DEKART, 46493
Orbit data source: Space-Track
DEKART, 46493 is a payload satellite owned by MGU (CIS) in SSO that was launched on Mon, 28 Sep 2020 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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46493 intel report (Beta)
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DEKART radio frequencies
DEKART details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 8 hours ago |
| Origin | |
| Manufacturer | MGU |
| Mission | Operational Amateur 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, Unknown HBR |
| Radar Cross Section | 0.035 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 DEKART
1 46493U 20068H 24361.20381921 .00018379 00000-0 81403-3 0 9991
2 46493 97.8399 328.3506 0014031 22.1800 338.0038 15.21609554233520Epoch: 2024-12-26T04:53Z
Definitive object data (Epoch: 2024-12-26T04:53:29.979Z)
| Latitude | -0.00013° |
| Longitude | 159.78913° |
| Altitude | 495.115 km |
| Speed | 7.622 km/s |
| True Right ascension | 21h 53m 24s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 75.29264° |
| Longitude | 11.5967° |
| Altitude | 512.377 km |
| Speed | 7.615 km/s |
| Apparent Right ascension | 00h 54m 43s |
| Apparent Declination | 39° 00' 11" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 12:35:30 |
| Azimuth | 356.199° N |
| Elevation | -10.959° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 507.616 km |
| Perigee altitude | 488.32 km |
| Semi-major axis | 6,876.105 km |
| Eccentricity | 0.0014031 |
| Inclination | 97.8399° |
| RAAN | 328.3506° |
| Arg. of periapsis | 22.18° |
| True anomaly | 337.94348° |
| Mean anomaly | 338.0038° |
| Eccentric anomaly | 337.97365° |
| Mean motion | 3.80653 °/min |
| BSTAR | 0.00081403 |
| Orbital period | 94.57 mins |
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Other satellites on launch #68 in the year 2020 (2020-09-28 UTC)
DEKART 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-26 22:23:52.079Z | 198.632° SSW | 2024-12-26 22:25:52.079Z | 280.703° WNW | 35.982° | 2024-12-26 22:28:52.079Z | 335.353° NNW |
| 5 mins | 2024-12-27 11:26:52.079Z | 343.48° N | 2024-12-27 11:28:52.079Z | 291.459° WNW | 30.392° | 2024-12-27 11:31:52.079Z | 223.869° SW |
Authenticating...
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