ONEWEB-0699, 61605
Orbit data source: Space-Track
ONEWEB-0699, 61605 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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61605 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-0699
1 61605U 24188M 26316.42516988 .00000141 00000-0 36880-3 0 9996
2 61605 87.8899 6.7935 0002225 113.9836 246.1524 13.10376107102726Epoch: 2026-11-12T10:12Z
TLE epoch observation values (Epoch: 2026-11-12T10:12:14.677Z)
Latitude
-0.00008°
Longitude
162.17349°
Altitude
1,225.276 km
Speed
7.241 km/s
True Right ascension
00h 27m 10s
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
15:40:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.514 km
Perigee altitude
1,217.134 km
Semi-major axis
7,596.961 km
Eccentricity
0.00022
Inclination
87.8899°
RAAN
6.7935°
Arg. of periapsis
113.9836°
True anomaly
246.12908°
Mean anomaly
246.1524°
Eccentric anomaly
246.14074°
Mean motion
3.27781 °/min
Orbital period
109.83 mins
BSTAR
0.0003688
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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-0699 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-11-13 02:48:35.717Z | 133.257° SE | 2026-11-13 02:54:35.717Z | 75.692° E | 29.647° | 2026-11-13 03:00:35.717Z | 21.282° NNE |
| 12 mins | 2026-11-13 04:38:35.717Z | 207.186° SW | 2026-11-13 04:43:35.717Z | 264.798° W | 48.909° | 2026-11-13 04:50:35.717Z | 348.412° N |
| 9 mins | 2026-11-13 14:19:35.717Z | 35.108° NE | 2026-11-13 14:23:35.717Z | 74.684° E | 23.782° | 2026-11-13 14:28:35.717Z | 122.6° SE |
| 12 mins | 2026-11-13 16:08:35.717Z | 349.205° N | 2026-11-13 16:14:35.717Z | 260.106° W | 60.436° | 2026-11-13 16:20:35.717Z | 198.296° SSW |
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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