[IGSREPORT-28083] Wk 2166 IGLOS Final Orbits
acc
acc at igs.org
Fri Jul 30 05:21:45 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2166 (Jul 11, 2021 - Jul 17, 2021)
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 2.2166.
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:
igl2166[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2166 in the SP3 format.
igl21667.sum Combination Report for GPS Week 2166.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | -7.6 ns
1 | 6.1 ns
2 | 5.9 ns
3 | -7.6 ns
4 | -8.3 ns
5 | -24.1 ns
6 | 1.8 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
3 | GFZ | R11
4 | IAC | R11
5 | ALL | R11
6 | ALL | R11
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 1.2166, 1a.2166).
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 2.2166.0-6)
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 3.2166.0-6).
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 2166 summary. (Jul 11, 2021 - Jul 17, 2021)
Table 1.2166.a GPS week : 2166 MJD: 59406.0-59412.0
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 3 4 -11 -48 .16 25 20 | -4484 680 3564 8665
| 1 1 1 15 9 21 .04 | 10644 1556
emx n/a| -4 1 -13 1 1 -36 -.10 49 37 | -10911 450 3580 9076
| 1 0 2 14 27 26 .06 | 16608 772
esx n/a| 0 2 0 21 10 -4 -.10 34 25 | -6386 1203 3568 9836
| 0 1 1 7 26 38 .03 | 13597 1353
gfz n/a| 0 1 4 -12 1 8 -.12 25 18 | 0 635 3470 8091
| 1 1 1 13 15 18 .02 | 0 1353
grg n/a| 4 -1 -4 -42 24 -102 .37 33 28 | -5180 328 3558 8199
| 2 1 6 26 11 63 .04 | 10724 1561
iac n/a| -2 -1 0 20 -17 207 -.16 29 27 | -2448 -232 3563 9182
| 2 1 4 30 48 90 .05 | 10838 1145
Table 1.2166.b GPS week : 2166 MJD: 59406.0-59412.0
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 | 20 20 20 19 20 20 19 |
R02 | 9 9 10 10 12 9 9 |
R03 | 9 9 8 8 8 8 9 |
R04 | 10 10 10 9 11 10 11 |
R05 | 9 10 9 10 8 10 11 |
R07 | 9 12 11 11 9 9 8 |
R08 | 11 12 12 9 8 11 12 |
R09 | 12 13 13 13 13 10 10 |
R11 | 8 11 10 30 136 --- --- |
R12 | 9 10 8 12 9 9 10 |
R13 | 20 17 17 16 17 15 13 |
R14 | 9 9 8 8 10 10 7 |
R15 | 7 7 8 9 7 7 6 |
R16 | 13 14 15 16 12 14 11 |
R17 | 9 9 8 8 7 7 8 |
R18 | 11 10 10 8 8 8 7 |
R19 | 28 25 19 23 27 31 26 |
R20 | 23 29 25 22 23 24 21 |
R21 | 8 7 7 10 8 9 8 |
R22 | 24 26 22 24 25 21 21 |
R24 | 11 9 11 11 10 10 11 |
Table 1.2166.c GPS week : 2166 MJD: 59406.0-59412.0
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 2166 0 | 24 33 177 1067 -783 8793 83.8 1605 1605 | -7554 0
brd 2166 1 | -2 -8 289 -734 -2432 7227 81.3 1775 1775 | 6130 0
brd 2166 2 | 17 60 366 -1529 1675 10230 83.3 3692 3692 | 5895 0
brd 2166 3 | 155 123 161 -1497 1732 11420 80.5 1553 1553 | -7613 0
brd 2166 4 | -17 9 209 713 1002 -1004 82.6 1738 1738 | -8276 0
brd 2166 5 | 12 -109 211 2566 225 4845 84.1 1601 1601 | -24084 0
