[IGSREPORT-27125] Wk 2093 IGLOS Final Orbits
acc
acc at igs.org
Mon Mar 9 01:32:18 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2093 (Feb 16, 2020 - Feb 22, 2020)
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 2.2093.
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:
igl2093[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2093 in the SP3 format.
igl20937.sum Combination Report for GPS Week 2093.
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 | -4.6 ns
1 | -3.5 ns
2 | -4.7 ns
3 | -3.3 ns
4 | -3.6 ns
5 | -5.2 ns
6 | -3.4 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 1.2093, 1a.2093).
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 2.2093.0-6)
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 3.2093.0-6).
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 2093 summary. (Feb 16, 2020 - Feb 22, 2020)
Table 1.2093.a GPS week : 2093 MJD: 58895.0-58901.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -1 0 -22 55 .03 19 17 | 20015 351 2995 7853
| 0 0 2 13 16 15 .02 | 385 1579
cof n/a| 0 0 -1 14 -10 53 .03 23 20 | 20005 358 2992 7853
| 1 1 1 20 25 32 .03 | 383 1579
emx n/a| 0 0 0 23 0 6 .02 31 30 | -8363 425 2982 7975
| 1 1 2 21 14 38 .05 | 8913 1057
esx n/a| 0 1 -1 3 -5 -47 .05 30 28 | -905 768 2996 9845
| 0 1 1 15 17 30 .04 | 8553 1373
gfz n/a| 0 -1 2 -19 -5 -65 .17 23 19 | 0 154 3044 7531
| 0 0 2 36 24 40 .05 | 0 1377
grg n/a| 1 0 3 -53 29 30 -.41 31 24 | -4095 181 3001 7121
| 1 0 5 19 12 52 .06 | 385 1464
iac n/a| 0 0 1 27 16 -17 -.01 19 17 | -2593 -118 2997 8037
| 1 0 1 19 35 43 .05 | 640 1165
mcc n/a| 3 7 -6 126 -8 -306 -.38 170 170 | --- --- --- ---
| 8 6 19 136 117 693 .39 | --- ---
Table 1.2093.b GPS week : 2093 MJD: 58895.0-58901.0
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 18 14 17 23 27 |
R02 | 6 7 8 6 7 8 7 |
R03 | 7 7 8 8 7 6 6 |
R04 | 9 8 8 9 9 8 6 |
R05 | 8 9 8 10 8 9 7 |
R07 | 9 6 6 6 7 8 9 |
R08 | 9 7 8 9 8 9 7 |
R09 | 8 9 8 7 7 8 6 |
R11 | 6 5 6 5 6 6 5 |
R12 | 8 9 8 9 10 8 10 |
R13 | 15 17 16 16 15 18 15 |
R14 | 8 8 7 6 8 6 7 |
R15 | 9 6 6 8 8 8 6 |
R16 | 15 14 11 11 14 12 15 |
R17 | 9 10 11 9 10 11 10 |
R18 | 9 7 7 6 7 8 8 |
R19 | 19 21 20 19 21 21 21 |
R20 | 18 17 20 18 16 17 16 |
R21 | 12 12 10 11 11 9 10 |
R22 | 11 10 9 10 11 10 9 |
R23 | 7 9 12 11 8 8 7 |
R26 | 20 16 21 16 12 18 11 |
Table 1.2093.c GPS week : 2093 MJD: 58895.0-58901.0
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 2093 0 | -32 -52 103 588 2206 -37 81.3 1373 1373 | -4630 0
brd 2093 1 | -18 -2 105 -331 134 1385 81.9 1442 1442 | -3530 0
