[IGSREPORT-25234] Wk 1944 IGLOS Final Orbits
acc
acc at igs.org
Sun Apr 30 17:50:30 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1944 (Apr 09, 2017 - Apr 15, 2017)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1944.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed
to the values of the final IGS (GPS) combination.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl1944[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1944 in the SP3 format.
igl19447.sum Combination Report for GPS Week 1944.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 0.2 ns
1 | -1.3 ns
2 | 0.9 ns
3 | 3.0 ns
4 | -1.5 ns
5 | -0.1 ns
6 | -0.7 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1944, 1a.1944).
Table 2 contains the complete ephemeris and clock correction transformation
parameters (includes both the apriori and a posteriori values) for each
centre and each day (Tables 2.1944.0-6)
Table 3 contains two types of daily RMS for each satellite and centre, along
with the computed satellite position sigmas for the combined orbits
(tables 3.1944.0-6).
The first type of satellite RMS is based on orbit combination and the
second RMS type is a result of the 7-day arc evaluation of each centre
ephemerides.
Table 1: Week 1944 summary. (Apr 09, 2017 - Apr 15, 2017)
Table 1.1944.a GPS week : 1944 MJD: 57852.0-57858.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 17 -26 -8 4 .09 35 34 | 3480 -14 3412 11822
| 1 1 3 23 32 32 .05 | 1727 2839
cof n/a| 0 1 20 -31 15 -1 .11 38 36 | 3477 -10 3414 11820
| 3 1 3 18 37 36 .07 | 1723 2848
emx n/a| 0 0 0 -31 -30 7 .10 25 25 | -9754 1000 3396 10940
| 0 1 2 33 25 50 .05 | 10028 1791
esx n/a| 0 0 -1 7 2 -15 .12 16 15 | -1173 -693 3412 13728
| 0 1 1 17 19 29 .02 | 7137 2719
gfz n/a| -3 0 -10 -15 46 -19 .07 26 25 | 0 -129 3405 11721
| 1 1 1 30 17 34 .05 | 0 2958
grg n/a| 0 0 8 -24 24 -6 -.40 31 30 | 272 -151 3436 16176
| 1 1 7 19 23 40 .06 | 435 2603
iac n/a| 2 0 -5 59 -22 9 -.13 22 22 | 1017 -183 3402 10986
| 1 1 4 29 62 52 .04 | 1190 1455
mcc n/a| 0 1 15 185 -57 125 -.21 207 207 | --- --- --- ---
| 13 10 27 196 73 317 .46 | --- ---
Table 1.1944.b GPS week : 1944 MJD: 57852.0-57858.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 13 11 11 11 12 13 10 |
R02 | 12 11 8 7 7 8 6 |
R03 | 10 11 8 7 9 7 9 |
R04 | 10 10 8 7 8 8 7 |
R05 | 15 13 15 14 15 15 14 |
R06 | 16 7 7 7 7 8 11 |
R07 | 9 9 10 7 9 9 9 |
R08 | 9 10 9 9 9 10 9 |
R09 | 6 8 7 8 7 9 6 |
R10 | 9 7 9 11 10 11 10 |
R11 | 7 9 9 8 9 7 8 |
R12 | --- 0 --- --- --- --- 0 |
R13 | 8 6 9 8 7 7 8 |
R14 | 17 13 13 12 13 15 9 |
R15 | 10 10 9 10 10 11 11 |