brd 2166 6 | 55 2 203 263 -1619 7431 83.0 1284 1284 | 1799 0
-------------+------------------------------------------------------------+----------------
brd 2166 mean| 35 15 231 121 -28 6991 82.7 1892 1892 | -4814 0
brd 2166 sdev| 57 71 72 1489 1633 4125 1.3 809 809 | 10621 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 2.2166.0 GPS week: 2166 Day: 0 MJD: 59406
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 5 -20 -2 -47 .18 25 18 | -8526 831 3841 7648
emx n/a| -4 0 -18 -4 -28 -78 -.19 50 37 | -17702 26 3874 8099
esx n/a| -1 0 -1 24 -7 2 -.07 37 32 | -4230 1871 3847 7120
gfz n/a| 0 3 5 -9 0 -13 -.13 24 14 | 0 -46 3814 7393
grg n/a| 7 0 -14 -4 44 -215 .40 35 28 | -8000 616 3882 7385
iac n/a| 0 0 5 33 14 337 -.12 31 28 | -6204 216 3837 8209
Table 2.2166.1 GPS week: 2166 Day: 1 MJD: 59407
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 1 -3 -13 -13 .10 26 22 | 6081 606 3530 9985
emx n/a| -3 1 -13 -10 -14 -14 -.12 48 37 | -9767 593 3564 10517
esx n/a| 0 2 0 18 -2 -35 -.11 37 29 | -24671 678 3534 11969
gfz n/a| 2 3 8 -12 8 29 -.07 26 19 | 0 188 3584 8511
grg n/a| 4 0 -10 -5 32 -119 .36 36 33 | 6120 -562 3470 9457
iac n/a| -3 -3 1 71 20 102 -.10 33 27 | 7760 1060 3509 10585
Table 2.2166.2 GPS week: 2166 Day: 2 MJD: 59408
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 -9 -13 -34 .14 24 20 | 6364 -1363 3786 8870
emx n/a| -5 2 -12 -5 -7 -37 -.03 52 41 | 14208 -98 3735 9335
esx n/a| 0 2 2 34 -22 29 -.12 33 21 | 14522 -846 3769 8436
gfz n/a| 1 0 3 1 -5 24 -.11 26 21 | 0 -28 3367 8253
grg n/a| 5 1 -4 -74 17 -88 .36 31 25 | 6690 -1915 3772 8175
iac n/a| -5 -2 -2 3 1 152 -.18 27 25 | 9217 -1212 3777 9320
Table 2.2166.3 GPS week: 2166 Day: 3 MJD: 59409
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 9 -20 -37 .22 26 19 | -9238 -226 3161 7658
emx n/a| -4 1 -14 29 4 -60 -.10 48 39 | -26882 776 3192 8090
esx n/a| 0 0 1 20 11 3 -.15 31 21 | 4446 616 3172 10164
gfz n/a| 0 1 3 -27 -21 -15 -.12 23 19 | 0 -336 3171 7709
grg n/a| 2 -2 -4 -54 17 -29 .31 32 27 | -7618 -201 3180 7266
iac n/a| -2 -1 1 -19 15 248 -.16 32 32 | -6541 788 3166 8109
Table 2.2166.4 GPS week: 2166 Day: 4 MJD: 59410
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 11 -18 -61 .14 24 20 | -8610 2196 3305 7235
emx n/a| -4 0 -12 2 -21 -40 -.08 49 37 | 3570 682 3320 7475
esx n/a| 0 2 1 10 4 48 -.08 32 24 | -15801 2003 3319 10352
gfz n/a| 0 0 2 -2 10 -1 -.13 26 17 | 0 864 3158 6770
grg n/a| 2 -4 -6 -50 9 -43 .35 32 26 | -9244 1515 3315 7178
iac n/a| -6 0 0 12 -1 164 -.14 32 28 | -4393 -2144 3320 7648
Table 2.2166.5 GPS week: 2166 Day: 5 MJD: 59411
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 20 -17 -68 .14 24 22 | -22121 -413 4038 9986
emx n/a| -5 2 -13 -11 40 -7 -.04 51 36 | -33134 -616 4085 10423
esx n/a| 0 1 -1 22 33 -12 -.08 35 26 | -16838 700 4064 9846
