ONEWEB-0693, 61601
Orbit data source: Space-Track
ONEWEB-0693, 61601 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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61601 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ONEWEB-0693
1 61601U 24188H 25342.59556732 .00000039 00000-0 66983-4 0 9993
2 61601 87.9104 43.8165 0002591 101.4190 258.7233 13.17648706 60789Epoch: 2025-12-08T14:17Z
TLE epoch observation values (Epoch: 2025-12-08T14:17:37.016Z)
Latitude
0.00001°
Longitude
111.81993°
Altitude
1,196.997 km
Speed
7.255 km/s
True Right ascension
02h 55m 15s
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
20:30:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,192.784 km
Perigee altitude
1,188.862 km
Semi-major axis
7,568.96 km
Eccentricity
0.00026
Inclination
87.9104°
RAAN
43.8165°
Arg. of periapsis
101.419°
True anomaly
258.69418°
Mean anomaly
258.7233°
Eccentric anomaly
258.70874°
Mean motion
3.29601 °/min
Orbital period
109.22 mins
BSTAR
0.000066983
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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-0693 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-09 03:11:26.089Z | 114.401° SE | 2025-12-09 03:16:26.089Z | 68.7° E | 18.388° | 2025-12-09 03:20:26.089Z | 33.654° NE |
| 13 mins | 2025-12-09 04:58:26.089Z | 188.858° SSW | 2025-12-09 05:04:26.089Z | 266.9° W | 43.574° | 2025-12-09 05:11:26.089Z | 356.223° N |
| 5 mins | 2025-12-09 14:38:26.089Z | 52.385° ENE | 2025-12-09 14:40:26.089Z | 70.047° E | 13.664° | 2025-12-09 14:43:26.089Z | 96.122° ESE |
| 12 mins | 2025-12-09 16:25:26.089Z | 0.558° NNE | 2025-12-09 16:31:26.089Z | 164.327° S | 44.582° | 2025-12-09 16:37:26.089Z | 180.05° SSW |
| 5 mins | 2025-12-09 18:17:26.089Z | 305.623° NW | 2025-12-09 18:19:26.089Z | 287.129° WNW | 14.913° | 2025-12-09 18:22:26.089Z | 260.762° W |
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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