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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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, 2.9 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 26306.48035707 .00000736 00000-0 39783-4 0 9999
2 62626 97.3873 21.5227 0005405 196.3978 163.7082 15.17700100 99666Epoch: 2026-11-02T11:31Z
TLE epoch observation values (Epoch: 2026-11-02T11:31:42.850Z)
Latitude
-0.00004°
Longitude
166.83739°
Altitude
519.457 km
Speed
7.602 km/s
True Right ascension
01h 26m 05s
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
13:20:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.484 km
Perigee altitude
506.039 km
Semi-major axis
6,887.899 km
Eccentricity
0.00054
Inclination
97.3873°
RAAN
21.5227°
Arg. of periapsis
196.3978°
True anomaly
163.72556°
Mean anomaly
163.7082°
Eccentric anomaly
163.71688°
Mean motion
3.79676 °/min
Orbital period
94.82 mins
BSTAR
0.000039783
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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 | 2026-11-03 18:09:21.933Z | 5.706° NNE | 2026-11-03 18:12:21.933Z | 280.723° WNW | 70.268° | 2026-11-03 18:15:21.933Z | 201.616° SSW |
| 5 mins | 2026-11-04 04:49:21.933Z | 129.296° SE | 2026-11-04 04:51:21.933Z | 59.189° ENE | 42.109° | 2026-11-04 04:54:21.933Z | 3.37° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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