ONEWEB-0691, 61599
Orbit data source: Space-Track
ONEWEB-0691, 61599 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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61599 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, 2.5 m
Radar Cross Section
2.032 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 ONEWEB-0691
1 61599U 24188F 25256.23857785 -.00000170 00000-0 -51652-3 0 9990
2 61599 87.8711 76.1679 0002027 81.7656 278.3702 13.11419937 48183Epoch: 2025-09-13T05:43Z
TLE epoch observation values (Epoch: 2025-09-13T05:43:33.126Z)
Latitude
0.00002°
Longitude
-2.19493°
Altitude
1,220.336 km
Speed
7.244 km/s
True Right ascension
05h 04m 40s
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
18:54:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.329 km
Perigee altitude
1,213.25 km
Semi-major axis
7,592.927 km
Eccentricity
0.0002
Inclination
87.8711°
RAAN
76.1679°
Arg. of periapsis
81.7656°
True anomaly
278.34722°
Mean anomaly
278.3702°
Eccentric anomaly
278.35871°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
-0.00051652
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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-0691 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-14 11:09:14.688Z | 122.544° SE | 2025-09-14 11:14:14.688Z | 75.333° E | 22.4° | 2025-09-14 11:19:14.688Z | 28.866° NE |
| 12 mins | 2025-09-14 12:58:14.688Z | 199.538° SSW | 2025-09-14 13:03:14.688Z | 264.951° W | 40.722° | 2025-09-14 13:10:14.688Z | 352.354° N |
| 8 mins | 2025-09-14 22:39:14.688Z | 42.772° NE | 2025-09-14 22:42:14.688Z | 71.009° E | 18.169° | 2025-09-14 22:47:14.688Z | 115.683° SE |
| 13 mins | 2025-09-15 00:27:14.688Z | 354.364° N | 2025-09-15 00:33:14.688Z | 267.055° W | 43.879° | 2025-09-15 00:40:14.688Z | 189.723° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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