DECAYED
Showing default

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). Payload-class satellites include a variety of spacecraft 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
Identifier
42766, 2017-036B
Orbit
Decayed
Country
Flag of ININ / IND
Related business
Flag of INNoorul Islam Centre for Higher Education (IN)
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, 0.2 m
Radar Cross Section
0.189 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year 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
TLE epoch observation values (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 epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:18:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
177.028 km
Perigee altitude
163.626 km
Semi-major axis
6,548.464 km
Eccentricity
0.00102
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
Orbital period
87.9 mins
BSTAR
0.00090128
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|