[IGSREPORT-28362] Wk 2186 IGLOS Final Orbits
acc
acc at igs.org
Fri Dec 17 02:54:01 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2186 (Nov 28, 2021 - Dec 04, 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 2.2186.
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:
igl2186[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2186 in the SP3 format.
igl21867.sum Combination Report for GPS Week 2186.
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 | -1.4 ns
1 | -2.1 ns
2 | 80.0 ns
3 | 108.0 ns
4 | 91.9 ns
5 | -4.6 ns
6 | -1.9 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 1.2186, 1a.2186).
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 2.2186.0-6)
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 3.2186.0-6).
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 2186 summary. (Nov 28, 2021 - Dec 04, 2021)
Table 1.2186.a GPS week : 2186 MJD: 59546.0-59552.0
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| -1 0 2 -1 -7 61 .09 23 18 | 18868 -1754 18521 208338
| 0 1 2 12 8 21 .02 | 4511 2278
emx n/a| 0 0 0 16 12 -38 -.03 45 32 | 32268 -706 3496 8540
| 2 0 1 28 10 50 .04 | 45964 2046
esx n/a| 1 0 3 -20 4 -37 -.10 37 26 | 22862 -1267 9193 73352
| 1 0 3 14 25 54 .02 | 42084 3018
gfz n/a| 0 1 2 -8 11 -27 -.07 29 17 | 0 -1584 18962 213799
| 1 0 2 29 15 48 .08 | 0 2570
grg n/a| 0 -3 -10 -6 0 13 .22 30 21 | 25959 -419 8149 75865
| 1 1 11 17 14 45 .04 | 46566 2988
iac n/a| 1 0 5 33 -10 -14 -.20 28 26 | 2879 -1376 18508 208478
| 3 1 3 53 19 103 .06 | 3940 1534
mcc n/a| 2 -4 9 90 58 1008 -1.03 200 200 | --- --- --- ---
| 6 8 9 84 156 1139 .44 | --- ---
Table 1.2186.b GPS week : 2186 MJD: 59546.0-59552.0
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 | 15 16 19 14 13 16 17 |
R02 | 6 5 6 6 8 8 7 |
R03 | 7 7 8 6 6 7 7 |
R04 | 8 8 11 7 9 10 9 |
R05 | 10 9 9 12 7 9 9 |
R07 | 5 6 6 9 7 8 5 |
R08 | 10 8 10 10 8 8 8 |
R09 | 8 7 8 7 9 8 7 |
R11 | 9 22 38 11 8 8 10 |
R12 | 8 7 7 10 9 8 10 |
R13 | 15 17 14 13 16 16 17 |
R14 | 8 7 7 10 9 10 8 |
R15 | 7 8 8 9 11 10 10 |
R16 | 12 14 12 12 12 16 12 |
R17 | 8 8 7 9 8 8 10 |
R18 | 9 9 8 10 11 12 11 |
R19 | 31 29 26 28 33 32 26 |
R20 | 20 19 20 18 22 28 25 |
R21 | 9 8 11 10 8 8 11 |
R22 | 26 29 32 28 26 26 26 |
R24 | 10 9 9 9 9 10 10 |
Table 1.2186.c GPS week : 2186 MJD: 59546.0-59552.0
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 2186 0 | 25 -10 -41 -1678 1332 -5278 85.8 1654 1654 | -1448 0
brd 2186 1 | 39 99 -5 -19 -1166 -3961 82.3 1556 1556 | -2140 0
brd 2186 2 | -30 -72 31 827 -359 4922 82.5 1499 1499 | 80030 0
brd 2186 3 | 45 -78 -66 1048 -32 4757 82.5 1509 1509 | 107949 0
brd 2186 4 | -36 36 25 -1362 -361 -1643 84.3 1804 1804 | 91924 0
