sucess launch 19 december
First maneuver:
Perigee changed to 35786km
Inclination changed to 1.4563 degrees
Current Orbit: 35786.0000 km x 68931.0000 km x 1.4563 degrees;
Apogee Speed: 1949.2716 m/s; Perigee Speed: 3481.8429 m/s; delta v to this orbit: 1187.6282
Second maneuver:
Apogee changed to 35786km
Inclination changed to 0 degrees
Current Orbit: 35786.0000 km x 35786.0000 km x 0.0000 degrees;
Apogee Speed: 3074.9218 m/s; Perigee Speed: 3074.9218 m/s; delta v to this orbit: 1602.9613