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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Edit Public Description
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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-51
1 62252U 24232R 26035.17478285 .00000027 00000-0 22905-4 0 9999
2 62252 89.0009 35.8387 0014870 51.0826 309.1649 13.50984189 75070Epoch: 2026-02-04T04:11Z
TLE epoch observation values (Epoch: 2026-02-04T04:11:41.238Z)
Latitude
0.00005°
Longitude
-161.42827°
Altitude
1,064.608 km
Speed
7.323 km/s
True Right ascension
02h 23m 21s
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
12:23:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.76 km
Perigee altitude
1,054.622 km
Semi-major axis
7,443.828 km
Eccentricity
0.00149
Inclination
89.0009°
RAAN
35.8387°
Arg. of periapsis
51.0826°
True anomaly
309.03263°
Mean anomaly
309.1649°
Eccentric anomaly
309.09878°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.000022905
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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 | 2026-02-04 11:53:35.765Z | 8.478° NNE | 2026-02-04 11:59:35.765Z | 84.799° E | 41.535° | 2026-02-04 12:05:35.765Z | 167.773° S |
| 7 mins | 2026-02-04 13:42:35.765Z | 318.412° NNW | 2026-02-04 13:45:35.765Z | 285.669° WNW | 19.466° | 2026-02-04 13:49:35.765Z | 245° WSW |
| 11 mins | 2026-02-04 23:51:35.765Z | 155.264° SSE | 2026-02-04 23:56:35.765Z | 88.634° E | 39.059° | 2026-02-05 00:02:35.765Z | 9.63° NNE |
| 9 mins | 2026-02-05 01:39:35.765Z | 236.936° WSW | 2026-02-05 01:43:35.765Z | 280.463° WNW | 21.507° | 2026-02-05 01:48:35.765Z | 331.212° 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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