gfz n/a| -1 2 4 -32 25 19 -.13 26 16 | 0 215 4043 8624
grg n/a| 6 -2 3 -47 27 -77 .40 33 32 | -24255 -101 4016 9522
iac n/a| -1 -1 -3 41 -71 139 -.25 27 22 | -21848 -580 4048 10622
Table 2.2166.6 GPS week: 2166 Day: 6 MJD: 59412
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 20 6 -75 .16 25 20 | 4657 3132 3290 9278
emx n/a| -1 1 -12 10 37 -15 -.14 46 34 | -6671 1787 3291 9597
esx n/a| 0 4 0 19 55 -67 -.07 34 24 | -2135 3402 3272 10971
gfz n/a| -1 0 6 -1 -6 17 -.15 23 17 | 0 3588 3158 9381
grg n/a| 2 -1 3 -57 18 -145 .42 29 28 | 41 2944 3276 8413
iac n/a| 1 -3 -8 0 -102 306 -.20 24 24 | 4868 246 3285 9784
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 3.2166.0 GPS week: 2166 Day: 0 MJD: 59406
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1736 45 59 53 37 37 32 19 | 97 37 52 93 80 55 68
R02 | 2271 9 38 18 14 13 24 8 | 74 43 68 80 72 77 71
R03 | 1567 12 37 16 20 19 18 8 | 91 73 80 102 96 87 89
XR04 | 685 14 23 11 --- 26 28 10 | 98 73 88 --- 82 89 87
R05 | 1623 10 33 13 12 20 29 8 | 72 50 81 85 74 84 75
R07 | 954 15 37 15 17 16 29 9 | 104 82 89 100 92 103 95
R08 | 2069 16 39 18 30 16 24 11 | 108 84 95 127 109 96 105
R09 | 1552 22 24 25 21 47 23 12 | 54 56 46 51 23 53 42
XR11 | 2937 14 17 21 11 --- 19 8 | 361 36 165 417 --- 393 191
R12 | 674 19 32 17 12 12 25 8 | 72 46 68 73 71 63 66
R13 | 836 52 40 31 47 45 32 19 | 94 55 64 73 67 65 68
R14 | 737 10 24 27 14 26 24 9 | 55 40 74 60 49 54 54
R15 | 1034 13 23 7 8 23 21 7 | 71 54 63 61 55 67 62
R16 | 2410 22 37 34 11 29 39 12 | 57 50 86 69 60 90 66
R17 | 956 11 19 10 12 15 37 8 | 33 29 31 30 39 40 32
R18 | 2204 12 31 32 12 25 37 11 | 32 34 30 35 35 45 32
R19 | 1616 49 139 49 22 76 40 27 | 48 59 37 41 30 39 38
R20 | 859 39 66 76 50 39 34 23 | 42 58 39 42 31 38 34
R21 | 1132 10 33 12 16 19 20 8 | 50 47 40 47 48 45 44
R22 | 2629 26 53 90 30 60 44 23 | 53 53 43 56 70 64 48
R24 | 1477 10 44 16 10 38 32 11 | 31 32 38 29 50 36 31
------+-----------------------------------------+-------------------------------------
RMS | 1605 25 50 37 24 35 31 |T 80 51 65 83 61 80 66
WRMS | 1605 18 37 32 14 28 28 |NE 80 51 65 83 61 80 66
MEDI | 1552 14 37 18 14 25 29 |MD 71 50 64 61 60 64 66
Table 3.2166.1 GPS week: 2166 Day: 1 MJD: 59407
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1389 45 62 55 45 42 17 20 | 61 28 58 76 48 51 49
R02 | 1956 9 42 8 19 14 17 8 | 49 30 51 61 56 53 50
R03 | 2765 10 34 18 25 20 17 9 | 89 75 82 97 95 77 86
XR04 | 498 16 23 11 --- 18 26 9 | 64 51 61 --- 63 67 60
R05 | 1775 14 33 13 23 23 32 10 | 49 40 58 77 50 72 57
R07 | 815 12 32 22 22 21 43 11 | 104 83 97 112 93 108 100
R08 | 1920 14 45 17 26 28 28 11 | 111 88 104 125 126 111 111
R09 | 2342 19 23 29 26 40 29 12 | 44 48 42 49 19 44 36
XR11 | 2455 15 17 23 15 --- 36 11 | 364 21 175 417 --- 402 208
