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The point at which the spacecraft should leave the (almost circular) catch-up orbit can be calculated using this formula:  
 
The point at which the spacecraft should leave the (almost circular) catch-up orbit can be calculated using this formula:  
  
<math>\Delta \varphi = 2 \pi \left [ 1 - ( 2 m - 1 ) \left ( \frac {a}{r_z} \right )^{\frac{3}{2}} \right ] </math>
+
<math>\Delta \varphi = \pi \left [ 1 - ( 2 m - 1 ) \left ( \frac {a}{r_z} \right )^{\frac{3}{2}} \right ] </math>
  
 
where
 
where

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