R16 | 11 15 17 17 9 12 14 |
R17 | 9 9 12 11 11 10 12 |
R18 | 7 7 8 9 10 8 8 |
R19 | 17 16 14 14 17 19 15 |
R20 | 14 12 14 15 12 16 14 |
R21 | 12 9 10 9 9 12 12 |
R22 | 12 11 8 13 12 12 11 |
R23 | 9 9 9 10 10 10 11 |
R24 | 15 14 16 14 21 15 15 |
R26 | 17 36 25 20 34 25 21 |
Table 1.1944.c GPS week : 1944 MJD: 57852.0-57858.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 1944 0 | -21 -35 50 388 1259 -33 83.8 1386 1386 | 224 0
brd 1944 1 | -37 33 36 -1677 1378 -2608 83.4 1266 1266 | -1346 0
brd 1944 2 | -1 -15 62 -515 -137 -3436 84.6 1336 1336 | 873 0
brd 1944 3 | 49 -12 104 869 -1519 -4667 84.2 1256 1256 | 2998 0
brd 1944 4 | -80 -14 107 341 -1981 -4432 85.1 1330 1330 | -1452 0
brd 1944 5 | -49 26 188 -1789 -3378 -1385 85.4 1478 1478 | -50 0
brd 1944 6 | -21 37 87 -1377 -1841 2838 84.4 1321 1321 | -706 0
-------------+------------------------------------------------------------+----------------
brd 1944 mean| -23 2 91 -537 -888 -1960 84.4 1339 1339 | 77 0
brd 1944 sdev| 40 28 50 1093 1779 2680 .7 75 75 | 1537 0
Table 2: Daily transformation of each centre to the combined IGL orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1944.0 GPS week: 1944 Day: 0 MJD: 57852
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 16 -18 -41 14 .07 32 29 | 1444 172 3359 11865
cof n/a| 0 1 14 -46 -10 -21 .17 32 31 | 1454 163 3358 11864
emx n/a| 0 -1 0 -96 -38 -94 .13 26 26 | -12001 1002 3332 10962
esx n/a| -1 0 -1 26 2 -17 .13 16 14 | -10267 -1090 3354 13701
gfz n/a| -4 1 -12 39 28 -53 .07 28 28 | 0 268 3354 11656
grg n/a| 0 0 -1 4 46 -3 -.48 31 31 | 307 51 3403 11184
iac n/a| 3 -1 0 68 25 86 -.13 29 29 | 1180 769 3350 10938
mcc n/a| 14 -10 49 413 -27 308 -.51 237 237 | --- --- --- ---
Table 2.1944.1 GPS week: 1944 Day: 1 MJD: 57853
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 -1 11 -19 23 -20 .19 32 32 | 1242 -2115 3228 12444
cof n/a| 0 2 17 -16 70 28 .08 39 36 | 1245 -2143 3232 12446
emx n/a| 0 -1 1 4 8 -17 .12 24 24 | -21636 -391 3220 11659
esx n/a| -1 -2 0 -12 2 28 .14 16 16 | -7741 -1560 3240 14078
gfz n/a| 0 0 -10 7 68 38 .09 23 27 | 0 -2860 3232 12346
grg n/a| 0 0 7 -16 8 -12 -.49 30 26 | -105 -2383 3245 12317
iac n/a| 2 3 -7 23 -93 -36 -.15 22 22 | 472 -1967 3224 11503
mcc n/a| 11 4 34 -13 -112 -390 -.84 293 293 | --- --- --- ---
Table 2.1944.2 GPS week: 1944 Day: 2 MJD: 57854
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 0 18 -40 0 68 .02 34 34 | 2831 890 3299 11033
cof n/a| 0 0 19 -18 -21 42 .02 36 36 | 2810 914 3309 11031
emx n/a| 0 -1 4 -26 -62 32 .14 26 26 | -12846 1818 3276 10294