brd 2186 5 | 116 30 42 -414 -438 -7470 82.5 1675 1675 | -4560 0
brd 2186 6 | -74 30 19 -189 -1020 -681 81.2 1562 1562 | -1938 0
-------------+------------------------------------------------------------+----------------
brd 2186 mean| 12 4 0 -255 -292 -1336 83.0 1608 1608 | 38545 0
brd 2186 sdev| 63 63 40 1016 819 4776 1.5 109 109 | 51863 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 2.2186.0 GPS week: 2186 Day: 0 MJD: 59546
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 1 5 0 -4 90 .07 21 19 | 16479 -678 3686 7599
emx n/a| 0 1 1 51 24 -33 -.05 46 29 | 9562 -837 3694 7873
esx n/a| -1 0 8 -37 8 -44 -.13 39 25 | 10589 -805 3668 9513
gfz n/a| 0 2 4 32 11 -65 .08 30 18 | 0 774 3672 7445
grg n/a| -2 -3 -21 -5 9 -43 .23 29 20 | -1485 -437 3649 6957
iac n/a| 4 0 2 -9 -4 8 -.23 21 21 | 942 -969 3652 7929
mcc n/a| 7 0 27 18 -69 1566 -.85 134 134 | --- --- --- ---
Table 2.2186.1 GPS week: 2186 Day: 1 MJD: 59547
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 4 14 -9 82 .11 26 24 | 15948 -3427 3418 8419
emx n/a| -3 0 -1 37 8 -64 .01 52 37 | -10250 -1545 3400 8665
esx n/a| 1 1 4 -17 21 -113 -.06 37 29 | -18703 -3459 3426 11388
gfz n/a| -1 1 1 -33 -11 -76 -.10 29 17 | 0 -3116 3500 8042
grg n/a| 0 -5 -15 -21 14 -22 .19 27 19 | -954 -2743 3446 7693
iac n/a| 1 0 7 37 16 100 -.17 19 14 | -8 -2083 3431 8858
mcc n/a| 12 0 9 150 -54 2498 -.46 151 151 | --- --- --- ---
Table 2.2186.2 GPS week: 2186 Day: 2 MJD: 59548
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 4 6 -15 68 .07 25 19 | 21698 -13 32191 431457
emx n/a| 0 1 0 -25 10 -48 -.03 46 36 | 65433 2224 3680 8255
esx n/a| 1 1 4 -5 30 -14 -.13 36 25 | 70371 2974 3672 10995
gfz n/a| -2 1 7 -24 22 -48 -.05 33 17 | 0 -196 33744 441496
grg n/a| 0 -3 -21 1 -8 -27 .16 25 20 | 78066 3722 3669 7810
iac n/a| 3 0 9 29 -34 33 -.11 23 23 | 6541 -2296 32175 431223
mcc n/a| -1 7 4 93 94 931 -1.42 233 233 | --- --- --- ---
Table 2.2186.3 GPS week: 2186 Day: 3 MJD: 59549
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 3 -10 -19 32 .09 23 16 | 26562 -3265 47204 508709
emx n/a| 0 -1 0 -17 21 26 -.05 41 33 | 97970 539 3141 8650
esx n/a| 1 1 5 -31 -2 7 -.12 33 24 | 27512 -3939 42551 457406
gfz n/a| 0 0 0 -10 1 25 -.09 28 15 | 0 -4423 47050 526200
grg n/a| -1 -2 -17 -17 -3 28 .25 30 21 | 107790 189 3127 7633
iac n/a| 2 -3 9 69 0 -90 -.19 29 28 | 9169 -2788 47171 508345
mcc n/a| 1 1 -2 115 240 -68 -1.62 203 203 | --- --- --- ---
Table 2.2186.4 GPS week: 2186 Day: 4 MJD: 59550
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 1 -22 -6 64 .11 22 16 | 21655 1245 36012 484932
emx n/a| -4 0 -1 29 14 -76 .01 43 31 | 75085 760 3324 8382
esx n/a| 2 1 0 -14 -5 -59 -.10 36 26 | 89076 2059 3872 7655
