O3B MPOWER F09, 64866
Orbit data source: Space-Track
O3B MPOWER F09, 64866 is a payload satellite owned by O3B SES (LU) that was launched on Tue, 22 Jul 2025 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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64866 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, 14.5 m
Radar Cross Section
27.396 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 O3B MPOWER F09
1 64866U 25153A 26171.37412059 -.00000024 00000-0 00000+0 0 9990
2 64866 0.0589 9.4546 0006421 100.7311 249.8810 5.00115764 19717Epoch: 2026-06-20T08:58Z
TLE epoch observation values (Epoch: 2026-06-20T08:58:44.018Z)
Latitude
-0.00977°
Longitude
-43.27311°
Altitude
8,067.559 km
Speed
5.253 km/s
True Right ascension
23h 59m 59s
True Declination
0° 00' 35"
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
07:21:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,078.22 km
Perigee altitude
8,059.667 km
Semi-major axis
14,447.081 km
Eccentricity
0.00064
Inclination
0.0589°
RAAN
9.4546°
Arg. of periapsis
100.7311°
True anomaly
249.81193°
Mean anomaly
249.881°
Eccentric anomaly
249.84646°
Mean motion
1.24989 °/min
Orbital period
288.02 mins
BSTAR
0
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Other satellites on launch #153 in the year 2025 (2025-07-22 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 F09 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 | 2026-06-20 20:26:04.900Z | 138.761° SSE | 2026-06-20 20:26:04.900Z | 138.761° SSE | 16.352° | 2026-06-20 20:36:04.900Z | 128.015° SE |
| 78 mins | 2026-06-21 01:18:04.900Z | 231.377° WSW | 2026-06-21 01:57:04.900Z | 179.476° S | 24.362° | 2026-06-21 02:36:04.900Z | 128.075° SE |
| 78 mins | 2026-06-21 07:18:04.900Z | 231.291° WSW | 2026-06-21 07:57:04.900Z | 179.577° S | 24.325° | 2026-06-21 08:36:04.900Z | 128.168° SE |
| 78 mins | 2026-06-21 13:18:04.900Z | 231.396° WSW | 2026-06-21 13:57:04.900Z | 179.704° S | 24.378° | 2026-06-21 14:36:04.900Z | 128.107° SE |
| 68 mins | 2026-06-21 19:18:04.900Z | 231.481° WSW | 2026-06-21 19:57:04.900Z | 179.603° S | 24.414° | 2026-06-21 20:26:04.900Z | 138.761° SSE |
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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