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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-47
1 62248U 24232M 25256.23459847 .00000049 00000-0 56941-4 0 9999
2 62248 88.9963 50.3484 0016785 99.1389 261.1662 13.50963121 87029Epoch: 2025-09-13T05:37Z
TLE epoch observation values (Epoch: 2025-09-13T05:37:49.307Z)
Latitude
-0.00004°
Longitude
-26.57793°
Altitude
1,073.611 km
Speed
7.314 km/s
True Right ascension
03h 21m 23s
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
16:06:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.263 km
Perigee altitude
1,053.274 km
Semi-major axis
7,443.905 km
Eccentricity
0.00168
Inclination
88.9963°
RAAN
50.3484°
Arg. of periapsis
99.1389°
True anomaly
260.9762°
Mean anomaly
261.1662°
Eccentric anomaly
261.07119°
Mean motion
3.37942 °/min
Orbital period
106.53 mins
BSTAR
0.000056941
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-14 00:01:00.879Z | 327.572° NNW | 2025-09-14 00:05:00.879Z | 285.669° WNW | 20.73° | 2025-09-14 00:09:00.879Z | 243.134° WSW |
| 11 mins | 2025-09-14 10:11:00.879Z | 152.316° SSE | 2025-09-14 10:16:00.879Z | 88.93° E | 37.48° | 2025-09-14 10:22:00.879Z | 11.242° NNE |
| 9 mins | 2025-09-14 11:59:00.879Z | 234.675° WSW | 2025-09-14 12:03:00.879Z | 279.945° WNW | 23.091° | 2025-09-14 12:08:00.879Z | 332.189° NNW |
| 8 mins | 2025-09-14 21:22:00.879Z | 41.511° NE | 2025-09-14 21:25:00.879Z | 76.27° E | 22.023° | 2025-09-14 21:30:00.879Z | 129.009° SE |
| 11 mins | 2025-09-14 23:07:00.879Z | 347.585° N | 2025-09-14 23:12:00.879Z | 279.572° WNW | 38.573° | 2025-09-14 23:18:00.879Z | 203.557° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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