;;; start of header ;;;
40 lines of header
1 lines of data
17 columns of data separated by commas
Sources of data are JPL server MMONT1, file M01-AB/NAV/Reconstruction_Data/Nav_reconstr_thru_P0338.xls
and pXXXacc.dat from Jim Murphy/PDS
                                          orbit number (-):       6.0
                               periapsis UTC date/time (-):      27-OCT-2001 23:18:28.2634
   periapsis altitude above unknown reference surface (km):  1.58418E+02
            periapsis altitude above 3397.2 km sphere (km):  1.42008E+02
                                     periapsis radius (km):  3.53921E+03
                                 periapsis latitude (degN):  6.79800E+01
                                periapsis longitude (degE):  1.70980E+02
                                       periapsis LST (hrs):  1.82300E+01
                                        periapsis Ls (deg):  2.60860E+02
                                   periapsis vrel (km s-1):  4.67000E+00
                            periapsis semi-major axis (km):  1.66415E+04
                                periapsis eccentricity (-):  7.87327E-01
                               periapsis inclination (deg):  9.35200E+01
                                      spacecraft mass (kg):  4.57800E+02
                                              period (hrs):  1.81000E+01
                     noise in raw acc measurements (m s-2):  6.62801E-04
 1: time after periapsis (s)
 2: radial distance (km)
 3: altitude = radius - periapsis radius + periapsis altitude (km)
 4: raw acceleration, nominally 1-s average (m s-2)
 5: 1-sigma uncertainty in raw acceleration (m s-2)
 6: density derived from raw acceleration (kg m-3)
 7: 1-sigma uncertainty in density derived from raw acceleration (kg m-3)
 8: 7-point running mean of raw acceleration, nominally 7-s average (m s-2)
 9: 1-sigma uncertainty in 7-point mean acceleration (m s-2)
10: density derived from 7-point mean acceleration (kg m-3)
11: 1-sigma uncertainty in density derived from 7-point mean acceleration (kg m-3)
12: 39-point running mean of raw acceleration, nominally 39-s average (m s-2)
13: 1-sigma uncertainty in 39-point mean acceleration (m s-2)
14: density derived from 39-point mean acceleration (kg m-3)
15: 1-sigma uncertainty in density derived from 39-point mean acceleration (kg m-3)
16: latitude (degN)
17: longitude (degE)
;;; end of header ;;;
 1.58960E+00, 3.53921E+03, 1.58416E+02, 9.57888E-04, 6.62801E-04, 1.84320E-09, 1.27538E-09, 0.00000E+00, 0.00000E+00, 0.00000E+00, 0.00000E+00, 0.00000E+00, 0.00000E+00, 0.00000E+00, 0.00000E+00, 6.78619E+01, 1.70928E+02