GPS Navigation File Explanation
2 N RINEX VERSION / TYPE 3SRINEXN 3SRINEX 18-Apr-97 18:00 PGM / RUN BY / DATE R100 COMMENT 9.3132e-09 -1.4901e-08 -5.9605e-08 1.1921e-07 ION ALPHA 9.6256e+04 -1.4746e+05 -1.3107e+05 9.1750e+05 ION BETA -9.313225746200e-10 8.881784197000e-15 589824 882 DELTA-UTC 11 LEAP SECONDS END OF HEADER
_2 | 96 12 6 2 0 0.0 | -3.146445378700e-04 | -3.637978807100e-12 | 0.000000000000e+00 |
_9.200000000000e+01 | 6.143750000000e+01 | 5.021637742904e-09 | -2.822725844843e+00 | |
_3.054738044700e-06 | 1.605378929500e-02 | 3.721565008200e-06 | 5.153678703300e+03 | |
_4.392000000000e+05 | 7.823109626800e-08 | -2.631856873482e+00 | -2.924352884300e-07 | |
_9.571452696386e-01 | -4.906250000000e+00 | 9.571452696386e-01 | 1.250052069700e-11 | |
_2.585107680114e-09 | 0.000000000000e+00 | 8.820000000000e+02 | 0.000000000000e+00 | |
_3.200000000000e+01 | 0.000000000000e+00 | -2.328306436500e-09 | 9.200000000000e+01 | |
_4.320060000000e+05 | 0.000000000000e+00 | 0.000000000000e+00 | 0.000000000000e+00 | |
10 | 96 12 6 2 0 0.0 | 3.091990947700e-07 | 5.684341886100e-13 | 0.000000000000e+00 |
7.000000000000e+00 | -3.750000000000e-01 | 4.820915096284e-09 | -2.645536801844e+00 | |
3.352761268600e-08 | 1.698388485200e-03 | 5.751848220800e-06 | 5.153680217700e+03 | |
4.392000000000e+05 | -5.587935447700e-09 | 5.463796836005e-01 | 5.587935447700e-09 | |
9.615771814051e-01 | 2.710000000000e+02 | -3.633249945094e-01 | -8.219628094709e-09 | |
2.260808457468e-10 | 0.000000000000e+00 | 8.820000000000e+02 | 0.000000000000e+00 | |
3.200000000000e+01 | 0.000000000000e+00 | -1.862645149200e-09 | 7.000000000000e+00 | |
4.323060000000e+05 | 0.000000000000e+00 | 0.000000000000e+00 | 0.000000000000e+00 |
Any entry marked by an asterix (*) is an optional entry and may not be included.RINEX VERSION/TYPE Format version (2) I6,14x, File type ('N' for Navigation Data) Al,19X
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PGM / RUN BY / DATE - Name of program creating current file A20, - Name of agency creating current file A20, - Date of file creation A20Top of Page
*COMMENT Comment lines (2) I6,14XTop of Page
*ION ALPHA Ionosphere parameters A0-A3 of almanac 2X,4D12.4 (page 18 of subframe 4)Top of Page
*ION BETA Ionosphere parameters B0-B3 of almanac 2X,4D12.4Top of Page
*DELTA UTC: A0,A1,T,W Almanac parameters to compute time in 3X,2D l9.12, UTC (page 18 of subframe 4) 219 AO,Al: term of polynomial T : reference time for UTC data W : UTC reference week numberTop of Page
*LEAP SECONDS Delta time due to leap seconds I6Top of Page
END OF HEADER Last record in the header section. 60XTop of Page
2 | 96 12 6 2 0 0.0 | -3.146445378700e-04 | -3.637978807100e-12 | 0.000000000000e+00 |
2 | 96 12 6 2 0 0.0 | -3.146445378700e-04 | -3.637978807100e-12 | 0.000000000000e+00 |
Epoch: | Toc - Time of Clock |
year (2 digits) | |
month | |
day | |
hour | |
minute | |
second |
2 | 96 12 6 2 0 0.0 | -3.146445378700e-04 | -3.637978807100e-12 | 0.000000000000e+00 |
SV clock bias (seconds) | ||
