ONEWEB-0699, 61605
Orbit data source: Space-Track
ONEWEB-0699, 61605 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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61605 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 ONEWEB-0699
1 61605U 24188M 25256.26685456 -.00000581 00000-0 -16998-2 0 9994
2 61605 87.8746 91.4781 0001249 104.0895 256.0371 13.10373593 47047
TLE epoch observation values (Epoch: 2025-09-13T06:24:16.233Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #188 in the year 2024 (2024-10-20 UTC)
ONEWEB-0699 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. |
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7 mins | 2025-09-14 03:11:51.103Z | 318.742° NNW | 2025-09-14 03:15:51.103Z | 284.942° WNW | 14.262° | 2025-09-14 03:18:51.103Z | 259.998° W |
7 mins | 2025-09-14 11:53:51.103Z | 98.535° ESE | 2025-09-14 11:56:51.103Z | 70.534° E | 16.85° | 2025-09-14 12:00:51.103Z | 36.282° NE |
13 mins | 2025-09-14 13:39:51.103Z | 184.593° SSW | 2025-09-14 13:45:51.103Z | 291.009° WNW | 44.51° | 2025-09-14 13:52:51.103Z | 358.391° N |
5 mins | 2025-09-14 23:22:51.103Z | 53.246° ENE | 2025-09-14 23:24:51.103Z | 70.476° E | 13.283° | 2025-09-14 23:27:51.103Z | 95.677° ESE |
13 mins | 2025-09-15 01:09:51.103Z | 1.251° NNE | 2025-09-15 01:15:51.103Z | 67.785° E | 44.831° | 2025-09-15 01:22:51.103Z | 178.516° S |
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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