program sunsync1
 
sun-synchronous orbits - j2 solution
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<1> input mean semimajor axis and eccentricity
 
<2> input mean perigee and apogee altitudes
 
? 2
 
please input the mean perigee altitude (kilometers)
? 350
 
please input the mean apogee altitude (kilometers)
? 1000
 
 
program sunsync1
 
sun-synchronous orbits - j2 solution
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mean perigee altitude        	350.0000 kilometers
 
mean apogee altitude         	1000.0000 kilometers
 
mean semimajor axis          	7053.1400 kilometers
 
mean orbital eccentricity    	0.0460787678
 
mean orbital inclination     	98.0571 degrees
 
number of iterations         	 3
 