[Isocops] IBEX Orbit# 114 SSR_Dump Contact 25 Feb 11 @ 1945 UTC

[Ibex Mission Operations]

Guys,
     Here are the current J2000 Target Vectors after the inertial maneuver
25 Feb 11 @ 1836 UTC
The ATS for ORbit# 116 was uploaded and the SSR was dumped with (0) errors
VC1=1492/1
VC2= 19532/0


    J2000 *Spin Axis* ECI X *0.925310* ECI Y *-0.352226* ECI Z *-0.140492*

    0.60505400 ActNor.EstInrToBdy[0] 0.45183600 ActNor.EstInrToBdy[1]
0.35135200 ActNor.EstInrToBdy[2] 0.55344900 ActNor.EstInrToBdy[3]     *
982699000.000* ActNor.EstTime

    *IBEX Spin Zxis (+Z S/C)* Right Ascension - RA *339.160* deg Declination
- DEC *-8.076* deg                   *IBEX Spin Axis vs. Sun Vector* IBEX
Sun Angle *1.091* deg


    *Precession Maneuver*    **  MPS Diff 0.631 deg   *MPS Diff should be <
1.5*

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