ONEWEB-0090, 45427
Orbit data source: Space-Track
ONEWEB-0090, 45427 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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45427 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: 8 hours ago
TLE from 8 hours ago
0 ONEWEB-0090
1 45427U 20020D 26305.08936110 -.00000513 00000-0 -14821-2 0 9999
2 45427 87.8922 353.8841 0001808 95.4067 264.7267 13.11416309320615Epoch: 2026-11-01T02:08Z
TLE epoch observation values (Epoch: 2026-11-01T02:08:40.799Z)
Latitude
-0.00002°
Longitude
-78.67163°
Altitude
1,220.701 km
Speed
7.244 km/s
True Right ascension
23h 35m 32s
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
05:25:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.176 km
Perigee altitude
1,213.431 km
Semi-major axis
7,592.94 km
Eccentricity
0.00018
Inclination
87.8922°
RAAN
353.8841°
Arg. of periapsis
95.4067°
True anomaly
264.70607°
Mean anomaly
264.7267°
Eccentric anomaly
264.71638°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0014821
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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-0090 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-01 13:46:05.521Z | 42.683° NE | 2026-11-01 13:49:05.521Z | 67.338° ENE | 13.771° | 2026-11-01 13:52:05.521Z | 93.066° ESE |
| 13 mins | 2026-11-01 15:34:05.521Z | 0.925° NNE | 2026-11-01 15:40:05.521Z | 33.355° NE | 80.759° | 2026-11-01 15:47:05.521Z | 178.759° S |
| 6 mins | 2026-11-01 17:27:05.521Z | 308.707° NW | 2026-11-01 17:29:05.521Z | 290.448° WNW | 16.38° | 2026-11-01 17:33:05.521Z | 255.735° W |
| 7 mins | 2026-11-02 02:07:05.521Z | 98.271° ESE | 2026-11-02 02:10:05.521Z | 71.897° E | 15.886° | 2026-11-02 02:14:05.521Z | 38.238° NE |
| 13 mins | 2026-11-02 03:53:05.521Z | 180.387° SSW | 2026-11-02 03:59:05.521Z | 312.017° NW | 85.869° | 2026-11-02 04:06:05.521Z | 359.979° N |
| 5 mins | 2026-11-02 05:48:05.521Z | 272.825° WNW | 2026-11-02 05:50:05.521Z | 290.509° WNW | 14.299° | 2026-11-02 05:53:05.521Z | 315.779° NNW |
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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