TYVAK-0092, 44852 (Decayed)

Orbit data source: Space-Track

TYVAK-0092, 44852 was a payload satellite owned by Elbit Systems (US) in LEO that was launched on Wed, 11 Dec 2019 UTC via a PSLV-QL launch vehicle from the Sirharikota (SRI). 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

TYVAK-0092 details

Identifier	44852, 2019-089A
Orbit	Decayed
Last TLE update	2 months ago
Origin	Elbit Systems (US)
Manufacturer	Tyvak Intl
Mission	Decayed Commercial Communications
Bus & Motor	CUBESAT 3U, Unknown motor
Mass	4 kg wet, 4 kg dry
Launch date (UTC)	2019-12-11 (5 years ago)
Launch vehicle	PSLV-QL
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, Unknown HBR
Radar Cross Section	0.035 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 months ago

0 TYVAK-0092
1 44852U 19089A   24276.54381567  .07513138  36447-5  30607-2 0  9995
2 44852  36.9114  19.7052 0009890  30.3005 329.8345 16.22156038265506

Epoch: 2024-10-02T13:03Z

Definitive object data (Epoch: 2024-10-02T13:03:05.673Z)

Latitude	-0.00008°
Longitude	172.18979°
Altitude	207.142 km
Speed	7.788 km/s
True Right ascension	01h 18m 49s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow 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	223.298 km
Perigee altitude	210.254 km
Semi-major axis	6,594.913 km
Eccentricity	0.000989
Inclination	36.9114°
RAAN	19.7052°
Arg. of periapsis	30.3005°
True anomaly	329.77749°
Mean anomaly	329.8345°
Eccentric anomaly	329.806°
Mean motion	4.05256 °/min
BSTAR	0.0030607
Orbital period	88.83 mins