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: 17 hours ago
TLE from 17 hours ago
0 QIANFAN-38
1 62239U 24232C 25287.91372829 .00000162 00000-0 23160-3 0 9994
2 62239 89.0018 47.1667 0014419 12.4933 347.6573 13.50979257 91285Epoch: 2025-10-14T21:55Z
TLE epoch observation values (Epoch: 2025-10-14T21:55:46.124Z)
Latitude
0.00002°
Longitude
54.52919°
Altitude
1,061.12 km
Speed
7.327 km/s
True Right ascension
03h 08m 40s
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
09:07:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.442 km
Perigee altitude
1,054.976 km
Semi-major axis
7,443.846 km
Eccentricity
0.00144
Inclination
89.0018°
RAAN
47.1667°
Arg. of periapsis
12.4933°
True anomaly
347.62192°
Mean anomaly
347.6573°
Eccentric anomaly
347.63962°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.0002316
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-15 19:50:38.105Z | 10.342° NNE | 2025-10-15 19:56:38.105Z | 74.908° E | 38.83° | 2025-10-15 20:02:38.105Z | 161.614° S |
| 8 mins | 2025-10-15 21:39:38.105Z | 323.194° NNW | 2025-10-15 21:42:38.105Z | 290.002° WNW | 22.024° | 2025-10-15 21:47:38.105Z | 237.132° WSW |
| 10 mins | 2025-10-16 07:49:38.105Z | 146.726° SSE | 2025-10-16 07:53:38.105Z | 94.725° ESE | 35.882° | 2025-10-16 07:59:38.105Z | 13.197° NNE |
| 9 mins | 2025-10-16 09:36:38.105Z | 231.161° WSW | 2025-10-16 09:40:38.105Z | 276.384° WNW | 24.254° | 2025-10-16 09:45:38.105Z | 331.694° 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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