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CASSINI SATURN MIMI INCA CALIBRATED DATA ARCHIVE
CO-S-MIMI-4-INCA-CALIB-V1.0	PDS 3 CERTIFIED

Start Time: 2004-01-01 16:00:00 - Stop Time: 2017-09-15 03:28:13

CASSINI SATURN MIMI INCA CALIBRATED DATA ARCHIVE

Citiation Information

Author	Vandegriff J., Kusterer M.B.
Title	CASSINI SATURN MIMI INCA CALIBRATED DATA ARCHIVE
Publisher	NASA Planetary Data System
Publication Year	2018
doi	https://doi.org/10.17189/1519607

Top/ DATA/ ANCILLARY/ MIMI_SPIN /

MIMI_SPIN_1999_01

Start Time:	1999-001T00:00:00.000	Stop Time:	1999-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2000_01

Start Time:	2000-001T00:00:00.000	Stop Time:	2000-366T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2001_01

Start Time:	2001-001T00:00:00.000	Stop Time:	2001-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2002_01

Start Time:	2002-001T00:00:00.000	Stop Time:	2002-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2003_01

Start Time:	2003-001T00:00:00.000	Stop Time:	2003-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2004_01

Start Time:	2004-001T00:00:00.000	Stop Time:	2004-366T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2005_01

Start Time:	2005-001T00:00:00.000	Stop Time:	2005-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2006_01

Start Time:	2006-001T00:00:00.000	Stop Time:	2006-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2007_01

Start Time:	2007-001T00:00:00.000	Stop Time:	2007-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2008_01

Start Time:	2008-001T00:00:00.000	Stop Time:	2008-366T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2009_01

Start Time:	2009-001T00:00:00.000	Stop Time:	2009-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2010_01

Start Time:	2010-001T00:00:00.000	Stop Time:	2010-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2011_01

Start Time:	2011-001T00:00:00.000	Stop Time:	2011-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2012_01

Start Time:	2012-001T00:00:00.000	Stop Time:	2012-366T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2013_01

Start Time:	2013-001T00:00:00.000	Stop Time:	2013-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2014_01

Start Time:	2014-001T00:00:00.000	Stop Time:	2014-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2015_01

Start Time:	2015-001T00:00:00.000	Stop Time:	2015-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2016_01

Start Time:	2016-001T00:00:00.000	Stop Time:	2016-366T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

MIMI_SPIN_2017_01

Start Time:	2017-001T00:00:00.000	Stop Time:	2017-365T23:59:59.999
The MIMI stare/spin mode files are comma delimited files, containing either spin or stare mode start and stop times, spin mode, spin direction and spin direction validity values. The spin and stare modes are determined by the MIMI DPU using the current spacecraft spin rate about the spacecraft Z axis. The values are (0=Stare, 1=Spin). Spin and stare mode does affect how INCA images are collected. The spin direction flag values are (0 = clockwise, 1 = counter clockwise and 2 = both). During some spacecraft manuvers, the instrument interprets the motion as a spin about the spacecraft Z axis, and can erroneously detect both directions. These spins will be reported to have a spin direction as 2. The validity flag values are (0 = invalid (or for stare mode), 1 = valid). The spin direction validity flag is only included when the instrument detects a spin and is 0 otherwise. During spacecraft spin up and spin down periods, the spin direction can be difficult to detect and if the spin is short and the direction value is not trusted, it will be marked as invalid.

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