Vinti Orbit Propagator Analysis regarding Short Time to Demise

[G5STER]

Our mission objectives have a mission life expectation of at least a week. We have looked at Burnout velocity (varying from 7.5 km/s to 7.55 km/s). With a burnout velocity of 7.55 km/s, we are estimating the life to be ~7 days. An insight into this value along with Initial Orbit Altitude (km), Burnout Latitude, and Burnout Longitude could provide a better prediction.

Run analysis using Octave orbit simulation (and maybe GMAT).