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Orbital Mechanics

vis-viva · Hohmann transfer · plane change · escape · J2 regression

Hohmann Transfer — Animated

Two-burn transfer between circular orbits. Δv₁ at departure, Δv₂ at arrival; to-scale ellipse animated.

Vis-Viva Velocity

v=√(µ(2/r−1/a)); circular & escape too.

Orbital Period & Escape

T=2π√(a³/µ); v_esc=√(2µ/r).

Plane Change Δv

Δv=2v·sin(Δi/2) — do it where v is slow.

J2 Nodal Regression

Ω̇=−1.5√µ·J₂R_E²/((1−e²)²a^3.5)·cos i.
Formula reference & constants

vis-viva v=√(µ(2/r−1/a)); Hohmann Δv₁=√(µ/r₁)(√(2r₂/(r₁+r₂))−1), Δv₂=√(µ/r₂)(1−√(2r₁/(r₁+r₂))), t=π√(a_t³/µ).

plane change 2v·sin(Δi/2); escape √(2µ/r); period 2π√(a³/µ); J2 nodal Ω̇=−1.5√µ J₂R_E²/((1−e²)²a^3.5)cos i.

Earth µ=3.986e5 km³/s², R_E=6378 km, J₂=1.0826e-3. Sun-sync at i≈98° gives Ω̇≈0.986°/day.