[Isocops] Fwd: IBEX Goat Herder 12 July 10
Ibex Mission Operations
ibexops at gmail.com
Mon Jul 12 07:42:00 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
--
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
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