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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-48
1 62249U 24232N 25353.22213406 .00000083 00000-0 10919-3 0 9998
2 62249 89.0021 40.5701 0017563 175.4918 184.6394 13.50980450100123Epoch: 2025-12-19T05:19Z
TLE epoch observation values (Epoch: 2025-12-19T05:19:52.382Z)
Latitude
-0.0001°
Longitude
-127.46455°
Altitude
1,084.645 km
Speed
7.303 km/s
True Right ascension
02h 42m 16s
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
15:37:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.778 km
Perigee altitude
1,052.631 km
Semi-major axis
7,443.841 km
Eccentricity
0.00176
Inclination
89.0021°
RAAN
40.5701°
Arg. of periapsis
175.4918°
True anomaly
184.62316°
Mean anomaly
184.6394°
Eccentric anomaly
184.63127°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00010919
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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
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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-20 02:48:00.307Z | 128.872° SE | 2025-12-20 02:52:00.307Z | 77.159° E | 28.666° | 2025-12-20 02:57:00.307Z | 21.303° NNE |
| 10 mins | 2025-12-20 04:34:00.307Z | 217.61° SW | 2025-12-20 04:38:00.307Z | 270.061° WNW | 32.151° | 2025-12-20 04:44:00.307Z | 341.929° N |
| 5 mins | 2025-12-20 13:58:00.307Z | 50.939° ENE | 2025-12-20 14:00:00.307Z | 70.434° E | 14.494° | 2025-12-20 14:03:00.307Z | 100.175° ESE |
| 11 mins | 2025-12-20 15:43:00.307Z | 357.656° N | 2025-12-20 15:48:00.307Z | 239.346° WSW | 44.471° | 2025-12-20 15:54:00.307Z | 187.276° 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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