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, 1.3 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-66
1 62796U 25016M 26141.88439837 .00000100 00000-0 13654-3 0 9991
2 62796 88.9733 86.4240 0012878 232.2712 127.7272 13.51012839 68914Epoch: 2026-05-21T21:13Z
TLE epoch observation values (Epoch: 2026-05-21T21:13:32.019Z)
Latitude
-0.00007°
Longitude
-111.48261°
Altitude
1,077.364 km
Speed
7.31 km/s
True Right ascension
05h 45m 41s
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
15:20:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.172 km
Perigee altitude
1,056 km
Semi-major axis
7,443.723 km
Eccentricity
0.00129
Inclination
88.9733°
RAAN
86.424°
Arg. of periapsis
232.2712°
True anomaly
127.8438°
Mean anomaly
127.7272°
Eccentric anomaly
127.78551°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00013654
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-05-22 08:29:47.682Z | 4.393° NNE | 2026-05-22 08:34:47.682Z | 66.878° ENE | 44.469° | 2026-05-22 08:40:47.682Z | 177.426° S |
| 5 mins | 2026-05-22 10:18:47.682Z | 307.072° NW | 2026-05-22 10:20:47.682Z | 286.691° WNW | 15.236° | 2026-05-22 10:23:47.682Z | 258.02° W |
| 11 mins | 2026-05-22 20:26:47.682Z | 165.338° S | 2026-05-22 20:31:47.682Z | 89.489° E | 43.244° | 2026-05-22 20:37:47.682Z | 4.741° NNE |
| 7 mins | 2026-05-22 22:15:47.682Z | 250.801° W | 2026-05-22 22:18:47.682Z | 281.19° WNW | 17.394° | 2026-05-22 22:22:47.682Z | 320.827° NNW |
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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