diff --git a/trick_source/trick_utils/SAIntegrator/examples/Orbit/README.md b/trick_source/trick_utils/SAIntegrator/examples/Orbit/README.md
index 6f87c0a3..6a5fd88e 100644
--- a/trick_source/trick_utils/SAIntegrator/examples/Orbit/README.md
+++ b/trick_source/trick_utils/SAIntegrator/examples/Orbit/README.md
@@ -3,15 +3,15 @@
 This program uses the *SemiImplicitEuler* integrator to simulate the orbit of an Earth satellite.
 
 Generate the results as follows:
-'''
+```
 $ make
 $ ./Orbit > orbit.csv
-'''
+```
 
 Plot the results as follows:
 
-'''
+```
 $ python plot_position.py
-'''
+```
 
 ![Orbit](images/Orbit.png)