ONEWEB-0126, 47272
Orbit data source: Space-Track
ONEWEB-0126, 47272 is a payload satellite owned by One Web (UK) in LEO that was launched on Fri, 18 Dec 2020 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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47272 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: 9 hours ago
TLE from 9 hours ago
0 ONEWEB-0126
1 47272U 20100Q 26095.31234734 -.00000529 00000-0 -15064-2 0 9990
2 47272 87.9013 5.1451 0001789 73.9256 286.2069 13.12442863255149Epoch: 2026-04-05T07:29Z
TLE epoch observation values (Epoch: 2026-04-05T07:29:46.810Z)
Latitude
-0.00005°
Longitude
59.08048°
Altitude
1,216.236 km
Speed
7.246 km/s
True Right ascension
00h 20m 34s
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
22:47:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,212.198 km
Perigee altitude
1,209.483 km
Semi-major axis
7,588.977 km
Eccentricity
0.00018
Inclination
87.9013°
RAAN
5.1451°
Arg. of periapsis
73.9256°
True anomaly
286.18721°
Mean anomaly
286.2069°
Eccentric anomaly
286.19706°
Mean motion
3.28298 °/min
Orbital period
109.66 mins
BSTAR
-0.0015064
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Other satellites on launch #100 in the year 2020 (2020-12-18 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-0126 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-05 16:51:47.328Z | 72.312° E | 2026-04-05 16:51:47.328Z | 72.312° E | 17.022° | 2026-04-05 16:55:47.328Z | 37.231° NE |
| 13 mins | 2026-04-05 18:34:47.328Z | 185.148° SSW | 2026-04-05 18:40:47.328Z | 288.58° WNW | 44.418° | 2026-04-05 18:47:47.328Z | 358.127° N |
| 5 mins | 2026-04-06 04:16:47.328Z | 52.491° ENE | 2026-04-06 04:18:47.328Z | 69.65° E | 13.095° | 2026-04-06 04:21:47.328Z | 94.953° ESE |
| 13 mins | 2026-04-06 06:03:47.328Z | 1.491° NNE | 2026-04-06 06:09:47.328Z | 83.644° E | 44.824° | 2026-04-06 06:16:47.328Z | 178.322° S |
| 7 mins | 2026-04-06 07:55:47.328Z | 313.581° NW | 2026-04-06 07:58:47.328Z | 286.298° WNW | 15.931° | 2026-04-06 08:02:47.328Z | 252.432° W |
| 6 mins | 2026-04-06 16:36:47.328Z | 91.681° ESE | 2026-04-06 16:38:47.328Z | 73.821° E | 14.786° | 2026-04-06 16:42:47.328Z | 39.831° NE |
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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