[IGSREPORT-26630] Wk 2055 IGLOS Final Orbits
acc
acc at igs.org
Sun Jun 16 05:16:14 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2055 (May 26, 2019 - Jun 01, 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 2.2055.
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:
igl2055[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2055 in the SP3 format.
igl20557.sum Combination Report for GPS Week 2055.
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 | 1.1 ns
1 | 1.4 ns
2 | 2.5 ns
3 | 0.7 ns
4 | 0.8 ns
5 | 2.9 ns
6 | 1.6 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 1.2055, 1a.2055).
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 2.2055.0-6)
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 3.2055.0-6).
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 2055 summary. (May 26, 2019 - Jun 01, 2019)
Table 1.2055.a GPS week : 2055 MJD: 58629.0-58635.0
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 1 17 -18 3 .18 22 18 | 14598 -556 3365 11830
| 0 1 1 24 17 16 .09 | 640 1499
cof n/a| 0 0 0 16 3 -5 .16 25 20 | 14589 -554 3365 11843
| 1 1 3 21 23 19 .15 | 659 1503
emx n/a| 0 0 5 13 -27 99 .03 23 23 | 1544 -95 3214 11357
| 1 0 2 18 27 26 .08 | 964 1024
esx n/a| 0 0 0 16 16 -15 .07 21 16 | -3480 336 3302 14121
| 0 0 1 15 14 15 .09 | 16975 1608
gfz n/a| 1 0 0 11 3 -13 -.01 28 19 | 0 -586 3306 12122
| 1 1 2 27 18 23 .16 | 0 1495
grg n/a| 2 0 -6 -66 22 -57 -.27 26 20 | 1407 -784 4255 14558
| 1 1 3 20 28 37 .15 | 2273 1476
iac n/a| -3 0 0 -6 -3 -32 -.04 23 21 | 2261 -657 4290 14717
| 2 2 0 16 23 29 .05 | 2387 1217
mcc n/a| 0 -2 -14 -8 19 51 .18 215 215 | --- --- --- ---
| 8 14 24 120 169 454 .63 | --- ---
Table 1.2055.b GPS week : 2055 MJD: 58629.0-58635.0
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 16 17 19 19 19 18 |
R02 | 7 7 6 7 8 9 7 |
R03 | 7 6 6 7 6 6 7 |
R04 | 8 5 6 4 6 6 7 |
R05 | 9 11 10 11 12 12 15 |
R07 | 6 5 7 6 5 6 7 |
R08 | 7 9 9 9 10 7 8 |
R09 | 6 7 6 8 8 13 14 |
R10 | 8 9 6 8 10 8 7 |
R11 | 6 6 7 7 6 7 7 |
R13 | 9 8 8 7 8 10 10 |
R14 | 7 7 8 7 8 10 8 |
R15 | 9 10 8 9 9 9 9 |
R16 | 15 14 14 13 14 15 16 |
R17 | 8 9 9 7 9 10 13 |
R18 | 6 6 5 6 6 7 9 |
R19 | 19 21 19 21 20 22 23 |
R20 | 13 14 14 14 14 14 13 |
R21 | 9 9 8 11 10 8 10 |
R22 | 9 9 10 10 10 8 10 |
R23 | 9 9 8 9 10 10 12 |
R24 | 13 18 12 13 14 15 16 |
R26 | 19 13 17 16 15 13 19 |
Table 1.2055.c GPS week : 2055 MJD: 58629.0-58635.0
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 2055 0 | 54 -56 136 -37 799 1620 85.4 1417 1417 | 1063 0
brd 2055 1 | -13 -72 153 -83 967 -827 83.8 1366 1366 | 1394 0
