QIANFAN-129
Satellite information QIANFAN-129 - QIANFAN-130
| Spacetrack Directory Name | QIANFAN-129 |
| Alternative name | QIANFAN-130 |
| Group | QIANFAN |
| Follow QIANFAN-129 | QIANFAN-129 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-129 | Pass predictions QIANFAN-129 |
| Orbit launches |
2026-05-12 (3 months ago)
|
| Days in orbit | 92 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 793 km |
| Apogee | 813 km |
| Orbit slope (inclination) | 88.99° |
| Laps per day | 14 |
| Height QIANFAN-129 | 1096.63 km |
Additional information QIANFAN-129
QIANFAN-130, 69075 is a Chinese payload satellite in LEO that was launched on Tue, 12 May 2026 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). Payload-class satellites include a variety of spacecraft 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 QIANFAN-129 Date of exalting 12.05.2026y. Average height of ISS QIANFAN-129 hundred 1096.63 km. Average velocity QIANFAN-129 is 26300.04 km/h. Inclination QIANFAN-129 satellite 88.99°.TLE
Average orbit height QIANFAN-129
Average velocity QIANFAN-129
Average inclination QIANFAN-129
Mean right ascension of the ascending node (RAAN) QIANFAN-129
Mean argument of perigee QIANFAN-129
Mean semi-major axis of the orbit QIANFAN-129
Mean orbital eccentricity QIANFAN-129
ISS
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