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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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
2.032 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ONEWEB-0698
1 61604U 24188L 25261.28093927 -.00000466 00000-0 -13504-2 0 9999
2 61604 87.8771 75.2602 0000788 122.9585 237.1619 13.11417568 48833Epoch: 2025-09-18T06:44Z
TLE epoch observation values (Epoch: 2025-09-18T06:44:33.152Z)
Latitude
-0.00002°
Longitude
-23.32273°
Altitude
1,220.894 km
Speed
7.244 km/s
True Right ascension
05h 01m 02s
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
05:58:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.397 km
Perigee altitude
1,214.2 km
Semi-major axis
7,592.936 km
Eccentricity
0.00008
Inclination
87.8771°
RAAN
75.2602°
Arg. of periapsis
122.9585°
True anomaly
237.15431°
Mean anomaly
237.1619°
Eccentric anomaly
237.15811°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0013504
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 14:15:27.558Z | 273.723° WNW | 2025-09-18 14:17:27.558Z | 290.573° WNW | 12.31° | 2025-09-18 14:19:27.558Z | 307.329° NW |
| 4 mins | 2025-09-18 22:03:27.558Z | 56.773° ENE | 2025-09-18 22:05:27.558Z | 74.207° E | 13.114° | 2025-09-18 22:07:27.558Z | 91.157° ESE |
| 12 mins | 2025-09-18 23:50:27.558Z | 1.748° NNE | 2025-09-18 23:56:27.558Z | 142.373° SSE | 44.552° | 2025-09-19 00:02:27.558Z | 178.049° S |
| 6 mins | 2025-09-19 01:42:27.558Z | 310.729° NW | 2025-09-19 01:44:27.558Z | 292.62° NW | 15.854° | 2025-09-19 01:48:27.558Z | 257.072° W |
| 6 mins | 2025-09-19 10:23:27.558Z | 92.211° ESE | 2025-09-19 10:25:27.558Z | 74.361° E | 14.96° | 2025-09-19 10:29:27.558Z | 40.197° NE |
| 13 mins | 2025-09-19 12:08:27.558Z | 179.645° S | 2025-09-19 12:14:27.558Z | 215.664° SW | 44.954° | 2025-09-19 12:21:27.558Z | 0.199° 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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