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general navigation structure General ilrs support retroreflector info center of mass

IRNSS

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

Mission Photos:

IRNSS
Courtesy of Inside GNSS

Mission Objectives:

The Indian Regional Navigation Satellite System (IRNSS) consists of a constellation of seven satellites and a ground segment for positioning and timing applications. IRNSS is under development by the Indian Space Research Organisation (ISRO). INRSS will include three satellites in geostationary orbit and four satellites in geosynchronous orbit, transmitting L-band and S-band signals and providing coverage primarily for the Indian land mass.

SLR tracking data will be used for orbit determination and calibration of the orbit determined from other sources.

Mission Instrumentation:

INRSS satellites will have the following instrumentation onboard:

  1. Atomic clocks
  2. L and S-band transmitters
  3. Retroreflector array
Mission Parameters:
IRNSS Mission Parameters
Satellite: IRNSS
Sponsor: ISRO, India
Expected Life: 10 years
Primary Applications: Positioning and timing
Primary SLR Applications: Orbit determination
COSPAR ID: TBD
SIC Code: TBD
NORAD SSC Code: TBD
Launch Date: 2012
NP Bin Size: 10 seconds
RRA Shape:
Cube Diameter: 38 mm
Reflectors: 40 corner cubes
Inclination: 29 degrees
Eccentricity: 0.002
Altitude: 42,164 km
Weight:
Additional Information:
  • Web sites:
  • Publications:

 
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