QIANFAN-52, 62253
Orbit data source: Space-Track
QIANFAN-52, 62253 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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62253 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-52
1 62253U 24232S 25287.92191542 .00000145 00000-0 20646-3 0 9999
2 62253 89.0013 47.0353 0015116 9.2823 350.8605 13.50978685 60006Epoch: 2025-10-14T22:07Z
TLE epoch observation values (Epoch: 2025-10-14T22:07:33.492Z)
Latitude
0.00003°
Longitude
51.44235°
Altitude
1,060.498 km
Speed
7.327 km/s
True Right ascension
03h 08m 08s
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
02:14:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.963 km
Perigee altitude
1,054.459 km
Semi-major axis
7,443.848 km
Eccentricity
0.00151
Inclination
89.0013°
RAAN
47.0353°
Arg. of periapsis
9.2823°
True anomaly
350.83294°
Mean anomaly
350.8605°
Eccentric anomaly
350.84672°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00020646
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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-52 Visibility forecast
Loading observer location...
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 | 2025-10-15 08:52:58.870Z | 192.817° SSW | 2025-10-15 08:58:58.870Z | 261.423° W | 40.764° | 2025-10-15 09:04:58.870Z | 350.068° N |
| 11 mins | 2025-10-15 20:03:58.870Z | 9.725° NNE | 2025-10-15 20:08:58.870Z | 98.253° ESE | 42.682° | 2025-10-15 20:14:58.870Z | 171.107° S |
| 7 mins | 2025-10-15 21:51:58.870Z | 315.089° NNW | 2025-10-15 21:54:58.870Z | 282.743° WNW | 18.214° | 2025-10-15 21:58:58.870Z | 244.932° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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