DECAYED
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YARILO-1, 46490 (Decayed)

Orbit data source: Space-Track

YARILO-1, 46490 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
46490, 2020-068E
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: 9 months ago

TLE from 9 months ago
0 YARILO-1
1 46490U 20068E   25066.35364862  .10022604  28760-5  11298-2 0  9991
2 46490  97.8124  62.1734 0007670 207.0829 153.0069 16.37034918245633
Epoch: 2025-03-07T08:29Z
TLE epoch observation values (Epoch: 2025-03-07T08:29:15.240Z)
Latitude
0.00001°
Longitude
129.54468°
Altitude
181.416 km
Speed
7.795 km/s
True Right ascension
04h 08m 41s
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
17:52:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
175.555 km
Perigee altitude
165.51 km
Semi-major axis
6,548.669 km
Eccentricity
0.00077
Inclination
97.8124°
RAAN
62.1734°
Arg. of periapsis
207.0829°
True anomaly
153.04676°
Mean anomaly
153.0069°
Eccentric anomaly
153.02683°
Mean motion
4.09556 °/min
Orbital period
87.9 mins
BSTAR
0.0011298
Loading maneuver chart data...
Computing Atmospheric mass density...

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