[IGSREPORT-24413] Wk 1892 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Apr 28 16:15:18 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1892 (Apr 10, 2016 - Apr 16, 2016)
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 2.1892.
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:
igl1892[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1892 in the SP3 format.
igl18927.sum Combination Report for GPS Week 1892.
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
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 | -8.6 ns
1 | -6.4 ns
2 | -5.7 ns
3 | -7.5 ns
4 | -7.7 ns
5 | -5.6 ns
6 | -8.7 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 1.1892, 1a.1892).
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 2.1892.0-6)
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 3.1892.0-6).
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 1892 summary. (Apr 10, 2016 - Apr 16, 2016)
Table 1.1892.a GPS week : 1892 MJD: 57488.0-57494.0
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 16 5 -7 -22 .22 30 30 | --- --- --- ---
| 1 1 2 23 30 41 .04 | --- ---
cof n/a| 0 1 16 11 0 -29 .23 33 32 | --- --- --- ---
| 1 1 2 13 23 60 .06 | --- ---
emx n/a| 0 0 4 -17 -80 -55 .20 28 28 | -1465 -652 3609 7197
| 1 1 1 25 34 29 .03 | 8131 643
esx n/a| 0 0 0 29 -16 21 -.16 17 16 | -7488 -2094 3648 8484
| 1 0 1 17 13 32 .03 | 4708 1858
gfz n/a| -1 1 -4 14 44 44 .00 20 18 | 0 -1334 3520 6826
| 1 1 1 34 25 22 .03 | 0 1531
grg n/a| 1 -1 -1 -39 54 -86 -.29 34 34 | -431524 -1611 5256 617002
| 1 1 4 19 26 35 .07 | 3546 1503
iac n/a| 1 0 -4 -12 4 0 .09 17 17 | -6486 -420 3647 6966
| 1 1 1 35 34 30 .03 | 1588 981
mcc n/a| 3 0 6 -16 59 -6 .07 152 152 | --- --- --- ---
| 12 5 21 251 106 366 .63 | --- ---
Table 1.1892.b GPS week : 1892 MJD: 57488.0-57494.0
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 | 11 13 12 14 12 12 12 |
R02 | 9 8 8 7 8 8 7 |
R03 | 9 8 8 10 8 9 10 |
R04 | 8 8 7 9 9 8 9 |
R05 | 13 11 13 10 13 11 11 |
R06 | 9 9 9 8 9 7 8 |
R07 | 8 8 8 9 8 7 9 |
R08 | 8 10 10 9 9 8 9 |
R09 | 9 9 8 8 7 7 8 |
R10 | 10 10 10 10 9 7 7 |
R13 | 8 9 10 8 10 11 12 |
R14 | 14 16 12 13 15 15 15 |
R15 | 14 13 14 11 11 12 13 |
R16 | 17 14 13 10 11 12 16 |
R17 | 12 10 9 9 11 8 8 |
R18 | 9 8 7 7 7 8 9 |
R19 | 6 9 10 10 8 9 9 |
R20 | 14 15 10 11 12 12 12 |
R21 | 10 8 9 10 8 10 9 |
R22 | 10 11 10 8 10 9 11 |
R23 | 9 7 8 9 9 9 10 |
R24 | 18 15 11 14 14 16 11 |
R26 | 43 112 76 20 80 0 0 |
Table 1.1892.c GPS week : 1892 MJD: 57488.0-57494.0
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 1892 0 | 90 36 -6 298 2090 -889 85.3 1498 1498 | -8580 0
