ONEWEB-0006, 44061
Orbit data source: Space-Track
ONEWEB-0006, 44061 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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44061 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: 16 hours ago
TLE from 16 hours ago
0 ONEWEB-0006
1 44061U 19010E 25312.70070104 -.00000104 00000-0 -30954-3 0 9999
2 44061 87.8965 303.1719 0002084 93.4612 266.6757 13.15548679322435Epoch: 2025-11-08T16:49Z
TLE epoch observation values (Epoch: 2025-11-08T16:49:00.569Z)
Latitude
-0.00001°
Longitude
2.79298°
Altitude
1,204.757 km
Speed
7.252 km/s
True Right ascension
20h 12m 41s
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
05:10:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,200.461 km
Perigee altitude
1,197.303 km
Semi-major axis
7,577.019 km
Eccentricity
0.00021
Inclination
87.8965°
RAAN
303.1719°
Arg. of periapsis
93.4612°
True anomaly
266.65186°
Mean anomaly
266.6757°
Eccentric anomaly
266.66378°
Mean motion
3.29076 °/min
Orbital period
109.4 mins
BSTAR
-0.00030954
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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-0006 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 | 2025-11-09 09:52:58.188Z | 43.839° NE | 2025-11-09 09:55:58.188Z | 69.128° E | 13.518° | 2025-11-09 09:58:58.188Z | 95.067° ESE |
| 13 mins | 2025-11-09 11:40:58.188Z | 0.761° NNE | 2025-11-09 11:46:58.188Z | 134.059° SE | 44.883° | 2025-11-09 11:53:58.188Z | 179.724° S |
| 6 mins | 2025-11-09 13:32:58.188Z | 309.542° NW | 2025-11-09 13:34:58.188Z | 291.435° WNW | 15.184° | 2025-11-09 13:38:58.188Z | 256.593° W |
| 6 mins | 2025-11-09 22:11:58.188Z | 94.401° ESE | 2025-11-09 22:14:58.188Z | 67.358° ENE | 14.732° | 2025-11-09 22:17:58.188Z | 41.865° NE |
| 13 mins | 2025-11-09 23:56:58.188Z | 179.588° S | 2025-11-10 00:02:58.188Z | 244.915° WSW | 44.983° | 2025-11-10 00:09:58.188Z | 0.245° NNE |
| 6 mins | 2025-11-10 01:50:58.188Z | 265.679° W | 2025-11-10 01:53:58.188Z | 292.117° WNW | 13.892° | 2025-11-10 01:56:58.188Z | 317.408° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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