BDSBCNAV2EPHEMERIS
Decoded BDS B-CNAV2 ephemeris
Platform: |
OEM719, OEM729, OEM7500, OEM7600, OEM7700, OEM7720, PwrPak7, CPT7, CPT7700, SMART7, SMART2 |
This log provides the Decoded BDS B-CNAV2 ephemeris for the BeiDou B2a signals.
Message ID: 2372
Log Type: Asynch
Recommended Input:
log bdsbcnav2ephemerisa onall
Example log:
#BDSBCNAV2EPHEMERISA,USB1,6,63.5,SATTIME,2209,496514.000,02000020,21df,16809;
34,853,00000000,25,493200,3,25.591797,0.006489,3.8598036335e-09,
-5.7266440902e-14,-1.169634521,6.7982793553e-04,0.749691829,2.199470739e+00,
9.6205966277e-01,-6.88135806e-09,-3.976951370e-10,3.259629011e-08,
-3.166496754e-08,-104.0195313,198.4492188,8.173286915e-06,-5.176290870e-06,
25,493200,-4.04388702e-04,8.52029558e-12,0.00000000,-3.085006028e-09,
-1.635635272e-08,-2.735760063e-09,0*ecfc685f
#BDSBCNAV2EPHEMERISA,USB1,5,63.5,SATTIME,2209,496514.000,02000020,21df,16809;
39,853,00000000,25,493200,2,5263.894531,-0.062899,7.7092496926e-10,
1.9584381616e-13,-2.140521199,2.2453696001e-03,-2.871042649,-9.3801678773e-01,
9.6155928554e-01,-1.86489911e-09,-1.102724504e-09,-4.284083843e-08,
4.004687071e-08,-83.8671875,-507.8242188,2.449937165e-05,-3.319233656e-06,
25,493200,3.49998591e-05,3.10862447e-14,0.00000000,7.799826562e-09,
-1.426087692e-08,-2.502929419e-09,0*4bceb44d
...
#BDSBCNAV2EPHEMERISA,USB1,1,63.5,SATTIME,2209,496514.000,02000020,21df,16809;
24,853,00000000,25,493200,3,19.027344,0.006292,3.9494502247e-09,
-6.8209628314e-14,1.247259053,4.9585988745e-04,0.517626996,1.3024422419e-01,
9.4798221860e-01,-6.90885921e-09,3.485859486e-10,2.421438694e-08,
-5.587935448e-09,115.0976563,154.5429688,9.900890291e-06,5.632638931e-06,
25,493200,-9.63939528e-04,-4.78550533e-12,0.00000000,1.175794750e-08,
-1.484295353e-08,-2.502929419e-09,0*f6bbff08
#BDSBCNAV2EPHEMERISA,USB1,0,63.5,SATTIME,2209,496514.000,02000020,21df,16809;
26,853,00000000,25,493200,3,107.203125,-0.005850,3.7798003010e-09,
4.1571032661e-14,2.051998724,7.3472585063e-04,0.436791966,1.0602762178e-01,
9.4940386191e-01,-6.82564146e-09,3.775157250e-10,-3.166496754e-08,
-3.073364496e-08,103.6250000,136.3750000,1.077353954e-05,5.120411515e-06,25,
493200,7.38367089e-04,-5.27311528e-12,0.00000000,0.000000000,-1.699663699e-08,
-2.561137080e-09,0*bf8175af
Field |
Field Type |
Description |
Format |
Binary Bytes |
Binary Offset |
---|---|---|---|---|---|
1 |
Log header |
BDSBCNAV2EPHEMERIS header For information about log headers, see ASCII, Abbreviated ASCII or Binary. |
– |
H |
0 |
2 |
Satellite ID |
ID/ranging code |
Ulong |
4 |
H |
3 |
WN |
Week number in BeiDou time (BDT). This will be offset from GPS time by 1356 weeks. |
Ulong |
4 |
H+4 |
4 |
Satellite Status |
Satellite Status Information: Bits 0 to 1: Health Status (HS) Bit 2: Data Integrity Flag (DIF) Bit 3: Signal Integrity Flag (SIF) Bit 4: Accuracy Integrity Flag (AIF) Bits 5 to 8: Signal In Space Monitoring Accuracy Index (SISMAI) |
