[Isocops] IBEX Orbit# 227 SSR_Dump/Tracking Contact

[Ibex Mission Operations]

The SSR_Dump/Tracking Contact for ORbit# 227 was nominal for
command/telemetry and the
inertial maneuver successful.
The following objectives were accomplished


1. reset_master_timer.scr
2. ops_set_sc_time.scr
3. SSR_Dump.scr (new)
4. CAR#656 Upload Orbit# 228 IBEX_Lo Gain Test
1.IBEX_2013_333_o0228a_lgc_v001.scr(5-58)
5. CAR#657 Upload Orbit# 229 ATS 1.IBEX_2013_342_o0229a_v001.scr (59-142)
IBEX Orbit# 227 PERIGEE Target Vectors
J2000 Spin Axis
ECI X -0.430129
ECI Y -0.828905
ECI Z -0.357640

Precession Maneuver
MPS Diff 0.780 deg
 *MPS Diff should be < 1.5 *

0.82374200 ActNor.EstInrToBdy[0]
-0.01639940 ActNor.EstInrToBdy[1]
-0.25096600 ActNor.EstInrToBdy[2]
0.50813000 ActNor.EstInrToBdy[3]
1069760000.000 ActNor.EstTime
Right Ascension - RA 242.575 deg
Declination - DEC -20.955 deg

IBEX Spin Axis vs. Sun Vector
IBEX Sun Angle -2.905 deg

    CSS Angle TLM 1.12709  CSS Sun-Pointing Angle 2.25418  25 Nov 13 @0600 CSS
Angle TLM 0.989525  CSS Sun-Pointing Angle 1.97905  29 Nov 13 @1100
*Pre-Burn*     Thruster 1 8752 25 Nov 13 @0600 Thruster 2 8528  Thruster 3
9264  Thruster 4 9488  *Post-Burn*   Thruster 1 9056 25 Nov 13 @0600 Thruster
2 8832  Thruster 3 9568  Thruster 4 9792  *Number of Pulses*    Thruster 1
304  Thruster 2 304  Thruster 3 304  Thruster 4 304  *Thruster Pairs*
 Thruster
1 & 2 608  Thruster 3 & 4 608

-- 
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
CYGNUS Mission Planning
(304) 279-6678
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