[IGSREPORT-26941] Wk 2079 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 29 15:22:51 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2079 (Nov 10, 2019 - Nov 16, 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 2.2079.
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:
igl2079[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2079 in the SP3 format.
igl20797.sum Combination Report for GPS Week 2079.
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 | 0.2 ns
2 | -1.2 ns
3 | -0.1 ns
4 | -11.5 ns
5 | 1.0 ns
6 | -0.3 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
----+--------+---------------
0 | IAC | ALL (high Transformation - See Table 2)
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 1.2079, 1a.2079).
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 2.2079.0-6)
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 3.2079.0-6).
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 2079 summary. (Nov 10, 2019 - Nov 16, 2019)
Table 1.2079.a GPS week : 2079 MJD: 58797.0-58803.0
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 0 12 41 48 .11 17 15 | 23684 -678 2939 7245
| 1 1 1 10 12 13 .04 | 5174 1093
cof n/a| 0 0 0 18 49 59 .07 21 18 | 23670 -671 2937 7247
| 1 1 2 9 19 28 .02 | 5173 1088
emx n/a| 1 -1 -2 24 -17 45 -.04 25 25 | -5155 -383 2946 7367
| 1 0 2 24 17 32 .04 | 9978 768
esx n/a| 0 1 0 32 -12 0 .15 22 20 | 1958 -1818 2946 9040
| 1 0 0 22 15 42 .04 | 8648 1654
gfz n/a| 0 0 3 11 -5 9 .16 30 20 | 0 -562 2924 7329
| 1 1 1 28 23 32 .03 | 0 1276
grg n/a| 3 0 2 -64 -30 -106 -.35 23 20 | -1497 -618 2940 6546
| 1 0 1 16 13 34 .04 | 4411 1335
iac n/a| -1 0 -2 137 8 10 -.09 29 28 | -226 -482 2951 7447
| 1 0 4 393 49 109 .09 | 4432 776
mcc n/a| -1 -3 8 51 1 -46 -.36 199 199 | --- --- --- ---
| 12 4 13 233 105 306 .50 | --- ---
Table 1.2079.b GPS week : 2079 MJD: 58797.0-58803.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 19 16 17 18 18 16 13 |
R02 | 6 6 7 5 6 7 7 |
R03 | 6 6 6 7 6 5 6 |
R05 | 10 7 8 7 9 10 11 |
R07 | 5 6 7 8 6 6 6 |
R08 | 7 7 9 9 7 7 7 |
R09 | 7 6 7 7 7 6 8 |
R11 | 7 8 8 7 6 7 7 |
R12 | 11 11 13 12 12 11 13 |
R13 | 9 8 7 7 7 8 7 |
R14 | 9 10 9 8 9 11 10 |
R15 | 12 14 12 12 12 13 11 |
R16 | 10 14 16 16 15 12 11 |
R17 | 7 8 6 8 8 8 8 |
R18 | 9 7 8 8 7 7 7 |
R19 | 22 23 17 19 19 21 21 |
R20 | 14 10 15 13 13 12 11 |
R21 | 10 8 9 8 7 9 6 |
R22 | 9 9 8 7 8 8 61 |
R23 | 10 9 10 10 9 13 11 |
R24 | 17 14 11 17 14 10 17 |
R26 | 0 42 24 18 25 24 27 |
Table 1.2079.c GPS week : 2079 MJD: 58797.0-58803.0
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 2079 0 | -49 17 170 -514 165 -2303 81.0 1554 1554 | -327 0
