[IGSREPORT-26644] Wk 2056 IGLOS Final Orbits
acc
acc at igs.org
Sun Jun 23 00:16:36 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2056 (Jun 02, 2019 - Jun 08, 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 2.2056.
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:
igl2056[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2056 in the SP3 format.
igl20567.sum Combination Report for GPS Week 2056.
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 | 1.7 ns
1 | 0.7 ns
2 | 0.9 ns
3 | 1.5 ns
4 | 1.7 ns
5 | 1.3 ns
6 | 2.4 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 1.2056, 1a.2056).
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 2.2056.0-6)
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 3.2056.0-6).
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 2056 summary. (Jun 02, 2019 - Jun 08, 2019)
Table 1.2056.a GPS week : 2056 MJD: 58636.0-58642.0
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 22 -35 11 .19 24 20 | 14512 -45 3204 11948
| 1 1 2 15 15 15 .05 | 826 1885
cof n/a| 0 0 -1 16 -9 13 .12 27 22 | 14491 -32 3204 11955
| 0 1 0 18 18 26 .12 | 826 1892
emx n/a| 0 0 6 -12 -21 61 .10 23 23 | 903 -61 3201 11533
| 1 1 3 6 13 31 .08 | 642 1192
esx n/a| 0 0 0 25 25 -9 .02 23 19 | 3460 320 3204 14581
| 0 1 1 17 19 19 .05 | 12611 1564
gfz n/a| 0 0 -4 24 28 -3 -.01 32 21 | 0 -117 3204 12417
| 1 1 2 23 25 24 .08 | 0 1978
grg n/a| 1 -1 -2 -69 43 -81 -.32 28 24 | 1410 2 3201 11452
| 1 2 7 20 8 60 .12 | 654 1874
iac n/a| -2 0 0 -6 -14 -11 -.07 25 23 | 2354 -478 3205 11761
| 1 2 0 26 28 33 .04 | 1128 1194
mcc n/a| -2 10 -23 -33 -1 385 -.55 212 212 | --- --- --- ---
| 4 13 11 201 99 558 .52 | --- ---
Table 1.2056.b GPS week : 2056 MJD: 58636.0-58642.0
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 | 16 17 19 21 18 18 14 |
R02 | 8 7 7 9 8 8 7 |
R03 | 9 6 7 8 8 6 8 |
R04 | 7 9 7 6 6 7 8 |
R05 | 14 12 10 9 14 11 9 |
R07 | 6 7 5 8 7 6 7 |
R08 | 10 7 10 9 8 9 6 |
R09 | 11 8 7 8 9 8 9 |
R10 | 10 11 11 7 8 8 7 |
R11 | 8 7 7 7 6 8 6 |
R13 | 9 9 7 10 8 8 8 |
R14 | 10 8 8 8 8 8 6 |
R15 | 10 11 9 8 10 10 9 |
R16 | 16 12 14 14 12 11 17 |
R17 | 12 10 9 8 10 11 9 |
R18 | 7 7 6 7 7 6 8 |
R19 | 24 26 21 25 26 24 28 |
R20 | 20 14 11 13 13 15 14 |
R21 | 11 9 9 9 10 10 9 |
R22 | 10 10 10 10 10 10 12 |
R23 | 14 12 12 12 15 13 10 |
R24 | 18 15 17 16 16 18 16 |
R26 | 27 20 21 14 13 17 18 |
Table 1.2056.c GPS week : 2056 MJD: 58636.0-58642.0
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 2056 0 | -23 20 187 -429 -879 1469 81.5 1128 1128 | 1720 0
brd 2056 1 | 51 -29 247 -232 -832 -742 81.9 1332 1332 | 677 0
brd 2056 2 | -19 71 353 -2120 -123 793 81.6 1523 1523 | 904 0
