general navigation structure general satellite info ilrs support retroreflector info center of mass site performance info

COMPASS

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

Mission Photos:

COMPASS-M1 Satellite
COMPASS (Courtesy of Shanghai Astronomical Observatory)

Mission Objectives:

The Compass Navigation Satellite Experimental System is a satellite constellation developed by the Chinese Defense Ministry. The system, also known as BeiDou, is the first space-based regional navigation and positioning network developed by China. COMPASS provides all-weather, two-dimensional positioning data for both military and civilian users. The system has both navigation and communication capabilities and spans most areas of the East Asia region. The satellite network consists of four BeiDou 1 satellites launched in 2000, 2003, and 2007 in geostationary orbit; a fifth satellite, COMPASS-M1, was launched in MEO in April 2007. Additional satellites in the COMPASS constellation have been launched in 2009, 2010, 2011, and 2012.

COMPASS Mission Parameters:
  COMPASS-M1 COMPASS-M3 COMPASS-G1 COMPASS-I3 COMPASS-I5
Sponsor: Chinese Defense Ministry Chinese Defense Ministry Chinese Defense Ministry Chinese Defense Ministry Chinese Defense Ministry
Expected Life: 3 years 3 years 3 years 3 years 3 years
Primary Applications: Positioning Positioning Positioning Positioning Positioning
Primary SLR Application: Precision orbit determination Precision orbit determination Precision orbit determination Precision orbit determination Precision orbit determination
Launch Date: 13-Apr-2007 29-Apr-2012 17-Jan-2010 10-Apr-2011 01-Dec-2011
COSPAR ID: 0701101 1201801 1000101 1101301 1107301
SIC: 2001 2004 2002 2003 2005
NORAD: 31115 38250 36287 37384 37948
NP Bin Size 300 seconds 300 seconds 300 seconds 300 seconds 300 seconds
RRA Diameter:          
RRA Shape: Hexagonal Hexagonal Hexagonal Hexagonal Hexagonal
Reflectors: 42 corner cubes 42 corner cubes 90 corner cubes 90 corner cubes 90 corner cubes
Orbit: MEO MEO GEO GEO GEO
Inclination: 55.5 degrees 55.0 degrees 1.53 degrees 55.6 degrees 55.6 degrees
Eccentricity: 0.00068 0.0025 0.00018 0.0023 0.0023
Perigee: 21,500 km 21,528 km 42,163.9 km 42,161.2 km 42,161.2 km
Period: 773.39 min        
Weight: 2,200 kg        
Additional Information:

Web sites:

Publications: