Create Spacecraft mySat
mySat.DateFormat = 'UTCGregorian'
mySat.Epoch = '03 Feb 2009 12:34:56.123'
mySat.CoordinateSystem = EarthMJ2000Eq

Create CoordinateSystem MarsInertial
MarsInertial.Origin =  Mars
MarsInertial.Axes   =  BodyInertial

Create ReportFile rf
rf.Filename = 'Params_LhsDeps_OutgoingAsymptote.report'
rf.WriteHeaders = false

Create Variable E1 E2 E3 E4 E5 E6

BeginMissionSequence

E1 = 5000.000000019102
E2 = 8.565662851678859
E3 = 129.2315204833889
E4 = 37.7612439071457
E5 = 63.43494882309343
E6 = 0

%  Report lines should match
Report rf E1 E2 E3 E4 E5 E6

mySat.Mars.HyperbolicRadPer = E1
mySat.Mars.C3Energy = E2
mySat.MarsInertial.OutgoingRHA = E3
mySat.MarsInertial.OutgoingDHA = E4
mySat.MarsInertial.OutgoingBVAZI = E5
mySat.Mars.TA = E6

Report rf mySat.Mars.HyperbolicRadPer mySat.Mars.C3Energy mySat.MarsInertial.OutgoingRHA mySat.MarsInertial.OutgoingDHA mySat.MarsInertial.OutgoingBVAZI mySat.Mars.TA