[IGSREPORT-26578] Wk 2051 IGLOS Final Orbits
acc
acc at igs.org
Sat May 18 04:44:19 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2051 (Apr 28, 2019 - May 04, 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 2.2051.
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:
igl2051[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2051 in the SP3 format.
igl20517.sum Combination Report for GPS Week 2051.
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 | -0.3 ns
1 | -1.7 ns
2 | -1.5 ns
3 | -3.5 ns
4 | -2.2 ns
5 | -2.9 ns
6 | -2.5 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 1.2051, 1a.2051).
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 2.2051.0-6)
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 3.2051.0-6).
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 2051 summary. (Apr 28, 2019 - May 04, 2019)
Table 1.2051.a GPS week : 2051 MJD: 58601.0-58607.0
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 4 49 10 7 .05 22 18 | 13502 962 3200 9077
| 1 0 1 20 21 30 .03 | 634 1582
cof n/a| 0 0 3 32 24 0 .07 24 20 | 13493 970 3201 9079
| 0 1 2 18 18 33 .02 | 635 1586
emx n/a| 0 0 0 12 -59 59 .08 25 25 | -6023 881 3167 8995
| 1 1 3 19 21 46 .02 | 16398 991
esx n/a| -1 0 -3 12 -11 -17 .13 21 16 | -1054 1393 3167 11158
| 0 1 1 14 12 20 .04 | 8515 1420
gfz n/a| 0 0 1 -20 17 -12 .10 24 17 | 0 1019 3169 8844
| 1 0 3 20 13 35 .06 | 0 1121
grg n/a| 2 0 -2 -78 20 -21 -.34 23 20 | -2866 619 3638 10308
| 1 0 4 16 10 82 .03 | 1568 1332
iac n/a| -2 0 2 27 8 -13 -.04 26 25 | -1045 -40 3830 10707
| 1 1 1 23 12 52 .06 | 1635 1070
mcc n/a| 3 -1 -10 72 -61 -74 -.44 131 131 | --- --- --- ---
| 9 4 13 115 128 281 .29 | --- ---
Table 1.2051.b GPS week : 2051 MJD: 58601.0-58607.0
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 | 22 20 19 19 20 18 18 |
R02 | 8 6 7 7 8 8 8 |
R03 | 10 9 8 7 7 7 12 |
R04 | 7 8 7 6 6 7 6 |
R05 | 12 13 8 8 9 9 9 |
R07 | 7 8 8 8 7 8 6 |
R08 | 8 7 8 7 7 7 6 |
R09 | 6 7 7 6 7 6 10 |
R10 | 8 9 8 7 10 8 10 |
R11 | 10 7 6 8 7 6 7 |
R13 | 10 13 10 8 11 13 8 |
R14 | 8 7 8 9 9 8 9 |
R15 | 11 9 9 12 8 9 11 |
R16 | 17 16 14 17 20 20 20 |
R17 | 7 9 9 7 6 6 8 |
R18 | 6 7 8 7 6 7 7 |
R19 | 16 19 19 21 23 20 16 |
R20 | 15 11 9 13 12 11 11 |
R21 | 8 9 7 7 8 8 9 |
R22 | 10 8 8 7 7 9 8 |
R23 | 11 10 10 10 11 11 10 |
R24 | 11 12 10 11 15 12 11 |
R26 | 17 15 13 12 11 14 21 |
Table 1.2051.c GPS week : 2051 MJD: 58601.0-58607.0
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 2051 0 | -3 32 114 126 436 3277 83.0 1504 1504 | -286 0
brd 2051 1 | 37 -35 169 -397 295 4746 84.1 1469 1469 | -1697 0
