[Isocops] IBEX Orbit# 86 J2000 Vectors

[Ibex Mission Operations]

J2000
*Spin Axis*   ECI X *-0.566786*   ECI Y *0.751292*   ECI Z *0.338103*
  *Precession Maneuver*   Cmd Diff *165.090* deg MPS Diff *0.684* deg   *MPS
Diff should be < 1.5*


    0.23105700 ActNor.EstInrToBdy[0] -0.52684100 ActNor.EstInrToBdy[1]
-0.79585100 ActNor.EstInrToBdy[2] 0.18887400 ActNor.EstInrToBdy[3]    *
964266000.000* ActNor.EstTime


    J2000 *Spin Axis* ECI X *-0.566786* ECI Y *0.751292* ECI Z *0.338103*


    *IBEX Spin Zxis (+Z S/C)* Right Ascension - RA *127.031* deg Declination
- DEC *19.761* deg                   *IBEX Spin Axis vs. Sun Vector* IBEX
Sun Angle *0.681* deg




The Goat Herder will be sent out this afternoon after I get some sleep
-- 
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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