esx n/a| 0 0 -1 15 4 -3 .13 16 15 | -2024 -725 3298 12903
gfz n/a| -2 0 -11 -36 50 -7 .03 27 24 | 0 1243 3282 11045
grg n/a| 1 0 0 -51 28 54 -.36 34 26 | 859 1110 3311 44005
iac n/a| 2 0 -5 29 2 -48 -.08 17 17 | 671 676 3283 10227
mcc n/a| -17 20 8 314 -94 -242 -.28 179 179 | --- --- --- ---
Table 2.1944.3 GPS week: 1944 Day: 3 MJD: 57855
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 2 21 -61 -3 7 .06 36 36 | 5700 5596 3787 11405
cof n/a| 0 2 25 -40 -22 -37 .06 39 37 | 5686 5619 3787 11401
emx n/a| 0 3 0 -24 -58 34 .07 25 25 | -12348 4615 3779 10401
esx n/a| 0 -1 -2 -7 -38 -69 .11 15 14 | 1331 4290 3795 13250
gfz n/a| -2 0 -12 -25 19 -65 .07 27 26 | 0 5390 3789 11453
grg n/a| 0 -1 20 -45 -15 16 -.37 32 33 | 811 4588 3853 10919
iac n/a| 0 0 -9 109 84 72 -.10 20 20 | 3603 1583 3788 10710
mcc n/a| -15 0 -31 330 23 304 -.35 172 172 | --- --- --- ---
Table 2.1944.4 GPS week: 1944 Day: 4 MJD: 57856
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 19 -31 -61 -2 .10 37 33 | 5117 -2859 3456 11851
cof n/a| 3 2 21 -53 5 -28 .18 42 36 | 5120 -2854 3454 11850
emx n/a| 0 -1 -2 -4 -12 7 .00 24 24 | -17092 -508 3434 10975
esx n/a| -1 0 -1 -7 15 -21 .13 16 15 | -243 -3960 3435 13621
gfz n/a| -3 0 -7 -47 57 -32 .16 25 24 | 0 -3314 3424 11745
grg n/a| 0 1 11 -27 14 3 -.33 30 33 | -119 -2981 3493 11433
iac n/a| 2 0 -11 74 -48 14 -.13 23 23 | 719 -2300 3430 11197
mcc n/a| -1 2 4 232 -157 136 -.13 164 164 | --- --- --- ---
Table 2.1944.5 GPS week: 1944 Day: 5 MJD: 57857
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 17 15 28 -28 .13 36 36 | 3743 113 3321 11677
cof n/a| -6 -1 19 -3 45 39 .19 38 39 | 3748 97 3324 11676
emx n/a| 1 0 -2 -48 -28 37 .11 23 23 | 786 498 3316 10536
esx n/a| 0 -2 -1 31 8 -14 .08 18 15 | 11940 1078 3332 13442
gfz n/a| -2 2 -9 -34 58 -2 .08 25 26 | 0 41 3333 11521
grg n/a| 2 0 9 -22 53 -76 -.41 32 31 | -178 489 3290 11486
iac n/a| 1 -1 -6 56 -50 -17 -.19 23 23 | 60 314 3311 10819
mcc n/a| -2 1 2 144 42 325 .60 199 199 | --- --- --- ---
Table 2.1944.6 GPS week: 1944 Day: 6 MJD: 57858
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 0 17 -29 0 -8 .08 35 35 | 4289 -1896 3439 12484
cof n/a| 0 1 21 -42 43 -37 .06 38 37 | 4280 -1872 3440 12476
emx n/a| 0 1 -1 -26 -23 53 .10 25 25 | 6858 -28 3418 11759
esx n/a| 0 0 -2 6 21 -9 .13 15 14 | -1212 -2890 3432 15107
gfz n/a| -5 1 -10 -13 39 -16 .01 26 20 | 0 -1677 3425 12286
grg n/a| 1 -2 12 -15 33 -26 -.35 31 30 | 334 -1933 3458 11888
iac n/a| 3 -1 -2 54 -76 -1 -.16 22 22 | 415 -360 3429 11508
mcc n/a| 11 -7 37 -126 -79 438 .06 206 206 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGL orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1944.0 GPS week: 1944 Day: 0 MJD: 57852
