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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-62
1 62792U 25016H 26272.14359021 .00000026 00000-0 21497-4 0 9999
2 62792 88.9675 72.9324 0014950 219.0869 140.9203 13.51027539 86449Epoch: 2026-09-29T03:26Z
TLE epoch observation values (Epoch: 2026-09-29T03:26:46.194Z)
Latitude
-0.00001°
Longitude
13.3271°
Altitude
1,080.084 km
Speed
7.308 km/s
True Right ascension
04h 51m 43s
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
09:23:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.66 km
Perigee altitude
1,054.403 km
Semi-major axis
7,443.669 km
Eccentricity
0.0015
Inclination
88.9675°
RAAN
72.9324°
Arg. of periapsis
219.0869°
True anomaly
141.02814°
Mean anomaly
140.9203°
Eccentric anomaly
140.97424°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.000021497
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-29 21:50:04.090Z | 32.997° NE | 2026-09-29 21:54:04.090Z | 73.795° E | 22.73° | 2026-09-29 21:59:04.090Z | 126.24° SE |
| 11 mins | 2026-09-29 23:36:04.090Z | 349.338° N | 2026-09-29 23:41:04.090Z | 286.855° WNW | 55.688° | 2026-09-29 23:47:04.090Z | 202.095° SSW |
| 7 mins | 2026-09-30 09:49:04.090Z | 108.592° ESE | 2026-09-30 09:52:04.090Z | 77.569° E | 20.241° | 2026-09-30 09:56:04.090Z | 36.244° NE |
| 11 mins | 2026-09-30 11:33:04.090Z | 192.68° SSW | 2026-09-30 11:38:04.090Z | 262.268° W | 64.524° | 2026-09-30 11:44:04.090Z | 351.593° 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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