[IGSREPORT-26669] Wk 2057 IGLOS Final Orbits
acc
acc at igs.org
Sun Jul 7 18:46:36 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2057 (Jun 09, 2019 - Jun 15, 2019)
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 2.2057.
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:
igl2057[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2057 in the SP3 format.
igl20577.sum Combination Report for GPS Week 2057.
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 | -0.9 ns
1 | 1.4 ns
2 | 0.4 ns
3 | 2.6 ns
4 | 0.6 ns
5 | 2.0 ns
6 | 0.2 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 1.2057, 1a.2057).
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 2.2057.0-6)
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 3.2057.0-6).
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 2057 summary. (Jun 09, 2019 - Jun 15, 2019)
Table 1.2057.a GPS week : 2057 MJD: 58643.0-58649.0
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 0 25 -12 19 .15 23 21 | 16040 164 3620 12246
| 1 0 1 17 19 26 .03 | 463 1906
cof n/a| 0 0 0 24 3 19 .13 26 23 | 16028 169 3621 12250
| 1 0 1 14 30 37 .04 | 459 1900
emx n/a| 0 1 5 -11 -23 39 .03 24 24 | -9398 -9 3510 11530
| 1 1 3 17 15 39 .05 | 12313 1059
esx n/a| 0 0 1 40 15 34 .07 22 20 | 2931 830 3556 14582
| 0 1 2 10 15 19 .03 | 14687 2119
gfz n/a| 0 0 -3 -14 15 14 .03 27 20 | 0 218 3556 12442
| 0 1 1 12 18 26 .07 | 0 2228
grg n/a| 1 -1 -1 -67 14 -152 -.35 28 24 | -653 302 4750 16892
| 0 1 3 17 22 105 .03 | 3606 2460
iac n/a| -2 0 0 6 -10 10 -.03 25 22 | 598 168 4790 17121
| 1 1 0 11 25 69 .04 | 3558 1916
mcc n/a| 3 -1 -15 16 28 38 -.29 214 214 | --- --- --- ---
| 9 5 17 64 136 667 .46 | --- ---
Table 1.2057.b GPS week : 2057 MJD: 58643.0-58649.0
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 | 19 15 14 13 15 16 15 |
R02 | 7 8 7 7 6 7 7 |
R03 | 8 8 5 5 7 5 7 |
R04 | 7 8 6 5 5 6 5 |
R05 | 8 8 8 9 9 8 11 |
R07 | 6 6 6 7 6 5 6 |
R08 | 7 9 8 8 8 7 8 |
R09 | 8 7 7 8 7 7 7 |
R10 | 7 10 8 9 8 8 7 |
R11 | 7 6 7 8 7 7 7 |
R13 | 9 7 7 7 7 7 6 |
R14 | 8 11 7 7 6 8 8 |
R15 | 9 8 9 8 8 9 9 |
R16 | 13 16 12 13 12 12 12 |
R17 | 10 9 10 9 8 11 12 |
R18 | 7 7 6 7 8 8 6 |
R19 | 26 26 26 24 25 25 27 |
R20 | 16 18 11 11 16 16 18 |
R21 | 8 10 11 10 11 11 10 |
R22 | 9 10 11 11 11 12 14 |
R23 | 11 11 11 12 10 12 12 |
R24 | 15 15 16 16 19 17 16 |
R26 | 17 13 14 14 14 13 14 |
Table 1.2057.c GPS week : 2057 MJD: 58643.0-58649.0
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 2057 0 | 1 -51 192 1152 -37 977 85.2 1391 1391 | -932 0
brd 2057 1 | 26 -32 209 656 22 1766 84.4 1389 1389 | 1409 0
