ONEWEB-0690, 61598
Orbit data source: Space-Track
ONEWEB-0690, 61598 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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61598 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
One Web
Mission
Operational spacecraft
Bus & Motor
ARROW, Unknown motor
Mass
148 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 6.7 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ONEWEB-0690
1 61598U 24188E 25340.62789298 -.00000343 00000-0 -10046-2 0 9992
2 61598 87.8878 59.3929 0002420 98.4287 261.7115 13.11416988 59391Epoch: 2025-12-06T15:04Z
TLE epoch observation values (Epoch: 2025-12-06T15:04:09.953Z)
Latitude
-0.00005°
Longitude
117.69852°
Altitude
1,220.837 km
Speed
7.244 km/s
True Right ascension
03h 57m 34s
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
22:12:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.638 km
Perigee altitude
1,212.963 km
Semi-major axis
7,592.938 km
Eccentricity
0.00024
Inclination
87.8878°
RAAN
59.3929°
Arg. of periapsis
98.4287°
True anomaly
261.68406°
Mean anomaly
261.7115°
Eccentric anomaly
261.69778°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0010046
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Other satellites on launch #188 in the year 2024 (2024-10-20 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ONEWEB-0690 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 | 2025-12-07 04:03:44.989Z | 94.153° ESE | 2025-12-07 04:06:44.989Z | 68.709° E | 13.442° | 2025-12-07 04:09:44.989Z | 43.867° NE |
| 12 mins | 2025-12-07 05:49:44.989Z | 175.405° S | 2025-12-07 05:55:44.989Z | 26.202° NE | 44.464° | 2025-12-07 06:01:44.989Z | 2.017° NNE |
| 6 mins | 2025-12-07 07:43:44.989Z | 266.187° W | 2025-12-07 07:45:44.989Z | 284.469° WNW | 15.597° | 2025-12-07 07:49:44.989Z | 319.601° NNW |
| 14 mins | 2025-12-07 17:17:44.989Z | 4.245° NNE | 2025-12-07 17:24:44.989Z | 75.171° E | 42.943° | 2025-12-07 17:31:44.989Z | 170.101° S |
| 8 mins | 2025-12-07 19:10:44.989Z | 318.477° NNW | 2025-12-07 19:13:44.989Z | 289.618° WNW | 19.559° | 2025-12-07 19:18:44.989Z | 243.76° WSW |
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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