gfz n/a| 0 0 0 0 33 -12 -.16 26 15 | 0 1890 37743 496188
grg n/a| 0 -2 -1 -29 15 82 .21 33 23 | 2077 2025 36001 484767
iac n/a| 2 0 2 71 -33 -47 -.17 34 34 | 4740 1325 35999 484767
mcc n/a| -9 -13 12 -61 -162 628 -1.20 203 203 | --- --- --- ---
Table 2.2186.5 GPS week: 2186 Day: 5 MJD: 59551
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 -6 -7 43 .08 21 17 | 15552 -5242 3256 8102
emx n/a| 2 0 -1 27 16 29 -.09 42 30 | 3541 -3816 3253 8455
esx n/a| 2 0 0 -2 27 45 -.11 39 28 | -8198 -4905 3276 7550
gfz n/a| 0 2 1 25 0 48 -.10 32 21 | 0 -4686 3271 8045
grg n/a| 0 -2 8 22 -22 26 .27 33 23 | -1884 -5387 3277 7767
iac n/a| -3 1 0 -60 -20 -190 -.23 33 28 | -945 -2704 3268 8653
mcc n/a| 4 -13 8 137 224 2134 -1.17 300 300 | --- --- --- ---
Table 2.2186.6 GPS week: 2186 Day: 6 MJD: 59552
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 7 7 45 .12 22 17 | 14188 -903 3880 9150
emx n/a| 0 0 2 13 -9 -104 -.04 43 28 | -15460 -2270 3981 9500
esx n/a| 4 0 -1 -34 -44 -85 -.08 38 27 | -10612 -798 3888 8957
gfz n/a| -1 2 1 -46 22 -63 -.08 24 14 | 0 -1337 3759 9177
grg n/a| 1 -4 -4 5 -7 48 .20 31 23 | -1897 -308 3875 8430
iac n/a| -3 2 4 93 3 85 -.30 36 36 | -286 -122 3861 9576
mcc n/a| 1 -12 7 181 139 -628 -.51 175 175 | --- --- --- ---
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 3.2186.0 GPS week: 2186 Day: 0 MJD: 59546
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 688 37 27 45 38 27 17 --- 14 | 101 88 75 81 84 82 --- 83
R02 | 2148 7 11 17 11 11 17 239 5 | 46 42 44 45 51 43 101 43
R03 | 950 6 12 14 18 20 22 87 7 | 66 60 75 77 86 53 94 68
XR04 | 667 16 13 15 --- 13 17 --- 7 | 105 105 108 --- 109 92 --- 103
R05M | 747 24 19 21 18 16 23 83 9 | 62 64 62 50 53 45 94 53
R07 | 1251 8 12 11 17 13 10 --- 5 | 71 73 69 63 73 63 --- 68
R08M | 1170 23 20 20 28 15 24 --- 10 | 56 61 66 78 68 77 --- 66
R09E | 3984 16 21 10 21 13 19 --- 7 | 39 42 44 51 37 48 --- 41
XR11E | 5572 18 --- 22 15 20 16 --- 9 | 81 --- 88 94 46 91 --- 86
R12E | 952 13 31 12 20 14 15 --- 7 | 79 75 81 85 84 79 --- 79
R13E | 2189 29 44 33 40 32 27 --- 15 | 47 38 41 64 50 44 --- 42
R14E | 1565 13 26 21 16 13 16 --- 7 | 75 77 79 76 85 76 --- 76
R15E | 1482 9 31 11 16 15 17 87 7 | 122 130 120 128 123 117 69 121
R16E | 1522 17 38 25 40 20 26 --- 12 | 46 32 53 65 53 54 --- 47
R17 | 1126 10 33 15 16 14 15 --- 7 | 78 58 74 79 77 76 --- 74
R18M | 634 15 30 18 19 19 17 --- 8 | 64 58 82 73 74 77 --- 70
R19 | 1554 34 144 80 61 73 32 --- 31 | 127 70 80 140 120 128 --- 110
R20 | 1790 34 68 75 31 30 26 --- 20 | 113 71 64 107 107 103 --- 92
R21 | 1648 15 28 13 15 17 23 104 8 | 88 64 81 80 78 83 92 80
R22 | 1693 34 53 97 59 69 12 --- 25 | 58 104 125 70 67 66 --- 72
