ONEWEB-0080, 45426
Orbit data source: Space-Track
ONEWEB-0080, 45426 is a payload satellite owned by One Web (UK) in LEO that was launched on Sat, 21 Mar 2020 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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45426 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 ONEWEB-0080
1 45426U 20020C 25257.53307075 -.00000360 00000-0 -10519-2 0 9995
2 45426 87.8783 75.9776 0001315 88.3540 271.7739 13.11416037266572
TLE epoch observation values (Epoch: 2025-09-14T12:47:37.312Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #20 in the year 2020 (2020-03-21 UTC)
ONEWEB-0080 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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9 mins | 2025-09-15 10:54:04.405Z | 117.021° SE | 2025-09-15 10:59:04.405Z | 72.962° E | 19.086° | 2025-09-15 11:03:04.405Z | 36.308° NE |
13 mins | 2025-09-15 12:42:04.405Z | 189.918° SSW | 2025-09-15 12:48:04.405Z | 272.397° WNW | 43.399° | 2025-09-15 12:55:04.405Z | 355.955° N |
6 mins | 2025-09-15 22:24:04.405Z | 46.507° ENE | 2025-09-15 22:27:04.405Z | 73.222° E | 15.16° | 2025-09-15 22:30:04.405Z | 99.614° ESE |
13 mins | 2025-09-16 00:12:04.405Z | 358.536° N | 2025-09-16 00:18:04.405Z | 209.435° SW | 44.825° | 2025-09-16 00:25:04.405Z | 183.073° SSW |
5 mins | 2025-09-16 02:04:04.405Z | 310.612° NW | 2025-09-16 02:06:04.405Z | 293.486° NW | 13.835° | 2025-09-16 02:09:04.405Z | 267.378° W |
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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