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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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: 19 hours ago
TLE from 19 hours ago
0 ONEWEB-0688
1 61596U 24188C 26071.82053066 -.00000011 00000-0 -60820-4 0 9990
2 61596 87.9145 25.0192 0001003 41.1969 318.9238 13.17649338 73207Epoch: 2026-03-12T19:41Z
TLE epoch observation values (Epoch: 2026-03-12T19:41:33.849Z)
Latitude
-0.00001°
Longitude
-80.83677°
Altitude
1,196.038 km
Speed
7.256 km/s
True Right ascension
01h 40m 04s
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
19:08:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,191.58 km
Perigee altitude
1,190.062 km
Semi-major axis
7,568.958 km
Eccentricity
0.0001
Inclination
87.9145°
RAAN
25.0192°
Arg. of periapsis
41.1969°
True anomaly
318.91625°
Mean anomaly
318.9238°
Eccentric anomaly
318.92002°
Mean motion
3.29601 °/min
Orbital period
109.22 mins
BSTAR
-0.00006082
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-13 19:32:38.143Z | 102.981° ESE | 2026-03-13 19:36:38.143Z | 67.544° E | 15.309° | 2026-03-13 19:39:38.143Z | 41.59° NE |
| 13 mins | 2026-03-13 21:18:38.143Z | 181.335° SSW | 2026-03-13 21:24:38.143Z | 293.894° NW | 44.88° | 2026-03-13 21:31:38.143Z | 359.576° N |
| 4 mins | 2026-03-13 23:13:38.143Z | 277.064° WNW | 2026-03-13 23:14:38.143Z | 285.931° WNW | 13.206° | 2026-03-13 23:17:38.143Z | 311.873° NW |
| 12 mins | 2026-03-14 08:45:38.143Z | 5.505° NNE | 2026-03-14 08:50:38.143Z | 62.249° ENE | 43.619° | 2026-03-14 08:57:38.143Z | 172.989° S |
| 7 mins | 2026-03-14 10:36:38.143Z | 314.646° NW | 2026-03-14 10:39:38.143Z | 285.493° WNW | 18.024° | 2026-03-14 10:43:38.143Z | 249.219° W |
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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