QIANFAN-50, 62251
Orbit data source: Space-Track
QIANFAN-50, 62251 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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62251 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: 14 hours ago
TLE from 14 hours ago
0 QIANFAN-50
1 62251U 24232Q 26171.39296161 .00000069 00000-0 88586-4 0 9997
2 62251 89.0082 22.1998 0016403 15.6872 344.4784 13.51009224 93473Epoch: 2026-06-20T09:25Z
TLE epoch observation values (Epoch: 2026-06-20T09:25:51.883Z)
Latitude
-0.00001°
Longitude
-27.87461°
Altitude
1,059.731 km
Speed
7.328 km/s
True Right ascension
01h 28m 47s
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
10:18:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.809 km
Perigee altitude
1,053.389 km
Semi-major axis
7,443.736 km
Eccentricity
0.00164
Inclination
89.0082°
RAAN
22.1998°
Arg. of periapsis
15.6872°
True anomaly
344.428°
Mean anomaly
344.4784°
Eccentric anomaly
344.45321°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.000088586
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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-50 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-06-21 02:00:40.638Z | 7.556° NNE | 2026-06-21 02:06:40.638Z | 68.221° E | 41.362° | 2026-06-21 02:13:40.638Z | 169.414° S |
| 7 mins | 2026-06-21 03:49:40.638Z | 321.302° NNW | 2026-06-21 03:52:40.638Z | 290.079° WNW | 19.321° | 2026-06-21 03:56:40.638Z | 248.026° W |
| 10 mins | 2026-06-21 13:59:40.638Z | 153.225° SSE | 2026-06-21 14:03:40.638Z | 99.42° ESE | 38.916° | 2026-06-21 14:09:40.638Z | 10.223° NNE |
| 8 mins | 2026-06-21 15:47:40.638Z | 242.74° WSW | 2026-06-21 15:50:40.638Z | 276.339° WNW | 21.22° | 2026-06-21 15:55:40.638Z | 329.009° NNW |
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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