ONEWEB-0015, 61594
Orbit data source: Space-Track
ONEWEB-0015, 61594 is a payload satellite owned by Eut. One Web (UK) in LEO that was launched on Sun, 20 Oct 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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61594 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: 7 hours ago
TLE from 7 hours ago
0 ONEWEB-0015
1 61594U 24188A 26253.60927215 .00000514 00000-0 14141-2 0 9991
2 61594 87.8957 4.1040 0002088 113.9995 246.1352 13.11416772 95656Epoch: 2026-09-10T14:37Z
TLE epoch observation values (Epoch: 2026-09-10T14:37:21.113Z)
Latitude
-0.00001°
Longitude
155.12151°
Altitude
1,221.215 km
Speed
7.243 km/s
True Right ascension
00h 16m 24s
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
13:30:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.387 km
Perigee altitude
1,213.216 km
Semi-major axis
7,592.939 km
Eccentricity
0.00021
Inclination
87.8957°
RAAN
4.104°
Arg. of periapsis
113.9995°
True anomaly
246.11332°
Mean anomaly
246.1352°
Eccentric anomaly
246.12426°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
0.0014141
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Other satellites on launch #188 in the year 2024 (2024-10-20 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-0015 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-09-11 07:12:27.143Z | 149.551° SSE | 2026-09-11 07:18:27.143Z | 82.879° E | 45.91° | 2026-09-11 07:24:27.143Z | 15.576° NNE |
| 11 mins | 2026-09-11 09:03:27.143Z | 226.417° WSW | 2026-09-11 09:08:27.143Z | 279.713° WNW | 31.826° | 2026-09-11 09:14:27.143Z | 339.25° N |
| 12 mins | 2026-09-11 18:42:27.143Z | 21.539° NNE | 2026-09-11 18:47:27.143Z | 74.611° E | 36.444° | 2026-09-11 18:54:27.143Z | 146.222° SSE |
| 11 mins | 2026-09-11 20:32:27.143Z | 338.868° N | 2026-09-11 20:37:27.143Z | 283.541° WNW | 39.727° | 2026-09-11 20:43:27.143Z | 216.744° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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