brd 2051 2 | 29 -33 168 95 -181 5143 83.1 1612 1612 | -1480 0
brd 2051 3 | 56 -23 157 1216 -1700 2739 82.4 1669 1669 | -3547 0
brd 2051 4 | -8 74 125 50 -1215 3133 82.4 1416 1416 | -2194 0
brd 2051 5 | -35 6 195 1501 -45 1603 84.5 1354 1354 | -2925 0
brd 2051 6 | 53 -35 209 739 944 1322 82.9 1412 1412 | -2451 0
-------------+------------------------------------------------------------+----------------
brd 2051 mean| 18 -2 163 475 -209 3137 83.2 1490 1490 | -2082 0
brd 2051 sdev| 34 42 34 692 936 1439 .8 113 113 | 1060 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 2.2051.0 GPS week: 2051 Day: 0 MJD: 58601
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 45 -28 -21 .04 23 16 | 12400 3398 3267 8808
cof n/a| 1 0 3 9 15 1 .05 27 18 | 12388 3415 3274 8815
emx n/a| 0 0 -3 18 -17 60 .09 25 25 | -20578 2209 3238 8938
esx n/a| -2 0 -6 13 -11 -13 .12 21 17 | -4783 3362 3255 11059
gfz n/a| 0 -1 2 -28 15 43 .14 25 17 | 0 2584 3233 8659
grg n/a| 2 0 0 -91 16 -31 -.36 25 22 | -1895 2613 3247 8242
iac n/a| -5 0 2 46 15 -60 -.15 27 26 | 533 -366 4659 9300
mcc n/a| 0 -6 -30 176 -216 -84 .05 161 161 | --- --- --- ---
Table 2.2051.1 GPS week: 2051 Day: 1 MJD: 58602
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 77 15 12 .10 23 18 | 13256 176 3193 9539
cof n/a| 0 0 3 44 17 4 .08 23 19 | 13244 191 3193 9539
emx n/a| 2 -1 -1 13 -60 9 .04 27 27 | 4674 495 3034 9270
esx n/a| -1 -1 -2 23 -18 -22 .12 21 17 | -6180 941 3043 11766
gfz n/a| -2 0 7 -48 30 -31 .04 23 17 | 0 687 3042 9004
grg n/a| 2 0 -6 -91 6 45 -.36 26 21 | -2131 422 3366 8858
iac n/a| -2 1 1 6 5 -43 .02 26 25 | -643 525 3369 8966
mcc n/a| 1 3 -9 178 -82 -463 -.30 114 114 | --- --- --- ---
Table 2.2051.2 GPS week: 2051 Day: 2 MJD: 58603
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 63 30 -27 .01 22 19 | 13120 1883 3161 8884
cof n/a| 0 -1 6 29 33 -45 .05 26 23 | 13102 1916 3158 8885
emx n/a| 0 1 0 25 -63 1 .08 23 23 | -13259 1102 3147 8885
esx n/a| 0 0 -3 17 -12 -46 .13 20 15 | 4514 1671 3145 11115
gfz n/a| 1 0 1 -38 25 -46 .03 19 17 | 0 2186 3149 8643
grg n/a| 2 -1 -4 -77 7 71 -.39 24 21 | -1213 1602 3468 8663
iac n/a| -2 0 3 9 6 99 -.05 25 25 | 273 800 3520 9703
mcc n/a| 4 -2 12 -28 34 -432 -.57 119 119 | --- --- --- ---
Table 2.2051.3 GPS week: 2051 Day: 3 MJD: 58604
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 12 21 4 .05 20 18 | 14024 -581 2899 8531
cof n/a| 0 0 0 35 54 3 .11 22 21 | 14019 -565 2901 8532
emx n/a| 0 -1 0 33 -48 34 .05 23 23 | -8353 -295 2892 8459
esx n/a| 0 2 -2 -1 -3 -35 .13 22 17 | -12581 -46 2889 10032
