INSAT 2B, 22724
Orbit data source: Space-Track
INSAT 2B, 22724 is a payload satellite owned by ISRO (IN) in GEO that was launched on Thu, 22 Jul 1993 UTC via an ARIANE 44L launch vehicle from the French Guiana (FRGUI). 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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22724 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Non-operational Civil Com/Cal
Bus & Motor
I2K, ISRO LAM
Mass
1,931 kg wet, 916 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Poly + 1 Pan, 11.5 m
Radar Cross Section
14.695 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 INSAT 2B
1 22724U 93048B 26093.04281049 -.00000079 00000-0 00000+0 0 9995
2 22724 14.4288 3.1627 0015779 230.4899 333.7897 0.99986418119824Epoch: 2026-04-03T01:01Z
TLE epoch observation values (Epoch: 2026-04-03T01:01:38.826Z)
Latitude
-5.87515°
Longitude
-0.08749°
Altitude
35,807.3 km
Speed
3.076 km/s
True Right ascension
13h 46m 49s
True Declination
-5° 52' 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
06:26:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,934.415 km
Perigee altitude
35,801.095 km
Semi-major axis
42,245.892 km
Eccentricity
0.00158
Inclination
14.4288°
RAAN
3.1627°
Arg. of periapsis
230.4899°
True anomaly
333.7097°
Mean anomaly
333.7897°
Eccentric anomaly
333.74971°
Mean motion
0.24996 °/min
Orbital period
1,440.24 mins
BSTAR
0
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Other satellites on launch #48 in the year 1993 (1993-07-22 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 2B 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. |
|---|---|---|---|---|---|---|---|
| INSAT 2B is likely not visible in the next few days. |
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22724 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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