brd 2079 1 | -69 60 150 1101 -371 -2821 81.4 1477 1477 | 214 0
brd 2079 2 | -54 -18 142 -173 -1235 -3741 81.6 1478 1478 | -1197 0
brd 2079 3 | -67 4 152 518 329 -103 82.6 1485 1485 | -57 0
brd 2079 4 | -42 65 69 -636 -1464 4762 85.0 1707 1707 | -11535 0
brd 2079 5 | -36 100 69 -1054 -307 2502 83.2 1956 1956 | 1041 0
brd 2079 6 | -38 33 145 -1449 96 428 81.8 2005 2005 | -334 0
-------------+------------------------------------------------------------+----------------
brd 2079 mean| -51 37 128 -315 -398 -182 82.4 1666 1666 | -1742 0
brd 2079 sdev| 13 40 41 884 699 3059 1.4 230 230 | 4370 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 2.2079.0 GPS week: 2079 Day: 0 MJD: 58797
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 0 1 31 28 .06 16 12 | 25889 -769 2812 6991
cof n/a| -2 -3 -2 13 37 44 .07 23 17 | 25873 -764 2815 6997
emx n/a| -1 -1 -1 12 0 13 .01 24 24 | -963 -1036 2798 7165
esx n/a| 0 1 0 76 -36 27 .20 26 23 | 11140 -693 2818 8375
gfz n/a| 0 2 2 34 -13 20 .19 26 20 | 0 -986 2812 7101
grg n/a| 1 0 2 -71 -13 -56 -.40 20 16 | 250 -1156 2806 6544
iac n/a| 0 2 -12 1026 69 4 .10 57 56 | 770 -577 2802 7121
mcc n/a| 0 -4 1 388 -31 -307 -.45 222 222 | --- --- --- ---
Table 2.2079.1 GPS week: 2079 Day: 1 MJD: 58798
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 0 0 28 57 57 .12 16 14 | 26634 -496 3181 8034
cof n/a| 0 -1 2 6 70 95 .07 19 16 | 26625 -510 3178 8042
emx n/a| 1 -2 0 -16 -7 43 -.05 23 23 | -6247 -404 3175 8196
esx n/a| -2 2 0 12 -10 13 .16 21 19 | 5622 -2398 3170 9501
gfz n/a| -1 0 4 -6 -12 -25 .16 35 22 | 0 209 3167 8193
grg n/a| 2 1 0 -88 -45 -103 -.34 24 20 | 30 49 3184 7248
iac n/a| -2 0 -2 25 6 -22 -.11 27 25 | 1768 68 3188 8259
mcc n/a| -8 3 0 215 169 23 -.60 205 205 | --- --- --- ---
Table 2.2079.2 GPS week: 2079 Day: 2 MJD: 58799
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 0 12 48 60 .07 18 15 | 24661 -2338 3111 6958
cof n/a| 1 2 1 21 44 31 .08 24 18 | 24647 -2318 3111 6963
emx n/a| 1 0 0 39 -18 58 -.05 25 25 | 1732 -913 3112 7057
esx n/a| -1 1 0 39 4 -26 .09 22 18 | 1491 -3741 3114 8507
gfz n/a| 0 -1 3 15 -20 -19 .13 28 18 | 0 -2389 3009 7013
grg n/a| 2 1 1 -53 -40 -83 -.31 27 23 | 60 -2731 3113 6469
iac n/a| -1 0 -3 -33 -13 -40 -.07 23 22 | 349 -1255 3131 7145
mcc n/a| 0 -9 33 55 62 -209 .67 219 219 | --- --- --- ---
Table 2.2079.3 GPS week: 2079 Day: 3 MJD: 58800
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 0 30 51 .09 17 15 | 24238 -524 2945 6989
cof n/a| -1 1 0 12 22 73 .05 21 17 | 24217 -499 2946 6989