brd 2057 2 | -42 36 182 -250 -595 3764 83.2 1571 1571 | 401 0
brd 2057 3 | -64 83 135 111 537 4447 84.2 1701 1701 | 2638 0
brd 2057 4 | -20 -2 116 74 -113 3820 83.2 1612 1612 | 578 0
brd 2057 5 | 34 -63 95 911 -506 788 83.7 1450 1450 | 1998 0
brd 2057 6 | -4 -61 130 128 -176 -648 84.0 1326 1326 | 152 0
-------------+------------------------------------------------------------+----------------
brd 2057 mean| -9 -13 151 397 -124 2130 84.0 1491 1491 | 892 0
brd 2057 sdev| 35 55 43 513 373 1909 .7 138 138 | 1207 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 2.2057.0 GPS week: 2057 Day: 0 MJD: 58643
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 0 28 7 -36 .16 25 22 | 15684 -2165 3227 12271
cof n/a| 0 0 1 12 -18 -51 .07 28 24 | 15662 -2145 3239 12281
emx n/a| 0 1 6 -28 -29 16 -.04 21 21 | -15871 -1070 3050 11719
esx n/a| 0 0 0 42 -11 30 .07 24 18 | 11317 -2337 3137 14769
gfz n/a| 0 0 -7 -14 34 -16 .07 29 18 | 0 -2934 3164 12561
grg n/a| 1 -1 1 -82 43 18 -.31 31 28 | 3630 -3667 4546 15610
iac n/a| -1 -1 0 24 -13 -26 -.06 24 22 | 4266 -2629 4632 16339
mcc n/a| 11 -2 9 14 222 1343 -.50 265 265 | --- --- --- ---
Table 2.2057.1 GPS week: 2057 Day: 1 MJD: 58644
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 0 -10 2 10 .16 22 19 | 15758 1454 3592 12712
cof n/a| 0 0 0 8 60 20 .07 27 22 | 15749 1446 3588 12723
emx n/a| 2 1 0 0 -48 29 .07 25 26 | -24688 1320 3483 12440
esx n/a| 1 -1 2 49 11 13 .02 24 20 | 28396 407 3476 14991
gfz n/a| 1 0 -1 -7 21 -7 -.03 28 18 | 0 2031 3481 12812
grg n/a| 1 0 0 -48 40 -36 -.35 28 24 | 32 1218 3999 12819
iac n/a| -3 1 -1 -8 -19 -51 -.01 28 24 | 1641 996 3993 12740
mcc n/a| 4 -6 -18 62 107 72 -.35 293 293 | --- --- --- ---
Table 2.2057.2 GPS week: 2057 Day: 2 MJD: 58645
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 0 43 -8 38 .18 23 26 | 15321 -1460 4012 11854
cof n/a| -1 0 0 36 0 38 .18 23 26 | 15319 -1475 4014 11858
emx n/a| 0 2 9 -11 -25 -2 .02 24 24 | 3060 -444 3951 11364
esx n/a| 0 -1 -2 28 10 24 .08 20 18 | 8799 -35 3955 14095
gfz n/a| 1 0 -4 -30 3 9 -.02 24 21 | 0 -1523 3936 11830
grg n/a| 0 0 3 -60 8 -147 -.32 27 22 | -1568 -2069 5042 18384
iac n/a| 0 1 -1 10 -20 49 -.05 23 21 | -572 -2248 5284 18934
mcc n/a| -12 9 -20 11 -205 -211 -.97 246 246 | --- --- --- ---
Table 2.2057.3 GPS week: 2057 Day: 3 MJD: 58646
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 0 24 -39 23 .17 26 23 | 16210 2879 3342 13110
cof n/a| 0 1 0 32 -11 48 .15 29 25 | 16209 2864 3343 13111
emx n/a| 0 -1 5 -15 -21 68 .13 23 23 | 8154 1174 3111 10250
esx n/a| 1 0 -1 34 16 70 .07 20 20 | -1256 4007 3300 15515
