INSAT 3DR, 41752
Orbit data source: Space-Track
INSAT 3DR, 41752 is a payload satellite owned by ISRO (IN) in GEO that was launched on Thu, 08 Sep 2016 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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41752 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Operational Civil Weather
Bus & Motor
I2K, ISRO LAM
Mass
2,211 kg wet, 956 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: 7 hours ago
TLE from 7 hours ago
0 INSAT 3DR
1 41752U 16054A 26296.86296196 -.00000065 00000-0 00000-0 0 9999
2 41752 0.1312 85.4678 0012909 180.2751 151.2196 1.00271727 37104Epoch: 2026-10-23T20:42Z
TLE epoch observation values (Epoch: 2026-10-23T20:42:39.913Z)
Latitude
-0.06893°
Longitude
74.04967°
Altitude
35,833.787 km
Speed
3.071 km/s
True Right ascension
03h 47m 58s
True Declination
0° 04' 08"
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
22:41:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,842.113 km
Perigee altitude
35,733.25 km
Semi-major axis
42,165.819 km
Eccentricity
0.00129
Inclination
0.1312°
RAAN
85.4678°
Arg. of periapsis
180.2751°
True anomaly
151.29072°
Mean anomaly
151.2196°
Eccentric anomaly
151.25517°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #54 in the year 2016 (2016-09-08 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.INSAT 3DR 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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| INSAT 3DR is likely not visible in the next few days. |
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41752 neighbors
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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
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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