QIANFAN-54, 62255
Orbit data source: Space-Track
QIANFAN-54, 62255 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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62255 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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-54
1 62255U 24232U 25321.78997236 -.00000008 00000-0 -30329-4 0 9998
2 62255 89.0041 43.4085 0000729 12.7750 347.3420 13.50971481 96049Epoch: 2025-11-17T18:57Z
TLE epoch observation values (Epoch: 2025-11-17T18:57:33.611Z)
Latitude
0.00001°
Longitude
61.93309°
Altitude
1,071.11 km
Speed
7.317 km/s
True Right ascension
02h 53m 38s
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
02:18:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,066.28 km
Perigee altitude
1,065.195 km
Semi-major axis
7,443.874 km
Eccentricity
0.00007
Inclination
89.0041°
RAAN
43.4085°
Arg. of periapsis
12.775°
True anomaly
347.34017°
Mean anomaly
347.342°
Eccentric anomaly
347.34108°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
-0.000030329
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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-54 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 | 2025-11-18 05:43:32.348Z | 164.886° S | 2025-11-18 05:49:32.348Z | 73.632° E | 42.579° | 2025-11-18 05:55:32.348Z | 5.148° NNE |
| 7 mins | 2025-11-18 07:33:32.348Z | 252.34° W | 2025-11-18 07:36:32.348Z | 284.28° WNW | 17.951° | 2025-11-18 07:40:32.348Z | 323.486° NNW |
| 9 mins | 2025-11-18 16:54:32.348Z | 30.196° NE | 2025-11-18 16:58:32.348Z | 79.684° E | 27.954° | 2025-11-18 17:03:32.348Z | 138.818° SSE |
| 10 mins | 2025-11-18 18:40:32.348Z | 340.044° N | 2025-11-18 18:45:32.348Z | 273.314° WNW | 32.562° | 2025-11-18 18:50:32.348Z | 216.133° SW |
| 9 mins | 2025-11-19 04:52:32.348Z | 122.134° SE | 2025-11-19 04:56:32.348Z | 72.817° E | 25.292° | 2025-11-19 05:01:32.348Z | 22.285° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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