[IGSREPORT-26592] Wk 2052 IGLOS Final Orbits
acc
acc at igs.org
Sat May 25 03:19:14 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2052 (May 05, 2019 - May 11, 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 2.2052.
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:
igl2052[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2052 in the SP3 format.
igl20527.sum Combination Report for GPS Week 2052.
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 | -3.8 ns
1 | -2.1 ns
2 | -2.5 ns
3 | -2.1 ns
4 | -0.2 ns
5 | -1.7 ns
6 | -2.9 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 1.2052, 1a.2052).
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 2.2052.0-6)
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 3.2052.0-6).
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 2052 summary. (May 05, 2019 - May 11, 2019)
Table 1.2052.a GPS week : 2052 MJD: 58608.0-58614.0
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 -1 3 25 -6 6 .08 22 19 | 12419 -520 3180 9457
| 1 0 2 16 22 13 .02 | 915 1732
cof n/a| 1 0 2 27 -2 -1 .08 23 20 | 12410 -510 3181 9459
| 1 1 2 23 27 26 .06 | 913 1719
emx n/a| 0 0 2 17 -60 54 .02 23 23 | -8802 -155 3183 9310
| 1 1 1 18 18 38 .05 | 9279 1241
esx n/a| -1 0 -2 15 -9 -16 .17 20 15 | -252 -113 3185 11349
| 0 0 1 15 10 13 .04 | 16657 1776
gfz n/a| 0 0 -1 1 23 -24 .09 25 18 | 0 -649 3188 9256
| 0 0 2 17 13 39 .04 | 0 1562
grg n/a| 2 0 -1 -75 50 -73 -.34 22 19 | -1811 -735 3186 8758
| 0 1 4 22 20 77 .04 | 496 1802
iac n/a| -1 0 0 12 0 44 -.05 23 22 | -894 -160 3181 9235
| 0 1 2 31 24 59 .05 | 1028 822
mcc n/a| -1 -1 -18 58 -61 -170 -.49 181 181 | --- --- --- ---
| 4 6 16 133 102 265 .15 | --- ---
Table 1.2052.b GPS week : 2052 MJD: 58608.0-58614.0
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 21 16 16 17 15 16 |
R02 | 7 7 8 7 8 9 8 |
R03 | 7 7 6 8 7 8 7 |
R04 | 6 6 7 7 5 7 6 |
R05 | 9 10 10 8 9 9 11 |
R07 | 7 7 6 9 8 6 7 |
R08 | 8 8 9 6 6 4 8 |
R09 | 8 7 7 7 7 7 8 |
R10 | 8 8 8 6 7 7 8 |
R11 | 8 7 7 7 6 5 6 |
R13 | 7 12 10 8 10 9 9 |
R14 | 7 8 8 9 10 11 9 |
R15 | 11 10 9 10 12 12 10 |
R16 | 14 14 17 16 16 19 17 |
R17 | 6 7 8 9 8 7 6 |
R18 | 6 6 6 7 6 6 7 |
R19 | 16 18 20 21 19 18 17 |
R20 | 13 12 10 12 15 11 11 |
R21 | 9 7 8 6 6 6 7 |
R22 | 10 9 8 8 9 7 8 |
R23 | 10 11 10 9 10 9 10 |
R24 | 15 11 12 12 12 13 11 |
R26 | 12 15 12 15 34 31 12 |
Table 1.2052.c GPS week : 2052 MJD: 58608.0-58614.0
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 2052 0 | 56 -83 269 987 789 3152 83.5 >>>>> >>>>> | -3823 0
brd 2052 1 | -25 68 318 -1131 1309 3266 81.7 1575 1575 | -2136 0
