UM5-RIBAT, 60554
Orbit data source: Space-Track
UM5-RIBAT, 60554 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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60554 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
MARelated business
Manufacturer
UM5R
Mission
Operational Amateur Technology
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: 8 hours ago
TLE from 8 hours ago
0 UM5-RIBAT
1 60554U 24149CQ 25291.14618794 .00006531 00000-0 54567-3 0 9994
2 60554 97.7002 6.9436 0009094 159.7236 200.4350 14.98826604 63900Epoch: 2025-10-18T03:30Z
TLE epoch observation values (Epoch: 2025-10-18T03:30:30.638Z)
Latitude
0.00004°
Longitude
-72.56546°
Altitude
579.497 km
Speed
7.568 km/s
True Right ascension
00h 27m 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
05:51:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.844 km
Perigee altitude
561.211 km
Semi-major axis
6,945.664 km
Eccentricity
0.00091
Inclination
97.7002°
RAAN
6.9436°
Arg. of periapsis
159.7236°
True anomaly
200.39865°
Mean anomaly
200.435°
Eccentric anomaly
200.41682°
Mean motion
3.74949 °/min
Orbital period
96.01 mins
BSTAR
0.00054567
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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-RIBAT Visibility forecast
Loading observer location...
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 | 2025-10-18 18:30:42.644Z | 343.281° N | 2025-10-18 18:32:42.644Z | 283.813° WNW | 34.001° | 2025-10-18 18:35:42.644Z | 219.887° SW |
| 6 mins | 2025-10-19 05:16:42.644Z | 172.264° S | 2025-10-19 05:19:42.644Z | 313.947° NW | 43.535° | 2025-10-19 05:22:42.644Z | 344.534° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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