brd 1892 1 | -78 55 75 -1749 -9 -865 85.5 1612 1612 | -6356 0
brd 1892 2 | 103 -25 37 1216 -1400 -580 86.0 1540 1540 | -5678 0
brd 1892 3 | -24 0 120 -584 -401 -258 85.8 1554 1554 | -7459 0
brd 1892 4 | 37 5 92 -554 -360 155 84.7 1392 1392 | -7674 0
brd 1892 5 | -6 21 132 -840 42 -684 84.2 1360 1360 | -5618 0
brd 1892 6 | -93 -8 180 -2266 -902 1002 83.3 1342 1342 | -8672 0
-------------+------------------------------------------------------------+----------------
brd 1892 mean| 4 12 90 -639 -134 -302 85.0 1471 1471 | -7148 0
brd 1892 sdev| 76 27 62 1172 1103 683 .9 106 106 | 1282 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 2.1892.0 GPS week: 1892 Day: 0 MJD: 57488
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 3 17 19 -44 -9 .17 32 31 | --- --- --- ---
cof n/a| 0 3 14 27 0 -39 .15 33 31 | --- --- --- ---
emx n/a| 0 -2 4 -42 -114 -88 .18 33 35 | -5477 -903 3309 6051
esx n/a| 2 0 -2 22 -10 64 -.20 19 18 | -5182 -3737 3342 7295
gfz n/a| -2 1 -4 36 50 41 -.04 21 19 | 0 -2479 3308 5606
grg n/a| -1 -2 1 -64 28 -133 -.22 34 32 | -429481 -2564 3308 617744
iac n/a| 2 0 -4 -12 23 2 .10 15 15 | -8726 244 3350 5818
mcc n/a| 1 5 -11 30 -57 -464 .40 189 189 | --- --- --- ---
Table 2.1892.1 GPS week: 1892 Day: 1 MJD: 57489
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 12 -16 -43 30 .23 30 29 | --- --- --- ---
cof n/a| -1 2 18 6 -19 -2 .31 34 32 | --- --- --- ---
emx n/a| 1 0 2 4 -104 -56 .22 29 31 | -8723 415 3774 6325
esx n/a| 0 0 1 48 -28 -2 -.18 17 17 | -5951 -1527 3800 8108
gfz n/a| 0 1 -2 36 39 13 .02 19 19 | 0 402 3663 5866
grg n/a| 0 0 2 -45 30 -81 -.27 38 41 | -429346 156 3780 617338
iac n/a| 0 0 -5 -54 53 1 .13 19 19 | -5829 -392 3822 6057
mcc n/a| -1 -3 -14 1 83 -443 -.06 142 142 | --- --- --- ---
Table 2.1892.2 GPS week: 1892 Day: 2 MJD: 57490
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 8 -11 8 .28 31 32 | --- --- --- ---
cof n/a| 0 -1 13 19 10 21 .26 31 31 | --- --- --- ---
emx n/a| 1 0 3 7 -27 -81 .18 25 25 | 10597 96 3290 7265
esx n/a| 1 0 -1 57 -13 57 -.15 16 16 | -11754 837 3292 8233
gfz n/a| -3 1 -4 61 44 19 -.02 23 16 | 0 -374 3106 6898
grg n/a| 3 0 2 -45 80 -118 -.20 29 28 | -430432 368 7960 616152
iac n/a| 1 1 -5 -59 -27 14 .10 17 17 | -5031 187 3295 6981
mcc n/a| 3 3 -2 84 2 -158 -.48 88 88 | --- --- --- ---
Table 2.1892.3 GPS week: 1892 Day: 3 MJD: 57491
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 14 -27 29 -1 .27 30 30 | --- --- --- ---
cof n/a| 0 1 15 -11 -11 53 .20 33 33 | --- --- --- ---
emx n/a| 2 2 2 6 -48 -33 .24 25 25 | -10266 -1269 3295 8601
esx n/a| 0 -2 0 23 0 45 -.15 16 15 | 1119 -3812 3326 9223
