JAISAT 1, 44419 (Decayed)

Orbit data source: Space-Track

JAISAT 1, 44419 was a payload satellite owned by RAST (TH) 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

JAISAT 1 details

Identifier	44419, 2019-038F
Orbit	Decayed
Last TLE update	7 months ago
Origin	RAST (TH / THAI)
Manufacturer	German Orb Sys
Mission	Decayed Amateur Communications
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 7 months ago

0 JAISAT 1
1 44419U 19038F   24161.30699751  .14138513  27681-5  32002-3 0  9992
2 44419  97.6384 170.8746 0011571 240.3842 119.6307 16.45656077273974

Epoch: 2024-06-09T07:22Z

Definitive object data (Epoch: 2024-06-09T07:22:04.584Z)

Latitude	-0.0001°
Longitude	162.19671°
Altitude	157.794 km
Speed	7.809 km/s
True Right ascension	11h 23m 29s
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	155.162 km
Perigee altitude	140.06 km
Semi-major axis	6,525.748 km
Eccentricity	0.0011571
Inclination	97.6384°
RAAN	170.8746°
Arg. of periapsis	240.3842°
True anomaly	119.74587°
Mean anomaly	119.6307°
Eccentric anomaly	119.68829°
Mean motion	4.11716 °/min
BSTAR	0.00032002
Orbital period	87.44 mins