Constants:
   Earth radius: 6371000 meter
   Earth mass: 5.97219e+24 kg
   Gravity: 6.67384e-11
   mu: 398574405096000

Source orbit is using eccentricity notation, converting...
Converting to meter...
Adding earth radius...
Orbital parameters for Source orbit:
   Periapsis: 6871000 m
   Apoapsis: 7871000 m
   Inclination: 0 deg

Converting to meter...
Adding earth radius...
Orbital parameters for Target orbit:
   Periapsis: 7371000 m
   Apoapsis: 7371000 m
   Inclination: 10 deg

Calculating semi major axis...
Defining Hohman orbit...
Orbital parameters for Hohman orbit:
   Periapsis: 6871000 m
   Apoapsis: 7371000 m
   Inclination: 0 deg

Calculating first burn...
Data for burn at source orbit periapsis:
   Speed before burn: 7870.39409917514 m/s
   Speed after burn: 7748.85334888779 m/s
   Required Delta-V: 121.540750287353 m/s

Calculating second burn...
Need to include plane change in second burn...
Data for burn at Hohman orbit apoapsis:
   Speed before burn: 7223.22227109049 m/s
   Speed after burn: 7353.45599234394 m/s
   Inclination before burn: 0 deg
   Inclination after burn: 10 deg
   Inclination change: 10 deg
   Required Delta-V: 1277.04850388302 m/s

Total Delta-V requirement: 1398.58925417037 m/s