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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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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-64
1 62794U 25016K 26141.85970163 .00000095 00000-0 12868-3 0 9997
2 62794 88.9717 86.4047 0011899 235.1847 124.8185 13.51011235 68888Epoch: 2026-05-21T20:37Z
TLE epoch observation values (Epoch: 2026-05-21T20:37:58.220Z)
Latitude
-0.00007°
Longitude
-102.58674°
Altitude
1,076.561 km
Speed
7.311 km/s
True Right ascension
05h 45m 37s
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
15:21:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.449 km
Perigee altitude
1,056.734 km
Semi-major axis
7,443.728 km
Eccentricity
0.00119
Inclination
88.9717°
RAAN
86.4047°
Arg. of periapsis
235.1847°
True anomaly
124.93035°
Mean anomaly
124.8185°
Eccentric anomaly
124.87443°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00012868
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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 | 2026-05-22 07:53:22.534Z | 15.448° NNE | 2026-05-22 07:59:22.534Z | 85.765° E | 34.189° | 2026-05-22 08:05:22.534Z | 154.506° SSE |
| 9 mins | 2026-05-22 09:41:22.534Z | 332.294° NNW | 2026-05-22 09:45:22.534Z | 286.072° WNW | 26.533° | 2026-05-22 09:50:22.534Z | 228.731° WSW |
| 10 mins | 2026-05-22 19:52:22.534Z | 135.428° SSE | 2026-05-22 19:56:22.534Z | 83.238° E | 31.363° | 2026-05-22 20:02:22.534Z | 16.086° NNE |
| 10 mins | 2026-05-22 21:38:22.534Z | 220.111° SW | 2026-05-22 21:43:22.534Z | 283.254° WNW | 29.358° | 2026-05-22 21:48:22.534Z | 338.094° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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