gfz n/a| 1 0 -1 -15 -5 -12 .21 27 20 | 0 -519 2893 8424
grg n/a| 2 0 2 -46 21 24 -.36 23 19 | -4655 -1386 3656 12532
iac n/a| -1 0 0 44 12 -10 -.01 26 24 | -2368 -1623 3634 12428
mcc n/a| -9 4 -19 -133 -127 13 -.81 153 153 | --- --- --- ---
Table 2.2051.4 GPS week: 2051 Day: 4 MJD: 58605
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 57 -10 18 .01 22 18 | 13571 1810 3449 9320
cof n/a| 0 0 1 18 12 1 .08 22 17 | 13570 1806 3445 9319
emx n/a| 0 1 2 -3 -89 80 .08 26 26 | -24925 1771 3453 9234
esx n/a| -1 0 -5 -10 10 -24 .15 23 16 | -3453 1892 3455 11434
gfz n/a| 0 0 -1 -19 28 0 .13 25 15 | 0 882 3461 9171
grg n/a| 0 0 2 -66 28 -55 -.32 24 19 | -4318 844 4183 11721
iac n/a| -2 -1 1 55 -9 -19 -.02 29 27 | -3269 1020 4251 11600
mcc n/a| -2 -4 -17 82 -203 18 -.51 135 135 | --- --- --- ---
Table 2.2051.5 GPS week: 2051 Day: 5 MJD: 58606
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 0 6 37 21 -1 .06 24 24 | 13901 -1152 3509 9935
cof n/a| 0 0 4 65 36 -27 .07 26 26 | 13903 -1157 3513 9935
emx n/a| 0 3 3 23 -68 112 .11 27 27 | 23363 -385 3524 9809
esx n/a| -1 1 -3 31 -28 4 .19 21 16 | 13761 -654 3509 12122
gfz n/a| 0 1 1 -2 21 -53 .12 25 16 | 0 -43 3532 9852
grg n/a| 2 0 -5 -85 30 -24 -.32 19 22 | -1309 -623 3952 12476
iac n/a| -2 -1 3 -5 30 -24 .01 28 24 | 647 -1309 3981 13223
mcc n/a| 5 -1 -6 146 77 291 -.69 103 103 | --- --- --- ---
Table 2.2051.6 GPS week: 2051 Day: 6 MJD: 58607
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 6 49 22 63 .08 21 15 | 14248 1206 2925 8528
cof n/a| 0 -3 5 26 -1 63 .07 22 17 | 14228 1190 2926 8534
emx n/a| 0 0 6 -23 -67 115 .08 23 23 | -3085 1276 2883 8374
esx n/a| -1 1 -3 12 -18 11 .06 20 17 | 1343 2591 2873 10581
gfz n/a| 2 0 -2 10 7 18 .05 21 20 | 0 1362 2879 8158
grg n/a| 4 -1 -8 -87 29 -178 -.29 22 18 | -4542 863 3598 9666
iac n/a| -2 0 2 32 2 -34 -.07 24 24 | -2493 669 3399 9730
mcc n/a| 21 -6 -3 86 83 136 -.25 131 131 | --- --- --- ---
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 3.2051.0 GPS week: 2051 Day: 0 MJD: 58601
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 | 679 60 69 54 58 33 37 39 --- 22 | 91 111 88 80 95 60 45 --- 71
R02 | 832 13 15 23 11 16 21 21 85 8 | 45 47 42 38 39 40 37 45 38
R03 | 737 10 10 17 17 20 33 29 77 9 | 64 62 55 54 73 82 58 94 62
R04 | 1900 18 24 15 15 9 10 21 --- 6 | 55 60 49 41 50 52 45 --- 47
R05 | 532 19 17 28 30 15 15 39 --- 11 | 53 52 56 58 57 59 44 --- 50
R07 | 1248 12 13 14 10 16 9 23 94 6 | 69 72 63 60 72 62 50 49 62
R08 | 769 18 18 14 10 25 12 21 --- 7 | 64 62 51 55 50 53 49 --- 53
R09 | 2313 13 14 11 7 15 11 15 --- 5 | 38 41 32 35 43 29 35 --- 35