gfz n/a| 0 0 -1 -23 -1 64 .03 24 20 | 0 2755 3305 13480
grg n/a| 0 -2 -1 -42 22 -211 -.34 24 19 | -1965 3120 4231 16540
iac n/a| -3 1 0 13 44 -38 -.05 23 20 | 91 2131 4185 16128
mcc n/a| -8 -4 -15 -19 101 -623 -.65 187 187 | --- --- --- ---
Table 2.2057.4 GPS week: 2057 Day: 4 MJD: 58647
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 -1 37 -35 29 .11 23 20 | 16638 -929 3897 11213
cof n/a| -1 0 -1 13 -33 -7 .16 26 21 | 16615 -901 3896 11219
emx n/a| 2 0 5 -7 1 9 .03 23 23 | -3246 -856 3747 10637
esx n/a| 1 0 2 26 15 15 .10 23 19 | -7820 -42 3750 13351
gfz n/a| 0 0 -3 7 -8 5 .15 26 17 | 0 -726 3732 10990
grg n/a| 1 -1 -2 -83 -12 -222 -.35 27 21 | 2794 -428 4372 11777
iac n/a| -2 -1 -1 -2 -6 148 -.03 25 22 | 3623 117 4461 12718
mcc n/a| 4 -6 3 45 -59 -572 .07 183 183 | --- --- --- ---
Table 2.2057.5 GPS week: 2057 Day: 5 MJD: 58648
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 0 23 -14 32 .13 20 17 | 16370 1905 3643 12482
cof n/a| 1 0 -2 20 14 30 .13 24 21 | 16354 1926 3640 12479
emx n/a| 0 0 5 -35 -15 39 .03 25 25 | -20421 776 3606 12196
esx n/a| 0 1 4 53 30 43 .12 21 21 | -2348 3095 3652 14530
gfz n/a| 0 0 -3 -9 23 22 .03 31 20 | 0 2561 3645 12952
grg n/a| 1 -2 -5 -69 16 -204 -.41 30 26 | -165 2146 4077 12119
iac n/a| 0 0 0 -2 -31 10 -.06 25 23 | 1592 784 4053 12542
mcc n/a| 8 -3 -26 99 22 -67 .03 175 175 | --- --- --- ---
Table 2.2057.6 GPS week: 2057 Day: 6 MJD: 58649
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 -2 27 3 39 .10 22 21 | 16302 -534 3630 12080
cof n/a| 1 0 0 46 14 59 .12 24 22 | 16293 -531 3628 12082
emx n/a| 1 3 5 16 -26 111 .00 24 24 | -12777 -968 3626 12109
esx n/a| -1 0 3 46 35 41 .05 24 22 | -16565 720 3628 14826
gfz n/a| 0 2 -2 -24 38 20 -.04 32 25 | 0 -637 3631 12473
grg n/a| 2 -3 -4 -85 -13 -265 -.36 28 29 | -7329 1799 6989 30999
iac n/a| -4 0 0 6 -28 -20 .04 26 23 | -6451 2026 6923 30447
mcc n/a| 12 3 -40 -100 13 331 .32 150 150 | --- --- --- ---
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 3.2057.0 GPS week: 2057 Day: 0 MJD: 58643
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 | 2125 46 39 21 52 49 47 31 --- 18 | 71 69 61 58 58 63 64 --- 53
R02 | 1001 9 10 11 11 12 18 22 450 6 | 57 59 57 58 56 61 69 552 58
R03 | 1008 11 11 9 12 13 40 18 103 8 | 61 64 66 61 59 79 63 58 63
R04 | 776 6 11 11 10 21 23 17 --- 6 | 57 56 54 57 58 68 54 --- 56
R05 | 760 20 28 16 23 12 21 16 --- 8 | 49 52 54 65 52 45 49 --- 51
R07 | 1963 9 19 8 16 13 24 15 210 6 | 61 64 67 71 68 72 63 201 66
XR08 | 1658 15 21 --- 7 13 16 14 --- 6 | 57 60 --- 65 65 69 58 --- 61
