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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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-0704
1 61609U 24188R 25340.80126411 .00000615 00000-0 17253-2 0 9994
2 61609 87.8825 74.5773 0001075 67.7587 292.3654 13.10371342 58096Epoch: 2025-12-06T19:13Z
TLE epoch observation values (Epoch: 2025-12-06T19:13:49.219Z)
Latitude
-0.00003°
Longitude
70.29843°
Altitude
1,224.3 km
Speed
7.242 km/s
True Right ascension
04h 58m 18s
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
06:22:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,219.659 km
Perigee altitude
1,218.026 km
Semi-major axis
7,596.98 km
Eccentricity
0.00011
Inclination
87.8825°
RAAN
74.5773°
Arg. of periapsis
67.7587°
True anomaly
292.35401°
Mean anomaly
292.3654°
Eccentric anomaly
292.3597°
Mean motion
3.27779 °/min
Orbital period
109.83 mins
BSTAR
0.0017253
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-07 08:18:01.330Z | 305.682° NW | 2025-12-07 08:18:01.330Z | 305.682° NW | 22.629° | 2025-12-07 08:22:01.330Z | 337.251° NNW |
| 12 mins | 2025-12-07 17:50:01.330Z | 16.696° NNE | 2025-12-07 17:56:01.330Z | 86.34° E | 34.212° | 2025-12-07 18:02:01.330Z | 150.117° SSE |
| 10 mins | 2025-12-07 19:41:01.330Z | 332.594° NNW | 2025-12-07 19:46:01.330Z | 274.167° WNW | 29.113° | 2025-12-07 19:51:01.330Z | 224.044° SW |
| 12 mins | 2025-12-08 06:10:01.330Z | 148.779° SSE | 2025-12-08 06:15:01.330Z | 89.302° E | 36.685° | 2025-12-08 06:22:01.330Z | 12.456° NNE |
| 10 mins | 2025-12-08 08:01:01.330Z | 232.201° WSW | 2025-12-08 08:05:01.330Z | 274.765° WNW | 26.56° | 2025-12-08 08:11:01.330Z | 336.579° NNW |
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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