ONEWEB-0036, 45144
Orbit data source: Space-Track
ONEWEB-0036, 45144 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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45144 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: 19 hours ago
TLE from 19 hours ago
0 ONEWEB-0036
1 45144U 20008P 25333.01692644 -.00000730 00000-0 -21289-2 0 9992
2 45144 87.8812 76.1468 0001603 114.5746 245.5549 13.10373712282154Epoch: 2025-11-29T00:24Z
TLE epoch observation values (Epoch: 2025-11-29T00:24:22.444Z)
Latitude
0.00003°
Longitude
1.90211°
Altitude
1,225.106 km
Speed
7.242 km/s
True Right ascension
05h 04m 35s
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
16:52:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.051 km
Perigee altitude
1,217.616 km
Semi-major axis
7,596.971 km
Eccentricity
0.00016
Inclination
87.8812°
RAAN
76.1468°
Arg. of periapsis
114.5746°
True anomaly
245.53818°
Mean anomaly
245.5549°
Eccentric anomaly
245.54654°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0021289
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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-0036 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-11-29 19:20:04.853Z | 357.746° N | 2025-11-29 19:27:04.853Z | 215.862° SW | 44.512° | 2025-11-29 19:33:04.853Z | 184.8° SSW |
| 4 mins | 2025-11-29 21:14:04.853Z | 301.497° NW | 2025-11-29 21:15:04.853Z | 292.799° NW | 13.262° | 2025-11-29 21:18:04.853Z | 267.335° W |
| 8 mins | 2025-11-30 05:53:04.853Z | 106.436° ESE | 2025-11-30 05:57:04.853Z | 69.142° E | 17.932° | 2025-11-30 06:01:04.853Z | 34.662° NE |
| 13 mins | 2025-11-30 07:40:04.853Z | 187.632° SSW | 2025-11-30 07:46:04.853Z | 293.921° NW | 43.906° | 2025-11-30 07:53:04.853Z | 357.382° N |
| 5 mins | 2025-11-30 17:23:04.853Z | 53.822° ENE | 2025-11-30 17:25:04.853Z | 71.613° E | 14.305° | 2025-11-30 17:28:04.853Z | 97.488° ESE |
| 7 mins | 2025-11-30 19:10:04.853Z | 359.83° N | 2025-11-30 19:16:04.853Z | 103.993° ESE | 44.995° | 2025-11-30 19:17:04.853Z | 177.835° 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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