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, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 UM5-EOSAT
1 60555U 24149CR 26083.65620137 .00002832 00000-0 22648-3 0 9990
2 60555 97.6788 163.4444 0006950 64.9648 295.2297 15.01001121 87532Epoch: 2026-03-24T15:44Z
TLE epoch observation values (Epoch: 2026-03-24T15:44:55.798Z)
Latitude
-0.00001°
Longitude
105.08118°
Altitude
564.81 km
Speed
7.58 km/s
True Right ascension
10h 53m 46s
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
21:57:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.633 km
Perigee altitude
555.988 km
Semi-major axis
6,938.948 km
Eccentricity
0.0007
Inclination
97.6788°
RAAN
163.4444°
Arg. of periapsis
64.9648°
True anomaly
295.15763°
Mean anomaly
295.2297°
Eccentric anomaly
295.19367°
Mean motion
3.75494 °/min
Orbital period
95.87 mins
BSTAR
0.00022648
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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 | 2026-03-25 17:54:55.740Z | 21.765° NNE | 2026-03-25 17:57:55.740Z | 81.222° E | 40.765° | 2026-03-25 18:01:55.740Z | 181.378° SSW |
| 6 mins | 2026-03-26 04:40:55.740Z | 131.781° SE | 2026-03-26 04:43:55.740Z | 74.959° E | 28.095° | 2026-03-26 04:46:55.740Z | 12.81° NNE |
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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