MBZ-SAT, 62626
Orbit data source: Space-Track
MBZ-SAT, 62626 is a payload satellite owned by Rashid Space Ctr (AE) in SSO that was launched on Tue, 14 Jan 2025 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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62626 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AE / UAERelated business
Manufacturer
Rashid Space Ctr
Mission
Operational Civil Imaging
Bus & Motor
MBZSAT, Unknown motor
Mass
750 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 4 Pan, 2.3 m
Radar Cross Section
14.173 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 MBZ-SAT
1 62626U 25009T 25300.49106006 .00000583 00000-0 30918-4 0 9995
2 62626 97.4190 18.5298 0005431 93.7965 266.3890 15.19169722 43373Epoch: 2025-10-27T11:47Z
TLE epoch observation values (Epoch: 2025-10-27T11:47:07.589Z)
Latitude
-0.00008°
Longitude
165.65604°
Altitude
511.675 km
Speed
7.608 km/s
True Right ascension
01h 14m 07s
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
10:09:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.055 km
Perigee altitude
501.578 km
Semi-major axis
6,883.453 km
Eccentricity
0.00054
Inclination
97.419°
RAAN
18.5298°
Arg. of periapsis
93.7965°
True anomaly
266.32689°
Mean anomaly
266.389°
Eccentric anomaly
266.35795°
Mean motion
3.80044 °/min
Orbital period
94.73 mins
BSTAR
0.000030918
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.MBZ-SAT 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 | 2025-10-28 18:23:02.759Z | 3.31° NNE | 2025-10-28 18:26:02.759Z | 266.146° W | 41.71° | 2025-10-28 18:29:02.759Z | 203.968° SW |
| 5 mins | 2025-10-29 05:02:02.759Z | 136.619° SSE | 2025-10-29 05:04:02.759Z | 74.421° E | 35.579° | 2025-10-29 05:07:02.759Z | 3.462° NNE |
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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