ONEWEB-0700, 61606
Orbit data source: Space-Track
ONEWEB-0700, 61606 is a payload satellite owned by Eut. One Web (UK) in LEO that was launched on Sun, 20 Oct 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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61606 intel report (Beta)
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TLE from 12 hours ago
0 ONEWEB-0700
1 61606U 24188N 25199.45853392 -.00000536 00000-0 -15720-2 0 9990
2 61606 87.8777 102.7160 0001751 54.1845 305.9445 13.10374503 39596
TLE epoch observation values (Epoch: 2025-07-18T11:00:17.33Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #188 in the year 2024 (2024-10-20 UTC)
ONEWEB-0700 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. |
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9 mins | 2025-07-19 04:07:09.919Z | 34.005° NE | 2025-07-19 04:12:09.919Z | 77.368° E | 16.664° | 2025-07-19 04:16:09.919Z | 111.394° ESE |
12 mins | 2025-07-19 05:57:09.919Z | 356.048° N | 2025-07-19 06:02:09.919Z | 311.216° NW | 44.327° | 2025-07-19 06:09:09.919Z | 186.717° SSW |
4 mins | 2025-07-19 07:50:09.919Z | 299.78° NW | 2025-07-19 07:51:09.919Z | 291.222° WNW | 12.543° | 2025-07-19 07:54:09.919Z | 266.593° W |
8 mins | 2025-07-19 16:29:09.919Z | 106.018° ESE | 2025-07-19 16:32:09.919Z | 77.741° E | 18.811° | 2025-07-19 16:37:09.919Z | 32.915° NE |
12 mins | 2025-07-19 18:16:09.919Z | 190.14° SSW | 2025-07-19 18:22:09.919Z | 299.398° NW | 43.191° | 2025-07-19 18:28:09.919Z | 355.442° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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