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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-48
1 62249U 24232N 25308.78346479 .00000179 00000-0 25891-3 0 9997
2 62249 89.0045 45.0441 0015405 313.0476 46.9384 13.50981957 94126Epoch: 2025-11-04T18:48Z
TLE epoch observation values (Epoch: 2025-11-04T18:48:11.357Z)
Latitude
-0.00007°
Longitude
78.73125°
Altitude
1,063.776 km
Speed
7.324 km/s
True Right ascension
03h 00m 10s
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
23:04:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.166 km
Perigee altitude
1,054.232 km
Semi-major axis
7,443.836 km
Eccentricity
0.00154
Inclination
89.0045°
RAAN
45.0441°
Arg. of periapsis
313.0476°
True anomaly
47.06754°
Mean anomaly
46.9384°
Eccentric anomaly
47.00296°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.00025891
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-05 05:37:01.304Z | 111.89° ESE | 2025-11-05 05:41:01.304Z | 69.346° E | 19.353° | 2025-11-05 05:45:01.304Z | 30.832° NE |
| 11 mins | 2025-11-05 07:22:01.304Z | 195.992° SSW | 2025-11-05 07:27:01.304Z | 293.055° NW | 41.105° | 2025-11-05 07:33:01.304Z | 352.376° N |
| 11 mins | 2025-11-05 18:31:01.304Z | 9.831° NNE | 2025-11-05 18:36:01.304Z | 80.243° E | 42.161° | 2025-11-05 18:42:01.304Z | 169.093° S |
| 7 mins | 2025-11-05 20:19:01.304Z | 318.493° NNW | 2025-11-05 20:22:01.304Z | 286.638° WNW | 18.976° | 2025-11-05 20:26:01.304Z | 246.52° WSW |
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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