Orbital Mechanics Planner - JPL Apps

Hohmann Transfer Planner

● Planning

Central Body

Mission Profile

Orbit Presets

Initial Periapsis Alt (km)

Initial Eccentricity 0.00

Initial Inclination (°) 0°

Target Periapsis Alt (km)

Target Eccentricity 0.00

Target Inclination (°) 0°

Time Warp

Initial

Transfer

Target

Mission Insights

PhasePlanning

Current Alt400 km

Current Vel0 km/s

Elapsed / TOF0s / 0h 0m

Model2-Body Kepler

Δv₁ (plane)0 / 0 m/s

Δv₂ (total)0 / 0 m/s

v₁ / v₂0 km/s / 0 km/s

Pe / Ap0 km / 0 km

a / e0 km / 0.000

Inclination0° → 0°

Target Period0h 0m

True Anomaly0°

Mission Timeline

Orbit Warnings