ONEWEB-0698, 61604
Orbit data source: Space-Track
ONEWEB-0698, 61604 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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61604 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: 12 hours ago
TLE from 12 hours ago
0 ONEWEB-0698
1 61604U 24188L 25305.60936767 -.00000560 00000-0 -16151-2 0 9998
2 61604 87.8840 66.4091 0002742 111.1775 248.9646 13.11418237 54647Epoch: 2025-11-01T14:37Z
TLE epoch observation values (Epoch: 2025-11-01T14:37:29.366Z)
Latitude
-0.00004°
Longitude
165.89975°
Altitude
1,221.315 km
Speed
7.243 km/s
True Right ascension
04h 25m 38s
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
21:54:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.878 km
Perigee altitude
1,212.714 km
Semi-major axis
7,592.933 km
Eccentricity
0.00027
Inclination
87.884°
RAAN
66.4091°
Arg. of periapsis
111.1775°
True anomaly
248.93528°
Mean anomaly
248.9646°
Eccentric anomaly
248.94994°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
-0.0016151
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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-0698 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 | 2025-11-02 07:14:09.009Z | 120.762° SE | 2025-11-02 07:19:09.009Z | 74.974° E | 21.189° | 2025-11-02 07:24:09.009Z | 29.578° NE |
| 13 mins | 2025-11-02 09:02:09.009Z | 194.239° SSW | 2025-11-02 09:08:09.009Z | 264.803° W | 41.792° | 2025-11-02 09:15:09.009Z | 353.578° N |
| 7 mins | 2025-11-02 18:44:09.009Z | 43.843° NE | 2025-11-02 18:47:09.009Z | 71.456° E | 17.033° | 2025-11-02 18:51:09.009Z | 107.702° ESE |
| 13 mins | 2025-11-02 20:32:09.009Z | 355.876° N | 2025-11-02 20:38:09.009Z | 261.47° W | 44.425° | 2025-11-02 20:45:09.009Z | 187.297° SSW |
| 4 mins | 2025-11-02 22:25:09.009Z | 303.202° NW | 2025-11-02 22:27:09.009Z | 286.272° WNW | 12.069° | 2025-11-02 22:29:09.009Z | 269.961° 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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