ONEWEB-0008, 44059
Orbit data source: Space-Track
ONEWEB-0008, 44059 is a payload satellite owned by One Web (UK) in LEO that was launched on Wed, 27 Feb 2019 UTC via a SOYUZ-ST-B launch vehicle from the French Guiana (FRGUI). 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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44059 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
Airbus/Toulouse
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: 7 hours ago
TLE from 7 hours ago
0 ONEWEB-0008
1 44059U 19010C 26128.25344588 .00000001 00000-0 -29927-4 0 9996
2 44059 87.9095 236.7056 0001869 109.1749 250.9585 13.16593489346473Epoch: 2026-05-08T06:04Z
TLE epoch observation values (Epoch: 2026-05-08T06:04:57.724Z)
Latitude
0.00007°
Longitude
-80.6228°
Altitude
1,201.119 km
Speed
7.253 km/s
True Right ascension
15h 46m 49s
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
21:35:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,196.285 km
Perigee altitude
1,193.455 km
Semi-major axis
7,573.007 km
Eccentricity
0.00019
Inclination
87.9095°
RAAN
236.7056°
Arg. of periapsis
109.1749°
True anomaly
250.93826°
Mean anomaly
250.9585°
Eccentric anomaly
250.94838°
Mean motion
3.29337 °/min
Orbital period
109.31 mins
BSTAR
-0.000029927
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Other satellites on launch #10 in the year 2019 (2019-02-27 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-0008 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 | 2026-05-08 17:39:20.530Z | 39.879° NE | 2026-05-08 17:43:20.530Z | 74.071° E | 14.341° | 2026-05-08 17:46:20.530Z | 99.995° ESE |
| 13 mins | 2026-05-08 19:27:20.530Z | 359.401° N | 2026-05-08 19:33:20.530Z | 356.574° N | 44.925° | 2026-05-08 19:40:20.530Z | 181.7° SSW |
| 6 mins | 2026-05-08 21:19:20.530Z | 311.436° NW | 2026-05-08 21:22:20.530Z | 284.743° WNW | 14.24° | 2026-05-08 21:25:20.530Z | 259.459° W |
| 6 mins | 2026-05-09 05:58:20.530Z | 93.947° ESE | 2026-05-09 06:00:20.530Z | 75.669° E | 15.476° | 2026-05-09 06:04:20.530Z | 40.426° NE |
| 13 mins | 2026-05-09 07:43:20.530Z | 181.641° SSW | 2026-05-09 07:49:20.530Z | 304.35° NW | 44.825° | 2026-05-09 07:56:20.530Z | 359.509° N |
| 4 mins | 2026-05-09 09:38:20.530Z | 276.959° WNW | 2026-05-09 09:39:20.530Z | 285.779° WNW | 13.147° | 2026-05-09 09:42:20.530Z | 311.645° 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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