brd 2093 2 | 96 -37 129 518 548 1962 83.8 1689 1689 | -4650 0
brd 2093 3 | 48 28 101 -1469 -442 3131 84.1 1787 1787 | -3291 0
brd 2093 4 | -26 61 118 -736 286 2470 83.0 1750 1750 | -3617 0
brd 2093 5 | -71 40 106 85 2635 3991 81.7 1615 1615 | -5250 0
brd 2093 6 | 3 22 103 990 507 1746 81.7 1401 1401 | -3367 0
-------------+------------------------------------------------------------+----------------
brd 2093 mean| 0 8 109 -50 839 2092 82.5 1579 1579 | -4047 0
brd 2093 sdev| 56 41 10 855 1135 1290 1.1 172 172 | 778 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 2.2093.0 GPS week: 2093 Day: 0 MJD: 58895
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 -6 -27 47 .01 19 18 | 19784 -637 3068 7341
cof n/a| 1 0 -3 34 -27 71 .01 22 22 | 19771 -625 3067 7343
emx n/a| 3 0 -4 2 -14 2 .04 31 31 | -12973 218 3060 7512
esx n/a| -1 1 -3 -5 11 -8 .07 32 33 | -12687 -844 3073 9476
gfz n/a| -1 -1 1 35 -44 -20 .25 21 19 | 0 -603 3154 7205
grg n/a| 0 0 13 -43 57 -40 -.48 29 27 | -3992 -1160 3090 7216
iac n/a| 0 0 2 -3 25 -18 -.07 19 17 | -2402 -909 3076 7423
mcc n/a| 8 -1 17 -97 192 -740 .26 156 156 | --- --- --- ---
Table 2.2093.1 GPS week: 2093 Day: 1 MJD: 58896
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 0 6 -44 67 .06 20 19 | 19812 1171 3037 7892
cof n/a| 0 0 0 15 -34 30 .01 21 20 | 19799 1183 3024 7887
emx n/a| 0 0 -1 2 -5 -11 -.05 29 29 | -14902 773 3013 8047
esx n/a| 1 2 -3 -13 -28 -58 .01 28 27 | -1908 1038 3027 9366
gfz n/a| 0 0 -1 -6 -1 -50 .16 20 16 | 0 463 3056 7779
grg n/a| 1 0 5 -40 28 81 -.33 36 29 | -3635 529 3065 7393
iac n/a| -1 0 2 41 53 -10 -.04 20 18 | -2910 818 3045 8064
mcc n/a| 9 8 -30 99 -71 -646 -.30 120 120 | --- --- --- ---
Table 2.2093.2 GPS week: 2093 Day: 2 MJD: 58897
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -2 0 -26 67 .01 17 17 | 19723 -1588 2884 8928
cof n/a| -1 0 -2 -16 -25 54 .06 22 22 | 19726 -1597 2885 8926
emx n/a| -2 0 3 8 -15 6 .01 30 30 | -20811 -941 2871 9065
esx n/a| 0 0 0 -4 -21 -28 .12 31 26 | 4193 -701 2896 10394
gfz n/a| 0 0 2 -35 18 -109 .14 23 20 | 0 -1418 2948 8634
grg n/a| 2 0 1 -33 22 26 -.38 33 24 | -3970 -1390 2881 8007
iac n/a| 1 0 0 33 46 -21 -.04 19 17 | -2627 -958 2883 9127
mcc n/a| 6 17 -13 345 5 -342 -.84 172 172 | --- --- --- ---
Table 2.2093.3 GPS week: 2093 Day: 3 MJD: 58898
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 -8 -19 53 .04 18 15 | 19914 450 3059 8263
cof n/a| 3 0 0 22 25 102 .07 23 19 | 19895 461 3058 8270
emx n/a| 0 -1 0 18 15 56 .09 34 34 | -3246 14 3051 8402
