YUNHAI 1-04
Satellite information YUNHAI 1-04 - 2023-159A
| Spacetrack Directory Name | YUNHAI 1-04 |
| Alternative name | 2023-159A |
| Follow YUNHAI 1-04 | YUNHAI 1-04 Tracker |
| Pass predictions YUNHAI 1-04 | Pass predictions YUNHAI 1-04 |
| Orbit launches |
2023-10-15 (2 years ago)
|
| Days in orbit | 1090 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| WWW | Here |
| Perigee | 756 km |
| Apogee | 773 km |
| Orbit slope (inclination) | 98.49° |
| Laps per day | 14 |
| Height YUNHAI 1-04 | 794.85 km |
Additional information YUNHAI 1-04
YUNHAI 1-04, 58073 is a payload satellite owned by SAST (CN) in SSO that was launched on Sun, 15 Oct 2023 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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 YUNHAI 1-04 Date of exalting 15.10.2023y. Average height of ISS YUNHAI 1-04 hundred 794.85 km. Average velocity YUNHAI 1-04 is 26847.75 km/h. Inclination YUNHAI 1-04 satellite 98.51°.TLE
Average velocity YUNHAI 1-04
Average inclination YUNHAI 1-04
Mean right ascension of the ascending node (RAAN) YUNHAI 1-04
Mean argument of perigee YUNHAI 1-04
Mean semi-major axis of the orbit YUNHAI 1-04
Mean orbital eccentricity YUNHAI 1-04
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