CARTOSAT 2E, 42767
Orbit data source: Space-Track
CARTOSAT 2E, 42767 is a payload satellite owned by ISRO (IN) in SSO that was launched on Fri, 23 Jun 2017 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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42767 intel report (Beta)
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Edit Public Description
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: 14 hours ago
TLE from 14 hours ago
0 CARTOSAT 2E
1 42767U 17036C 25287.89854733 .00006610 00000-0 31618-3 0 9999
2 42767 97.4641 346.2226 0003810 81.2411 278.9255 15.19311530460909Epoch: 2025-10-14T21:33Z
TLE epoch observation values (Epoch: 2025-10-14T21:33:54.489Z)
Latitude
-0.00001°
Longitude
-0.9348°
Altitude
510.602 km
Speed
7.609 km/s
True Right ascension
23h 04m 53s
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
06:17:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.512 km
Perigee altitude
502.267 km
Semi-major axis
6,883.026 km
Eccentricity
0.00038
Inclination
97.4641°
RAAN
346.2226°
Arg. of periapsis
81.2411°
True anomaly
278.88237°
Mean anomaly
278.9255°
Eccentric anomaly
278.90393°
Mean motion
3.80079 °/min
Orbital period
94.72 mins
BSTAR
0.00031618
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Other satellites on launch #36 in the year 2017 (2017-06-23 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 2E 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-15 17:05:19.029Z | 3.291° NNE | 2025-10-15 17:08:19.029Z | 307.029° NW | 40.263° | 2025-10-15 17:11:19.029Z | 207.814° SW |
| 5 mins | 2025-10-16 03:44:19.029Z | 142.892° SSE | 2025-10-16 03:46:19.029Z | 95.885° ESE | 36.182° | 2025-10-16 03:49:19.029Z | 3.978° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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