gfz n/a| -1 1 -3 20 75 46 -.02 19 16 | 0 -2845 3342 7920
grg n/a| 0 -1 -3 -2 23 -80 -.32 35 36 | -429148 -3461 3940 616651
iac n/a| 0 0 -4 -21 -46 -66 .05 17 17 | -5125 -1917 3307 8370
mcc n/a| 10 -2 22 263 210 249 -.13 71 71 | --- --- --- ---
Table 2.1892.4 GPS week: 1892 Day: 4 MJD: 57492
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 15 27 -56 .21 29 28 | --- --- --- ---
cof n/a| -1 1 17 1 46 -88 .27 33 32 | --- --- --- ---
emx n/a| 0 -2 5 -11 -65 -82 .18 30 31 | -499 -845 3689 6849
esx n/a| 0 0 0 13 -35 -17 -.14 17 17 | -7543 -3927 3706 8459
gfz n/a| 0 3 -6 -34 52 56 .02 20 18 | 0 -3121 3684 6786
grg n/a| 0 -1 -3 -48 73 -19 -.30 33 35 | -431341 -3016 3690 617865
iac n/a| 1 0 -3 33 -5 27 .05 16 16 | -6687 -1519 3697 6510
mcc n/a| -4 -4 -6 10 34 504 -.84 180 180 | --- --- --- ---
Table 2.1892.5 GPS week: 1892 Day: 5 MJD: 57493
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 19 -6 7 -40 .24 29 28 | --- --- --- ---
cof n/a| 0 0 16 14 -20 -31 .21 33 30 | --- --- --- ---
emx n/a| 0 0 5 -31 -111 -14 .18 25 25 | 8354 -948 3909 8143
esx n/a| 0 0 -2 9 -25 3 -.11 18 17 | -11433 -423 4072 9707
gfz n/a| 0 4 -6 10 56 59 .03 18 19 | 0 495 3691 7676
grg n/a| 1 0 -2 -29 85 -88 -.34 32 34 | -431676 -1147 4198 616990
iac n/a| 1 -1 -3 16 3 8 .08 17 17 | -5400 -354 4067 7986
mcc n/a| -10 -5 45 42 -46 218 .81 157 157 | --- --- --- ---
Table 2.1892.6 GPS week: 1892 Day: 6 MJD: 57494
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 14 43 -20 -89 .17 30 29 | --- --- --- ---
cof n/a| 0 0 19 22 -10 -120 .18 33 33 | --- --- --- ---
emx n/a| -1 -2 5 -55 -90 -34 .24 27 26 | -4241 -1116 3998 7146
esx n/a| -1 0 0 31 -2 2 -.14 16 17 | -11672 -2074 4001 8369
gfz n/a| 0 1 -5 -26 -5 77 .04 22 19 | 0 -1418 3849 7030
grg n/a| 4 -1 -8 -38 60 -86 -.38 36 34 | -439247 -1617 9920 616279
iac n/a| 3 1 -1 13 32 6 .08 18 18 | -8607 810 3991 7046
mcc n/a| 27 8 13 -548 187 50 .79 238 238 | --- --- --- ---
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 3.1892.0 GPS week: 1892 Day: 0 MJD: 57488
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 | 995 41 39 28 16 25 27 19 --- 11 | 80 76 69 74 82 84 82 --- 76
R02E | 1579 27 28 36 16 15 22 8 --- 9 | 29 33 24 40 33 40 32 --- 30
R03E | 1364 28 37 28 11 20 27 12 142 8 | 50 51 46 42 45 50 49 97 43
R04E | 1408 23 23 19 11 19 27 11 --- 7 | 32 29 33 32 37 39 27 --- 29
R05E | 1398 38 47 49 28 19 34 18 --- 13 | 92 103 83 82 81 79 88 --- 81
R06E | 2038 16 23 23 16 14 36 13 --- 8 | 25 25 32 23 24 31 29 --- 23
R07E | 1528 20 23 24 11 17 24 13 280 7 | 52 55 48 51 50 56 46 85 48
R08E | 1977 20 22 21 15 22 27 11 --- 8 | 34 35 26 33 35 41 27 --- 28