brd 2056 3 | 59 68 247 572 644 1273 82.4 1641 1641 | 1533 0
brd 2056 4 | 5 0 225 2092 133 -524 83.4 >>>>> >>>>> | 1725 0
brd 2056 5 | -2 -45 228 519 -59 -1235 82.8 58110 58110 | 1344 0
brd 2056 6 | 22 -40 145 199 403 -1111 83.0 1505 1505 | 2429 0
-------------+------------------------------------------------------------+----------------
brd 2056 mean| 13 6 233 85 -101 -11 82.4 29605 29605 | 1476 0
brd 2056 sdev| 32 49 64 1271 578 1154 .7 53875 53875 | 579 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 2.2056.0 GPS week: 2056 Day: 0 MJD: 58636
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 4 37 -23 -5 .28 25 17 | 14569 146 3233 11948
cof n/a| 1 0 0 9 -7 -9 .33 31 21 | 14569 142 3230 11956
emx n/a| 2 0 11 -3 -36 80 .17 26 24 | 1844 406 3238 11920
esx n/a| 0 0 -3 4 40 -27 .01 25 21 | -4482 617 3227 14734
gfz n/a| 0 0 -1 0 35 -2 .03 27 20 | 0 154 3224 12458
grg n/a| 0 0 -16 -77 31 -168 -.56 34 30 | 1618 174 3242 11584
iac n/a| -6 4 0 19 -2 12 -.08 31 27 | 2961 -359 3236 11735
mcc n/a| -9 32 -14 -72 -136 199 -.99 146 146 | --- --- --- ---
Table 2.2056.1 GPS week: 2056 Day: 1 MJD: 58637
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 -1 13 -54 24 .17 25 21 | 14738 -1784 3582 11276
cof n/a| 0 0 0 1 -31 30 .17 26 20 | 14721 -1774 3581 11285
emx n/a| 0 1 7 -24 -11 68 .11 22 22 | 1249 -999 3581 11275
esx n/a| 0 0 0 27 4 -18 .09 20 20 | 15413 -1431 3576 13852
gfz n/a| -1 -2 -3 1 38 -6 .01 30 19 | 0 -2668 3577 11710
grg n/a| 1 -3 -4 -61 41 -111 -.39 28 28 | 1522 -1963 3567 10696
iac n/a| -2 1 0 15 10 5 -.11 28 24 | 2825 -2354 3574 11051
mcc n/a| -1 3 -45 301 47 -363 -.23 279 279 | --- --- --- ---
Table 2.2056.2 GPS week: 2056 Day: 2 MJD: 58638
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 1 18 -51 31 .20 23 20 | 12782 456 3048 13696
cof n/a| 0 0 -2 6 -17 31 .06 25 20 | 12758 473 3046 13709
emx n/a| 0 1 11 -12 -9 61 -.03 21 21 | 177 -111 2984 10702
esx n/a| 0 3 0 19 22 0 .07 24 20 | 20235 640 3042 15917
gfz n/a| 0 0 -2 53 54 27 .12 26 17 | 0 1210 3052 13900
grg n/a| -1 -4 -6 -76 59 -115 -.25 25 20 | 457 817 3041 13304
iac n/a| -2 0 0 -10 -45 -5 -.07 25 23 | -40 735 3046 13403
mcc n/a| 0 -4 -19 -103 -15 6 .06 240 240 | --- --- --- ---
Table 2.2056.3 GPS week: 2056 Day: 3 MJD: 58639
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 12 -44 -7 .18 25 22 | 14835 -366 3122 11298
cof n/a| 0 -1 0 0 8 -1 .19 27 26 | 14817 -373 3125 11306
emx n/a| 0 -1 5 -7 -1 110 .14 23 23 | 907 -535 3135 11294
esx n/a| 0 1 0 37 22 15 -.06 22 18 | 10829 182 3133 14086
gfz n/a| 1 1 -1 47 43 -1 -.09 36 25 | 0 -532 3128 11895
grg n/a| 1 -3 -6 -51 43 -98 -.23 26 21 | 1602 -250 3130 10844
