QIANFAN-135
Satellite information QIANFAN-135 - QIANFAN-136
| Spacetrack Directory Name | QIANFAN-135 |
| Alternative name | QIANFAN-136 |
| Group | QIANFAN |
| Follow QIANFAN-135 | QIANFAN-135 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-135 | Pass predictions QIANFAN-135 |
| Orbit launches |
2026-05-12 (4 months ago)
|
| Days in orbit | 131 |
| 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-135 | 1081.79 km |
Additional information QIANFAN-135
QIANFAN-136, 69081 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-135 Date of exalting 12.05.2026y. Average height of ISS QIANFAN-135 hundred 1081.79 km. Average velocity QIANFAN-135 is 26326.1 km/h. Inclination QIANFAN-135 satellite 88.99°.TLE
Average velocity QIANFAN-135
Average inclination QIANFAN-135
Mean right ascension of the ascending node (RAAN) QIANFAN-135
Mean argument of perigee QIANFAN-135
Mean semi-major axis of the orbit QIANFAN-135
Mean orbital eccentricity QIANFAN-135
ISS
Buy us a coffee!
