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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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 26141.91736187 .00000093 00000-0 12572-3 0 9991
2 62786 88.9704 86.3916 0013653 246.3498 113.6221 13.51013427 68865Epoch: 2026-05-21T22:01Z
TLE epoch observation values (Epoch: 2026-05-21T22:01:00.065Z)
Latitude
0.00003°
Longitude
-123.41436°
Altitude
1,075.572 km
Speed
7.312 km/s
True Right ascension
05h 45m 33s
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
15:20:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.746 km
Perigee altitude
1,055.421 km
Semi-major axis
7,443.72 km
Eccentricity
0.00137
Inclination
88.9704°
RAAN
86.3916°
Arg. of periapsis
246.3498°
True anomaly
113.76534°
Mean anomaly
113.6221°
Eccentric anomaly
113.69373°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00012572
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-05-22 07:30:09.197Z | 24.18° NE | 2026-05-22 07:35:09.197Z | 74.751° E | 25.248° | 2026-05-22 07:40:09.197Z | 132.825° SE |
| 11 mins | 2026-05-22 09:17:09.197Z | 344.252° N | 2026-05-22 09:22:09.197Z | 280.759° WNW | 35.416° | 2026-05-22 09:28:09.197Z | 209.249° SW |
| 9 mins | 2026-05-22 19:29:09.197Z | 120.455° SE | 2026-05-22 19:33:09.197Z | 76.673° E | 22.927° | 2026-05-22 19:38:09.197Z | 25.778° NE |
| 11 mins | 2026-05-22 21:14:09.197Z | 201.664° SSW | 2026-05-22 21:19:09.197Z | 268.967° W | 38.284° | 2026-05-22 21:25:09.197Z | 347.533° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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