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 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: 13 hours ago
TLE from 13 hours ago
0 ONEWEB-0690
1 61598U 24188E 26035.52086417 -.00000510 00000-0 -14743-2 0 9990
2 61598 87.8828 47.4511 0001176 82.9481 277.1781 13.11417477 67249Epoch: 2026-02-04T12:30Z
TLE epoch observation values (Epoch: 2026-02-04T12:30:02.664Z)
Latitude
0.00002°
Longitude
85.25374°
Altitude
1,220.458 km
Speed
7.244 km/s
True Right ascension
03h 09m 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
03:07:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.692 km
Perigee altitude
1,213.906 km
Semi-major axis
7,592.936 km
Eccentricity
0.00012
Inclination
87.8828°
RAAN
47.4511°
Arg. of periapsis
82.9481°
True anomaly
277.16473°
Mean anomaly
277.1781°
Eccentric anomaly
277.17141°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0014743
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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-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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-02-05 01:24:43.388Z | 188.341° SSW | 2026-02-05 01:31:43.388Z | 298.186° NW | 43.273° | 2026-02-05 01:37:43.388Z | 355.479° N |
| 6 mins | 2026-02-05 11:07:43.388Z | 50.187° ENE | 2026-02-05 11:09:43.388Z | 67.925° E | 14.799° | 2026-02-05 11:13:43.388Z | 102.6° ESE |
| 13 mins | 2026-02-05 12:54:43.388Z | 358.956° N | 2026-02-05 13:00:43.388Z | 345.217° N | 44.83° | 2026-02-05 13:07:43.388Z | 182.409° SSW |
| 5 mins | 2026-02-05 14:47:43.388Z | 307.249° NW | 2026-02-05 14:49:43.388Z | 289.585° WNW | 14.205° | 2026-02-05 14:52:43.388Z | 263.803° W |
| 7 mins | 2026-02-05 23:27:43.388Z | 99.293° ESE | 2026-02-05 23:30:43.388Z | 71.462° E | 16.775° | 2026-02-05 23:34:43.388Z | 36.895° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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