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: 10 hours ago
TLE from 10 hours ago
0 ONEWEB-0080
1 45426U 20020C 25260.89013346 -.00000379 00000-0 -11058-2 0 9992
2 45426 87.8783 75.3066 0001336 91.6108 268.5173 13.11413959267014
TLE epoch observation values (Epoch: 2025-09-17T21:21:47.53Z)
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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5 mins | 2025-09-18 10:21:31.733Z | 92.919° ESE | 2025-09-18 10:24:31.733Z | 67.38° ENE | 13.312° | 2025-09-18 10:26:31.733Z | 50.39° ENE |
12 mins | 2025-09-18 12:07:31.733Z | 175.032° S | 2025-09-18 12:12:31.733Z | 141.508° SSE | 44.62° | 2025-09-18 12:19:31.733Z | 2.145° NNE |
7 mins | 2025-09-18 14:00:31.733Z | 259.153° W | 2025-09-18 14:03:31.733Z | 285.896° WNW | 15.746° | 2025-09-18 14:07:31.733Z | 320.767° NNW |
13 mins | 2025-09-18 23:36:31.733Z | 6.229° NNE | 2025-09-18 23:42:31.733Z | 82.787° E | 42.948° | 2025-09-18 23:49:31.733Z | 170.08° S |
8 mins | 2025-09-19 01:28:31.733Z | 317.41° NNW | 2025-09-19 01:31:31.733Z | 288.068° WNW | 19.714° | 2025-09-19 01:36:31.733Z | 242.739° WSW |
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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