#
# $Id: ems-moon.hnb,v 1.2 2002/05/08 20:26:47 rauch Exp $
#
# EMS driver values specific to the satellite integration.
#
# DE405 state vectors for JD 2440400.5 = 1969-Jun-28 00:00:00.0000 (TDB)
# in ICRF/J2000.0 reference frame.
#
include: ems-base.hnb

# Earth
M = 3.0034895963250727E-6
#OblateJ2  = 1.083e-3
#OblateRad = 4.263e-5

InputOrder: mass x1 x2 x3 v1 v2 v3

# Moon (EMRAT = 81.30056)
3.694303700152954E-8 \
 -8.081773279114836E-04 -1.994630001620399E-03 -1.087262660838102E-03 \
  6.010848166591268E-04 -1.674454606151511E-04 -8.556214497398488E-05


# Jupiter
#M=9.5473783030132410E-4
#
# Callisto (JCRAT = 17645)
#5.4108122998091476E-8 \
  6.674104269469700E-03 -9.586549910545399E-03 -4.460573906724564E-03 \
  4.022222368286020E-03  2.292115446800328E-03  1.143384432206465E-03


#
# These files are handled manually by the EMS driver.
#
OutputFile: ems-moon.dat
SaveFile:   ems-msave.dat