QIANFAN-47, 62248
Orbit data source: Space-Track
QIANFAN-47, 62248 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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62248 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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-47
1 62248U 24232M 25309.93137290 .00000117 00000-0 16265-3 0 9990
2 62248 89.0041 44.9281 0013075 306.8337 53.1614 13.50970656 94274Epoch: 2025-11-05T22:21Z
TLE epoch observation values (Epoch: 2025-11-05T22:21:10.618Z)
Latitude
-0.00006°
Longitude
24.23689°
Altitude
1,065.812 km
Speed
7.322 km/s
True Right ascension
02h 59m 42s
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
03:15:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.473 km
Perigee altitude
1,056.008 km
Semi-major axis
7,443.877 km
Eccentricity
0.00131
Inclination
89.0041°
RAAN
44.9281°
Arg. of periapsis
306.8337°
True anomaly
53.28143°
Mean anomaly
53.1614°
Eccentric anomaly
53.2214°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00016265
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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-47 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-06 07:20:21.472Z | 194.941° SSW | 2025-11-06 07:26:21.472Z | 277.072° WNW | 40.333° | 2025-11-06 07:32:21.472Z | 350.315° N |
| 12 mins | 2025-11-06 18:30:21.472Z | 7.352° NNE | 2025-11-06 18:36:21.472Z | 117.193° SE | 42.72° | 2025-11-06 18:42:21.472Z | 172.829° S |
| 6 mins | 2025-11-06 20:19:21.472Z | 311.77° NW | 2025-11-06 20:21:21.472Z | 290.627° WNW | 17.674° | 2025-11-06 20:25:21.472Z | 250.545° W |
| 11 mins | 2025-11-07 06:27:21.472Z | 160.408° S | 2025-11-07 06:32:21.472Z | 103.261° ESE | 40.768° | 2025-11-07 06:38:21.472Z | 8.221° NNE |
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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