PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM OBJECT = TEXT INTERCHANGE_FORMAT = ASCII PUBLICATION_DATE = 2015-06-03 NOTE = "This file describes the files in the extras/orbnum directory of this volume." END_OBJECT = TEXT END Orbit Number Files for the Mars Reconnaissance Orbiter Mission ============================================================== This directory contains the orbit number files generated during the mission using the NAIF's ORBNUM utility program for some the final merged spacecraft trajectory SPK files for the orbital phases of the mission. Normally the orbit number files have the same names as the corresponding SPK files but with the extension ``.bsp'' replaced by ``.orb'' or ``.nrb''. In a few cases more than one orbit number file may exist for a given SPK, with only one file having the same name as the SPK and other files having a version token appended to the SPK name. In such cases the orbit number file with the latest version in the name supersedes all other orbit number files for that SPK. The orbit number files are plain ASCII text files that have lines terminated with a line feed character, LF (ASCII 10). The orbit number files with the ``.orb'' extension contain data that follow the ``periapsis-to-periapsis'' orbit numbering scheme -- with the orbit number changing at periapsis. The orbit number files with the ``.nrb'' extension contain data that follow the ``node-to-node'' orbit numbering scheme -- with the orbit number changing at the descending node. The information contained in the orbit number files includes the orbit number (``No.''), periapsis or descending node UTC time (``Event UTC PERI'' or ``Event UTC D-NODE'') and SCLK time (``Event SCLK PERI'' or ``Event SCLK D-NODE'' ), apoapsis or ascending UTC time (``OP-Event UTC APO'' or ``OP-Event UTC A-NODE''). It also includes a few additional items computed at the time of periapsis or descending node such as planetocentric subsolar longitude and latitude (``SolLon'' and ``SolLat'') in the Mars body-fixed frame based on the IAU 2000 Mars rotation model, planetocentric subspacecraft longitude and latitude (``SC Lon'' and ``SC Lat'') in the Mars body-fixed frame based on the IAU 2000 Mars rotation model, spacecraft altitude above Mars (``Alt'') relative to the IAU 2000 Mars ellipsoid, and Sun-Mars distance (``Sol Dist''). Contact Information =================== Regarding Mars Reconnaissance Orbiter project specific information provided in this data set and for general information about SPICE system, contact: Boris Semenov (818)-354-8136 Boris.Semenov@jpl.nasa.gov address: Navigation and Ancillary Information Facility (NAIF) Jet Propulsion Laboratory MS 301-125L 4800 Oak Grove Drive Pasadena CA 91109 USA