esx n/a| 0 0 -1 31 6 -20 .10 27 21 | 8608 1174 3053 10650
gfz n/a| 0 0 2 -41 10 -88 .19 21 22 | 0 685 3094 7769
grg n/a| 0 0 4 -46 22 36 -.47 26 21 | -3683 896 3044 7347
iac n/a| 0 0 0 24 -4 -64 -.02 19 17 | -2264 232 3057 8412
mcc n/a| -10 -2 14 166 -129 308 -.57 168 168 | --- --- --- ---
Table 2.2093.4 GPS week: 2093 Day: 4 MJD: 58899
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 26 10 59 .00 19 17 | 20773 1499 2981 6832
cof n/a| 0 -3 -3 24 28 33 .05 21 19 | 20765 1507 2979 6829
emx n/a| 1 -2 -1 52 24 -8 .08 34 29 | -10930 1117 2990 6878
esx n/a| 0 3 0 11 -4 -66 .04 30 28 | -10317 1555 2982 9021
gfz n/a| 0 -1 3 -47 5 -56 .18 24 19 | 0 1261 3007 6465
grg n/a| 1 0 6 -88 26 12 -.36 26 21 | -4242 1106 2981 5889
iac n/a| -3 -1 0 26 -41 -7 -.01 18 17 | -1543 672 2987 7027
mcc n/a| -7 11 8 206 48 959 -.80 265 265 | --- --- --- ---
Table 2.2093.5 GPS week: 2093 Day: 5 MJD: 58900
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -1 -13 -23 25 .04 20 16 | 20300 -1201 2965 8033
cof n/a| -1 1 0 -9 -16 6 -.01 21 18 | 20280 -1184 2967 8038
emx n/a| 0 0 -1 32 -1 -53 -.00 31 31 | 836 -439 2930 8145
esx n/a| 1 0 0 12 15 -96 .00 30 30 | -2830 94 2956 9884
gfz n/a| -1 -1 6 -63 8 -117 .09 26 18 | 0 -1480 2998 7607
grg n/a| 1 0 -1 -54 30 111 -.44 32 25 | -4629 -1182 2976 7136
iac n/a| -1 0 1 55 -6 63 .02 19 17 | -2778 -1939 2959 8261
mcc n/a| 6 7 -12 75 -142 -734 -.30 139 139 | --- --- --- ---
Table 2.2093.6 GPS week: 2093 Day: 6 MJD: 58901
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 0 -6 -26 68 .04 23 16 | 19804 2765 2977 7682
cof n/a| 0 2 0 32 -19 75 .03 28 21 | 19802 2764 2969 7683
emx n/a| 0 1 0 48 2 55 -.01 26 26 | 3484 2238 2961 7779
esx n/a| 0 2 -2 -4 -17 -55 .03 31 29 | 8603 3061 2985 10126
gfz n/a| 1 -2 0 19 -33 -17 .17 24 18 | 0 2171 3057 7259
grg n/a| 2 0 -2 -69 21 -15 -.40 36 22 | -4518 2473 2976 6862
iac n/a| -1 -1 3 11 42 -67 .08 20 17 | -3631 1255 2974 7951
mcc n/a| 9 7 -28 86 35 -950 -.15 169 169 | --- --- --- ---
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 3.2093.0 GPS week: 2093 Day: 0 MJD: 58895
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1163 22 36 50 34 35 34 27 --- 14 | 127 128 124 125 128 124 136 --- 126
R02E | 1405 8 10 23 9 11 10 17 126 6 | 47 47 45 54 61 49 53 139 50
R03E | 1280 12 12 29 10 12 14 11 198 6 | 64 67 59 63 65 70 61 127 63
XR04E | 2149 11 12 27 16 --- 19 19 --- 9 | 77 80 73 76 --- 80 86 --- 79
R05E | 936 15 21 25 12 16 16 14 --- 7 | 122 120 113 118 114 120 118 --- 117
R07E | 634 9 9 27 17 28 16 11 --- 8 | 122 125 121 120 134 116 120 --- 122
