ONEWEB-0082, 45452
Orbit data source: Space-Track
ONEWEB-0082, 45452 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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45452 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-0082
1 45452U 20020AE 25258.51222082 -.00000422 00000-0 -12270-2 0 9992
2 45452 87.8786 75.7509 0001525 86.2514 273.8788 13.11414669266674
TLE epoch observation values (Epoch: 2025-09-15T12:17:35.878Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #20 in the year 2020 (2020-03-21 UTC)
ONEWEB-0082 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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4 mins | 2025-09-16 10:27:28.929Z | 85.896° E | 2025-09-16 10:29:28.929Z | 69.099° E | 12.298° | 2025-09-16 10:31:28.929Z | 52.392° ENE |
12 mins | 2025-09-16 12:12:28.929Z | 172.016° S | 2025-09-16 12:18:28.929Z | 48.049° ENE | 44.17° | 2025-09-16 12:24:28.929Z | 3.585° NNE |
7 mins | 2025-09-16 14:05:28.929Z | 256.576° W | 2025-09-16 14:08:28.929Z | 283.956° WNW | 16.879° | 2025-09-16 14:12:28.929Z | 320.185° NNW |
13 mins | 2025-09-16 23:41:28.929Z | 7.311° NNE | 2025-09-16 23:47:28.929Z | 75.531° E | 41.894° | 2025-09-16 23:54:28.929Z | 167.2° S |
8 mins | 2025-09-17 01:33:28.929Z | 319.871° NNW | 2025-09-17 01:36:28.929Z | 290.362° WNW | 20.881° | 2025-09-17 01:41:28.929Z | 242.371° 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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