brd 2055 2 | 21 -34 168 296 1100 874 82.8 1471 1471 | 2485 0
brd 2055 3 | 21 60 158 -180 1251 2211 83.3 1257 1257 | 746 0
brd 2055 4 | 11 24 221 -307 -643 4329 81.6 1390 1390 | 816 0
brd 2055 5 | 21 0 213 -120 -722 4546 82.9 1594 1594 | 2909 0
brd 2055 6 | 10 30 242 475 -3226 3482 82.4 1404 1404 | 1634 0
-------------+------------------------------------------------------------+----------------
brd 2055 mean| 18 -6 184 5 -67 2319 83.2 1414 1414 | 1578 0
brd 2055 sdev| 20 48 40 277 1615 1950 1.2 102 102 | 833 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 2.2055.0 GPS week: 2055 Day: 0 MJD: 58629
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 2 3 -11 20 .08 20 17 | 15222 -1328 2922 11084
cof n/a| 0 -1 1 -3 1 15 .26 21 19 | 15229 -1332 2921 11090
emx n/a| 0 0 5 3 -11 62 .01 23 23 | 1030 -861 2929 10945
esx n/a| -1 -1 -2 18 10 -14 .12 19 14 | -16712 709 2925 13652
gfz n/a| 2 0 2 19 -4 -50 .19 28 23 | 0 -709 2933 11540
grg n/a| 0 -1 -8 -45 27 5 -.30 22 18 | -3180 -1783 4332 25628
iac n/a| -1 2 0 4 -38 -9 -.09 19 19 | -2175 -1436 4259 24755
mcc n/a| 0 0 3 93 -59 -412 .27 258 258 | --- --- --- ---
Table 2.2055.1 GPS week: 2055 Day: 1 MJD: 58630
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 2 0 -30 11 .07 21 15 | 15608 -1450 3352 11426
cof n/a| 0 -1 0 0 -7 -2 .14 24 18 | 15626 -1481 3355 11443
emx n/a| -1 1 5 28 -62 94 -.04 26 26 | 1442 -685 3375 11262
esx n/a| 0 0 -1 28 19 -7 .14 17 16 | 27357 -780 3354 13537
gfz n/a| 0 0 0 37 11 15 .10 30 18 | 0 -1188 3351 11885
grg n/a| 3 0 -5 -95 72 -82 -.26 27 18 | 1435 -1120 3942 10921
iac n/a| 0 -1 0 -10 -17 -31 -.11 22 20 | 1441 -473 4184 11223
mcc n/a| 14 5 1 9 -7 -217 .50 279 279 | --- --- --- ---
Table 2.2055.2 GPS week: 2055 Day: 2 MJD: 58631
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 11 -25 -25 .21 21 16 | 14467 2013 3261 12430
cof n/a| 0 -2 1 33 -10 -16 .18 25 18 | 14452 2022 3262 12436
emx n/a| 1 0 4 -5 -70 81 -.04 22 22 | 1811 1828 3224 12120
esx n/a| 0 1 -1 37 7 -5 .10 22 16 | -1163 2703 3228 14800
gfz n/a| 1 1 -2 49 33 -15 -.09 24 16 | 0 1650 3226 12749
grg n/a| 3 -1 -1 -69 39 -50 -.21 21 15 | 4215 1712 4341 17152
iac n/a| -4 0 0 -16 18 -22 -.02 21 19 | 5668 799 4357 17917
mcc n/a| 0 14 17 114 123 28 1.12 176 176 | --- --- --- ---
Table 2.2055.3 GPS week: 2055 Day: 3 MJD: 58632
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 10 -12 -12 .19 21 16 | 14783 -1463 2949 11392
cof n/a| -2 0 0 14 46 -36 .21 25 21 | 14784 -1480 2951 11415
emx n/a| 1 1 3 19 -19 93 .00 24 24 | 769 -1088 2795 11471
esx n/a| -1 0 1 10 4 -11 -.04 20 16 | -23990 635 2782 13514
