Two satellites are flying in formation in LEO. The chief is in a circular orbit with altitude of 600 km. At t0 the deputy’s LVLH coordinates relative to the chief are x0 = 69.78 km, y0 = 139.56 km, z0 = 139.56 km, ẏ0 = −151.116 m/s, ẋ0 = ż0 = 0 m/s - Calculate the effective impulsive ∆v imparted on the satellite when it was impacted by the debris - Calculate the two impulsive burns required to maneuver the satellite back to its original position in 6 hrs

Two satellites are flying in formation in LEO. The chief is in a circular orbit with altitude of 600 km. At t0 the deputy’s LVLH coordinates relative to the chief are x0 = 69.78 km, y0 = 139.56 km, z0 = 139.56 km, ẏ0 = −151.116 m/s, ẋ0 = ż0 = 0 m/s - Calculate the effective impulsive ∆v imparted on the satellite when it was impacted by the debris - Calculate the two impulsive burns required to maneuver the satellite back to its original position in 6 hrs

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