body.frame = GTOD/1996 without EOP
inertial.frame = EME2000

orbit.date = 2015-08-29T05:12:02.000
orbit.keplerian.a = 29233.2378
orbit.keplerian.e = 0.017822
orbit.keplerian.i = 55.0025
orbit.keplerian.raan = 211.0774
orbit.keplerian.pa = 176.2165
orbit.keplerian.anomaly = 223.193
orbit.angle.type = TRUE

initial.orbit.is.osculating = false
output.orbit.is.osculating = false

central.body.rotation.rate = 7.2921e-05
central.body.degree = 8
central.body.order = 8

max.degree.zonal.short.periods = 8
max.eccentricity.power.zonal.short.periods = 4
max.frequency.true.longitude.zonal.short.periods = 17
max.degree.tesseral.short.periods = 8
max.order.tesseral.short.periods = 8
max.eccentricity.power.tesseral.short.periods = 4
max.frequency.mean.longitude.tesseral.short.periods = 12
max.degree.tesseral.m.dailies.short.periods = 8
max.order.tesseral.m.dailies.short.periods = 8
max.eccentricity.power.tesseral.m.dailies.short.periods = 4

third.body.moon = true
third.body.sun = true

drag = false
drag.cd = 2.2
drag.sf = 25

solar.radiation.pressure = true
solar.radiation.pressure.cr = 1.2
solar.radiation.pressure.sf = 25

duration.in.days = 1826.25
output.step = 86400

output.Keplerian = true
output.equinoctial = false
output.Cartesian = false
output.short.period.coefficients = none

min.variable.integration.step = 6000
max.variable.integration.step = 86400
position.tolerance.variable.integration.step = 1

max.time.gap.between.interpolation.points = 86400

numerical.comparison = false