calc all values

tle2ssc

@@ -8,11 +8,11 @@
 # tle2ssc foo-tle.txt
 
 import os
-import skyfield
 import math
+from math import remainder
 from datetime import datetime
-from skyfield.api import EarthSatellite, load, wgs84
 from sgp4.api import Satrec, WGS72
+from skyfield.api import EarthSatellite, load, wgs84
 
 xpdotp = 1440.0 / (2.0 * math.pi)
 
@@ -84,7 +84,7 @@ satellite_eccentricity=satellite.model.ecco
 satellite_arg_of_pericenter=math.degrees(satellite.model.argpo)
 
 #    Mean anomaly in radians.
-satellite_mean_anomoly=math.degrees(satellite.model.mo)
+satellite_mean_anomaly=math.degrees(satellite.model.mo)
 
 #    Mean motion in radians per minute.
 satellite_no_kozai=satellite.model.no_kozai
@@ -93,12 +93,18 @@ satellite_period=(1 / (satellite.model.no_kozai * xpdotp))
 #    Revolution number at epoch [Revs]
 satellite_revnum=satellite.model.revnum
 
-# SemiMajor Axis
+# Semi-Major Axis
 satellite_semimajor_axis=pow((pow(satellite_period,2) * 75371000000000),0.33333333)
 
+# Rotation Offset
+satellite_rotation_offset=((satellite_arg_of_pericenter)+(satellite_mean_anomaly)+360*
+	((2451545-satellite_epochdays)/satellite_period-
+	round((2451545-satellite_epochdays)/satellite_period)))
+
+# Output for .ssc file
 print('"', satellite_name, '-', satellite_number, '" ','"Sol/Earth" {',sep="")
 print('    Class "spacecraft"')
-print('    # Mesh "foo.3ds XXX"')
+print('    # Mesh "foo.3ds" XXX')
 print('    radius', satellite_radius)
 print()
 print('  EllipticalOrbit {')
@@ -109,11 +115,11 @@ print('    Eccentricity', satellite_eccentricity)
 print('    Inclination', satellite_inclination)
 print('    AscendingNode', satellite_ascending_node)
 print('    ArgOfPericenter', satellite_arg_of_pericenter)
-print('    MeanAnomaly', satellite_mean_anomoly)
+print('    MeanAnomaly', satellite_mean_anomaly)
 print('  }')
 print('  Obliquity', satellite_obliquity)
 print('  EquatorAscendingNode', satellite_equator_ascending_node)
-print('  RotationOffset  312.7348 XXX')
+print('  RotationOffset', satellite_rotation_offset)
 print('  # Orientation  [  ]')
 print('}')