QIANFAN-64, 62794
Orbit data source: Space-Track
QIANFAN-64, 62794 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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62794 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-64
1 62794U 25016K 25306.44358696 .00000076 00000-0 99102-4 0 9991
2 62794 88.9733 107.1985 0015787 97.7106 262.5838 13.50975205 41823Epoch: 2025-11-02T10:38Z
TLE epoch observation values (Epoch: 2025-11-02T10:38:45.913Z)
Latitude
-0.00006°
Longitude
-94.45204°
Altitude
1,073.162 km
Speed
7.315 km/s
True Right ascension
07h 08m 47s
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
1,077.476 km
Perigee altitude
1,053.972 km
Semi-major axis
7,443.861 km
Eccentricity
0.00158
Inclination
88.9733°
RAAN
107.1985°
Arg. of periapsis
97.7106°
True anomaly
262.40445°
Mean anomaly
262.5838°
Eccentric anomaly
262.49412°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000099102
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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-64 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-03 22:47:29.445Z | 7.836° NNE | 2025-11-03 22:53:29.445Z | 104.398° ESE | 42.371° | 2025-11-03 22:59:29.445Z | 170.938° S |
| 6 mins | 2025-11-04 00:36:29.445Z | 314.221° NW | 2025-11-04 00:39:29.445Z | 281.338° WNW | 18.06° | 2025-11-04 00:42:29.445Z | 251.09° W |
| 11 mins | 2025-11-04 10:45:29.445Z | 156.751° SSE | 2025-11-04 10:50:29.445Z | 75.848° E | 40.253° | 2025-11-04 10:56:29.445Z | 7.716° NNE |
| 8 mins | 2025-11-04 12:33:29.445Z | 241.188° WSW | 2025-11-04 12:37:29.445Z | 284.869° WNW | 20.326° | 2025-11-04 12:41:29.445Z | 325.845° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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