DECAYED
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YARILO-2, 46491 (Decayed)

Orbit data source: Space-Track

YARILO-2, 46491 was a payload satellite owned by MGTU Bauman (CIS) in LEO 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.

Not visible in the next 10 days
Identifier
46491, 2020-068F
Orbit
Decayed
Country
Flag of CISCIS
Related business
Flag of RUMoscow State Technical University of Civil Aviation (RU)
Manufacturer
MGTU Bauman
Mission
Decayed Amateur Science
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
2020-09-28 (5 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, Unknown HBR
Radar Cross Section
0.025 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 months ago

TLE from 10 months ago
0 YARILO-2
1 46491U 20068F   25039.82307463  .09519039  28755-5  10124-2 0  9990
2 46491  97.7749  32.6421 0006725 182.3651 177.7615 16.37592311241495
Epoch: 2025-02-08T19:45Z
TLE epoch observation values (Epoch: 2025-02-08T19:45:13.648Z)
Latitude
-0.00003°
Longitude
-42.83019°
Altitude
179.855 km
Speed
7.796 km/s
True Right ascension
02h 10m 34s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
00:48:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
173.446 km
Perigee altitude
164.64 km
Semi-major axis
6,547.18 km
Eccentricity
0.00067
Inclination
97.7749°
RAAN
32.6421°
Arg. of periapsis
182.3651°
True anomaly
177.76451°
Mean anomaly
177.7615°
Eccentric anomaly
177.763°
Mean motion
4.09696 °/min
Orbital period
87.87 mins
BSTAR
0.0010124
Loading maneuver chart data...
Computing Atmospheric mass density...

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