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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-51
1 62252U 24232R 26305.20658949 .00000092 00000-0 12452-3 0 9997
2 62252 89.0158 8.8182 0012490 354.3476 5.7532 13.51034308111536Epoch: 2026-11-01T04:57Z
TLE epoch observation values (Epoch: 2026-11-01T04:57:29.331Z)
Latitude
-0.00007°
Longitude
-106.0553°
Altitude
1,062.153 km
Speed
7.325 km/s
True Right ascension
00h 35m 16s
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
07:36:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.804 km
Perigee altitude
1,056.209 km
Semi-major axis
7,443.643 km
Eccentricity
0.00125
Inclination
89.0158°
RAAN
8.8182°
Arg. of periapsis
354.3476°
True anomaly
5.76757°
Mean anomaly
5.7532°
Eccentric anomaly
5.76038°
Mean motion
3.3796 °/min
Orbital period
106.52 mins
BSTAR
0.00012452
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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 | 2026-11-01 16:12:40.190Z | 10.794° NNE | 2026-11-01 16:18:40.190Z | 81.606° E | 54.665° | 2026-11-01 16:24:40.190Z | 162.531° S |
| 8 mins | 2026-11-01 18:01:40.190Z | 321.241° NNW | 2026-11-01 18:04:40.190Z | 287.166° WNW | 23.902° | 2026-11-01 18:09:40.190Z | 236.054° WSW |
| 11 mins | 2026-11-02 04:10:40.190Z | 150.04° SSE | 2026-11-02 04:15:40.190Z | 86.754° E | 47.577° | 2026-11-02 04:21:40.190Z | 12.078° NNE |
| 9 mins | 2026-11-02 05:58:40.190Z | 233.729° WSW | 2026-11-02 06:02:40.190Z | 280.913° WNW | 26.748° | 2026-11-02 06:07:40.190Z | 333.362° 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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