NARSSCUBE-2, 44415 (Decayed)

Orbit data source: Space-Track

NARSSCUBE-2, 44415 was a payload satellite owned by EgSA (EG) in LEO that was launched on Wed, 17 Apr 2019 UTC via an FALCON 9 launch vehicle from the Wallops Island (WLPIS). 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

NARSSCUBE-2 details

Identifier	44415, 2019-022E
Orbit	Decayed
Last TLE update	9 months ago
Origin	EgSA (EG / EGYP)
Manufacturer	EgSA
Mission	Decayed Civil Technology
Bus & Motor	CUBESAT 1U, Unknown motor
Mass	1 kg wet, 1 kg dry
Launch date (UTC)	2019-04-17 (6 years ago)
Launch vehicle	FALCON 9
Launch site	Wallops Island (WLPIS)
Object type	Payload Rocket body Debris
Shape & HBR	Box, Unknown HBR
Radar Cross Section	0.015 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 9 months ago

0 NARSSCUBE-2
1 44415U 19022E   24092.07861115  .12359287  12624-4  24570-3 0  9995
2 44415  51.6010 111.7418 0002972 304.4343  55.6405 16.47098938261589

Epoch: 2024-04-01T01:53Z

Definitive object data (Epoch: 2024-04-01T01:53:12.003Z)

Latitude	-0.00002°
Longitude	-106.48225°
Altitude	146.66 km
Speed	7.82 km/s
True Right ascension	07h 26m 58s
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	149.461 km
Perigee altitude	145.582 km
Semi-major axis	6,525.659 km
Eccentricity	0.0002972
Inclination	51.601°
RAAN	111.7418°
Arg. of periapsis	304.4343°
True anomaly	55.66862°
Mean anomaly	55.6405°
Eccentric anomaly	55.65456°
Mean motion	4.11724 °/min
BSTAR	0.0002457
Orbital period	87.44 mins