jgg     2007 27 (1):  85-90    ISSN: 0412-1961  CN: 21-1139/TG

LEO SATELLITE EPHEMERIS PARAMETERS FITTING METHOD BASED ON ORBIT CHARACTER OF SATELLITE
Ma Kaifeng 1,2) ; Peng Bibo 1) ; and Hong Ying 3)
1)Institute of Geodesy and Geophysics,CAS,Wuhan 4300772)Graduate School of the Chinese Academy of Science,Beijing 1000493)Department of Math. and Physics,Wuhan University of Science and Engineering,Wuhan 430073
Received: 1900-01-01  Revised: 1900-01-01  Online: null
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