Cartosat-1 Explained

Cartosat-1
Names List:IRS-P5
Indian Remote Sensing Satellite-P5
Mission Type:Earth observation
Operator:NTRO
Cospar Id:2005-017A
Satcat:28649
Website:https://www.isro.gov.in/
Mission Duration:5 years (planned)
14 years (achieved)
Spacecraft:IRS-P5
Spacecraft Bus:IRS-1[1]
Manufacturer:Indian Space Research Organisation
Launch Mass: [2]
Power:1100 watts
Launch Date:5 May 2005, 04:44:00 UTC
Launch Rocket:Polar Satellite Launch Vehicle (PSLV-C6) [3]
Launch Site:Satish Dhawan Space Centre, Second Launch Pad (SLP)
Launch Contractor:ISRO
Entered Service:August 2005
Deactivated:5 May 2019 [4]
Orbit Reference:Geocentric orbit[5]
Orbit Regime:Sun-synchronous orbit
Orbit Inclination:97.87°
Orbit Period:97.1 minutes
Apsis:gee
Instruments List:
Acronym1:PAN
Name1:Panchromatic Camera
Programme:Earth observation satellites series
Previous Mission:Resourcesat-1
Next Mission:Cartosat-2

Cartosat-1 (formerly IRS-P5) is a stereoscopic Earth observation satellite in a Sun-synchronous orbit, and the first one of the Cartosat series of satellites. The eleventh satellite of ISRO in Indian Remote Sensing Satellite (IRS) series. The satellite was launched by Indian Space Research Organisation and is operated by NTRO. Weighing around 1560 kg at launch, its applications will mainly be towards cartography in India.

Launch

It was launched by PSLV-C6, on 5 May 2005 at 04:44:00 UTC from the newly built Second Launch Pad at Sriharikota.[6] Images from the satellite will be available from GeoEye 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]

History

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 the Indian 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.

Specifications

Payload

Cartosat-1 carries two state-of-the-art panchromatic (PAN) cameras that take black and white stereoscopic pictures of the Earth in the visible region of the electromagnetic 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.

Communications

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. The National 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.

Optics and detectors

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 enhanced aluminium oxide (AlO2) coating. In order to meet the high resolution and the swath requirement a 12K, 7 μm linear array charge-coupled device (CCD) is used as a detector.[8]

Imaging capabilities

Spatial resolution

Temporal resolution

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

Radiometric resolution

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

Swath

30 km (PAN-F) and 25 km (PAN-A) [8]

See also

External links

Notes and References

  1. Web site: IRS P5 (Cartosat 1). Gunter's Space Page. 19 June 2017.
  2. Web site: Cartosat-1. ISRO. 5 May 2005. 19 June 2017. 31 July 2017. https://web.archive.org/web/20170731201845/http://www.isro.gov.in/Spacecraft/cartosat-1. dead.
  3. Web site: PSLV C6/IRS-P5/HAMSAT Mission Brochure. ISRO. 19 June 2017. 31 July 2017. https://web.archive.org/web/20170731194316/http://www.isro.gov.in/sites/default/files/flipping_book/PSLV-C6/files/assets/common/downloads/publication.pdf. dead.
  4. Web site: Cartosat-1. World Meteorological Organization. 3 January 2020. 12 May 2021.
  5. Web site: Trajectory: Cartosat-1 2005-017A . NASA. 27 April 2021. 10 May 2021.
  6. News: PSLV-C6 launched from Sriharikota. 18 September 2012. 5 May 2005. The Economic Times. India.
  7. Web site: Cartosat-1. 18 September 2012. https://web.archive.org/web/20150829044009/http://www.nrsc.gov.in/#app=a097&cd0b-selectedIndex=8. 29 August 2015. dead.
  8. http://www.gisdevelopment.net/technology/rs/techrs023.htm Indian Remote Sensing Satellite Cartosat-1: Technical features and data products