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 689 32 24 26 10 32 34 36 --- 12 | 4 8 7 4 4 7 4 --- 2
R02E | 1113 29 28 21 11 27 23 41 --- 11 | 6 6 6 5 6 9 10 --- 4
R03E | 2563 30 31 22 9 27 23 29 70 10 | 3 4 3 5 6 9 4 28 3
R04E | 734 33 29 24 13 22 22 17 --- 9 | 4 4 3 5 6 7 5 --- 4
R05E | 2090 48 33 38 23 36 27 36 --- 15 | 3 14 9 3 6 8 4 --- 3
R06E | 969 22 29 25 19 19 33 72 --- 16 | 4 8 3 5 4 10 5 --- 3
R07E | 433 23 24 19 16 17 23 23 --- 9 | 3 8 4 5 5 9 4 --- 3
R08E | 1049 29 22 19 13 19 27 15 --- 9 | 3 6 5 4 5 7 4 --- 2
XR09 | 1588 12 19 14 8 16 --- 14 --- 6 | 1 3 3 2 3 --- 2 --- 1
R10 | 595 20 20 14 21 16 26 18 --- 8 | 3 4 2 2 2 38 3 --- 2
R11 | 860 14 15 17 11 24 17 14 220 7 | 2 4 2 4 4 7 1 9 2
R13 | 914 10 12 16 17 24 14 17 --- 7 | 1 4 3 4 5 3 2 --- 3
R14 | 2181 46 58 38 25 39 58 26 --- 16 | 2 14 6 8 9 6 4 --- 5
R15 | 1168 29 26 24 16 29 20 10 --- 9 | 1 2 2 3 4 7 2 --- 2
R16 | 516 23 24 33 11 30 37 19 --- 11 | 2 5 3 6 6 8 2 --- 3
R17 | 775 27 25 23 8 21 19 22 --- 8 | 2 4 2 4 3 3 2 --- 2
R18 | 624 20 18 19 9 19 13 20 --- 7 | 2 3 2 3 3 3 2 --- 1
R19 | 2146 56 58 38 20 45 43 29 --- 16 | 2 3 2 4 2 5 2 --- 2
R20 | 1616 48 50 23 21 34 46 24 --- 14 | 4 7 5 5 7 7 3 --- 3
R21 | 457 37 41 27 12 29 20 32 340 11 | 2 4 2 5 6 6 2 37 3
R22 | 1471 35 31 29 6 35 15 33 --- 11 | 2 4 3 5 8 4 3 --- 3
R23 | 776 20 11 23 20 26 23 11 --- 9 | 2 3 3 3 7 5 2 --- 2
R24 | 2705 25 42 40 19 23 64 27 --- 15 | 5 9 4 8 7 6 3 --- 4
XR26 | ---- 17 107 --- --- --- --- 15 --- 16 | 7 7 --- --- --- --- 5 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1386 32 32 26 16 28 31 29 237 |T 2 5 3 4 5 7 3 24 2
WRMS | 1386 29 31 26 14 28 31 29 237 |NE 2 5 2 4 5 7 2 23 2
MEDI | 969 27 26 23 13 26 23 22 220 |MD 2 4 3 4 5 7 3 28 3
Table 3.1944.1 GPS week: 1944 Day: 1 MJD: 57853
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 723 44 55 22 13 25 27 20 --- 11 | 3 5 6 4 5 5 4 --- 2
R02 | 797 29 26 19 14 23 30 35 355 11 | 4 5 6 5 5 9 4 9999 3
R03 | 2134 31 39 28 8 23 36 21 57 10 | 3 5 6 4 6 9 2 3 3
R04 | 653 28 30 25 14 19 26 23 --- 9 | 3 5 4 4 5 6 4 --- 3
R05 | 1530 32 38 25 21 23 41 30 --- 12 | 4 13 7 6 10 8 3 --- 3
R06 | 747 16 20 10 10 19 24 15 --- 7 | 3 7 4 4 4 7 2 --- 2
R07 | 1202 31 36 20 17 24 22 12 465 9 | 4 7 4 7 6 7 2 9999 3
R08E | 904 33 29 27 16 16 30 13 --- 10 | 3 6 6 6 6 8 3 --- 3
XR09 | 1855 14 14 13 10 25 --- 16 --- 8 | 2 4 3 3 5 --- 2 --- 2
R10 | 746 25 23 11 11 16 11 20 --- 7 | 2 5 3 2 3 40 2 --- 1
R11 | 935 24 32 18 15 18 30 14 169 8 | 2 4 2 4 4 6 2 2 2
