QIANFAN-38, 62239
Orbit data source: Space-Track
QIANFAN-38, 62239 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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62239 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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-38
1 62239U 24232C 25339.90698538 .00000198 00000-0 28842-3 0 9990
2 62239 89.0034 41.9341 0014015 207.4765 152.5647 13.50979329 98300Epoch: 2025-12-05T21:46Z
TLE epoch observation values (Epoch: 2025-12-05T21:46:03.536Z)
Latitude
-0.00001°
Longitude
0.47702°
Altitude
1,080.879 km
Speed
7.307 km/s
True Right ascension
02h 47m 44s
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
06:50:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.141 km
Perigee altitude
1,055.276 km
Semi-major axis
7,443.846 km
Eccentricity
0.0014
Inclination
89.0034°
RAAN
41.9341°
Arg. of periapsis
207.4765°
True anomaly
152.63858°
Mean anomaly
152.5647°
Eccentric anomaly
152.60165°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00028842
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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-38 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-06 16:08:33.374Z | 11.804° NNE | 2025-12-06 16:14:33.374Z | 103.494° ESE | 39.407° | 2025-12-06 16:19:33.374Z | 162.732° S |
| 8 mins | 2025-12-06 17:56:33.374Z | 324.019° NNW | 2025-12-06 18:00:33.374Z | 279.124° WNW | 21.055° | 2025-12-06 18:04:33.374Z | 239.179° WSW |
| 10 mins | 2025-12-07 04:06:33.374Z | 148.862° SSE | 2025-12-07 04:11:33.374Z | 70.918° E | 37.027° | 2025-12-07 04:16:33.374Z | 12.893° NNE |
| 9 mins | 2025-12-07 05:53:33.374Z | 231.507° WSW | 2025-12-07 05:57:33.374Z | 274.633° WNW | 23.7° | 2025-12-07 06:02:33.374Z | 329.993° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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