R10 | 4255 10 8 20 14 26 14 11 --- 7 | 46 46 39 50 51 47 39 --- 43
R11 | 1108 11 13 13 12 29 32 25 224 9 | 54 56 48 49 64 46 32 85 47
R13 | 1374 9 12 26 16 14 35 22 --- 9 | 72 73 61 76 73 85 60 --- 70
R14 | 1276 19 19 17 15 21 12 18 --- 7 | 70 72 55 63 78 68 55 --- 64
R15 | 605 14 20 13 32 24 30 30 --- 11 | 98 99 83 73 96 107 74 --- 87
R16 | 521 39 36 42 15 16 65 33 --- 17 | 81 90 62 65 90 84 60 --- 75
R17E | 1228 9 12 20 11 16 12 18 --- 6 | 51 50 47 53 56 53 48 --- 50
R18E | 1038 11 10 16 10 9 9 24 --- 6 | 30 29 28 34 29 28 35 --- 29
R19E | 1219 43 53 35 27 41 23 42 --- 16 | 30 38 38 40 54 29 51 --- 29
R20E | 940 17 17 33 19 54 34 29 --- 14 | 90 88 87 90 105 91 89 --- 88
R21E | 1075 18 15 22 12 15 14 23 240 7 | 67 70 64 71 74 71 75 39 69
R22E | 497 17 20 24 15 22 14 40 --- 10 | 97 99 101 100 103 97 114 --- 100
R23E | 2017 27 31 27 27 14 19 23 --- 10 | 76 77 74 82 79 82 82 --- 78
R24E | 1657 24 41 16 23 36 21 26 --- 11 | 33 55 29 41 42 37 39 --- 31
XR26E | 2642 15 40 --- --- --- --- 18 --- 16 | 41 55 --- --- --- --- 47 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1504 23 27 25 21 25 25 27 161 |T 61 65 56 59 66 61 54 62 57
WRMS | 1504 16 18 25 17 17 22 26 161 |NE 64 67 56 56 66 62 48 68 57
MEDI | 1108 17 17 20 15 16 15 23 94 |MD 64 62 55 55 64 59 49 49 53
Table 3.2051.1 GPS week: 2051 Day: 1 MJD: 58602
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 | 1003 55 34 49 43 37 28 52 --- 20 | 66 64 64 62 76 50 31 --- 53
R02 | 843 12 22 10 13 10 12 18 59 5 | 31 35 24 31 29 30 22 51 26
R03 | 898 16 18 22 16 24 15 26 71 9 | 45 47 40 34 51 32 29 70 36
R04 | 1420 25 25 15 15 14 17 22 --- 8 | 38 40 31 28 32 40 24 --- 29
R05 | 614 24 19 29 31 21 34 32 --- 13 | 37 34 40 34 36 53 24 --- 31
R07 | 706 10 16 19 12 16 10 36 118 8 | 46 51 45 47 56 44 31 21 44
R08 | 874 8 15 24 13 14 17 19 --- 7 | 46 51 42 47 53 39 50 --- 45
R09 | 2604 11 13 15 19 18 16 13 --- 7 | 35 33 30 33 42 36 30 --- 33
R10 | 4109 14 16 23 19 16 22 21 --- 8 | 28 29 29 39 30 42 29 --- 30
R11 | 807 16 17 19 11 18 15 17 132 7 | 35 38 41 32 28 27 25 30 28
R13 | 1131 11 11 25 15 11 55 28 --- 12 | 45 51 42 49 47 84 45 --- 49
R14 | 1688 15 21 12 11 18 16 24 --- 7 | 48 52 43 49 45 45 40 --- 44
R15 | 1016 26 27 13 21 13 15 27 --- 9 | 74 74 64 56 66 63 55 --- 62
R16 | 588 23 31 42 19 32 61 29 --- 16 | 45 50 60 51 59 38 41 --- 47
R17E | 1053 20 12 30 12 21 15 19 --- 9 | 49 46 38 48 50 46 45 --- 44
R18E | 923 8 9 18 14 12 14 20 --- 6 | 31 33 27 36 30 36 38 --- 31
R19E | 860 47 36 47 41 48 35 36 --- 19 | 32 37 44 57 53 50 39 --- 30
R20E | 904 22 29 33 21 31 16 18 --- 11 | 84 83 77 91 85 86 89 --- 83
