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This tab will contain alphanumeric output data displayed for each propagation. You will have at least initial and final Keplerian parameters:

---------------- JPSIMU ---------------- 
Initial conditions: 
Date (TAI)     2010-01-01T12:00:34.000  
Frame          EME2000                  
Mass (kg)      1000.0                   
T (h)          1.4917487906426035       
A (km)         6628.137000000006        
Ex             8.881784197001211E-16    
Ey             -8.542591124194022E-23   
Inc (deg)      51.59999810577826        
Raan (deg)     7.714051151482253E-6     

Propagation starts...

Propagation ends

Final conditions: 
Date (TAI)     2010-01-01T12:00:34.000  
Frame          EME2000                  
Mass (kg)      1000.0                   
T (h)          1.4917488212977439       
A (km)         6628.137068103452        
Ex             1.0274900930085038E-8    
Ey             -1.0596989223166918E-15  
Inc (deg)      51.59999810577826        
Raan (deg)     7.71405115146883E-6