R09 | 1252 25 20 27 19 14 24 12 --- 8 | 28 20 28 32 33 25 20 --- 23
R10 | 796 32 21 26 18 19 36 8 --- 9 | 34 27 22 29 14 26 17 --- 17
R13 | 685 31 35 17 12 21 25 11 --- 8 | 30 34 20 20 17 33 13 --- 13
R14 | 2154 58 59 36 19 32 27 20 --- 14 | 42 67 31 43 34 32 27 --- 28
R15 | 2551 45 46 36 21 39 47 13 --- 14 | 52 54 32 33 35 22 21 --- 23
XR16 | 601 38 69 44 --- 22 61 14 --- 16 | 34 48 49 --- 31 39 27 --- 27
XR17 | 698 37 40 30 --- 17 24 17 --- 12 | 71 76 62 --- 50 45 33 --- 46
R18 | 952 22 19 31 19 12 22 12 --- 8 | 56 56 56 46 38 34 30 --- 39
R19 | 2589 21 20 20 9 13 20 9 --- 6 | 66 66 58 50 43 41 37 --- 45
R20 | 637 34 41 36 20 17 65 20 --- 13 | 61 63 66 59 57 31 43 --- 50
R21 | 529 32 37 28 19 15 35 16 95 10 | 70 70 65 51 40 39 34 56 45
R22 | 702 40 37 35 16 12 25 16 --- 10 | 76 75 63 45 41 28 33 --- 42
R23 | 817 18 17 13 25 19 27 15 --- 9 | 39 41 44 60 47 58 40 --- 46
R24 | 1376 33 33 71 33 30 60 26 --- 18 | 85 80 93 76 52 48 50 --- 62
XR26 | ---- 71 881 --- --- --- --- 26 --- 43 | 88 9999 --- --- --- --- 33 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1497 32 33 33 19 21 34 15 189 |T 53 53 47 46 41 41 36 79 39
WRMS | 1497 31 31 35 18 19 32 15 189 |NE 55 55 49 45 38 35 30 56 36
MEDI | 1252 32 35 28 16 19 27 13 142 |MD 52 54 46 43 38 39 33 85 40
Table 3.1892.1 GPS week: 1892 Day: 1 MJD: 57489
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 | 1029 39 39 39 18 32 37 23 --- 13 | 66 68 53 65 76 66 49 --- 58
R02E | 2106 25 28 28 14 13 27 11 --- 8 | 24 28 33 28 30 27 23 --- 23
R03E | 1996 32 31 23 12 15 22 10 96 8 | 45 51 41 37 39 43 40 60 37
R04E | 1692 24 30 25 12 17 27 11 --- 8 | 28 39 26 28 29 31 20 --- 22
R05E | 1082 26 44 17 21 19 27 30 --- 10 | 96 106 96 93 99 91 98 --- 93
R06E | 936 23 28 13 11 24 21 21 --- 8 | 35 36 25 25 26 27 20 --- 20
R07E | 1307 24 24 18 12 24 21 15 212 8 | 52 53 43 48 53 48 42 23 45
R08E | 1195 25 18 21 21 20 29 15 --- 9 | 33 36 27 37 35 37 24 --- 27
R09 | 1565 28 28 19 9 11 42 13 --- 8 | 21 24 18 24 27 36 19 --- 19
R10 | 1101 32 32 18 18 10 45 12 --- 9 | 34 35 22 31 23 22 14 --- 20
R13 | 927 33 31 24 15 14 31 11 --- 9 | 22 24 21 25 21 20 15 --- 14
R14 | 2081 58 47 53 22 19 46 19 --- 15 | 28 31 41 43 43 20 27 --- 29
R15 | 3691 41 48 28 23 33 34 23 --- 13 | 38 46 26 32 35 23 15 --- 20
R16 | 711 27 24 32 25 21 55 30 --- 13 | 45 55 36 41 28 24 24 --- 22
R17 | 674 34 37 29 17 22 18 19 --- 10 | 46 49 42 45 34 33 22 --- 30
R18 | 696 18 20 20 17 19 19 17 --- 8 | 32 36 38 37 30 31 23 --- 28
R19 | 2872 25 28 26 14 18 27 18 --- 9 | 41 48 39 39 32 29 18 --- 29
R20 | 634 18 34 48 12 10 88 15 --- 14 | 39 49 50 35 40 23 29 --- 31
R21 | 490 23 24 19 15 14 26 19 76 8 | 47 48 42 40 43 27 27 19 35