emx n/a| 1 0 -4 17 -51 78 -.07 25 25 | 5438 -255 2983 7098
esx n/a| 0 0 0 35 -30 44 .12 23 19 | 5881 156 2960 9050
gfz n/a| -2 0 3 2 -18 15 .18 31 19 | 0 -245 2955 7127
grg n/a| 2 0 1 -72 -13 -115 -.35 27 24 | 140 -357 2940 6140
iac n/a| 0 0 0 -19 64 -69 -.11 24 22 | 1090 802 2956 7239
mcc n/a| 5 -4 16 43 5 -491 -.13 189 189 | --- --- --- ---
Table 2.2079.4 GPS week: 2079 Day: 4 MJD: 58801
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 10 30 52 .12 19 17 | 12145 -735 2891 7248
cof n/a| -1 -2 -1 14 38 20 .08 22 19 | 12136 -741 2884 7250
emx n/a| 1 -1 -1 18 -28 24 -.08 27 27 | -25546 -42 2888 7330
esx n/a| 0 1 0 36 -8 -59 .20 21 20 | -11218 -2428 2899 9667
gfz n/a| -1 0 3 -26 -6 8 .15 29 19 | 0 -420 2897 7143
grg n/a| 4 1 1 -63 -29 -144 -.30 23 18 | -11499 -165 2902 6520
iac n/a| -2 0 -1 22 18 113 -.13 22 20 | -10131 -1085 2912 7502
mcc n/a| 11 0 10 107 40 198 -.61 135 135 | --- --- --- ---
Table 2.2079.5 GPS week: 2079 Day: 5 MJD: 58802
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 19 35 57 .18 19 17 | 25444 1335 2891 7038
cof n/a| 0 0 2 24 53 88 .08 20 19 | 25430 1338 2886 7034
emx n/a| 0 -1 -2 37 -4 8 -.05 25 25 | -6507 1087 2895 7118
esx n/a| 0 0 0 10 3 -42 .16 19 18 | -8462 38 2887 8657
gfz n/a| -2 1 1 1 47 -6 .10 27 22 | 0 1533 2886 7129
grg n/a| 3 0 1 -34 -28 -154 -.35 21 18 | 329 1503 2886 6308
iac n/a| -4 0 0 1 -74 201 -.14 28 25 | 2556 -104 2893 7179
mcc n/a| -26 -3 2 -104 -158 393 -.73 155 155 | --- --- --- ---
Table 2.2079.6 GPS week: 2079 Day: 6 MJD: 58803
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 56 30 .12 16 14 | 26778 -1225 2747 7460
cof n/a| 0 0 -1 36 76 62 .04 21 17 | 26767 -1205 2740 7457
emx n/a| 1 0 -6 60 -15 92 .04 27 27 | -3992 -1120 2772 7609
esx n/a| -2 3 1 15 -10 42 .15 20 20 | 9253 -3664 2778 9526
gfz n/a| 1 0 3 59 -15 72 .20 34 20 | 0 -1636 2748 7603
grg n/a| 4 0 6 -68 -42 -87 -.41 21 17 | 205 -1470 2752 6594
iac n/a| -1 0 1 -63 -12 -112 -.16 26 24 | 2014 -1223 2775 7687
mcc n/a| 3 -5 -6 -347 -80 68 -.71 267 267 | --- --- --- ---
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 3.2079.0 GPS week: 2079 Day: 0 MJD: 58797
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 | 1223 36 31 44 44 44 23 65 --- 19 | 98 107 101 63 82 68 86 --- 80
R02 | 1247 6 15 10 15 14 13 51 157 6 | 61 68 55 58 63 58 84 84 58
R03 | 661 13 16 10 13 12 13 68 364 6 | 62 63 59 61 59 56 98 170 59
R05 | 989 15 25 24 20 25 10 57 --- 9 | 54 57 62 40 40 42 78 --- 46
R07 | 612 6 11 9 14 13 11 56 161 5 | 65 66 66 56 67 64 90 242 62
R08 | 1420 13 26 11 18 13 13 51 --- 7 | 63 62 67 69 75 71 96 --- 67
