ASTROSAT, 40930
Orbit data source: Space-Track
ASTROSAT, 40930 is a payload satellite owned by ISRO (IN) in LEO that was launched on Mon, 28 Sep 2015 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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40930 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ASTROSAT
1 40930U 15052A 25241.04709133 .00002365 00000-0 21104-3 0 9997
2 40930 5.9975 96.8872 0008182 189.5573 170.4399 14.81588557536414
Epoch: 2025-08-29T01:07Z
TLE epoch observation values (Epoch: 2025-08-29T01:07:48.69Z)
Latitude
-0.00001°
Longitude
102.4329°
Altitude
626.9 km
Speed
7.545 km/s
True Right ascension
06h 27m 32s
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
15:57:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.244 km
Perigee altitude
624.775 km
Semi-major axis
7,008.646 km
Eccentricity
0.00082
Inclination
5.9975°
RAAN
96.8872°
Arg. of periapsis
189.5573°
True anomaly
170.45546°
Mean anomaly
170.4399°
Eccentric anomaly
170.44768°
Mean motion
3.69907 °/min
Orbital period
97.32 mins
BSTAR
0.00021104
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Other satellites on launch #52 in the year 2015 (2015-09-28 UTC)
ASTROSAT Visibility
Observer location: undefined°, undefined°
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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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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