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). Payloads include a variety of satellites, spacecraft, and rockets 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
MT-CUBE-2 details
| Identifier | |
| Orbit | Active |
| Last TLE update | 20 hours ago |
| Origin | |
| Manufacturer | ENEA/UNF2 |
| Mission | 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 | Payload Rocket body Debris |
| Shape & HBR | Box, 0.3 m |
| Radar Cross Section | 0.035 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 20 hours ago
0 MT-CUBE-2
1 53106U 22080B 24346.40082951 -.00000003 00000-0 00000+0 0 9998
2 53106 70.1337 130.9545 0008301 67.0662 293.0873 6.42557702 56656Epoch: 2024-12-11T09:37Z
Definitive object data (Epoch: 2024-12-11T09:37:11.669Z)
| Latitude | -0.00002° |
| Longitude | -93.94018° |
| Altitude | 5,840.85 km |
| Speed | 5.713 km/s |
| True Right ascension | 08h 43m 49s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 51.09286° |
| Longitude | 59.2693° |
| Altitude | 5,845.368 km |
| Speed | 5.715 km/s |
| Apparent Right ascension | 17h 48m 56s |
| Apparent Declination | 24° 49' 43" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 04:00:13 |
| Azimuth | 333.734° NNW |
| Elevation | -20.474° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 5,852.41 km |
| Perigee altitude | 5,832.121 km |
| Semi-major axis | 12,220.402 km |
| Eccentricity | 0.0008301 |
| Inclination | 70.1337° |
| RAAN | 130.9545° |
| Arg. of periapsis | 67.0662° |
| True anomaly | 292.99976° |
| Mean anomaly | 293.0873° |
| Eccentric anomaly | 293.04353° |
| Mean motion | 1.60663 °/min |
| BSTAR | Unknown |
| Orbital period | 224.07 mins |
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Other satellites on launch #80 in the year 2022 (2022-07-13 UTC)
| LARES-2, 53105 |
| MT-CUBE-2, 53106 |
| OBJECT C, 53107 |
| TRISAT-R, 53108 |
| AVUM R/B, 53109 |
| ALPHA, 53110 |
| CELESTA, 53111 |
| OBJECT H, 53112 |
MT-CUBE-2 Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 45 mins | 2024-12-12 08:04:01.661Z | 130.77° SE | 2024-12-12 08:27:01.661Z | 79.733° E | 25.955° | 2024-12-12 08:49:01.661Z | 32.129° NE |
| 62 mins | 2024-12-12 11:45:01.661Z | 212.353° SW | 2024-12-12 12:15:01.661Z | 296.562° NW | 43.742° | 2024-12-12 12:47:01.661Z | 28.312° NE |
| 57 mins | 2024-12-12 16:00:01.661Z | 298.045° NW | 2024-12-12 16:28:01.661Z | 3.944° NNE | 29.379° | 2024-12-12 16:57:01.661Z | 71.418° E |
| 63 mins | 2024-12-12 20:07:01.661Z | 332.863° NNW | 2024-12-12 20:38:01.661Z | 60.301° ENE | 44.638° | 2024-12-12 21:10:01.661Z | 155.667° SSE |
| 39 mins | 2024-12-13 00:06:01.661Z | 323.971° NNW | 2024-12-13 00:25:01.661Z | 283.099° WNW | 21.755° | 2024-12-13 00:45:01.661Z | 240.06° WSW |
Authenticating...
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