R09 | 2380 9 14 12 11 23 11 41 --- 6 | 60 59 58 59 59 58 79 --- 57
R11 | 811 7 9 16 12 18 18 63 239 7 | 60 58 47 54 67 45 89 140 53
R12 | 613 13 18 23 31 23 17 48 --- 10 | 82 85 55 56 93 80 93 --- 71
R13 | 4126 8 14 8 24 9 26 60 --- 8 | 51 53 43 65 48 34 103 --- 47
R14 | 680 12 19 29 21 19 7 55 --- 9 | 82 87 56 79 92 78 115 --- 76
R15 | 565 15 18 22 40 15 19 74 --- 11 | 84 87 62 51 87 88 91 --- 73
R16 | 1219 14 17 21 22 20 18 53 --- 9 | 64 58 54 65 75 72 88 --- 63
R17E | 1434 12 12 19 14 10 16 50 --- 7 | 54 53 52 51 53 58 79 --- 52
R18E | 1317 10 11 16 18 23 21 59 --- 8 | 33 36 33 40 37 35 78 --- 33
R19E | 1087 26 63 53 45 56 42 58 --- 22 | 178 188 190 159 173 175 165 --- 172
R20E | 1727 19 25 25 19 44 31 63 --- 14 | 45 46 46 49 68 61 90 --- 48
R21E | 709 11 9 27 22 25 12 50 76 9 | 47 49 45 51 60 44 96 45 47
R22E | 1799 14 13 25 14 22 12 50 --- 8 | 84 9999 44 41 45 31 104 --- 84
R23E | 993 13 19 16 21 26 19 55 --- 9 | 54 57 44 53 46 52 93 --- 48
R24E | 2267 25 33 27 47 40 33 50 --- 17 | 52 60 54 75 73 58 98 --- 49
XR26E | ---- 3 244 --- --- --- --- 79 --- 0 | 81 186 --- --- --- --- 113 --- 78
------+---------------------------------------------------+-----------------------------------------------
RMS | 1553 16 23 24 26 26 20 56 222 |T 68 75 61 61 69 63 95 136 64
WRMS | 1553 12 17 24 23 20 16 56 222 |NE 68 70 60 59 69 62 91 159 62
MEDI | 1219 13 17 21 20 22 17 55 161 |MD 61 60 55 56 67 58 91 140 58
Table 3.2079.1 GPS week: 2079 Day: 1 MJD: 58798
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 | 805 29 34 47 37 36 32 20 --- 15 | 67 74 70 56 62 41 56 --- 56
R02 | 829 10 10 13 14 16 8 22 205 6 | 42 42 36 46 48 41 56 98 43
R03 | 785 10 8 12 16 13 8 12 312 5 | 43 43 35 53 49 45 42 160 43
R05 | 950 13 14 19 18 16 13 14 --- 7 | 41 41 38 43 49 41 39 --- 40
R07 | 906 9 9 7 15 12 12 17 126 5 | 45 45 45 43 47 50 42 104 43
R08 | 1249 15 11 13 16 28 10 15 --- 7 | 42 48 48 52 63 49 57 --- 48
R09 | 1225 8 11 8 13 22 13 18 --- 6 | 48 49 50 53 49 54 47 --- 49
R11 | 1356 14 16 14 11 28 19 23 217 8 | 42 43 32 35 54 34 26 126 35
R12 | 1088 21 26 22 25 36 15 33 --- 11 | 57 61 50 45 67 48 49 --- 48
R13 | 3540 9 9 13 21 9 26 15 --- 7 | 33 34 33 46 39 18 37 --- 33
R14 | 735 16 15 25 19 18 25 31 --- 10 | 60 55 39 65 70 73 47 --- 56
R15 | 605 17 23 22 24 39 39 51 --- 14 | 59 64 48 41 77 81 36 --- 52
R16 | 1347 17 28 28 26 50 44 24 --- 14 | 45 50 51 45 76 73 49 --- 50
R17E | 2024 12 12 23 11 29 18 19 --- 8 | 54 55 52 54 51 52 52 --- 51
R18E | 628 10 11 16 19 13 18 14 --- 7 | 31 29 28 33 30 30 31 --- 28