iac n/a| 0 0 0 -59 -48 -47 -.04 25 24 | 2329 29 3126 11090
mcc n/a| -3 0 -14 -250 -122 714 -.42 155 155 | --- --- --- ---
Table 2.2056.4 GPS week: 2056 Day: 4 MJD: 58640
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 -2 45 -14 20 .15 23 21 | 14390 -596 2802 12473
cof n/a| 1 0 0 10 -31 -1 -.02 26 23 | 14356 -564 2804 12477
emx n/a| 0 3 3 -10 -36 56 .21 24 24 | 1320 -28 2813 12518
esx n/a| -1 0 -1 11 -1 -38 -.01 22 18 | -15650 -533 2807 15299
gfz n/a| 0 0 -6 0 -21 -51 .02 37 21 | 0 -762 2807 13073
grg n/a| 0 1 6 -43 37 -53 -.26 28 24 | 1821 -421 2801 11985
iac n/a| -1 -4 1 6 30 34 -.12 25 23 | 2298 -176 2810 12314
mcc n/a| 4 20 -25 82 77 212 -.28 262 262 | --- --- --- ---
Table 2.2056.5 GPS week: 2056 Day: 5 MJD: 58641
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 27 -26 17 .17 23 21 | 14859 -1893 2859 10803
cof n/a| 0 -1 -1 41 -3 56 .09 24 22 | 14847 -1886 2856 10809
emx n/a| 0 0 1 -14 -25 48 .02 25 25 | 794 -1418 2856 10887
esx n/a| 0 1 0 25 43 11 .03 23 18 | 745 -668 2856 13528
gfz n/a| -1 0 -6 41 8 -7 -.13 32 23 | 0 -1618 2862 11314
grg n/a| 1 -1 4 -104 40 -39 -.30 27 23 | 2264 -1899 2849 10186
iac n/a| -2 0 -1 -7 -25 -58 .01 23 21 | 2651 -1871 2852 10722
mcc n/a| -2 18 -27 74 133 564 -1.46 203 203 | --- --- --- ---
Table 2.2056.6 GPS week: 2056 Day: 6 MJD: 58642
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 1 -30 0 .14 25 21 | 15411 3722 3787 12147
cof n/a| 1 -2 -2 44 17 -12 .05 27 22 | 15375 3753 3791 12147
emx n/a| 1 0 6 -12 -26 8 .13 20 20 | 30 2254 3805 12141
esx n/a| 1 0 1 55 48 -7 .03 24 21 | -2870 3437 3793 14654
gfz n/a| 0 1 -7 25 38 15 -.05 37 20 | 0 3392 3781 12569
grg n/a| 3 0 1 -72 48 15 -.27 26 23 | 590 3561 3779 11567
iac n/a| -3 -1 -1 -8 -20 -23 -.09 21 19 | 3459 647 3793 12017
mcc n/a| -3 3 -16 -263 3 1367 -.51 200 200 | --- --- --- ---
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 3.2056.0 GPS week: 2056 Day: 0 MJD: 58636
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 | 564 31 23 36 35 43 32 26 --- 15 | 116 122 100 132 139 112 116 --- 116
R02 | 1267 16 33 10 21 23 18 20 --- 8 | 55 59 54 64 64 58 58 --- 56
R03E | 915 8 11 10 15 25 18 32 143 8 | 48 45 50 51 58 50 42 33 47
R04E | 609 16 14 15 18 10 13 17 --- 7 | 43 41 47 34 40 43 38 --- 39
R05 | 815 28 23 23 34 33 29 37 --- 14 | 37 58 53 78 77 60 40 --- 53
R07 | 1111 15 16 8 12 12 9 21 --- 6 | 42 42 44 48 49 49 57 --- 46
R08E | 1035 10 18 15 33 11 34 20 --- 9 | 33 46 34 51 35 40 38 --- 36
R09E | 1427 31 27 19 20 14 25 27 --- 10 | 52 44 46 36 43 47 44 --- 40
R10E | 1789 15 12 20 13 17 43 15 --- 9 | 79 83 80 79 81 76 73 --- 76
