QIANFAN-22, 61555
Orbit data source: Space-Track
QIANFAN-22, 61555 is a Chinese payload satellite in LEO that was launched on Tue, 15 Oct 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
61555 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-22
1 61555U 24185D 25243.28337627 .00000274 00000-0 22578-3 0 9996
2 61555 88.9751 90.5960 0005510 327.4910 32.5921 13.86247255 54608
TLE epoch observation values (Epoch: 2025-08-31T06:48:03.709Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #185 in the year 2024 (2024-10-15 UTC)
QIANFAN-22 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 | 2025-09-01 00:44:28.733Z | 45.485° ENE | 2025-09-01 00:47:28.733Z | 77.878° E | 15.644° | 2025-09-01 00:50:28.733Z | 109.821° ESE |
10 mins | 2025-09-01 02:27:28.733Z | 352.951° N | 2025-09-01 02:31:28.733Z | 295.152° NW | 42.727° | 2025-09-01 02:37:28.733Z | 192.872° SSW |
10 mins | 2025-09-01 14:06:28.733Z | 167.24° S | 2025-09-01 14:10:28.733Z | 90.524° ESE | 43.811° | 2025-09-01 14:16:28.733Z | 3.142° NNE |
4 mins | 2025-09-01 15:53:28.733Z | 267.007° W | 2025-09-01 15:55:28.733Z | 289.378° WNW | 14.378° | 2025-09-01 15:57:28.733Z | 310.392° NW |
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 |
---|