ONEWEB-0704, 61609
Orbit data source: Space-Track
ONEWEB-0704, 61609 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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61609 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: 9 hours ago
TLE from 9 hours ago
0 ONEWEB-0704
1 61609U 24188R 26265.73055544 -.00000610 00000-0 -17827-2 0 9995
2 61609 87.8914 16.8438 0000750 120.9253 239.1949 13.10374905 96066Epoch: 2026-09-22T17:31Z
TLE epoch observation values (Epoch: 2026-09-22T17:31:59.990Z)
Latitude
0.00009°
Longitude
112.25201°
Altitude
1,224.889 km
Speed
7.242 km/s
True Right ascension
01h 07m 22s
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
19:55:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,219.399 km
Perigee altitude
1,218.259 km
Semi-major axis
7,596.966 km
Eccentricity
0.00008
Inclination
87.8914°
RAAN
16.8438°
Arg. of periapsis
120.9253°
True anomaly
239.18752°
Mean anomaly
239.1949°
Eccentric anomaly
239.19121°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0017827
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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-0704 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-09-23 06:29:31.142Z | 118.756° SE | 2026-09-23 06:34:31.142Z | 75.053° E | 21.039° | 2026-09-23 06:39:31.142Z | 30.824° NE |
| 13 mins | 2026-09-23 08:17:31.142Z | 190.698° SSW | 2026-09-23 08:23:31.142Z | 257.728° W | 68.443° | 2026-09-23 08:30:31.142Z | 354.927° N |
| 7 mins | 2026-09-23 18:00:31.142Z | 47.88° ENE | 2026-09-23 18:03:31.142Z | 75.246° E | 16.512° | 2026-09-23 18:07:31.142Z | 108.976° ESE |
| 13 mins | 2026-09-23 19:48:31.142Z | 357.57° N | 2026-09-23 19:54:31.142Z | 217.238° SW | 80.152° | 2026-09-23 20:01:31.142Z | 184.47° SSW |
| 5 mins | 2026-09-23 21:40:31.142Z | 309.972° NW | 2026-09-23 21:42:31.142Z | 293.087° NW | 13.751° | 2026-09-23 21:45:31.142Z | 267.584° 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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