R08E | 1460 15 13 31 25 21 22 11 --- 9 | 74 76 71 77 80 66 73 --- 72
R09 | 683 9 21 10 18 20 19 19 --- 7 | 13 18 11 28 30 12 20 --- 14
R11 | 762 7 13 10 14 14 23 13 184 6 | 43 49 39 39 48 51 41 104 42
R12 | 1187 19 24 18 22 14 7 15 --- 7 | 73 75 62 52 66 67 71 --- 65
R13 | 1958 30 43 29 51 34 46 15 --- 15 | 55 59 45 33 47 49 37 --- 40
R14 | 1205 24 21 12 18 23 11 6 --- 8 | 45 46 36 33 35 31 33 --- 34
R15 | 1844 9 14 12 39 16 14 21 --- 8 | 59 62 53 39 52 60 58 --- 52
R16 | 651 20 19 57 22 19 57 25 --- 15 | 40 44 39 54 51 62 41 --- 44
R17 | 672 10 13 28 33 13 30 13 --- 9 | 51 51 39 36 53 62 54 --- 48
R18 | 736 21 22 31 10 19 17 17 --- 8 | 31 30 29 36 45 44 41 --- 36
R19 | 1984 34 33 49 79 24 26 36 --- 19 | 62 60 48 36 65 52 68 --- 51
R20 | 1333 42 39 46 36 30 57 28 --- 17 | 40 52 34 43 55 39 46 --- 40
R21 | 744 7 13 28 44 13 45 23 94 12 | 57 57 41 38 61 74 69 80 56
R22 | 3131 10 12 36 36 25 15 18 --- 10 | 52 60 38 42 70 62 62 --- 54
R23 | 833 16 15 17 20 13 16 12 --- 7 | 23 25 26 35 35 34 32 --- 27
XR26 | ---- 19 73 --- --- --- --- 20 --- 19 | 30 76 --- --- --- --- 32 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1373 19 22 31 32 21 29 19 156 |T 59 63 54 56 64 63 61 112 57
WRMS | 1373 18 22 31 33 19 27 17 156 |NE 44 50 38 38 50 49 47 92 42
MEDI | 1187 15 15 28 22 19 19 17 126 |MD 52 59 45 42 55 62 54 104 50
Table 3.2093.1 GPS week: 2093 Day: 1 MJD: 58896
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1253 30 29 41 29 40 52 25 --- 16 | 121 121 113 124 116 112 133 --- 117
R02E | 867 7 15 24 15 19 16 15 165 7 | 41 43 38 48 51 45 37 99 42
R03E | 809 8 8 25 11 16 12 13 91 6 | 47 47 47 49 54 52 53 94 49
XR04E | 2915 12 13 23 17 --- 17 15 --- 8 | 58 58 60 63 --- 66 63 --- 61
R05E | 1579 11 14 40 13 14 19 17 --- 9 | 91 88 89 82 80 93 91 --- 86
R07E | 630 8 11 22 10 12 17 12 --- 6 | 91 91 93 87 95 84 91 --- 90
R08E | 972 8 11 25 10 17 18 13 --- 7 | 58 58 60 60 61 65 64 --- 59
R09 | 777 16 23 12 11 23 40 15 --- 8 | 18 23 13 16 29 34 21 --- 15
R11 | 927 9 9 13 11 7 15 12 95 5 | 31 35 28 40 38 41 28 45 32
R12 | 1060 23 18 17 35 10 16 14 --- 9 | 53 41 46 40 46 55 53 --- 47
R13 | 2949 42 28 19 33 35 68 24 --- 16 | 35 42 34 21 33 33 28 --- 25
R14 | 656 23 23 14 11 18 15 12 --- 7 | 24 21 25 21 25 25 21 --- 20
R15 | 1161 12 15 12 18 9 19 9 --- 5 | 36 36 30 33 30 38 31 --- 31
R16 | 857 21 26 43 25 19 58 25 --- 13 | 30 28 22 40 38 52 33 --- 29
R17 | 970 9 8 28 30 13 16 25 --- 9 | 31 30 26 29 32 36 36 --- 29
R18 | 739 12 13 18 12 10 30 15 --- 7 | 22 24 20 27 29 35 21 --- 21