brd 2052 2 | -22 -40 253 251 752 3664 83.7 1385 1385 | -2463 0
brd 2052 3 | 78 19 188 402 -1016 3577 83.8 22580 22580 | -2115 0
brd 2052 4 | -73 7 169 68 -1002 3696 82.6 1490 1490 | -189 0
brd 2052 5 | 2 40 194 260 -182 719 85.6 1301 1301 | -1687 0
brd 2052 6 | 28 21 60 662 1171 632 84.6 1248 1248 | -2891 0
-------------+------------------------------------------------------------+----------------
brd 2052 mean| 6 4 207 214 260 2672 83.6 24596 24596 | -2186 0
brd 2052 sdev| 52 51 83 666 989 1378 1.3 52629 52629 | 1117 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 2.2052.0 GPS week: 2052 Day: 0 MJD: 58608
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 4 17 9 -12 .05 19 15 | 13428 -2635 3303 9242
cof n/a| 0 0 6 34 22 -41 .10 23 19 | 13412 -2618 3295 9243
emx n/a| 0 2 3 9 -69 53 .05 23 23 | -13525 -1638 3305 9087
esx n/a| -1 0 -4 9 9 0 .20 19 15 | -23995 -2380 3319 11122
gfz n/a| 0 0 1 -1 4 -59 .07 28 18 | 0 -2717 3304 9110
grg n/a| 3 0 -5 -85 53 -111 -.37 23 20 | -2451 -3184 3241 8855
iac n/a| -3 1 0 34 -10 133 -.08 23 22 | -2468 -1608 3303 9069
mcc n/a| 2 6 3 -59 -61 -119 -.59 159 159 | --- --- --- ---
Table 2.2052.1 GPS week: 2052 Day: 1 MJD: 58609
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| 2 -2 6 29 24 25 .09 21 17 | 12822 -538 3302 10730
cof n/a| 2 0 2 26 13 1 .04 22 18 | 12807 -521 3305 10733
emx n/a| -1 1 4 24 -84 55 .00 21 20 | 1240 -534 3303 10439
esx n/a| -1 0 -2 20 -7 -12 .14 20 16 | 3859 600 3308 13248
gfz n/a| 1 -1 -1 2 38 13 .05 24 16 | 0 166 3325 10490
grg n/a| 2 -1 -6 -86 40 -204 -.31 26 21 | -1807 53 3320 10397
iac n/a| -1 1 0 -6 13 82 -.10 23 22 | -1672 865 3306 10480
mcc n/a| 3 -6 -16 84 -8 -328 -.71 128 128 | --- --- --- ---
Table 2.2052.2 GPS week: 2052 Day: 2 MJD: 58610
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 40 -23 2 .06 20 16 | 12462 -1006 3178 8743
cof n/a| 2 -3 2 65 -23 -7 .12 19 17 | 12446 -982 3178 8746
emx n/a| 0 -1 0 -8 -76 114 .10 21 21 | -12672 -731 3172 8721
esx n/a| -2 -1 -2 39 -13 -11 .18 23 18 | 17938 -510 3177 11189
gfz n/a| 0 1 1 20 23 -3 .07 25 16 | 0 -1181 3165 8551
grg n/a| 1 0 -1 -63 62 -98 -.32 20 17 | -1377 -2130 3197 7633
iac n/a| -1 1 0 -4 34 -16 -.08 21 20 | -1043 284 3170 8679
mcc n/a| -3 -2 -1 330 -71 -296 -.37 119 119 | --- --- --- ---
Table 2.2052.3 GPS week: 2052 Day: 3 MJD: 58611
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 7 36 -13 17 .09 24 22 | 11200 -1266 2947 8931
cof n/a| 2 0 5 18 -28 -3 .13 26 27 | 11181 -1228 2949 8933
emx n/a| 0 -2 1 17 -47 -8 .01 24 24 | 5635 -432 2951 8844
esx n/a| -1 1 -1 5 -9 -43 .20 20 15 | -20295 -991 2953 9114
