O3B MPOWER F8, 62363
Orbit data source: Space-Track
O3B MPOWER F8, 62363 is a payload satellite owned by O3B SES (LU) that was launched on Tue, 17 Dec 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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62363 intel report (Beta)
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Identifier
Orbit
Country
LU / SESRelated business
Manufacturer
Boeing/ES
Mission
Operational Commercial Communications
Bus & Motor
702X, PPS5000
Mass
1,700 kg wet, 1,700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 13.5 m
Radar Cross Section
27.396 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 O3B MPOWER F8
1 62363U 24244B 26171.24081174 -.00000024 00000-0 00000+0 0 9996
2 62363 0.0157 335.6790 0005944 102.2989 282.0863 5.00115152 21025Epoch: 2026-06-20T05:46Z
TLE epoch observation values (Epoch: 2026-06-20T05:46:46.134Z)
Latitude
0.00666°
Longitude
4.8495°
Altitude
8,062.586 km
Speed
5.255 km/s
True Right ascension
23h 59m 59s
True Declination
0° 00' 24"
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
07:11:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,077.543 km
Perigee altitude
8,060.368 km
Semi-major axis
14,447.092 km
Eccentricity
0.00059
Inclination
0.0157°
RAAN
335.679°
Arg. of periapsis
102.2989°
True anomaly
282.01969°
Mean anomaly
282.0863°
Eccentric anomaly
282.05299°
Mean motion
1.24989 °/min
Orbital period
288.02 mins
BSTAR
0
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Other satellites on launch #244 in the year 2024 (2024-12-17 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.O3B MPOWER F8 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. |
|---|---|---|---|---|---|---|---|
| 79 mins | 2026-06-20 21:17:13.579Z | 232.161° WSW | 2026-06-20 21:56:13.579Z | 180.709° SSW | 24.368° | 2026-06-20 22:36:13.579Z | 127.806° SE |
| 78 mins | 2026-06-21 03:18:13.579Z | 231.086° WSW | 2026-06-21 03:56:13.579Z | 180.733° SSW | 24.363° | 2026-06-21 04:36:13.579Z | 127.896° SE |
| 78 mins | 2026-06-21 09:18:13.579Z | 231.153° WSW | 2026-06-21 09:57:13.579Z | 179.324° S | 24.369° | 2026-06-21 10:36:13.579Z | 127.926° SE |
| 78 mins | 2026-06-21 15:18:13.579Z | 231.231° WSW | 2026-06-21 15:57:13.579Z | 179.297° S | 24.373° | 2026-06-21 16:36:13.579Z | 127.837° SE |
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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