NIUSAT, 42766 (Decayed)

Orbit data source: Space-Track

NIUSAT, 42766 was a payload satellite owned by Noorul Islam U (IN) in LEO that was launched on Fri, 23 Jun 2017 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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

NIUSAT details

Identifier	42766, 2017-036B
Orbit	Decayed
Last TLE update	8 months ago
Origin	Noorul Islam U (IN / IND)
Manufacturer	Noorul Islam U
Mission	Decayed Amateur Imaging
Bus & Motor	NIUSAT, Unknown motor
Mass	15 kg wet, 15 kg dry
Launch date (UTC)	2017-06-23 (8 years ago)
Launch vehicle	PSLV-XL
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.37 m
Radar Cross Section	0.189 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 8 months ago

0 NIUSAT
1 42766U 17036B   24118.29613428  .08122670  23474-5  90128-3 0  9997
2 42766  97.0758 154.7708 0010233 252.0492 107.9692 16.37099332381647

Epoch: 2024-04-27T07:06Z

Definitive object data (Epoch: 2024-04-27T07:06:26.001Z)

Latitude	-0°
Longitude	-167.60279°
Altitude	178.862 km
Speed	7.798 km/s
True Right ascension	10h 19m 04s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow 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	177.028 km
Perigee altitude	163.626 km
Semi-major axis	6,548.464 km
Eccentricity	0.0010233
Inclination	97.0758°
RAAN	154.7708°
Arg. of periapsis	252.0492°
True anomaly	108.0807°
Mean anomaly	107.9692°
Eccentric anomaly	108.02495°
Mean motion	4.09576 °/min
BSTAR	0.00090128
Orbital period	87.9 mins