Issues related to multiple iterations

[wanglishuo]

Sorry to bother you again@schaubh ,
I have established a basic orbital simulation. The difference is that I want to implement a solution that, after conducting a simulation, takes the orbit information of the last position of the satellite as the input for the next simulation, repeating this process multiple times.
But I encountered some problems. When I assigned the results of each simulation to the initial state, it did not change, and each simulation still started from the state I set at the beginning.
Perhaps this question is a bit foolish, but I really don't understand where the problem lies. Can you point out where the problem lies, or can you provide me with a feasible solution.Here is my code.
`oe = orbitalMotion.ClassicElements()
rLEO = 7000. * 1000 # meters
oe.a = rLEO
oe.e = 0.0001
oe.i = 33.3 * macros.D2R
oe.Omega = 48.2 * macros.D2R
oe.omega = 347.8 * macros.D2R
oe.f = 85.3 * macros.D2R
rN, vN = orbitalMotion.elem2rv(mu, oe)
oe = orbitalMotion.rv2elem(mu, rN, vN)
scObject.hub.r_CN_NInit = rN # m - r_BN_N
scObject.hub.v_CN_NInit = vN # m/s - v_BN_N

simulationTime = macros.min2nano(10)
numDataPoints = 100
samplingTime = unitTestSupport.samplingTime(simulationTime, simulationTimeStep, numDataPoints)
dataRec = scObject.scStateOutMsg.recorder(samplingTime)
scSim.AddModelToTask(simTaskName, dataRec)

for i in range(3):
    scSim.InitializeSimulation()
    scSim.ConfigureStopTime(simulationTime)
    scSim.ExecuteSimulation()

    posData = dataRec.r_BN_N
    velData = dataRec.v_BN_N
    scObject.hub.r_CN_NInit = posData[-1]
    scObject.hub.v_CN_NInit = velData[-1]

    figureList = plotOrbits(dataRec.times(), posData)

    plt.show()
return figureList`

Thank you very much for your answer!

[wanglishuo]

If anyone sees it, can you answer my question? Thank you very much!