ONEWEB-0701, 61607
Orbit data source: Space-Track
ONEWEB-0701, 61607 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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61607 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: 14 hours ago
TLE from 14 hours ago
0 ONEWEB-0701
1 61607U 24188P 26035.60079159 .00000655 00000-0 18402-2 0 9999
2 61607 87.8757 62.6831 0001890 120.7100 239.4214 13.10374127 65947Epoch: 2026-02-04T14:25Z
TLE epoch observation values (Epoch: 2026-02-04T14:25:08.393Z)
Latitude
0.00001°
Longitude
71.63309°
Altitude
1,225.331 km
Speed
7.241 km/s
True Right ascension
04h 10m 43s
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
06:07:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.268 km
Perigee altitude
1,217.396 km
Semi-major axis
7,596.969 km
Eccentricity
0.00019
Inclination
87.8757°
RAAN
62.6831°
Arg. of periapsis
120.71°
True anomaly
239.40276°
Mean anomaly
239.4214°
Eccentric anomaly
239.41208°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
0.0018402
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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-0701 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-02-05 13:00:37.784Z | 15.374° NNE | 2026-02-05 13:06:37.784Z | 72.86° E | 32.158° | 2026-02-05 13:13:37.784Z | 148.275° SSE |
| 11 mins | 2026-02-05 14:51:37.784Z | 338.15° N | 2026-02-05 14:56:37.784Z | 285.867° WNW | 30.962° | 2026-02-05 15:02:37.784Z | 219.852° SW |
| 11 mins | 2026-02-06 01:21:37.784Z | 144.12° SSE | 2026-02-06 01:26:37.784Z | 82.38° E | 34.964° | 2026-02-06 01:32:37.784Z | 16.175° NNE |
| 11 mins | 2026-02-06 03:11:37.784Z | 224.992° SW | 2026-02-06 03:16:37.784Z | 278.697° WNW | 28.508° | 2026-02-06 03:22:37.784Z | 339.525° N |
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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