QIANFAN-48, 62249
Orbit data source: Space-Track
QIANFAN-48, 62249 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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62249 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: 17 hours ago
TLE from 17 hours ago
0 QIANFAN-48
1 62249U 24232N 25287.89732409 .00000162 00000-0 23303-3 0 9995
2 62249 89.0023 47.1465 0017123 16.7625 343.4088 13.50974704 91308Epoch: 2025-10-14T21:32Z
TLE epoch observation values (Epoch: 2025-10-14T21:32:08.801Z)
Latitude
-0.00007°
Longitude
60.43067°
Altitude
1,059.407 km
Speed
7.328 km/s
True Right ascension
03h 08m 35s
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
09:06:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.472 km
Perigee altitude
1,052.979 km
Semi-major axis
7,443.863 km
Eccentricity
0.00171
Inclination
89.0023°
RAAN
47.1465°
Arg. of periapsis
16.7625°
True anomaly
343.35266°
Mean anomaly
343.4088°
Eccentric anomaly
343.38074°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00023303
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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-48 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 | 2025-10-15 19:27:18.703Z | 18.437° NNE | 2025-10-15 19:33:18.703Z | 84.313° E | 30.307° | 2025-10-15 19:38:18.703Z | 143.616° SSE |
| 10 mins | 2025-10-15 21:15:18.703Z | 336.315° NNW | 2025-10-15 21:19:18.703Z | 288.094° WNW | 30.348° | 2025-10-15 21:25:18.703Z | 218.441° SW |
| 9 mins | 2025-10-16 07:26:18.703Z | 130.669° SE | 2025-10-16 07:30:18.703Z | 84.981° E | 27.159° | 2025-10-16 07:35:18.703Z | 24.671° NE |
| 10 mins | 2025-10-16 09:12:18.703Z | 212.876° SW | 2025-10-16 09:17:18.703Z | 281.495° WNW | 32.962° | 2025-10-16 09:22:18.703Z | 340.896° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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