gfz n/a| 0 1 0 9 -14 -4 .05 27 19 | 0 -1597 2783 11923
grg n/a| 3 1 -4 -76 28 -35 -.21 23 18 | 1416 -1428 3386 10965
iac n/a| -2 -3 0 2 17 -29 -.05 24 22 | 2131 -512 3386 11121
mcc n/a| -4 15 -37 -8 -250 618 -.62 226 226 | --- --- --- ---
Table 2.2055.4 GPS week: 2055 Day: 4 MJD: 58633
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 12 12 12 .14 22 19 | 13855 -1913 3665 12677
cof n/a| 0 0 -6 -2 16 -16 -.02 27 21 | 13818 -1873 3662 12692
emx n/a| 0 1 1 44 -12 143 -.01 26 26 | 253 -170 2944 10984
esx n/a| 0 0 1 25 8 -10 -.00 20 14 | -14016 -2205 3585 15259
gfz n/a| 2 0 0 -1 -18 10 .08 26 17 | 0 -2513 3577 12864
grg n/a| 1 -1 -3 -48 1 -44 -.11 29 22 | 2563 -2460 4661 13077
iac n/a| -3 0 1 -37 14 -93 -.04 23 21 | 3660 -2336 4682 13665
mcc n/a| 0 -19 -32 -27 107 -317 -.64 189 189 | --- --- --- ---
Table 2.2055.5 GPS week: 2055 Day: 5 MJD: 58634
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 2 72 -21 8 .30 24 18 | 14090 1100 3578 11771
cof n/a| 0 0 -2 18 -27 2 -.02 25 19 | 14051 1114 3571 11779
emx n/a| 0 0 6 -5 -8 101 .09 21 21 | 2613 677 3514 11524
esx n/a| 0 0 -1 0 15 -50 -.02 24 17 | 3528 1595 3539 14390
gfz n/a| 0 0 3 -33 1 -15 -.27 33 20 | 0 1195 3554 12217
grg n/a| 5 0 -10 -46 -12 -91 -.22 28 22 | 2239 755 4751 11902
iac n/a| -4 4 1 10 9 0 .02 23 21 | 2766 915 4768 12008
mcc n/a| 6 -10 -10 15 281 -80 .43 257 257 | --- --- --- ---
Table 2.2055.6 GPS week: 2055 Day: 6 MJD: 58635
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 2 2 11 -41 7 .27 27 22 | 14164 -851 3832 12035
cof n/a| -2 2 3 55 4 17 .40 30 24 | 14164 -848 3838 12050
emx n/a| 0 1 9 9 -3 117 .19 23 23 | 2895 -369 3717 11198
esx n/a| 0 -1 0 -7 47 -12 .18 23 16 | 630 -300 3707 13698
gfz n/a| 3 0 -3 3 18 -30 -.12 28 20 | 0 -943 3719 11682
grg n/a| 2 -3 -9 -85 1 -100 -.57 32 26 | 1164 -1167 4374 12265
iac n/a| -5 0 0 0 -26 -36 .02 26 23 | 2342 -1561 4400 12335
mcc n/a| -13 -20 -46 -254 -57 742 .21 118 118 | --- --- --- ---
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 3.2055.0 GPS week: 2055 Day: 0 MJD: 58629
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 | 644 29 27 35 21 46 24 21 --- 13 | 62 63 57 38 63 38 48 --- 43
R02 | 1002 16 12 22 16 9 16 14 388 7 | 79 82 81 68 79 69 74 84 73
R03 | 627 14 14 16 10 10 15 22 172 7 | 56 57 56 58 63 64 54 50 58
R04 | 1052 9 11 15 10 31 13 18 --- 7 | 53 53 52 52 50 51 58 --- 51
R05 | 674 22 16 21 23 27 12 10 --- 8 | 53 61 56 71 73 61 63 --- 60
R07 | 1325 11 17 12 17 14 11 15 318 6 | 48 46 52 59 55 52 51 106 52
R08 | 1416 9 14 16 12 23 7 21 --- 6 | 45 47 47 49 55 45 36 --- 44
R09 | 3495 12 17 11 11 19 16 10 --- 6 | 142 144 145 152 152 140 151 --- 147
