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.
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42766 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
Noorul Islam U
Mission
Decayed Amateur Imaging
Bus & Motor
NIUSAT, Unknown motor
Mass
15 kg wet, 15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.189 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast 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 16.37099332381647Epoch: 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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
20:49:26
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
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Other satellites on launch #36 in the year 2017 (2017-06-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NIUSAT Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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