QIANFAN-51, 62252
Orbit data source: Space-Track
QIANFAN-51, 62252 is a Chinese payload satellite in LEO that was launched on Thu, 05 Dec 2024 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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62252 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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-51
1 62252U 24232R 26246.84595253 .00000084 00000-0 11155-3 0 9999
2 62252 89.0142 14.6210 0014559 148.5122 211.6904 13.51026614103651Epoch: 2026-09-03T20:18Z
TLE epoch observation values (Epoch: 2026-09-03T20:18:10.298Z)
Latitude
0.00002°
Longitude
87.09982°
Altitude
1,080.668 km
Speed
7.307 km/s
True Right ascension
00h 58m 29s
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
20:52:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.372 km
Perigee altitude
1,054.697 km
Semi-major axis
7,443.672 km
Eccentricity
0.00146
Inclination
89.0142°
RAAN
14.621°
Arg. of periapsis
148.5122°
True anomaly
211.60289°
Mean anomaly
211.6904°
Eccentric anomaly
211.64663°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.00011155
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Other satellites on launch #232 in the year 2024 (2024-12-05 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-51 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 | 2026-09-04 08:50:59.485Z | 168.957° S | 2026-09-04 08:56:59.485Z | 52.93° ENE | 43.584° | 2026-09-04 09:02:59.485Z | 2.887° NNE |
| 6 mins | 2026-09-04 10:40:59.485Z | 256.061° W | 2026-09-04 10:43:59.485Z | 286.503° WNW | 16.106° | 2026-09-04 10:46:59.485Z | 315.874° NNW |
| 10 mins | 2026-09-04 20:00:59.485Z | 23.255° NE | 2026-09-04 20:05:59.485Z | 84.581° E | 30.124° | 2026-09-04 20:10:59.485Z | 143.969° SSE |
| 10 mins | 2026-09-04 21:47:59.485Z | 336.248° NNW | 2026-09-04 21:51:59.485Z | 287.78° WNW | 30.006° | 2026-09-04 21:57:59.485Z | 218.364° SW |
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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