MT-CUBE-2, 53106
Orbit data source: Space-Track
MT-CUBE-2, 53106 is a French payload satellite that was launched on Wed, 13 Jul 2022 UTC via a VEGA C 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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53106 intel report (Beta)
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MT-CUBE-2 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
ENEA/UNF2
Mission
Non-operational Civil Science
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 MT-CUBE-2
1 53106U 22080B 25051.21822557 -.00000003 00000-0 00000+0 0 9995
2 53106 70.1434 106.3440 0008542 48.0089 312.1297 6.42557744 61200Epoch: 2025-02-20T05:14Z
TLE epoch observation values (Epoch: 2025-02-20T05:14:14.689Z)
Latitude
-0.00002°
Longitude
-122.61424°
Altitude
5,837.822 km
Speed
5.714 km/s
True Right ascension
07h 05m 22s
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
07:31:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,852.703 km
Perigee altitude
5,831.826 km
Semi-major axis
12,220.401 km
Eccentricity
0.00085
Inclination
70.1434°
RAAN
106.344°
Arg. of periapsis
48.0089°
True anomaly
312.05705°
Mean anomaly
312.1297°
Eccentric anomaly
312.09338°
Mean motion
1.60663 °/min
Orbital period
224.07 mins
BSTAR
0
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Other satellites on launch #80 in the year 2022 (2022-07-13 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.MT-CUBE-2 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. |
|---|---|---|---|---|---|---|---|
| 60 mins | 2025-09-18 16:08:27.937Z | 311.912° NW | 2025-09-18 16:38:27.937Z | 22.388° NNE | 31.674° | 2025-09-18 17:08:27.937Z | 93.343° ESE |
| 61 mins | 2025-09-18 20:12:27.937Z | 333.728° NNW | 2025-09-18 20:42:27.937Z | 249.947° W | 44.415° | 2025-09-18 21:13:27.937Z | 173.42° S |
| 12 mins | 2025-09-19 00:18:27.937Z | 305.44° NW | 2025-09-19 00:24:27.937Z | 293.159° NW | 11.245° | 2025-09-19 00:30:27.937Z | 280.909° WNW |
| 34 mins | 2025-09-19 06:37:27.937Z | 109.822° ESE | 2025-09-19 06:54:27.937Z | 73.061° E | 19.093° | 2025-09-19 07:11:27.937Z | 37.335° NE |
| 62 mins | 2025-09-19 10:09:27.937Z | 200.137° SSW | 2025-09-19 10:39:27.937Z | 290.44° WNW | 44.928° | 2025-09-19 11:11:27.937Z | 27.049° NE |
| 20 mins | 2025-09-19 14:20:27.937Z | 285.594° WNW | 2025-09-19 14:40:27.937Z | 328.518° NNW | 28.166° | 2025-09-19 14:40:27.937Z | 328.518° NNW |
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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