In the Double Pulsar, the Lense-Thirring periastron precession ωLT could be used to measure/constrain the moment of inertia I A of A. Conversely, if I A will be independently determined with sufficient accuracy by other means, tests of the Lense-Thirring effect could be performed. Such findings rely upon a formula for ωLT, A induced by the spin angular momentum S A of A, valid if the orbital angular momentum L and S A are aligned, and neglecting ωLT, B because of the smallness of S B . The impact on ωLT, A of the departures of the S A -L geometry from the ideal alignment is calculated. With the current upper bound on the misalignment angle δ A between them, the angles λ A , η A of S A are constrained within 85In units of the first order post-Newtonian mass-dependent periastron precession ωGR = 16.89 • yr −1 , a range variation ∆ ωLT, A ωLT, A max − ωLT, A min = 8 × 10 −8 ω GR is implied. The experimental uncertainty σ ωobs in measuring the periastron rate should become smaller by 2028-2030. Then, the spatial orientation of S B is constrained from the existing bounds on the misalignment angle δ B , and ωLT, B 2 × 10 −7 ωGR is correspondingly calculated. The error σ ωobs should become smaller around 2025. The Lense-Thirring inclination and node precessions İLT , ΩLT are predicted to be 0.05 arcseconds per year, far below the current experimental accuracies σ I obs = 0.5 • , σ Ω obs = 2 • in measuring I, Ω over 1.5 year with the scintillation technique. The Lense-Thirring rate ẋLT A of the projected semimajor axis x A of PSR J0737-3039A is 2 × 10 −16 s s −1 , just two orders of magnitude smaller than a putative experimental uncertainty σ ẋobs A 10 −14 s s −1 guessed from 2006 data.