ONEWEB-0060, 45455
Orbit data source: Space-Track
ONEWEB-0060, 45455 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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45455 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: 12 hours ago
TLE from 12 hours ago
0 ONEWEB-0060
1 45455U 20020AH 26126.74382520 -.00000316 00000-0 -92828-3 0 9999
2 45455 87.8919 29.3080 0002792 72.7960 287.3473 13.11416007297118Epoch: 2026-05-06T17:51Z
TLE epoch observation values (Epoch: 2026-05-06T17:51:06.497Z)
Latitude
-0.00005°
Longitude
-103.069°
Altitude
1,219.944 km
Speed
7.245 km/s
True Right ascension
01h 57m 13s
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
13:34:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.924 km
Perigee altitude
1,212.685 km
Semi-major axis
7,592.942 km
Eccentricity
0.00028
Inclination
87.8919°
RAAN
29.308°
Arg. of periapsis
72.796°
True anomaly
287.31676°
Mean anomaly
287.3473°
Eccentric anomaly
287.33203°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.00092828
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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-0060 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-07 05:34:30.935Z | 145.12° SSE | 2026-05-07 05:34:30.935Z | 145.12° SSE | 39.728° | 2026-05-07 05:39:30.935Z | 170.526° S |
| 8 mins | 2026-05-07 07:18:30.935Z | 320.007° NNW | 2026-05-07 07:22:30.935Z | 281.311° WNW | 19.188° | 2026-05-07 07:26:30.935Z | 245.704° WSW |
| 4 mins | 2026-05-07 16:01:30.935Z | 81.498° E | 2026-05-07 16:02:30.935Z | 73.128° E | 11.944° | 2026-05-07 16:05:30.935Z | 48.445° ENE |
| 13 mins | 2026-05-07 17:45:30.935Z | 171.592° S | 2026-05-07 17:51:30.935Z | 91.418° ESE | 44.373° | 2026-05-07 17:58:30.935Z | 3.646° NNE |
| 7 mins | 2026-05-07 19:39:30.935Z | 260.578° W | 2026-05-07 19:42:30.935Z | 289.24° WNW | 17.177° | 2026-05-07 19:46:30.935Z | 324.181° NNW |
| 12 mins | 2026-05-08 05:15:30.935Z | 9.043° NNE | 2026-05-08 05:21:30.935Z | 97.637° ESE | 41.584° | 2026-05-08 05:27:30.935Z | 165.508° 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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