[Isocops] IBEX Orbit# 130 Post Burn APogee Contact

[Ibex Mission Operations]

Guys,
   The apogee post burn contact was nominal for command/telemetry
The station power was increased from 277 watts to 370 watts to avoid
telemetry drop outs during the contact
@1628 ebno=19.67 - 20.94 db (2ksps)
agc signal strength= -121.584
@1649 ebno=19.73 - 20.72 db (2ksps)
agc signal strength= -119.902 with power increase

VC0=104/22


Orbit# 130b ATS  command vectors

    MPS Cmd Vector X -0.030163000 MPS Cmd Vector Y 0.921876000 MPS Cmd
Vector Z 0.386309000

Orbit# 130 post Apogee Burn Contact
    J2000 *Spin Axis* ECI X *-0.023411* ECI Y *0.917537* ECI Z *0.396961*

    0.01304900 ActNor.EstInrToBdy[0] -0.54895300 ActNor.EstInrToBdy[1]
-0.83575000 ActNor.EstInrToBdy[2] 0.00145723 ActNor.EstInrToBdy[3]     *
993057000.000* ActNor.EstTime

    *Precession Maneuver*    **  MPS Diff 0.765 deg   *MPS Diff should be <
1.5*


    *IBEX Spin Zxis (+Z S/C)* Right Ascension - RA *91.462* deg Declination
- DEC *23.388* deg                   *IBEX Spin Axis vs. Sun Vector* IBEX
Sun Angle *-2.472* deg


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