R10 | 959 10 15 26 16 15 26 11 --- 8 | 73 72 58 79 68 66 74 --- 69
R11 | 795 7 7 17 6 15 18 13 196 5 | 83 82 80 83 80 88 85 132 83
R13 | 1447 15 23 18 19 28 15 19 --- 8 | 82 82 80 84 74 87 84 --- 81
R14 | 684 19 18 16 13 13 11 12 --- 6 | 61 66 53 67 62 53 65 --- 59
R15 | 2041 22 31 20 9 16 19 29 --- 9 | 70 75 46 50 60 63 45 --- 54
R16 | 1107 30 26 24 40 36 47 19 --- 15 | 68 89 67 97 81 72 65 --- 71
R17E | 1479 13 16 21 13 24 16 18 --- 7 | 76 76 69 70 77 72 77 --- 72
R18E | 830 8 13 19 11 15 12 12 --- 5 | 39 38 42 40 35 36 38 --- 37
R19E | 1596 42 35 40 38 64 44 33 --- 19 | 49 47 38 35 67 49 40 --- 33
R20E | 2014 32 33 28 21 34 25 33 --- 13 | 105 102 102 117 105 103 111 --- 105
R21E | 866 16 16 27 11 24 12 22 117 8 | 73 76 72 73 80 75 75 75 73
R22E | 829 14 15 21 18 23 18 21 --- 8 | 150 150 151 163 158 140 154 --- 152
R23E | 1877 20 23 18 22 28 22 12 --- 9 | 90 92 92 95 89 94 90 --- 91
R24E | 921 18 23 35 20 45 38 16 --- 13 | 45 50 44 49 61 58 45 --- 46
XR26E | 5912 17 34 --- --- --- 35 27 --- 19 | 38 48 --- --- --- 59 40 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1416 20 21 23 19 28 22 19 258 |T 71 73 70 74 76 71 70 89 69
WRMS | 1416 17 19 23 14 23 18 19 258 |NE 69 72 66 71 72 67 68 93 67
MEDI | 1052 16 17 20 16 23 16 18 196 |MD 68 72 57 68 68 64 65 84 60
Table 3.2055.1 GPS week: 2055 Day: 1 MJD: 58630
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 | 744 35 29 39 31 55 35 22 --- 16 | 40 40 37 35 65 26 20 --- 26
R02 | 1118 8 15 19 13 15 14 17 --- 6 | 64 71 70 57 68 52 61 --- 60
R03 | 451 10 11 12 9 10 9 20 215 5 | 34 31 32 37 38 38 38 41 35
R04 | 741 9 14 7 9 13 10 15 --- 4 | 34 36 33 38 35 35 37 --- 33
R05 | 946 17 14 20 26 38 18 27 --- 11 | 35 37 36 44 55 52 55 --- 41
R07 | 550 6 9 15 9 10 13 12 476 4 | 30 32 30 29 28 31 30 204 28
R08 | 1554 14 13 25 18 16 14 30 --- 9 | 27 32 28 32 28 29 21 --- 24
R09 | 2901 16 15 14 16 21 11 15 --- 7 | 86 88 92 99 93 81 94 --- 91
R10 | 2225 7 16 23 9 33 26 13 --- 8 | 47 47 43 48 59 61 38 --- 47
R11 | 702 9 13 18 10 11 19 11 154 6 | 59 63 59 60 57 68 62 145 60
R13 | 1125 17 19 25 15 20 14 18 --- 8 | 56 60 56 63 60 57 60 --- 58
R14 | 645 18 21 17 9 9 17 12 --- 6 | 47 47 38 42 35 28 40 --- 37
R15 | 2050 20 21 26 12 20 19 27 --- 9 | 46 45 36 37 47 35 34 --- 37
R16 | 822 37 50 28 14 35 50 17 --- 14 | 66 79 52 53 67 57 55 --- 54
R17E | 1971 17 16 22 15 20 14 23 --- 8 | 71 67 68 68 75 61 75 --- 68
R18E | 881 9 12 16 14 10 15 12 --- 5 | 29 34 32 36 34 35 36 --- 32
R19E | 1113 45 59 50 27 67 36 51 --- 20 | 42 52 46 42 83 62 42 --- 39
R20E | 1274 24 27 40 24 36 31 28 --- 13 | 95 99 97 89 95 99 83 --- 89
