PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM DATA_RECORDS = 10307 INSTRUMENT_NAME = "MARS EXPRESS ORBITER RADIO SCIENCE" TARGET_NAME = MARS DATA_SET_ID = "MEX-M-MRS-1/2/3-MCO-0084-V1.0" MISSION_NAME = "MARS EXPRESS" INSTRUMENT_HOST_NAME = "MARS EXPRESS" INSTRUMENT_HOST_ID = "MEX" STANDARD_DATA_PRODUCT_ID = OPT PRODUCT_ID = "M00DSN0L1A_OPT_041711402_00.TXT" SOURCE_PRODUCT_ID = "optg_mex_040511-040707" START_TIME = 2004-05-11T00:00:00 STOP_TIME = 2004-07-07T00:00:00 PRODUCT_CREATION_TIME = 2005-08-10T16:40:18.000 PRODUCER_ID = "NAV" DESCRIPTION = " The Orbit Propagation and Timing Geometry (OPT) file was generated at the NASA Jet Propulsion Laboratory to facilitate JPL/DSN support of Mars Express (MEX). It was derived from materials provided by the MEX Project. The OPT is an ASCII file having several header records followed by a table of time-ordered orbit events (equator crossings, occultations, eclipses, periapsis times, etc.). The table columns are separated by commas and are defined as follows: 1. event title (e.g., PERIAP for periapsis passage) 2. body name (e.g., MARS) 3. spacecraft ephemeris time of event (yyyy-dddThh:mm:ss.fff format) 4. Julian date 5. ET-UTC 6. orbit number 7. time from periapsis (sDDDDDThh:mm:ss.fff format) 8. Sun-Earth-probe angle (degrees) After certain event lines, there are listings of body constants. For example, after the ascending equator crossing line, there is a single line giving the spacecraft longitude. For more details on file contents and format see OPTG_SIS.TXT in the DOCUMENT directory of this archive. " ^TEXT = "M00DSN0L1A_OPT_041711402_00.TXT" OBJECT = TEXT PUBLICATION_DATE = 2004-05-11 NOTE = "N/A" END_OBJECT = TEXT END