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: 13 hours ago
TLE from 13 hours ago
0 ONEWEB-0704
1 61609U 24188R 26305.89460236 -.00000602 00000-0 -17609-2 0 9994
2 61609 87.8906 8.8773 0002536 121.3247 238.8129 13.10371586101326Epoch: 2026-11-01T21:28Z
TLE epoch observation values (Epoch: 2026-11-01T21:28:13.643Z)
Latitude
-0.00003°
Longitude
5.64103°
Altitude
1,225.608 km
Speed
7.241 km/s
True Right ascension
00h 35m 30s
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
06:40:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.768 km
Perigee altitude
1,216.915 km
Semi-major axis
7,596.979 km
Eccentricity
0.00025
Inclination
87.8906°
RAAN
8.8773°
Arg. of periapsis
121.3247°
True anomaly
238.78804°
Mean anomaly
238.8129°
Eccentric anomaly
238.80047°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0017609
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-02 14:36:35.975Z | 47.483° ENE | 2026-11-02 14:39:35.975Z | 72.014° E | 12.309° | 2026-11-02 14:41:35.975Z | 88.467° E |
| 13 mins | 2026-11-02 16:24:35.975Z | 3.364° NNE | 2026-11-02 16:30:35.975Z | 95.858° ESE | 78.198° | 2026-11-02 16:37:35.975Z | 175.516° S |
| 7 mins | 2026-11-02 18:16:35.975Z | 314.885° NW | 2026-11-02 18:19:35.975Z | 286.98° WNW | 18.202° | 2026-11-02 18:23:35.975Z | 251.641° W |
| 5 mins | 2026-11-03 02:58:35.975Z | 89.767° E | 2026-11-03 03:00:35.975Z | 72.385° E | 14.451° | 2026-11-03 03:03:35.975Z | 46.715° ENE |
| 13 mins | 2026-11-03 04:43:35.975Z | 176.802° S | 2026-11-03 04:49:35.975Z | 92.549° ESE | 87.025° | 2026-11-03 04:56:35.975Z | 1.415° NNE |
| 7 mins | 2026-11-03 06:37:35.975Z | 261.824° W | 2026-11-03 06:40:35.975Z | 288.422° WNW | 15.825° | 2026-11-03 06:44:35.975Z | 322.141° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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