NSL-1, 44391 (Decayed)

Orbit data source: Space-Track

NSL-1, 44391 was an Israeli payload satellite 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

NSL-1 details

Identifier	44391, 2019-038E
Orbit	Decayed
Last TLE update	5 months ago
Origin	NSLC/CLAAC (IL / ISRA)
Manufacturer	AAC ClydeSpace
Mission	Decayed Commercial Technology
Bus & Motor	CUBESAT 6U, Unknown motor
Mass	10 kg wet, 10 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 Dish, 1 m
Radar Cross Section	0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 5 months ago

0 NSL-1
1 44391U 19038E   24218.25224336  .15623426  28611-5  15061-2 0  9993
2 44391  97.8531 233.2807 0011701 237.5528 122.4638 16.38276424279796

Epoch: 2024-08-05T06:03Z

Definitive object data (Epoch: 2024-08-05T06:03:13.826Z)

Latitude	-0.00004°
Longitude	-171.81364°
Altitude	177.747 km
Speed	7.797 km/s
True Right ascension	15h 33m 07s
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	174.881 km
Perigee altitude	159.564 km
Semi-major axis	6,545.359 km
Eccentricity	0.0011701
Inclination	97.8531°
RAAN	233.2807°
Arg. of periapsis	237.5528°
True anomaly	122.57684°
Mean anomaly	122.4638°
Eccentric anomaly	122.52033°
Mean motion	4.09867 °/min
BSTAR	0.0015061
Orbital period	87.83 mins