| Fixed point: | |
| Orbit | |
| Body | |
| Semi-major axis (km) | |
| Periapsis radius (km) | |
| Apoapsis radius (km) | |
| Periapsis altitude (km) | |
| Apoapsis altitude (km) | |
| Eccentricity | |
| Period (sec) | |
| Position | |
| Distance (km) | |
| Altitude (km) | |
| Speed (km/s) | |
| Mean anomaly | |
| Eccentric anomaly | |
| True anomaly | |
| Hohmann transfer | |
| Orbit 1 altitude | |
| Orbit 1 radius | |
| Orbit 2 altitude | |
| Orbit 2 radius | |
| Burn 1 (m/s) | {{hohmannBurn1}} |
| Burn 2 (m/s) | {{hohmannBurn2}} |
| Total (m/s) | {{hohmannTotal}} |
| Rocket | |
| Fuel mass (kg) | |
| Empty mass (kg) | |
| Full mass (kg) | |
| Specific impulse (s) | |
| Specific impulse (m/s) | |
| Delta-V (m/s) | |