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: 7 hours ago
TLE from 7 hours ago
0 ONEWEB-0067
1 45425U 20020B 25256.91353727 -.00000509 00000-0 -14723-2 0 9996
2 45425 87.8765 76.0055 0001766 83.7921 276.3408 13.11417732266527
TLE epoch observation values (Epoch: 2025-09-13T21:55:29.62Z)
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 | 2025-09-14 10:53:01.073Z | 112.495° ESE | 2025-09-14 10:58:01.073Z | 68.85° E | 17.337° | 2025-09-14 11:02:01.073Z | 34.777° NE |
12 mins | 2025-09-14 12:41:01.073Z | 186.391° SSW | 2025-09-14 12:47:01.073Z | 305.929° NW | 44.005° | 2025-09-14 12:53:01.073Z | 357.047° N |
5 mins | 2025-09-14 22:23:01.073Z | 50.686° ENE | 2025-09-14 22:25:01.073Z | 67.891° E | 13.596° | 2025-09-14 22:28:01.073Z | 93.787° ESE |
13 mins | 2025-09-15 00:10:01.073Z | 0.584° NNE | 2025-09-15 00:16:01.073Z | 31.599° NE | 44.753° | 2025-09-15 00:23:01.073Z | 179.402° S |
6 mins | 2025-09-15 02:03:01.073Z | 308.026° NW | 2025-09-15 02:05:01.073Z | 289.805° WNW | 15.43° | 2025-09-15 02:09:01.073Z | 255.514° 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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