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.
Embed this page
62239 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-38
1 62239U 24232C 25242.88230124 .00000075 00000-0 96550-4 0 9999
2 62239 88.9947 51.7240 0016052 130.8996 229.3549 13.50965147 85208
TLE epoch observation values (Epoch: 2025-08-30T21:10:30.827Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #232 in the year 2024 (2024-12-05 UTC)
QIANFAN-38 Visibility forecast
Observer location: undefined°, undefined°
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 | 2025-08-31 11:29:35.507Z | 166.903° S | 2025-08-31 11:35:35.507Z | 86.147° E | 43.258° | 2025-08-31 11:41:35.507Z | 4.583° NNE |
7 mins | 2025-08-31 13:19:35.507Z | 251.196° W | 2025-08-31 13:22:35.507Z | 281.74° WNW | 17.187° | 2025-08-31 13:26:35.507Z | 321.248° NNW |
10 mins | 2025-08-31 22:40:35.507Z | 28.034° NE | 2025-08-31 22:44:35.507Z | 76.709° E | 28.62° | 2025-08-31 22:50:35.507Z | 144.729° SSE |
10 mins | 2025-09-01 00:26:35.507Z | 340.017° N | 2025-09-01 00:31:35.507Z | 276.892° WNW | 31.514° | 2025-09-01 00:36:35.507Z | 218.268° SW |
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 |
---|
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
---|
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|