XR12 | ---- 7 16 --- --- --- --- --- --- 0 | 1 1 --- --- --- --- --- --- 1
R13 | 463 14 17 14 13 21 9 10 --- 6 | 2 4 4 4 5 2 2 --- 2
R14 | 1969 36 43 37 16 28 39 14 --- 12 | 2 12 6 7 8 9 3 --- 5
R15 | 2557 23 28 20 19 20 30 16 --- 9 | 2 5 3 4 5 8 2 --- 2
R16 | 665 34 41 38 24 13 53 28 --- 14 | 2 8 3 9 6 7 2 --- 4
R17 | 578 37 41 19 8 30 13 13 --- 9 | 2 5 2 8 10 4 2 --- 3
R18 | 591 19 24 15 10 18 12 19 --- 7 | 2 4 2 4 4 3 2 --- 2
R19 | 1887 56 53 39 17 41 26 33 --- 15 | 2 3 3 5 5 7 2 --- 2
R20 | 1110 48 63 21 22 23 31 14 --- 11 | 5 9 6 5 6 7 3 --- 3
R21 | 559 35 40 21 12 18 15 24 234 9 | 3 5 3 5 6 7 2 2 3
R22 | 1580 39 46 30 11 27 20 26 --- 11 | 2 4 3 6 8 6 3 --- 3
R23 | 955 14 23 24 28 15 18 12 --- 9 | 2 4 4 3 6 5 2 --- 2
R24 | 1489 22 57 25 17 27 58 34 --- 14 | 5 12 5 8 7 6 4 --- 4
XR26 | ---- 49 106 --- --- --- --- 26 --- 36 | 6 19 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1265 32 39 24 16 23 30 22 293 |T 2 6 4 5 5 8 2 2 2
WRMS | 1265 32 36 24 16 27 26 22 293 |NE 2 6 3 5 5 8 2 2 2
MEDI | 935 31 36 21 14 23 26 19 234 |MD 2 5 4 5 6 7 2 2 3
Table 3.1944.2 GPS week: 1944 Day: 2 MJD: 57854
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 658 54 57 21 12 25 29 12 --- 10 | 4 6 4 5 5 6 3 --- 3
R02 | 837 22 25 23 15 15 21 12 192 8 | 3 5 5 7 4 6 3 9999 3
R03 | 2547 30 33 16 12 20 16 13 59 7 | 3 4 5 4 5 4 3 3 2
R04 | 1008 30 32 15 8 19 27 10 --- 7 | 4 5 4 5 5 5 4 --- 2
R05 | 885 28 32 26 24 43 51 32 --- 15 | 4 10 4 6 17 6 3 --- 3
R06 | 1939 21 19 15 11 16 20 8 --- 6 | 3 6 4 6 4 3 2 --- 3
R07 | 1606 37 44 20 15 30 24 13 290 9 | 3 6 4 9 8 3 2 9999 4
R08 | 1712 27 37 19 16 28 31 7 --- 9 | 4 6 5 6 7 3 3 --- 3
XR09 | 1287 10 16 18 14 18 --- 10 --- 7 | 3 4 3 5 5 --- 2 --- 2
R10 | 565 31 43 23 13 18 14 16 --- 8 | 3 5 3 3 5 41 2 --- 2
R11 | 491 34 36 13 15 20 19 18 129 8 | 3 5 3 7 7 2 1 2 3
R13 | 624 19 20 18 9 29 33 13 --- 8 | 3 4 4 4 5 3 2 --- 2
R14 | 1970 41 38 26 23 34 40 16 --- 12 | 3 9 5 6 5 7 2 --- 3
R15 | 2724 23 26 14 15 29 33 14 --- 9 | 3 5 3 4 5 5 2 --- 2
R16 | 887 37 45 58 18 22 62 20 --- 16 | 3 7 4 7 5 7 2 --- 3
R17 | 921 47 43 21 14 32 21 26 --- 11 | 3 6 4 8 9 4 3 --- 3
R18 | 623 31 31 17 8 25 12 12 --- 7 | 3 4 3 5 4 6 2 --- 2
R19 | 948 59 60 38 15 36 26 24 --- 14 | 3 4 4 4 6 6 3 --- 2
R20 | 1014 30 25 27 17 29 70 17 --- 14 | 4 9 5 5 6 5 2 --- 2
R21 | 606 38 36 31 14 25 19 12 140 10 | 3 4 4 4 3 6 3 2 2
R22 | 1773 30 28 19 9 18 23 16 --- 8 | 3 5 4 5 7 4 2 --- 2
R23 | 656 22 22 20 18 24 21 13 --- 8 | 3 5 4 6 6 3 2 --- 3
R24 | 624 33 31 44 25 29 58 24 --- 15 | 4 10 6 6 7 6 3 --- 4
