ONEWEB-0028, 45140
Orbit data source: Space-Track
ONEWEB-0028, 45140 is a payload satellite owned by One Web (UK) in LEO that was launched on Thu, 06 Feb 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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45140 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: 17 hours ago
TLE from 17 hours ago
0 ONEWEB-0028
1 45140U 20008K 26271.97290159 -.00000527 00000-0 -15218-2 0 9999
2 45140 87.8962 0.4437 0002352 97.2455 262.8940 13.11416431322225Epoch: 2026-09-28T23:20Z
TLE epoch observation values (Epoch: 2026-09-28T23:20:58.697Z)
Latitude
-0.00005°
Longitude
2.45454°
Altitude
1,220.795 km
Speed
7.244 km/s
True Right ascension
00h 01m 46s
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
10:18:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.589 km
Perigee altitude
1,213.017 km
Semi-major axis
7,592.94 km
Eccentricity
0.00024
Inclination
87.8962°
RAAN
0.4437°
Arg. of periapsis
97.2455°
True anomaly
262.86726°
Mean anomaly
262.894°
Eccentric anomaly
262.88063°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0015218
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Other satellites on launch #8 in the year 2020 (2020-02-06 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-0028 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 | 2026-09-29 18:15:48.963Z | 358.807° N | 2026-09-29 18:22:48.963Z | 194.696° SSW | 80.673° | 2026-09-29 18:28:48.963Z | 182.734° SSW |
| 5 mins | 2026-09-29 20:08:48.963Z | 309.277° NW | 2026-09-29 20:10:48.963Z | 291.913° WNW | 14.557° | 2026-09-29 20:13:48.963Z | 265.895° W |
| 7 mins | 2026-09-30 04:48:48.963Z | 101.127° ESE | 2026-09-30 04:51:48.963Z | 73.617° E | 17.787° | 2026-09-30 04:55:48.963Z | 38.295° NE |
| 13 mins | 2026-09-30 06:34:48.963Z | 184.608° SSW | 2026-09-30 06:40:48.963Z | 266.153° W | 79.598° | 2026-09-30 06:47:48.963Z | 358.066° N |
| 4 mins | 2026-09-30 08:30:48.963Z | 280.44° WNW | 2026-09-30 08:31:48.963Z | 288.953° WNW | 12.61° | 2026-09-30 08:34:48.963Z | 313.562° NW |
| 5 mins | 2026-09-30 16:17:48.963Z | 54.894° ENE | 2026-09-30 16:19:48.963Z | 72.203° E | 13.572° | 2026-09-30 16:22:48.963Z | 97.095° ESE |
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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