KOREASAT 2 - Norad Identifikationsnummer: 23768
| Name im Katalog Spacetrack | ABS 1A (KOREASAT 2) |
| Alternative Bezeichnung | KOREASAT 2 |
| Folge ABS 1A (KOREASAT 2) | ABS 1A (KOREASAT 2) Tracker |
| Flugzeiten ABS 1A (KOREASAT 2) | Flugzeiten ABS 1A (KOREASAT 2) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 11194 |
| Herkunftsland/-organisation | Korea (SKOR) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perygeum | 35911 km |
| Apogäum | 35926 km |
| Neigung der Umlaufbahn (Inklination) | 12.71° |
| Runden pro Tag | 1 |
| Höhe ABS 1A (KOREASAT 2) | 35921.55 km |
ABS 1A (KOREASAT 2), 23768 is a payload satellite owned by KTEL (KR) in GEO that was launched on Sun, 14 Jan 1996 UTC via a DELTA 7925 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 ABS 1A (KOREASAT 2) hinausgetragen 14.01.1996r. Durchschnittshöhe ABS 1A (KOREASAT 2) Text Nummer 1: das. 35921.55 km. Durchschnittsgeschwindigkeit ABS 1A (KOREASAT 2) beträgt 11051.29 km/h. Neigung ABS 1A (KOREASAT 2) Satelliten 12.7°.