QIANFAN-53, 62254
Orbit data source: Space-Track
QIANFAN-53, 62254 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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62254 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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-53
1 62254U 24232T 25339.96870076 .00000172 00000-0 24808-3 0 9992
2 62254 89.0036 41.8986 0013735 205.3030 154.7450 13.50977240 66999Epoch: 2025-12-05T23:14Z
TLE epoch observation values (Epoch: 2025-12-05T23:14:55.745Z)
Latitude
-0.00003°
Longitude
-21.83685°
Altitude
1,080.873 km
Speed
7.307 km/s
True Right ascension
02h 47m 35s
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
05:10:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.94 km
Perigee altitude
1,055.492 km
Semi-major axis
7,443.853 km
Eccentricity
0.00137
Inclination
89.0036°
RAAN
41.8986°
Arg. of periapsis
205.303°
True anomaly
154.81205°
Mean anomaly
154.745°
Eccentric anomaly
154.77853°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00024808
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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-53 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-06 15:50:38.334Z | 17.507° NNE | 2025-12-06 15:56:38.334Z | 93.185° ESE | 33.098° | 2025-12-06 16:01:38.334Z | 150.591° SSE |
| 9 mins | 2025-12-06 17:38:38.334Z | 330.765° NNW | 2025-12-06 17:42:38.334Z | 280.669° WNW | 27.285° | 2025-12-06 17:47:38.334Z | 225.706° WSW |
| 10 mins | 2025-12-07 03:48:38.334Z | 138.344° SSE | 2025-12-07 03:53:38.334Z | 77.4° E | 30.675° | 2025-12-07 03:58:38.334Z | 19.715° NNE |
| 10 mins | 2025-12-07 05:35:38.334Z | 220.819° SW | 2025-12-07 05:39:38.334Z | 270.275° WNW | 30.087° | 2025-12-07 05:45:38.334Z | 340.121° N |
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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