R21E | 697 19 26 22 16 18 12 24 124 8 | 62 65 67 64 65 61 59 54 61
R22E | 782 16 17 22 13 32 20 20 --- 9 | 143 144 142 139 143 149 138 --- 141
R23E | 1841 22 20 18 24 16 21 15 --- 9 | 76 74 81 75 82 81 77 --- 77
R24E | 1554 20 22 38 21 52 76 20 --- 18 | 24 31 30 34 49 82 29 --- 31
XR26E | 3833 18 82 --- --- --- 19 15 --- 12 | 32 60 --- --- --- 36 30 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1365 21 24 26 17 30 27 22 279 |T 54 58 54 55 61 57 52 111 52
WRMS | 1365 15 18 26 16 18 18 20 279 |NE 47 50 45 48 52 46 46 130 45
MEDI | 1113 17 17 22 14 20 18 18 154 |MD 47 52 43 44 59 57 42 54 41
Table 3.2055.2 GPS week: 2055 Day: 2 MJD: 58631
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 | 615 32 35 26 48 29 50 34 --- 17 | 48 57 42 68 61 31 57 --- 43
R02 | 1227 16 17 16 11 9 11 15 --- 6 | 64 63 64 77 69 80 76 --- 71
R03 | 510 9 9 11 16 13 9 16 243 5 | 41 43 44 53 38 46 37 76 42
R04 | 854 10 13 11 14 18 9 17 --- 6 | 39 41 40 34 33 39 41 --- 36
R05 | 1236 18 21 18 34 21 17 15 --- 9 | 38 41 37 43 32 40 41 --- 34
R07 | 887 8 15 12 22 12 15 20 --- 7 | 39 38 40 48 44 36 30 --- 37
R08 | 1025 21 18 19 14 28 10 20 --- 8 | 30 31 40 34 49 34 32 --- 33
R09 | 2430 14 19 14 10 17 9 15 --- 6 | 159 158 157 161 159 160 169 --- 161
R10 | 3045 5 12 18 9 17 17 8 --- 6 | 41 48 30 43 51 46 35 --- 40
R11 | 613 8 13 19 8 20 14 15 146 6 | 50 56 46 50 63 61 50 159 52
R13 | 1374 14 19 23 11 24 18 15 --- 8 | 41 45 34 41 49 47 48 --- 42
R14 | 682 18 23 14 22 9 19 12 --- 7 | 43 47 29 40 30 20 29 --- 29
R15 | 1811 22 19 18 12 18 10 19 --- 7 | 46 41 26 34 44 31 36 --- 34
R16 | 644 37 53 32 22 38 35 23 --- 14 | 52 64 39 44 36 38 38 --- 34
R17E | 2117 14 16 22 21 18 11 25 --- 8 | 61 64 72 75 70 61 54 --- 63
R18E | 734 8 11 14 11 10 7 12 --- 4 | 24 25 30 29 31 22 27 --- 25
R19E | 1674 49 55 42 39 56 31 36 --- 19 | 33 42 41 42 63 34 45 --- 31
R20E | 913 29 26 35 35 38 23 30 --- 14 | 113 112 107 102 104 117 101 --- 105
R21E | 1178 23 18 21 14 17 17 12 115 8 | 50 50 46 46 54 52 43 60 47
R22E | 1137 21 23 24 16 19 22 22 --- 9 | 100 99 104 94 92 98 107 --- 98
R23E | 2565 20 23 16 18 19 18 16 --- 8 | 51 55 50 59 51 53 52 --- 51
R24E | 1362 13 21 29 29 28 33 29 --- 12 | 44 50 41 49 69 52 44 --- 44
XR26E | 3468 19 61 --- --- --- 25 27 --- 17 | 19 67 --- --- --- 27 28 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS | 1471 21 25 22 22 24 21 21 176 |T 53 58 52 57 58 53 53 98 51
WRMS | 1471 16 18 22 16 16 15 19 176 |NE 52 55 47 55 54 50 51 117 49
MEDI | 1178 18 19 18 16 18 17 17 146 |MD 44 50 41 46 51 46 43 76 42
Table 3.2055.3 GPS week: 2055 Day: 3 MJD: 58632
