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Jump to: Mission Objectives, Mission Instrumentation, Mission Parameters, Additional Information

Mission Photos:

Courtesy of CNES

Satellite with ARgos and ALtika (SARAL) is a cooperative mission between CNES and the Indian Space Research Organization (ISRO) The mission is complemenatary to Jason-2 and will provide observations of ice, rain, coastal zones, and wave heights. SARAL results from the common interests of CNES and ISRO in studying the oceans from space using altimetry and providing maximum use of ARGOS (Advanced Research and Global Observation Satellite), a joint NOAA CNES data collection system.

Mission Objectives:

The main mission objectives of SARAL are to:

  • Create precise, repetative global measurements of sea surface height, wave heights, and wind speed
  • Ensure continutity of the altimetry service currently available from Envisat and Jason-1/-2
  • Contribute to global ocean and climate studies to build a global ocean observing system

These objectives will be accomplished by studying mesoscale ocean variability through observations of:

  • coastal areas
  • inland waters
  • surface of continental ice sheets
Mission Instrumentation:

The SARAL satellite will be provided by ISRO; the mission will have the following instrumentation onboard:

  • Altimeter/Radiometer (AltiKa) built by CNES
  • DORIS built by CNES
  • Laser Retroreflector Array built by CNES
  • ARGOS-3 instrument

The DORIS instrument will be used for POD, which is a fundamental requirement for achieving the goals of the SARAL mission. SLR will play an important role by providing strong tracking information to complement DORIS and by providing a unique and unambiguous verification of the absolute radial orbit accuracy.

Mission Parameters:
Satellite: SARAL
Sponsor: CNES and ISRO
Expected Life: 5 years (ARGOS); 3 years (AltiKa)
Primary Applications: Earth sensing
Primary SLR Applications: Precision orbit determination
COSPAR ID: 1300901
SIC Code: 3201
NORAD SSC Code: 39086
Launch Date: Feb 25, 2013
NP Bin Size: 15 seconds
RRA Diameter: TBD
RRA Shape: Octagonal
Reflectors: 9 corner cubes
Inclination: 98.55 degrees
Eccentricity: 1.165 x 10-3
Altitude: 814 km
Weight: 350-400 kg

Additional Information:

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