ONEWEB-0020, 45133
Orbit data source: Space-Track
ONEWEB-0020, 45133 is a payload satellite owned by One Web (UK) in LEO that was launched on Thu, 06 Feb 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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45133 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ONEWEB-0020
1 45133U 20008C 25292.13828157 -.00000547 00000-0 -16041-2 0 9993
2 45133 87.8763 84.3139 0001743 88.8102 271.3225 13.10369495276779
TLE epoch observation values (Epoch: 2025-10-19T03:19:07.527Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #8 in the year 2020 (2020-02-06 UTC)
ONEWEB-0020 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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13 mins | 2025-10-19 22:15:42.462Z | 5.264° NNE | 2025-10-19 22:21:42.462Z | 108.936° ESE | 43.652° | 2025-10-19 22:28:42.462Z | 173.274° S |
8 mins | 2025-10-20 00:06:42.462Z | 321.535° NNW | 2025-10-20 00:10:42.462Z | 284.578° WNW | 18.445° | 2025-10-20 00:14:42.462Z | 248.741° W |
4 mins | 2025-10-20 08:50:42.462Z | 79.357° E | 2025-10-20 08:51:42.462Z | 70.693° E | 12.895° | 2025-10-20 08:54:42.462Z | 45.881° ENE |
13 mins | 2025-10-20 10:34:42.462Z | 173.838° S | 2025-10-20 10:40:42.462Z | 64.683° ENE | 44.674° | 2025-10-20 10:47:42.462Z | 2.616° NNE |
7 mins | 2025-10-20 12:28:42.462Z | 262.371° W | 2025-10-20 12:31:42.462Z | 290.268° WNW | 16.273° | 2025-10-20 12:35:42.462Z | 324.242° NNW |
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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