R21E | 1357 12 17 24 18 23 12 21 158 8 | 85 92 81 94 90 89 93 39 88
R22E | 967 16 17 22 13 17 14 18 --- 7 | 82 83 77 82 83 93 87 --- 83
R23E | 1162 23 36 25 25 19 18 20 --- 10 | 63 59 62 74 65 66 68 --- 65
R24E | 1951 17 26 35 20 28 37 22 --- 12 | 27 35 33 35 37 31 25 --- 23
XR26E | 4626 20 39 --- --- --- 20 21 --- 14 | 46 61 --- --- --- 53 48 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 1469 22 23 27 21 23 26 26 114 |T 48 51 47 50 51 51 43 42 45
WRMS | 1469 18 19 27 17 17 21 25 114 |NE 44 46 42 42 46 44 34 43 39
MEDI | 1003 16 19 23 16 18 16 21 118 |MD 45 50 42 47 50 45 39 39 44
Table 3.2051.2 GPS week: 2051 Day: 2 MJD: 58603
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 | 687 52 61 35 47 22 40 40 --- 18 | 67 79 61 39 57 46 30 --- 44
R02 | 995 15 12 12 12 13 14 20 101 6 | 44 40 34 43 39 35 31 127 36
R03 | 680 10 14 20 17 18 22 15 105 7 | 60 64 51 51 62 65 52 92 55
R04 | 612 18 16 19 16 8 13 20 --- 7 | 48 45 45 33 41 34 36 --- 38
R05 | 720 16 18 25 19 16 7 22 --- 8 | 46 51 55 42 57 38 38 --- 44
R07 | 880 16 12 18 13 12 11 34 174 8 | 56 53 55 43 48 48 29 92 46
R08 | 675 13 13 14 16 19 27 16 --- 8 | 48 47 43 48 46 33 37 --- 42
R09 | 1860 10 16 14 19 19 16 15 --- 7 | 29 29 29 34 44 27 33 --- 32
R10 | 4656 11 16 23 8 17 25 18 --- 7 | 40 35 37 43 52 58 34 --- 43
R11 | 765 12 19 17 6 10 16 21 72 6 | 46 46 42 41 43 48 32 81 41
R13 | 2760 12 18 20 10 28 28 30 --- 9 | 51 48 43 51 63 63 32 --- 49
R14 | 1599 17 14 14 9 17 15 30 --- 7 | 61 56 53 55 65 73 42 --- 57
R15 | 1045 24 29 19 15 8 19 31 --- 8 | 81 81 64 66 69 79 63 --- 69
R16 | 602 36 51 34 15 20 50 25 --- 14 | 68 79 61 48 67 62 48 --- 59
R17E | 1043 14 14 24 14 17 25 18 --- 8 | 32 32 29 33 42 34 38 --- 32
R18E | 1073 10 12 21 14 14 22 22 --- 7 | 29 31 25 35 22 29 37 --- 27
R19E | 955 46 48 43 44 36 27 46 --- 18 | 29 32 31 64 55 50 63 --- 35
R20E | 1275 17 15 22 16 19 28 15 --- 9 | 93 99 83 91 88 89 87 --- 88
R21E | 1766 11 16 20 10 20 14 19 117 7 | 41 47 41 40 50 33 42 38 39
R22E | 1490 13 16 21 11 22 14 21 --- 7 | 46 47 41 38 47 43 50 --- 41
R23E | 1261 21 27 25 22 24 14 17 --- 9 | 33 37 31 37 38 40 38 --- 33
R24E | 1999 17 22 26 19 19 28 20 --- 9 | 28 40 30 32 34 36 35 --- 26
XR26E | 5537 14 46 --- --- --- 14 24 --- 12 | 24 43 --- --- --- 33 27 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1611 22 26 23 20 19 24 25 119 |T 47 50 44 45 51 47 41 86 43
WRMS | 1611 19 23 23 15 17 21 25 119 |NE 53 53 48 45 53 50 38 98 46
MEDI | 1045 15 16 20 15 18 19 21 105 |MD 46 47 42 42 48 43 37 92 41
Table 3.2051.3 GPS week: 2051 Day: 3 MJD: 58604