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 | 1053 44 48 34 45 24 55 35 --- 18 | 47 69 44 65 55 46 45 --- 41
R02 | 1344 11 18 14 10 17 22 18 378 7 | 44 50 51 52 54 52 44 164 47
R03 | 490 11 18 15 10 11 15 23 203 6 | 44 46 50 53 52 56 37 33 47
R04 | 1027 7 11 9 8 14 9 10 --- 4 | 37 43 42 38 45 38 35 --- 37
R05 | 831 25 28 26 33 22 15 19 --- 11 | 38 43 40 39 42 37 28 --- 31
R07 | 644 10 18 9 6 21 10 21 124 6 | 41 44 45 46 35 41 53 318 42
R08 | 1565 17 12 20 18 33 10 21 --- 9 | 32 37 36 47 45 41 43 --- 36
R09 | 2175 15 16 16 16 19 24 18 --- 8 | 113 116 112 122 118 121 114 --- 116
R10 | 1060 8 11 18 15 22 23 11 --- 7 | 43 45 42 52 41 43 42 --- 43
R11 | 1360 11 14 15 16 12 16 18 222 6 | 40 44 38 37 36 35 35 154 36
R13 | 1544 11 16 19 12 16 24 12 --- 7 | 44 49 38 47 42 60 42 --- 44
R14 | 745 15 16 20 8 13 13 16 --- 6 | 54 53 46 44 44 39 42 --- 44
R15 | 1563 24 34 19 15 15 17 27 --- 9 | 55 64 34 35 43 47 30 --- 39
R16 | 757 25 33 33 25 43 25 16 --- 12 | 58 68 31 46 41 49 39 --- 37
R17E | 1163 17 20 21 12 18 9 18 --- 7 | 87 87 85 91 92 82 85 --- 86
R18E | 771 11 15 18 12 15 10 13 --- 6 | 21 25 28 28 26 25 26 --- 23
R19E | 771 43 53 45 35 77 29 46 --- 21 | 43 51 48 42 76 41 43 --- 33
R20E | 1503 27 32 34 25 26 37 37 --- 14 | 99 108 112 115 116 102 106 --- 106
R21E | 1496 23 23 27 14 24 14 34 81 10 | 41 46 39 31 48 38 32 64 34
R22E | 1739 25 24 29 13 25 21 24 --- 10 | 153 153 143 151 158 151 151 --- 150
R23E | 1657 18 19 20 21 22 17 15 --- 8 | 45 41 36 44 43 49 42 --- 40
R24E | 699 18 25 37 30 26 39 26 --- 13 | 41 55 36 48 41 58 37 --- 38
XR26E | 3839 24 31 --- --- --- 24 16 --- 15 | 23 40 --- --- --- 31 32 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1256 21 25 24 20 27 23 23 226 |T 54 59 53 57 58 55 51 146 51
WRMS | 1256 16 21 24 16 19 18 22 226 |NE 49 55 46 51 49 50 44 167 45
MEDI | 1163 17 19 20 15 21 17 18 203 |MD 44 49 42 46 44 46 42 154 40
Table 3.2055.4 GPS week: 2055 Day: 4 MJD: 58633
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 | 876 50 42 48 42 40 37 32 --- 19 | 35 65 62 58 53 43 32 --- 38
R02 | 1500 16 21 19 18 21 17 15 --- 8 | 57 62 54 57 57 57 61 --- 55
R03 | 547 8 16 13 9 7 18 18 158 5 | 37 36 41 44 40 50 34 31 40
R04 | 600 5 10 10 6 11 21 21 --- 6 | 38 38 39 40 40 55 30 --- 38
R05 | 805 29 27 22 29 34 15 20 --- 11 | 39 46 47 73 63 45 46 --- 49
R07 | 715 9 11 13 8 11 9 17 234 5 | 36 38 40 34 35 43 39 81 36
R08 | 2284 15 18 22 12 33 23 24 --- 10 | 30 29 28 37 50 53 25 --- 33
R09 | 1995 15 15 16 10 15 28 17 --- 7 | 113 115 116 122 119 125 117 --- 118
XR10 | 1949 16 22 --- 18 27 17 12 --- 9 | 42 42 --- 42 24 21 40 --- 33
