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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 UM5-RIBAT
1 60554U 24149CQ 26178.47105985 .00003266 00000-0 25960-3 0 9995
2 60554 97.6629 256.1324 0002725 44.8741 315.2703 15.01129941101734Epoch: 2026-06-27T11:18Z
TLE epoch observation values (Epoch: 2026-06-27T11:18:19.571Z)
Latitude
-0°
Longitude
170.96611°
Altitude
565.124 km
Speed
7.579 km/s
True Right ascension
17h 04m 31s
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
09:16:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.304 km
Perigee altitude
558.522 km
Semi-major axis
6,938.55 km
Eccentricity
0.00027
Inclination
97.6629°
RAAN
256.1324°
Arg. of periapsis
44.8741°
True anomaly
315.24832°
Mean anomaly
315.2703°
Eccentric anomaly
315.25931°
Mean motion
3.75526 °/min
Orbital period
95.87 mins
BSTAR
0.0002596
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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
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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 | 2026-06-28 05:01:22.473Z | 155.832° SSE | 2026-06-28 05:05:22.473Z | 46.579° ENE | 41.182° | 2026-06-28 05:08:22.473Z | 355.695° N |
| 6 mins | 2026-06-28 18:16:22.473Z | 3.358° NNE | 2026-06-28 18:19:22.473Z | 261.296° W | 42.091° | 2026-06-28 18:22:22.473Z | 204.243° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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