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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-56
1 62786U 25016B 26035.78487660 .00000117 00000-0 16265-3 0 9997
2 62786 88.9711 97.4514 0016137 187.4136 172.6779 13.50995197 54538Epoch: 2026-02-04T18:50Z
TLE epoch observation values (Epoch: 2026-02-04T18:50:13.338Z)
Latitude
-0.00001°
Longitude
39.94934°
Altitude
1,083.474 km
Speed
7.305 km/s
True Right ascension
06h 29m 48s
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
03:17:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.662 km
Perigee altitude
1,053.638 km
Semi-major axis
7,443.787 km
Eccentricity
0.00161
Inclination
88.9711°
RAAN
97.4514°
Arg. of periapsis
187.4136°
True anomaly
172.70142°
Mean anomaly
172.6779°
Eccentric anomaly
172.68966°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
0.00016265
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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 | 2026-02-05 03:49:58.348Z | 151.387° SSE | 2026-02-05 03:55:58.348Z | 69.147° E | 36.316° | 2026-02-05 04:00:58.348Z | 13.238° NNE |
| 9 mins | 2026-02-05 05:37:58.348Z | 231.333° WSW | 2026-02-05 05:41:58.348Z | 275.782° WNW | 24.332° | 2026-02-05 05:46:58.348Z | 331.097° NNW |
| 8 mins | 2026-02-05 15:00:58.348Z | 39.131° NE | 2026-02-05 15:04:58.348Z | 84.641° E | 21.069° | 2026-02-05 15:08:58.348Z | 125.38° SE |
| 10 mins | 2026-02-05 16:46:58.348Z | 346.36° N | 2026-02-05 16:50:58.348Z | 292.41° WNW | 39.104° | 2026-02-05 16:56:58.348Z | 202.798° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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