R22 | 1019 24 32 35 20 19 31 26 --- 11 | 45 56 55 52 47 32 25 --- 40
R23 | 1179 14 20 14 12 11 26 13 --- 6 | 33 35 31 30 29 40 22 --- 27
R24 | 2090 27 60 42 29 22 64 29 --- 15 | 63 97 55 56 47 33 41 --- 47
XR26 | ---- 161 >>>> --- --- --- --- 77 --- 112 | 141 9999 --- --- --- --- 33 --- 53
------+---------------------------------------------------+-----------------------------------------------
RMS | 1611 30 34 29 17 19 38 19 141 |T 45 47 39 40 39 34 29 34 33
WRMS | 1611 29 32 31 17 19 41 19 141 |NE 45 45 36 37 34 28 23 19 29
MEDI | 1101 26 31 24 15 19 27 18 96 |MD 39 46 38 37 34 31 24 23 29
Table 3.1892.2 GPS week: 1892 Day: 2 MJD: 57490
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 | 1541 40 28 27 20 24 30 21 --- 11 | 59 58 37 53 53 57 34 --- 42
R02E | 1988 19 19 23 12 18 28 10 --- 8 | 24 23 23 28 38 46 20 --- 24
R03E | 3037 29 33 19 14 16 30 10 53 8 | 50 50 33 39 44 44 38 77 37
R04E | 1588 24 21 15 11 14 18 8 --- 6 | 29 33 29 28 31 28 24 --- 24
R05E | 1044 29 35 50 22 20 31 19 --- 13 | 49 59 78 55 45 48 51 --- 49
R06E | 1794 30 30 20 19 20 24 16 --- 9 | 32 32 18 32 26 35 21 --- 19
R07E | 1970 25 29 16 13 28 19 14 124 8 | 49 48 33 45 46 45 40 27 40
R08E | 1113 26 26 18 22 27 21 23 --- 10 | 33 35 20 38 44 35 21 --- 25
R09 | 2210 34 35 15 12 22 20 13 --- 8 | 25 27 21 22 31 28 22 --- 19
R10 | 608 32 36 22 17 27 26 20 --- 10 | 36 42 29 29 25 15 16 --- 19
R13 | 897 28 28 27 17 20 38 9 --- 10 | 27 26 22 21 18 30 17 --- 13
R14 | 1075 41 51 30 17 18 36 20 --- 11 | 31 48 40 31 31 16 25 --- 23
R15 | 2689 43 33 30 13 51 23 20 --- 13 | 39 35 28 26 70 17 14 --- 21
R16 | 602 45 42 30 19 29 44 21 --- 13 | 39 48 37 34 43 24 27 --- 29
R17 | 830 36 37 21 15 19 28 9 --- 9 | 55 55 40 24 33 36 29 --- 30
R18 | 686 20 18 17 12 18 15 7 --- 6 | 41 41 35 29 27 35 27 --- 28
R19 | 1342 36 31 28 17 15 24 19 --- 10 | 49 46 40 36 26 21 16 --- 25
R20 | 1116 20 31 28 17 17 37 12 --- 9 | 40 50 42 37 47 25 34 --- 33
R21 | 651 19 25 22 10 16 30 19 70 8 | 52 53 53 40 35 51 28 20 38
R22 | 501 26 19 30 15 11 33 23 --- 10 | 57 50 62 46 39 32 24 --- 39
R23 | 1326 28 25 12 24 15 19 10 --- 8 | 32 33 43 58 42 50 41 --- 44
R24 | 1796 34 28 25 14 25 39 22 --- 11 | 81 71 68 56 52 58 45 --- 53
XR26 | ---- 124 1976 --- --- --- --- 45 --- 76 | 97 9999 --- --- --- --- 30 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1540 31 31 25 16 23 29 17 88 |T 44 43 37 36 38 35 28 41 31
WRMS | 1540 32 31 25 16 16 28 17 88 |NE 46 44 40 34 37 31 26 20 30
MEDI | 1116 29 30 22 15 19 28 19 70 |MD 40 46 35 34 38 35 27 27 29
Table 3.1892.3 GPS week: 1892 Day: 3 MJD: 57491
