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 26246.82126907 .00000083 00000-0 10979-3 0 9998
2 62255 89.0136 14.2664 0002908 149.3123 210.8199 13.51027111135207Epoch: 2026-09-03T19:42Z
TLE epoch observation values (Epoch: 2026-09-03T19:42:37.647Z)
Latitude
-0°
Longitude
95.65559°
Altitude
1,073.296 km
Speed
7.314 km/s
True Right ascension
00h 57m 03s
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
20:52:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.698 km
Perigee altitude
1,063.368 km
Semi-major axis
7,443.67 km
Eccentricity
0.00029
Inclination
89.0136°
RAAN
14.2664°
Arg. of periapsis
149.3123°
True anomaly
210.80283°
Mean anomaly
210.8199°
Eccentric anomaly
210.81137°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.00010979
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-09-04 08:15:55.173Z | 144.92° SSE | 2026-09-04 08:20:55.173Z | 87.391° E | 33.167° | 2026-09-04 08:26:55.173Z | 15.065° NNE |
| 9 mins | 2026-09-04 10:03:55.173Z | 228.735° WSW | 2026-09-04 10:07:55.173Z | 279.957° WNW | 27.367° | 2026-09-04 10:12:55.173Z | 335.515° NNW |
| 7 mins | 2026-09-04 19:26:55.173Z | 44.2° NE | 2026-09-04 19:29:55.173Z | 75.838° E | 18.382° | 2026-09-04 19:33:55.173Z | 116.597° SE |
| 11 mins | 2026-09-04 21:11:55.173Z | 352.594° N | 2026-09-04 21:16:55.173Z | 284.643° WNW | 42.207° | 2026-09-04 21:22:55.173Z | 196.11° SSW |
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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