Console

This tab will contain alphanumeric output data displayed for each propagation. Basically, you will only have information as follows:

---------------- PSIMU ---------------- Propagation starts ... Initial conditions: Date (UTC): 2000-01-01T00:00:00.000 Frame: EME2000 Mass: 0.000 kg Geocentric altitude: 621.864 km Geodetic altitude: 621.864 km Semi major axis: 7000.000 km Eccentricity: 0.00000001 Inclination: 0.000 deg RAAN: 112.312 deg Argument of perigee: -112.312 deg Mean anomaly: -0.000 deg Final conditions: Final Date (UTC): 2000-01-02T00:00:00.000 Propagation duration: 86400.000 s Frame: EME2000 Mass: 0.000 kg Geocentric altitude: 621.864 km Geodetic altitude: 621.864 km Semi major axis: 7000.000 km Eccentricity: 0.00000001 Inclination: 0.000 deg RAAN: 112.312 deg Argument of perigee: -112.311 deg Mean anomaly: -63.481 deg Propagation ends Computation time for propagation: 3.487 seconds

But if you activate the debug mode ...

... you will obtain more information with at least initial and final Keplerian and Cartesian parameters:

---------------- JPSIMU ---------------- Initial conditions: Date (TAI) 2010-01-01T00:00:34.000 Frame EME2000 Mass (kg) 1000.0 T (h) 1.5086600770138687 A (km) 6678.136300000004 Ex -1.685973170121102E-16 Ey -4.1084080980541744E-16 Inc (deg) 4.9894244122984115E-6 Raan (deg) 112.31184620490887 X (km) 6678.136299999963 Y (km) 4.7269715122624133E-4 Z (km) -5.380051773266002E-4 Vx (km/s) -5.468509500470877E-7 Vy (km/s) 7.725760634075565 Vz (km/s) -2.554168051610141E-7 Propagation starts... Propagation ends Final conditions: Date (TAI) 2010-01-02T00:00:34.000 Frame EME2000 Mass (kg) 1000.0 T (h) 1.5083455172945863 A (km) 6677.207973520151 Ex -1.2697350060411008E-5 Ey 6.069045286482817E-4 Inc (deg) 0.008726511065778222 Raan (deg) 175.41590951266258 X (km) 6437.012577231219 Y (km) -1771.6342519476977 Z (km) 0.1906124882201188 Vx (km/s) 2.054926497916515 Vy (km/s) 7.4490312552975135 Vz (km/s) -0.0011559194205059266 Computation time for propagation: 3.646 seconds