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
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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
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