[Isocops] IBEX Goat Herder 12 July 10

Ibex Mission Operations ibexops at gmail.com
Mon Jul 12 06:30:21 EDT 2010


Nominal perigee contacts for Orbit# 84.
The SSR and flight computer were dumped.

*Upcoming Orbit# 85 Contacts are listed below in UTC
IBEX,USHI01,ADD,07/15/10,196,14:00:00,07/15/10,196,14:35:00,,LAHO 2K IBEX
Orbit# 85 Apogee Contact
IBEX,USAK01,ADD,07/19/10,200,11:00:00,07/19/10,200,12:10:00,,LAHO 160K IBEX
Orbit# 85 SSR_Dump/Tracking
IBEX,USHI01,ADD,07/20/10,201,07:30:00,07/20/10,201,08:05:00,,LAHO 2K IBEX
Orbit# 85 Tracking Contact *

IBEX Target Vectors  12 July 10
Orbit# 84 MPS Vectors
MPS Cmd Vector X= -0.346602980
MPS Cmd Vector Y= 0.860471570
MPS Cmd Vector Z= 0.373436790

Target Vectors 12July10 @0800 UTC
-0.55213500=ActNor.EstInrToBdy[0]
-0.05103500=ActNor.EstInrToBdy[1]
0.23841000=ActNor.EstInrToBdy[2]
0.79731000=ActNor.EstInrToBdy[3]
962957000.000=ActNor.EstTime

J2000  Spin Axis
ECI X= -0.344650
ECI Y= 0.856111
ECI Z= 0.385085

Precession Maneuver
MPS Diff=0.721 deg
***MPS Diff should be < 1.5***

IBEX Spin Zxis (+Z S/C)
Right Ascension - RA= 111.929 deg
Declination - DEC=  22.649 deg

IBEX Spin Axis vs. Sun Vector
IBEX Sun Angle= 0.785 deg



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