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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Identifier
Orbit
Country
UKRelated business
Manufacturer
One Web
Mission
Operational Commercial Communications
Bus & Motor
ARROW, Unknown motor
Mass
148 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 6.7 m
Radar Cross Section
3.464 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ONEWEB-0082
1 45452U 20020AE 26281.25227883 -.00000554 00000-0 -15983-2 0 9994
2 45452 87.8973 358.6011 0002149 91.0476 269.0898 13.11418608317490Epoch: 2026-10-08T06:03Z
TLE epoch observation values (Epoch: 2026-10-08T06:03:16.890Z)
Latitude
-0.00006°
Longitude
-109.11006°
Altitude
1,220.592 km
Speed
7.244 km/s
True Right ascension
23h 54m 24s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:11:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.426 km
Perigee altitude
1,213.163 km
Semi-major axis
7,592.931 km
Eccentricity
0.00021
Inclination
87.8973°
RAAN
358.6011°
Arg. of periapsis
91.0476°
True anomaly
269.06518°
Mean anomaly
269.0898°
Eccentric anomaly
269.07749°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
-0.0015983
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Other satellites on launch #20 in the year 2020 (2020-03-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-09 15:39:20.701Z | 43.806° NE | 2026-10-09 15:42:20.701Z | 69.479° E | 15.07° | 2026-10-09 15:46:20.701Z | 103.449° ESE |
| 13 mins | 2026-10-09 17:27:20.701Z | 359.444° N | 2026-10-09 17:33:20.701Z | 356.253° N | 87.302° | 2026-10-09 17:40:20.701Z | 181.667° SSW |
| 5 mins | 2026-10-09 19:20:20.701Z | 306.006° NW | 2026-10-09 19:22:20.701Z | 288.077° WNW | 15.076° | 2026-10-09 19:25:20.701Z | 262.317° W |
| 7 mins | 2026-10-10 04:00:20.701Z | 97.328° ESE | 2026-10-10 04:03:20.701Z | 69.457° E | 17.218° | 2026-10-10 04:07:20.701Z | 35.773° NE |
| 13 mins | 2026-10-10 05:46:20.701Z | 183.798° SSW | 2026-10-10 05:52:20.701Z | 313.24° NW | 78.632° | 2026-10-10 05:59:20.701Z | 358.862° N |
| 4 mins | 2026-10-10 07:41:20.701Z | 275.463° WNW | 2026-10-10 07:43:20.701Z | 292.617° NW | 13.026° | 2026-10-10 07:45:20.701Z | 309.348° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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