XR26 | ---- 43 73 --- --- --- --- 14 --- 25 | 4 18 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1335 34 36 26 16 27 34 17 179 |T 3 6 4 5 6 6 2 2 2
WRMS | 1335 34 36 26 15 24 26 17 179 |NE 3 6 3 5 5 7 2 2 2
MEDI | 921 30 32 20 15 25 24 13 140 |MD 3 5 4 5 5 5 2 2 3
Table 3.1944.3 GPS week: 1944 Day: 3 MJD: 57855
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 894 60 54 25 14 30 20 13 --- 11 | 6 7 5 11 9 5 3 --- 5
R02 | 1027 20 18 20 12 20 11 11 248 6 | 5 8 6 7 5 5 2 1 2
R03 | 1394 30 31 17 10 18 18 13 107 7 | 5 6 5 6 6 5 3 7 2
R04 | 1047 28 34 14 11 21 17 8 --- 7 | 5 6 5 6 8 5 2 --- 3
R05 | 802 25 31 35 21 27 29 42 --- 14 | 6 11 7 7 15 6 3 --- 4
R06 | 1229 23 32 14 12 18 21 10 --- 7 | 5 8 5 7 6 5 3 --- 2
R07 | 2051 34 33 17 10 23 12 9 191 7 | 5 7 5 8 8 4 2 9999 3
R08 | 2982 28 28 22 11 24 22 15 --- 8 | 5 6 5 7 8 3 4 --- 3
XR09 | 1253 16 19 21 10 14 --- 19 --- 8 | 5 5 5 5 5 --- 3 --- 2
XR10 | 681 31 22 30 14 20 --- 13 --- 10 | 5 6 6 8 6 --- 4 --- 4
R11 | 700 29 34 12 10 36 20 10 105 8 | 4 5 4 7 8 4 2 6 3
R13 | 1127 24 20 8 14 24 22 18 --- 8 | 5 6 5 5 5 6 2 --- 2
R14 | 691 52 52 25 17 43 21 18 --- 12 | 5 9 5 7 8 5 3 --- 4
R15 | 1154 27 33 21 19 16 27 22 --- 9 | 5 5 5 6 5 4 3 --- 2
R16 | 1402 31 47 43 22 31 71 25 --- 17 | 4 6 6 6 5 6 3 --- 3
R17 | 736 44 42 18 11 27 19 29 --- 10 | 5 8 6 10 12 5 3 --- 5
R18 | 582 26 28 12 7 27 34 21 --- 9 | 5 6 5 6 6 5 3 --- 2
R19 | 783 68 68 28 13 36 27 24 --- 13 | 5 5 6 9 7 4 2 --- 2
R20 | 1506 16 19 34 24 18 67 20 --- 14 | 6 9 6 10 9 4 3 --- 4
R21 | 654 34 30 27 6 33 12 17 163 9 | 5 7 5 5 5 5 2 5 2
R22 | 1145 46 46 33 16 35 34 19 --- 12 | 4 5 6 5 6 4 2 --- 2
R23 | 1042 27 27 29 21 15 25 13 --- 9 | 5 6 5 7 8 6 4 --- 3
R24 | 911 36 67 29 18 28 54 23 --- 13 | 6 10 5 7 6 5 3 --- 3
XR26 | ---- 29 61 --- --- --- --- 15 --- 20 | 7 26 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1255 36 39 25 15 27 32 20 172 |T 5 7 5 7 7 4 2 4 2
WRMS | 1255 36 37 25 14 26 33 20 172 |NE 5 7 5 6 6 4 2 5 2
MEDI | 1042 29 32 22 13 24 22 17 163 |MD 5 6 5 7 6 5 3 5 3
Table 3.1944.4 GPS week: 1944 Day: 4 MJD: 57856
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 553 60 76 19 14 29 25 17 --- 11 | 9 12 9 13 12 5 3 --- 4
R02 | 1980 16 21 17 12 18 13 12 63 6 | 10 11 9 10 10 3 3 1 2
R03 | 1192 32 29 19 16 21 21 17 137 9 | 9 11 9 10 10 5 3 12 2
R04 | 1127 26 23 14 10 23 19 14 --- 7 | 9 9 10 10 11 3 2 --- 3
R05 | 1035 25 32 32 27 34 37 44 --- 15 | 10 12 10 15 16 4 4 --- 5
R06 | 1799 24 22 11 12 19 19 16 --- 7 | 9 10 10 11 11 5 3 --- 2
R07 | 1715 44 41 17 10 24 9 12 117 8 | 9 10 9 10 11 4 2 9999 2
R08 | 2718 29 30 19 13 18 22 19 --- 8 | 9 10 9 11 11 6 3 --- 3