R11 | 1498 12 17 16 10 10 13 18 210 6 | 58 62 47 56 54 47 50 121 51
R13 | 2296 17 19 19 19 21 20 15 --- 8 | 51 50 40 48 48 52 44 --- 45
R14 | 1050 15 20 20 11 15 21 17 --- 7 | 46 51 37 42 46 27 40 --- 38
R15 | 1078 28 30 19 20 9 21 17 --- 9 | 54 60 32 35 38 48 39 --- 38
R16 | 559 15 41 49 18 31 47 23 --- 14 | 49 81 49 54 81 74 46 --- 51
R17E | 2126 24 37 22 17 19 16 17 --- 8 | 56 62 54 52 55 50 51 --- 51
R18E | 745 12 16 20 16 9 14 7 --- 6 | 23 23 21 24 21 25 23 --- 21
R19E | 691 40 48 38 36 57 52 49 --- 20 | 33 47 27 49 63 48 41 --- 30
R20E | 1868 24 33 36 23 32 42 30 --- 14 | 94 101 105 99 95 98 102 --- 95
R21E | 1069 19 25 23 19 19 24 25 134 9 | 67 68 60 63 71 68 67 35 64
R22E | 1726 24 28 26 14 22 13 25 --- 9 | 93 92 85 91 96 86 87 --- 89
R23E | 1042 17 20 21 22 15 33 16 --- 9 | 69 64 65 69 55 60 64 --- 62
R24E | 1481 19 34 23 19 39 58 26 --- 14 | 36 55 41 36 47 35 36 --- 30
XR26E | 3934 22 26 --- --- --- 22 18 --- 15 | 28 33 --- --- --- 38 24 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1390 22 27 26 20 26 29 23 189 |T 51 57 51 55 56 54 49 67 49
WRMS | 1390 19 21 26 14 17 22 21 189 |NE 48 55 48 53 53 52 45 77 47
MEDI | 1078 17 22 21 18 19 21 18 158 |MD 46 55 47 49 53 50 41 35 40
Table 3.2055.5 GPS week: 2055 Day: 5 MJD: 58634
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 | 627 44 38 27 51 60 27 36 --- 18 | 26 52 27 71 76 51 40 --- 37
R02 | 1141 18 15 17 24 26 18 14 --- 8 | 45 40 46 37 45 39 38 --- 38
R03 | 829 7 11 10 11 16 12 17 129 5 | 31 32 31 27 36 28 28 26 28
R04 | 612 13 12 12 12 17 13 13 --- 6 | 37 35 32 26 22 24 34 --- 28
R05 | 866 27 17 12 30 42 16 23 --- 11 | 39 46 54 77 79 50 49 --- 53
R07 | 656 10 12 14 13 18 14 13 457 6 | 28 26 30 29 41 23 28 179 27
R08 | 2580 14 15 15 20 15 18 13 --- 7 | 22 23 26 39 45 21 41 --- 29
R09 | 2329 18 27 21 19 23 57 26 --- 13 | 400 404 407 401 396 381 404 --- 398
R10 | 4133 11 16 14 19 28 16 15 --- 7 | 31 35 33 42 34 28 33 --- 30
R11 | 1612 8 15 18 9 19 17 12 177 6 | 49 56 44 52 53 49 50 95 48
R13 | 1410 12 14 19 15 32 37 13 --- 10 | 53 49 53 59 60 72 54 --- 55
R14 | 1327 19 19 15 25 20 18 28 --- 9 | 41 41 32 51 50 29 34 --- 35
R15 | 1159 23 31 21 15 17 19 22 --- 9 | 45 51 32 34 38 39 36 --- 34
R16 | 515 30 31 28 24 38 56 23 --- 15 | 36 39 42 34 55 71 47 --- 39
R17E | 2949 32 23 20 16 18 16 20 --- 9 | 77 75 70 73 79 68 73 --- 72
R18E | 719 14 16 16 19 11 18 12 --- 7 | 36 37 41 38 37 31 38 --- 35
R19E | 645 50 57 38 43 88 25 42 --- 22 | 35 52 34 44 93 44 35 --- 34
R20E | 1247 24 21 30 28 33 40 32 --- 14 | 60 60 66 59 74 73 66 --- 61
