diff --git a/boot/debug_satellite.ks b/boot/debug_satellite.ks
new file mode 100644
index 0000000..32d7d6c
--- /dev/null
+++ b/boot/debug_satellite.ks
@@ -0,0 +1 @@
+runpath("0:/boot/satellite", true).
diff --git a/boot/satellite.ks b/boot/satellite.ks
index 0994822..3da8f9c 100644
--- a/boot/satellite.ks
+++ b/boot/satellite.ks
@@ -12,7 +12,8 @@ local compiled is list(
 local copied is list(
   "/lib/ui",
   "/prog/execnode",
-  "/prog/circ"
+  "/prog/circ",
+  "/prog/satdeploy"
 ).
 
 Bootstrap(
diff --git a/lib/navigation.ks b/lib/navigation.ks
index eb0bc74..a4c33ca 100644
--- a/lib/navigation.ks
+++ b/lib/navigation.ks
@@ -17,12 +17,32 @@ function GetAscentVector {
   return newHeading.
 }
 
+// Create a node that will circularize the orbit.
+// 'where' can be one of:
+// the special string "APO", for the next Apoapsis.
+// the special string "PERI", for the next Periapsis.
+// a time value (either a Time struct or a scalar), representing a target time.
 function CreateCircularizationNode {
-  parameter nodeAtPeriapsis is false.
+  parameter where is "APO".
 
-  local dt is choose SHIP:ORBIT:ETA:PERIAPSIS if nodeAtPeriapsis else SHIP:ORBIT:ETA:APOAPSIS.
-  local a is choose SHIP:ORBIT:PERIAPSIS if nodeAtPeriapsis else SHIP:ORBIT:APOAPSIS.
-  local t is TIME + dt.
+  local dt is 0.
+  local a is 0.
+  local t is 0.
+  if where:IsType("String") {
+    if where = "APO" {
+      set dt to SHIP:ORBIT:ETA:APOAPSIS.
+      set a to SHIP:ORBIT:APOAPSIS.
+    } else if where = "PERI" {
+      set dt to SHIP:ORBIT:ETA:PERIAPSIS.
+      set a to SHIP:ORBIT:PERIAPSIS.
+    } else {
+      print "WARNING: Invalid string passed to CreateCirculazationNode(). Node is invalid.".
+    }
+
+    set t to TIME + dt.
+  } else {
+    set t to where.
+  }
 
   local Vc is sqrt(SHIP:BODY:MU/(SHIP:BODY:RADIUS + a)).
   local dV is Vc - VelocityAt(SHIP, t):ORBIT:MAG.
diff --git a/prog/satdeploy.ks b/prog/satdeploy.ks
new file mode 100644
index 0000000..7ec7700
--- /dev/null
+++ b/prog/satdeploy.ks
@@ -0,0 +1,26 @@
+// Run this program on a staged multi-satellite deploy mission. (e.g. using a fairing with interstage nodes and stack separators) To use:
+//
+// 1. Make sure the next stage will decouple a satellite and activate its engines.
+// 2. Pull up the PAW for the satellite's probe core and "Control from Here".
+// 3. Run this program from that satellite's computer.
+//
+// This program will decouple the satellite and circularize its orbit. Ideally done on a resonant satellite injection orbit.
+
+@lazyglobal off.
+
+parameter name is "New Satellite".
+
+runoncepath("/lib/navigation").
+runoncepath("/lib/node").
+
+stage.
+PANELS on.
+set SHIP:NAME to name.
+CreateCircularizationNode(TIME + 2).
+ExecNode().
+
+for p in SHIP:PARTS {
+  if p:MODULES:Find("ModuleRTAntenna") > -1 {
+    p:GetModule("ModuleRTAntenna"):DoEvent("ACTIVATE").
+  }
+}