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 | 1250 37 32 22 18 38 37 34 --- 14 | 54 60 51 67 79 72 33 --- 53
R02E | 970 19 19 19 10 15 34 9 --- 7 | 24 27 19 25 29 39 19 --- 20
R03E | 2740 26 35 29 13 23 28 13 64 9 | 38 42 32 39 42 41 35 155 33
R04E | 1624 27 32 15 12 18 34 19 --- 8 | 34 36 30 28 34 43 22 --- 25
R05E | 670 24 32 28 20 15 33 24 --- 10 | 47 49 61 58 51 51 49 --- 49
R06E | 921 31 37 19 14 15 23 14 --- 8 | 31 36 22 33 27 26 17 --- 19
R07E | 2312 29 26 17 13 26 28 15 62 9 | 51 51 42 49 53 48 37 30 42
R08E | 869 29 27 21 21 18 24 16 --- 9 | 35 39 24 38 39 36 23 --- 28
R09 | 1927 20 30 22 8 10 43 9 --- 7 | 24 38 30 23 31 26 18 --- 20
R10 | 789 28 29 19 19 25 37 14 --- 9 | 37 36 37 34 23 16 16 --- 22
R13 | 1634 28 33 15 13 13 31 9 --- 7 | 28 33 30 20 17 20 12 --- 15
R14 | 1075 46 47 44 19 8 49 13 --- 12 | 39 38 40 43 37 19 31 --- 32
R15 | 3625 34 31 19 12 33 38 18 --- 11 | 38 40 31 25 48 20 11 --- 22
R16 | 520 36 56 25 19 9 43 15 --- 10 | 43 52 24 39 32 22 29 --- 29
R17 | 1106 38 36 19 19 13 24 19 --- 9 | 62 62 43 41 42 36 25 --- 38
R18 | 508 18 16 24 9 12 21 12 --- 6 | 44 46 40 42 39 25 32 --- 35
R19 | 1312 36 43 27 10 17 31 19 --- 9 | 55 65 46 41 38 36 17 --- 32
R20 | 1203 31 25 26 22 16 43 16 --- 10 | 56 56 46 45 31 27 29 --- 33
R21 | 985 27 20 36 16 14 22 16 86 9 | 52 49 56 43 36 28 30 35 35
R22 | 524 29 36 22 10 12 30 16 --- 8 | 59 63 52 46 45 23 29 --- 40
R23 | 1788 33 28 14 19 18 23 12 --- 8 | 40 44 46 61 60 38 40 --- 48
R24 | 1545 27 37 44 27 11 61 21 --- 13 | 66 79 65 81 62 49 50 --- 61
XR26 | ---- 31 489 --- --- --- --- 13 --- 19 | 66 9999 --- --- --- --- 29 --- 47
------+---------------------------------------------------+-----------------------------------------------
RMS | 1553 30 33 25 16 19 35 17 71 |T 44 47 39 41 40 33 27 73 33
WRMS | 1553 30 33 25 15 16 36 17 71 |NE 47 50 41 41 38 27 26 35 33
MEDI | 1106 29 32 22 14 15 31 15 64 |MD 43 44 40 41 38 28 29 35 33
Table 3.1892.4 GPS week: 1892 Day: 4 MJD: 57492
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 | 2543 46 47 27 17 30 33 20 --- 12 | 59 57 43 50 57 55 35 --- 42
R02E | 601 19 21 21 12 19 28 12 --- 7 | 24 28 20 28 31 29 23 --- 20
R03E | 1819 21 19 27 12 18 27 15 264 8 | 47 40 40 48 48 47 37 154 41
R04E | 798 23 24 20 13 22 26 15 --- 8 | 30 29 24 25 36 37 24 --- 24
R05E | 1165 38 53 40 27 23 35 21 --- 13 | 69 89 58 63 62 46 54 --- 54
R06E | 992 26 29 26 17 18 26 15 --- 9 | 28 33 25 30 29 30 21 --- 20
R07E | 1061 28 37 15 13 13 27 11 159 7 | 41 51 37 40 37 49 28 68 33
R08E | 725 29 25 21 14 18 23 16 --- 8 | 42 44 22 34 31 37 22 --- 24
R09 | 1518 16 17 13 9 16 21 18 --- 7 | 15 20 18 16 24 16 19 --- 15