R09E | 1839 13 15 16 11 26 16 14 --- 7 | 27 28 21 26 48 24 35 --- 27
R10E | 2363 12 10 20 14 15 14 18 --- 7 | 93 94 100 97 99 98 95 --- 97
R11E | 780 10 12 19 11 13 23 17 289 7 | 53 53 50 55 51 51 58 171 51
R13E | 1715 9 14 25 19 18 20 19 --- 8 | 91 91 91 92 87 100 86 --- 90
R14E | 702 15 13 22 16 13 15 21 --- 8 | 113 114 113 112 112 121 106 --- 112
R15E | 2482 16 16 21 16 17 17 22 --- 8 | 105 109 105 113 115 113 110 --- 109
R16E | 1242 29 34 22 23 38 41 26 --- 13 | 98 100 88 96 107 108 106 --- 97
R17 | 499 30 33 16 8 24 17 26 --- 9 | 59 57 39 36 52 39 24 --- 39
R18 | 1363 12 11 14 16 16 25 11 --- 7 | 39 37 34 44 33 32 38 --- 34
R19 | 757 71 74 46 56 72 46 54 --- 26 | 77 86 48 68 83 50 33 --- 41
R20 | 1395 25 34 28 41 34 58 31 --- 16 | 58 65 31 37 48 69 24 --- 36
R21 | 899 22 27 18 11 15 13 20 97 7 | 55 58 39 35 47 39 35 141 39
R22 | 681 21 17 20 14 17 18 25 --- 8 | 53 55 29 29 47 45 25 --- 35
R23 | 1240 25 23 17 29 27 24 24 --- 11 | 33 35 36 64 33 51 60 --- 43
R24 | 940 25 40 28 25 46 55 27 --- 15 | 48 64 35 59 53 51 47 --- 41
XR26 | 3275 24 70 --- --- --- 14 28 --- 17 | 32 73 --- --- --- 35 40 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1390 25 28 21 24 29 31 24 265 |T 62 67 58 63 65 64 58 224 57
WRMS | 1390 22 24 21 18 18 28 22 265 |NE 54 59 46 53 54 54 46 238 46
MEDI | 1240 16 19 19 16 17 21 21 210 |MD 57 64 54 59 56 61 58 171 51
Table 3.2057.1 GPS week: 2057 Day: 1 MJD: 58644
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 | 2334 18 23 31 40 26 49 31 --- 14 | 49 55 57 57 57 63 54 --- 51
R02 | 1045 8 13 14 19 23 20 21 361 8 | 43 46 40 49 53 43 45 293 42
R03 | 662 8 12 10 9 12 24 30 157 7 | 44 39 39 46 50 53 37 32 43
R04 | 1022 7 9 14 12 11 37 20 --- 8 | 47 47 43 49 46 67 41 --- 46
R05 | 833 16 12 13 19 22 16 9 --- 7 | 44 46 47 56 49 46 43 --- 45
R07 | 1116 9 12 13 15 17 9 14 331 5 | 50 52 51 57 58 62 53 161 54
R08 | 1656 10 15 21 29 21 20 21 --- 9 | 44 51 61 58 56 49 40 --- 48
R09E | 2694 14 15 21 11 23 11 11 --- 7 | 18 18 25 20 35 17 25 --- 19
R10E | 2471 12 12 18 9 41 32 15 --- 10 | 75 82 70 84 98 106 73 --- 81
R11E | 900 8 12 15 12 12 16 16 341 6 | 32 36 36 40 38 38 38 134 35
R13E | 911 10 13 15 16 19 19 16 --- 7 | 73 76 69 76 73 81 72 --- 73
R14E | 1339 17 13 34 23 16 27 22 --- 10 | 96 100 99 97 99 111 99 --- 98
R15E | 2410 8 12 22 14 18 25 18 --- 8 | 83 88 87 82 82 99 81 --- 84
R16E | 999 28 40 27 21 52 33 44 --- 15 | 77 77 64 66 86 83 86 --- 72
R17 | 756 25 29 21 18 13 13 26 --- 9 | 37 40 31 23 27 36 19 --- 27
R18 | 1258 11 15 20 13 18 16 17 --- 7 | 28 32 24 29 23 32 33 --- 25