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 | 558 54 50 32 54 18 28 47 --- 19 | 72 68 56 35 40 45 22 --- 39
R02 | 1780 9 19 13 15 10 8 27 197 6 | 39 48 35 48 42 38 25 136 37
R03 | 655 11 13 18 14 14 15 24 180 7 | 58 58 45 54 58 64 40 70 53
R04 | 657 9 17 11 13 9 11 19 --- 5 | 48 53 42 36 49 55 35 --- 43
R05 | 738 14 13 19 21 19 16 16 --- 8 | 43 43 43 39 44 33 32 --- 36
R07 | 801 8 15 13 24 11 23 17 130 7 | 57 60 58 41 58 74 44 98 54
R08 | 1339 13 15 18 14 20 11 19 --- 7 | 51 51 49 51 56 42 36 --- 46
R09 | 1443 9 13 13 9 13 18 13 --- 5 | 21 26 19 20 27 25 27 --- 20
R10 | 4050 6 16 20 6 31 6 20 --- 7 | 47 56 34 48 70 49 37 --- 47
R11 | 934 12 16 14 12 29 10 24 103 7 | 50 54 36 40 65 45 31 91 43
R13 | 3939 12 13 20 11 28 19 17 --- 8 | 42 45 39 43 43 48 40 --- 40
R14 | 1107 16 23 16 19 27 20 23 --- 9 | 49 59 42 39 58 42 31 --- 41
R15 | 953 13 13 17 23 21 37 43 --- 12 | 65 67 51 50 69 83 37 --- 58
R16 | 604 28 37 35 25 44 55 26 --- 16 | 64 70 34 48 73 47 46 --- 50
R17E | 676 11 14 21 15 15 14 10 --- 6 | 31 31 26 31 39 30 27 --- 29
R18E | 1064 9 12 22 11 15 17 16 --- 6 | 24 22 21 28 23 22 33 --- 22
R19E | 685 45 51 38 45 66 32 54 --- 21 | 40 50 32 59 77 48 63 --- 34
R20E | 1692 19 19 36 17 41 35 27 --- 13 | 114 120 114 126 122 133 122 --- 120
R21E | 2331 14 10 20 13 15 11 13 136 6 | 48 46 36 52 55 45 50 68 47
R22E | 1748 13 14 21 14 15 13 17 --- 7 | 30 34 31 37 37 34 35 --- 31
R23E | 859 16 12 27 22 23 21 21 --- 9 | 27 31 27 33 27 37 30 --- 25
R24E | 1552 17 23 28 19 36 24 18 --- 10 | 29 46 27 40 59 38 34 --- 33
XR26E | 7350 15 35 --- --- --- 17 20 --- 12 | 24 37 --- --- --- 36 33 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1668 20 22 23 22 27 23 26 153 |T 46 51 40 45 54 48 39 92 42
WRMS | 1668 18 21 23 17 20 19 24 153 |NE 50 54 41 42 53 49 34 98 43
MEDI | 1064 13 15 20 15 19 17 20 136 |MD 47 50 36 40 55 45 35 91 40
Table 3.2051.4 GPS week: 2051 Day: 4 MJD: 58605
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 | 575 55 50 36 56 17 25 55 --- 19 | 69 69 55 31 50 55 29 --- 40
R02 | 2037 20 11 22 13 9 9 31 135 8 | 37 28 40 24 24 23 20 77 25
R03 | 719 7 9 14 11 16 11 29 213 6 | 50 50 49 49 59 56 35 92 50
R04 | 1122 12 10 12 13 9 11 17 --- 5 | 48 46 45 42 45 37 42 --- 42
R05 | 560 15 20 19 20 24 20 21 --- 9 | 33 51 39 41 50 22 41 --- 34
R07 | 885 13 9 15 18 10 15 21 111 7 | 58 54 57 42 52 60 43 43 51
R08 | 1296 13 12 12 13 14 16 18 --- 6 | 48 50 49 54 47 42 41 --- 46
R09 | 1864 16 11 16 8 12 26 11 --- 7 | 33 32 32 32 38 32 35 --- 30
R10 | 1813 15 12 19 19 18 29 32 --- 10 | 45 41 33 52 51 37 32 --- 39
