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: 1 day ago
TLE from 1 day ago
0 QIANFAN-47
1 62248U 24232M 25339.26097619 .00000179 00000-0 25948-3 0 9995
2 62248 89.0031 41.9759 0014146 212.3674 147.6610 13.50975532 98238Epoch: 2025-12-05T06:15Z
TLE epoch observation values (Epoch: 2025-12-05T06:15:48.342Z)
Latitude
-0.00011°
Longitude
-126.28114°
Altitude
1,080.531 km
Speed
7.307 km/s
True Right ascension
02h 47m 54s
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
03:52:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.253 km
Perigee altitude
1,055.192 km
Semi-major axis
7,443.86 km
Eccentricity
0.00141
Inclination
89.0031°
RAAN
41.9759°
Arg. of periapsis
212.3674°
True anomaly
147.74758°
Mean anomaly
147.661°
Eccentric anomaly
147.7043°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00025948
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-06 14:53:38.464Z | 48.736° ENE | 2025-12-06 14:56:38.464Z | 77.028° E | 13.388° | 2025-12-06 14:58:38.464Z | 96.002° ESE |
| 11 mins | 2025-12-06 16:38:38.464Z | 0.054° NNE | 2025-12-06 16:43:38.464Z | 312.072° NW | 44.938° | 2025-12-06 16:49:38.464Z | 184.262° SSW |
| 4 mins | 2025-12-06 18:27:38.464Z | 305.051° NW | 2025-12-06 18:29:38.464Z | 286.067° WNW | 12.51° | 2025-12-06 18:31:38.464Z | 267.81° W |
| 11 mins | 2025-12-07 04:35:38.464Z | 172.985° S | 2025-12-07 04:40:38.464Z | 84.719° E | 44.773° | 2025-12-07 04:46:38.464Z | 1.091° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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