R19E | 1352 26 36 50 29 99 44 62 --- 22 | 138 150 140 146 211 133 139 --- 141
R20E | 2375 16 17 26 19 23 19 28 --- 9 | 32 30 37 31 39 40 43 --- 31
R21E | 1070 13 10 23 9 18 15 20 85 7 | 39 41 42 41 47 42 42 47 40
R22E | 2052 8 10 25 15 31 16 19 --- 8 | 65 9999 24 24 30 18 31 --- 64
R23E | 1242 15 14 15 19 28 16 27 --- 8 | 43 48 41 52 57 43 57 --- 45
R24E | 1391 26 31 18 41 48 30 25 --- 14 | 38 45 32 69 53 40 41 --- 38
XR26E | ---- 31 134 --- --- --- --- 57 --- 42 | 56 118 --- --- --- --- 60 --- 49
------+---------------------------------------------------+-----------------------------------------------
RMS | 1477 16 19 23 21 35 24 27 205 |T 50 55 46 51 60 49 49 107 49
WRMS | 1477 14 16 23 19 22 20 25 205 |NE 48 49 44 47 57 49 44 122 45
MEDI | 1225 14 14 19 19 28 18 20 205 |MD 43 48 41 46 51 43 43 104 45
Table 3.2079.2 GPS week: 2079 Day: 2 MJD: 58799
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 | 1318 28 31 55 56 29 27 17 --- 17 | 73 79 84 61 76 54 61 --- 64
R02 | 978 9 10 11 22 13 17 16 268 6 | 47 45 51 44 52 58 60 201 50
R03 | 467 7 8 11 11 13 13 16 308 5 | 50 51 48 57 59 53 59 210 54
R05 | 1299 12 13 22 15 18 24 8 --- 7 | 38 44 44 48 46 32 35 --- 38
R07 | 812 13 16 15 9 18 16 23 159 7 | 57 59 54 49 45 61 38 133 49
R08 | 758 7 11 10 11 35 26 22 --- 8 | 56 53 53 53 78 51 44 --- 54
R09 | 1118 11 13 10 11 18 12 22 --- 6 | 60 57 59 57 56 54 63 --- 57
R11 | 1772 18 16 13 13 12 19 24 193 7 | 50 48 40 39 45 28 26 126 38
R12 | 1019 25 29 30 23 33 27 33 --- 12 | 61 60 31 43 69 59 27 --- 44
R13 | 1010 9 11 14 18 17 16 12 --- 6 | 45 42 37 55 45 39 37 --- 43
R14 | 649 14 22 25 11 21 22 22 --- 8 | 69 76 48 68 75 68 51 --- 62
R15 | 1192 21 19 18 26 27 30 38 --- 12 | 65 63 45 41 72 70 37 --- 52
R16 | 839 21 43 35 34 29 62 24 --- 15 | 55 71 36 47 63 92 49 --- 51
R17E | 1914 8 9 18 9 21 15 13 --- 6 | 50 48 47 51 52 55 48 --- 50
R18E | 1047 15 17 17 15 23 19 12 --- 7 | 24 28 30 35 34 33 31 --- 28
R19E | 2345 36 59 40 38 40 50 30 --- 17 | 66 92 67 72 72 85 64 --- 64
R20E | 2092 18 35 34 17 68 29 31 --- 15 | 32 54 26 41 72 33 41 --- 31
R21E | 2056 18 14 26 17 13 19 23 99 9 | 45 45 42 53 51 41 55 58 47
R22E | 1955 10 12 21 11 20 25 15 --- 7 | 45 9999 23 21 27 26 28 --- 45
R23E | 924 16 15 19 24 29 11 23 --- 9 | 27 32 22 41 31 27 35 --- 27
R24E | 2739 22 24 20 19 33 26 25 --- 10 | 41 58 44 46 65 50 37 --- 41
XR26E | ---- 18 65 --- --- --- --- 29 --- 23 | 54 80 --- --- --- --- 59 --- 51
------+---------------------------------------------------+-----------------------------------------------
RMS | 1478 18 24 25 22 28 27 23 219 |T 50 56 44 48 56 50 44 145 47
