Acquiring signal
Interplanetary systems lab
Mars Mission Planner · Beta
Browser simulation
Heliocentric model
Earth to Mars Transfer
Top-down view · J2000 ecliptic plane
- Earth orbit
- Mars orbit
- Schematic transfer
Transfer output
Scenario Results
Key indicators for the selected model.
- Transit time
- 210days
- Earth departure C3
- 13.9km²/s²
- Mars arrival excess speed
- 5.15km/s
- Result confidence
- illustrative
Default Earth–Mars scenario ready.