Cartosat-1

Cartosat-1 satellite
Names	IRS-P5 Indian Remote Sensing Satellite-P5
Mission type	Earth observation
Operator	NTRO
COSPAR ID	2005-017A
SATCATno.	28649
Website	https://www.isro.gov.in/
Mission duration	5 years (planned) 14 years (achieved)
Spacecraft properties
Spacecraft	IRS-P5
Bus	IRS-1[1]
Manufacturer	ISRO
Launch mass	1,560 kg (3,440 lb)[2]
Power	1100watts[2]
Start of mission
Launch date	5 May 2005, 04:44:00UTC[3]
Rocket	Polar Satellite Launch Vehicle (PSLV-C6)[4]
Launch site	Satish Dhawan Space Centre,Second Launch Pad (SLP)[4]
Contractor	ISRO
Entered service	August 2005
End of mission
Deactivated	5 May 2019[5]
Orbital parameters
Reference system	Geocentric orbit[3]
Regime	Sun-synchronous orbit
Perigee altitude	620 km (390 mi)
Apogee altitude	622 km (386 mi)
Inclination	97.87°
Period	97.1 minutes
Instruments PAN Panchromatic Camera
Earth observation satellites series ← Resourcesat-1 Cartosat-2 →

Cartosat-1 (formerlyIRS-P5) is a stereoscopicEarth observation satellite in aSun-synchronous orbit, and the first one of theCartosat series of satellites. The eleventh satellite of ISRO inIndian Remote Sensing Satellite (IRS) series. The satellite was launched byIndian Space Research Organisation and is operated by NTRO. Weighing around 1560 kg at launch, its applications will mainly be towardscartography in India.

It was launched byPSLV-C6, on 5 May 2005 at 04:44:00UTC from the newly builtSecond Launch Pad atSriharikota.^[6] Images from the satellite will be available fromGeoEye for worldwide distribution. The satellite covers the entire globe in 1867 orbits on a 126-day cycle. Adjacent paths are covered by a separation of eleven days.^[7]

Department of Space (DoS),government of India, has launched a series of satellites for Earth's resource management and monitoring. These satellites have been very successful in providing data in various scales ranging from 1:1 million to 1:12,500 scale.^[7] Each of theIndian Remote Sensing satellite missions ensured data continuity while introducing improvements in the spatial, spectral and radiometric resolutions. Considering increase demand for large scale and topographic mapping data DoS launched the Cartosat-1 in 2005. Cartosat-1 is dedicated to stereo viewing for large scale mapping and terrain modelling.

Cartosat-1 carries two state-of-the-artpanchromatic (PAN) cameras that takeblack and white stereoscopic pictures of theEarth in thevisible region of theelectromagnetic spectrum. The swath covered by these high resolution PAN cameras is 30 km and their spatial resolution is 2.5 metres. For acquire two images simultaneously, one forward (PAN FORE) looking at +26° and one aft (PAN AFT) of the satellite at -5° for near instantaneous stereo data. The time difference between the acquisitions of the same scene by the two cameras is about 52 seconds.^[7] The spacecraft body is steerable to compensate the Earth rotation effect and to force both fore and aft cameras to look at the same ground strip when operated in stereo mode. The cameras are mounted on the satellite in such a way that near simultaneous imaging of the same area from two different angles is possible. This facilitates the generation of accurate three-dimensional maps. The cameras are steerable across the direction of the satellite's movement to facilitate the imaging of an area more frequently.

The images taken by Cartosat-1 cameras are compressed, encrypted, formatted and transmitted to the ground stations. The images are reconstructed from the data received at the ground stations. TheNational Remote Sensing Centre is responsible for acquisition, processing of data relayed by the Cartosat-1. A spherical Phased Array Antenna with steerable beam is used to transmit the data to the required ground station. A solid state recorder with 120 Gb capacity to store about 9 minutes of payload data is available for global operation of the payloads. The stored images can be transmitted when the satellite comes within the visibility zone of a ground station.

Each Panchromatic camera consists of three 3 mirror off-axis all reflective telescope with primary, secondary and tertiary mirrors. These mirrors are made from special zerodur glass blanks and are light weighted to about 60%. These mirrors are polished to an accuracy of l/80 and are coated with enhancedaluminium oxide (AlO₂) coating. In order to meet the high resolution and the swath requirement a 12K, 7 μm linear arraycharge-coupled device (CCD) is used as a detector.^[8]

• 2.5 m panchromatic band (0.5-0.85 μm)^[8]

The revisit rate for Cartosat-1 is five days.^[8]

The sensor collects data with a 10-bit sensitivity.^[8]

30 km (PAN-F) and 25 km (PAN-A)^[8]

• List of Indian satellites

• Cartosat-1 websiteArchived 31 July 2017 at theWayback Machine

• Cartosat
• Spacecraft launched in 2005
• Spacecraft launched by PSLV rockets

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