ONEWEB-0061, 45428
Orbit data source: Space-Track
ONEWEB-0061, 45428 is a payload satellite owned by One Web (UK) in LEO that was launched on Sat, 21 Mar 2020 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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45428 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: 20 hours ago
TLE from 20 hours ago
0 ONEWEB-0061
1 45428U 20020E 26186.09833107 -.00000457 00000-0 -13248-2 0 9999
2 45428 87.8888 17.4912 0001807 89.8131 270.3204 13.11416504304979Epoch: 2026-07-05T02:21Z
TLE epoch observation values (Epoch: 2026-07-05T02:21:35.804Z)
Latitude
-0.00002°
Longitude
58.98947°
Altitude
1,220.566 km
Speed
7.244 km/s
True Right ascension
01h 09m 57s
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
10:41:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.175 km
Perigee altitude
1,213.431 km
Semi-major axis
7,592.94 km
Eccentricity
0.00018
Inclination
87.8888°
RAAN
17.4912°
Arg. of periapsis
89.8131°
True anomaly
270.29969°
Mean anomaly
270.3204°
Eccentric anomaly
270.31005°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0013248
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Other satellites on launch #20 in the year 2020 (2020-03-21 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-0061 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 | 2026-07-05 23:09:10.081Z | 48.998° ENE | 2026-07-05 23:12:10.081Z | 74.865° E | 13.45° | 2026-07-05 23:15:10.081Z | 99.6° ESE |
| 12 mins | 2026-07-06 00:57:10.081Z | 1.226° NNE | 2026-07-06 01:03:10.081Z | 154.558° SSE | 44.521° | 2026-07-06 01:09:10.081Z | 179.012° S |
| 6 mins | 2026-07-06 02:49:10.081Z | 309.946° NW | 2026-07-06 02:51:10.081Z | 291.906° WNW | 15.511° | 2026-07-06 02:55:10.081Z | 256.936° W |
| 6 mins | 2026-07-06 11:30:10.081Z | 91.948° ESE | 2026-07-06 11:32:10.081Z | 73.795° E | 15.357° | 2026-07-06 11:36:10.081Z | 39.488° NE |
| 13 mins | 2026-07-06 13:15:10.081Z | 180.664° SSW | 2026-07-06 13:21:10.081Z | 249.981° W | 44.934° | 2026-07-06 13:28:10.081Z | 359.767° N |
| 5 mins | 2026-07-06 15:10:10.081Z | 271.197° WNW | 2026-07-06 15:12:10.081Z | 288.707° WNW | 13.694° | 2026-07-06 15:15:10.081Z | 314.224° 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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