gfz n/a| 0 0 -1 2 8 -38 .08 23 15 | 0 -1759 2966 8725
grg n/a| 2 -2 -5 -42 37 -27 -.38 21 20 | -1349 -1273 2983 8023
iac n/a| -2 0 4 -9 6 87 -.01 23 22 | -754 194 2948 8735
mcc n/a| -6 -5 -13 -15 120 -608 -.23 160 160 | --- --- --- ---
Table 2.2052.4 GPS week: 2052 Day: 4 MJD: 58612
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 -1 -4 -3 .08 22 21 | 11135 2744 3088 9942
cof n/a| 0 -1 3 -9 29 44 .16 24 21 | 11140 2737 3090 9946
emx n/a| 0 1 4 17 -28 86 .01 21 21 | -14357 2095 3094 9836
esx n/a| -1 0 -3 -4 -13 -12 .21 23 15 | 12205 3113 3078 11567
gfz n/a| 0 0 -6 19 35 28 .15 26 18 | 0 1562 3080 9677
grg n/a| 2 -2 4 -55 50 -94 -.39 21 18 | -1303 2293 3078 9245
iac n/a| 0 0 -1 72 -10 11 -.11 26 24 | 519 190 3087 9650
mcc n/a| -6 0 -32 15 -110 -94 -.54 195 195 | --- --- --- ---
Table 2.2052.5 GPS week: 2052 Day: 5 MJD: 58613
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 12 1 0 .11 22 17 | 12661 553 3327 9628
cof n/a| 0 0 -1 16 9 10 .06 24 19 | 12666 521 3332 9632
emx n/a| 0 1 3 9 -59 39 .04 24 24 | -20522 891 3329 9528
esx n/a| -3 1 -2 29 -7 -16 .15 18 14 | 13082 654 3344 11996
gfz n/a| 1 -1 -2 -32 32 -28 .15 26 22 | 0 932 3364 9498
grg n/a| 1 0 3 -82 20 17 -.31 21 19 | -1961 356 3350 8886
iac n/a| -2 -2 -2 15 -41 -25 -.01 25 23 | 202 -845 3339 9361
mcc n/a| 0 6 -43 -36 -85 180 -.48 226 226 | --- --- --- ---
Table 2.2052.6 GPS week: 2052 Day: 6 MJD: 58614
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 4 42 -42 14 .05 23 21 | 13230 -1493 3121 8983
cof n/a| 1 0 0 39 -40 -12 -.02 23 20 | 13220 -1485 3118 8983
emx n/a| -3 0 2 52 -54 41 -.07 24 24 | -7413 -740 3128 8720
esx n/a| 0 0 -2 11 -26 -18 .10 16 13 | -4562 -1283 3122 11207
gfz n/a| 0 0 -4 0 21 -82 .09 24 19 | 0 -1549 3115 8742
grg n/a| 0 0 0 -108 86 3 -.30 23 20 | -2433 -1262 3139 8270
iac n/a| -1 0 -2 -12 11 41 .01 22 21 | -1043 -200 3115 8677
mcc n/a| 2 -9 -25 91 -217 71 -.53 283 283 | --- --- --- ---
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 3.2052.0 GPS week: 2052 Day: 0 MJD: 58608
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 | 977 46 59 43 46 28 52 27 --- 19 | 85 97 72 54 71 51 42 --- 55
R02 | 1378 10 12 29 12 12 12 14 189 7 | 39 40 43 26 26 31 28 107 30
R03 | 599 11 14 15 14 17 11 21 174 6 | 56 58 56 46 58 58 45 50 51
R04 | 655 11 15 11 9 8 10 20 --- 5 | 55 51 54 48 51 51 41 --- 49
R05 | 747 16 17 23 22 17 17 26 --- 9 | 46 48 51 52 50 48 35 --- 44
R07 | 757 8 9 10 12 17 17 25 101 6 | 66 66 61 69 76 68 58 141 65
R08 | 951 13 15 14 17 26 27 11 --- 8 | 57 59 52 53 50 71 50 --- 54
XR09 | 3119 10 21 10 --- 17 --- 15 --- 7 | 41 36 36 --- 45 --- 44 --- 40
