ONEWEB-0067, 45425
Orbit data source: Space-Track
ONEWEB-0067, 45425 is a payload satellite owned by One Web (UK) in LEO that was launched on Sat, 21 Mar 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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45425 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: 1 day ago
TLE from 1 day ago
0 ONEWEB-0067
1 45425U 20020B 26095.85539814 -.00000597 00000-0 -17231-2 0 9998
2 45425 87.8929 35.3573 0001665 85.8667 274.2651 13.11258184293251Epoch: 2026-04-05T20:31Z
TLE epoch observation values (Epoch: 2026-04-05T20:31:46.399Z)
Latitude
-0.00002°
Longitude
-106.74086°
Altitude
1,221.091 km
Speed
7.244 km/s
True Right ascension
02h 21m 25s
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
04:16:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.679 km
Perigee altitude
1,214.15 km
Semi-major axis
7,593.551 km
Eccentricity
0.00017
Inclination
87.8929°
RAAN
35.3573°
Arg. of periapsis
85.8667°
True anomaly
274.24607°
Mean anomaly
274.2651°
Eccentric anomaly
274.25559°
Mean motion
3.28001 °/min
Orbital period
109.76 mins
BSTAR
-0.0017231
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Other satellites on launch #20 in the year 2020 (2020-03-21 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-0067 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 | 2026-04-06 22:20:05.831Z | 261.88° W | 2026-04-06 22:23:05.831Z | 286.679° WNW | 13.233° | 2026-04-06 22:26:05.831Z | 312.198° NW |
| 13 mins | 2026-04-07 07:56:05.831Z | 2.804° NNE | 2026-04-07 08:02:05.831Z | 77.415° E | 44.476° | 2026-04-07 08:09:05.831Z | 175.94° S |
| 7 mins | 2026-04-07 09:48:05.831Z | 315.61° NNW | 2026-04-07 09:51:05.831Z | 288.041° WNW | 17.011° | 2026-04-07 09:55:05.831Z | 252.591° W |
| 5 mins | 2026-04-07 18:30:05.831Z | 88.21° E | 2026-04-07 18:32:05.831Z | 70.554° E | 14.036° | 2026-04-07 18:35:05.831Z | 45.061° ENE |
| 13 mins | 2026-04-07 20:15:05.831Z | 177.093° S | 2026-04-07 20:21:05.831Z | 23.452° NE | 44.846° | 2026-04-07 20:28:05.831Z | 1.31° NNE |
| 6 mins | 2026-04-07 22:09:05.831Z | 264.68° W | 2026-04-07 22:12:05.831Z | 291.706° WNW | 14.977° | 2026-04-07 22:15:05.831Z | 317.462° 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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