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(2) "initial conditions" for that orbit (orbital inclination and ascending mode) (3) to plot ground track through a given "rectangle," (a) write eq'ns for boundaries (in terms of theta and phi) (b) ask if theta_min < theta < theta_max and phi_min < phi < phi_max (c) no? lift pen go to (e) (d) yes on last pass? yes - move with pen down to this point no - move to point with pen up, put pen down (e) go to next point 7/29 result of ground track program (over flying SW USA): 4 passes in daylight: 1. 000:03:07 3 min <-- PDP (IMU/ST, FC [[?]]) 2. 000:07:51 4 min <-- OSTA ops 3. 001:03:08 2 min <-- RMS ops 4. 001:07:55 2 min <-- RMS ops 5. 003:06:20 4 min <-- (initial prep, SMIRR ops)