R24 | 1014 18 27 17 23 15 27 --- 9 | 85 67 83 85 82 79 --- 79
------+----------------------------------------------+------------------------------------------
RMS | 1653 21 46 39 30 29 21 134 |T 76 68 75 79 76 75 90 73
WRMS | 1653 19 29 25 18 20 21 134 |NE 83 71 80 82 85 78 95 78
MEDI | 1482 16 27 18 19 16 17 87 |MD 75 64 75 77 77 77 94 74
Table 3.2186.1 GPS week: 2186 Day: 1 MJD: 59547
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 627 51 41 46 37 21 17 --- 16 | 80 72 68 73 64 58 --- 64
R02 | 2360 7 15 16 7 9 12 273 5 | 50 53 58 53 54 48 198 51
R03 | 923 9 16 12 15 23 17 100 7 | 61 62 74 69 79 52 76 65
XR04 | 772 18 20 12 --- 12 19 --- 8 | 98 108 105 --- 105 93 --- 99
R05M | 988 24 25 20 23 20 9 107 9 | 64 60 69 64 52 55 92 58
R07 | 1144 12 17 11 12 9 14 --- 5 | 68 69 70 69 69 61 --- 66
R08M | 1055 25 20 18 22 12 11 --- 8 | 58 57 66 72 63 60 --- 61
R09E | 3476 12 14 10 20 15 14 --- 6 | 34 43 41 48 30 37 --- 37
XR11E | 8021 52 --- --- 37 38 26 --- 22 | 111 --- --- 185 92 161 --- 154
R12E | 1008 12 28 14 17 19 10 --- 7 | 106 100 105 110 103 102 --- 104
R13E | 1882 24 48 29 66 27 22 --- 16 | 65 58 66 108 70 66 --- 68
R14E | 1899 15 26 17 10 17 11 --- 7 | 90 95 96 96 92 90 --- 92
R15E | 782 10 30 23 20 11 12 78 7 | 150 157 160 150 149 148 107 151
R16E | 1413 15 51 31 49 19 19 --- 13 | 63 74 67 92 66 60 --- 65
R17 | 908 16 28 12 16 15 21 --- 8 | 49 51 50 49 51 35 --- 44
R18M | 529 14 28 26 17 15 16 --- 8 | 46 52 57 54 51 41 --- 49
R19 | 1310 54 150 72 28 68 23 --- 29 | 90 47 67 70 79 68 --- 70
R20 | 1747 38 84 58 38 18 20 --- 18 | 64 52 42 65 65 50 --- 53
R21 | 1163 19 32 9 18 19 14 111 8 | 54 43 58 48 47 49 77 49
R22 | 2181 46 88 101 49 65 43 --- 28 | 28 73 82 38 58 44 --- 42
R24 | 968 13 38 13 16 20 21 --- 9 | 51 55 52 54 57 46 --- 49
------+----------------------------------------------+------------------------------------------
RMS | 1556 26 52 37 29 27 19 151 |T 70 69 72 78 71 67 110 71
WRMS | 1556 24 37 29 17 19 14 151 |NE 61 61 65 57 66 54 117 58
MEDI | 1144 16 28 17 20 19 17 107 |MD 64 58 67 69 65 58 92 64
Table 3.2186.2 GPS week: 2186 Day: 2 MJD: 59548
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 686 46 41 62 42 25 22 --- 18 | 125 115 105 111 115 113 --- 112
R02 | 2225 6 11 10 20 9 18 290 6 | 73 69 71 72 77 72 240 72
R03 | 491 8 19 12 18 20 25 284 8 | 84 82 91 88 98 76 155 86
XR04 | 1028 18 18 14 --- 19 32 --- 11 | 123 125 125 --- 141 123 --- 127
R05M | 1692 16 21 19 17 10 27 66 8 | 87 89 89 91 86 77 73 85
R07 | 1030 15 16 13 11 9 17 272 6 | 97 100 101 95 101 90 182 97
R08M | 877 25 15 22 20 12 31 --- 10 | 91 91 93 98 99 106 --- 95
R09E | 3137 14 18 13 20 11 22 --- 7 | 66 68 72 71 67 65 --- 66
