For the following orbital elements express the r and v vectors for the satellite in the perifocal system along the unit vectors P, Q, W.

p=.23 DUp e = .82 i= 900 uo = 900 1800 = 2600 vo = 1900 10-2700 C) p=.23 DUp e = .82 i= 900 uo = 900 1800 = 2600 vo = 1900 10-2700 C)