R19 | 923 39 38 59 66 34 62 33 --- 21 | 39 46 57 50 49 32 43 --- 38
R20 | 1102 37 41 49 24 17 75 27 --- 17 | 24 32 24 37 38 30 40 --- 28
R21 | 503 9 12 26 46 21 9 30 116 11 | 29 31 28 21 37 26 38 59 28
R22 | 3493 7 11 25 42 15 24 15 --- 10 | 31 29 30 28 35 36 30 --- 29
R23 | 2226 14 19 18 34 16 20 16 --- 9 | 18 22 25 28 31 25 29 --- 23
XR26 | ---- 15 81 --- --- --- --- 17 --- 16 | 26 82 --- --- --- --- 31 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1442 20 21 29 28 20 36 20 120 |T 43 46 43 44 47 48 46 74 42
WRMS | 1442 19 20 29 27 16 29 18 120 |NE 29 34 29 30 35 35 32 52 28
MEDI | 970 12 15 24 18 16 19 15 95 |MD 31 36 30 40 38 38 36 59 29
Table 3.2093.2 GPS week: 2093 Day: 2 MJD: 58897
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 851 28 17 45 35 57 52 27 --- 18 | 199 201 192 199 214 179 200 --- 197
R02E | 1312 9 16 26 13 19 21 12 84 7 | 32 34 29 29 41 27 32 80 30
R03E | 763 7 9 29 12 17 17 15 148 7 | 49 50 43 53 52 46 53 73 49
XR04E | 2007 9 12 22 16 --- 12 17 --- 7 | 46 42 40 47 --- 46 49 --- 44
R05E | 2242 13 14 22 10 21 18 13 --- 7 | 66 64 65 66 69 72 67 --- 66
R07E | 1282 8 9 17 10 17 13 10 307 5 | 71 75 73 77 72 72 72 112 72
R08E | 1169 12 11 19 20 22 21 15 --- 8 | 40 43 41 45 42 39 46 --- 40
R09 | 1300 11 11 8 21 17 18 26 --- 8 | 17 19 14 24 23 17 39 --- 18
R11 | 845 9 12 13 13 19 8 13 109 6 | 36 37 33 28 35 30 27 39 30
R12 | 799 9 30 19 24 20 13 17 --- 7 | 56 72 48 45 65 55 61 --- 55
R13 | 4185 36 49 31 48 22 48 18 --- 15 | 48 61 41 36 47 37 42 --- 37
R14 | 986 13 16 11 17 16 13 22 --- 7 | 35 34 28 27 23 30 42 --- 30
R15 | 695 13 14 11 21 13 9 13 --- 6 | 46 45 36 33 38 41 38 --- 38
R16 | 1108 22 24 13 20 29 46 10 --- 11 | 28 34 46 37 27 48 34 --- 30
R17 | 1024 8 13 26 44 28 14 17 --- 10 | 38 37 30 34 47 37 42 --- 36
R18 | 2243 14 14 19 12 13 21 16 --- 7 | 26 30 28 31 33 33 29 --- 28
R19 | 1910 34 42 57 70 21 47 36 --- 19 | 41 50 33 40 41 43 44 --- 31
R20 | 1326 19 38 71 41 23 75 32 --- 19 | 28 30 27 37 46 42 57 --- 34
R21 | 481 8 9 25 36 18 9 24 112 9 | 42 43 39 34 47 35 53 43 41
R22 | 2645 9 12 23 38 18 23 14 --- 9 | 37 39 34 24 40 39 32 --- 33
R23 | 2000 20 24 24 30 14 52 11 --- 11 | 22 26 24 34 27 42 20 --- 20
XR26 | ---- 18 27 --- --- --- --- 24 --- 21 | 43 41 --- --- --- --- 32 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1688 17 22 30 31 23 33 19 172 |T 47 50 44 46 51 48 50 69 45
WRMS | 1688 17 22 30 26 20 24 17 172 |NE 36 39 32 33 38 37 39 41 33
MEDI | 1282 12 14 22 21 19 18 16 112 |MD 40 41 36 36 41 41 42 73 35
Table 3.2093.3 GPS week: 2093 Day: 3 MJD: 58898