XR11E |11476 48 --- --- 78 --- 30 --- 37 | 86 --- --- 115 --- 108 --- 94
R12E | 910 10 28 13 14 12 16 --- 7 | 106 107 102 105 109 110 --- 105
R13E | 2009 20 38 35 56 19 20 --- 14 | 86 84 83 114 94 86 --- 88
R14E | 1071 12 26 20 14 12 17 --- 7 | 102 108 107 110 110 107 --- 107
R15E | 1050 11 30 18 22 16 16 278 8 | 101 103 109 117 104 108 145 106
R16E | 1894 17 33 20 41 25 21 --- 12 | 84 85 82 89 77 82 --- 80
R17 | 1030 12 27 16 9 10 18 --- 7 | 79 75 75 74 82 72 --- 75
R18M | 610 13 36 18 17 14 16 --- 8 | 74 71 78 82 84 81 --- 77
R19 | 1202 54 109 62 55 51 13 --- 26 | 122 120 102 118 108 104 --- 109
R20 | 855 42 85 59 36 27 21 --- 20 | 95 76 67 82 96 91 --- 82
R21 | 895 19 35 21 12 18 31 69 10 | 89 73 81 89 76 96 130 84
R22 | 2554 44 94 92 82 69 47 --- 31 | 76 110 97 93 81 73 --- 76
R24 | 915 7 40 12 15 20 21 --- 8 | 78 78 76 84 82 87 --- 80
------+----------------------------------------------+------------------------------------------
RMS | 1498 25 46 36 33 25 23 233 |T 91 91 90 94 94 91 154 90
WRMS | 1498 19 36 25 17 20 23 233 |NE 91 90 88 88 94 88 176 88
MEDI | 1030 16 28 18 20 16 21 272 |MD 87 85 89 91 94 90 145 86
Table 3.2186.3 GPS week: 2186 Day: 3 MJD: 59549
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 618 34 30 39 30 26 13 --- 13 | 79 69 47 65 62 66 --- 62
R02 | 3011 9 17 13 10 12 17 165 5 | 36 37 30 36 36 39 120 33
R03 | 454 9 19 10 9 14 17 259 5 | 43 39 47 55 62 50 89 48
XR04 | 958 11 11 15 --- 10 16 --- 6 | 55 56 48 --- 68 54 --- 55
R05M | 1460 32 20 24 23 18 30 76 11 | 46 35 42 37 32 31 61 30
R07 | 624 17 17 14 10 17 33 246 8 | 56 52 54 50 45 33 82 47
R08M | 744 16 16 13 8 23 43 --- 9 | 51 51 62 61 52 89 --- 59
R09E | 3546 15 20 15 14 18 15 --- 7 | 36 34 38 44 37 40 --- 35
XR11E | 1004 14 --- 17 21 --- 25 --- 11 | 108 --- 61 115 --- 112 --- 110
R12E | 1575 11 34 13 23 14 33 --- 9 | 38 34 35 45 40 46 --- 37
R13E | 1675 17 38 29 29 33 34 --- 13 | 32 18 30 58 51 43 --- 34
R14E | 1282 14 29 22 28 20 23 --- 10 | 36 32 45 53 38 44 --- 37
R15E | 576 12 30 12 26 14 16 290 8 | 173 169 171 172 178 181 111 173
R16E | 1110 26 32 24 30 24 17 --- 11 | 27 26 34 45 36 40 --- 30
R17 | 889 8 30 9 14 14 36 --- 8 | 53 38 53 46 48 75 --- 50
R18M | 547 10 44 21 9 13 31 --- 9 | 49 42 53 53 46 60 --- 48
R19 | 1173 34 101 69 72 53 46 --- 27 | 97 55 64 125 82 107 --- 86
R20 | 1055 50 55 51 19 33 29 --- 18 | 90 43 41 73 72 72 --- 64
R21 | 725 17 32 17 17 19 28 54 9 | 60 33 51 53 51 72 68 53
R22 | 2156 35 69 84 59 85 28 --- 28 | 42 62 68 38 46 32 --- 34
R24 | 820 13 44 15 8 11 25 --- 9 | 51 31 42 43 45 60 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 1508 23 41 33 28 30 29 203 |T 59 47 53 63 56 64 88 55
