QIANFAN-56, 62786
Orbit data source: Space-Track
QIANFAN-56, 62786 is a Chinese payload satellite in LEO that was launched on Thu, 23 Jan 2025 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.
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62786 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.1 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-56
1 62786U 25016B 25292.28081661 .00000077 00000-0 99604-4 0 9991
2 62786 88.9713 108.6858 0016941 143.4387 216.7924 13.50976409 39887Epoch: 2025-10-19T06:44Z
TLE epoch observation values (Epoch: 2025-10-19T06:44:22.555Z)
Latitude
-0.00001°
Longitude
-20.40792°
Altitude
1,081.734 km
Speed
7.306 km/s
True Right ascension
07h 14m 44s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:42:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.33 km
Perigee altitude
1,053.109 km
Semi-major axis
7,443.856 km
Eccentricity
0.00169
Inclination
88.9713°
RAAN
108.6858°
Arg. of periapsis
143.4387°
True anomaly
216.67633°
Mean anomaly
216.7924°
Eccentric anomaly
216.73435°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000099604
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Other satellites on launch #16 in the year 2025 (2025-01-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.QIANFAN-56 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-10-19 23:19:58.071Z | 19.104° NNE | 2025-10-19 23:25:58.071Z | 91.517° ESE | 30.814° | 2025-10-19 23:30:58.071Z | 147.044° SSE |
| 9 mins | 2025-10-20 01:07:58.071Z | 333.114° NNW | 2025-10-20 01:11:58.071Z | 281.233° WNW | 29.261° | 2025-10-20 01:16:58.071Z | 222.741° SW |
| 9 mins | 2025-10-20 11:18:58.071Z | 129.701° SE | 2025-10-20 11:22:58.071Z | 79.59° E | 28.407° | 2025-10-20 11:27:58.071Z | 22.154° NNE |
| 10 mins | 2025-10-20 13:04:58.071Z | 216.442° SW | 2025-10-20 13:08:58.071Z | 267.096° W | 32.107° | 2025-10-20 13:14:58.071Z | 341.533° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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