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1342 20 24 51 33 36 18 32 --- 14 | 129 133 130 148 158 130 122 --- 134
R02E | 1874 9 17 24 9 13 12 9 108 5 | 34 35 35 37 39 36 37 74 35
R03E | 1109 10 12 33 13 24 15 14 145 8 | 40 44 37 43 55 46 45 53 43
XR04E | 1371 11 17 29 14 --- 25 15 --- 9 | 38 37 35 38 --- 40 39 --- 36
R05E | 471 13 13 24 22 26 25 17 --- 9 | 38 40 33 45 46 44 41 --- 38
R07E | 1171 11 11 21 11 17 12 8 285 6 | 46 45 39 52 62 40 48 85 47
R08E | 1521 13 16 28 16 19 26 16 --- 8 | 33 30 31 35 33 35 30 --- 30
R09 | 1262 12 17 14 13 13 19 18 --- 7 | 11 12 14 18 21 18 25 --- 12
R11 | 1671 6 8 10 13 12 11 9 102 4 | 31 33 32 30 37 31 27 37 30
R12 | 749 11 11 25 25 22 18 19 --- 9 | 47 41 37 40 61 32 60 --- 46
R13 | 4615 40 42 48 44 23 38 10 --- 15 | 54 58 37 29 50 33 45 --- 41
R14 | 1276 16 16 10 12 9 13 13 --- 5 | 40 40 33 32 32 28 29 --- 32
R15 | 883 15 19 17 16 13 18 22 --- 7 | 50 53 46 37 37 53 37 --- 42
R16 | 1185 19 21 34 19 23 33 16 --- 10 | 32 34 37 38 32 35 22 --- 29
R17 | 621 10 12 27 28 22 11 17 --- 8 | 39 38 30 32 46 35 42 --- 36
R18 | 2840 14 14 15 13 14 10 9 --- 5 | 27 28 23 26 31 29 29 --- 25
R19 | 2431 26 36 56 65 26 30 43 --- 18 | 44 51 34 30 52 45 61 --- 40
R20 | 1926 26 44 76 17 13 73 16 --- 18 | 40 58 35 39 42 42 32 --- 35
R21 | 499 8 13 28 38 34 16 19 128 11 | 47 51 38 40 68 48 61 42 49
R22 | 1843 11 10 28 38 19 9 20 --- 9 | 48 47 35 46 54 50 47 --- 45
R23 | 1268 29 42 22 13 26 31 15 --- 10 | 23 36 20 27 41 39 25 --- 22
XR26 | ---- 14 48 --- --- --- --- 17 --- 15 | 17 50 --- --- --- --- 21 --- 16
------+---------------------------------------------------+-----------------------------------------------
RMS | 1786 18 23 34 27 21 26 19 168 |T 41 45 37 41 49 42 42 58 39
WRMS | 1786 15 19 34 21 22 21 17 168 |NE 36 42 32 33 43 37 37 39 33
MEDI | 1276 13 16 27 16 19 18 16 128 |MD 39 40 35 37 42 39 37 53 36
Table 3.2093.4 GPS week: 2093 Day: 4 MJD: 58899
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1167 29 27 54 38 45 25 33 --- 16 | 163 167 156 152 147 163 172 --- 158
R02E | 2243 11 14 24 9 19 19 12 158 7 | 30 30 27 29 37 31 35 145 29
R03E | 539 10 17 25 13 15 16 14 202 7 | 38 39 34 36 45 32 42 118 36
XR04E | 876 9 9 29 11 --- 19 17 --- 8 | 42 40 38 42 --- 43 47 --- 42
R05E | 586 12 14 33 9 20 21 12 --- 8 | 54 58 56 66 62 67 62 --- 60
R07E | 696 10 8 23 11 18 16 9 510 6 | 65 67 71 65 62 56 63 214 62
R08E | 2074 11 11 26 15 17 21 14 --- 7 | 40 40 37 43 43 36 36 --- 37
R09 | 808 13 16 18 12 14 15 17 --- 6 | 13 17 16 18 29 21 30 --- 18
