TYVAK-0129, 44853 (Decayed)

Orbit data source: Space-Track

TYVAK-0129, 44853 was a payload satellite owned by Tyvak NSS (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-0129 details

Identifier	44853, 2019-089B
Orbit	Decayed
Last TLE update	3 months ago
Origin	Tyvak NSS (US)
Manufacturer	Tyvak NSS
Mission	Decayed Commercial Technology
Bus & Motor	CUBESAT 6U, Unknown motor
Mass	11 kg wet, 11 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	0.077 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 3 months ago

0 TYVAK-0129
1 44853U 19089B   24268.55600073  .13853753  37346-5  17063-2 0  9991
2 44853  36.9359  64.2361 0007440 313.4482  46.5684 16.35014491264440

Epoch: 2024-09-24T13:20Z

Definitive object data (Epoch: 2024-09-24T13:20:38.463Z)

Latitude	0.00002°
Longitude	-139.79263°
Altitude	174.816 km
Speed	7.806 km/s
True Right ascension	04h 16m 56s
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	187.063 km
Perigee altitude	177.301 km
Semi-major axis	6,560.319 km
Eccentricity	0.000744
Inclination	36.9359°
RAAN	64.2361°
Arg. of periapsis	313.4482°
True anomaly	46.63035°
Mean anomaly	46.5684°
Eccentric anomaly	46.59937°
Mean motion	4.08466 °/min
BSTAR	0.0017063
Orbital period	88.13 mins