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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 UM5-RIBAT
1 60554U 24149CQ 26260.18483430 .00001642 00000-0 13184-3 0 9990
2 60554 97.6385 336.6567 0004145 125.1890 234.9723 15.01421559113992Epoch: 2026-09-17T04:26Z
TLE epoch observation values (Epoch: 2026-09-17T04:26:09.683Z)
Latitude
-0.00003°
Longitude
-86.00935°
Altitude
567.223 km
Speed
7.577 km/s
True Right ascension
22h 26m 37s
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
15:56:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.388 km
Perigee altitude
556.637 km
Semi-major axis
6,937.65 km
Eccentricity
0.00041
Inclination
97.6385°
RAAN
336.6567°
Arg. of periapsis
125.189°
True anomaly
234.93342°
Mean anomaly
234.9723°
Eccentric anomaly
234.95286°
Mean motion
3.75599 °/min
Orbital period
95.85 mins
BSTAR
0.00013184
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-18 04:34:03.482Z | 126.614° SE | 2026-09-18 04:37:03.482Z | 67.946° E | 29.344° | 2026-09-18 04:40:03.482Z | 13.203° NNE |
| 4 mins | 2026-09-18 06:10:03.482Z | 231.163° WSW | 2026-09-18 06:12:03.482Z | 268.113° W | 19.582° | 2026-09-18 06:14:03.482Z | 303.549° NW |
| 6 mins | 2026-09-18 17:48:03.482Z | 26.916° NE | 2026-09-18 17:51:03.482Z | 114.856° SE | 53.193° | 2026-09-18 17:54:03.482Z | 175.652° 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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