E-STAR-2, 41459 (Decayed)

Orbit data source: Space-Track

E-STAR-2, 41459 was a payload satellite owned by PolyTorino (IT) in LEO that was launched on Mon, 25 Apr 2016 UTC via a SOYUZ-ST-A launch vehicle from the French Guiana (FRGUI). 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

E-STAR-2 details

Identifier	41459, 2016-025D
Orbit	Decayed
Last TLE update	8 months ago
Origin	PolyTorino (IT)
Manufacturer	PolyTorino
Mission	Decayed Amateur Technology
Bus & Motor	CUBESAT 1U, Unknown motor
Mass	1 kg wet, 1 kg dry
Launch date (UTC)	2016-04-25 (9 years ago)
Launch vehicle	SOYUZ-ST-A
Launch site	French Guiana (FRGUI)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.1 m
Radar Cross Section	0.015 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 8 months ago

0 E-STAR-2
1 41459U 16025D   24126.07714411  .16156611  31653-5  27264-3 0  9991
2 41459  98.0991  14.5477 0007120 232.8921 127.1731 16.47786158442898

Epoch: 2024-05-05T01:51Z

Definitive object data (Epoch: 2024-05-05T01:51:05.251Z)

Latitude	0.00008°
Longitude	123.34122°
Altitude	151.221 km
Speed	7.814 km/s
True Right ascension	00h 58m 11s
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	146.645 km
Perigee altitude	137.36 km
Semi-major axis	6,520.139 km
Eccentricity	0.000712
Inclination	98.0991°
RAAN	14.5477°
Arg. of periapsis	232.8921°
True anomaly	127.23808°
Mean anomaly	127.1731°
Eccentric anomaly	127.20559°
Mean motion	4.12247 °/min
BSTAR	0.00027264
Orbital period	87.33 mins