R11 | 2134 9 10 12 13 10 11 16 94 5 | 27 31 29 33 30 30 36 36 28
R12 | 1930 22 25 28 26 17 18 22 --- 10 | 52 56 53 49 52 40 64 --- 49
R13 | 4211 33 45 37 31 43 37 15 --- 15 | 50 63 50 41 64 47 48 --- 47
R14 | 1233 18 25 16 13 9 27 16 --- 7 | 38 43 36 36 34 16 30 --- 30
R15 | 826 18 19 21 26 12 13 12 --- 7 | 39 40 38 26 30 23 29 --- 29
R16 | 1538 27 25 47 24 28 45 17 --- 14 | 30 36 52 38 36 30 24 --- 28
R17 | 702 12 9 24 36 22 27 15 --- 10 | 35 33 30 23 29 41 31 --- 28
R18 | 1764 8 8 18 18 17 15 11 --- 6 | 24 24 22 31 24 24 21 --- 19
R19 | 2474 28 36 79 74 41 28 31 --- 21 | 42 42 43 34 66 35 59 --- 41
R20 | 2501 37 34 44 19 22 58 18 --- 15 | 28 38 48 38 47 36 38 --- 33
R21 | 466 6 9 27 48 23 18 17 136 11 | 38 38 29 26 48 44 47 28 38
R22 | 1263 6 9 27 46 17 16 26 --- 11 | 38 41 28 28 48 45 54 --- 40
R23 | 631 10 14 13 31 17 15 13 --- 7 | 17 21 27 34 28 19 21 --- 20
XR26 | ---- 12 33 --- --- --- --- 12 --- 12 | 12 30 --- --- --- --- 25 --- 17
------+---------------------------------------------------+-----------------------------------------------
RMS | 1750 19 21 34 30 24 26 18 265 |T 41 45 43 42 48 41 46 108 40
WRMS | 1750 17 19 29 28 19 21 17 265 |NE 32 36 35 32 40 32 37 32 31
MEDI | 1233 12 14 26 19 17 19 15 158 |MD 38 39 37 36 43 36 36 118 33
Table 3.2093.5 GPS week: 2093 Day: 5 MJD: 58900
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1064 38 34 40 44 75 64 40 --- 22 | 105 112 107 119 122 127 125 --- 108
R02E | 3695 9 11 26 10 22 19 16 175 7 | 43 41 42 44 51 42 46 174 43
R03E | 1399 11 13 24 9 16 14 11 95 6 | 45 47 43 50 51 48 40 163 44
XR04E | 1240 7 14 19 10 --- 28 14 --- 8 | 71 76 70 69 --- 74 68 --- 70
R05E | 1664 15 16 28 11 25 19 14 --- 8 | 105 106 109 107 108 106 100 --- 104
R07E | 1336 10 12 24 14 20 17 15 159 7 | 97 99 101 91 95 97 94 198 95
R08E | 2689 15 17 23 13 24 22 18 --- 8 | 81 83 85 86 94 74 72 --- 80
R09 | 665 17 17 23 8 18 10 24 --- 8 | 29 35 35 30 42 26 37 --- 29
R11 | 1230 6 12 13 19 14 15 12 143 6 | 44 47 45 43 43 43 44 64 42
R12 | 1989 10 17 18 29 16 23 9 --- 7 | 66 69 64 63 63 76 64 --- 64
R13 | 2146 44 34 38 43 37 55 19 --- 17 | 58 58 69 59 63 58 58 --- 57
R14 | 1134 16 14 14 18 11 17 9 --- 6 | 47 46 48 42 50 42 49 --- 46
R15 | 658 14 16 21 15 8 15 21 --- 7 | 48 52 51 55 47 49 38 --- 45
R16 | 1135 23 25 34 24 26 31 21 --- 11 | 43 40 46 43 43 42 38 --- 37
R17 | 847 11 14 28 37 28 26 10 --- 10 | 42 46 46 42 49 40 32 --- 38
R18 | 881 13 16 19 18 16 18 17 --- 7 | 41 43 41 34 44 37 39 --- 38
R19 | 1811 26 37 70 77 31 43 31 --- 21 | 52 63 58 45 53 59 56 --- 48
