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). 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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46493 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
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
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 DEKART
1 46493U 20068H 26142.68675870 .00010063 00000-0 28294-3 0 9992
2 46493 97.8753 150.1439 0009602 28.0533 332.1225 15.36683667311855Epoch: 2026-05-22T16:28Z
TLE epoch observation values (Epoch: 2026-05-22T16:28:55.951Z)
Latitude
-0.00008°
Longitude
22.59674°
Altitude
453.223 km
Speed
7.644 km/s
True Right ascension
10h 00m 34s
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
19:19:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.448 km
Perigee altitude
446.329 km
Semi-major axis
6,831.026 km
Eccentricity
0.00096
Inclination
97.8753°
RAAN
150.1439°
Arg. of periapsis
28.0533°
True anomaly
332.071°
Mean anomaly
332.1225°
Eccentric anomaly
332.09675°
Mean motion
3.84427 °/min
Orbital period
93.65 mins
BSTAR
0.00028294
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Other satellites on launch #68 in the year 2020 (2020-09-28 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.DEKART 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-23 13:21:44.135Z | 14.891° NNE | 2026-05-23 13:24:44.135Z | 179.747° S | 41.589° | 2026-05-23 13:26:44.135Z | 190.452° SSW |
| 4 mins | 2026-05-23 23:53:44.135Z | 110.68° ESE | 2026-05-23 23:55:44.135Z | 56.784° ENE | 22.258° | 2026-05-23 23:57:44.135Z | 17.601° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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