R12 | 651 15 22 17 10 23 36 9 | 50 42 56 55 60 37 48
R13 | 1311 49 55 49 20 23 20 17 | 62 26 63 59 52 41 47
R14 | 645 12 24 15 13 23 26 8 | 44 36 54 50 48 44 44
R15 | 982 13 24 14 10 16 21 7 | 49 37 44 45 46 47 44
R16 | 1626 26 36 38 27 32 30 14 | 46 38 63 53 44 62 48
R17 | 1052 11 22 11 13 20 33 8 | 25 18 24 25 31 26 21
R18 | 2342 8 22 27 14 30 24 9 | 22 18 20 21 32 40 21
R19 | 1400 42 106 35 36 81 39 25 | 40 34 33 43 39 46 34
R20 | 2349 41 105 77 58 75 39 29 | 34 51 35 43 34 43 30
R21 | 1064 8 33 11 12 8 16 6 | 54 49 44 59 52 51 51
R22 | 3075 45 33 89 24 47 76 25 | 35 47 28 50 33 89 28
R24 | 1615 18 37 14 15 17 26 9 | 22 27 24 26 24 34 20
------+-----------------------------------------+-------------------------------------
RMS | 1774 26 48 37 26 36 33 |T 67 42 57 77 52 73 56
WRMS | 1774 22 37 29 19 33 27 |NE 67 42 57 77 52 73 56
MEDI | 1615 15 33 18 20 23 28 |MD 49 38 54 53 48 51 48
Table 3.2166.2 GPS week: 2166 Day: 2 MJD: 59408
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 879 39 62 58 42 42 22 19 | 63 28 54 62 50 49 44
R02 | 2333 12 40 10 31 18 16 9 | 47 24 46 70 49 35 46
R03 | 2605 10 31 8 15 14 24 7 | 76 58 74 78 71 73 72
XR04 | 598 20 34 14 --- 15 22 10 | 76 69 70 --- 87 84 77
R05 | 1550 11 32 14 13 23 29 9 | 55 44 57 54 51 71 54
R07 | 2203 13 30 14 17 26 41 11 | 75 61 70 83 65 87 73
R08 | 1013 18 39 17 11 14 50 12 | 79 62 68 78 74 107 77
R09 | 2532 24 18 34 19 37 26 12 | 51 48 53 52 33 45 41
XR11 | 3402 14 20 23 16 --- 25 10 | 342 30 178 438 --- 393 175
R12 | 744 14 37 14 16 17 20 8 | 72 63 68 65 68 69 66
R13 | 1142 33 58 31 34 51 25 16 | 62 39 54 67 70 43 53
R14 | 625 12 28 17 18 18 17 8 | 46 32 49 38 47 35 39
R15 | 949 19 23 8 14 14 24 7 | 57 43 48 43 48 40 45
R16 | 1646 27 40 47 15 38 25 14 | 48 38 85 66 49 45 55
R17 | 1464 8 36 12 19 11 17 7 | 28 30 28 29 31 34 27
R18 | 1454 20 34 30 12 18 19 9 | 27 23 32 31 29 35 26
R19 | 1505 25 82 41 55 33 27 19 | 42 43 25 39 49 48 28
R20 | 2956 47 134 56 33 55 32 25 | 35 75 40 43 26 26 30
R21 |14389 17 27 15 12 13 18 7 | 40 42 43 40 36 43 38
R22 | 1327 34 43 72 44 62 21 21 | 40 36 45 43 37 32 34
R24 | 1162 22 69 11 9 13 26 11 | 25 21 26 26 26 31 23
------+-----------------------------------------+-------------------------------------
RMS | 3692 24 52 33 26 31 27 |T 66 43 57 72 49 67 53
WRMS | 3692 20 41 21 21 25 25 |NE 66 43 57 72 49 67 53
MEDI | 1464 19 36 17 16 18 24 |MD 51 42 53 52 49 45 45
Table 3.2166.3 GPS week: 2166 Day: 3 MJD: 59409
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 804 39 54 43 42 37 35 18 | 71 32 48 74 49 52 50
R02 | 1674 12 47 14 18 20 26 9 | 64 34 58 69 71 73 61
R03 | 1438 10 33 13 14 18 17 7 | 91 82 89 93 99 89 90
XR04 | 854 13 31 17 --- 17 14 9 | 58 45 57 --- 62 57 53
R05 | 914 14 41 14 13 19 35 9 | 63 51 64 69 72 84 66
