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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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
ENEA/UNF2
Mission
Non-operational Civil Bio/Tech
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: 6 months ago
TLE from 6 months ago
0 MT-CUBE-2
1 53106U 22080B 25119.54530882 -.00000003 00000-0 00000+0 0 9993
2 53106 70.1441 82.5809 0008360 32.9040 327.2139 6.42557753 65597Epoch: 2025-04-29T13:05Z
TLE epoch observation values (Epoch: 2025-04-29T13:05:14.682Z)
Latitude
0°
Longitude
28.52629°
Altitude
5,836.233 km
Speed
5.715 km/s
True Right ascension
05h 30m 19s
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
02:31:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,852.48 km
Perigee altitude
5,832.048 km
Semi-major axis
12,220.401 km
Eccentricity
0.00084
Inclination
70.1441°
RAAN
82.5809°
Arg. of periapsis
32.904°
True anomaly
327.16198°
Mean anomaly
327.2139°
Eccentric anomaly
327.18794°
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. |
|---|---|---|---|---|---|---|---|
| 18 mins | 2025-11-03 06:40:58.945Z | 22.993° NE | 2025-11-03 06:40:58.945Z | 22.993° NE | 36.742° | 2025-11-03 06:58:58.945Z | 26.749° NE |
| 57 mins | 2025-11-03 10:05:58.945Z | 280.099° WNW | 2025-11-03 10:33:58.945Z | 346.625° N | 30.117° | 2025-11-03 11:02:58.945Z | 54.563° ENE |
| 62 mins | 2025-11-03 14:18:58.945Z | 331.172° NNW | 2025-11-03 14:49:58.945Z | 58.799° ENE | 42.084° | 2025-11-03 15:20:58.945Z | 139.293° SSE |
| 50 mins | 2025-11-03 18:15:58.945Z | 329.587° NNW | 2025-11-03 18:39:58.945Z | 276.14° WNW | 30.747° | 2025-11-03 19:05:58.945Z | 217.104° SW |
| 57 mins | 2025-11-04 04:20:58.945Z | 165.067° S | 2025-11-04 04:48:58.945Z | 97.13° ESE | 39.509° | 2025-11-04 05:17:58.945Z | 27.042° NE |
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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