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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-56
1 62786U 25016B 26092.29526861 .00000021 00000-0 13686-4 0 9992
2 62786 88.9655 91.5598 0017270 37.7650 322.4710 13.50999444 62166Epoch: 2026-04-02T07:05Z
TLE epoch observation values (Epoch: 2026-04-02T07:05:11.207Z)
Latitude
0°
Longitude
154.6173°
Altitude
1,061.344 km
Speed
7.326 km/s
True Right ascension
06h 06m 14s
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
21:31:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.49 km
Perigee altitude
1,052.779 km
Semi-major axis
7,443.772 km
Eccentricity
0.00173
Inclination
88.9655°
RAAN
91.5598°
Arg. of periapsis
37.765°
True anomaly
322.35024°
Mean anomaly
322.471°
Eccentric anomaly
322.41064°
Mean motion
3.37951 °/min
Orbital period
106.52 mins
BSTAR
0.000013686
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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 | 2026-04-02 23:12:15.872Z | 130.628° SE | 2026-04-02 23:17:15.872Z | 77.532° E | 24.914° | 2026-04-02 23:22:15.872Z | 24.085° NE |
| 10 mins | 2026-04-03 00:59:15.872Z | 210.934° SW | 2026-04-03 01:03:15.872Z | 268.298° W | 35.489° | 2026-04-03 01:09:15.872Z | 345.121° N |
| 11 mins | 2026-04-03 12:08:15.872Z | 2.308° NNE | 2026-04-03 12:13:15.872Z | 155.889° SSE | 44.763° | 2026-04-03 12:19:15.872Z | 181.207° SSW |
| 4 mins | 2026-04-03 13:57:15.872Z | 301.866° NW | 2026-04-03 13:58:15.872Z | 292.03° WNW | 13.83° | 2026-04-03 14:01:15.872Z | 263.626° W |
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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