D STAR ONE (LIGHTSAT), 44393 (Decayed)

Orbit data source: Space-Track

D STAR ONE (LIGHTSAT), 44393 was a payload satellite owned by German Orb Sys (DE) 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

D STAR ONE (LIGHTSAT) details

Identifier	44393, 2019-038H
Orbit	Decayed
Last TLE update	6 months ago
Origin	German Orb Sys (DE / GER)
Manufacturer	German Orb Sys
Mission	Decayed Commercial 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 + 1 Ant, 0.6 m
Radar Cross Section	0.093 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 6 months ago

0 D STAR ONE (LIGHTSAT)
1 44393U 19038H   24158.74650028  .17230582  28215-5  20417-3 0  9994
2 44393  97.6364 167.6855 0010284 238.2250 121.8052 16.49618950273555

Epoch: 2024-06-06T17:54Z

Definitive object data (Epoch: 2024-06-06T17:54:57.624Z)

Latitude	-0.00006°
Longitude	3.31035°
Altitude	147.135 km
Speed	7.816 km/s
True Right ascension	11h 10m 44s
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	143.845 km
Perigee altitude	130.445 km
Semi-major axis	6,515.282 km
Eccentricity	0.0010284
Inclination	97.6364°
RAAN	167.6855°
Arg. of periapsis	238.225°
True anomaly	121.90528°
Mean anomaly	121.8052°
Eccentric anomaly	121.85525°
Mean motion	4.12708 °/min
BSTAR	0.00020417
Orbital period	87.23 mins