# This file contains the orbital elements in Celestia's SSC format.
# for ESA's INTEGRAL satellite
#
# The information was obtained from JPL's Horizons ephemeris server
# Nov 22. 2002.
# by Selden Ball seb+cel@lns.cornell.edu 
#
# Integral satellite model courtesy of 
#  <a href="http:sci.esa.int/integral">ESA</a>
#
"INTEGRAL" "Sol/Earth"
{
	Class "spacecraft"
	Mesh "integral.cmod" # warning: 5MB
	Radius 0.003       #4x4x6 meters w/o solar panels
#	EllipticalOrbit
#	{
#2452600.500000000 = A.D. 2002-Nov-22 00:00:00.0000 (CT)
# EC= 8.234577927435308E-01 QR= 1.548414639838864E+04 IN= 5.305319831508738E+01
# OM= 1.014890638402147E+02 W = 3.024416289547550E+02 Tp= 2.452599790605179E+06
# N = 1.203225930959157E+02 MA= 8.535622442451043E+01 TA= 1.613366092163504E+02
# A = 8.770790078484899E+04 AD= 1.599316551713093E+05 PR= 2.991956794955576E+00
#		Period            2.991956794955576E+00
#		SemiMajorAxis     8.770790078484899E+04 
#		Eccentricity      8.234577927435308E-01 
#		Inclination       5.305319831508738E+01
#		AscendingNode     1.014890638402147E+02 
#		ArgOfPericenter   3.024416289547550E+02 
#                MeanAnomaly       8.535622442451043E+01 
#		Epoch       2452600.5
#	}
   Albedo            0.7
   SampledOrbit "integral_orbit.xyz"
   SampledOrientation "integral.q"
   BodyFrame { EquatorJ2000 { Center "Sol/Earth" } }
}