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: 14 hours ago
TLE from 14 hours ago
0 ONEWEB-0691
1 61599U 24188F 25258.22228630 -.00000406 00000-0 -11804-2 0 9998
2 61599 87.8712 75.7702 0001983 81.2725 278.8627 13.11419422 48447
TLE epoch observation values (Epoch: 2025-09-15T05:20:05.536Z)
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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8 mins | 2025-09-15 22:26:18.743Z | 35.375° NE | 2025-09-15 22:30:18.743Z | 69.195° E | 16.179° | 2025-09-15 22:34:18.743Z | 105.074° ESE |
13 mins | 2025-09-16 00:15:18.743Z | 357.106° N | 2025-09-16 00:21:18.743Z | 291.544° WNW | 44.704° | 2025-09-16 00:28:18.743Z | 185.564° SSW |
4 mins | 2025-09-16 02:08:18.743Z | 305.417° NW | 2025-09-16 02:10:18.743Z | 288.249° WNW | 12.89° | 2025-09-16 02:12:18.743Z | 271.336° WNW |
8 mins | 2025-09-16 10:47:18.743Z | 107.26° ESE | 2025-09-16 10:51:18.743Z | 69.835° E | 18.13° | 2025-09-16 10:55:18.743Z | 34.921° NE |
13 mins | 2025-09-16 12:34:18.743Z | 188.244° SSW | 2025-09-16 12:40:18.743Z | 293.756° NW | 43.762° | 2025-09-16 12:47:18.743Z | 357.203° 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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