Showing default

BRO-8, 55011

Orbit data source: Space-Track

BRO-8, 55011 is a payload satellite owned by Unseen Labs (FR) in SSO that was launched on Tue, 03 Jan 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.

Loading next visibility...
Identifier
55011, 2023-001C
Orbit
SSO
Country
Flag of FRFR
Related business
Manufacturer
GOMSpace
Mission
Operational Commercial Sigint
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
2023-01-03 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 BRO-8
1 55011U 23001C   26227.86039093  .00026139  00000-0  42588-3 0  9996
2 55011  97.3137 294.0398 0003996 238.3252 121.7611 15.52606523201457
Epoch: 2026-08-15T20:38Z
TLE epoch observation values (Epoch: 2026-08-15T20:38:57.776Z)
Latitude
-0.00008°
Longitude
20.03387°
Altitude
413.685 km
Speed
7.662 km/s
True Right ascension
19h 36m 09s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
17:39:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
408.749 km
Perigee altitude
403.327 km
Semi-major axis
6,784.175 km
Eccentricity
0.0004
Inclination
97.3137°
RAAN
294.0398°
Arg. of periapsis
238.3252°
True anomaly
121.80002°
Mean anomaly
121.7611°
Eccentric anomaly
121.78056°
Mean motion
3.88416 °/min
Orbital period
92.68 mins
BSTAR
0.00042588
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|