ONEWEB-0689, 61597
Orbit data source: Space-Track
ONEWEB-0689, 61597 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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61597 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: 16 hours ago
TLE from 16 hours ago
0 ONEWEB-0689
1 61597U 24188D 26313.45983359 -.00000254 00000-0 -75225-3 0 9999
2 61597 87.8927 352.2020 0002157 96.6475 263.4899 13.11419011103497Epoch: 2026-11-09T11:02Z
TLE epoch observation values (Epoch: 2026-11-09T11:02:09.622Z)
Latitude
0.00005°
Longitude
138.02584°
Altitude
1,220.75 km
Speed
7.244 km/s
True Right ascension
23h 28m 48s
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
23:05:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.431 km
Perigee altitude
1,213.155 km
Semi-major axis
7,592.93 km
Eccentricity
0.00022
Inclination
87.8927°
RAAN
352.202°
Arg. of periapsis
96.6475°
True anomaly
263.46534°
Mean anomaly
263.4899°
Eccentric anomaly
263.47762°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
-0.00075225
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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-0689 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-11-10 03:35:57.985Z | 193.159° SSW | 2026-11-10 03:42:57.985Z | 266.804° W | 62.214° | 2026-11-10 03:49:57.985Z | 353.238° N |
| 8 mins | 2026-11-10 13:18:57.985Z | 43.568° NE | 2026-11-10 13:21:57.985Z | 71.334° E | 18.316° | 2026-11-10 13:26:57.985Z | 114.864° SE |
| 13 mins | 2026-11-10 15:06:57.985Z | 355.424° N | 2026-11-10 15:12:57.985Z | 263.635° W | 77.21° | 2026-11-10 15:19:57.985Z | 188.069° SSW |
| 4 mins | 2026-11-10 16:59:57.985Z | 303.157° NW | 2026-11-10 17:00:57.985Z | 294.858° NW | 12.109° | 2026-11-10 17:03:57.985Z | 270.255° WNW |
| 8 mins | 2026-11-11 01:38:57.985Z | 106.469° ESE | 2026-11-11 01:41:57.985Z | 77.539° E | 20.711° | 2026-11-11 01:46:57.985Z | 32.293° 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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