R10 |>>>>> 15 15 14 13 21 25 10 --- 7 | 59 59 47 54 58 42 52 --- 51
R11 | 2039 9 16 15 11 29 13 27 186 8 | 62 68 56 56 78 67 42 85 59
R13 | 1902 8 13 16 12 17 24 19 --- 7 | 79 84 70 85 94 103 74 --- 83
R14 | 1363 19 19 17 15 16 10 18 --- 7 | 84 83 62 68 82 77 60 --- 71
R15 | 1446 22 27 18 22 23 26 34 --- 11 | 99 101 81 81 97 103 70 --- 87
XR16 | 764 32 38 40 17 21 --- 20 --- 13 | 86 85 46 65 79 --- 60 --- 66
R17E | 853 12 10 18 10 18 13 14 --- 6 | 49 47 46 51 53 55 54 --- 50
R18E | 658 9 10 14 15 20 12 12 --- 6 | 37 33 34 35 35 33 44 --- 34
R19E | 882 39 32 38 27 52 15 33 --- 15 | 46 48 31 59 78 49 64 --- 47
R20E | 1689 12 27 28 15 62 25 23 --- 13 | 74 82 75 78 101 84 78 --- 78
R21E | 691 18 19 24 11 13 22 22 124 8 | 40 41 38 40 39 36 41 44 37
R22E | 1114 18 19 30 15 15 24 28 --- 10 | 73 69 78 73 74 70 67 --- 71
R23E | 1149 17 20 20 24 22 19 25 --- 9 | 54 55 58 63 57 60 63 --- 57
R24E | 920 27 28 32 25 50 36 29 --- 15 | 33 43 35 43 71 50 44 --- 37
XR26E | ---- 17 33 --- --- --- 13 18 --- 11 | 55 43 --- --- --- 59 58 --- 55
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 19 23 23 19 28 23 23 159 |T 59 60 53 57 64 60 52 85 55
WRMS |>>>>> 15 19 23 15 18 20 22 159 |NE 65 66 56 58 65 64 50 95 57
MEDI | 951 15 19 18 15 18 17 21 174 |MD 56 58 52 54 58 58 52 85 54
Table 3.2052.1 GPS week: 2052 Day: 1 MJD: 58609
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 | 847 53 41 45 51 35 54 26 --- 20 | 55 71 58 62 71 44 34 --- 45
R02 | 1043 10 13 18 10 16 27 13 146 7 | 25 29 28 28 22 31 30 61 23
R03 | 912 13 13 18 12 16 12 17 104 6 | 40 40 42 33 29 40 30 32 34
R04 | 868 12 18 12 12 9 14 23 --- 6 | 39 42 40 30 40 34 32 --- 34
R05 | 823 20 21 19 21 17 23 34 --- 10 | 33 32 34 44 44 46 28 --- 33
R07 | 550 8 8 8 10 18 15 27 108 7 | 47 47 48 48 58 59 46 93 49
R08 | 844 17 20 21 12 19 16 23 --- 8 | 41 38 38 41 47 45 39 --- 40
XR09 | 3102 11 11 16 12 16 --- 10 --- 6 | 37 39 24 32 40 --- 38 --- 34
R10 | 2736 14 14 12 16 14 32 8 --- 7 | 39 40 37 41 38 29 33 --- 35
R11 | 2068 18 13 11 11 13 20 15 157 6 | 45 43 42 38 40 42 32 35 38
R13 | 3397 15 12 25 10 36 43 21 --- 11 | 62 65 57 66 93 107 53 --- 70
R14 | 1618 20 19 14 10 18 20 24 --- 8 | 63 63 57 68 77 65 47 --- 62
R15 | 1872 26 32 17 20 12 22 24 --- 9 | 69 73 59 57 57 73 56 --- 59
XR16 | 662 25 48 43 16 28 --- 18 --- 13 | 51 76 36 50 47 --- 45 --- 41
R17E | 1377 12 13 17 13 15 16 19 --- 6 | 28 28 29 30 25 30 26 --- 25
R18E | 879 9 9 9 16 14 16 16 --- 6 | 17 22 20 27 23 20 22 --- 18
R19E | 896 40 37 36 31 54 27 42 --- 17 | 30 38 53 62 73 27 53 --- 42