R10 | 1213 17 22 11 22 16 37 18 --- 9 | 27 27 19 39 28 26 16 --- 23
R13 | 1701 30 28 20 20 20 34 14 --- 9 | 31 32 26 22 28 16 16 --- 16
R14 | 790 48 37 68 17 19 38 14 --- 15 | 44 42 41 32 24 16 29 --- 20
R15 | 3433 32 44 30 19 27 34 15 --- 11 | 31 41 31 30 26 23 14 --- 17
R16 | 771 21 41 28 23 14 49 14 --- 10 | 32 56 37 50 41 33 32 --- 37
R17 | 1330 37 42 27 12 20 41 18 --- 10 | 54 57 44 30 36 23 17 --- 27
R18 | 567 21 32 15 14 10 25 14 --- 7 | 39 48 33 37 26 18 22 --- 27
R19 | 908 24 25 26 12 15 23 16 --- 8 | 48 49 40 32 26 21 31 --- 30
R20 | 1073 18 39 41 20 32 38 18 --- 12 | 45 66 37 46 41 54 26 --- 33
R21 | 908 28 30 21 10 13 22 12 42 7 | 47 48 44 30 24 27 22 41 27
R22 | 731 37 35 28 15 20 31 13 --- 10 | 50 51 47 40 31 31 25 --- 31
R23 | 1344 31 33 16 19 17 16 15 --- 8 | 30 34 41 48 41 38 42 --- 39
R24 | 964 17 25 51 21 19 64 24 --- 14 | 45 47 84 58 58 24 38 --- 47
XR26 | ---- 124 115 --- --- --- --- 52 --- 80 | 87 9999 --- --- --- --- 59 --- 65
------+---------------------------------------------------+-----------------------------------------------
RMS | 1391 29 33 30 17 20 33 16 180 |T 41 44 36 37 35 31 28 87 30
WRMS | 1391 28 32 31 17 18 35 16 180 |NE 41 44 38 36 32 26 27 41 30
MEDI | 992 28 32 26 15 18 28 15 159 |MD 42 44 37 34 31 29 25 68 27
Table 3.1892.5 GPS week: 1892 Day: 5 MJD: 57493
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 | 2667 41 36 30 24 25 32 14 --- 12 | 49 50 39 49 48 54 40 --- 40
R02E | 872 23 22 18 16 15 22 17 --- 8 | 28 26 25 25 25 26 20 --- 18
R03E | 779 25 25 17 14 19 25 17 179 8 | 46 46 37 39 42 51 50 81 41
R04E | 1741 23 15 15 14 18 20 19 --- 8 | 37 33 38 40 48 43 21 --- 34
R05E | 1555 31 38 25 19 21 27 23 --- 10 | 60 67 59 59 65 56 62 --- 57
R06E | 1278 20 27 14 14 16 20 14 --- 7 | 21 24 24 27 26 33 21 --- 20
R07E | 1281 24 28 16 15 14 14 9 177 6 | 59 56 52 55 55 47 50 40 51
R08E | 911 29 41 11 19 14 24 7 --- 7 | 41 48 23 24 27 33 26 --- 23
R09 | 832 21 21 17 10 10 20 16 --- 6 | 15 17 18 22 26 28 24 --- 19
R10 | 1065 18 21 20 10 14 17 13 --- 6 | 24 26 21 17 19 18 15 --- 13
R13 | 699 28 32 28 16 23 45 13 --- 11 | 24 33 29 30 27 30 16 --- 19
R14 | 1680 57 73 45 24 17 30 24 --- 14 | 46 63 30 37 40 19 22 --- 24
R15 | 2834 30 31 24 20 28 48 13 --- 11 | 32 32 27 27 32 22 13 --- 18
R16 | 720 15 31 25 30 14 56 14 --- 12 | 27 48 39 33 14 19 26 --- 18
R17 | 1116 20 20 12 17 10 22 21 --- 7 | 47 47 40 39 46 35 29 --- 39
R18 | 516 27 19 21 11 17 25 14 --- 8 | 40 31 35 26 24 23 21 --- 23
R19 | 1169 29 28 24 11 17 16 16 --- 8 | 39 40 34 20 22 29 15 --- 21
R20 | 1192 33 36 30 23 21 38 23 --- 12 | 55 56 45 38 26 41 27 --- 31
