# This file contains the orbital elements in Celestia's SSC format.
# for the near-earth asteroid 1994 XM1
# before and after its flyby of the Earth
# by Selden Ball seb+cel@lns.cornell.edu 
#
# The ephemeris information was obtained from Horizons
# The NEO info was obtained from the IAU's Minor Planet Center
# at http://cfa-www.harvard.edu/iau/mpc.html
# on their page http://cfa-www.harvard.edu/iau/lists/Closest.html
#
#Distance  Date (TT)       Permanent designation   Provisional   H     Reference
#0.0007 *  1994 Dec.  9.8                          1994 XM1     28.0   MPEC 1994-X05
# *   This approach is to within 112000 km = 70000 miles.
#
"1994 XM1-1" "Sol"
{
	Class           "moon"   # to show orbit even when not selected
	Mesh    "asteroid.cms"
        Texture "asteroid.jpg"
	Radius            0.005
        Albedo            0.2

#2449504.500000000 = A.D. 1994-Jun-01 00:00:00.0000 (CT)
# EC= 5.500738531020368E-01 QR= 8.966996055338805E-01 IN= 5.598040705719483E+00
# OM= 7.716210863977393E+01 W = 4.198143625921699E+01 Tp= 2.449726986913055E+06
# N = 3.503042887669860E-01 MA= 2.820618801622164E+02 TA=-1.371927240605005E+02
# A = 1.992992876089149E+00 AD= 3.089286146644417E+00 PR= 1.027677968965614E+03
	EllipticalOrbit
	{
		Period            2.813575797403461
		SemiMajorAxis     1.992992876089149E+00 
		Eccentricity      5.500738531020368E-01 
		Inclination       5.598040705719483E+00
		AscendingNode     7.716210863977393E+01 
		ArgOfPericenter   4.198143625921699E+01 
                MeanAnomaly       2.820618801622164E+02 
		Epoch       2449504.5
	}
}
"1994 XM1-2" "Sol"
{
	Class           "moon"   # to show orbit even when not selected
	Mesh    "asteroid.cms"
        Texture "asteroid.jpg"
	Radius            0.005
        Albedo            0.2

#2449869.500000000 = A.D. 1995-Jun-01 00:00:00.0000 (CT)
# EC= 5.662749379488603E-01 QR= 8.988497355733488E-01 IN= 4.595446744254060E+00
# OM= 7.703199831837411E+01 W = 4.117337105729801E+01 Tp= 2.449726187537481E+06
# N = 3.303658958727397E-01 MA= 4.734555006999492E+01 TA= 1.150956950753782E+02
# A = 2.072395197368989E+00 AD= 3.245940659164630E+00 PR= 1.089700857435586E+03
	EllipticalOrbit
	{
		Period            2.983382004361280
		SemiMajorAxis     2.072395197368989E+00 
		Eccentricity      5.662749379488603E-01 
		Inclination       4.595446744254060E+00
		AscendingNode     7.703199831837411E+01 
		ArgOfPericenter   4.117337105729801E+01 
                MeanAnomaly       4.734555006999492E+01 
		Epoch       2449869.5
	}
}