ONEWEB-0017, 45132
Orbit data source: Space-Track
ONEWEB-0017, 45132 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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45132 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, 2.5 m
Radar Cross Section
2.957 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ONEWEB-0017
1 45132U 20008B 25260.93792829 -.00000620 00000-0 -18132-2 0 9996
2 45132 87.8736 90.5665 0001497 93.7690 266.3608 13.10371001272292Epoch: 2025-09-17T22:30Z
TLE epoch observation values (Epoch: 2025-09-17T22:30:37.004Z)
Latitude
-0.00006°
Longitude
115.80561°
Altitude
1,224.684 km
Speed
7.242 km/s
True Right ascension
06h 02m 15s
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
21:12:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,219.981 km
Perigee altitude
1,217.707 km
Semi-major axis
7,596.981 km
Eccentricity
0.00015
Inclination
87.8736°
RAAN
90.5665°
Arg. of periapsis
93.769°
True anomaly
266.34368°
Mean anomaly
266.3608°
Eccentric anomaly
266.35224°
Mean motion
3.27779 °/min
Orbital period
109.83 mins
BSTAR
-0.0018132
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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-0017 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-18 11:30:19.667Z | 99.675° ESE | 2025-09-18 11:33:19.667Z | 73.26° E | 15.644° | 2025-09-18 11:37:19.667Z | 38.981° NE |
| 13 mins | 2025-09-18 13:16:19.667Z | 181.278° SSW | 2025-09-18 13:22:19.667Z | 247.81° W | 44.888° | 2025-09-18 13:29:19.667Z | 359.504° N |
| 5 mins | 2025-09-18 15:11:19.667Z | 270.39° WNW | 2025-09-18 15:13:19.667Z | 287.659° WNW | 13.504° | 2025-09-18 15:16:19.667Z | 313.16° NW |
| 4 mins | 2025-09-18 23:00:19.667Z | 59.642° ENE | 2025-09-18 23:01:19.667Z | 68.098° E | 12.162° | 2025-09-18 23:04:19.667Z | 92.732° ESE |
| 12 mins | 2025-09-19 00:47:19.667Z | 3.724° NNE | 2025-09-19 00:52:19.667Z | 53.464° ENE | 44.208° | 2025-09-19 00:59:19.667Z | 175.528° S |
| 7 mins | 2025-09-19 02:38:19.667Z | 318.328° NNW | 2025-09-19 02:41:19.667Z | 291.572° WNW | 17.03° | 2025-09-19 02:45:19.667Z | 255.09° W |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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