摘要:2.如图所示是人造地球卫星绕地球沿椭圆运动的轨道.则卫星在近地点P处的动能Ek1和引力势能EP1与在远地点M处的动能Ek2和引力势能Ep2的关系是,( ) A.Ek1>Ek2.Ep1<Ep2, B.Ek1>Ek2.Ep1>Ep2, C.Ek1<Ek2.Ep1<Ep2, D.Ek1<Ek2.Ep1>Ep2,

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