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: 18 hours ago
TLE from 18 hours ago
0 ONEWEB-0028
1 45140U 20008K 25287.13454033 .00000372 00000-0 10129-2 0 9998
2 45140 87.8812 70.0852 0001126 80.9611 279.1644 13.11414175276373Epoch: 2025-10-14T03:13Z
TLE epoch observation values (Epoch: 2025-10-14T03:13:44.284Z)
Latitude
-0.00006°
Longitude
-1.27664°
Altitude
1,220.446 km
Speed
7.244 km/s
True Right ascension
04h 40m 20s
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
15:47:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.667 km
Perigee altitude
1,213.957 km
Semi-major axis
7,592.949 km
Eccentricity
0.00011
Inclination
87.8812°
RAAN
70.0852°
Arg. of periapsis
80.9611°
True anomaly
279.15166°
Mean anomaly
279.1644°
Eccentric anomaly
279.15803°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
0.0010129
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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 | 2025-10-14 22:08:12.440Z | 354.296° N | 2025-10-14 22:15:12.440Z | 265.914° W | 43.276° | 2025-10-14 22:22:12.440Z | 191.673° SSW |
| 9 mins | 2025-10-15 08:40:12.440Z | 116.192° SE | 2025-10-15 08:44:12.440Z | 78.041° E | 21.254° | 2025-10-15 08:49:12.440Z | 31.097° NE |
| 12 mins | 2025-10-15 10:28:12.440Z | 196.224° SSW | 2025-10-15 10:33:12.440Z | 254.543° W | 41.445° | 2025-10-15 10:40:12.440Z | 352.954° N |
| 8 mins | 2025-10-15 20:09:12.440Z | 41.65° NE | 2025-10-15 20:12:12.440Z | 68.708° E | 17.07° | 2025-10-15 20:17:12.440Z | 112.863° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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