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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-54
1 62255U 24232U 25310.30995385 .00000201 00000-0 29302-3 0 9998
2 62255 89.0039 44.5640 0001797 37.4292 322.6984 13.50984311 94490Epoch: 2025-11-06T07:26Z
TLE epoch observation values (Epoch: 2025-11-06T07:26:20.012Z)
Latitude
-0.00004°
Longitude
-112.78949°
Altitude
1,070.528 km
Speed
7.317 km/s
True Right ascension
02h 58m 15s
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
09:19:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.028 km
Perigee altitude
1,064.353 km
Semi-major axis
7,443.827 km
Eccentricity
0.00018
Inclination
89.0039°
RAAN
44.564°
Arg. of periapsis
37.4292°
True anomaly
322.68592°
Mean anomaly
322.6984°
Eccentric anomaly
322.69216°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.00029302
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-06 16:58:21.723Z | 56.003° ENE | 2025-11-06 17:00:21.723Z | 74.601° E | 12.23° | 2025-11-06 17:02:21.723Z | 93.007° ESE |
| 11 mins | 2025-11-06 18:42:21.723Z | 2.098° NNE | 2025-11-06 18:47:21.723Z | 24.412° NE | 44.666° | 2025-11-06 18:53:21.723Z | 180.924° SSW |
| 5 mins | 2025-11-06 20:31:21.723Z | 307.791° NW | 2025-11-06 20:33:21.723Z | 288.322° WNW | 13.871° | 2025-11-06 20:36:21.723Z | 260.575° W |
| 11 mins | 2025-11-07 06:39:21.723Z | 169.651° S | 2025-11-07 06:44:21.723Z | 111.495° ESE | 44.045° | 2025-11-07 06:50:21.723Z | 2.969° NNE |
| 6 mins | 2025-11-07 08:29:21.723Z | 259.029° W | 2025-11-07 08:31:21.723Z | 278.961° WNW | 15.562° | 2025-11-07 08:35:21.723Z | 317.997° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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