ONEWEB-0688, 61596
Orbit data source: Space-Track
ONEWEB-0688, 61596 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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61596 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: 12 hours ago
TLE from 12 hours ago
0 ONEWEB-0688
1 61596U 24188C 25286.61879666 .00000111 00000-0 25218-3 0 9996
2 61596 87.9087 54.9381 0001561 51.1726 308.9545 13.17651205 53422Epoch: 2025-10-13T14:51Z
TLE epoch observation values (Epoch: 2025-10-13T14:51:04.031Z)
Latitude
0.00001°
Longitude
169.75232°
Altitude
1,195.86 km
Speed
7.256 km/s
True Right ascension
03h 39m 45s
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
21:09:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,191.995 km
Perigee altitude
1,189.632 km
Semi-major axis
7,568.951 km
Eccentricity
0.00016
Inclination
87.9087°
RAAN
54.9381°
Arg. of periapsis
51.1726°
True anomaly
308.94059°
Mean anomaly
308.9545°
Eccentric anomaly
308.94754°
Mean motion
3.29602 °/min
Orbital period
109.22 mins
BSTAR
0.00025218
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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-0688 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 | 2025-10-14 07:25:24.870Z | 97.613° ESE | 2025-10-14 07:28:24.870Z | 70.728° E | 15.057° | 2025-10-14 07:31:24.870Z | 44.263° NE |
| 13 mins | 2025-10-14 09:10:24.870Z | 180.369° SSW | 2025-10-14 09:16:24.870Z | 214.92° SW | 44.854° | 2025-10-14 09:23:24.870Z | 359.791° N |
| 5 mins | 2025-10-14 11:05:24.870Z | 274.075° WNW | 2025-10-14 11:07:24.870Z | 291.994° WNW | 13.5° | 2025-10-14 11:10:24.870Z | 317.189° NNW |
| 12 mins | 2025-10-14 20:37:24.870Z | 5.417° NNE | 2025-10-14 20:43:24.870Z | 107.403° ESE | 43.529° | 2025-10-14 20:49:24.870Z | 171.811° S |
| 8 mins | 2025-10-14 22:28:24.870Z | 317.51° NNW | 2025-10-14 22:31:24.870Z | 288.945° WNW | 18.331° | 2025-10-14 22:36:24.870Z | 244.404° 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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