QIANFAN-66, 62796
Orbit data source: Space-Track
QIANFAN-66, 62796 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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62796 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-66
1 62796U 25016M 26305.78408175 .00000098 00000-0 13309-3 0 9996
2 62796 88.9733 69.3860 0016640 120.9456 239.3333 13.51034555 91048Epoch: 2026-11-01T18:49Z
TLE epoch observation values (Epoch: 2026-11-01T18:49:04.663Z)
Latitude
-0.00001°
Longitude
106.04608°
Altitude
1,077.744 km
Speed
7.31 km/s
True Right ascension
04h 37m 32s
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
22:58:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.892 km
Perigee altitude
1,053.12 km
Semi-major axis
7,443.643 km
Eccentricity
0.00166
Inclination
88.9733°
RAAN
69.386°
Arg. of periapsis
120.9456°
True anomaly
239.16946°
Mean anomaly
239.3333°
Eccentric anomaly
239.25136°
Mean motion
3.3796 °/min
Orbital period
106.52 mins
BSTAR
0.00013309
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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-66 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-02 07:24:06.210Z | 114.2° SE | 2026-11-02 07:28:06.210Z | 74.578° E | 19.801° | 2026-11-02 07:32:06.210Z | 34.408° NE |
| 11 mins | 2026-11-02 09:09:06.210Z | 192.837° SSW | 2026-11-02 09:14:06.210Z | 274.774° WNW | 65.222° | 2026-11-02 09:20:06.210Z | 352.374° N |
| 11 mins | 2026-11-02 20:18:06.210Z | 9.882° NNE | 2026-11-02 20:23:06.210Z | 67.729° E | 60.523° | 2026-11-02 20:29:06.210Z | 166.807° S |
| 7 mins | 2026-11-02 22:06:06.210Z | 321.755° NNW | 2026-11-02 22:09:06.210Z | 290.434° WNW | 20.47° | 2026-11-02 22:13:06.210Z | 247.827° 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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