[IGSREPORT-27224] Wk 2100 IGLOS Final Orbits
acc
acc at igs.org
Wed Apr 29 22:40:04 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2100 (Apr 05, 2020 - Apr 11, 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 2.2100.
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:
igl2100[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2100 in the SP3 format.
igl21007.sum Combination Report for GPS Week 2100.
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 | -2.3 ns
1 | -3.1 ns
2 | -0.8 ns
3 | -0.2 ns
4 | -3.6 ns
5 | -3.7 ns
6 | -3.0 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
----+--------+---------------
5 | GFZ | R22
6 | COD | R22
6 | EMX | R22
6 | ESX | R22
6 | GFZ | R22
6 | GRG | R22
6 | IAC | R22
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 1.2100, 1a.2100).
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 2.2100.0-6)
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 3.2100.0-6).
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 2100 summary. (Apr 05, 2020 - Apr 11, 2020)
Table 1.2100.a GPS week : 2100 MJD: 58944.0-58950.0
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 32 8 46 .11 24 19 | 22561 479 3160 8466
| 0 1 3 16 25 20 .03 | 1242 1163
cof n/a| 0 0 4 22 18 42 .11 27 20 | 22563 465 3163 8469
| 1 1 3 23 15 25 .04 | 1241 1172
emx n/a| 0 -1 -7 30 -21 32 .06 31 30 | -5206 681 3151 8602
| 1 1 2 24 28 35 .04 | 13089 1148
esx n/a| 1 0 -8 16 -31 -78 .13 34 26 | -2292 2078 3149 10050
| 1 1 2 19 7 37 .05 | 8457 1815
gfz n/a| 0 -1 -2 -9 1 -65 .08 28 15 | 0 188 3192 7902
| 1 1 1 13 19 21 .06 | 0 1947
grg n/a| 1 1 4 -85 17 50 -.37 28 23 | -2529 414 3128 7459
| 1 1 6 20 22 38 .08 | 1129 2043
iac n/a| -1 0 4 22 14 0 -.01 25 25 | -503 -312 3156 8550
| 1 1 1 21 25 42 .03 | 1020 1462
Table 1.2100.b GPS week : 2100 MJD: 58944.0-58950.0
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 | 17 19 17 18 19 18 17 |
R02 | 7 7 9 8 7 8 8 |
R03 | 10 8 10 9 9 9 8 |
R04 | 12 13 13 13 12 11 13 |
R05 | 10 9 8 9 13 10 9 |
R07 | 8 9 11 7 8 7 7 |
R08 | 8 9 8 7 7 7 8 |
R09 | 6 6 7 8 8 6 8 |
R11 | 7 6 6 7 6 6 5 |
R12 | 9 8 9 10 10 10 7 |
R13 | 13 15 20 22 20 17 17 |
R14 | 7 7 7 7 7 6 7 |
R15 | 8 9 7 9 9 8 9 |
R16 | 12 13 19 15 14 13 15 |
R17 | 7 8 12 14 10 8 8 |
R18 | 8 7 10 16 8 6 6 |
R19 | 20 22 21 18 20 22 19 |
R20 | 25 24 28 28 26 27 25 |
R21 | 10 9 11 15 9 9 9 |
R22 | 9 9 10 11 12 19 --- |
R23 | 11 11 13 11 10 10 10 |
R24 | 14 16 18 20 23 0 0 |
R26 | 15 22 30 45 23 30 22 |
Table 1.2100.c GPS week : 2100 MJD: 58944.0-58950.0
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 2100 0 | -56 0 280 513 1476 2573 81.8 1148 1148 | -2308 0
brd 2100 1 | 24 16 282 1079 1816 3640 82.2 1277 1277 | -3137 0
brd 2100 2 | 61 -1 275 -123 879 4636 81.7 1411 1411 | -779 0
brd 2100 3 | 7 55 250 532 -597 4606 81.5 1355 1355 | -176 0
brd 2100 4 | -51 8 204 -590 -367 7378 83.0 1512 1512 | -3569 0
brd 2100 5 | 3 0 162 -463 477 6884 81.1 1323 1323 | -3678 0
brd 2100 6 | -4 -23 203 1303 1174 6952 81.5 1321 1321 | -2977 0
-------------+------------------------------------------------------------+----------------
brd 2100 mean| -2 7 236 321 694 5238 81.8 1335 1335 | -2374 0
brd 2100 sdev| 41 24 47 737 910 1854 .6 112 112 | 1381 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 2.2100.0 GPS week: 2100 Day: 0 MJD: 58944
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 3 61 33 41 .11 26 20 | 20526 1427 2942 8077
cof n/a| 2 1 4 52 21 89 .14 31 22 | 20539 1398 2944 8079
emx n/a| 1 -1 -9 6 -3 76 .01 27 27 | -6206 1752 2927 8288
esx n/a| 0 1 -6 19 -36 -51 .10 31 23 | -13678 2544 2925 9228
gfz n/a| 1 -3 0 -3 -7 -71 .15 30 16 | 0 734 2950 7333
grg n/a| 0 0 -2 -103 -18 55 -.46 25 25 | -2991 1534 2952 6790
iac n/a| -1 1 7 13 9 -52 -.02 18 18 | -114 -541 2935 8193
Table 2.2100.1 GPS week: 2100 Day: 1 MJD: 58945
