QIANFAN-42, 62243
Orbit data source: Space-Track
QIANFAN-42, 62243 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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62243 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Partially 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: 17 hours ago
TLE from 17 hours ago
0 QIANFAN-42
1 62243U 24232G 25287.90508722 .00000733 00000-0 31056-3 0 9998
2 62243 89.0019 44.0629 0012845 276.7651 83.2079 14.24391329 92991Epoch: 2025-10-14T21:43Z
TLE epoch observation values (Epoch: 2025-10-14T21:43:19.535Z)
Latitude
-0.00012°
Longitude
54.54469°
Altitude
812.519 km
Speed
7.447 km/s
True Right ascension
02h 56m 15s
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
09:06:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
816.715 km
Perigee altitude
798.255 km
Semi-major axis
7,185.622 km
Eccentricity
0.00128
Inclination
89.0019°
RAAN
44.0629°
Arg. of periapsis
276.7651°
True anomaly
83.35409°
Mean anomaly
83.2079°
Eccentric anomaly
83.28099°
Mean motion
3.56325 °/min
Orbital period
101.03 mins
BSTAR
0.00031056
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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-42 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-15 20:14:16.661Z | 358.868° N | 2025-10-15 20:18:16.661Z | 202.894° SW | 43.929° | 2025-10-15 20:22:16.661Z | 185.183° SSW |
| 8 mins | 2025-10-16 07:34:16.661Z | 140.341° SSE | 2025-10-16 07:38:16.661Z | 72.463° E | 30.889° | 2025-10-16 07:42:16.661Z | 18.593° NNE |
| 7 mins | 2025-10-16 09:16:16.661Z | 236.596° WSW | 2025-10-16 09:19:16.661Z | 281.832° WNW | 22.97° | 2025-10-16 09:23:16.661Z | 331.784° NNW |
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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