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 25352.89708853 .00000089 00000-0 11900-3 0 9999
2 62255 89.0015 40.2735 0002170 161.8091 198.3138 13.50980382100241Epoch: 2025-12-18T21:31Z
TLE epoch observation values (Epoch: 2025-12-18T21:31:48.448Z)
Latitude
-0.00007°
Longitude
-10.42438°
Altitude
1,073.141 km
Speed
7.315 km/s
True Right ascension
02h 41m 05s
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
03:42:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.32 km
Perigee altitude
1,064.089 km
Semi-major axis
7,443.842 km
Eccentricity
0.00022
Inclination
89.0015°
RAAN
40.2735°
Arg. of periapsis
161.8091°
True anomaly
198.30599°
Mean anomaly
198.3138°
Eccentric anomaly
198.30989°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.000119
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-19 04:51:01.949Z | 288.901° WNW | 2025-12-19 04:51:01.949Z | 288.901° WNW | 28.292° | 2025-12-19 04:56:01.949Z | 339.282° N |
| 6 mins | 2025-12-19 14:10:01.949Z | 49.335° ENE | 2025-12-19 14:13:01.949Z | 81.363° E | 17.269° | 2025-12-19 14:16:01.949Z | 111.285° ESE |
| 11 mins | 2025-12-19 15:55:01.949Z | 353.146° N | 2025-12-19 16:00:01.949Z | 256.94° W | 42.949° | 2025-12-19 16:06:01.949Z | 193.12° SSW |
| 5 mins | 2025-12-20 02:09:01.949Z | 92.051° ESE | 2025-12-20 02:11:01.949Z | 71.682° E | 15.442° | 2025-12-20 02:14:01.949Z | 42.571° NE |
| 11 mins | 2025-12-20 03:52:01.949Z | 184.328° SSW | 2025-12-20 03:57:01.949Z | 305.425° NW | 44.201° | 2025-12-20 04:03:01.949Z | 356.481° 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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