ONEWEB-0697, 61603
Orbit data source: Space-Track
ONEWEB-0697, 61603 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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61603 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: 6 hours ago
TLE from 6 hours ago
0 ONEWEB-0697
1 61603U 24188K 26118.47919296 -.00000473 00000-0 -13703-2 0 9996
2 61603 87.8926 30.9502 0001676 53.5691 306.5592 13.11417896 77933Epoch: 2026-04-28T11:30Z
TLE epoch observation values (Epoch: 2026-04-28T11:30:02.271Z)
Latitude
0.00003°
Longitude
1.98682°
Altitude
1,219.81 km
Speed
7.245 km/s
True Right ascension
02h 03m 48s
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
00:54:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.07 km
Perigee altitude
1,213.525 km
Semi-major axis
7,592.934 km
Eccentricity
0.00017
Inclination
87.8926°
RAAN
30.9502°
Arg. of periapsis
53.5691°
True anomaly
306.54377°
Mean anomaly
306.5592°
Eccentric anomaly
306.55149°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0013703
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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-0697 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-04-28 18:54:52.967Z | 189.524° SSW | 2026-04-28 19:01:52.967Z | 283.554° WNW | 43.071° | 2026-04-28 19:08:52.967Z | 355.849° N |
| 7 mins | 2026-04-29 04:36:52.967Z | 40.248° NE | 2026-04-29 04:40:52.967Z | 75.175° E | 15.468° | 2026-04-29 04:43:52.967Z | 101.486° ESE |
| 12 mins | 2026-04-29 06:25:52.967Z | 358.02° N | 2026-04-29 06:31:52.967Z | 205.866° SW | 44.501° | 2026-04-29 06:37:52.967Z | 183.952° SSW |
| 5 mins | 2026-04-29 08:17:52.967Z | 308.818° NW | 2026-04-29 08:19:52.967Z | 291.617° WNW | 13.591° | 2026-04-29 08:22:52.967Z | 266.018° W |
| 7 mins | 2026-04-29 16:57:52.967Z | 101.728° ESE | 2026-04-29 17:00:52.967Z | 73.742° E | 17.444° | 2026-04-29 17:04:52.967Z | 37.978° NE |
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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