R11E | 1250 7 11 20 13 14 23 26 172 7 | 67 74 70 74 72 75 60 173 69
R13E | 760 14 15 24 16 23 22 17 --- 8 | 79 84 84 77 78 78 78 --- 78
R14E | 1146 13 12 20 24 14 32 25 --- 9 | 103 110 108 118 112 99 105 --- 107
R15E | 882 24 21 21 13 17 30 31 --- 10 | 111 112 99 109 115 108 109 --- 107
R16E | 760 28 35 26 24 37 40 51 --- 15 | 59 62 60 55 55 55 76 --- 54
R17 | 1265 28 25 26 20 23 37 32 --- 12 | 72 64 44 39 62 66 31 --- 49
R18E | 805 9 13 13 17 13 20 16 --- 6 | 46 47 38 52 44 37 48 --- 43
R19E | 605 60 93 57 50 46 65 43 --- 24 | 110 146 56 89 134 122 81 --- 86
R20E | 1502 29 55 40 35 55 37 68 --- 20 | 116 158 138 134 146 145 85 --- 123
R21 | 730 25 17 22 17 19 26 31 116 10 | 116 113 103 106 110 115 103 105 107
R22 | 1182 21 22 25 16 13 32 27 --- 10 | 49 53 31 28 47 58 31 --- 37
R23 | 1586 29 25 19 32 33 44 21 --- 13 | 33 38 35 73 34 76 64 --- 47
R24 | 1577 32 36 43 37 40 65 21 --- 18 | 62 65 54 69 55 79 58 --- 55
XR26E | ---- 31 50 --- --- --- 28 52 --- 27 | 34 50 --- --- --- 31 65 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1127 25 31 26 25 27 34 31 146 |T 67 74 64 72 75 73 65 103 65
WRMS | 1127 17 21 24 21 20 30 27 146 |NE 58 61 52 63 62 70 55 105 56
MEDI | 1035 24 22 20 20 19 30 26 143 |MD 59 62 54 69 62 66 60 105 54
Table 3.2056.1 GPS week: 2056 Day: 1 MJD: 58637
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 | 595 35 32 24 39 48 50 17 --- 16 | 96 101 86 100 98 84 78 --- 86
R02 | 1586 16 15 12 14 27 15 13 457 7 | 39 40 44 41 60 43 52 383 43
R03E | 548 9 13 7 8 18 19 22 82 6 | 28 31 31 34 45 38 30 28 32
R04E | 869 11 9 14 19 29 23 23 --- 9 | 26 30 27 30 35 39 34 --- 26
R05 | 578 26 32 19 23 35 25 33 --- 12 | 27 63 38 58 66 51 27 --- 40
R07 | 613 7 11 18 12 13 14 21 396 6 | 30 34 38 34 32 41 46 245 33
R08E | 1084 10 10 13 14 21 12 19 --- 6 | 23 27 30 28 28 31 25 --- 24
R09E | 2784 17 18 21 11 16 16 18 --- 7 | 33 35 39 40 38 35 34 --- 33
R10E | 1788 23 28 18 16 22 34 33 --- 11 | 87 89 87 87 89 81 71 --- 81
R11E | 1957 11 20 20 11 19 22 11 108 7 | 31 28 36 31 33 25 30 138 28
R13E | 1490 10 10 17 16 25 23 20 --- 8 | 39 38 38 35 45 42 36 --- 36
R14E | 1113 20 20 20 15 17 19 13 --- 8 | 64 62 61 59 54 58 57 --- 57
R15E | 621 30 31 24 13 23 25 29 --- 11 | 80 79 83 79 83 87 72 --- 78
R16E | 986 29 30 20 21 33 33 29 --- 12 | 43 56 44 48 59 38 52 --- 42
R17 | 1365 20 20 22 12 19 30 32 --- 10 | 42 42 37 33 42 51 30 --- 35
R18E | 634 7 10 13 16 21 19 14 --- 7 | 38 35 36 42 35 35 38 --- 35
R19E | 553 65 64 49 38 80 51 69 --- 26 | 64 68 44 53 83 88 47 --- 50
R20E | 1453 25 30 27 23 25 35 45 --- 13 | 76 73 72 83 76 75 75 --- 71
R21 | 1062 28 27 18 11 16 16 24 67 8 | 103 99 97 98 92 98 103 68 98
