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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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 ONEWEB-0028
1 45140U 20008K 25336.26965110 -.00000526 00000-0 -15189-2 0 9994
2 45140 87.8862 60.2932 0002044 120.3240 239.8090 13.11417697282811Epoch: 2025-12-02T06:28Z
TLE epoch observation values (Epoch: 2025-12-02T06:28:17.855Z)
Latitude
-0.00003°
Longitude
-108.13842°
Altitude
1,221.35 km
Speed
7.243 km/s
True Right ascension
04h 01m 10s
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
15:47:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.35 km
Perigee altitude
1,213.246 km
Semi-major axis
7,592.935 km
Eccentricity
0.0002
Inclination
87.8862°
RAAN
60.2932°
Arg. of periapsis
120.324°
True anomaly
239.78876°
Mean anomaly
239.809°
Eccentric anomaly
239.79888°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0015189
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-12-02 18:03:31.512Z | 358.305° N | 2025-12-02 18:10:31.512Z | 212.043° SW | 44.734° | 2025-12-02 18:17:31.512Z | 183.568° SSW |
| 5 mins | 2025-12-02 19:56:31.512Z | 310.075° NW | 2025-12-02 19:58:31.512Z | 292.974° NW | 13.633° | 2025-12-02 20:01:31.512Z | 267.1° W |
| 7 mins | 2025-12-03 04:36:31.512Z | 102.812° ESE | 2025-12-03 04:39:31.512Z | 75.285° E | 17.316° | 2025-12-03 04:43:31.512Z | 39.149° NE |
| 13 mins | 2025-12-03 06:22:31.512Z | 185.435° SSW | 2025-12-03 06:28:31.512Z | 251.773° W | 44.285° | 2025-12-03 06:35:31.512Z | 357.509° N |
| 5 mins | 2025-12-03 16:05:31.512Z | 53.708° ENE | 2025-12-03 16:07:31.512Z | 71.148° E | 13.532° | 2025-12-03 16:10:31.512Z | 96.534° ESE |
| 8 mins | 2025-12-03 17:52:31.512Z | 0.923° NNE | 2025-12-03 17:58:31.512Z | 102.898° ESE | 44.912° | 2025-12-03 18:00:31.512Z | 174.375° S |
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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