MOHAMMED VI-B, 43717
Orbit data source: Space-Track
MOHAMMED VI-B, 43717 is a payload satellite owned by RMAF (MA) in SSO that was launched on Wed, 21 Nov 2018 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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43717 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
MARelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Defense Imaging
Bus & Motor
ASTROSAT-1000, Unknown motor
Mass
1,108 kg wet, ~900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 3 Pan, 4.0 m
Radar Cross Section
12.145 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 MOHAMMED VI-B
1 43717U 18095A 25300.95750214 .00001206 00000-0 17800-3 0 9996
2 43717 97.9617 11.5869 0001211 99.8591 260.2756 14.77065838373908Epoch: 2025-10-27T22:58Z
TLE epoch observation values (Epoch: 2025-10-27T22:58:48.184Z)
Latitude
-0.00004°
Longitude
-9.66575°
Altitude
641.76 km
Speed
7.537 km/s
True Right ascension
00h 46m 20s
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
01:04:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.498 km
Perigee altitude
634.799 km
Semi-major axis
7,013.786 km
Eccentricity
0.00012
Inclination
97.9617°
RAAN
11.5869°
Arg. of periapsis
99.8591°
True anomaly
260.26192°
Mean anomaly
260.2756°
Eccentric anomaly
260.26876°
Mean motion
3.695 °/min
Orbital period
97.43 mins
BSTAR
0.000178
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Other satellites on launch #95 in the year 2018 (2018-11-21 UTC)
No other RSOs were in this launch
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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.MOHAMMED VI-B 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 | 2025-10-28 05:37:35.833Z | 224.193° SW | 2025-10-28 05:39:35.833Z | 266.058° W | 24.923° | 2025-10-28 05:42:35.833Z | 317.598° NNW |
| 7 mins | 2025-10-28 17:26:35.833Z | 25.241° NE | 2025-10-28 17:29:35.833Z | 85.827° E | 39.665° | 2025-10-28 17:33:35.833Z | 177.94° S |
| 6 mins | 2025-10-29 04:23:35.833Z | 131.963° SE | 2025-10-29 04:25:35.833Z | 88.06° E | 34.066° | 2025-10-29 04:29:35.833Z | 3.592° 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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