[Isocops] IBEX Orbit# 159 Apogee Contact

[Ibex Mission Operations]

Guys,
   The Apogee contact for Orbit# 159 was nominal for command/telemetry.
The Sun Maneuver was successful.
The staticZrate will be set on the next contact when we are >90% valid.

1. StaPctValid=59%
2. StaticZRate rpm=4.16641
3. SpinRate (ST)=4.17041

VC0=396 with 4 errors
VC1=1453 with 29 errors


    CSS Angle TLM 1.68109  CSS Sun-Pointing Angle 3.36218  3/11/2012 21:09 CSS
Angle TLM 1.1896  CSS Sun-Pointing Angle 2.3792  3/16/2012 18:36   *Pre-Burn
*   3/11/2012 21:09 Thruster 1 1680  Thruster 2 1632  Thruster 3 1840  Thruster
4 1888  *Post-Burn* ** 3/16/2012 18:36 Thruster 1 2032  Thruster 2
1984  Thruster
3 2240  Thruster 4 2288  *Number of Pulses* ** ** Thruster 1 352  Thruster 2
352  Thruster 3 400  Thruster 4 400  *Thruster Pairs* ** ** Thruster 1 & 2
704  Thruster 3 & 4 800



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