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: 11 hours ago
TLE from 11 hours ago
0 MOHAMMED VI-B
1 43717U 18095A 26039.94155896 .00000436 00000-0 68900-4 0 9992
2 43717 97.9471 114.1193 0001359 78.5981 281.5381 14.77073745389257Epoch: 2026-02-08T22:35Z
TLE epoch observation values (Epoch: 2026-02-08T22:35:50.694Z)
Latitude
-0.00008°
Longitude
-3.88542°
Altitude
641.402 km
Speed
7.537 km/s
True Right ascension
07h 36m 28s
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
12:05:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.576 km
Perigee altitude
634.67 km
Semi-major axis
7,013.76 km
Eccentricity
0.00014
Inclination
97.9471°
RAAN
114.1193°
Arg. of periapsis
78.5981°
True anomaly
281.52284°
Mean anomaly
281.5381°
Eccentric anomaly
281.53047°
Mean motion
3.69502 °/min
Orbital period
97.43 mins
BSTAR
0.0000689
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Other satellites on launch #95 in the year 2018 (2018-11-21 UTC)
No other RSOs were in this launch
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-09 17:03:30.803Z | 36.267° NE | 2026-02-09 17:07:30.803Z | 109.645° ESE | 27.042° | 2026-02-09 17:10:30.803Z | 156.986° SSE |
| 5 mins | 2026-02-09 18:41:30.803Z | 325.955° NNW | 2026-02-09 18:43:30.803Z | 288.804° WNW | 21.003° | 2026-02-09 18:46:30.803Z | 243.256° WSW |
| 5 mins | 2026-02-10 04:01:30.803Z | 105.814° ESE | 2026-02-10 04:03:30.803Z | 66.412° ENE | 23.228° | 2026-02-10 04:06:30.803Z | 17.487° NNE |
| 6 mins | 2026-02-10 05:37:30.803Z | 219.243° SW | 2026-02-10 05:39:30.803Z | 257.255° W | 24.749° | 2026-02-10 05:43:30.803Z | 322.878° NNW |
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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