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: 19 hours ago
TLE from 19 hours ago
0 UM5-EOSAT
1 60555U 24149CR 26126.18391077 .00002911 00000-0 23114-3 0 9991
2 60555 97.6655 205.4483 0005983 242.4186 117.6431 15.01248700 93912Epoch: 2026-05-06T04:24Z
TLE epoch observation values (Epoch: 2026-05-06T04:24:49.890Z)
Latitude
-0.00001°
Longitude
-84.80762°
Altitude
568.031 km
Speed
7.576 km/s
True Right ascension
13h 41m 47s
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
07:41:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.198 km
Perigee altitude
555.896 km
Semi-major axis
6,938.184 km
Eccentricity
0.0006
Inclination
97.6655°
RAAN
205.4483°
Arg. of periapsis
242.4186°
True anomaly
117.70381°
Mean anomaly
117.6431°
Eccentric anomaly
117.67346°
Mean motion
3.75556 °/min
Orbital period
95.86 mins
BSTAR
0.00023114
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-07 04:33:19.556Z | 119.826° SE | 2026-05-07 04:36:19.556Z | 59.075° ENE | 23.564° | 2026-05-07 04:38:19.556Z | 21.948° NNE |
| 4 mins | 2026-05-07 06:09:19.556Z | 234.058° WSW | 2026-05-07 06:11:19.556Z | 275.879° WNW | 20.122° | 2026-05-07 06:13:19.556Z | 309.924° NW |
| 6 mins | 2026-05-07 17:47:19.556Z | 32.761° NE | 2026-05-07 17:49:19.556Z | 75.327° E | 34.95° | 2026-05-07 17:53:19.556Z | 172.657° S |
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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