R21E | 1044 20 14 21 10 17 15 24 90 8 | 72 74 69 66 68 67 70 56 67
R22E | 1052 23 30 20 9 17 14 23 --- 8 | 114 113 115 118 112 111 113 --- 113
R23E | 679 20 22 20 25 23 23 27 --- 10 | 95 103 97 99 97 101 83 --- 94
R24E | 967 23 31 23 29 43 55 25 --- 15 | 49 59 44 55 58 65 55 --- 47
XR26E | 3269 16 36 --- --- --- 21 17 --- 13 | 24 41 --- --- --- 26 33 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1593 23 25 21 24 33 28 23 257 |T 62 67 64 69 74 64 64 89 61
WRMS | 1593 18 19 21 17 20 22 21 257 |NE 63 66 63 69 73 64 65 100 62
MEDI | 1052 19 19 19 19 20 18 22 129 |MD 41 49 42 51 55 49 41 56 38
Table 3.2055.6 GPS week: 2055 Day: 6 MJD: 58635
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 | 550 46 53 19 44 52 42 26 --- 18 | 48 60 51 59 71 60 44 --- 44
R02 | 1482 17 23 11 17 21 13 17 --- 7 | 62 67 59 53 63 55 61 --- 57
R03 | 895 11 18 15 8 19 13 20 133 6 | 50 57 48 49 58 55 41 29 48
R04 | 764 12 18 18 14 16 20 18 --- 7 | 54 59 49 45 46 45 44 --- 46
R05 | 971 30 20 26 39 38 31 25 --- 14 | 50 58 64 94 86 57 66 --- 66
R07 | 904 9 12 11 4 9 20 27 --- 6 | 48 48 53 51 49 45 62 --- 50
R08 | 1812 9 7 19 17 12 31 13 --- 7 | 35 36 40 46 41 40 39 --- 38
R09 | 1461 42 22 29 23 30 25 37 --- 14 | 379 387 385 395 390 375 384 --- 384
R10 | 2771 15 14 18 11 16 14 12 --- 6 | 42 45 32 51 51 40 46 --- 43
R11 | 1254 9 10 20 7 18 28 13 143 7 | 55 57 45 55 61 69 53 97 54
R13 | 1213 8 10 19 11 21 47 10 --- 9 | 69 68 62 72 63 96 74 --- 70
R14 | 1539 15 18 15 14 16 33 11 --- 8 | 52 54 34 47 38 51 45 --- 41
R15 | 1308 20 21 19 9 15 21 29 --- 8 | 60 62 42 42 52 49 36 --- 44
R16 | 649 25 40 28 25 48 54 39 --- 16 | 90 105 79 90 90 105 65 --- 81
R17E | 3453 33 26 33 18 36 26 26 --- 13 | 76 79 67 78 83 81 79 --- 74
R18E | 859 18 9 20 14 17 28 21 --- 8 | 50 54 56 50 48 56 53 --- 50
R19E | 676 67 70 36 46 50 42 52 --- 22 | 52 58 43 62 61 43 61 --- 43
R20E | 795 17 43 24 26 31 47 25 --- 12 | 65 71 67 63 77 71 70 --- 64
R21E | 786 24 33 25 11 19 24 29 60 10 | 87 90 82 91 92 85 102 89 88
R22E | 1030 20 23 22 11 23 29 28 --- 10 | 92 93 91 91 89 92 93 --- 89
R23E | 958 30 30 24 28 19 30 23 --- 11 | 169 172 154 173 166 159 174 --- 165
R24E | 851 38 44 34 31 37 43 35 --- 16 | 121 131 116 105 112 112 107 --- 108
XR26E | 5515 24 31 --- --- --- 31 27 --- 19 | 32 27 --- --- --- 39 29 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS | 1404 27 30 23 23 28 32 26 118 |T 79 84 78 84 85 81 79 71 76
WRMS | 1404 22 24 23 16 20 26 23 118 |NE 78 83 74 82 82 81 75 63 76
MEDI | 971 20 22 20 14 19 29 25 133 |MD 55 60 56 59 63 57 61 89 54
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