R22 | 689 24 26 23 18 19 27 20 --- 10 | 33 35 29 27 35 34 31 --- 27
R23 | 2176 32 26 22 31 22 23 25 --- 12 | 30 31 22 44 33 35 46 --- 32
R24 | 1606 28 25 26 29 43 42 27 --- 14 | 46 46 30 50 58 50 39 --- 38
XR26E | ---- 24 77 --- --- --- 19 37 --- 19 | 24 79 --- --- --- 30 33 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1331 25 26 22 20 30 28 28 279 |T 47 53 47 51 55 51 47 172 45
WRMS | 1331 21 20 22 20 19 28 24 279 |NE 43 48 41 48 52 50 46 232 43
MEDI | 1062 23 25 20 16 22 23 23 108 |MD 39 42 38 42 45 42 39 138 36
Table 3.2056.2 GPS week: 2056 Day: 2 MJD: 58638
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 | 582 45 30 20 51 47 43 36 --- 18 | 54 59 50 62 69 38 50 --- 45
R02 | 1578 8 14 12 10 8 26 20 404 6 | 28 26 31 31 30 27 37 363 27
R03E | 527 12 19 9 8 18 25 11 60 6 | 34 33 32 33 38 30 31 27 29
R04E | 918 6 10 11 20 21 13 17 --- 6 | 28 28 30 26 42 32 30 --- 28
R05 | 756 18 15 18 31 21 8 22 --- 9 | 26 29 30 50 43 38 28 --- 31
R07 | 728 9 28 8 11 11 8 17 298 5 | 30 39 35 41 39 31 29 157 32
R08E | 1252 15 13 20 27 27 11 28 --- 10 | 21 22 26 46 37 27 23 --- 24
R09E | 4088 13 16 13 15 16 12 17 --- 6 | 18 21 22 22 31 23 20 --- 19
XR10E | 3893 13 15 --- 15 24 25 29 --- 11 | 54 55 --- 59 54 66 56 --- 54
R11E | 1911 8 17 15 15 15 18 23 163 7 | 26 26 25 33 24 26 24 117 24
R13E | 1597 12 13 15 13 13 17 19 --- 6 | 32 34 33 32 33 37 30 --- 31
R14E | 1422 19 13 18 23 11 16 19 --- 8 | 49 44 41 44 44 49 51 --- 43
R15E | 671 16 11 25 13 24 16 15 --- 8 | 48 46 44 42 48 45 41 --- 42
R16E | 1401 35 50 28 23 38 29 31 --- 14 | 54 59 54 66 84 53 62 --- 56
R17 | 1832 21 21 19 13 14 15 28 --- 8 | 50 48 37 35 43 40 37 --- 39
R18E | 718 7 11 13 17 11 12 12 --- 5 | 37 39 33 48 39 36 38 --- 37
R19E | 685 60 52 52 34 37 34 56 --- 21 | 92 86 52 49 66 72 33 --- 55
R20E | 1294 18 37 19 21 31 30 28 --- 11 | 52 69 40 54 45 47 60 --- 45
R21 | 798 26 27 16 16 16 19 17 74 8 | 108 108 104 114 113 108 105 73 107
R22 | 864 24 23 23 24 23 18 21 --- 10 | 38 39 21 22 35 36 23 --- 26
R23 | 2083 21 16 25 36 30 16 29 --- 12 | 25 32 27 59 31 36 55 --- 35
R24 | 1726 17 21 18 34 48 65 20 --- 16 | 47 58 37 43 41 71 50 --- 43
XR26E | ---- 31 53 --- --- --- 35 13 --- 20 | 42 64 --- --- --- 83 38 --- 52
------+---------------------------------------------------+-----------------------------------------------
RMS | 1523 23 25 21 24 26 25 25 240 |T 43 46 38 45 46 45 41 147 40
WRMS | 1523 20 20 21 20 17 20 23 240 |NE 44 47 40 49 46 48 45 197 42
MEDI | 1252 17 17 18 17 21 18 20 163 |MD 38 39 33 43 41 38 37 117 37
Table 3.2056.3 GPS week: 2056 Day: 3 MJD: 58639