R19 | 577 66 80 55 49 54 28 73 --- 25 | 56 71 51 36 46 46 38 --- 31
R20 | 908 20 43 48 32 43 59 37 --- 17 | 37 65 59 34 63 52 20 --- 36
R21 | 598 22 23 25 17 17 21 33 219 10 | 38 41 36 34 36 40 33 166 34
R22 | 984 24 25 20 20 18 20 20 --- 9 | 34 35 28 27 31 25 26 --- 27
R23 | 589 24 22 16 34 21 20 23 --- 11 | 29 30 34 44 31 33 42 --- 32
R24 | 1074 25 35 32 32 46 39 12 --- 14 | 36 45 26 47 44 47 28 --- 31
XR26 | 3722 18 42 --- --- --- 22 14 --- 13 | 27 46 --- --- --- 38 29 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1389 22 27 25 24 28 28 28 293 |T 47 52 48 50 53 55 45 157 46
WRMS | 1389 19 22 26 20 18 24 24 293 |NE 40 46 41 43 44 45 36 163 37
MEDI | 1022 16 15 20 18 19 21 20 331 |MD 44 46 43 47 49 47 40 161 42
Table 3.2057.2 GPS week: 2057 Day: 2 MJD: 58645
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 | 1755 30 24 27 31 32 45 22 --- 14 | 59 56 52 39 48 41 47 --- 43
R02 | 1300 11 12 18 12 9 22 16 206 6 | 41 42 47 52 45 46 53 173 46
R03 | 1023 9 9 10 14 7 13 8 165 4 | 47 47 48 42 39 46 51 31 44
R04 | 1170 8 10 14 12 12 17 12 --- 5 | 36 36 35 27 42 36 33 --- 32
R05 | 899 13 10 25 16 21 15 20 --- 8 | 32 37 43 36 44 42 24 --- 32
R07 | 489 9 15 11 11 11 18 17 355 6 | 42 42 47 40 42 59 53 114 45
R08 | 1830 7 9 11 9 20 25 26 --- 7 | 38 41 31 37 48 52 39 --- 40
R09E | 3267 13 20 17 11 21 13 16 --- 6 | 23 22 23 21 37 25 26 --- 23
R10E | 1921 14 16 19 8 18 31 11 --- 7 | 59 56 53 55 61 35 50 --- 51
R11E | 1041 11 13 25 7 19 9 15 314 6 | 53 55 52 50 57 46 46 58 49
R13E | 3324 9 11 17 10 21 17 12 --- 6 | 37 34 36 37 30 39 37 --- 34
R14E | 1281 14 13 23 14 16 15 11 --- 7 | 45 49 45 59 59 47 53 --- 50
R15E | 2003 8 14 33 14 20 14 18 --- 8 | 58 54 58 59 57 54 60 --- 56
R16E | 1600 26 20 30 19 34 26 27 --- 12 | 53 65 49 61 53 57 59 --- 52
R17 | 1157 20 22 23 14 23 13 33 --- 9 | 38 40 32 28 45 31 22 --- 30
R18 | 700 9 12 16 11 12 15 13 --- 5 | 29 31 23 35 29 33 36 --- 28
R19 | 539 73 67 54 50 46 61 58 --- 26 | 71 67 53 38 47 64 24 --- 33
R20 | 868 30 28 26 19 21 19 22 --- 10 | 41 37 26 35 36 25 25 --- 24
R21 | 790 28 31 23 13 23 20 29 92 10 | 64 65 62 60 71 50 51 86 58
R22 | 1269 28 29 22 18 20 22 26 --- 10 | 40 44 22 26 40 40 22 --- 27
R23 | 859 22 30 20 32 27 23 19 --- 11 | 25 25 27 48 24 25 41 --- 30
R24 | 1450 17 19 32 31 40 61 10 --- 15 | 39 47 26 47 38 41 36 --- 33
XR26 | 3446 16 39 --- --- --- 20 21 --- 13 | 24 27 --- --- --- 48 37 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1570 23 23 24 20 24 27 23 246 |T 43 44 40 42 45 42 40 92 38
WRMS | 1570 26 26 24 18 21 22 21 246 |NE 41 42 38 39 42 42 37 101 36
MEDI | 1269 14 16 22 14 20 19 18 206 |MD 41 42 43 39 44 42 39 86 34
