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: 15 hours ago
TLE from 15 hours ago
0 MOHAMMED VI-B
1 43717U 18095A 25260.31224950 .00000696 00000-0 10563-3 0 9995
2 43717 97.9455 331.5435 0001270 97.6127 262.5227 14.77126140367903Epoch: 2025-09-17T07:29Z
TLE epoch observation values (Epoch: 2025-09-17T07:29:38.356Z)
Latitude
-0.00009°
Longitude
-137.35631°
Altitude
641.543 km
Speed
7.537 km/s
True Right ascension
22h 06m 10s
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
15:02:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.348 km
Perigee altitude
634.566 km
Semi-major axis
7,013.594 km
Eccentricity
0.00013
Inclination
97.9455°
RAAN
331.5435°
Arg. of periapsis
97.6127°
True anomaly
262.50827°
Mean anomaly
262.5227°
Eccentric anomaly
262.51549°
Mean motion
3.69515 °/min
Orbital period
97.42 mins
BSTAR
0.00010563
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Other satellites on launch #95 in the year 2018 (2018-11-21 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.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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-18 04:44:41.369Z | 161.648° S | 2025-09-18 04:48:41.369Z | 79.543° E | 44.495° | 2025-09-18 04:52:41.369Z | 350.303° N |
| 6 mins | 2025-09-18 18:12:41.369Z | 351.056° N | 2025-09-18 18:15:41.369Z | 280.129° WNW | 34.387° | 2025-09-18 18:18:41.369Z | 221.678° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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