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 | 776 47 39 45 46 57 38 47 --- 20 | 63 72 80 67 84 37 67 --- 55
R02 | 1354 17 21 15 16 25 16 24 --- 8 | 35 40 48 38 55 52 55 --- 43
R03E | 622 11 18 12 12 21 27 17 72 7 | 42 48 51 40 51 51 43 32 43
R04E | 723 7 17 9 11 23 20 10 --- 6 | 39 36 39 36 42 41 37 --- 36
R05 | 832 25 24 18 23 24 17 13 --- 9 | 37 45 35 56 52 49 41 --- 40
R07 | 738 14 12 19 11 24 16 24 270 8 | 41 42 46 50 54 38 44 291 42
R08E | 913 9 17 13 8 47 13 26 --- 9 | 31 40 34 34 62 26 30 --- 31
R09E | 4476 15 14 18 14 23 12 23 --- 7 | 35 31 31 35 37 36 29 --- 31
R10E | 3052 11 13 20 7 20 16 16 --- 6 | 70 70 82 71 73 71 75 --- 71
R11E | 1366 10 15 19 9 18 19 21 123 7 | 25 34 23 30 35 32 27 97 26
R13E | 1409 11 13 23 14 23 32 24 --- 9 | 28 31 36 31 41 56 29 --- 32
R14E | 1548 14 17 19 14 17 21 21 --- 8 | 48 54 52 56 53 36 34 --- 45
R15E | 648 15 13 20 11 21 11 23 --- 7 | 105 104 110 103 113 107 97 --- 105
R16E | 1683 24 33 30 24 56 30 17 --- 13 | 42 53 44 50 62 33 45 --- 38
R17 | 1789 25 20 18 16 12 13 16 --- 8 | 57 56 45 46 55 54 34 --- 46
R18E | 678 9 11 16 21 11 16 9 --- 6 | 44 49 41 55 43 39 43 --- 43
R19E | 669 69 72 45 43 90 34 55 --- 25 | 92 97 42 33 91 53 21 --- 45
R20E | 893 25 18 30 24 39 41 16 --- 13 | 57 48 44 43 66 50 38 --- 43
R21 | 598 31 36 19 9 19 16 23 55 9 | 76 79 74 68 73 67 58 63 67
R22 | 767 27 31 23 15 25 17 22 --- 9 | 43 45 28 30 45 26 28 --- 29
R23 | 1669 22 36 17 33 35 25 26 --- 12 | 30 27 27 54 25 23 47 --- 33
R24 | 2513 27 34 27 33 44 58 21 --- 16 | 50 55 36 58 46 84 54 --- 51
XR26E | ---- 21 56 --- --- --- 18 17 --- 13 | 65 93 --- --- --- 43 58 --- 53
------+---------------------------------------------------+-----------------------------------------------
RMS | 1641 25 27 23 22 36 26 25 155 |T 50 54 47 49 57 48 44 120 45
WRMS | 1641 22 26 23 18 25 21 24 155 |NE 46 48 42 50 50 49 45 177 43
MEDI | 893 17 18 19 14 23 18 21 72 |MD 43 48 42 46 53 43 43 63 43
Table 3.2056.4 GPS week: 2056 Day: 4 MJD: 58640
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 | 1045 37 40 44 26 57 45 31 --- 17 | 55 74 76 66 96 45 62 --- 60
R02 | 618 15 15 15 6 13 23 25 326 7 | 25 30 35 31 28 49 46 293 32
R03E | 632 13 18 12 13 19 27 23 129 8 | 34 37 36 42 30 58 29 41 36
R04E | 708 9 11 13 13 13 19 15 --- 6 | 29 34 26 42 36 32 35 --- 31
R05 | 652 24 21 18 24 65 21 24 --- 13 | 33 39 38 40 77 32 46 --- 35
R07 | 784 11 13 14 13 18 13 19 407 6 | 38 40 38 38 31 48 42 269 37
R08E | 919 9 12 21 13 23 16 21 --- 7 | 32 37 33 38 48 45 48 --- 37
R09E |>>>>> 19 15 24 15 23 11 19 --- 8 | 31 37 35 34 43 28 32 --- 30
R10E | 1487 12 9 27 13 20 23 10 --- 8 | 66 67 70 66 70 64 68 --- 65
R11E | 1221 11 12 18 8 20 9 17 203 6 | 26 28 26 25 28 16 18 142 21
