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, 5.0 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 26305.81691573 .00000103 00000-0 13999-3 0 9997
2 62786 88.9704 69.3064 0017453 131.8671 228.3973 13.51034365 90994Epoch: 2026-11-01T19:36Z
TLE epoch observation values (Epoch: 2026-11-01T19:36:21.519Z)
Latitude
0.00002°
Longitude
94.11389°
Altitude
1,080.052 km
Speed
7.308 km/s
True Right ascension
04h 37m 13s
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
22:57:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.498 km
Perigee altitude
1,052.515 km
Semi-major axis
7,443.643 km
Eccentricity
0.00175
Inclination
88.9704°
RAAN
69.3064°
Arg. of periapsis
131.8671°
True anomaly
228.24797°
Mean anomaly
228.3973°
Eccentric anomaly
228.32261°
Mean motion
3.3796 °/min
Orbital period
106.52 mins
BSTAR
0.00013999
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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 | 2026-11-02 08:09:20.186Z | 149.734° SSE | 2026-11-02 08:15:20.186Z | 70.258° E | 45.041° | 2026-11-02 08:20:20.186Z | 14.215° NNE |
| 9 mins | 2026-11-02 09:57:20.186Z | 229.853° WSW | 2026-11-02 10:01:20.186Z | 275.505° WNW | 28.081° | 2026-11-02 10:06:20.186Z | 331.933° NNW |
| 8 mins | 2026-11-02 19:20:20.186Z | 40.235° NE | 2026-11-02 19:23:20.186Z | 72.304° E | 21.486° | 2026-11-02 19:28:20.186Z | 124.416° SE |
| 11 mins | 2026-11-02 21:05:20.186Z | 350.648° N | 2026-11-02 21:10:20.186Z | 292.553° NW | 57.223° | 2026-11-02 21:16:20.186Z | 200.804° SSW |
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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