Showing default

UM5-EOSAT, 60555

Orbit data source: Space-Track

UM5-EOSAT, 60555 is a Moroccan payload satellite in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
60555, 2024-149CR
Orbit
SSO
Country
Flag of MAMA
Related business
Manufacturer
UM5R
Mission
Operational Amateur Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2024-08-16 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 UM5-EOSAT
1 60555U 24149CR  25338.68986316  .00009235  00000-0  74896-3 0  9995
2 60555  97.7031  54.5765 0007818  40.6741 319.5065 14.99867455 71047
Epoch: 2025-12-04T16:33Z
TLE epoch observation values (Epoch: 2025-12-04T16:33:24.177Z)
Latitude
0.00001°
Longitude
92.48307°
Altitude
566.231 km
Speed
7.58 km/s
True Right ascension
03h 38m 18s
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
09:17:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.739 km
Perigee altitude
558.883 km
Semi-major axis
6,942.448 km
Eccentricity
0.00078
Inclination
97.7031°
RAAN
54.5765°
Arg. of periapsis
40.6741°
True anomaly
319.44828°
Mean anomaly
319.5065°
Eccentric anomaly
319.4774°
Mean motion
3.7521 °/min
Orbital period
95.95 mins
BSTAR
0.00074896
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...

Documentation

Showing up to 5 results
|