ONEWEB-0010, 44058
Orbit data source: Space-Track
ONEWEB-0010, 44058 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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44058 intel report (Beta)
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Edit Public Description
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: 14 hours ago
TLE from 14 hours ago
0 ONEWEB-0010
1 44058U 19010B 26038.01971367 .00000039 00000-0 68055-4 0 9995
2 44058 87.9004 254.6904 0001389 101.7636 258.3651 13.16593928334485Epoch: 2026-02-07T00:28Z
TLE epoch observation values (Epoch: 2026-02-07T00:28:23.261Z)
Latitude
0.00002°
Longitude
110.44424°
Altitude
1,200.867 km
Speed
7.253 km/s
True Right ascension
16h 58m 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
16:22:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,195.92 km
Perigee altitude
1,193.817 km
Semi-major axis
7,573.005 km
Eccentricity
0.00014
Inclination
87.9004°
RAAN
254.6904°
Arg. of periapsis
101.7636°
True anomaly
258.34951°
Mean anomaly
258.3651°
Eccentric anomaly
258.35731°
Mean motion
3.29337 °/min
Orbital period
109.31 mins
BSTAR
0.000068055
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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-0010 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-02-07 15:09:39.030Z | 192.501° SSW | 2026-02-07 15:15:39.030Z | 256.777° W | 42.085° | 2026-02-07 15:22:39.030Z | 353.943° N |
| 7 mins | 2026-02-08 00:49:39.030Z | 45.408° ENE | 2026-02-08 00:52:39.030Z | 72.528° E | 15.524° | 2026-02-08 00:56:39.030Z | 107.245° ESE |
| 12 mins | 2026-02-08 02:37:39.030Z | 357.62° N | 2026-02-08 02:42:39.030Z | 324.971° NNW | 44.62° | 2026-02-08 02:49:39.030Z | 184.441° SSW |
| 4 mins | 2026-02-08 04:29:39.030Z | 304.022° NW | 2026-02-08 04:31:39.030Z | 286.39° WNW | 13.155° | 2026-02-08 04:33:39.030Z | 269.265° W |
| 6 mins | 2026-02-08 13:07:39.030Z | 96.23° ESE | 2026-02-08 13:09:39.030Z | 77.444° E | 16.613° | 2026-02-08 13:13:39.030Z | 40.84° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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