FR1007

Looking at the Restart states from Rev 1008 we have the following results for FR1007
FR1007		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 26 2019 14:54:49.574	97417.006	97426.199	97426.433	9.193	9.427	-0.23376	-2.543%	
MMS2	May 26 2019 14:54:53.139	97409.303	97426.256	97426.339	16.953	17.036	-0.08292	-0.489%	
MMS3	May 26 2019 14:54:27.686	97426.362	97426.347	97426.364	-0.015	0.002	-0.01686		
MMS4	May 26 2019 14:54:21.476	97422.688	97426.273	97426.277	3.586	3.590	-0.00410	-0.114%	
 
MMS1 was 0.311 m/s (net delta-v) and 18.34% axial, MMS2 was 0.382 m/s and 5.24% axial, and MMS4 was 0.167 m/s and 38.32% 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 second maneuver extracted from the DVTABLE files, 
•	The associated predicted velocity maneuver planning requirement for 1 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 second 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) 	
MMS4 	2019_142/01:49:17 to 2019_142/01:49:37 	-0.0153 	0.002 	-2.484e-05 	-0.1021 	0.002 	-0.000676 	-0.1311 	0.002 	-0.0002611 	
MMS1	2019_142/03:39:07 to 2019_142/03:39:37 	-0.0038 	0.002 	2.799e-05 	-0.3059 	0.003059 	-0.00101 	-0.0519 	0.002 	-0.0001339 	
MMS2	2019_142/05:28:57 to 2019_142/05:29:37 	0.2017 	0.002017 	8.065e-05 	-0.3063 	0.003063 	-0.0005454 	-0.1062 	0.002 	-0.0001317