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About THEMIS
The Thermal Emission Imaging System (THEMIS) is an instrument on board the Mars Odyssey spacecraft. It combines a 5-wavelength visual imaging system with a 9-wavelength infrared imaging system.
The orbiter launched from Kennedy Space Center on April 7, 2001 and arrived at Mars on October 24, 2001. The orbiter spent the next several months achieving a circular mapping orbit by aerobraking (dipping into the atmosphere to slow and shrink the orbit). Aerobraking concluded in early February 2002, and primary mapping operations began a few weeks later.
Read more about THEMIS at ASU's THEMIS site.
The orbiter launched from Kennedy Space Center on April 7, 2001 and arrived at Mars on October 24, 2001. The orbiter spent the next several months achieving a circular mapping orbit by aerobraking (dipping into the atmosphere to slow and shrink the orbit). Aerobraking concluded in early February 2002, and primary mapping operations began a few weeks later.
Read more about THEMIS at ASU's THEMIS site.
THEMIS: V58476006
Image Data
Click on the field name to see the glossary definition for that field.
| Name | Value | Type | Idx |
|---|---|---|---|
| Image ID | V58476006 | Basic | 10 |
| Description | No Description Given | Basic | 11 |
| Band Numbers | (1, 2, 3, 4) | Basic | 12 |
| Start Timestamp | 2015-02-18 15:13:10.924 | Basic | 13 |
| Duration (sec) | 17 | Basic | 14 |
| Resolution (km) | 0.031924 km | Basic | 15 |
| Local Time (24.0 hr) | 16.099855 | Basic | 16 |
| Start Time (et) | 477544448 | Advanced | 17 |
| orbit | 58476 | Basic | 18 |
| Start Time (sclk) | 1108740152.204 | Advanced | 19 |
| Solar Longitude | 293.71863° | Basic | 20 |
| Summing | 2 | Advanced | 21 |
| Geometry Level | R | Advanced | 22 |
| Mars Year | 32 | Basic | 23 |
| Center Latitude | -80.77127° | Basic | 24 |
| Incidence Angle | 62.925583° | Advanced | 25 |
| Center Longitude | 296.63412° | Basic | 26 |
| Solar Distance | 1.4132138 | Advanced | 27 |
| MOLA Avg | 0 | Advanced | 28 |
| North Azimuth Angle | 250.17577° | Basic | 29 |
| Albedo Min | 0.172 | Advanced | 30 |
| Emission Angle | 0.459919° | Basic | 31 |
| Avg Albedo | 0.265 | Advanced | 32 |
| Spacecraft Orientation | (0,0,0) | Basic | 33 |
| Albedo Max | 0.393 | Advanced | 34 |
| Pointing Mode | NADIR | Basic | 35 |
| IR Calibration Flag | 0 | Advanced | 36 |
| Image Rating | 5 | Basic | 37 |
| Max Brightness Temperature | 0 | Advanced | 38 |
| Release ID | 0053 | Basic | 39 |
| Min Brightness Temperature | 0 | Advanced | 40 |
| Product Modification Date | 2017-08-05 | Basic | 41 |
| Avg Surface Temp | 0 | Advanced | 42 |
| Avg Dust Opacity | 0 | Advanced | 43 |
| Avg Water Ice Opacity | 0 | Advanced | 44 |
| THM Band10 Temp | 0 | Advanced | 45 |
| TES Band10 Temp | 0 | Advanced | 46 |
| TES Albedo Avg | 0.176 | Advanced | 47 |
| TES Thermal Inertia Avg | 0 | Advanced | 48 |
| TES Rock Abundance Avg | 0 | Advanced | 49 |
About THEMIS
The Thermal Emission Imaging System (THEMIS) is an instrument on board the Mars Odyssey spacecraft. It combines a 5-wavelength visual imaging system with a 9-wavelength infrared imaging system.
The orbiter launched from Kennedy Space Center on April 7, 2001 and arrived at Mars on October 24, 2001. The orbiter spent the next several months achieving a circular mapping orbit by aerobraking (dipping into the atmosphere to slow and shrink the orbit). Aerobraking concluded in early February 2002, and primary mapping operations began a few weeks later.
Read more about THEMIS at ASU's THEMIS site.
The orbiter launched from Kennedy Space Center on April 7, 2001 and arrived at Mars on October 24, 2001. The orbiter spent the next several months achieving a circular mapping orbit by aerobraking (dipping into the atmosphere to slow and shrink the orbit). Aerobraking concluded in early February 2002, and primary mapping operations began a few weeks later.
Read more about THEMIS at ASU's THEMIS site.