ONEWEB-0067, 45425
Orbit data source: Space-Track
ONEWEB-0067, 45425 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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45425 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 ONEWEB-0067
1 45425U 20020B 25286.44038179 -.00000329 00000-0 -96273-3 0 9999
2 45425 87.8819 70.1053 0001458 91.3784 268.7511 13.11417930270390
TLE epoch observation values (Epoch: 2025-10-13T10:34:08.986Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #20 in the year 2020 (2020-03-21 UTC)
ONEWEB-0067 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 | 2025-10-14 08:41:02.626Z | 115.653° SE | 2025-10-14 08:45:02.626Z | 79.088° E | 20.197° | 2025-10-14 08:50:02.626Z | 32.492° NE |
12 mins | 2025-10-14 10:29:02.626Z | 193.59° SSW | 2025-10-14 10:35:02.626Z | 293.035° NW | 42.262° | 2025-10-14 10:41:02.626Z | 353.822° N |
6 mins | 2025-10-14 20:11:02.626Z | 49.521° ENE | 2025-10-14 20:14:02.626Z | 77.596° E | 16.151° | 2025-10-14 20:17:02.626Z | 104.049° ESE |
13 mins | 2025-10-14 21:58:02.626Z | 357.174° N | 2025-10-14 22:04:02.626Z | 307.492° NW | 44.603° | 2025-10-14 22:11:02.626Z | 185.629° SSW |
5 mins | 2025-10-14 23:51:02.626Z | 306.537° NW | 2025-10-14 23:53:02.626Z | 289.452° WNW | 12.904° | 2025-10-14 23:56:02.626Z | 264.74° 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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