ONEWEB-0691, 61599
Orbit data source: Space-Track
ONEWEB-0691, 61599 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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61599 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ONEWEB-0691
1 61599U 24188F 25288.81730937 -.00000448 00000-0 -13001-2 0 9991
2 61599 87.8770 69.6403 0001433 84.8188 275.3103 13.11417697 52452
TLE epoch observation values (Epoch: 2025-10-15T19:36:55.529Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #188 in the year 2024 (2024-10-20 UTC)
ONEWEB-0691 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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10 mins | 2025-10-16 08:33:42.068Z | 121.573° SE | 2025-10-16 08:38:42.068Z | 76.695° E | 21.127° | 2025-10-16 08:43:42.068Z | 30.506° NE |
12 mins | 2025-10-16 10:22:42.068Z | 196.204° SSW | 2025-10-16 10:27:42.068Z | 258.674° W | 41.708° | 2025-10-16 10:34:42.068Z | 353.346° N |
8 mins | 2025-10-16 20:03:42.068Z | 42.65° NE | 2025-10-16 20:06:42.068Z | 69.908° E | 16.984° | 2025-10-16 20:11:42.068Z | 113.491° SE |
13 mins | 2025-10-16 21:51:42.068Z | 356.021° N | 2025-10-16 21:57:42.068Z | 277.449° WNW | 44.454° | 2025-10-16 22:04:42.068Z | 187.306° SSW |
4 mins | 2025-10-16 23:44:42.068Z | 304.473° NW | 2025-10-16 23:46:42.068Z | 287.596° WNW | 12.157° | 2025-10-16 23:48:42.068Z | 271.138° WNW |
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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