AMGU-1 (AMURSAT), 44394 (Decayed)

Orbit data source: Space-Track

AMGU-1 (AMURSAT), 44394 was a payload satellite owned by AmGU (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

AMGU-1 (AMURSAT) details

Identifier	44394, 2019-038J
Orbit	Decayed
Last TLE update	8 months ago
Origin	AmGU (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 8 months ago

0 AMGU-1 (AMURSAT)
1 44394U 19038J   24125.75384495  .12668029  27460-5  42747-3 0  9999
2 44394  97.6493 133.6124 0012922 237.3428 122.6626 16.43402849268528

Epoch: 2024-05-04T18:05Z

Definitive object data (Epoch: 2024-05-04T18:05:32.203Z)

Latitude	-0.00008°
Longitude	-0.8877°
Altitude	164.58 km
Speed	7.805 km/s
True Right ascension	08h 54m 26s
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	162.021 km
Perigee altitude	145.14 km
Semi-major axis	6,531.718 km
Eccentricity	0.0012922
Inclination	97.6493°
RAAN	133.6124°
Arg. of periapsis	237.3428°
True anomaly	122.78715°
Mean anomaly	122.6626°
Eccentric anomaly	122.72489°
Mean motion	4.11152 °/min
BSTAR	0.00042747
Orbital period	87.56 mins