R13E | 2054 12 20 21 9 17 20 19 --- 7 | 32 34 37 31 36 33 30 --- 30
R14E | 833 12 11 16 16 28 17 23 --- 8 | 35 37 36 47 54 29 29 --- 35
R15E | 834 14 17 25 13 33 28 16 --- 9 | 105 111 96 102 107 116 103 --- 103
R16E | 1711 18 18 28 24 32 37 17 --- 11 | 56 58 51 56 64 47 52 --- 50
R17 | 988 23 26 24 18 18 20 22 --- 9 | 51 53 33 36 48 49 30 --- 39
R18E | 1084 12 15 10 18 13 15 18 --- 6 | 61 56 58 64 64 53 63 --- 59
R19E | 807 52 60 47 50 109 34 57 --- 26 | 84 92 48 51 127 60 31 --- 57
R20E | 1479 20 34 27 25 33 42 25 --- 12 | 48 65 36 51 61 59 28 --- 42
R21 | 1143 32 33 23 15 16 13 28 110 10 | 109 109 98 104 101 98 94 93 100
R22 | 825 30 30 21 8 21 19 25 --- 9 | 45 44 22 29 37 25 23 --- 27
R23 | 1111 30 29 20 39 33 39 30 --- 14 | 28 38 27 52 29 24 43 --- 28
R24 | 2177 24 36 20 36 40 59 27 --- 16 | 36 63 48 58 61 58 47 --- 46
XR26E | ---- 16 73 --- --- --- 21 18 --- 13 | 48 95 --- --- --- 35 58 --- 45
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 23 26 24 22 37 28 25 261 |T 48 55 45 50 58 47 45 167 45
WRMS |>>>>> 21 23 24 18 21 24 23 261 |NE 45 52 42 48 51 47 46 218 43
MEDI | 988 16 18 21 15 21 21 22 203 |MD 38 44 36 42 48 47 43 142 37
Table 3.2056.5 GPS week: 2056 Day: 5 MJD: 58641
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 | 949 41 35 42 41 52 26 28 --- 17 | 35 44 53 53 65 43 36 --- 39
R02 | 751 15 17 18 15 20 25 13 134 8 | 21 21 30 29 28 21 23 137 20
R03E | 665 9 15 9 13 22 15 14 156 6 | 25 26 32 18 34 31 32 29 24
R04E | 897 9 11 12 13 25 22 11 --- 7 | 26 25 27 26 21 47 27 --- 26
R05 | 555 21 20 25 24 21 28 28 --- 11 | 27 38 30 57 50 31 49 --- 36
R07 | 1140 9 9 15 12 10 14 16 270 5 | 27 29 22 29 26 33 31 105 25
R08E | 911 19 18 26 16 18 20 21 --- 9 | 22 25 21 43 46 52 47 --- 35
R09E | 3962 14 12 16 14 24 16 14 --- 7 | 42 40 40 44 42 45 32 --- 38
R10E | 1932 16 15 20 17 24 15 15 --- 8 | 117 118 124 118 122 110 116 --- 117
R11E | 1129 7 7 24 14 17 27 11 237 7 | 28 28 29 33 38 32 27 168 28
R13E | 1114 16 17 20 8 24 26 12 --- 8 | 53 55 55 51 56 62 50 --- 53
R14E | 791 17 17 27 16 21 10 17 --- 8 | 60 56 58 65 64 58 60 --- 59
R15E | 1587 14 19 21 12 37 29 17 --- 10 | 64 67 65 63 75 62 61 --- 62
R16E | 759 13 20 33 15 32 28 25 --- 11 | 77 83 73 80 74 70 80 --- 73
R17 | 614 28 33 23 17 29 15 24 --- 10 | 48 49 37 37 51 35 36 --- 37
R18E | 692 15 17 14 18 11 15 6 --- 6 | 98 99 97 92 101 101 94 --- 96
R19E | 999 54 54 45 54 74 39 47 --- 23 | 67 70 43 52 82 50 35 --- 46
R20E | 1605 29 29 32 28 39 39 30 --- 14 | 58 54 43 48 48 48 38 --- 40
R21 |>>>>> 27 27 23 12 18 18 31 185 10 | 58 57 40 48 43 48 42 80 44
R22 | 781 26 28 22 11 23 16 30 --- 10 | 38 38 23 28 39 29 18 --- 26
