Names | IRS-P7 CartoSat-2AT | ||||
---|---|---|---|---|---|
Mission type | Earth observation | ||||
Operator | ISRO | ||||
COSPAR ID | 2007-001B![]() | ||||
SATCATno. | 29710 | ||||
Website | https://www.isro.gov.in/ | ||||
Mission duration | 5 years (planned) 12 years (achieved) | ||||
Spacecraft properties | |||||
Spacecraft | IRS-P7 | ||||
Bus | IRS-2[1] | ||||
Manufacturer | Indian Space Research Organisation | ||||
Launch mass | 680 kg (1,500 lb)[2] | ||||
Power | 900watts[3][4] | ||||
Start of mission | |||||
Launch date | 10 January 2007, 03:57:00UTC[5] | ||||
Rocket | Polar Satellite Launch Vehicle (PSLV C7)[2] | ||||
Launch site | Satish Dhawan Space Centre,FLP[2] | ||||
Contractor | Indian Space Research Organisation | ||||
Entered service | 2007 | ||||
End of mission | |||||
Deactivated | 2019 | ||||
Decay date | 14 Feb 2024 | ||||
Orbital parameters | |||||
Reference system | Geocentric orbit | ||||
Regime | Sun-synchronous orbit[5] | ||||
Perigee altitude | 621 km (386 mi) | ||||
Apogee altitude | 641 km (398 mi) | ||||
Inclination | 97.9° | ||||
Period | 97.3 minutes | ||||
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Cartosat-2 was anEarth observation satellite in aSun-synchronous orbit and the second of theCartosat series of satellites. The satellite was built, launched and maintained by theIndian Space Research Organisation (ISRO). Weighing around 680 kg at launch, its applications were mainly be towardscartography . It was launched by thePolar Satellite Launch VehiclePSLV C7 launch vehicle on 10 January 2007.
Cartosat-2 carried a state-of-the-artpanchromatic (PAN) camera that took black and white pictures of theEarth in thevisible region of theelectromagnetic spectrum. The swath covered by this high resolution PAN camera was 9.6 km and their spatial resolution is less than 1 metre. The satellite could be steered up to 45° along as well as across the track. Cartosat-2 was an advancedremote sensing satellite capable of providing scene-specific spot imagery. The data from the satellite was used for detailed mapping and other cartographic applications at cadastral level, urban and rural infrastructure development and management, as well as applications inLand information system (LIS) andGeographic information system (GIS). The first imagery, received on 12 January 2007, covered a length of 240 km fromPaonta Sahib in Shivalik region toDelhi. Another set of imagery of about 50 km length coveredRadhanagari to Sagoan inGoa. Analysis of the first imagery received atNational Remote Sensing Agency's data reception station atShadnagar, inHyderabad, confirmed excellent performance of the on-board camera.
Cartosat-2'spanchromatic camera was able to produce images better than 1 metre in resolution,[6] compared to the 82 cm panchromatic resolution offered by theIkonos satellite.[7] India had previously purchased images from Ikonos at about US$20 per square kilometre; the use of Cartosat-2 will provide imagery at 20 times lower cost. At the time of Cartosat-2's launch, India was buying about₹20 crore per year from Ikonos.[8]
After 12 years of service in a circular orbit of almost 630 km altitude Cartosat-2 would have taken about 30 years to de-orbit naturally. With 25 kg of propellant remaining it was decided by ISRO's Directorate for Space Situational Awareness and Management (DSSAM) to decommission the spacecraft and lower the perigee using left-over propellant so that it meetsUnited Nations Office for Outer Space Affairs (UNOOSA)'s space debris mitigation guidelines. Between 6 March to 3 September 2020, perigee was lowered incrementally by performing 26 perigee reduction burns putting the spacecraft in 630 × 390 km orbit. This was ISRO's firstlow Earth orbit satellite to be decommissioned in this manner. Orbit of Cartosat-2 is expected to decay naturally within 10 years.[9][10]
The satellite re-entered Earth's atmosphere and was subsequently destroyed on 14 February 2024 at 10:18 UTC over the southern Indian Ocean.[11][12]
After providing uninterrupted payload services for 12 years, it was decided to decommission the satellite in late 2019 following on-board subsystem degradation. At an orbit of 630 km altitude, the lifetime of Cartosat-2 was estimated to be more than 30 years. The satellite also had about 26 kg left-over propellant. Although the satellite was not specifically designed for end-of-life de-orbiting, it was proposed by ISRO's Directorate for Space Situational Awareness and Management (DSSAM) to lower the perigee of the satellite, so as to limit its post mission orbital life time in compliance with the 25-year guideline of IADC for post mission disposal of LEO objects, and at the same time, deplete the left-over fuel to mitigate any accidental break-up risk. The de-orbiting operations were planned and executed by the operational team atISRO Telemetry, Tracking and Command Network (ISTRAC) in close coordination with mission and subsystem designers from various ISRO centres. Starting with the first perigee-lowering manoeuvre on 6 March 2020, 26 perigee reduction burns were conducted till 3 September 2020 to progressively lower the perigee below 400 km.