R20 | 1510 30 35 53 19 18 71 21 --- 16 | 39 48 48 48 45 32 37 --- 38
R21 | 450 8 8 27 29 10 21 19 106 8 | 46 45 47 43 45 38 42 90 42
R22 | 1560 14 14 21 39 11 23 20 --- 10 | 49 50 45 41 44 44 36 --- 41
R23 | 644 18 21 14 23 23 16 10 --- 8 | 45 45 40 38 40 36 33 --- 36
XR26 | ---- 18 45 --- --- --- --- 16 --- 17 | 54 65 --- --- --- --- 46 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1615 20 21 31 30 26 32 19 139 |T 56 59 59 56 59 56 54 137 54
WRMS | 1615 16 18 31 30 18 25 17 139 |NE 46 50 48 44 47 44 43 77 43
MEDI | 1240 14 16 24 19 18 21 16 143 |MD 47 48 48 45 49 44 44 163 44
Table 3.2093.6 GPS week: 2093 Day: 6 MJD: 58901
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 908 51 53 33 40 69 115 40 --- 27 | 134 135 134 156 180 174 136 --- 142
R02E | 4614 7 21 21 10 20 15 11 134 6 | 35 43 28 33 46 36 42 114 36
R03E | 1005 14 17 15 11 13 15 12 101 6 | 36 32 31 32 29 36 35 117 31
XR04E | 1205 9 15 12 14 --- 18 11 --- 6 | 63 61 57 63 --- 66 71 --- 63
R05E | 553 16 45 22 13 17 11 11 --- 7 | 110 110 104 107 109 108 108 --- 107
R07E | 1129 19 17 25 12 19 17 24 259 9 | 103 106 101 102 106 108 105 104 103
R08E | 1477 13 13 20 13 16 12 18 --- 7 | 67 68 70 66 62 68 67 --- 65
R09 | 670 15 31 15 13 12 9 16 --- 6 | 18 28 25 21 20 15 26 --- 17
R11 | 987 7 9 8 11 10 12 12 180 4 | 42 42 41 39 44 48 38 57 41
R12 | 1482 18 15 17 29 26 29 15 --- 10 | 77 73 73 56 62 79 73 --- 68
R13 | 1171 39 52 28 41 30 47 19 --- 15 | 60 70 49 39 57 61 59 --- 52
R14 | 677 16 19 15 19 12 18 9 --- 6 | 51 50 35 38 38 44 42 --- 39
R15 | 662 8 13 13 21 15 18 9 --- 6 | 53 54 53 44 54 59 47 --- 50
R16 | 594 31 36 43 35 36 23 27 --- 15 | 41 48 58 57 63 39 34 --- 41
R17 | 666 8 12 26 38 13 19 18 --- 9 | 54 55 45 39 58 59 52 --- 50
R18 | 729 12 15 23 20 22 20 12 --- 8 | 35 35 30 31 45 40 39 --- 35
R19 | 1272 36 39 52 85 20 44 31 --- 20 | 70 71 38 32 69 70 75 --- 53
R20 | 969 36 41 41 13 19 64 25 --- 15 | 42 51 28 30 49 54 36 --- 35
R21 | 818 8 11 25 38 13 21 26 123 10 | 57 57 46 42 66 58 70 76 56
R22 | 908 13 20 25 29 12 16 18 --- 8 | 60 61 41 41 63 63 60 --- 54
R23 | 1039 14 18 11 26 14 14 13 --- 7 | 34 36 28 44 32 36 28 --- 29
XR26 | ---- 11 43 --- --- --- --- 10 --- 11 | 27 48 --- --- --- --- 27 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1400 23 28 26 31 24 36 20 169 |T 57 60 53 52 62 62 57 93 54
WRMS | 1400 16 21 26 29 18 22 17 169 |NE 48 51 42 39 51 51 47 66 42
MEDI | 969 14 18 22 20 16 18 15 134 |MD 53 54 45 41 57 59 47 104 50
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