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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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO SAC/Banga
Mission
Operational Civil Astronomy
Bus & Motor
ASTROSAT, AOCS
Mass
1,513 kg wet, 1,470 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.5 m
Radar Cross Section
5.447 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ASTROSAT
1 40930U 15052A 26171.05152111 .00001334 00000-0 80735-4 0 9990
2 40930 5.9956 134.7258 0007591 74.7193 285.3774 14.82511277580259Epoch: 2026-06-20T01:14Z
TLE epoch observation values (Epoch: 2026-06-20T01:14:11.423Z)
Latitude
-0°
Longitude
-152.09352°
Altitude
616.941 km
Speed
7.555 km/s
True Right ascension
08h 58m 54s
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
21:34:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.924 km
Perigee altitude
622.288 km
Semi-major axis
7,005.743 km
Eccentricity
0.00076
Inclination
5.9956°
RAAN
134.7258°
Arg. of periapsis
74.7193°
True anomaly
285.29351°
Mean anomaly
285.3774°
Eccentric anomaly
285.33546°
Mean motion
3.70136 °/min
Orbital period
97.26 mins
BSTAR
0.000080735
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Other satellites on launch #52 in the year 2015 (2015-09-28 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.ASTROSAT 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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| ASTROSAT is likely not visible in the next few days. |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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