diff --git a/Luminary099/P32-P35_P72-P75.agc b/Luminary099/P32-P35_P72-P75.agc
index 3bba50a..8e36ba7 100644
--- a/Luminary099/P32-P35_P72-P75.agc
+++ b/Luminary099/P32-P35_P72-P75.agc
@@ -322,9 +322,9 @@ P32/P72F	STORE	T2TOT3
 
 # Page 624
 # CONSTANT DELTA HEIGHT (CDH) PROGRAMS (P33 AND P73)
-# MOD NO -1			LOC SECTION -- P32-P35, P72-P75
-# MOD BY WHITE, P.		DATE: 1 JUNE 67
 #
+# MOD NO -1			LOG SECTION - P32-P35, P72-P75
+# MOD BY WHITE.P		DATE 1JUNE67
 # PURPOSE
 #
 #	(1)	TO CALCULATE PARAMETERS ASSOCIATED WITH THE CONSTANT DELTA
@@ -344,7 +344,7 @@ P32/P72F	STORE	T2TOT3
 #
 #	(1)	THIS PROGRAM IS BASED UPON PREVIOUS COMPLETION OF THE
 #		CO-ELLIPTIC SEQUENCE INITIATION (CSI) PROGRAM (P32/P72).
-#		THEREFORE --
+#		THERFORE -
 #
 #		(A)	AT A SELECTED TPI TIME (NOW IN STORAGE) THE LINE OF SIGHT
 #			BETWEEN THE ACTIVE AND PASSIVE VEHICLES WAS SELECTED TO BE
@@ -358,13 +358,14 @@ P32/P72F	STORE	T2TOT3
 #			COMPUTED TO BE GREATER THAN 10 MINUTES.
 #
 #		(D)	THE VARIATION OF THE ALTITUDE DIFFERENCE BETWEEN THE
-#			ORBITS WAS MINIMIZED.
+#			ORBITS WAS MINMIZED.
 #
 #		(E)	CSI BURN WAS DEFINED SUCH THAT THE IMPULSIVE DELTA V WAS
 #			IN THE HORIZONTAL PLANE DEFINED BY ACTIVE VEHICLE
+#
 #			POSITION AT CSI IGNITION.
 #
-#		(F) 	THE PERICENTER ALTITUDES OF THE ORBITS FOLLOWING CSI AND
+#		(F)	THE PERICENTER ALTITUDES OF THE ORBITS FOLLOWING CSI AND
 #			CDH WERE COMPUTED TO BE GREATER THAN 35,000 FT FOR LUNAR
 #			ORBIT OR 85 NM FOR EARTH ORBIT.
 #