R11 | 1184 11 10 18 12 12 12 23 75 6 | 42 42 39 47 48 37 34 47 40
R13 | 2704 18 25 27 6 19 35 28 --- 10 | 49 50 49 62 62 75 47 --- 57
R14 | 1350 17 17 18 16 22 16 24 --- 8 | 58 52 52 51 61 48 49 --- 52
R15 | 1120 19 20 17 17 14 15 27 --- 8 | 76 76 67 62 67 77 66 --- 68
R16 | 657 32 21 40 54 43 47 41 --- 19 | 77 83 57 50 93 46 57 --- 63
R17E | 1283 13 10 19 9 10 13 19 --- 6 | 30 30 24 29 35 28 30 --- 28
R18E | 657 6 11 22 8 8 10 13 --- 5 | 25 27 24 27 29 24 28 --- 24
R19E | 580 40 51 59 41 57 48 61 --- 22 | 38 50 41 48 73 64 36 --- 37
R20E | 2364 26 38 23 20 29 34 28 --- 12 | 82 77 73 72 66 67 84 --- 71
R21E | 1895 10 11 25 16 18 14 21 95 7 | 32 32 30 41 39 34 36 34 33
R22E | 1254 12 13 24 11 15 11 22 --- 7 | 38 38 38 36 43 42 47 --- 38
R23E | 634 20 22 30 21 31 20 17 --- 10 | 37 40 35 41 35 40 35 --- 33
R24E | 1575 32 22 30 21 50 32 22 --- 15 | 44 56 46 62 88 59 47 --- 54
XR26E | 5578 12 58 --- --- --- 15 20 --- 11 | 24 53 --- --- --- 22 34 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1415 22 22 26 23 25 24 29 135 |T 46 49 44 45 52 44 41 58 42
WRMS | 1415 18 17 26 16 15 19 27 135 |NE 51 51 47 45 53 46 40 64 45
MEDI | 1254 15 13 19 16 16 16 22 111 |MD 44 50 41 42 50 42 36 47 40
Table 3.2051.5 GPS week: 2051 Day: 5 MJD: 58606
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 | 576 61 61 46 45 15 14 40 --- 18 | 64 65 56 38 41 31 30 --- 36
R02 | 1374 12 20 15 11 11 9 40 78 7 | 28 39 32 36 35 33 28 26 29
R03 | 657 11 14 15 13 9 8 30 133 6 | 56 50 55 44 45 55 53 72 50
R04 | 809 9 12 20 11 16 15 15 --- 6 | 36 36 45 39 48 40 36 --- 38
R05 | 541 19 16 20 25 20 13 19 --- 8 | 32 28 39 39 43 39 33 --- 34
R07 | 940 17 24 21 12 16 16 19 132 7 | 48 57 49 38 50 34 37 39 40
R08 | 1057 14 17 18 13 23 8 12 --- 6 | 45 45 51 45 31 36 46 --- 40
R09 | 1916 9 10 18 9 23 6 13 --- 6 | 24 27 25 28 42 27 31 --- 27
R10 | 2042 17 18 17 19 17 13 26 --- 8 | 38 38 28 39 39 30 20 --- 30
R11 | 1414 8 10 16 10 10 13 25 58 6 | 33 36 32 39 32 40 21 36 32
R13 | 2390 23 25 30 15 39 29 29 --- 12 | 34 35 31 42 76 60 32 --- 46
R14 | 1133 21 21 14 19 14 18 21 --- 8 | 47 51 43 50 45 60 37 --- 46
R15 | 1413 24 27 21 12 20 15 33 --- 9 | 68 70 60 62 69 69 55 --- 63
R16 | 838 49 59 47 34 51 43 36 --- 19 | 66 92 72 66 93 65 51 --- 67
R17E | 1459 12 15 19 8 17 9 13 --- 6 | 47 45 41 44 52 41 43 --- 43
R18E | 874 12 13 22 8 16 16 17 --- 6 | 28 26 34 30 26 29 29 --- 27
R19E | 671 37 34 52 39 53 28 57 --- 19 | 33 41 38 49 65 41 51 --- 33
R20E | 1748 16 23 25 22 33 27 22 --- 11 | 89 90 79 87 87 79 87 --- 83
R21E | 1234 17 17 22 13 18 12 21 94 7 | 60 62 57 56 62 61 55 47 57