R20E | 2472 16 17 24 20 42 27 23 --- 11 | 45 50 43 48 63 53 43 --- 45
R21E | 808 12 12 20 11 15 16 15 114 6 | 34 37 31 36 38 33 34 30 32
R22E | 535 14 20 25 13 19 14 29 --- 8 | 64 69 71 73 66 65 68 --- 67
R23E | 1745 26 29 18 26 24 20 22 --- 10 | 35 39 30 38 33 33 33 --- 30
R24E | 1220 21 41 17 23 28 35 22 --- 11 | 23 46 24 34 39 40 22 --- 21
XR26E | ---- 20 36 --- --- --- 26 16 --- 15 | 27 48 --- --- --- 37 19 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1574 21 22 21 20 24 26 23 128 |T 41 46 40 44 48 45 37 50 39
WRMS | 1574 17 18 20 16 16 21 22 128 |NE 46 49 42 45 50 51 38 55 42
MEDI | 912 16 18 18 13 17 20 22 114 |MD 39 42 38 41 40 40 34 35 35
Table 3.2052.2 GPS week: 2052 Day: 2 MJD: 58610
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 | 645 36 39 31 45 40 25 26 --- 15 | 67 73 61 56 68 60 42 --- 54
R02 | 744 14 14 15 17 12 18 21 93 7 | 26 28 25 31 24 19 26 33 21
R03 | 909 10 14 12 15 12 11 14 115 5 | 42 46 42 39 42 43 45 44 41
R04 | 1102 10 9 12 19 15 16 14 --- 6 | 47 44 44 35 40 51 38 --- 41
R05 | 993 16 15 21 29 22 26 19 --- 10 | 36 39 42 32 38 55 31 --- 35
R07 | 782 7 12 8 14 18 10 20 169 6 | 51 55 48 47 62 46 44 56 48
R08 | 1304 10 13 15 20 16 13 33 --- 8 | 44 45 43 56 52 46 42 --- 43
XR09 | 2737 13 21 15 11 14 --- 10 --- 6 | 32 37 28 30 42 --- 27 --- 31
R10 | 1615 10 10 14 20 25 17 16 --- 7 | 41 39 35 38 26 44 40 --- 34
R11 | 1707 20 23 10 11 16 21 12 139 7 | 48 49 41 38 31 35 31 52 35
R13 | 2671 12 12 24 13 37 27 17 --- 10 | 58 62 46 56 85 76 51 --- 60
R14 | 1340 24 28 13 10 22 12 17 --- 7 | 62 64 52 54 43 46 51 --- 50
R15 | 2293 21 23 16 19 14 16 32 --- 9 | 88 88 79 72 79 79 68 --- 76
XR16 | 1128 27 31 57 22 27 --- 19 --- 17 | 58 57 46 50 54 --- 44 --- 46
R17E | 1363 21 12 20 10 17 15 13 --- 7 | 27 27 28 30 32 30 28 --- 26
R18E | 737 7 10 15 17 13 15 15 --- 6 | 22 21 18 26 30 25 26 --- 21
R19E | 1767 40 24 47 60 51 26 33 --- 19 | 29 38 40 78 71 45 42 --- 37
R20E | 1619 21 16 24 18 27 15 21 --- 9 | 40 43 46 53 58 36 44 --- 42
R21E | 1197 13 10 22 10 15 18 17 37 7 | 31 30 35 35 33 27 35 30 30
R22E | 634 16 10 22 15 12 23 14 --- 8 | 40 42 42 46 47 55 46 --- 44
R23E | 1154 22 27 17 24 30 13 17 --- 9 | 38 36 46 51 50 48 45 --- 43
R24E | 1006 26 23 21 16 29 40 25 --- 12 | 29 37 40 45 53 65 41 --- 40
XR26E | ---- 15 40 --- --- --- 14 22 --- 12 | 30 60 --- --- --- 23 34 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1385 20 19 21 23 25 20 21 119 |T 42 46 42 45 48 45 40 43 40
WRMS | 1385 16 17 21 18 16 17 20 119 |NE 50 51 45 45 49 50 41 46 43
MEDI | 1154 16 15 16 17 17 16 17 115 |MD 40 43 42 45 43 46 42 44 41
