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: 14 hours ago
TLE from 14 hours ago
0 ONEWEB-0697
1 61603U 24188K 26072.31965208 -.00000484 00000-0 -14025-2 0 9992
2 61603 87.8864 40.1277 0002625 84.7238 275.4189 13.11417001 71886Epoch: 2026-03-13T07:40Z
TLE epoch observation values (Epoch: 2026-03-13T07:40:17.939Z)
Latitude
-0.00008°
Longitude
114.09607°
Altitude
1,220.384 km
Speed
7.244 km/s
True Right ascension
02h 40m 30s
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
02:12:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.794 km
Perigee altitude
1,212.808 km
Semi-major axis
7,592.938 km
Eccentricity
0.00026
Inclination
87.8864°
RAAN
40.1277°
Arg. of periapsis
84.7238°
True anomaly
275.38895°
Mean anomaly
275.4189°
Eccentric anomaly
275.40393°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0014025
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-03-13 22:24:54.020Z | 185.095° SSW | 2026-03-13 22:30:54.020Z | 231.077° WSW | 43.944° | 2026-03-13 22:37:54.020Z | 357.247° N |
| 4 mins | 2026-03-14 00:20:54.020Z | 276.826° WNW | 2026-03-14 00:22:54.020Z | 293.64° NW | 11.874° | 2026-03-14 00:24:54.020Z | 310.002° NW |
| 5 mins | 2026-03-14 08:07:54.020Z | 51.405° ENE | 2026-03-14 08:09:54.020Z | 68.628° E | 13.49° | 2026-03-14 08:12:54.020Z | 94.342° ESE |
| 13 mins | 2026-03-14 09:54:54.020Z | 0.8° NNE | 2026-03-14 10:00:54.020Z | 43.348° NE | 44.814° | 2026-03-14 10:07:54.020Z | 179.156° S |
| 6 mins | 2026-03-14 11:47:54.020Z | 307.401° NW | 2026-03-14 11:49:54.020Z | 289.036° WNW | 15.556° | 2026-03-14 11:53:54.020Z | 254.826° W |
| 6 mins | 2026-03-14 20:27:54.020Z | 97.666° ESE | 2026-03-14 20:30:54.020Z | 70.976° E | 15.369° | 2026-03-14 20:33:54.020Z | 44.602° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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