Table 3.2057.3 GPS week: 2057 Day: 3 MJD: 58646
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 | 972 40 40 29 23 27 28 27 --- 13 | 66 67 56 40 49 44 55 --- 47
R02 | 1533 9 10 14 11 10 18 25 124 7 | 48 50 47 50 56 41 63 115 50
R03 | 996 7 16 13 9 8 17 10 150 5 | 53 58 61 56 54 45 56 30 53
R04 | 1508 10 12 11 11 8 17 11 --- 5 | 47 41 50 50 43 38 46 --- 44
R05 | 936 21 20 22 18 21 16 16 --- 8 | 35 35 34 38 35 29 34 --- 30
R07 | 720 10 12 22 17 10 18 15 317 7 | 48 48 55 59 53 59 50 55 52
R08 | 1176 23 23 12 10 25 22 8 --- 8 | 42 41 44 44 55 71 51 --- 50
R09E | 4520 15 17 18 10 23 12 18 --- 7 | 19 20 24 25 35 22 24 --- 22
XR10E | 1215 11 16 --- 12 23 12 25 --- 8 | 39 39 --- 39 38 30 36 --- 35
R11E | 1099 9 7 24 10 17 16 23 184 7 | 46 48 60 53 44 51 33 66 46
R13E | 3209 10 11 18 12 15 16 17 --- 6 | 28 29 23 35 26 32 38 --- 29
R14E | 1230 14 14 19 15 17 10 16 --- 7 | 68 72 64 70 60 73 75 --- 67
R15E | 1684 11 9 22 10 19 16 20 --- 7 | 36 33 31 34 39 31 37 --- 33
R16E | 1873 29 40 35 25 38 17 23 --- 12 | 42 45 43 48 47 37 53 --- 39
R17 | 1658 21 20 23 14 18 18 24 --- 9 | 50 49 43 35 43 39 30 --- 37
R18 | 664 11 15 19 14 16 13 13 --- 6 | 31 33 31 45 38 36 38 --- 35
R19 | 629 75 75 48 40 44 44 57 --- 23 | 84 84 33 30 68 49 29 --- 37
R20 | 660 24 35 26 24 25 23 23 --- 11 | 35 49 28 40 38 31 30 --- 27
R21 | 652 34 35 23 13 18 24 20 50 10 | 55 56 30 39 46 43 35 65 37
R22 | 914 30 34 23 19 18 29 27 --- 11 | 47 49 25 31 43 45 29 --- 31
R23 | 916 24 31 20 37 34 12 20 --- 12 | 31 38 29 59 29 31 48 --- 36
R24 | 2348 20 30 24 31 43 57 10 --- 15 | 40 54 40 52 43 58 47 --- 43
XR26 | 2771 16 37 --- --- --- 25 13 --- 13 | 25 56 --- --- --- 30 32 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1701 26 29 23 20 24 24 23 187 |T 44 47 40 44 44 41 42 66 39
WRMS | 1701 23 25 23 20 20 19 20 187 |NE 46 50 40 44 46 43 42 66 39
MEDI | 1176 16 20 22 14 18 17 20 150 |MD 42 48 40 40 43 39 38 65 37
Table 3.2057.4 GPS week: 2057 Day: 4 MJD: 58647
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 | 769 40 38 32 24 17 49 30 --- 15 | 60 61 63 35 45 32 57 --- 44
R02 | 1898 15 13 9 5 16 8 17 170 5 | 38 43 53 46 49 52 44 132 46
R03 | 1027 11 12 8 18 13 18 20 132 6 | 50 48 48 62 59 49 43 40 50
R04 | 2256 7 11 10 10 9 18 12 --- 5 | 39 44 44 48 46 38 41 --- 41
R05 | 848 17 17 18 24 27 16 14 --- 9 | 38 37 44 44 38 42 35 --- 35
R07 | 745 8 9 11 12 12 13 17 304 5 | 45 43 47 50 40 42 38 89 42
R08 | 794 13 15 11 16 19 19 20 --- 7 | 39 40 40 51 49 53 41 --- 45
R09E | 4129 12 12 16 12 18 16 21 --- 7 | 22 22 16 26 34 26 29 --- 22
