FR1006

Looking at the Restart states from Rev 1007 we have the following results for FR1006
FR1006		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	May 23 2019 02:48:11.940	97455.548	97446.129	97446.072	-9.419	-9.476	0.05674	-0.602%	
MMS2	May 23 2019 02:47:56.777	97455.506	97438.411	97438.357	-17.095	-17.148	0.05353	-0.313%	
MMS3	May 23 2019 02:48:20.574	97455.526	97455.526	97455.526	0.000	0.001	-0.00087		
MMS4	May 23 2019 02:48:03.511	97455.465	97451.909	97451.866	-3.555	-3.599	0.04370	-1.229%	
 
MMS1 was 0.168 m/s (net delta-v) and 55.54% axial, MMS2 was 0.389 m/s and 24.27% axial, and MMS4 was 0.204 m/s and 47.34% axial.

The Table below provides the following information:
•	The start and end times and planned maneuver 
•	Total delta-V (DeltaV_X, DeltaV_Y, and DeltaV_Z) for the first maneuver extracted from the DVTABLE files, 
•	The associated predicted velocity maneuver planning requirement for 1 and 2 orbit predictions (DeltaV_X Req, DeltaV_Y Req, and DeltaV_Z Req)
•	The difference between the predicted velocity and the GEONS definitive velocity at the start time of the first maneuver (Diff_V_X, Diff_V_Y, and Diff_V_Z).Planned maneuver total delta-V values based on the associated DVTABLEs  
As shown in the table below, all maneuvering spacecraft meet the requirement .
Mnvr ID 	Time Span 	DeltaV_X (m/s) 	DeltaV_X Req (m/s) 	Diff_V_X (m/s) 	DeltaV_Y (m/s) 	DeltaV_Y Req (m/s) 	Diff_V_Y (m/s) 	DeltaV_Z (m/s) 	DeltaV_Z Req (m/s) 	Diff_V_Z (m/s) 	
MMS2 	2019_140/16:11:12 to 2019_140/16:11:42 	0.3662 	0.01 	-0.006831 	-0.1136 	0.01 	0.007491 	0.054 	0.01 	0.001578 	
MMS4	2019_140/17:46:12 to 2019_140/17:46:42 	0.1354 	0.01 	-0.007976 	0.0158 	0.01 	0.007819 	0.149 	0.01 	0.001662 	
MMS1	2019_140/19:21:12 to 2019_140/19:21:42 	0.0701 	0.01 	-0.008428 	-0.1092 	0.01 	0.007189 	0.098 	0.01 	0.001718