# Heliocentric trajectory of spacecraft # # ALL QUANTITIES HAVE TO BE GIVEN IN THE J2000 HELIOCENTRIC ECLIPTIC FRAME # PHASE NUMBER: 1 # DESCRIPTION: From the Earth to Asteroid XXXXXXX (SPKID) # Time (MJD) x (km) y (km) z (km) vx (km/s) vy (km/s) vz (km/s) mass (kg) Thrust_x (N) Thrust_y (N) Thrust_z (N) 0.57023500000123e+05 -0.27025737734192e+08 0.14459351078733e+09 -0.21938939142504e+04 -0.28767115533317e+02 -0.55852496269116e+01 0.1228771969598E-03 0.15000000000000e+04 -0.12345678901234e-01 0.12345678901234e-02 0.52345678901234e-01 0.57024500000123e+05 ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... 0.57123500000123e+05 ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... 0.57124500000123e+05 ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... 0.57124512300123e+05 ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... # PHASE NUMBER: 2 # DESCRIPTION: From Asteroid XXXXXXX to Asteroid YYYYYYY # Time (MJD) x (km) y (km) z (km) vx (km/s) vy (km/s) vz (km/s) mass (kg) Thrust_x (N) Thrust_y (N) Thrust_z (N) 0.57224500000789e+05 ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... 0.57225500000789e+05 ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... # PHASE NUMBER: 3 # DESCRIPTION: From Asteroid YYYYYYY to Asteroid ZZZZZZZ # Time (MJD) x (km) y (km) z (km) vx (km/s) vy (km/s) vz (km/s) mass (kg) Thrust_x (N) Thrust_y (N) Thrust_z (N) .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... # PHASE NUMBER: 4 # DESCRIPTION: From Asteroid ZZZZZZZ to Asteroid QQQQQQQ # Time (MJD) x (km) y (km) z (km) vx (km/s) vy (km/s) vz (km/s) mass (kg) Thrust_x (N) Thrust_y (N) Thrust_z (N) .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... .................... .................... ..................... .................... .................... ..................... ..................... .................... .................... .................... .................... ....................