R10E | 1228 13 16 23 12 21 16 14 --- 7 | 44 48 47 46 46 41 40 --- 42
R11E | 1393 8 10 13 14 18 12 27 157 7 | 53 51 46 50 49 51 53 77 48
R13E | 3228 11 21 20 13 18 17 16 --- 7 | 43 53 44 46 45 47 44 --- 43
R14E | 1429 8 15 17 10 19 14 14 --- 6 | 55 59 58 55 72 62 54 --- 58
R15E | 692 16 11 20 12 21 16 16 --- 7 | 49 55 58 54 56 61 56 --- 54
R16E | 1763 24 33 24 25 38 23 20 --- 11 | 55 57 53 52 65 56 49 --- 50
R17 | 1484 22 24 20 16 12 18 19 --- 8 | 43 46 34 29 32 32 25 --- 31
R18 | 659 14 12 15 21 18 21 17 --- 8 | 31 29 33 37 32 34 35 --- 31
R19 | 577 63 67 58 56 63 29 59 --- 25 | 69 78 47 34 56 48 20 --- 35
R20 | 846 34 40 32 29 37 41 34 --- 15 | 44 48 30 36 52 31 33 --- 27
R21 | 794 26 26 20 21 20 14 34 60 10 | 78 78 75 81 81 67 62 121 72
R22 | 823 22 23 21 16 37 14 32 --- 11 | 39 39 20 21 54 24 27 --- 27
R23 | 1315 19 19 18 29 16 25 24 --- 10 | 31 31 22 45 33 19 42 --- 29
R24 | 1284 27 40 29 44 38 75 22 --- 19 | 35 40 32 50 40 79 43 --- 40
XR26 | 2240 14 50 --- --- --- 25 20 --- 14 | 24 54 --- --- --- 37 32 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1612 23 26 23 23 26 27 25 183 |T 44 48 43 45 48 44 41 91 40
WRMS | 1612 20 21 23 19 17 21 22 183 |NE 43 47 42 44 47 42 38 95 38
MEDI | 1228 15 17 18 16 18 18 20 157 |MD 43 48 44 46 46 42 41 89 42
Table 3.2057.5 GPS week: 2057 Day: 5 MJD: 58648
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 | 1140 27 39 28 29 40 55 32 --- 15 | 45 57 57 55 66 36 44 --- 43
R02 | 2122 10 11 20 14 13 12 19 234 6 | 33 32 46 30 33 43 40 163 34
R03 | 696 10 13 9 8 13 11 12 93 4 | 38 42 40 45 39 40 39 43 39
R04 | 1325 14 12 13 8 16 18 10 --- 6 | 34 31 33 28 23 27 31 --- 27
R05 | 1045 11 13 24 9 26 22 10 --- 8 | 32 33 39 34 47 27 39 --- 32
R07 | 905 5 15 8 6 16 11 16 273 4 | 39 44 39 35 35 47 42 145 38
R08 | 1106 12 14 11 13 18 12 19 --- 6 | 36 39 29 46 50 41 40 --- 40
R09E | 3816 13 14 19 12 25 15 14 --- 7 | 22 24 18 29 39 31 28 --- 25
R10E | 2171 13 15 20 15 21 20 13 --- 7 | 68 71 72 72 72 68 76 --- 70
R11E | 822 7 8 13 14 20 18 22 102 7 | 40 41 38 47 43 36 41 98 39
R13E | 2096 7 15 15 9 23 21 10 --- 6 | 59 53 60 57 59 59 55 --- 57
R14E | 1328 12 13 19 10 11 23 24 --- 7 | 60 57 57 57 60 67 61 --- 58
R15E | 776 11 13 22 17 29 16 20 --- 8 | 70 72 69 79 85 75 70 --- 72
R16E | 1180 10 22 26 21 42 30 25 --- 11 | 60 62 68 68 82 74 70 --- 65
R17 | 619 29 31 24 19 21 18 30 --- 11 | 43 44 24 23 38 34 18 --- 27
R18 | 656 18 18 14 22 13 16 9 --- 7 | 30 33 29 35 29 33 28 --- 29
R19 | 591 48 46 49 48 82 52 63 --- 25 | 61 70 54 45 86 62 25 --- 47
R20 | 676 31 48 55 21 26 45 30 --- 16 | 38 56 47 37 42 34 22 --- 28
