O3B MPOWER F05, 58346
Orbit data source: Space-Track
O3B MPOWER F05, 58346 is a payload satellite owned by O3B SES (LU) that was launched on Sun, 12 Nov 2023 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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58346 intel report (Beta)
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Identifier
Orbit
Country
LU / SESRelated business
Manufacturer
Boeing/ES
Mission
Partially 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: 18 hours ago
TLE from 18 hours ago
0 O3B MPOWER F05
1 58346U 23175A 26185.09935693 -.00000013 00000-0 00000-0 0 9995
2 58346 0.0509 10.1276 0005369 110.6442 239.2807 5.00115957 50289Epoch: 2026-07-04T02:23Z
TLE epoch observation values (Epoch: 2026-07-04T02:23:04.438Z)
Latitude
-0.01103°
Longitude
42.11362°
Altitude
8,068.328 km
Speed
5.253 km/s
True Right ascension
00h 00m 00s
True Declination
0° 00' 40"
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
07:54:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,076.697 km
Perigee altitude
8,061.183 km
Semi-major axis
14,447.077 km
Eccentricity
0.00054
Inclination
0.0509°
RAAN
10.1276°
Arg. of periapsis
110.6442°
True anomaly
239.22783°
Mean anomaly
239.2807°
Eccentric anomaly
239.25426°
Mean motion
1.24989 °/min
Orbital period
288.02 mins
BSTAR
0
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Other satellites on launch #175 in the year 2023 (2023-11-12 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 F05 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 | 2026-07-04 23:16:22.025Z | 232.096° WSW | 2026-07-04 23:55:22.025Z | 180.579° SSW | 24.375° | 2026-07-05 00:35:22.025Z | 127.744° SE |
| 78 mins | 2026-07-05 05:17:22.025Z | 230.988° WSW | 2026-07-05 05:55:22.025Z | 180.601° SSW | 24.328° | 2026-07-05 06:35:22.025Z | 127.828° SE |
| 78 mins | 2026-07-05 11:17:22.025Z | 231.041° WSW | 2026-07-05 11:56:22.025Z | 179.177° S | 24.363° | 2026-07-05 12:35:22.025Z | 127.813° SE |
| 78 mins | 2026-07-05 17:17:22.025Z | 231.15° WSW | 2026-07-05 17:55:22.025Z | 180.712° SSW | 24.408° | 2026-07-05 18:35:22.025Z | 127.729° 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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