R07 | 3277 15 28 12 19 30 39 10 | 107 90 96 107 94 108 99
R08 | 897 11 35 12 17 18 24 8 | 111 96 103 117 109 115 108
R09 | 2196 31 11 33 14 42 30 13 | 65 44 57 52 32 62 47
XR11 |11252 35 29 --- 414 --- 56 29 | 344 45 --- 626 --- 336 293
R12 | 725 12 56 15 11 15 46 11 | 61 45 62 59 68 92 61
R13 | 1159 35 39 29 37 40 34 15 | 72 36 44 53 63 81 56
R14 | 787 8 21 17 16 15 22 7 | 49 39 56 40 51 61 47
R15 | 1291 15 18 11 16 24 32 8 | 57 45 52 40 59 44 47
R16 | 966 29 38 43 22 47 26 15 | 50 37 71 46 55 44 48
R17 | 947 13 30 13 12 18 20 7 | 36 32 37 35 40 34 33
R18 | 896 11 32 19 11 12 21 7 | 36 29 34 35 42 43 34
R19 | 2365 44 91 52 29 58 46 22 | 44 68 42 48 40 50 40
R20 | 1311 49 108 50 17 43 19 21 | 41 63 55 49 32 41 40
R21 | 998 22 27 23 17 27 24 10 | 53 53 47 58 53 47 49
R22 | 2729 44 26 69 49 58 52 23 | 43 49 46 40 36 62 35
R24 | 716 19 68 10 12 9 27 11 | 36 30 37 37 40 44 35
------+-----------------------------------------+-------------------------------------
RMS | 1552 26 48 31 23 32 32 |T 73 49 57 87 58 77 66
WRMS | 1552 19 39 21 19 27 32 |NE 73 49 57 87 58 77 66
MEDI | 998 15 33 17 17 20 27 |MD 58 45 55 52 53 61 49
Table 3.2166.4 GPS week: 2166 Day: 4 MJD: 59410
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 905 40 53 56 53 37 15 20 | 68 38 32 78 46 51 48
R02 | 1225 17 36 12 16 17 56 12 | 54 29 51 40 48 90 49
R03 | 733 13 39 11 13 18 21 8 | 70 48 61 68 73 66 64
XR04 | 1207 22 26 15 --- 27 18 11 | 60 54 58 --- 62 56 56
R05 | 1450 13 37 16 13 16 22 8 | 54 46 66 65 64 64 59
R07 | 3779 15 32 21 10 17 29 9 | 93 71 79 87 81 98 85
R08 | 993 12 34 14 18 14 24 8 | 91 71 90 100 94 87 89
R09 | 1842 24 14 19 23 50 24 12 | 66 51 57 60 27 59 51
XR11 | 7713 126 --- --- 146 --- 342 135 | 514 --- --- 636 --- 818 512
R12 | 675 8 38 12 10 16 31 8 | 65 51 66 68 60 72 63
R13 | 2095 22 36 37 30 35 62 16 | 69 51 61 77 65 116 70
R14 | 1118 14 22 15 22 16 39 9 | 37 30 53 35 53 72 44
R15 | 939 12 16 19 11 10 25 7 | 56 45 55 60 56 62 54
R16 | 1078 25 29 25 26 26 24 11 | 40 37 57 49 63 45 45
R17 | 710 7 33 6 17 14 21 7 | 31 27 39 39 38 31 33
R18 | 1237 16 32 18 13 18 17 8 | 30 29 30 28 33 30 27
R19 | 3409 41 126 61 41 63 36 26 | 38 41 36 49 42 37 35
R20 | 924 37 83 64 46 48 32 23 | 35 57 37 46 39 41 34
R21 | 819 17 31 15 8 18 14 7 | 31 32 40 35 34 28 31
R22 | 3109 49 56 60 47 70 47 24 | 52 66 50 51 66 75 49
R24 | 885 19 51 9 10 16 25 9 | 24 20 24 23 29 33 22
------+-----------------------------------------+-------------------------------------
RMS | 1738 24 49 32 26 32 32 |T 75 44 52 84 53 96 72
WRMS | 1738 20 37 24 17 26 28 |NE 75 44 52 84 53 96 72
MEDI | 1118 17 34 16 17 18 25 |MD 54 45 53 51 53 62 49
Table 3.2166.5 GPS week: 2166 Day: 5 MJD: 59411
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 938 50 48 51 47 40 20 19 | 56 36 25 51 32 37 33