SV clock drift (sec/sec) | ||
SV clock drift rate (sec/sec sq) | ||
9.200000000000e+01 | 6.143750000000e+01 | 5.021637742904e-09 | -2.822725844843e+00 |
9.200000000000e+01 | 6.143750000000e+01 | 5.021637742904e-09 | -2.822725844843e+00 |
Amplitude of the sine harmonic correction term to the orbit radius
9.200000000000e+01 | 6.143750000000e+01 | 5.021637742904e-09 | -2.822725844843e+00 |
Mean motion difference from computed value
9.200000000000e+01 | 6.143750000000e+01 | 5.021637742904e-09 | -2.822725844843e+00 |
Mean anomaly at reference time
3.054738044700e-06 | 1.605378929500e-02 | 3.721565008200e-06 | 5.153678703300e+03 |
Amplitude of the cosine harmonic correction term to the argument of latitude
3.054738044700e-06 | 1.605378929500e-02 | 3.721565008200e-06 | 5.153678703300e+03 |
Eccentricity
3.054738044700e-06 | 1.605378929500e-02 | 3.721565008200e-06 | 5.153678703300e+03 |
Amplitude of the sine harmonic correction term to the argument of latitude
3.054738044700e-06 | 1.605378929500e-02 | 3.721565008200e-06 | 5.153678703300e+03 |
Square root of the semi-major axis
4.392000000000e+05 | 7.823109626800e-08 | -2.631856873482e+00 | -2.924352884300e-07 |
4.392000000000e+05 | 7.823109626800e-08 | -2.631856873482e+00 | -2.924352884300e-07 |
Amplitude of the cosine harmonic correction term to the angle of inclination
4.392000000000e+05 | 7.823109626800e-08 | -2.631856873482e+00 | -2.924352884300e-07 |
Longitude of ascending node of orbit plane at weekly epoch
4.392000000000e+05 | 7.823109626800e-08 | -2.631856873482e+00 | -2.924352884300e-07 |
Amplitude of the sine harmonic correction term to the angle of inclination
9.571452696386e-01 | -4.906250000000e+00 | 9.571452696386e-01 | 1.250052069700e-11 |
Inclination angle at reference time
9.571452696386e-01 | -4.906250000000e+00 | 9.571452696386e-01 | 1.250052069700e-11 |
Amplitude of the cosine harmonic correction term to the orbit radius
9.571452696386e-01 | -4.906250000000e+00 | 9.571452696386e-01 | 1.250052069700e-11 |
Argument of perigee
9.571452696386e-01 | -4.906250000000e+00 | 9.571452696386e-01 | 1.250052069700e-11 |
Rate of right ascension
2.585107680114e-09 | 0.000000000000e+00 | 8.820000000000e+02 | 0.000000000000e+00 |
Rate of inclination angle
2.585107680114e-09 | 0.000000000000e+00 | 8.820000000000e+02 | 0.000000000000e+00 |
2.585107680114e-09 | 0.000000000000e+00 | 8.820000000000e+02 | 0.000000000000e+00 |
2.585107680114e-09 | 0.000000000000e+00 | 8.820000000000e+02 | 0.000000000000e+00 |
3.200000000000e+01 | 0.000000000000e+00 | -2.328306436500e-09 | 9.200000000000e+01 |
3.200000000000e+01 | 0.000000000000e+00 | -2.328306436500e-09 | 9.200000000000e+01 |
3.200000000000e+01 | 0.000000000000e+00 | -2.328306436500e-09 | 9.200000000000e+01 |
3.200000000000e+01 | 0.000000000000e+00 | -2.328306436500e-09 | 9.200000000000e+01 |
4.320060000000e+05 | 0.000000000000e+00 | 0.000000000000e+00 | 0.000000000000e+00 |
4.320060000000e+05 | 0.000000000000e+00 | 0.000000000000e+00 | 0.000000000000e+00 |