GSAT 6A, 43241
Orbit data source: Space-Track
GSAT 6A, 43241 is a payload satellite owned by ISRO (IN) that was launched on Thu, 29 Mar 2018 UTC via a GSLV MK II 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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43241 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Non-operational Defense Communications
Bus & Motor
I2K, ISRO LAM
Mass
2,230 kg wet, 976 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 4.8 m
Radar Cross Section
8.526 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 GSAT 6A
1 43241U 18027A 26266.91428187 -.00000144 00000-0 00000-0 0 9994
2 43241 3.4514 79.3037 1322951 117.1732 229.9893 1.19317025 37031Epoch: 2026-09-23T21:56Z
TLE epoch observation values (Epoch: 2026-09-23T21:56:33.953Z)
Latitude
-1.38723°
Longitude
84.10149°
Altitude
34,708.729 km
Speed
2.964 km/s
True Right ascension
03h 44m 00s
True Declination
-1° 23' 09"
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
20:46:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,139.976 km
Perigee altitude
26,204.513 km
Semi-major axis
37,550.381 km
Eccentricity
0.1323
Inclination
3.4514°
RAAN
79.3037°
Arg. of periapsis
117.1732°
True anomaly
219.55455°
Mean anomaly
229.9893°
Eccentric anomaly
224.66125°
Mean motion
0.29828 °/min
Orbital period
1,206.93 mins
BSTAR
0
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Other satellites on launch #27 in the year 2018 (2018-03-29 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.GSAT 6A 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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| GSAT 6A 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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