R21 | 620 33 41 25 16 22 20 17 104 9 | 41 48 33 30 20 22 18 18 21
R22 | 501 34 32 19 16 19 19 13 --- 8 | 43 42 33 31 20 26 22 --- 24
R23 | 813 30 35 26 21 14 18 11 --- 8 | 19 22 30 31 18 29 28 --- 23
R24 | 1822 25 20 45 23 20 69 25 --- 15 | 42 43 66 43 45 14 30 --- 35
XR26 | ---- --- --- --- --- --- --- 2 --- 0 | --- --- --- --- --- --- 58 --- 58
------+---------------------------------------------------+-----------------------------------------------
RMS | 1359 29 33 25 18 18 32 17 157 |T 37 40 35 33 32 31 28 46 29
WRMS | 1359 28 30 25 17 19 34 17 157 |NE 35 39 34 30 27 25 24 18 25
MEDI | 1065 27 28 21 16 17 22 14 177 |MD 40 42 33 31 26 29 24 40 23
Table 3.1892.6 GPS week: 1892 Day: 6 MJD: 57494
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 | 1309 45 42 20 23 26 32 22 --- 12 | 50 51 46 58 58 57 34 --- 45
R02E | 787 26 23 16 9 15 31 8 --- 7 | 32 31 16 21 21 30 20 --- 16
R03E | 1435 29 34 25 15 23 29 22 222 10 | 64 63 44 47 47 64 60 108 49
R04E | 1345 21 20 18 13 22 26 18 --- 8 | 30 31 20 24 33 28 29 --- 22
R05E | 2250 25 32 32 16 22 32 28 --- 11 | 71 80 70 63 66 65 68 --- 64
R06E | 890 24 23 17 12 23 25 16 --- 8 | 24 26 22 26 32 38 20 --- 22
R07E | 962 30 29 23 12 21 22 20 304 9 | 117 118 120 122 122 110 112 58 116
R08E | 1401 32 33 19 18 21 20 16 --- 9 | 39 38 27 27 37 31 25 --- 25
R09 | 782 12 23 21 13 11 23 20 --- 7 | 18 27 21 17 19 18 25 --- 15
R10 | 721 13 33 14 15 17 22 9 --- 6 | 29 38 25 31 19 19 21 --- 21
R13 | 1439 35 44 40 10 27 42 16 --- 12 | 34 39 39 23 24 29 19 --- 17
R14 | 1021 46 31 52 20 32 40 22 --- 15 | 40 33 22 38 34 15 25 --- 23
R15 | 2939 29 33 25 24 41 49 8 --- 13 | 41 44 42 33 31 18 23 --- 23
R16 | 714 33 51 48 14 17 85 16 --- 15 | 36 43 28 33 27 17 29 --- 23
R17 | 1053 27 26 24 10 19 19 14 --- 8 | 62 62 53 33 32 23 28 --- 36
R18 | 592 17 26 19 17 11 18 27 --- 8 | 50 55 43 41 36 25 22 --- 32
R19 | 1877 33 37 20 9 13 30 18 --- 8 | 63 62 48 34 29 22 21 --- 32
R20 | 1895 32 41 29 12 27 55 14 --- 11 | 62 73 56 46 39 31 34 --- 39
R21 | 519 27 20 16 16 13 39 17 170 9 | 58 55 46 43 28 24 27 19 34
R22 | 621 42 39 30 12 20 31 14 --- 10 | 61 56 50 34 28 31 23 --- 31
R23 | 721 25 30 26 24 24 15 11 --- 9 | 21 22 29 51 36 35 38 --- 35
R24 | 1216 26 30 25 15 21 43 21 --- 10 | 60 57 57 54 39 29 40 --- 43
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 50 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1341 30 33 27 16 22 36 18 238 |T 48 50 42 40 38 34 34 61 35
WRMS | 1341 29 33 26 17 19 34 18 238 |NE 45 47 39 36 30 24 28 19 29
MEDI | 1021 27 31 23 14 21 30 16 222 |MD 41 44 42 34 32 29 27 58 32
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