ONEWEB-0698, 61604
Orbit data source: Space-Track
ONEWEB-0698, 61604 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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61604 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-0698
1 61604U 24188L 26208.41103300 -.00000486 00000-0 -14078-2 0 9992
2 61604 87.8892 13.0707 0002819 107.3765 252.7671 13.11415778 89744Epoch: 2026-07-27T09:51Z
TLE epoch observation values (Epoch: 2026-07-27T09:51:53.251Z)
Latitude
-0.00005°
Longitude
-79.99618°
Altitude
1,221.211 km
Speed
7.243 km/s
True Right ascension
00h 52m 16s
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
06:23:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.946 km
Perigee altitude
1,212.665 km
Semi-major axis
7,592.942 km
Eccentricity
0.00028
Inclination
87.8892°
RAAN
13.0707°
Arg. of periapsis
107.3765°
True anomaly
252.73625°
Mean anomaly
252.7671°
Eccentric anomaly
252.75167°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0014078
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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-0698 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 | 2026-07-27 21:29:48.393Z | 45.826° ENE | 2026-07-27 21:32:48.393Z | 72.116° E | 14.739° | 2026-07-27 21:35:48.393Z | 98.36° ESE |
| 13 mins | 2026-07-27 23:17:48.393Z | 359.155° N | 2026-07-27 23:23:48.393Z | 201.414° SSW | 44.95° | 2026-07-27 23:30:48.393Z | 182.175° SSW |
| 6 mins | 2026-07-28 01:09:48.393Z | 311.763° NW | 2026-07-28 01:12:48.393Z | 285.467° WNW | 14.238° | 2026-07-28 01:15:48.393Z | 260.365° W |
| 6 mins | 2026-07-28 09:50:48.393Z | 95.556° ESE | 2026-07-28 09:52:48.393Z | 76.98° E | 16.598° | 2026-07-28 09:56:48.393Z | 40.867° NE |
| 12 mins | 2026-07-28 11:36:48.393Z | 184.626° SSW | 2026-07-28 11:41:48.393Z | 230.844° WSW | 44.357° | 2026-07-28 11:48:48.393Z | 358.078° N |
| 4 mins | 2026-07-28 13:31:48.393Z | 277.494° WNW | 2026-07-28 13:32:48.393Z | 285.999° WNW | 12.426° | 2026-07-28 13:35:48.393Z | 311.119° NW |
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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