Table 3.2052.3 GPS week: 2052 Day: 3 MJD: 58611
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 | 559 47 54 36 51 16 24 25 --- 16 | 65 71 55 26 37 47 30 --- 36
R02 | 556 8 12 11 13 13 14 26 143 6 | 32 31 29 26 31 32 30 128 26
R03 | 567 9 13 17 18 16 20 19 137 7 | 45 45 38 34 45 51 39 74 40
R04 | 709 16 15 17 12 14 20 13 --- 7 | 42 37 39 34 33 25 28 --- 30
R05 | 843 18 19 26 18 19 12 12 --- 8 | 38 35 43 37 30 24 31 --- 30
R07 | 936 16 14 13 15 14 13 34 233 8 | 55 53 46 43 53 44 25 45 42
R08 | 2547 11 14 12 14 10 13 11 --- 5 | 42 42 41 31 34 36 31 --- 34
XR09 | 2755 13 14 16 13 13 --- 13 --- 7 | 22 22 20 19 28 --- 22 --- 19
R10 | 2559 9 12 15 12 15 16 13 --- 6 | 45 45 38 44 52 43 37 --- 42
R11 | 1162 15 20 16 9 12 12 28 153 7 | 54 55 41 45 51 52 34 102 45
R13 | 1355 11 8 21 11 23 13 21 --- 7 | 53 54 42 54 72 58 43 --- 53
R14 | 1362 17 17 14 19 18 20 27 --- 8 | 55 51 39 37 60 64 30 --- 46
R15 | 2057 28 30 18 18 11 19 37 --- 10 | 72 73 53 45 56 65 43 --- 54
R16 | 1443 39 59 30 14 33 55 15 --- 15 | 58 63 49 44 63 30 44 --- 48
R17E | 1191 15 17 41 12 16 14 17 --- 9 | 28 31 34 26 37 25 34 --- 25
R18E | 744 8 10 9 17 20 11 16 --- 6 | 26 27 21 30 23 28 29 --- 24
R19E | 950 62 42 49 43 58 25 41 --- 21 | 46 45 57 66 99 46 59 --- 48
R20E | 1256 18 22 21 24 32 28 26 --- 11 | 32 31 23 36 34 30 36 --- 23
R21E | 881 14 21 20 9 13 12 13 101 6 | 53 63 49 51 57 56 53 75 52
R22E |>>>>> 17 17 24 11 16 16 14 --- 7 | 55 53 51 52 60 51 55 --- 52
R23E | 1417 21 23 19 17 22 24 13 --- 9 | 45 46 40 46 38 60 45 --- 44
R24E | 883 23 35 35 16 32 19 24 --- 11 | 27 44 21 33 49 36 41 --- 28
XR26E | ---- 19 84 --- --- --- 19 25 --- 15 | 32 71 --- --- --- 22 36 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS |22580 24 26 24 20 23 21 23 160 |T 44 47 39 39 47 42 37 84 37
WRMS |22580 22 27 24 15 15 20 22 160 |NE 48 48 40 37 46 43 33 87 38
MEDI | 1162 16 17 18 14 16 16 19 143 |MD 45 45 40 37 45 43 36 75 40
Table 3.2052.4 GPS week: 2052 Day: 4 MJD: 58612
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 | 669 58 48 19 52 23 24 17 --- 17 | 66 58 47 46 43 44 25 --- 38
R02 | 728 12 21 15 13 9 13 32 151 7 | 28 36 33 23 21 36 18 100 23
R03 | 1086 9 10 16 10 12 18 24 93 7 | 41 45 45 43 47 59 43 70 45
R04 | 640 12 16 13 12 11 10 12 --- 5 | 45 49 41 47 42 36 48 --- 42
R05 | 733 16 11 20 21 21 18 15 --- 8 | 38 40 40 43 34 24 39 --- 32
R07 | 1139 10 12 18 15 20 12 23 376 7 | 53 56 54 45 61 56 45 65 51
R08 | 2795 6 11 11 11 21 20 9 --- 6 | 43 48 44 41 39 49 47 --- 42
R09 | 2446 12 13 17 14 12 20 13 --- 7 | 33 31 26 21 32 21 25 --- 29
R10 | 3549 13 15 23 13 11 15 19 --- 7 | 46 47 39 49 50 45 32 --- 42