R23 | 823 19 20 16 35 22 45 25 --- 12 | 30 33 23 42 24 37 34 --- 25
R24 | 1594 21 36 34 33 51 59 35 --- 17 | 31 36 53 48 39 33 50 --- 32
XR26E | ---- 23 71 --- --- --- 25 22 --- 16 | 65 59 --- --- --- 65 57 --- 60
------+---------------------------------------------------+-----------------------------------------------
RMS |58114 23 24 25 23 32 27 23 203 |T 48 50 46 50 53 49 46 103 45
WRMS |58114 20 22 25 18 23 23 21 203 |NE 35 37 32 39 37 33 35 107 30
MEDI | 911 17 19 22 15 23 25 21 185 |MD 42 44 40 48 46 47 38 105 38
Table 3.2056.6 GPS week: 2056 Day: 6 MJD: 58642
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 | 1880 38 32 26 29 52 18 11 --- 13 | 74 78 75 69 66 59 68 --- 64
R02 | 1151 12 11 16 15 16 18 19 230 7 | 40 44 44 42 41 43 49 303 40
R03E | 594 15 15 14 17 11 23 16 153 7 | 48 48 58 56 53 60 47 32 52
R04E | 792 11 14 14 22 25 15 13 --- 7 | 47 46 45 36 45 46 43 --- 41
R05 | 783 21 26 12 16 17 25 19 --- 8 | 47 50 51 53 57 59 62 --- 51
R07 | 2472 7 10 15 12 20 21 11 157 6 | 55 53 57 56 59 57 49 168 54
R08E | 779 14 14 17 12 10 16 13 --- 6 | 42 45 54 56 54 58 48 --- 50
R09E | 2719 14 15 17 18 27 19 27 --- 9 | 43 42 43 49 54 49 38 --- 43
R10E | 2863 9 12 17 15 16 23 14 --- 7 | 138 138 140 135 140 132 135 --- 137
R11E | 1011 9 12 17 12 11 12 9 286 5 | 31 30 33 40 36 31 36 184 33
R13E | 1659 7 16 19 15 17 27 12 --- 7 | 66 68 61 66 72 58 65 --- 63
R14E | 879 11 15 13 13 13 12 15 --- 6 | 69 73 68 67 71 65 69 --- 67
R15E | 2234 16 17 22 10 30 21 19 --- 8 | 148 148 140 139 148 145 138 --- 142
R16E | 1217 29 45 21 28 86 33 24 --- 17 | 77 77 81 74 106 65 84 --- 73
R17 | 504 31 34 18 10 19 13 19 --- 9 | 66 69 37 43 60 49 36 --- 45
R18E | 974 11 17 15 18 16 25 12 --- 7 | 75 80 74 81 79 75 76 --- 76
R19E | 771 78 79 40 61 95 48 44 --- 27 | 93 99 43 65 108 56 36 --- 50
R20E | 1832 22 23 22 37 27 47 21 --- 13 | 77 79 62 59 72 85 56 --- 65
R21 | 1285 22 18 18 16 19 19 26 134 9 | 79 79 60 69 75 65 70 102 68
R22 | 655 23 30 27 15 31 26 29 --- 11 | 54 59 28 30 56 47 25 --- 36
R23 | 1447 24 24 17 31 18 18 20 --- 10 | 34 41 34 61 30 36 51 --- 38
R24 | 857 19 27 28 38 59 41 29 --- 16 | 43 56 45 70 51 57 62 --- 49
XR26E | ---- 27 39 --- --- --- 17 28 --- 17 | 104 123 --- --- --- 109 109 --- 105
------+---------------------------------------------------+-----------------------------------------------
RMS | 1505 25 27 20 24 37 26 21 200 |T 67 70 60 64 69 65 63 157 62
WRMS | 1505 21 22 20 21 20 23 19 200 |NE 52 56 44 53 53 51 50 191 47
MEDI | 1011 16 17 17 16 19 21 19 157 |MD 66 68 54 59 59 58 56 168 52
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