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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-54
1 62255U 24232U 25307.86583717 .00000167 00000-0 23986-3 0 9990
2 62255 89.0038 44.8101 0002012 41.7539 318.3765 13.50983311 94169Epoch: 2025-11-03T20:46Z
TLE epoch observation values (Epoch: 2025-11-03T20:46:48.331Z)
Latitude
-0.00006°
Longitude
49.74765°
Altitude
1,070.476 km
Speed
7.317 km/s
True Right ascension
02h 59m 14s
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
01:14:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.192 km
Perigee altitude
1,064.196 km
Semi-major axis
7,443.831 km
Eccentricity
0.0002
Inclination
89.0038°
RAAN
44.8101°
Arg. of periapsis
41.7539°
True anomaly
318.36118°
Mean anomaly
318.3765°
Eccentric anomaly
318.36884°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.00023986
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-04 05:48:13.433Z | 121.103° SE | 2025-11-04 05:52:13.433Z | 78.939° E | 22.251° | 2025-11-04 05:57:13.433Z | 27.018° NE |
| 11 mins | 2025-11-04 07:33:13.433Z | 200.016° SSW | 2025-11-04 07:38:13.433Z | 263.215° W | 38.545° | 2025-11-04 07:44:13.433Z | 347.495° N |
| 12 mins | 2025-11-04 18:42:13.433Z | 4.92° NNE | 2025-11-04 18:48:13.433Z | 101.658° ESE | 44.067° | 2025-11-04 18:54:13.433Z | 175.561° S |
| 6 mins | 2025-11-04 20:31:13.433Z | 313.974° NW | 2025-11-04 20:34:13.433Z | 283.293° WNW | 16.079° | 2025-11-04 20:37:13.433Z | 254.637° W |
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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