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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 DEKART
1 46493U 20068H 25260.91929554 .00010707 00000-0 38099-3 0 9998
2 46493 97.8670 247.4449 0011804 156.0524 204.1266 15.29104118274046Epoch: 2025-09-17T22:03Z
TLE epoch observation values (Epoch: 2025-09-17T22:03:47.134Z)
Latitude
-0.00004°
Longitude
-80.58982°
Altitude
488.968 km
Speed
7.616 km/s
True Right ascension
16h 29m 46s
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
23:20:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.553 km
Perigee altitude
467.373 km
Semi-major axis
6,853.6 km
Eccentricity
0.00118
Inclination
97.867°
RAAN
247.4449°
Arg. of periapsis
156.0524°
True anomaly
204.07138°
Mean anomaly
204.1266°
Eccentric anomaly
204.09898°
Mean motion
3.8253 °/min
Orbital period
94.11 mins
BSTAR
0.00038099
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 11:12:33.893Z | 57.126° ENE | 2025-09-18 11:14:33.893Z | 94.418° ESE | 15.803° | 2025-09-18 11:16:33.893Z | 131.834° SE |
| 4 mins | 2025-09-18 12:46:33.893Z | 323.38° NNW | 2025-09-18 12:47:33.893Z | 297.634° NW | 23.036° | 2025-09-18 12:50:33.893Z | 234.111° WSW |
| 5 mins | 2025-09-18 23:19:33.893Z | 174.745° S | 2025-09-18 23:21:33.893Z | 204.166° SW | 41.797° | 2025-09-18 23:24:33.893Z | 341.618° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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