Showing default

O3B MPOWER F10, 64867

Orbit data source: Space-Track

O3B MPOWER F10, 64867 is a payload satellite owned by O3B SES (LU) in LEO 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.

Loading next visibility...
Identifier
64867, 2025-153B
Orbit
LEO
Country
Flag of LULU / SES
Related business
None
Manufacturer
Boeing/ES
Mission
Operational spacecraft
Bus & Motor
702X, PPS5000
Mass
1,700 kg wet, 1,700 kg dry
Launch date (UTC)
2025-07-22 (1 month ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 weeks ago

TLE from 4 weeks ago
0 O3B MPOWER F10
1 64867U 25153B   25217.95322121  .00000044  00000-0 -22486-2 0  9992
2 64867   8.7489  69.7549 1862051 220.3637 124.2432  7.19907856  1028
Epoch: 2025-08-05T22:52Z
TLE epoch observation values (Epoch: 2025-08-05T22:52:38.312Z)
Latitude
0.00001°
Longitude
131.85638°
Altitude
6,365.103 km
Speed
5.233 km/s
True Right ascension
04h 39m 01s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
18:35:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
7,065.877 km
Perigee altitude
2,845.116 km
Semi-major axis
11,333.634 km
Eccentricity
0.18621
Inclination
8.7489°
RAAN
69.7549°
Arg. of periapsis
220.3637°
True anomaly
139.64793°
Mean anomaly
124.2432°
Eccentric anomaly
132.1526°
Mean motion
1.79883 °/min
Orbital period
200.13 mins
BSTAR
-0.0022486
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #153 in the year 2025 (2025-07-22 UTC)

Documentation

Showing up to 5 results
|