QIANFAN-46, 62247
Orbit data source: Space-Track
QIANFAN-46, 62247 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
62247 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-46
1 62247U 24232L 25242.89877341 .00000093 00000-0 12565-3 0 9990
2 62247 88.9947 51.7654 0015862 134.0052 226.2409 13.50968721 85193
TLE epoch observation values (Epoch: 2025-08-30T21:34:14.022Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #232 in the year 2024 (2024-12-05 UTC)
QIANFAN-46 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. |
---|---|---|---|---|---|---|---|
6 mins | 2025-08-31 10:10:25.841Z | 102.292° ESE | 2025-08-31 10:13:25.841Z | 73.498° E | 15.42° | 2025-08-31 10:16:25.841Z | 43.984° NE |
11 mins | 2025-08-31 11:54:25.841Z | 184.111° SSW | 2025-08-31 11:59:25.841Z | 289.21° WNW | 44.404° | 2025-08-31 12:05:25.841Z | 356.332° N |
11 mins | 2025-08-31 23:03:25.841Z | 14.553° NNE | 2025-08-31 23:08:25.841Z | 76.194° E | 37.505° | 2025-08-31 23:14:25.841Z | 159.466° S |
8 mins | 2025-09-01 00:51:25.841Z | 324.28° NNW | 2025-09-01 00:54:25.841Z | 290.24° WNW | 22.815° | 2025-09-01 00:59:25.841Z | 235.416° WSW |
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 |
---|