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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-42
1 62243U 24232G 25342.27704398 .00000772 00000-0 32680-3 0 9994
2 62243 89.0019 37.8668 0017338 99.2800 261.0354 14.24482064100731Epoch: 2025-12-08T06:38Z
TLE epoch observation values (Epoch: 2025-12-08T06:38:56.599Z)
Latitude
-0.00007°
Longitude
-139.14742°
Altitude
815.258 km
Speed
7.445 km/s
True Right ascension
02h 31m 28s
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
10:52:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
819.637 km
Perigee altitude
794.721 km
Semi-major axis
7,185.316 km
Eccentricity
0.00173
Inclination
89.0019°
RAAN
37.8668°
Arg. of periapsis
99.28°
True anomaly
260.83921°
Mean anomaly
261.0354°
Eccentric anomaly
260.9373°
Mean motion
3.56348 °/min
Orbital period
101.02 mins
BSTAR
0.0003268
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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
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-08 15:39:40.753Z | 18.404° NNE | 2025-12-08 15:43:40.753Z | 78.915° E | 34.133° | 2025-12-08 15:48:40.753Z | 156.628° SSE |
| 5 mins | 2025-12-08 17:22:40.753Z | 311.611° NW | 2025-12-08 17:24:40.753Z | 282.153° WNW | 19.971° | 2025-12-08 17:27:40.753Z | 242.167° WSW |
| 5 mins | 2025-12-09 03:02:40.753Z | 100.049° ESE | 2025-12-09 03:04:40.753Z | 73.804° E | 16.296° | 2025-12-09 03:07:40.753Z | 38.187° NE |
| 8 mins | 2025-12-09 04:41:40.753Z | 200.924° SSW | 2025-12-09 04:44:40.753Z | 252.23° W | 38.644° | 2025-12-09 04:49:40.753Z | 347.893° N |
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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