PDS_VERSION_ID = PDS3 RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 80 OBJECT = TEXT PUBLICATION_DATE = 1998-04-11 NOTE = "Description of GEODYN SPK Files" END_OBJECT = TEXT END GEODYN SPK files (data type GDN) are QUICK LOOK orbits produced by the MOLA POD (Precise Orbit Determination) team. They are used for preliminary analysis of the MOLA data, and have been made available to other MGS project participants. They are produced on a best efforts basis, as time and resources permit. Each file is in SPK format, compatible with readers in the SPICE toolkit (see companion files TK_FTP.TXT, TK_DESC.TXT, and TK_INSTL.TXT in this DOCUMENT directory for more information on the SPICE toolkit and files). The data were orginally written out by GEODYN (the orbit processor) at five or ten second intervals. They were converted from the original true of date (IAU of date) coordinates to J2000, and then were written in an SPK-format (type 8, discrete states, evenly spaced, Lagrange Interpolation). A TOPEX-like/POE (ASCII) format is available upon request from the MOLA POD Team. File names have the format gdn_qlnn.ymmddhhmm.ymmddhhmm.tsp where the components refer to: gdn derived from analysis using the GEODYN orbit processor; ql quick-look; nn version number; yymmddhhmm start and stop times tsp suffix designating an SPK transfer file Files can also be obtained via anonymous ftp from geodesy.gsfc.nasa.gov (node number 128.183.201.91). Change directories (Unix command "cd") to directory /dist/MGS/quick-look-orbits/ and retrieve the data of interest. Each orbit was produced from a preliminary analysis of the Doppler and range data supplied by the DSN. They are preliminary because certain ancillary information may have been missing at the time the orbits were reconstructed -- for example, the dates and times of momentum dumps, weather data (used for Earth troposphere refraction corrections), and finalized Earth orientation (polar motion) values. The a priori modeling included the GMM-1 gravity field, the 1991 IAU model, the Stewart (LASP-JPL Internal Rep., PO\#NQ-802429, Jet Propulsion Laboratory, Pasadena, CA, March 1987) drag model, and the JPL DE403 ephemeris. For each arc, the state vector, a drag coefficient, and pass by pass range biases were estimated. Empirical parameters were adjusted at regular intervals to absorb orbit error and other mismodeling. The orbits will be refined on a schedule yet to be determined. Questions about the GDN files may be directed to: F.G. Lemoine flemoine@olympus.gsfc.nasa.gov or D.E. Smith dsmith@tharsis.gsfc.nasa.gov