WRMS | 1508 16 33 24 15 21 28 203 |NE 58 44 49 57 55 59 89 51
MEDI | 1004 15 30 17 19 18 28 165 |MD 51 38 47 53 46 54 82 48
Table 3.2186.4 GPS week: 2186 Day: 4 MJD: 59550
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 632 30 31 30 18 37 22 --- 13 | 90 80 69 71 65 87 --- 75
R02 | 5086 8 13 14 20 22 29 116 8 | 52 49 53 63 45 45 99 50
R03 | 532 8 13 16 13 10 22 234 6 | 63 62 58 73 68 55 98 63
XR04 | 776 13 21 18 --- 16 24 --- 9 | 111 111 114 --- 116 113 --- 112
R05M | 1860 15 10 18 15 12 23 133 7 | 68 58 67 66 65 51 47 62
R07 | 1259 16 21 12 7 15 24 287 7 | 71 70 63 64 61 56 82 64
R08M | 1061 17 9 25 15 16 18 --- 7 | 62 56 72 63 60 72 --- 62
R09E | 3201 19 14 13 20 15 33 --- 8 | 43 39 43 45 44 35 --- 39
XR11E | 2116 17 --- 15 12 17 22 --- 8 | 41 --- 38 55 86 51 --- 48
R12E | 1059 9 30 10 24 18 29 --- 9 | 73 68 73 80 77 80 --- 74
R13E | 2027 21 37 24 41 39 44 --- 15 | 54 45 50 65 52 60 --- 49
R14E | 639 13 27 23 18 16 24 --- 8 | 68 65 74 75 75 72 --- 69
R15E | 872 19 34 17 22 12 37 262 10 | 116 114 111 120 111 105 63 112
R16E | 2219 23 30 22 41 21 12 --- 12 | 46 58 59 69 60 50 --- 52
R17 | 614 9 38 10 9 11 30 --- 8 | 56 50 47 52 55 49 --- 50
R18M | 583 12 42 29 11 15 36 --- 10 | 56 43 64 54 57 74 --- 56
R19 | 1661 39 125 80 52 71 84 --- 32 | 90 93 82 103 88 129 --- 89
R20 | 1244 30 61 73 35 61 37 --- 22 | 78 58 60 80 87 82 --- 69
R21 | 683 14 30 14 12 20 15 100 7 | 68 52 57 58 69 59 53 60
R22 | 1177 45 62 82 39 71 45 --- 26 | 51 65 82 55 49 44 --- 47
R24 | 805 15 34 15 12 21 23 --- 8 | 66 60 58 59 60 72 --- 61
------+----------------------------------------------+------------------------------------------
RMS | 1804 22 43 36 26 33 34 203 |T 67 64 66 68 69 68 73 64
WRMS | 1804 16 31 26 15 23 34 203 |NE 70 67 67 67 69 70 83 66
MEDI | 1061 16 30 18 18 17 24 133 |MD 66 58 63 64 65 60 63 62
Table 3.2186.5 GPS week: 2186 Day: 5 MJD: 59551
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 813 39 40 28 40 38 17 --- 15 | 121 124 121 128 115 113 --- 117
R02 | 3431 11 13 17 13 22 22 241 7 | 44 43 51 43 35 53 121 42
R03 | 568 7 12 13 10 12 31 246 6 | 53 50 59 60 52 42 177 51
XR04 | 1093 16 19 31 --- 14 16 --- 10 | 66 69 70 --- 62 67 --- 65
R05M | 1618 17 18 19 30 13 21 244 9 | 60 68 78 73 61 69 166 65
R07 | 1150 15 23 12 27 11 19 353 8 | 65 66 64 62 62 54 205 60
R08M | 1076 11 17 20 15 19 24 --- 7 | 60 61 64 57 62 59 --- 57
R09E | 2855 14 18 12 22 15 23 --- 7 | 34 38 37 42 38 34 --- 34
R11E | 3523 15 22 15 16 13 28 --- 8 | 67 17 39 75 65 78 --- 73
R12E | 1318 9 31 11 13 15 22 --- 7 | 104 98 104 110 104 96 --- 102
R13E | 1605 18 43 38 59 30 22 --- 16 | 67 70 79 95 77 65 --- 69
