INSAT 3DS, 58990
Orbit data source: Space-Track
INSAT 3DS, 58990 is a payload satellite owned by ISRO (IN) in GEO that was launched on Sat, 17 Feb 2024 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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58990 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
2,275 kg wet, ~960 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: 1 day ago
TLE from 1 day ago
0 INSAT 3DS
1 58990U 24033A 26141.56086498 -.00000163 00000-0 00000+0 0 9993
2 58990 0.0408 253.6125 0001314 159.2939 110.2599 1.00269889 46804Epoch: 2026-05-21T13:27Z
TLE epoch observation values (Epoch: 2026-05-21T13:27:38.734Z)
Latitude
-0.0507°
Longitude
82.069°
Altitude
35,788.544 km
Speed
3.075 km/s
True Right ascension
10h 52m 44s
True Declination
0° 03' 02"
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
01:03:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,793.738 km
Perigee altitude
35,782.656 km
Semi-major axis
42,166.334 km
Eccentricity
0.00013
Inclination
0.0408°
RAAN
253.6125°
Arg. of periapsis
159.2939°
True anomaly
110.27402°
Mean anomaly
110.2599°
Eccentric anomaly
110.26696°
Mean motion
0.25067 °/min
Orbital period
1,436.18 mins
BSTAR
0
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Other satellites on launch #33 in the year 2024 (2024-02-17 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 3DS 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 3DS is likely not visible in the next few days. |
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58990 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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