AISTECHSAT-3, 44103 (Decayed)
Orbit data source: Space-Track
AISTECHSAT-3, 44103 was a payload satellite owned by AISTech (ES) in LEO that was launched on Mon, 01 Apr 2019 UTC via a PSLV-QL 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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44103 intel report (Beta)
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AISTECHSAT-3 radio frequencies
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Edit Public Description
Identifier
Orbit
Last TLE update
1 year ago
Origin
Manufacturer
AISTech
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
2.3 kg wet, 2.3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.040 m², Small (<0.1 m²)
Expand to show TLE details & history
TLE from 1 year ago
0 AISTECHSAT-3
1 44103U 19018AB 24110.23946520 .15151224 24602-5 24815-3 0 9993
2 44103 97.1722 178.6502 0011750 259.7908 100.2071 16.47479668282343Epoch: 2024-04-19T05:44Z
TLE epoch observation values (Epoch: 2024-04-19T05:44:49.793Z)
Latitude
-0.00002°
Longitude
-115.38149°
Altitude
150.616 km
Speed
7.815 km/s
True Right ascension
11h 54m 36s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
Orbital elements
Apogee altitude
150.431 km
Perigee altitude
135.107 km
Semi-major axis
6,520.906 km
Eccentricity
0.00118
Inclination
97.1722°
RAAN
178.6502°
Arg. of periapsis
259.7908°
True anomaly
100.33958°
Mean anomaly
100.2071°
Eccentric anomaly
100.27334°
Mean motion
4.12175 °/min
Orbital period
87.34 mins
BSTAR
0.00024815
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Other satellites on launch #18 in the year 2019 (2019-04-01 UTC)
AISTECHSAT-3 Visibility
Observer location: undefined°, undefined°
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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