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, 2.3 m
Radar Cross Section
14.173 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 MBZ-SAT
1 62626U 25009T 26104.16604391 .00000279 00000-0 16817-4 0 9996
2 62626 97.3978 183.8667 0005923 175.9801 184.1482 15.18318750 68973Epoch: 2026-04-14T03:59Z
TLE epoch observation values (Epoch: 2026-04-14T03:59:06.193Z)
Latitude
-0.00003°
Longitude
-78.2553°
Altitude
518.08 km
Speed
7.602 km/s
True Right ascension
12h 15m 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
22:23:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.968 km
Perigee altitude
503.811 km
Semi-major axis
6,886.026 km
Eccentricity
0.00059
Inclination
97.3978°
RAAN
183.8667°
Arg. of periapsis
175.9801°
True anomaly
184.14329°
Mean anomaly
184.1482°
Eccentric anomaly
184.14575°
Mean motion
3.79831 °/min
Orbital period
94.78 mins
BSTAR
0.000016817
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-14 17:13:32.629Z | 57.911° ENE | 2026-04-14 17:15:32.629Z | 94.185° ESE | 16.265° | 2026-04-14 17:17:32.629Z | 130.138° SE |
| 5 mins | 2026-04-14 18:47:32.629Z | 335.25° NNW | 2026-04-14 18:49:32.629Z | 287.496° WNW | 25.186° | 2026-04-14 18:52:32.629Z | 230.026° WSW |
| 6 mins | 2026-04-15 05:25:32.629Z | 175.258° S | 2026-04-15 05:28:32.629Z | 314.061° NW | 41.72° | 2026-04-15 05:31:32.629Z | 343.959° N |
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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