[Isocops] IBEX Orbit#156 Post apogee Sun Maneuver

[Ibex Mission Operations]

Guys,
    The Post Sun Maneuver contact for Orbit # 156 was successful for
command/telemetry.
The contact occured at 95% sta_pct_valid

    0.76820400 ActNor.EstInrToBdy[0] -0.11431300 ActNor.EstInrToBdy[1]
0.58150400 ActNor.EstInrToBdy[2] 0.24217600 ActNor.EstInrToBdy[3]     *
1013630000.000* ActNor.EstTime


    *IBEX Spin Zxis (+Z S/C)* Right Ascension - RA *328.926* deg Declination
- DEC *-11.912* deg                   *IBEX Spin Axis vs. Sun Vector* IBEX
Sun Angle *-2.683* deg






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