WRMS | 1478 15 18 25 18 18 23 22 219 |NE 55 57 48 50 60 55 45 167 50
MEDI | 1118 15 16 19 17 21 22 22 193 |MD 50 54 44 48 56 53 41 133 49
Table 3.2079.3 GPS week: 2079 Day: 3 MJD: 58800
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 | 1741 29 33 58 47 22 47 27 --- 17 | 83 87 95 55 66 51 51 --- 65
R02 | 758 7 13 12 10 9 11 14 198 4 | 57 60 63 60 63 61 50 188 58
R03 | 885 10 9 13 18 18 11 16 141 6 | 57 53 61 55 58 54 53 148 55
R05 | 838 12 11 20 15 12 20 11 --- 6 | 40 45 53 53 49 38 41 --- 44
R07 | 865 14 18 16 16 13 15 24 290 7 | 60 63 60 48 45 60 42 292 52
R08 | 1326 12 24 14 18 15 33 28 --- 9 | 60 82 56 72 66 60 60 --- 61
R09 | 1614 10 13 9 13 19 20 19 --- 6 | 41 40 34 34 40 30 40 --- 35
R11 | 2332 17 16 15 10 12 20 21 181 7 | 54 53 38 41 48 34 30 110 41
R12 | 1260 20 36 28 21 36 17 33 --- 11 | 56 71 31 41 71 45 21 --- 42
R13 | 2931 11 12 17 20 12 22 11 --- 7 | 52 55 41 64 58 41 48 --- 50
R14 | 522 19 12 21 19 14 19 15 --- 8 | 65 59 49 56 54 61 51 --- 55
R15 | 1119 19 23 24 24 33 25 35 --- 11 | 70 70 53 39 73 68 35 --- 55
R16 | 1106 19 18 36 35 36 58 27 --- 15 | 56 65 36 65 90 102 48 --- 61
R17E | 1186 9 10 22 12 22 20 19 --- 7 | 58 62 65 64 64 62 49 --- 59
R18E | 2057 8 8 14 22 17 25 18 --- 8 | 30 32 34 48 51 41 29 --- 35
R19E | 1076 33 35 39 34 62 46 40 --- 18 | 71 75 70 71 92 86 67 --- 68
R20E | 1127 19 33 31 28 32 32 31 --- 12 | 35 44 35 49 46 42 45 --- 32
R21E | 1370 18 13 23 16 10 15 17 46 7 | 40 42 37 46 50 38 54 92 41
R22E | 760 12 5 23 15 16 15 12 --- 7 | 87 9999 34 37 34 34 37 --- 85
R23E | 1477 15 19 15 20 40 20 21 --- 10 | 34 36 33 42 42 27 37 --- 32
R24E | 2236 18 32 25 30 83 27 29 --- 17 | 47 50 42 48 92 37 43 --- 38
XR26E | ---- 14 43 --- --- --- --- 22 --- 17 | 30 65 --- --- --- --- 41 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1484 17 21 25 23 31 27 24 189 |T 53 57 48 51 59 51 44 166 49
WRMS | 1484 15 17 25 19 19 24 22 189 |NE 57 61 51 52 60 54 43 184 51
MEDI | 1186 14 16 21 19 18 20 21 181 |MD 56 59 42 49 58 45 43 148 50
Table 3.2079.4 GPS week: 2079 Day: 4 MJD: 58801
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 | 1095 36 34 65 47 27 25 32 --- 18 | 77 75 88 41 56 58 64 --- 60
R02 | 1287 10 14 14 9 9 15 15 164 5 | 49 51 48 48 44 48 47 122 46
R03 | 1281 7 11 7 12 17 16 15 137 5 | 50 56 47 45 53 50 51 111 48
R05 | 792 10 11 34 17 26 12 12 --- 8 | 41 40 56 33 44 44 36 --- 39
R07 | 740 12 11 12 8 19 10 12 149 5 | 53 52 54 51 46 54 51 145 50
R08 | 1700 14 23 14 16 15 15 16 --- 6 | 55 53 49 65 67 67 60 --- 59
R09 | 3143 11 11 15 10 18 17 15 --- 6 | 61 65 56 60 63 62 61 --- 60
