ABS 1A (KOREASAT 2)
Satellite information ABS 1A (KOREASAT 2) - KOREASAT 2
| Spacetrack Directory Name | ABS 1A (KOREASAT 2) |
| Alternative name | KOREASAT 2 |
| Follow ABS 1A (KOREASAT 2) | ABS 1A (KOREASAT 2) Tracker |
| Pass predictions ABS 1A (KOREASAT 2) | Pass predictions ABS 1A (KOREASAT 2) |
| Orbit launches |
1996-01-14 (30 years ago)
|
| Days in orbit | 11194 |
| Country/organisation of origin | Korea (SKOR) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35911 km |
| Apogee | 35926 km |
| Orbit slope (inclination) | 12.71° |
| Laps per day | 1 |
| Height ABS 1A (KOREASAT 2) | 35921.55 km |
Additional information ABS 1A (KOREASAT 2)
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.
satellite ABS 1A (KOREASAT 2) Date of exalting 14.01.1996y. Average height of ISS ABS 1A (KOREASAT 2) hundred 35921.55 km. Average velocity ABS 1A (KOREASAT 2) is 11051.29 km/h. Inclination ABS 1A (KOREASAT 2) satellite 12.7°.TLE
Average velocity ABS 1A (KOREASAT 2)
Average inclination ABS 1A (KOREASAT 2)
Mean right ascension of the ascending node (RAAN) ABS 1A (KOREASAT 2)
Mean argument of perigee ABS 1A (KOREASAT 2)
Mean semi-major axis of the orbit ABS 1A (KOREASAT 2)
Mean orbital eccentricity ABS 1A (KOREASAT 2)
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