CARTOSAT 2F, 43111
Orbit data source: Space-Track
CARTOSAT 2F, 43111 is a payload satellite owned by ISRO (IN) in SSO that was launched on Fri, 12 Jan 2018 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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43111 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Operational Defense Imaging
Bus & Motor
IRS-2, AOCS
Mass
712 kg wet, 639 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 2 Pan, 4.0 m
Radar Cross Section
9.780 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CARTOSAT 2F
1 43111U 18004A 26251.92259859 .00002546 00000-0 12411-3 0 9997
2 43111 97.4715 310.6998 0001452 23.4315 336.6986 15.19239932480042Epoch: 2026-09-08T22:08Z
TLE epoch observation values (Epoch: 2026-09-08T22:08:32.518Z)
Latitude
0.00005°
Longitude
-9.41776°
Altitude
510.305 km
Speed
7.609 km/s
True Right ascension
20h 42m 47s
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
20:18:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.106 km
Perigee altitude
504.107 km
Semi-major axis
6,883.243 km
Eccentricity
0.00015
Inclination
97.4715°
RAAN
310.6998°
Arg. of periapsis
23.4315°
True anomaly
336.69202°
Mean anomaly
336.6986°
Eccentric anomaly
336.69531°
Mean motion
3.80061 °/min
Orbital period
94.72 mins
BSTAR
0.00012411
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Other satellites on launch #4 in the year 2018 (2018-01-12 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.CARTOSAT 2F Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-09 04:35:49.751Z | 205.687° SW | 2026-09-09 04:37:49.751Z | 249.16° W | 32.155° | 2026-09-09 04:40:49.751Z | 321.935° NNW |
| 4 mins | 2026-09-09 16:07:49.751Z | 68.862° E | 2026-09-09 16:08:49.751Z | 91.297° ESE | 21.475° | 2026-09-09 16:11:49.751Z | 146.085° SSE |
| 4 mins | 2026-09-09 17:40:49.751Z | 331.311° NNW | 2026-09-09 17:42:49.751Z | 289.372° WNW | 22.791° | 2026-09-09 17:44:49.751Z | 248.054° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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