ONEWEB-0400, 50480
Orbit data source: Space-Track
ONEWEB-0400, 50480 is a payload satellite owned by One Web (NAA) (UK) in LEO that was launched on Mon, 27 Dec 2021 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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50480 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-0400
1 50480U 21132M 26171.42319088 -.00000034 00000-0 -11925-3 0 9998
2 50480 87.9169 334.8007 0001947 99.0096 261.1256 13.18685183222034Epoch: 2026-06-20T10:09Z
TLE epoch observation values (Epoch: 2026-06-20T10:09:23.692Z)
Latitude
-0.00005°
Longitude
-86.18605°
Altitude
1,192.874 km
Speed
7.257 km/s
True Right ascension
22h 19m 12s
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
21:33:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,188.326 km
Perigee altitude
1,185.381 km
Semi-major axis
7,564.99 km
Eccentricity
0.00019
Inclination
87.9169°
RAAN
334.8007°
Arg. of periapsis
99.0096°
True anomaly
261.10356°
Mean anomaly
261.1256°
Eccentric anomaly
261.11458°
Mean motion
3.29861 °/min
Orbital period
109.14 mins
BSTAR
-0.00011925
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Other satellites on launch #132 in the year 2021 (2021-12-27 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-0400 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-06-22 11:24:29.485Z | 184.003° SSW | 2026-06-22 11:31:29.485Z | 262.934° W | 44.444° | 2026-06-22 11:38:29.485Z | 357.932° N |
| 4 mins | 2026-06-22 13:20:29.485Z | 276.849° WNW | 2026-06-22 13:22:29.485Z | 293.959° NW | 11.811° | 2026-06-22 13:24:29.485Z | 310.517° NW |
| 4 mins | 2026-06-22 21:05:29.485Z | 56.738° ENE | 2026-06-22 21:07:29.485Z | 73.903° E | 11.965° | 2026-06-22 21:09:29.485Z | 90.574° ESE |
| 13 mins | 2026-06-22 22:51:29.485Z | 2.744° NNE | 2026-06-22 22:57:29.485Z | 87.244° E | 44.519° | 2026-06-22 23:04:29.485Z | 176.278° S |
| 6 mins | 2026-06-23 00:43:29.485Z | 309.959° NW | 2026-06-23 00:45:29.485Z | 291.005° WNW | 16.576° | 2026-06-23 00:49:29.485Z | 254.468° W |
| 4 mins | 2026-06-23 09:22:29.485Z | 82.533° E | 2026-06-23 09:23:29.485Z | 73.789° E | 12.786° | 2026-06-23 09:26:29.485Z | 48.134° ENE |
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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