ONEWEB-0049, 45154
Orbit data source: Space-Track
ONEWEB-0049, 45154 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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45154 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: 8 hours ago
TLE from 8 hours ago
0 ONEWEB-0049
1 45154U 20008Z 25259.25226355 -.00000575 00000-0 -16831-2 0 9992
2 45154 87.8732 90.9153 0002312 88.5470 271.5922 13.10370982272152Epoch: 2025-09-16T06:03Z
TLE epoch observation values (Epoch: 2025-09-16T06:03:15.57Z)
Latitude
-0.00005°
Longitude
4.65519°
Altitude
1,224.563 km
Speed
7.242 km/s
True Right ascension
06h 03m 39s
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
06:48:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.601 km
Perigee altitude
1,217.088 km
Semi-major axis
7,596.981 km
Eccentricity
0.00023
Inclination
87.8732°
RAAN
90.9153°
Arg. of periapsis
88.547°
True anomaly
271.56572°
Mean anomaly
271.5922°
Eccentric anomaly
271.57896°
Mean motion
3.27779 °/min
Orbital period
109.83 mins
BSTAR
-0.0016831
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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-0049 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 | 2025-09-16 15:23:18.045Z | 264.381° W | 2025-09-16 15:26:18.045Z | 289.023° WNW | 12.663° | 2025-09-16 15:29:18.045Z | 313.844° NW |
| 5 mins | 2025-09-16 23:12:18.045Z | 52.386° ENE | 2025-09-16 23:14:18.045Z | 69.412° E | 12.993° | 2025-09-16 23:17:18.045Z | 94.537° ESE |
| 13 mins | 2025-09-17 00:59:18.045Z | 1.564° NNE | 2025-09-17 01:05:18.045Z | 55.559° ENE | 44.682° | 2025-09-17 01:12:18.045Z | 177.756° S |
| 7 mins | 2025-09-17 02:51:18.045Z | 316.541° NNW | 2025-09-17 02:54:18.045Z | 289.934° WNW | 16.168° | 2025-09-17 02:58:18.045Z | 254.892° W |
| 6 mins | 2025-09-17 11:33:18.045Z | 93.328° ESE | 2025-09-17 11:35:18.045Z | 75.688° E | 14.887° | 2025-09-17 11:39:18.045Z | 41.272° NE |
| 13 mins | 2025-09-17 13:18:18.045Z | 179.461° S | 2025-09-17 13:24:18.045Z | 192.429° SSW | 44.756° | 2025-09-17 13:31:18.045Z | 0.187° NNE |
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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