PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM OBJECT = TEXT INTERCHANGE_FORMAT = ASCII PUBLICATION_DATE = 2016-01-04 NOTE = "This file describes the files in the extras/orbnum directory of this volume." END_OBJECT = TEXT END Orbit number files for the Mars Odyssey 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", for example the ORBNUM file corresponding to the SPK "m01_ext31.bsp" has the name "m01_ext31.nrb". For a few intervals though the originally archived orbit number files contained incorrect data (orbit numbers were off by one). In such cases an additional orbit number file is present for each of such intervals and the name of this file includes the suffix "_fixed", for example for the SPK "m01_ext32.bsp" the incorrect orbit number file is "m01_ext32.nrb" while the correct one is "m01_ext32_fixed.nrb". In all cases when a "_fixed" file is present it supersedes the original file. All ORBNUM files are plain ASCII text files. 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 ("Periapsis UTC" or "Desc-Node UTC") and SCLK time ("Periapsis SCLK" or "Node SCLK" ), apoapsis or ascending UTC time ("Apoapsis UTC" or "Asc-Node UTC"). 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 Odyssey 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