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, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-56
1 62786U 25016B 25256.87780852 .00000058 00000-0 71118-4 0 9993
2 62786 88.9751 112.3550 0014159 249.6481 110.3150 13.50963378 35105Epoch: 2025-09-13T21:04Z
TLE epoch observation values (Epoch: 2025-09-13T21:04:02.656Z)
Latitude
0.00008°
Longitude
163.23908°
Altitude
1,075.344 km
Speed
7.313 km/s
True Right ascension
07h 29m 25s
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
00:20:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.307 km
Perigee altitude
1,055.228 km
Semi-major axis
7,443.904 km
Eccentricity
0.00142
Inclination
88.9751°
RAAN
112.355°
Arg. of periapsis
249.6481°
True anomaly
110.46706°
Mean anomaly
110.315°
Eccentric anomaly
110.39104°
Mean motion
3.37942 °/min
Orbital period
106.53 mins
BSTAR
0.000071118
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-14 13:14:02.448Z | 97.448° ESE | 2025-09-14 13:17:02.448Z | 68.598° E | 14.594° | 2025-09-14 13:20:02.448Z | 40.903° NE |
| 12 mins | 2025-09-14 14:57:02.448Z | 180.88° SSW | 2025-09-14 15:02:02.448Z | 216.326° SW | 44.537° | 2025-09-14 15:09:02.448Z | 357.84° N |
| 11 mins | 2025-09-15 02:07:02.448Z | 17.316° NNE | 2025-09-15 02:12:02.448Z | 86.417° E | 36.655° | 2025-09-15 02:18:02.448Z | 158.459° S |
| 9 mins | 2025-09-15 03:54:02.448Z | 330.122° NNW | 2025-09-15 03:58:02.448Z | 285.521° WNW | 24.322° | 2025-09-15 04:03:02.448Z | 231.872° WSW |
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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