[Isocops] Fwd: IBEX Goat Herder 12 July 10

[Ibex Mission Operations]

 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



-- 
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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	IBEX Goat Herder  12 July 10
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	
	

Date
	Sunday, July 11, 2010
Jday	Time	Station	Controller	CAR1	CAR2	CAR3	Razor#	USNPR#	Radius 	S-Band Rate
192	    1900	USAK	TPerry	    398	                                   10 Desc	  320ksps
VC 0	VC 0 Seq Err	VC 1	VC 1 Seq Err	VC 2	VC 2 Seq Err 	PASS/FAIL
803	          0	                             	19671	     0	           Pass
VC 2 Write Pointer Start	0	VC 2 Write Pointer End	0
VC 2 Read Pointer 	0	VC 2 Read Pointer End	0
Dumped SSR 
CAR 396 ATS upload  IBEX_2010_200_00_00_v001  52 cmds (817 - 868)
Reset the master timer 
Updated the SC Clock
	
 
Date
	Monday, July 12, 2010
Jday	Time	Station	Controller	CAR1	CAR2	CAR3	Razor#	USNPR#	Radius 	S-Band Rate
193	    0800	AUWA	SWesley	                                            11 asc	  160ksps
VC 0	VC 0 Seq Err	VC 1	VC 1 Seq Err	VC 2	VC 2 Seq Err 	PASS/FAIL
544	          3	         321	       0	                               Pass
VC 2 Write Pointer Start	35748	VC 2 Write Pointer End	35773
VC 2 Read Pointer 	34415	VC 2 Read Pointer End	34415
Orbit# 84 tracking contact
@ACT_FDC_ResetTaskRawFailed(AC_FDC)
@FTG_DumpBackOrbit(from start,0,0,0,0) 
@0802 ebno= 7-9 dbm
@0818 ebno= 7-9 dbm
@FMI_SetDownlink320K  ebno=3.6-6 dbm
@0819 FMI_SetDownlink2K
ebno= 28-29 dbm
autotrack

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