XR09 | 1306 16 20 12 8 10 --- 18 --- 6 | 9 10 10 10 10 --- 2 --- 3
R10 | 822 24 30 15 19 13 34 24 --- 9 | 9 11 10 12 10 9999 5 --- 4
R11 | 650 29 28 14 11 31 19 14 151 8 | 9 10 9 9 9 5 2 9 1
R13 | 1096 15 25 11 14 19 24 12 --- 7 | 9 9 9 9 10 5 2 --- 2
R14 | 758 60 68 23 24 18 26 25 --- 12 | 9 11 9 11 10 9 3 --- 4
R15 | 1063 35 34 26 14 24 15 17 --- 9 | 9 9 9 10 10 3 2 --- 2
R16 | 1268 24 31 15 16 13 30 18 --- 8 | 9 10 10 9 9 4 2 --- 2
R17 | 898 41 51 25 10 35 18 23 --- 11 | 9 10 10 12 14 4 2 --- 4
R18 | 584 34 23 18 12 32 20 18 --- 9 | 9 10 10 12 13 4 3 --- 4
R19 | 793 74 76 38 13 44 28 34 --- 16 | 9 9 10 12 11 5 2 --- 2
R20 | 1179 15 25 40 18 17 39 18 --- 12 | 10 13 11 15 12 6 3 --- 5
R21 | 577 30 38 17 13 19 19 25 274 8 | 9 10 10 10 10 3 2 9 2
R22 | 899 46 54 34 11 31 21 25 --- 12 | 9 10 9 9 10 5 2 --- 2
R23 | 959 21 27 15 24 14 35 17 --- 10 | 9 9 9 9 11 5 3 --- 2
R24 | 2553 46 50 49 25 21 81 43 --- 20 | 10 11 10 10 11 3 2 --- 4
XR26 | ---- 48 139 --- --- --- --- 23 --- 33 | 11 27 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1330 37 42 24 16 25 30 23 164 |T 9 11 9 10 10 4 2 7 2
WRMS | 1330 33 36 24 15 24 33 23 164 |NE 9 11 9 10 10 4 2 9 2
MEDI | 1063 29 30 18 13 21 21 18 137 |MD 9 10 10 10 11 5 2 9 2
Table 3.1944.5 GPS week: 1944 Day: 5 MJD: 57857
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 767 64 36 25 14 33 17 19 --- 12 | 14 14 14 14 13 3 2 --- 2
R02 | 2428 17 19 14 13 25 17 17 115 7 | 13 14 13 13 13 2 2 1 2
R03 | 1217 36 46 12 8 20 12 9 159 7 | 14 14 13 14 14 3 2 3 2
R04 | 2039 23 23 15 12 18 23 13 --- 7 | 14 14 14 14 14 3 2 --- 2
R05 | 948 21 15 26 32 23 48 36 --- 14 | 13 16 13 17 18 4 4 --- 4
R06 | 1272 26 27 14 19 18 12 14 --- 7 | 13 14 14 17 15 5 2 --- 5
R07 | 967 40 43 11 10 27 24 13 102 9 | 14 14 14 14 15 3 2 9999 2
R08 | 1696 38 38 24 14 17 25 14 --- 9 | 14 14 13 15 16 4 3 --- 3
XR09 | 1777 18 16 20 11 21 --- 16 --- 8 | 13 14 13 14 14 --- 2 --- 3
R10 | 1301 33 41 23 16 22 30 21 --- 10 | 14 14 14 14 14 9999 3 --- 4
R11 | 906 22 32 13 12 19 14 19 164 7 | 14 14 14 13 14 4 2 3 2
R13 | 1332 19 19 13 14 23 17 11 --- 7 | 13 14 13 13 13 5 3 --- 3
R14 | 1549 41 36 30 21 30 50 25 --- 14 | 13 15 13 15 14 7 1 --- 3
R15 | 2001 39 43 23 23 31 15 18 --- 11 | 14 14 13 14 15 5 2 --- 4
R16 | 1447 26 37 20 27 15 39 24 --- 11 | 13 14 15 13 13 4 2 --- 2
R17 | 938 37 39 22 12 23 14 23 --- 9 | 13 14 13 14 15 2 3 --- 3
R18 | 538 23 39 15 11 27 18 19 --- 8 | 13 14 13 14 15 4 2 --- 3
R19 | 739 65 75 51 17 52 29 45 --- 19 | 13 14 13 16 17 3 3 --- 4
R20 | 705 28 30 31 21 26 65 29 --- 15 | 14 15 14 16 15 6 4 --- 4
