ONEWEB-0107, 48048
Orbit data source: Space-Track
ONEWEB-0107, 48048 is a payload satellite owned by One Web (NAA) (UK) in LEO that was launched on Thu, 25 Mar 2021 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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48048 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-0107
1 48048U 21025G 26171.45643170 -.00000043 00000-0 -15349-3 0 9995
2 48048 87.8965 319.5596 0002040 102.1588 257.9770 13.13470725253952Epoch: 2026-06-20T10:57Z
TLE epoch observation values (Epoch: 2026-06-20T10:57:15.698Z)
Latitude
-0.00002°
Longitude
-113.4266°
Altitude
1,212.978 km
Speed
7.248 km/s
True Right ascension
21h 18m 14s
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
21:27:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,208.425 km
Perigee altitude
1,205.33 km
Semi-major axis
7,585.015 km
Eccentricity
0.0002
Inclination
87.8965°
RAAN
319.5596°
Arg. of periapsis
102.1588°
True anomaly
257.95414°
Mean anomaly
257.977°
Eccentric anomaly
257.96557°
Mean motion
3.28555 °/min
Orbital period
109.57 mins
BSTAR
-0.00015349
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Other satellites on launch #25 in the year 2021 (2021-03-25 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-0107 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 | 2026-06-22 10:34:46.879Z | 190.986° SSW | 2026-06-22 10:41:46.879Z | 285.877° WNW | 42.53° | 2026-06-22 10:47:46.879Z | 353.663° N |
| 7 mins | 2026-06-22 20:16:46.879Z | 47.553° ENE | 2026-06-22 20:19:46.879Z | 75.024° E | 15.682° | 2026-06-22 20:23:46.879Z | 108.977° ESE |
| 12 mins | 2026-06-22 22:04:46.879Z | 357.501° N | 2026-06-22 22:09:46.879Z | 323.624° NNW | 44.608° | 2026-06-22 22:16:46.879Z | 184.618° SSW |
| 5 mins | 2026-06-22 23:56:46.879Z | 306.105° NW | 2026-06-22 23:58:46.879Z | 288.727° WNW | 13.238° | 2026-06-23 00:01:46.879Z | 263.736° W |
| 7 mins | 2026-06-23 08:35:46.879Z | 100.728° ESE | 2026-06-23 08:38:46.879Z | 72.387° E | 17.367° | 2026-06-23 08:42:46.879Z | 36.989° NE |
| 4 mins | 2026-06-23 10:21:46.879Z | 186.207° SSW | 2026-06-23 10:25:46.879Z | 200.237° SSW | 39.462° | 2026-06-23 10:25:46.879Z | 200.237° SSW |
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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