ONEWEB-0706, 61611
Orbit data source: Space-Track
ONEWEB-0706, 61611 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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61611 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-0706
1 61611U 24188T 26305.66668980 .00012598 00000-0 36007-1 0 9995
2 61611 87.8893 8.9298 0002270 112.0518 301.5440 13.10366924 4933Epoch: 2026-11-01T16:00Z
TLE epoch observation values (Epoch: 2026-11-01T16:00:01.998Z)
Latitude
53.6134°
Longitude
90.819°
Altitude
1,229.671 km
Speed
7.245 km/s
True Right ascension
00h 47m 07s
True Declination
53° 27' 33"
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
00:23:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.584 km
Perigee altitude
1,217.135 km
Semi-major axis
7,596.997 km
Eccentricity
0.00023
Inclination
87.8893°
RAAN
8.9298°
Arg. of periapsis
112.0518°
True anomaly
301.52183°
Mean anomaly
301.544°
Eccentric anomaly
301.53291°
Mean motion
3.27778 °/min
Orbital period
109.83 mins
BSTAR
0.036007
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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-0706 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-11-02 04:38:14.153Z | 171.696° S | 2026-11-02 04:45:14.153Z | 112.8° SE | 75.314° | 2026-11-02 04:52:14.153Z | 4.202° NNE |
| 7 mins | 2026-11-02 06:33:14.153Z | 257.316° W | 2026-11-02 06:36:14.153Z | 285.587° WNW | 18.596° | 2026-11-02 06:40:14.153Z | 321.798° NNW |
| 12 mins | 2026-11-02 16:10:14.153Z | 9.72° NNE | 2026-11-02 16:16:14.153Z | 102.353° ESE | 61.439° | 2026-11-02 16:22:14.153Z | 165.327° S |
| 9 mins | 2026-11-02 18:01:14.153Z | 323.41° NNW | 2026-11-02 18:05:14.153Z | 283.666° WNW | 23.426° | 2026-11-02 18:10:14.153Z | 238.107° WSW |
| 9 mins | 2026-11-03 04:29:14.153Z | 166.171° S | 2026-11-03 04:35:14.153Z | 71.263° E | 69.417° | 2026-11-03 04:38:14.153Z | 14.102° NNE |
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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