#
# ico
#

set PI 3.14159
set MU 398601.2
set RADIUS_OF_EARTH 6378.14

set SATS_PER_PLANE 5
set NUM_PLANES 2
set INTERPLANE_SPACING 180.0

# setup orbital elements
set a [expr 10355.0+$RADIUS_OF_EARTH]
set e 0.0
set inc 45.0
set omega 0.0

# compute period of orbit
set T_per [expr 2 * $PI * pow($a,1.5) / sqrt($MU)]

satellites GV_BEGIN
for {set j 0} {$j < $NUM_PLANES} {incr j} {
	set Omega [expr $j * $INTERPLANE_SPACING]
	for {set i 0} {$i < $SATS_PER_PLANE} {incr i} {
		set T [expr $T_per * $i / $SATS_PER_PLANE]
		set n [satellites LOAD $a $e $inc $Omega $omega $T]
		if {$i > 0} {satellites ORBIT_SET $n 0}
	}
}
satellites GV_END