R22E | 2246 19 20 31 12 20 12 23 --- 8 | 67 65 73 72 78 71 73 --- 71
R23E | 855 18 17 31 25 24 22 26 --- 11 | 62 63 53 59 63 75 58 --- 60
R24E | 1214 25 29 29 24 33 17 25 --- 11 | 32 44 37 48 53 38 42 --- 37
XR26E | 5538 23 41 --- --- --- 14 21 --- 13 | 39 51 --- --- --- 38 47 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1354 24 26 27 21 25 19 28 103 |T 46 50 46 47 53 47 43 44 44
WRMS | 1354 24 26 27 16 16 22 24 103 |NE 44 47 44 43 49 44 36 43 41
MEDI | 1214 17 20 21 13 18 14 23 94 |MD 45 45 43 44 48 40 42 39 40
Table 3.2051.6 GPS week: 2051 Day: 6 MJD: 58607
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 | 843 56 56 31 46 22 36 28 --- 18 | 94 96 71 47 69 47 46 --- 56
R02 | 1278 12 13 21 13 21 9 22 72 7 | 51 48 53 41 44 47 40 52 44
R03 | 563 25 22 26 20 19 38 29 182 12 | 123 116 101 119 119 124 115 94 115
R04 | 1155 10 7 18 10 12 12 15 --- 5 | 51 51 52 41 52 50 43 --- 47
R05 | 1149 14 18 21 19 16 17 24 --- 8 | 43 43 50 47 48 53 33 --- 43
R07 | 707 9 9 12 17 15 12 16 188 6 | 71 67 63 55 70 63 61 67 62
R08 | 945 15 16 12 10 18 9 15 --- 6 | 65 65 60 62 55 61 61 --- 60
XR09 | 2677 14 24 26 11 23 --- 19 --- 9 | 32 31 29 31 42 --- 38 --- 30
R10 | 3146 7 14 23 18 31 22 23 --- 9 | 53 55 40 54 71 64 34 --- 51
R11 | 2045 8 8 14 13 9 23 25 98 7 | 54 52 46 51 58 61 35 66 50
R13 | 1329 12 16 24 13 26 17 18 --- 8 | 56 59 51 60 78 81 55 --- 63
R14 | 1076 15 24 24 18 19 24 17 --- 8 | 69 73 57 58 77 75 54 --- 64
R15 | 1045 17 16 18 23 30 24 36 --- 11 | 97 96 86 76 102 108 73 --- 90
XR16 | 903 42 75 50 28 42 --- 29 --- 19 | 91 119 77 84 111 --- 69 --- 87
R17E | 1228 11 12 22 11 24 14 15 --- 7 | 66 66 59 64 67 76 68 --- 65
R18E | 1092 15 17 21 14 9 19 15 --- 7 | 40 41 39 41 41 42 43 --- 39
R19E | 601 41 32 37 26 33 25 45 --- 15 | 40 45 31 49 63 43 56 --- 37
R20E | 2192 15 20 27 18 26 28 29 --- 10 | 91 93 92 88 92 104 101 --- 92
R21E | 921 15 15 31 16 14 14 26 50 8 | 75 76 77 78 82 80 78 49 77
R22E | 2171 20 18 23 12 15 14 16 --- 7 | 104 103 96 103 108 110 108 --- 104
R23E | 692 17 24 28 20 25 14 26 --- 9 | 92 91 91 92 96 98 101 --- 94
R24E | 1060 21 28 21 22 20 30 26 --- 10 | 34 37 37 47 48 48 42 --- 38
XR26E | 4578 34 92 --- --- --- 30 16 --- 20 | 67 76 --- --- --- 72 68 --- 67
------+---------------------------------------------------+-----------------------------------------------
RMS | 1411 21 22 23 20 21 22 24 131 |T 67 69 61 63 72 71 61 65 64
WRMS | 1411 15 17 23 17 20 18 24 131 |NE 67 69 59 59 71 69 54 69 61
MEDI | 1092 15 18 23 17 20 19 23 98 |MD 66 66 57 55 69 64 56 66 62
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