QIANFAN-62, 62792
Orbit data source: Space-Track
QIANFAN-62, 62792 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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62792 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, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-62
1 62792U 25016H 26305.84170612 .00000092 00000-0 12413-3 0 9990
2 62792 88.9723 69.4276 0017663 124.8148 235.4668 13.51031404 90993Epoch: 2026-11-01T20:12Z
TLE epoch observation values (Epoch: 2026-11-01T20:12:03.408Z)
Latitude
-0.00003°
Longitude
85.28611°
Altitude
1,078.893 km
Speed
7.309 km/s
True Right ascension
04h 37m 42s
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
22:57:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.665 km
Perigee altitude
1,052.37 km
Semi-major axis
7,443.654 km
Eccentricity
0.00177
Inclination
88.9723°
RAAN
69.4276°
Arg. of periapsis
124.8148°
True anomaly
235.30027°
Mean anomaly
235.4668°
Eccentric anomaly
235.38351°
Mean motion
3.37959 °/min
Orbital period
106.52 mins
BSTAR
0.00012413
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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-62 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-02 07:02:26.466Z | 92.158° ESE | 2026-11-02 07:04:26.466Z | 74.343° E | 12.264° | 2026-11-02 07:07:26.466Z | 47.096° ENE |
| 11 mins | 2026-11-02 08:45:26.466Z | 173.839° S | 2026-11-02 08:50:26.466Z | 75.242° E | 83.989° | 2026-11-02 08:56:26.466Z | 0.751° NNE |
| 5 mins | 2026-11-02 10:35:26.466Z | 263.201° W | 2026-11-02 10:37:26.466Z | 282.485° WNW | 14.54° | 2026-11-02 10:40:26.466Z | 311.271° NW |
| 10 mins | 2026-11-02 19:55:26.466Z | 23.958° NE | 2026-11-02 19:59:26.466Z | 76.064° E | 40.126° | 2026-11-02 20:05:26.466Z | 151.154° SSE |
| 9 mins | 2026-11-02 21:42:26.466Z | 329.29° NNW | 2026-11-02 21:46:26.466Z | 276.816° WNW | 31.177° | 2026-11-02 21:51:26.466Z | 224.133° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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