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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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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-66
1 62796U 25016M 25256.84481156 .00000065 00000-0 81802-4 0 9995
2 62796 88.9780 112.3153 0013331 236.0967 123.8917 13.50963638 35151Epoch: 2025-09-13T20:16Z
TLE epoch observation values (Epoch: 2025-09-13T20:16:31.718Z)
Latitude
-0.00002°
Longitude
175.11081°
Altitude
1,077.214 km
Speed
7.311 km/s
True Right ascension
07h 29m 15s
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
00:22:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.69 km
Perigee altitude
1,055.843 km
Semi-major axis
7,443.903 km
Eccentricity
0.00133
Inclination
88.978°
RAAN
112.3153°
Arg. of periapsis
236.0967°
True anomaly
124.01839°
Mean anomaly
123.8917°
Eccentric anomaly
123.95506°
Mean motion
3.37942 °/min
Orbital period
106.53 mins
BSTAR
0.000081802
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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 | 2025-09-14 14:09:48.742Z | 146.856° SSE | 2025-09-14 14:14:48.742Z | 88.372° E | 34.425° | 2025-09-14 14:20:48.742Z | 14.279° NNE |
| 9 mins | 2025-09-14 15:57:48.742Z | 230.253° WSW | 2025-09-14 16:01:48.742Z | 279.43° WNW | 26.412° | 2025-09-14 16:06:48.742Z | 334.351° NNW |
| 8 mins | 2025-09-15 01:20:48.742Z | 42.356° NE | 2025-09-15 01:23:48.742Z | 74.338° E | 19.457° | 2025-09-15 01:28:48.742Z | 124.159° SE |
| 11 mins | 2025-09-15 03:05:48.742Z | 351.406° N | 2025-09-15 03:10:48.742Z | 288.533° WNW | 41.173° | 2025-09-15 03:16:48.742Z | 198.584° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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