Parking orbit is a geostationary satellites orbit.
From Keplers third law of planetary motion, the square of period of revolution (T) is directly proportional to cube of semi-major axis of its elliptical orbit (a), i.e.. T2∝a3
Given, T1=1 day (geostationary) a1=a,a2=2a ∴T22T12=a23a13 ⇒T22=a13a23T12=a3(2a)3×1=8 ⇒T2=22 days