diff --git a/maneuvers/comsat.py b/maneuvers/comsat.py
new file mode 100644
index 0000000..d3d3cea
--- /dev/null
+++ b/maneuvers/comsat.py
@@ -0,0 +1,90 @@
+import math
+
+from maneuver_scheduler import ManeuverScheduler
+
+from . import MechJebManeuver
+
+
+class ComsatManeuver(MechJebManeuver):
+    def __init__(self, conn, vessel, target_body):
+        super().__init__(conn, vessel)
+        self.target_body = target_body
+
+        body = self.target_body
+        if body.satellites:
+            lowest_sat = min(body.satellites, key=lambda sat: sat.orbit.periapsis)
+            max_orbit = lowest_sat.orbit.periapsis - lowest_sat.sphere_of_influence
+        else:
+            max_orbit = body.sphere_of_influence
+
+        self.target_altitude = max_orbit - ((5 / 100) * max_orbit)
+
+    def start(self):
+        self.plan_next_maneuver()
+
+    def plan_next_maneuver(self):
+        sc = self.conn.space_center
+        vessel = sc.active_vessel
+
+        if vessel.orbit.body.name != self.target_body.name:
+            raise NotImplementedError
+
+        if not math.isclose(vessel.orbit.apoapsis, self.target_altitude, rel_tol=.01):
+            SetOrbitApoapsis(self.conn, vessel, self.target_altitude).prepare_maneuver()
+        elif not math.isclose(vessel.orbit.eccentricity, 0, rel_tol=.01):
+            CircularizeOrbitAndDeliver(self.conn, vessel, self.target_altitude).prepare_maneuver()
+        elif self.vessel.control.current_stage == 0:
+            return True
+
+        return False
+
+
+class SetOrbitApoapsis(ComsatManeuver):
+    name = "Set target orbit's apoapsis"
+
+    def prepare_maneuver(self):
+        oa = self.maneuver_planner.operation_apoapsis
+        oa.new_apoapsis = self.target_altitude
+        oa.time_selector.time_reference = self.mech_jeb.TimeReference.periapsis
+        nodes = oa.make_nodes()
+
+        node = nodes[0]
+
+        ManeuverScheduler.book_timeslot_for_node(self.vessel, node, self)
+
+
+class CircularizeOrbitAndDeliver(ComsatManeuver):
+    name = "Circularize orbit and deliver comsat"
+
+    def prepare_maneuver(self):
+        oc = self.maneuver_planner.operation_circularize
+        oc.time_selector.time_reference = self.mech_jeb.TimeReference.apoapsis
+        nodes = oc.make_nodes()
+
+        node = nodes[0]
+
+        ManeuverScheduler.book_timeslot_for_node(self.vessel, node, self)
+
+    def execute(self) -> bool:
+        sc = self.conn.space_center
+        if sc.active_vessel.name != self.vessel.name:
+            sc.active_vessel = self.vessel
+
+        while self.vessel.control.nodes:
+            self._execute_node()
+
+        if self.vessel.control.current_stage > 0:
+            self.vessel.control.activate_next_stage()
+
+            oro = self.maneuver_planner.operation_resonant_orbit
+            oro.resonance_numerator = 2
+            oro.resonance_denominator = 3
+            oro.time_selector.lead_time = 10
+            oro.time_selector.time_reference = self.mech_jeb.TimeReference.x_from_now
+            oro.make_nodes()
+
+            while self.vessel.control.nodes:
+                self._execute_node()
+            return self.plan_next_maneuver()
+        else:
+            return True