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: 10 hours ago
TLE from 10 hours ago
0 ONEWEB-0706
1 61611U 24188T 26097.88691662 -.00000555 00000-0 -16272-2 0 9995
2 61611 87.8821 50.2531 0001886 60.9103 299.2213 13.10373278 74171Epoch: 2026-04-07T21:17Z
TLE epoch observation values (Epoch: 2026-04-07T21:17:09.595Z)
Latitude
-0.00005°
Longitude
-105.19407°
Altitude
1,223.903 km
Speed
7.243 km/s
True Right ascension
03h 21m 00s
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
12:52:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.268 km
Perigee altitude
1,217.402 km
Semi-major axis
7,596.972 km
Eccentricity
0.00019
Inclination
87.8821°
RAAN
50.2531°
Arg. of periapsis
60.9103°
True anomaly
299.20244°
Mean anomaly
299.2213°
Eccentric anomaly
299.21187°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0016272
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-08 07:06:10.871Z | 51.011° ENE | 2026-04-08 07:08:10.871Z | 67.688° E | 12.508° | 2026-04-08 07:11:10.871Z | 92.645° ESE |
| 12 mins | 2026-04-08 08:54:10.871Z | 3.056° NNE | 2026-04-08 08:59:10.871Z | 45.856° ENE | 44.288° | 2026-04-08 09:06:10.871Z | 176.421° S |
| 6 mins | 2026-04-08 10:46:10.871Z | 310.463° NW | 2026-04-08 10:48:10.871Z | 291.954° WNW | 16.636° | 2026-04-08 10:52:10.871Z | 255.821° W |
| 6 mins | 2026-04-08 19:27:10.871Z | 94.539° ESE | 2026-04-08 19:30:10.871Z | 68.246° E | 14.442° | 2026-04-08 19:33:10.871Z | 42.987° NE |
| 12 mins | 2026-04-08 21:13:10.871Z | 178.279° S | 2026-04-08 21:19:10.871Z | 2.798° NNE | 44.644° | 2026-04-08 21:25:10.871Z | 0.735° NNE |
| 6 mins | 2026-04-08 23:07:10.871Z | 265.864° W | 2026-04-08 23:10:10.871Z | 292.6° NW | 14.561° | 2026-04-08 23:13:10.871Z | 317.927° 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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