R02 | 1526 13 34 10 22 22 16 8 | 47 26 35 49 39 46 40
R03 | 558 10 26 12 10 23 24 7 | 70 64 69 67 57 76 66
XR04 | 1060 17 27 19 --- 26 16 10 | 62 56 58 --- 60 62 58
R05 | 2504 19 37 19 17 23 26 10 | 52 36 47 38 50 50 43
R07 | 2901 10 35 25 14 14 18 8 | 98 78 81 95 90 102 91
R08 | 1302 13 41 23 10 28 28 10 | 93 76 88 93 105 112 94
R09 | 1981 13 15 19 21 36 24 10 | 48 40 55 56 33 51 45
R12 | 803 15 32 15 20 21 20 9 | 77 64 82 78 80 72 74
R13 | 1190 20 45 43 23 48 25 15 | 67 49 53 72 55 75 61
R14 | 1166 18 24 27 16 20 26 9 | 35 27 54 33 53 50 39
R15 | 796 10 22 12 12 14 18 6 | 47 31 37 38 48 53 41
R16 | 1866 17 27 29 24 40 45 14 | 34 37 45 45 37 38 33
R17 | 795 12 23 8 13 18 17 6 | 18 19 16 15 23 16 15
R18 | 1168 15 28 22 16 11 16 8 | 18 19 19 23 25 18 16
R19 | 1275 44 150 61 19 80 65 30 | 33 35 26 33 36 54 21
R20 | 875 45 78 71 63 36 27 24 | 37 45 32 37 22 25 22
R21 | 540 8 39 15 26 18 15 9 | 33 37 33 45 48 33 34
R22 | 3153 37 49 71 43 44 23 20 | 35 38 31 36 34 29 23
R24 | 1637 18 54 8 15 9 18 9 | 24 20 24 16 32 36 21
------+-----------------------------------------+-------------------------------------
RMS | 1600 24 51 35 26 33 27 |T 59 41 51 62 47 63 43
WRMS | 1600 22 36 26 16 32 22 |NE 59 41 51 62 47 63 43
MEDI | 1168 15 34 19 19 23 20 |MD 47 37 45 45 39 50 39
Table 3.2166.6 GPS week: 2166 Day: 6 MJD: 59412
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 722 53 60 52 36 24 27 19 | 82 36 34 69 50 57 49
R02 | 1931 8 39 12 22 17 21 9 | 69 40 60 77 62 73 64
R03 | 765 8 29 16 15 18 31 9 | 77 53 68 72 70 75 69
XR04 | 1330 17 29 12 --- 22 24 10 | 72 50 61 --- 72 71 65
R05 | 2314 16 35 27 20 20 25 10 | 68 66 94 86 69 72 73
R07 | 1419 13 33 18 14 12 22 8 | 100 75 80 102 94 100 93
R08 | 948 12 40 28 26 29 24 11 | 99 79 90 113 107 112 100
R09 | 1720 17 14 18 22 36 18 10 | 57 59 68 70 44 54 57
R12 | 901 17 35 16 22 13 25 9 | 85 78 96 98 93 82 88
R13 | 950 25 33 16 31 36 23 12 | 90 66 73 95 72 72 77
R14 | 1156 5 22 16 14 12 24 7 | 66 52 79 69 75 70 67
R15 | 741 10 20 11 13 16 16 6 | 81 64 73 80 73 73 74
R16 | 1376 22 17 34 22 30 20 11 | 58 49 79 60 61 50 58
R17 | 874 19 23 14 14 13 17 7 | 40 36 44 40 50 33 38
R18 | 1080 10 22 17 12 16 16 7 | 39 34 33 35 44 38 35
R19 | 1129 32 132 55 19 66 43 26 | 47 44 34 38 40 47 38
R20 | 892 52 61 57 36 46 37 21 | 40 42 46 57 60 35 39
R21 | 539 11 34 15 17 14 17 8 | 36 31 39 36 41 32 34
R22 | 1887 40 24 86 40 46 18 21 | 41 50 40 41 47 29 35
R24 | 1372 23 57 13 11 14 21 10 | 39 39 42 42 52 43 41
------+-----------------------------------------+-------------------------------------
RMS | 1283 25 46 34 23 29 24 |T 71 52 63 76 63 68 59
WRMS | 1283 20 34 24 17 28 24 |NE 71 52 63 76 63 68 59
MEDI | 1080 17 33 16 20 18 22 |MD 68 50 68 69 61 70 58
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