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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-50
1 62251U 24232Q 26096.88571364 .00000168 00000-0 24175-3 0 9991
2 62251 89.0114 29.6506 0014015 219.2185 140.7952 13.51010291 83415Epoch: 2026-04-06T21:15Z
TLE epoch observation values (Epoch: 2026-04-06T21:15:25.658Z)
Latitude
-0°
Longitude
-124.37667°
Altitude
1,079.592 km
Speed
7.308 km/s
True Right ascension
01h 58m 36s
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
14:05:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.027 km
Perigee altitude
1,055.162 km
Semi-major axis
7,443.732 km
Eccentricity
0.0014
Inclination
89.0114°
RAAN
29.6506°
Arg. of periapsis
219.2185°
True anomaly
140.89658°
Mean anomaly
140.7952°
Eccentric anomaly
140.8459°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00024175
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-04-07 08:30:38.476Z | 346.51° N | 2026-04-07 08:36:38.476Z | 278.802° WNW | 33.983° | 2026-04-07 08:42:38.476Z | 211.159° SW |
| 9 mins | 2026-04-07 18:43:38.476Z | 121.828° SE | 2026-04-07 18:47:38.476Z | 75.877° E | 24.298° | 2026-04-07 18:52:38.476Z | 24.372° NE |
| 11 mins | 2026-04-07 20:28:38.476Z | 204.578° SW | 2026-04-07 20:33:38.476Z | 271.051° WNW | 36.886° | 2026-04-07 20:39:38.476Z | 346.315° N |
| 11 mins | 2026-04-08 07:38:38.476Z | 3.991° NNE | 2026-04-08 07:43:38.476Z | 135.815° SSE | 44.532° | 2026-04-08 07:49:38.476Z | 179.234° S |
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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