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: 2 days ago
TLE from 2 days ago
0 ONEWEB-0082
1 45452U 20020AE 26171.30862808 -.00000406 00000-0 -11803-2 0 9993
2 45452 87.8893 20.4382 0001746 70.2787 289.8529 13.11419592303086Epoch: 2026-06-20T07:24Z
TLE epoch observation values (Epoch: 2026-06-20T07:24:25.466Z)
Latitude
-0.00002°
Longitude
0.80698°
Altitude
1,220.111 km
Speed
7.245 km/s
True Right ascension
01h 21m 45s
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
21:39:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.116 km
Perigee altitude
1,213.465 km
Semi-major axis
7,592.928 km
Eccentricity
0.00017
Inclination
87.8893°
RAAN
20.4382°
Arg. of periapsis
70.2787°
True anomaly
289.83408°
Mean anomaly
289.8529°
Eccentric anomaly
289.84349°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
-0.0011803
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 12:39:33.893Z | 108.269° ESE | 2026-06-22 12:43:33.893Z | 73.499° E | 16.795° | 2026-06-22 12:47:33.893Z | 38.271° NE |
| 13 mins | 2026-06-22 14:26:33.893Z | 184.312° SSW | 2026-06-22 14:32:33.893Z | 267.128° W | 44.572° | 2026-06-22 14:39:33.893Z | 358.234° N |
| 4 mins | 2026-06-22 16:22:33.893Z | 280.498° WNW | 2026-06-22 16:23:33.893Z | 289.055° WNW | 12.368° | 2026-06-22 16:26:33.893Z | 313.75° NW |
| 5 mins | 2026-06-23 00:09:33.893Z | 55.378° ENE | 2026-06-23 00:11:33.893Z | 72.685° E | 13.047° | 2026-06-23 00:14:33.893Z | 97.432° ESE |
| 13 mins | 2026-06-23 01:56:33.893Z | 1.793° NNE | 2026-06-23 02:02:33.893Z | 124.236° SE | 44.716° | 2026-06-23 02:09:33.893Z | 178.246° S |
| 6 mins | 2026-06-23 03:48:33.893Z | 312.206° NW | 2026-06-23 03:51:33.893Z | 284.625° WNW | 16.021° | 2026-06-23 03:54:33.893Z | 258.245° W |
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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