R11 | 1811 16 19 14 13 13 10 12 146 6 | 54 54 38 38 51 45 40 116 43
R12 | 1148 29 23 22 19 34 17 31 --- 11 | 61 49 40 39 67 51 33 --- 45
R13 | 3165 13 17 12 18 22 20 8 --- 7 | 48 48 38 52 39 33 42 --- 41
R14 | 973 20 40 23 18 17 18 23 --- 9 | 65 81 46 49 60 61 48 --- 53
R15 | 636 23 22 20 21 31 22 34 --- 11 | 61 60 42 44 62 60 32 --- 47
R16 | 2018 23 24 43 33 26 50 17 --- 15 | 49 54 43 60 65 79 51 --- 54
R17E | 1785 13 11 20 16 23 12 18 --- 7 | 43 42 40 45 48 41 37 --- 40
R18E | 3220 8 16 23 17 20 12 15 --- 7 | 26 28 35 34 34 26 39 --- 29
R19E | 2210 29 30 40 40 73 35 35 --- 18 | 68 70 68 78 95 69 64 --- 67
R20E | 909 20 29 30 21 38 34 27 --- 12 | 38 37 35 31 38 46 44 --- 31
R21E | 680 14 19 22 11 18 13 16 39 7 | 36 38 35 36 40 37 35 54 35
R22E | 706 14 11 25 13 22 15 16 --- 7 | 81 9999 22 24 24 27 26 --- 83
R23E | 901 15 20 16 15 31 17 20 --- 8 | 61 60 56 70 63 64 72 --- 63
R24E | 1280 27 30 22 17 37 45 31 --- 13 | 57 55 46 42 74 56 42 --- 47
XR26E | ---- 23 36 --- --- --- --- 27 --- 25 | 38 47 --- --- --- --- 68 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1706 19 22 27 21 29 23 22 135 |T 53 53 46 46 53 51 47 109 49
WRMS | 1706 17 19 27 20 19 18 20 135 |NE 55 56 49 48 55 54 47 123 49
MEDI | 1280 14 19 22 17 22 17 16 146 |MD 53 53 46 45 53 51 44 116 47
Table 3.2079.5 GPS week: 2079 Day: 5 MJD: 58802
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 | 585 35 31 55 33 21 24 35 --- 15 | 71 72 78 53 59 50 50 --- 57
R02 | 802 13 14 12 8 18 14 21 114 6 | 53 52 55 47 38 50 36 49 45
R03 | 764 8 10 10 7 13 12 11 158 4 | 54 53 55 58 60 58 51 136 55
R05 | 723 22 16 30 21 20 15 22 --- 9 | 48 41 56 40 47 42 28 --- 41
R07 | 568 11 8 10 14 18 13 16 242 6 | 47 47 51 59 50 59 48 119 51
R08 | 1810 8 14 10 19 10 13 30 --- 7 | 51 57 54 64 54 50 43 --- 52
R09 | 3811 13 16 13 11 18 10 14 --- 6 | 59 60 56 61 65 62 50 --- 59
R11 | 1123 10 19 17 8 24 13 22 141 7 | 56 61 50 48 63 50 44 98 50
R12 | 1420 21 30 27 24 29 23 26 --- 11 | 67 71 46 48 65 60 36 --- 52
R13 | 2250 11 14 17 18 14 19 17 --- 7 | 72 72 60 68 58 56 66 --- 63
R14 | 656 27 16 27 20 18 25 18 --- 10 | 139 133 122 134 137 121 135 --- 130
R15 | 394 22 24 24 22 36 20 43 --- 12 | 64 66 51 50 72 65 46 --- 56
R16 | 1690 19 21 30 22 26 34 24 --- 11 | 36 29 25 51 51 42 38 --- 36
R17E | 865 12 11 20 15 12 16 25 --- 7 | 62 60 62 64 56 64 51 --- 59
R18E | 3510 12 13 13 15 18 14 15 --- 6 | 26 27 28 37 33 33 24 --- 28
R19E | 3629 31 38 45 39 72 38 52 --- 20 | 57 59 56 65 79 53 62 --- 54
R20E | 1832 18 19 32 17 38 16 40 --- 12 | 28 26 28 31 34 29 32 --- 24
R21E | 913 9 15 27 10 32 17 18 65 8 | 43 48 47 51 60 49 39 36 46
