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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-54
1 62255U 24232U 26035.15004109 .00000022 00000-0 15022-4 0 9997
2 62255 89.0003 35.4949 0004078 84.8578 275.3039 13.50985559106629Epoch: 2026-02-04T03:36Z
TLE epoch observation values (Epoch: 2026-02-04T03:36:03.550Z)
Latitude
0.00005°
Longitude
-152.84065°
Altitude
1,071.308 km
Speed
7.316 km/s
True Right ascension
02h 21m 58s
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
12:22:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,068.721 km
Perigee altitude
1,062.65 km
Semi-major axis
7,443.823 km
Eccentricity
0.00041
Inclination
89.0003°
RAAN
35.4949°
Arg. of periapsis
84.8578°
True anomaly
275.25737°
Mean anomaly
275.3039°
Eccentric anomaly
275.28063°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.000015022
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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
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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-02-04 11:18:39.067Z | 22.115° NNE | 2026-02-04 11:23:39.067Z | 77.253° E | 29.07° | 2026-02-04 11:29:39.067Z | 145.237° SSE |
| 10 mins | 2026-02-04 13:05:39.067Z | 339.516° N | 2026-02-04 13:10:39.067Z | 276.232° WNW | 31.357° | 2026-02-04 13:15:39.067Z | 218.609° SW |
| 9 mins | 2026-02-04 23:17:39.067Z | 124.867° SE | 2026-02-04 23:21:39.067Z | 74.811° E | 26.461° | 2026-02-04 23:26:39.067Z | 22.091° NNE |
| 11 mins | 2026-02-05 01:02:39.067Z | 209.272° SW | 2026-02-05 01:07:39.067Z | 272.884° WNW | 34.193° | 2026-02-05 01:13:39.067Z | 344.373° 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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