R11 | 880 15 19 11 7 15 9 23 89 6 | 45 46 35 38 39 38 27 95 36
R13 | 1258 9 15 20 16 34 23 22 --- 9 | 54 58 59 65 49 64 58 --- 57
R14 | 1302 22 27 19 22 24 16 26 --- 9 | 65 72 59 63 78 61 45 --- 60
R15 | 1765 22 23 18 22 25 25 47 --- 12 | 79 81 69 67 88 83 60 --- 72
R16 | 1143 32 37 37 27 36 46 37 --- 16 | 62 52 28 43 55 29 40 --- 40
R17E | 1093 14 13 22 9 18 13 22 --- 7 | 26 25 25 26 31 33 34 --- 27
R18E | 892 6 10 13 12 16 15 13 --- 5 | 25 26 26 31 28 26 28 --- 26
R19E | 930 39 58 30 54 40 32 53 --- 18 | 42 58 39 87 55 54 49 --- 46
R20E | 1356 26 29 30 20 63 24 23 --- 14 | 36 54 39 49 74 52 41 --- 44
R21E | 969 11 8 15 11 17 9 15 99 6 | 30 32 31 35 36 34 36 74 32
R22E | 610 16 14 17 12 18 12 34 --- 8 | 100 105 100 111 105 109 87 --- 101
R23E | 754 19 13 27 26 25 20 18 --- 10 | 34 41 40 49 46 51 44 --- 40
R24E | 1735 22 27 29 24 39 23 21 --- 12 | 42 56 37 48 58 44 41 --- 40
XR26E | ---- 41 93 --- --- --- 59 33 --- 33 | 37 74 --- --- --- 84 35 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1490 22 24 21 23 26 21 26 195 |T 46 51 43 48 50 49 41 80 43
WRMS | 1490 21 21 21 15 18 18 24 195 |NE 49 51 44 45 48 46 39 82 43
MEDI | 1086 15 15 18 14 20 18 22 99 |MD 42 49 39 45 46 45 41 74 41
Table 3.2052.5 GPS week: 2052 Day: 5 MJD: 58613
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 | 1153 43 42 26 30 24 21 42 --- 14 | 54 56 43 43 56 55 25 --- 40
R02 | 1398 18 14 31 16 15 12 23 87 8 | 31 28 33 24 31 29 17 48 24
R03 | 1054 10 12 24 11 32 10 18 66 8 | 40 39 35 41 66 51 40 40 43
R04 | 669 8 10 14 6 19 21 25 --- 7 | 40 40 36 42 52 54 30 --- 41
R05 | 474 16 23 23 20 15 13 24 --- 8 | 33 49 44 48 48 38 42 --- 40
R07 | 661 11 14 20 9 13 7 18 468 6 | 43 45 55 43 38 39 44 104 42
R08 | 2029 7 7 9 8 9 10 13 --- 4 | 42 44 45 44 49 39 42 --- 42
R09 | 3319 12 16 13 11 16 20 15 --- 6 | 31 34 25 34 45 20 44 --- 33
R10 | 1672 14 20 16 11 17 22 17 --- 7 | 39 46 34 39 40 36 31 --- 34
R11 | 785 9 11 16 9 10 10 14 142 5 | 37 37 31 36 37 32 34 46 33
R13 | 1167 18 26 23 13 24 17 24 --- 8 | 54 56 48 67 59 61 52 --- 56
R14 | 938 28 28 21 21 27 22 21 --- 10 | 67 69 60 64 71 51 57 --- 59
R15 | 1814 22 28 20 20 33 23 42 --- 12 | 82 83 70 66 90 83 67 --- 74
R16 | 1272 34 36 47 38 59 39 35 --- 18 | 60 82 46 55 99 34 44 --- 55
R17E | 999 14 12 22 12 16 18 14 --- 7 | 28 30 36 36 32 28 35 --- 30
R18E | 874 9 18 16 10 14 15 14 --- 5 | 26 27 29 32 28 29 30 --- 27
R19E | 855 45 40 38 29 43 30 51 --- 17 | 37 42 30 49 56 57 54 --- 38
R20E | 659 24 41 21 16 30 26 26 --- 10 | 43 50 44 52 57 53 49 --- 45
R21E | 777 14 13 20 10 13 13 12 63 6 | 40 44 43 40 41 41 44 24 40
