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: 11 hours ago
TLE from 11 hours ago
0 MBZ-SAT
1 62626U 25009T 25315.18012827 .00000590 00000-0 31355-4 0 9998
2 62626 97.4181 32.9522 0003101 49.3934 310.7570 15.19058140 45606Epoch: 2025-11-11T04:19Z
TLE epoch observation values (Epoch: 2025-11-11T04:19:23.082Z)
Latitude
-0.00002°
Longitude
-82.46436°
Altitude
510.38 km
Speed
7.609 km/s
True Right ascension
02h 11m 48s
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
11:37:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.788 km
Perigee altitude
503.519 km
Semi-major axis
6,883.79 km
Eccentricity
0.00031
Inclination
97.4181°
RAAN
32.9522°
Arg. of periapsis
49.3934°
True anomaly
310.73008°
Mean anomaly
310.757°
Eccentric anomaly
310.74354°
Mean motion
3.80016 °/min
Orbital period
94.73 mins
BSTAR
0.000031355
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-11 17:32:33.644Z | 41.164° NE | 2025-11-11 17:35:33.644Z | 103.357° ESE | 23.829° | 2025-11-11 17:37:33.644Z | 145.469° SSE |
| 4 mins | 2025-11-11 19:07:33.644Z | 321.039° NNW | 2025-11-11 19:08:33.644Z | 301.942° NW | 17.259° | 2025-11-11 19:11:33.644Z | 247.395° WSW |
| 5 mins | 2025-11-12 05:45:33.644Z | 201.054° SSW | 2025-11-12 05:47:33.644Z | 266.428° W | 34.553° | 2025-11-12 05:50:33.644Z | 332.07° 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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