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: 9 hours ago
TLE from 9 hours ago
0 ONEWEB-0028
1 45140U 20008K 26035.05376200 -.00000549 00000-0 -15862-2 0 9997
2 45140 87.8811 47.5668 0001897 71.3095 288.8239 13.11416175291175Epoch: 2026-02-04T01:17Z
TLE epoch observation values (Epoch: 2026-02-04T01:17:25.036Z)
Latitude
-0.00001°
Longitude
-106.01338°
Altitude
1,220.11 km
Speed
7.245 km/s
True Right ascension
03h 10m 16s
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
11:46:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.244 km
Perigee altitude
1,213.364 km
Semi-major axis
7,592.941 km
Eccentricity
0.00019
Inclination
87.8811°
RAAN
47.5668°
Arg. of periapsis
71.3095°
True anomaly
288.80332°
Mean anomaly
288.8239°
Eccentric anomaly
288.81361°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0015862
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-04 11:05:14.625Z | 45.037° ENE | 2026-02-04 11:08:14.625Z | 70.061° E | 13.172° | 2026-02-04 11:11:14.625Z | 95.297° ESE |
| 13 mins | 2026-02-04 12:53:14.625Z | 1.389° NNE | 2026-02-04 12:59:14.625Z | 76.045° E | 44.827° | 2026-02-04 13:06:14.625Z | 178.364° S |
| 7 mins | 2026-02-04 14:45:14.625Z | 314.508° NW | 2026-02-04 14:48:14.625Z | 287.512° WNW | 15.937° | 2026-02-04 14:52:14.625Z | 253.356° W |
| 6 mins | 2026-02-04 23:26:14.625Z | 96.078° ESE | 2026-02-04 23:29:14.625Z | 69.456° E | 14.982° | 2026-02-04 23:32:14.625Z | 43.609° NE |
| 12 mins | 2026-02-05 01:12:14.625Z | 179.849° S | 2026-02-05 01:18:14.625Z | 345.799° N | 44.7° | 2026-02-05 01:24:14.625Z | 0.005° NNE |
| 6 mins | 2026-02-05 03:06:14.625Z | 266.549° W | 2026-02-05 03:09:14.625Z | 292.886° NW | 13.973° | 2026-02-05 03:12:14.625Z | 317.892° NNW |
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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