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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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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-54
1 62255U 24232U 26047.81490134 .00000041 00000-0 44786-4 0 9990
2 62255 89.0021 34.2158 0003881 64.7552 295.4001 13.51001141108337Epoch: 2026-02-16T19:33Z
TLE epoch observation values (Epoch: 2026-02-16T19:33:27.475Z)
Latitude
-0.00005°
Longitude
-45.95252°
Altitude
1,070.292 km
Speed
7.317 km/s
True Right ascension
02h 16m 51s
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
07:49:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,068.517 km
Perigee altitude
1,062.739 km
Semi-major axis
7,443.765 km
Eccentricity
0.00039
Inclination
89.0021°
RAAN
34.2158°
Arg. of periapsis
64.7552°
True anomaly
295.35992°
Mean anomaly
295.4001°
Eccentric anomaly
295.38001°
Mean motion
3.37951 °/min
Orbital period
106.52 mins
BSTAR
0.000044786
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-02-17 10:22:57.846Z | 23.727° NE | 2026-02-17 10:27:57.846Z | 82.941° E | 29.304° | 2026-02-17 10:32:57.846Z | 141.93° SSE |
| 10 mins | 2026-02-17 12:09:57.846Z | 337.652° N | 2026-02-17 12:13:57.846Z | 289.832° WNW | 31.011° | 2026-02-17 12:19:57.846Z | 217.374° SW |
| 10 mins | 2026-02-17 22:20:57.846Z | 129.707° SE | 2026-02-17 22:24:57.846Z | 85.609° E | 26.385° | 2026-02-17 22:30:57.846Z | 20.363° NNE |
| 10 mins | 2026-02-18 00:06:57.846Z | 211.108° SW | 2026-02-18 00:11:57.846Z | 280.557° WNW | 33.998° | 2026-02-18 00:16:57.846Z | 341.444° 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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