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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-64
1 62794U 25016K 25292.00096490 .00000100 00000-0 13544-3 0 9991
2 62794 88.9726 108.6945 0015262 134.9369 225.3023 13.50973591 39871Epoch: 2025-10-19T00:01Z
TLE epoch observation values (Epoch: 2025-10-19T00:01:23.367Z)
Latitude
-0.00002°
Longitude
80.62323°
Altitude
1,079.636 km
Speed
7.308 km/s
True Right ascension
07h 14m 46s
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
02:57:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.091 km
Perigee altitude
1,054.369 km
Semi-major axis
7,443.867 km
Eccentricity
0.00153
Inclination
88.9726°
RAAN
108.6945°
Arg. of periapsis
134.9369°
True anomaly
225.17815°
Mean anomaly
225.3023°
Eccentric anomaly
225.24021°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00013544
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-19 10:50:48.176Z | 105° ESE | 2025-10-19 10:53:48.176Z | 74.89° E | 17.125° | 2025-10-19 10:57:48.176Z | 35.823° NE |
| 11 mins | 2025-10-19 12:34:48.176Z | 188.701° SSW | 2025-10-19 12:39:48.176Z | 273.408° WNW | 43.472° | 2025-10-19 12:45:48.176Z | 354.136° N |
| 10 mins | 2025-10-19 23:44:48.176Z | 15.367° NNE | 2025-10-19 23:48:48.176Z | 69.88° E | 39.397° | 2025-10-19 23:54:48.176Z | 163.135° S |
| 8 mins | 2025-10-20 01:31:48.176Z | 323.483° NNW | 2025-10-20 01:34:48.176Z | 291.323° WNW | 20.781° | 2025-10-20 01:39:48.176Z | 238.869° WSW |
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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