGILA 2)
Mittlere große Halbachse der Umlaufbahn ABS 3 (AGILA 2)
Mittlere Bahnexzentrizität ABS 3 (AGILA 2)
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