Hex Ulong |
4 |
H+8 |
5 |
IODE |
Issue of data, ephemeris |
Ulong |
4 |
H+12 |
6 |
toe |
Reference time of ephemeris parameters in BeiDou time (BDT). This will be offset from GPS time. (s) |
Ulong |
4 |
H+16 |
7 |
Satellite Type |
2 bit orbit type: 01 indicates GEO, 10 indicates IGSO, 11 indicates MEO |
Ulong |
4 |
H+20 |
8 |
DeltaA |
Semi-major axis difference at reference time (m) |
Double |
8 |
H+24 |
9 |
ADot |
Change rate in Semi-major axis (m/s) |
Double |
8 |
H+32 |
10 |
DeltaN |
Mean motion difference from computed value (radians/s) |
Double |
8 |
H+40 |
11 |
NDot |
Rate of mean motion difference from computed value (radians/s2) |
Double |
8 |
H+48 |
12 |
M0 |
Mean anomaly at reference time (radians) |
Double |
8 |
H+56 |
13 |
e |
Eccentricity (unitless) |
Double |
8 |
H+64 |
14 |
Omega |
Argument of perigee (radians) |
Double |
8 |
H+72 |
15 |
Omega0 |
Longitude of ascending node of orbital of plane at weekly epoch (radians) |
Double |
8 |
H+80 |
16 |
i0 |
Inclination angle at reference time (radians) |
Double |
8 |
H+88 |
17 |
OmegaDot |
Rate of right ascension (radians/s) |
Double |
8 |
H+96 |
18 |
i0Dot |
Rate of inclination angle (radians/s) |
Double |
8 |
H+104 |
19 |
Cis |
Amplitude of sine harmonic correction term to the angle of inclination (radians) |
Double |
8 |
H+112 |
20 |
Cic |
Amplitude of cosine harmonic correction term to the angle of inclination (radians) |
Double |
8 |
H+120 |
21 |
Crs |
Amplitude of sine harmonic correction term to the orbit radius (m) |
Double |
8 |
H+128 |
22 |
Crc |
Amplitude of cosine harmonic correction term to the orbit radius (m) |
Double |
8 |
H+136 |
23 |
Cus |
Amplitude of sine harmonic correction term to the argument of latitude (radians) |
Double |
8 |
H+144 |
24 |
Cuc |
Amplitude of cosine harmonic correction term to the argument of latitude (radians) |
Double |
8 |
H+152 |
25 |
IODC |
Issue of data, clock |
Ulong |
4 |
H+160 |
26 |
toc |
Reference time of clock parameters in BeiDou time (BDT). (s) This will be offset from GPS time by 14 seconds. |
Ulong |
4 |
H+164 |
27 |
a0 |
Constant term of clock correction polynomial (s) |
Double |
8 |
H+168 |
28 |
a1 |
Linear term of clock correction polynomial (s/s) |
Double |
8 |
H+176 |
29 |
a2 |
Quadratic term of clock correction polynomial (s/s2) |
Double |
8 |
H+184 |
30 |
TGDB1Cp |
Group delay differential between the B1C pilot component and the B3I signal (s) |
Double |
8 |
H+192 |
31 |
TGDB2Ap |
Group delay differential between the B2a pilot component and the B3I signal (s) |
Double |
8 |
H+200 |
32 |
ISCB2ad |
Group delay differential between the B2a data and pilot components (s) |
Double |
8 |
H+208 |
33 |
Reserved |
Ulong |
4 |
H+216 |
|
34 |
xxxx |
32-bit CRC (ASCII and Binary only) |
Hex |
4 |
H+220 |
35 |
[CR][LF] |
Sentence Terminator (ASCII only) |
– |
– |
– |