R21 | 978 44 36 32 22 25 15 22 350 12 | 14 14 13 17 15 2 3 2 3
R22 | 1503 44 43 28 11 23 18 36 --- 12 | 14 14 14 14 14 5 3 --- 2
R23 | 1025 30 27 10 28 11 28 15 --- 9 | 13 14 13 15 14 4 2 --- 2
R24 | 3215 34 41 13 19 21 71 31 --- 15 | 14 15 14 15 14 3 3 --- 4
XR26 | ---- 34 97 --- --- --- --- 17 --- 24 | 15 19 --- --- --- --- 6 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1478 36 38 23 18 25 32 23 199 |T 13 14 13 14 14 3 2 2 3
WRMS | 1478 36 39 23 15 26 31 23 199 |NE 13 14 13 14 14 4 2 2 3
MEDI | 1272 33 36 20 14 23 18 19 159 |MD 14 14 13 14 14 4 2 2 3
Table 3.1944.6 GPS week: 1944 Day: 6 MJD: 57858
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 831 45 65 20 11 30 18 22 --- 10 | 17 17 17 17 17 3 2 --- 2
R02 | 1733 19 19 17 9 17 7 8 143 5 | 16 17 17 16 17 2 2 9999 2
R03 | 882 37 39 25 8 24 16 10 169 8 | 16 17 16 17 17 2 2 3 2
R04 | 1185 28 35 15 11 22 15 7 --- 7 | 17 17 17 17 17 3 2 --- 2
R05 | 563 22 27 24 24 27 47 32 --- 13 | 17 18 17 17 18 3 4 --- 2
R06 | 964 29 35 19 21 27 38 14 --- 11 | 16 17 17 19 17 4 2 --- 4
R07 | 798 42 49 14 10 24 19 15 102 8 | 17 17 17 17 17 2 2 9999 2
R08 | 699 28 29 14 12 26 28 12 --- 8 | 17 17 17 18 18 2 3 --- 3
XR09 | 2487 17 19 12 7 16 --- 12 --- 5 | 17 17 17 17 17 --- 2 --- 1
R10 | 1145 47 44 18 12 23 30 14 --- 10 | 16 16 16 17 17 9999 2 --- 3
R11 | 774 28 32 19 6 24 18 17 198 7 | 16 17 17 17 17 2 2 3 1
XR12 |18688 10 24 --- --- --- --- --- --- 0 | 1 1 --- --- --- --- --- --- 1
R13 | 2544 17 25 14 14 19 27 16 --- 7 | 17 17 17 17 17 4 3 --- 2
R14 | 968 39 47 14 12 15 30 19 --- 9 | 16 18 16 17 17 2 1 --- 2
R15 | 796 31 32 35 11 22 19 29 --- 11 | 16 17 17 17 17 3 3 --- 3
R16 | 1057 32 37 50 17 21 40 23 --- 14 | 17 17 17 17 17 4 2 --- 2
R17 | 949 41 30 37 16 37 17 24 --- 12 | 16 17 17 17 17 2 1 --- 2
R18 | 778 21 19 22 8 15 21 24 --- 8 | 16 17 16 17 17 1 2 --- 1
R19 | 1651 57 49 38 15 39 25 35 --- 14 | 17 17 17 18 18 3 3 --- 3
R20 | 1938 42 43 24 18 32 50 30 --- 14 | 17 17 17 17 17 3 4 --- 2
R21 | 1434 41 45 23 16 35 31 31 337 12 | 17 17 17 18 18 2 4 2 3
R22 | 1397 41 41 24 7 33 22 27 --- 10 | 17 17 17 17 18 3 2 --- 2
R23 | 919 36 40 13 28 8 36 20 --- 11 | 17 17 17 17 17 3 2 --- 2
R24 | 2497 23 18 29 24 19 66 29 --- 15 | 17 18 17 18 17 2 3 --- 3
XR26 | ---- 30 100 --- --- --- --- 15 --- 21 | 17 17 --- --- --- --- 2 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS | 1321 35 38 25 15 26 31 22 206 |T 16 16 16 17 17 2 2 2 2
WRMS | 1321 35 37 25 14 20 30 22 206 |NE 15 16 16 17 17 2 2 2 2
MEDI | 968 31 35 20 12 24 25 19 169 |MD 17 17 17 17 17 3 2 3 2
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