R14E | 797 9 26 21 16 20 39 --- 9 | 92 96 92 93 93 98 --- 91
R15E | 1201 9 31 16 24 12 40 459 10 | 159 166 158 148 160 179 129 159
R16E | 1673 33 42 24 49 27 41 --- 16 | 56 61 64 84 66 69 --- 60
R17 | 1111 5 36 12 15 16 15 --- 7 | 39 37 44 44 53 33 --- 40
R18M | 911 11 30 29 24 16 45 --- 11 | 32 34 39 37 35 43 --- 31
R19 | 1646 31 119 90 48 76 66 --- 31 | 58 74 72 62 68 79 --- 58
R20 | 1344 29 82 101 46 54 53 --- 27 | 63 64 47 91 98 95 --- 67
R21 | 806 17 29 10 8 9 27 160 8 | 50 52 52 50 51 38 111 45
R22 | 575 47 25 79 57 81 28 --- 26 | 41 73 57 59 72 45 --- 50
R24 | 946 17 42 12 21 18 27 --- 10 | 45 39 49 58 52 51 --- 46
------+----------------------------------------------+------------------------------------------
RMS | 1674 21 42 39 32 33 33 300 |T 65 66 68 73 70 69 151 65
WRMS | 1674 17 30 28 21 23 28 300 |NE 52 56 56 58 60 55 153 52
MEDI | 1150 15 29 19 22 16 27 244 |MD 60 64 64 62 62 65 129 60
Table 3.2186.6 GPS week: 2186 Day: 6 MJD: 59552
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 698 44 34 40 32 33 39 --- 17 | 135 126 122 121 115 114 --- 120
R02 | 875 7 16 21 8 13 30 178 7 | 54 50 63 52 48 57 114 52
R03 | 1171 13 14 13 9 10 26 132 6 | 66 63 76 76 70 83 193 70
XR04 | 1036 13 13 16 --- 12 32 --- 9 | 84 81 81 --- 77 77 --- 79
R05M | 1008 13 19 21 22 17 33 134 9 | 66 62 71 66 59 58 153 62
R07 | 892 7 10 13 10 11 19 305 5 | 72 73 74 63 66 58 194 67
R08M | 958 9 10 27 13 17 25 --- 7 | 73 67 82 73 64 75 --- 71
R09E | 2571 14 15 12 14 14 21 --- 6 | 26 23 23 33 22 31 --- 23
XR11E | 3911 17 --- 22 14 12 37 --- 10 | 59 --- 34 68 64 75 --- 64
R12E | 1002 9 34 16 20 24 30 --- 9 | 121 121 120 122 124 116 --- 120
R13E | 3644 34 39 45 35 39 35 --- 17 | 73 58 71 90 88 77 --- 71
R14E | 1066 14 24 15 19 14 19 --- 7 | 112 118 111 115 115 119 --- 114
R15E | 835 12 32 16 11 18 43 142 9 | 103 103 101 105 107 114 208 104
R16E | 1723 16 32 23 33 28 31 --- 12 | 54 49 55 62 60 61 --- 53
R17 | 1256 14 30 21 16 14 35 --- 9 | 62 43 55 59 64 75 --- 58
R18M | 2613 15 22 27 16 20 45 --- 10 | 77 73 89 79 80 86 --- 79
R19 | 1884 32 109 65 35 68 47 --- 26 | 96 75 53 114 97 110 --- 85
R20 | 986 40 84 91 24 50 49 --- 25 | 113 46 59 99 114 110 --- 87
R21 | 752 18 28 14 12 15 51 49 10 | 76 60 65 69 78 61 81 67
R22 | 830 33 69 83 53 67 52 --- 26 | 37 87 95 58 52 54 --- 49
R24 | 1057 18 47 13 12 15 24 --- 10 | 71 49 60 66 70 77 --- 65
------+----------------------------------------------+------------------------------------------
RMS | 1562 22 43 38 24 31 36 174 |T 77 71 74 79 77 80 157 74
WRMS | 1562 17 28 27 14 23 36 174 |NE 73 62 68 72 73 76 145 67
MEDI | 1036 14 28 21 16 17 33 134 |MD 73 63 71 69 70 77 153 70
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