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, 1.3 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 QIANFAN-66
1 62796U 25016M 25306.46835937 .00000071 00000-0 90945-4 0 9994
2 62796 88.9749 107.1857 0016735 95.2741 265.0320 13.50978245 41856Epoch: 2025-11-02T11:14Z
TLE epoch observation values (Epoch: 2025-11-02T11:14:26.249Z)
Latitude
-0.00005°
Longitude
-103.40732°
Altitude
1,072.715 km
Speed
7.315 km/s
True Right ascension
07h 08m 44s
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
14:39:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.17 km
Perigee altitude
1,053.255 km
Semi-major axis
7,443.85 km
Eccentricity
0.00167
Inclination
88.9749°
RAAN
107.1857°
Arg. of periapsis
95.2741°
True anomaly
264.84099°
Mean anomaly
265.032°
Eccentric anomaly
264.93649°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.000090945
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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 | 2025-11-03 21:37:29.079Z | 35.695° NE | 2025-11-03 21:41:29.079Z | 74.457° E | 17.711° | 2025-11-03 21:45:29.079Z | 115.03° SE |
| 11 mins | 2025-11-03 23:23:29.079Z | 353.55° N | 2025-11-03 23:28:29.079Z | 292.372° WNW | 42.492° | 2025-11-03 23:34:29.079Z | 195.049° SSW |
| 6 mins | 2025-11-04 09:37:29.079Z | 98.704° ESE | 2025-11-04 09:40:29.079Z | 68.299° E | 15.663° | 2025-11-04 09:43:29.079Z | 39.692° NE |
| 11 mins | 2025-11-04 11:20:29.079Z | 184.696° SSW | 2025-11-04 11:25:29.079Z | 237.752° WSW | 43.961° | 2025-11-04 11:31:29.079Z | 355.233° N |
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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