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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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: 17 hours ago
TLE from 17 hours ago
0 ONEWEB-0015
1 61594U 24188A 25309.60733461 .00000154 00000-0 39911-3 0 9993
2 61594 87.8854 65.6239 0001002 101.9922 258.1319 13.11418715 55152Epoch: 2025-11-05T14:34Z
TLE epoch observation values (Epoch: 2025-11-05T14:34:33.710Z)
Latitude
0.00006°
Longitude
161.90587°
Altitude
1,220.722 km
Speed
7.244 km/s
True Right ascension
04h 22m 29s
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
03:41:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.555 km
Perigee altitude
1,214.033 km
Semi-major axis
7,592.931 km
Eccentricity
0.0001
Inclination
87.8854°
RAAN
65.6239°
Arg. of periapsis
101.9922°
True anomaly
258.12066°
Mean anomaly
258.1319°
Eccentric anomaly
258.12628°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
0.00039911
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-11-06 08:58:41.241Z | 202.643° SW | 2025-11-06 09:05:41.241Z | 280.548° WNW | 37.074° | 2025-11-06 09:11:41.241Z | 347.23° N |
| 9 mins | 2025-11-06 18:40:41.241Z | 36.12° NE | 2025-11-06 18:44:41.241Z | 76.303° E | 21.788° | 2025-11-06 18:49:41.241Z | 123.397° SE |
| 12 mins | 2025-11-06 20:29:41.241Z | 348.783° N | 2025-11-06 20:34:41.241Z | 289.069° WNW | 41.091° | 2025-11-06 20:41:41.241Z | 197.622° SSW |
| 10 mins | 2025-11-07 06:59:41.241Z | 123.245° SE | 2025-11-07 07:04:41.241Z | 72.349° E | 23.933° | 2025-11-07 07:09:41.241Z | 26.385° NE |
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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