VDNH 80, 44392 (Decayed)

Orbit data source: Space-Track

VDNH 80, 44392 was a payload satellite owned by VDNKh (CIS) in LEO that was launched on Fri, 05 Jul 2019 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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.

Not visible in the next 10 days

VDNH 80 details

Identifier	44392, 2019-038G
Orbit	Decayed
Last TLE update	6 months ago
Origin	VDNKh (CIS)
Manufacturer	MGU
Mission	Decayed Amateur Technology
Bus & Motor	CUBESAT 3U, Unknown motor
Mass	3 kg wet, 3 kg dry
Launch date (UTC)	2019-07-05 (5 years ago)
Launch vehicle	SOYUZ-2-1B
Launch site	Vostochny Cosmodrome (VOSTO)
Object type	Payload Rocket body Debris
Shape & HBR	Box, Unknown HBR
Radar Cross Section	0.035 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 6 months ago

0 VDNH 80
1 44392U 19038G   24173.42682560  .14692379  27627-5  27521-3 0  9993
2 44392  97.6413 182.7271 0012680 243.0641 116.9366 16.46585171275672

Epoch: 2024-06-21T10:14Z

Definitive object data (Epoch: 2024-06-21T10:14:37.731Z)

Latitude	-0.00008°
Longitude	118.96522°
Altitude	155.354 km
Speed	7.811 km/s
True Right ascension	12h 10m 54s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	153.425 km
Perigee altitude	136.882 km
Semi-major axis	6,523.291 km
Eccentricity	0.001268
Inclination	97.6413°
RAAN	182.7271°
Arg. of periapsis	243.0641°
True anomaly	117.06604°
Mean anomaly	116.9366°
Eccentric anomaly	117.00133°
Mean motion	4.11949 °/min
BSTAR	0.00027521
Orbital period	87.39 mins