R22E | 941 11 13 24 12 23 18 23 --- 8 | 159 9999 41 41 46 46 45 --- 157
R23E | 756 30 35 18 19 27 38 34 --- 12 | 42 47 42 47 52 56 38 --- 40
R24E | 4057 18 17 20 17 23 25 33 --- 10 | 94 94 95 98 100 105 84 --- 95
XR26E | ---- 16 25 --- --- --- --- 33 --- 24 | 42 64 --- --- --- --- 47 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1956 19 20 25 19 27 21 28 155 |T 62 59 55 57 60 57 49 87 58
WRMS | 1956 17 19 25 18 22 18 25 155 |NE 62 62 58 60 63 58 51 100 57
MEDI | 941 13 16 20 17 21 17 23 141 |MD 54 59 54 51 58 53 45 98 52
Table 3.2079.6 GPS week: 2079 Day: 6 MJD: 58803
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 | 1138 24 29 40 26 22 37 18 --- 12 | 98 103 101 79 88 62 69 --- 80
R02 | 3050 12 15 19 17 13 12 21 173 7 | 62 65 65 56 57 61 54 75 58
R03 | 662 8 9 14 13 16 14 13 176 5 | 68 69 69 63 61 69 63 151 65
R05 | 1900 22 33 34 30 16 18 23 --- 11 | 54 58 64 47 48 42 33 --- 44
R07 | 591 6 8 12 12 19 9 17 497 5 | 62 60 67 58 56 65 61 268 60
R08 | 1212 13 14 9 21 17 12 14 --- 6 | 66 77 70 80 73 73 63 --- 70
R09 | 4165 11 13 12 19 30 16 19 --- 8 | 61 61 60 68 65 59 57 --- 61
R11 | 572 15 11 15 11 13 15 25 155 7 | 87 86 80 78 82 66 65 111 76
R12 | 1227 20 22 35 22 44 23 38 --- 13 | 80 79 52 55 100 74 42 --- 65
R13 | 3153 8 9 21 14 12 13 18 --- 6 | 90 90 83 98 92 71 78 --- 85
R14 | 1815 12 20 28 23 30 13 23 --- 9 | 170 175 161 183 180 158 157 --- 167
R15 | 542 21 24 23 18 33 12 36 --- 10 | 80 79 57 57 87 74 50 --- 66
R16 | 1064 13 21 20 28 23 29 23 --- 10 | 56 63 46 67 72 68 53 --- 57
R17E | 1099 15 10 28 14 14 19 20 --- 8 | 61 57 49 55 58 56 51 --- 54
R18E | 1748 7 17 14 9 29 13 15 --- 6 | 31 32 33 35 38 30 34 --- 31
R19E | 3700 27 33 55 36 78 38 53 --- 20 | 102 113 108 108 133 108 99 --- 103
R20E | 1990 18 27 28 15 27 23 32 --- 10 | 36 42 37 44 51 39 44 --- 36
R21E | 1329 6 9 19 10 21 13 18 157 6 | 49 49 39 49 57 44 54 65 47
XR22E |20462 26 >>>> --- --- --- --- 96 --- 60 | 205 9999 --- --- --- --- 70 --- 211
R23E | 820 22 30 26 18 30 30 21 --- 10 | 55 57 43 60 50 65 53 --- 53
R24E | 2401 25 28 37 25 80 22 28 --- 16 | 66 73 63 68 111 72 65 --- 66
XR26E | ---- 20 38 --- --- --- --- 35 --- 26 | 85 111 --- --- --- --- 86 --- 84
------+---------------------------------------------------+-----------------------------------------------
RMS | 2005 16 21 27 20 34 21 26 267 |T 78 76 67 70 77 67 63 134 74
WRMS | 2005 14 17 27 20 20 17 24 267 |NE 79 81 75 76 81 72 65 151 73
MEDI | 1329 15 20 21 18 22 15 21 173 |MD 66 69 63 60 65 65 57 111 65
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