R22E | 1059 14 12 17 10 21 16 14 --- 6 | 77 79 80 84 78 86 84 --- 81
R23E | 672 21 19 20 18 26 18 13 --- 8 | 54 63 49 55 50 51 54 --- 50
R24E | 959 27 28 34 15 41 38 18 --- 13 | 31 31 25 43 72 58 36 --- 40
XR26E | ---- 40 79 --- --- --- 55 30 --- 31 | 47 62 --- --- --- 85 42 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1301 22 24 24 18 26 21 25 226 |T 45 49 42 47 54 48 43 52 44
WRMS | 1301 17 19 24 14 22 19 23 226 |NE 46 50 43 46 55 44 40 59 44
MEDI | 959 16 19 20 12 19 18 18 87 |MD 40 45 43 43 50 51 42 46 41
Table 3.2052.6 GPS week: 2052 Day: 6 MJD: 58614
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 | 1296 48 40 43 33 25 19 30 --- 15 | 83 80 68 50 58 61 37 --- 54
R02 | 1296 12 14 23 12 16 13 25 51 7 | 39 47 47 45 51 45 27 81 40
R03 | 1009 10 11 8 12 21 16 17 45 6 | 53 56 45 45 65 55 51 64 50
R04 | 746 10 12 9 11 14 10 19 --- 5 | 51 50 50 53 50 56 42 --- 50
R05 | 594 21 15 24 22 28 26 27 --- 11 | 39 41 49 56 50 53 42 --- 45
R07 | 654 14 13 21 15 14 13 18 603 7 | 65 61 71 59 56 58 53 139 59
R08 | 1360 7 11 17 16 31 17 14 --- 8 | 56 57 62 67 49 62 56 --- 57
R09 | 2471 9 11 16 9 35 21 7 --- 8 | 43 43 30 30 63 13 46 --- 41
R10 | 2099 15 12 18 14 23 15 25 --- 8 | 60 60 42 58 63 45 36 --- 50
R11 | 906 13 15 15 10 15 15 16 170 6 | 62 65 48 56 57 56 44 92 53
R13 | 1233 16 16 20 10 12 30 26 --- 8 | 70 76 65 80 76 93 72 --- 75
R14 | 1102 27 28 20 14 20 12 15 --- 8 | 93 94 89 83 82 87 78 --- 84
R15 | 1719 28 25 20 12 9 19 32 --- 9 | 120 122 107 100 111 110 100 --- 107
R16 | 1567 41 46 46 29 32 49 22 --- 16 | 93 100 63 80 103 39 72 --- 79
R17E | 1248 10 15 18 6 15 16 11 --- 5 | 41 39 39 40 45 41 42 --- 40
R18E | 822 12 14 20 8 14 23 17 --- 7 | 39 38 34 45 38 49 51 --- 41
R19E | 636 52 51 35 21 44 22 44 --- 16 | 49 56 44 65 74 68 68 --- 56
R20E | 1049 17 18 27 15 32 32 24 --- 11 | 68 76 73 72 80 65 76 --- 70
R21E | 921 16 17 18 13 15 22 11 53 7 | 51 55 52 49 52 50 51 40 49
R22E | 717 16 19 17 9 14 22 29 --- 8 | 78 81 81 78 78 78 69 --- 75
R23E | 1149 19 16 21 14 21 37 11 --- 9 | 66 65 61 64 69 84 62 --- 65
R24E | 869 16 20 36 17 33 20 21 --- 10 | 38 45 45 44 63 51 39 --- 40
XR26E | ---- 17 98 --- --- --- 16 14 --- 11 | 49 100 --- --- --- 61 57 --- 53
------+---------------------------------------------------+-----------------------------------------------
RMS | 1247 23 23 24 16 24 23 22 283 |T 61 65 57 59 65 60 55 83 57
WRMS | 1247 21 20 24 13 19 20 21 283 |NE 66 68 59 61 66 59 54 94 60
MEDI | 1049 16 16 20 13 20 19 19 53 |MD 56 60 50 56 63 56 51 81 53
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