CHINASAT 4A
Satellite information CHINASAT 4A - 2024-151A
| Spacetrack Directory Name | CHINASAT 4A |
| Alternative name | 2024-151A |
| Follow CHINASAT 4A | CHINASAT 4A Tracker |
| Pass predictions CHINASAT 4A | Pass predictions CHINASAT 4A |
| Orbit launches |
2024-08-22 (2 years ago)
|
| Days in orbit | 736 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | WSC (Wenchang Spacecraft Launch Site) |
| Perigee | 220 km |
| Apogee | 35790 km |
| Orbit slope (inclination) | 1.14° |
| Laps per day | 1 |
| Height CHINASAT 4A | 35786.42 km |
Additional information CHINASAT 4A
CHINASAT 4A, 60606 is a payload satellite owned by PLA SSF (CN) in GEO that was launched on Thu, 22 Aug 2024 UTC via a CHANG ZHENG 7A launch vehicle from the Wenchang Satellite Launch Center (WSC). 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 CHINASAT 4A Date of exalting 22.08.2024y. Average height of ISS CHINASAT 4A hundred 35786.42 km. Average velocity CHINASAT 4A is 11068.94 km/h. Inclination CHINASAT 4A satellite 1.6°.TLE
Average velocity CHINASAT 4A
Average inclination CHINASAT 4A
Mean right ascension of the ascending node (RAAN) CHINASAT 4A
Mean argument of perigee CHINASAT 4A
Mean semi-major axis of the orbit CHINASAT 4A
Mean orbital eccentricity CHINASAT 4A
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