GALINAVEPHEMERIS
Decoded Galileo INAV Ephemeris
Platform: |
OEM719, OEM729, OEM7500, OEM7600, OEM7700, OEM7720, PwrPak7, CPT7, CPT7700, SMART7, SMART2 |
The GALINAVEPHEMERIS log contains the Galileo I/NAV ephemeris information. Multiple messages are transmitted, one for each SVID with date. The I/NAV messages are only transmitted on E1 and E5b.
Message ID: 1309
Log Type: Asynch
Recommended Input:
log galinavephemerisa onall
ASCII Example:
#GALINAVEPHEMERISA,USB1,21,54.0,SATTIME,2209,504514.000,02000020,dbe9,16809;
2,0,0,0,0,0,0,0,0,68,107,3,501600,501600,1.94195529e+00,3.0676e-09,
3.055053530e-04,5.44060316e+03,9.740321573e-01,5.6931e-10,6.473214246e-01,
3.503504077e-01,-5.8141708e-09,7.6238e-06,4.7404e-06,2.409e+02,1.610e+02,
-5.0291e-08,2.9802e-08,2.989528002e-04,2.359002e-12,0.0,-6.985e-10,-1.630e-09
*96bd12ad
#GALINAVEPHEMERISA,USB1,20,54.0,SATTIME,2209,492664.000,02000020,dbe9,16809;
3,0,0,0,0,0,0,0,0,52,107,3,492000,492000,-2.64850798e+00,3.4862e-09,
3.018563148e-04,5.44061768e+03,9.558740377e-01,-4.0323e-10,-1.45198786e+00,
-4.689335290e-01,-5.9263183e-09,-3.3025e-06,5.0087e-06,2.308e+02,-7.150e+01,
1.8626e-09,3.5390e-08,-5.578683922e-04,-3.907985e-12,0.0,3.260e-09,3.725e-09
*b4c17a47
...
#GALINAVEPHEMERISA,USB1,1,54.0,SATTIME,2209,504514.000,02000020,dbe9,16809;
34,0,0,0,0,0,0,0,0,69,107,3,502200,502200,-1.35918661e+00,2.4115e-09,
2.855090424e-04,5.44061144e+03,9.978304990e-01,-5.8931e-11,2.72810277e+00,
1.63000994e+00,-5.1241420e-09,-4.7926e-06,1.3456e-05,6.991e+01,-1.037e+02,
-3.9116e-08,-3.5390e-08,-5.168783828e-04,-1.961098e-12,0.0,4.657e-09,5.588e-09
*3526c71f
#GALINAVEPHEMERISA,USB1,0,54.0,SATTIME,2209,504514.000,02000020,dbe9,16809;
36,0,0,0,0,0,0,0,0,70,107,3,502800,502800,9.062661404e-01,2.4169e-09,
2.578824060e-04,5.44061532e+03,9.979634387e-01,-6.7860e-12,2.72986363e+00,
2.260476454e-01,-5.1745013e-09,-4.6510e-06,1.4180e-05,5.316e+01,-1.043e+02,
8.0094e-08,3.1665e-08,-3.731743782e-04,-5.456968e-12,0.0,6.286e-09,7.218e-09
*3ad372dc
Field |
Field Type |
Description |
Format |
Binary Bytes |
Binary Offset |
---|---|---|---|---|---|
1 |
Log header |
GALINAVEPHEMERIS header For information about log headers, see ASCII, Abbreviated ASCII or Binary. |
|
H |
0 |
2 |
SatId |
Satellite identifier |
Ulong |
4 |
H |
3 |
E5bHealth |
E5b health status bits |
Uchar |
1 |
H+4 |
4 |
E5bDVS |
E5b data validity status |
Uchar |
1 |
H+5 |
5 |
Reserved |
Uchar |
1 |
H+6 |
|
6 |
Reserved |
Uchar |
1 |
H+7 |
|
7 |
E1bHealth |
E1b health status bits |
Uchar |
1 |
H+8 |
8 |
E1bDVS |
E1b data validity status |
Uchar |
1 |
H+9 |
9 |
Reserved |
Uchar |
1 |
H+10 |
|
10 |
Reserved |
Uchar |
1 |
H+11 |
|
11 |
IODnav |
Issue of data ephemeris |
Ushort |
2 |
H+12 |
12 |
SISA Index |
Signal in space accuracy (unitless) |
Uchar |
1 |
H+14 |
13 |
INAV Source |
Identifies the source signal: 0 = Unknown 1 = E1b 2 = E5b 3 = E1b and E5b |
Uchar |
1 |
H+15 |
14 |
T0e |
Ephemeris reference time (s) |
Ulong |
4 |
H+16 |
15 |
T0c |
Clock correction data reference time of week from the I/NAV message (s) |
Ulong |
4 |
H+20 |
16 |
M0 |
Mean anomaly at ref time (radians) |
Double |
8 |
H+24 |
17 |
DeltaN |
Mean motion difference (radians/s) |
Double |
8 |
H+32 |
18 |
Ecc |
Eccentricity (unitless) |
Double |
8 |
H+40 |
19 |
RootA |
Square root of semi-major axis |
Double |
8 |
H+48 |
20 |
I0 |
Inclination angle at ref time (radians) |
Double |
8 |
H+56 |
21 |
IDot |
Rate of inclination angle (radians/s) |
Double |
8 |
H+64 |
22 |
Omega0 |
Longitude of ascending node of orbital plane at weekly epoch (radians) |
Double |
8 |
H+72 |
23 |
Omega |
Argument of perigee (radians) |
Double |
8 |
H+80 |
24 |
OmegaDot |
Rate of right ascension (radians/s) |
Double |
8 |
H+88 |
25 |
Cuc |
Amplitude of the cosine harmonic correction term to the argument of latitude (radians) |
Double |
8 |
H+96 |
26 |
Cus |
Amplitude of the sine harmonic correction term to the argument of latitude (radians) |
Double |
8 |
H+104 |
27 |
Crc |
Amplitude of the cosine harmonic correction term to the orbit radius (m) |
Double |
8 |
H+112 |
28 |
Crs |
Amplitude of the sine harmonic correction term to the orbit radius (m) |
Double |
8 |
H+120 |
29 |
Cic |
Amplitude of the cosine harmonic correction term to the angle of inclination (radians) |
Double |
8 |
H+128 |
30 |
Cis |
Amplitude of the sine harmonic correction term to the angle of inclination (radians) |
Double |
8 |
H+136 |
31 |
Af0 |
SV clock bias correction coefficient from the I/NAV message (s) |
Double |
8 |
H+144 |
32 |
Af1 |
SV clock drift correction coefficient from the I/NAV message (s/s) |
Double |
8 |
H+152 |
33 |
Af2 |
SV clock drift rate correction coefficient from the I/NAV message (s/s^2) |
Double |
8 |
H+160 |
34 |
E1E5aBGD |
E1, E5a broadcast group delay |
Double |
8 |
H+168 |
35 |
E1E5bBGD |
E1, E5b broadcast group delay |
Double |
8 |
H+176 |
36 |
xxxx |
32-bit CRC (ASCII and Binary only) |
Hex |
4 |
H+184 |
37 |
[CR][LF] |
Sentence terminator (ASCII only) |
- |
- |
- |