R21 | 576 28 31 26 22 16 16 30 74 11 | 55 57 48 37 52 49 40 43 44
R22 | 530 25 28 23 24 28 28 31 --- 11 | 40 44 22 20 43 42 20 --- 27
R23 | 1761 11 20 13 32 32 35 32 --- 12 | 19 25 17 30 22 26 31 --- 17
R24 | 1278 23 22 30 26 53 67 27 --- 17 | 30 51 45 43 60 60 37 --- 36
XR26 | 3335 15 67 --- --- --- 19 20 --- 12 | 30 82 --- --- --- 29 40 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1450 20 24 25 21 31 30 25 175 |T 42 48 43 43 50 45 40 98 40
WRMS | 1450 17 21 25 21 20 26 23 175 |NE 37 46 37 36 44 39 33 98 33
MEDI | 1106 13 15 20 15 21 19 20 102 |MD 39 44 40 37 43 41 40 98 38
Table 3.2057.6 GPS week: 2057 Day: 6 MJD: 58649
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 | 986 41 38 30 35 36 24 20 --- 14 | 71 76 72 48 61 61 59 --- 58
R02 | 1958 14 15 15 8 15 21 15 167 6 | 56 57 61 58 59 67 64 85 59
R03 | 530 7 13 11 9 18 26 16 85 6 | 63 58 66 63 59 77 61 44 63
R04 | 803 6 10 14 6 17 10 15 --- 5 | 55 55 54 54 47 55 52 --- 52
R05 | 740 24 21 13 27 28 31 14 --- 10 | 54 54 61 72 71 47 64 --- 57
R07 | 856 11 11 12 14 12 20 14 252 6 | 61 61 59 64 56 60 58 128 58
R08 | 1550 15 14 15 19 18 18 21 --- 8 | 54 55 45 71 66 65 64 --- 61
R09E | 3369 12 14 21 11 30 10 9 --- 7 | 24 24 23 28 46 26 30 --- 27
R10E | 1290 13 17 14 19 13 16 10 --- 6 | 95 92 93 100 92 96 101 --- 95
R11E | 1337 8 10 23 14 16 18 13 86 7 | 67 69 64 63 64 69 66 65 64
R13E | 2276 11 13 13 11 23 14 8 --- 6 | 82 88 82 82 80 91 83 --- 82
R14E | 952 10 10 28 15 20 21 15 --- 8 | 82 82 80 87 93 98 82 --- 85
R15E | 1001 9 17 25 18 32 17 19 --- 9 | 110 115 107 116 121 117 110 --- 112
R16E | 1011 15 19 25 18 43 27 26 --- 11 | 92 93 90 96 92 98 93 --- 91
R17 | 587 24 30 23 21 28 25 32 --- 11 | 60 62 33 34 62 56 25 --- 42
R18 | 867 10 17 14 14 11 16 16 --- 6 | 44 43 34 46 47 47 39 --- 41
R19 | 715 57 56 51 50 85 54 61 --- 26 | 92 96 41 44 95 61 28 --- 48
R20 | 1022 27 24 41 45 28 50 48 --- 18 | 61 55 35 47 57 58 43 --- 40
R21 | 1268 27 29 20 14 20 17 33 74 10 | 68 68 47 45 59 51 40 71 50
R22 | 599 26 31 28 23 20 43 36 --- 13 | 58 62 28 29 59 69 26 --- 41
R23 | 960 25 17 20 38 26 20 27 --- 12 | 27 24 25 55 24 22 50 --- 31
R24 | 895 15 31 33 29 59 49 24 --- 16 | 35 49 33 57 53 65 48 --- 42
XR26 | 3208 18 79 --- --- --- 24 18 --- 14 | 40 79 --- --- --- 51 49 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1326 22 24 24 24 32 28 26 149 |T 63 65 56 61 66 65 58 78 58
WRMS | 1326 21 22 24 22 25 29 23 149 |NE 56 59 46 52 58 57 48 82 49
MEDI | 986 15 17 20 18 20 21 18 86 |MD 61 62 54 57 59 61 58 71 57
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