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.
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60555 intel report (Beta)
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Identifier
Orbit
Country
MARelated business
Manufacturer
UM5R
Mission
Operational Amateur Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 UM5-EOSAT
1 60555U 24149CR 26219.74539328 .00001409 00000-0 11255-3 0 9993
2 60555 97.6762 297.9156 0006924 327.8790 32.2012 15.01852697107952Epoch: 2026-08-07T17:53Z
TLE epoch observation values (Epoch: 2026-08-07T17:53:21.979Z)
Latitude
0°
Longitude
73.30734°
Altitude
560.176 km
Speed
7.584 km/s
True Right ascension
19h 51m 39s
True Declination
0° 00' 00"
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
17:44:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.988 km
Perigee altitude
553.383 km
Semi-major axis
6,936.322 km
Eccentricity
0.00069
Inclination
97.6762°
RAAN
297.9156°
Arg. of periapsis
327.879°
True anomaly
32.24351°
Mean anomaly
32.2012°
Eccentric anomaly
32.22235°
Mean motion
3.75707 °/min
Orbital period
95.82 mins
BSTAR
0.00011255
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.UM5-EOSAT 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-08 05:12:13.769Z | 161.347° S | 2026-08-08 05:16:13.769Z | 15.209° NNE | 42.163° | 2026-08-08 05:19:13.769Z | 351.26° N |
| 7 mins | 2026-08-08 18:26:13.769Z | 0.968° NNE | 2026-08-08 18:29:13.769Z | 302.045° NW | 39.213° | 2026-08-08 18:33:13.769Z | 208.158° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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