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 5 42 -3 13 .15 25 24 | 22168 -818 2960 8194
cof n/a| 1 0 5 41 33 54 .08 29 27 | 22177 -850 2965 8195
emx n/a| 0 -2 -7 50 -6 83 .03 26 26 | -20600 -1130 2938 8345
esx n/a| 0 0 -6 41 -20 -88 .17 32 24 | -3937 -44 2943 10465
gfz n/a| 0 -2 -2 1 26 -60 .05 33 15 | 0 -2274 2937 7540
grg n/a| 4 3 2 -102 49 34 -.34 27 24 | -1981 -2130 2961 7008
iac n/a| -3 0 4 -11 -36 -53 .02 20 20 | -294 -1812 2951 8307
Table 2.2100.2 GPS week: 2100 Day: 2 MJD: 58946
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 4 1 38 35 49 .15 29 21 | 21746 951 3003 8141
cof n/a| 0 0 3 33 -4 25 .06 27 22 | 21739 949 3001 8143
emx n/a| 3 -3 -5 48 -4 14 .03 33 33 | 8440 968 2999 8241
esx n/a| 2 0 -6 4 -40 -60 .16 34 27 | 10267 2794 3008 10325
gfz n/a| 0 -1 -1 2 -36 -54 .08 29 13 | 0 799 3034 7516
grg n/a| -1 1 1 -107 14 99 -.47 32 28 | -1368 1119 3008 6793
iac n/a| 0 1 5 12 41 8 -.00 26 26 | -313 1101 3008 8225
Table 2.2100.3 GPS week: 2100 Day: 3 MJD: 58947
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 8 25 -25 69 .08 26 20 | 23819 2091 3688 8902
cof n/a| 0 1 10 27 11 19 .18 27 21 | 23807 2111 3695 8904
emx n/a| 0 0 -4 34 2 -14 .05 34 34 | 7286 1833 3682 9040
esx n/a| 2 -2 -9 -16 -27 -151 .11 38 29 | -6006 4121 3663 10573
gfz n/a| -1 0 0 -26 8 -70 .14 30 18 | 0 3683 3729 8327
grg n/a| 1 0 -1 -54 29 60 -.41 27 21 | -1599 2787 3686 7740
iac n/a| -1 2 4 58 10 64 .02 34 34 | 439 1699 3681 8889
Table 2.2100.4 GPS week: 2100 Day: 4 MJD: 58948
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 23 -18 49 .12 21 15 | 24139 870 3528 9373
cof n/a| 0 1 3 -11 24 39 .09 29 18 | 24155 831 3530 9371
emx n/a| 1 -1 -10 45 -22 32 .10 31 32 | -24590 1535 3511 9511
esx n/a| 1 0 -7 14 -24 -86 .04 35 26 | -2193 4290 3521 10675
gfz n/a| 0 -3 -1 -22 0 -88 .11 31 16 | 0 547 3620 9070
grg n/a| 0 1 10 -63 34 17 -.35 25 19 | -4744 2408 3276 8554
iac n/a| -4 0 2 32 18 25 -.08 27 27 | 170 -2326 3529 9431
Table 2.2100.5 GPS week: 2100 Day: 5 MJD: 58949
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 13 28 72 .07 21 16 | 23039 -982 3096 8475
cof n/a| 0 -1 -1 9 37 51 .10 25 16 | 23044 -1007 3097 8482
emx n/a| -1 1 -6 40 -71 16 .09 36 28 | 3185 -367 3091 8531
esx n/a| 1 0 -12 17 -39 -69 .14 35 27 | -7894 467 3092 9627
gfz n/a| 0 0 -4 0 6 -89 -.02 21 13 | 0 -1548 3154 7938
grg n/a| 0 0 16 -78 9 94 -.29 27 23 | -2614 -1945 3084 7726
iac n/a| -2 0 2 19 28 17 -.02 29 29 | -2649 284 3099 8606
Table 2.2100.6 GPS week: 2100 Day: 6 MJD: 58950
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 23 6 29 .10 22 16 | 22490 -182 2905 8105
cof n/a| 1 0 2 1 3 19 .12 24 19 | 22482 -175 2910 8111
emx n/a| 0 1 -6 -15 -48 17 .08 29 29 | -3963 180 2910 8259
esx n/a| 0 0 -8 35 -29 -37 .18 33 28 | 7397 378 2893 9461
gfz n/a| 0 -1 -5 -21 15 -26 .05 26 15 | 0 -625 2924 7596
grg n/a| 3 -1 5 -88 6 -4 -.28 30 24 | -2410 -872 2929 7604
iac n/a| 0 0 4 32 31 -12 -.01 20 20 | -762 -594 2891 8199
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 3.2100.0 GPS week: 2100 Day: 0 MJD: 58944
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1244 44 29 34 66 35 24 17 16 | 95 94 69 54 88 67 81 71
R02 | 889 13 14 15 15 13 15 14 6 | 56 58 45 38 43 39 50 44
R03 | 466 17 11 22 32 18 27 15 10 | 78 75 55 44 79 90 74 70
XR04 | 1552 21 31 28 36 --- 26 11 12 | 84 92 69 59 --- 93 89 78
R05 | 550 17 21 22 35 15 27 16 10 | 66 70 53 53 62 73 73 62
R07 | 967 10 12 26 22 22 15 14 8 | 88 92 66 68 99 92 91 84
R08 | 861 13 14 22 25 24 13 13 8 | 75 74 53 63 75 74 68 67
R09 | 1262 14 14 14 9 11 19 12 6 | 29 28 28 29 34 27 30 28
R11 | 1861 10 8 21 16 14 15 15 7 | 50 57 42 47 59 66 60 54
R12 | 819 17 17 19 31 19 18 8 8 | 76 79 70 59 86 78 70 72
R13 | 1117 40 42 20 30 38 29 18 13 | 97 101 79 73 107 98 107 93
R14 | 1346 13 17 14 21 14 14 12 6 | 69 72 54 59 61 62 67 62
R15 | 637 9 13 16 28 16 16 14 7 | 89 91 81 73 92 99 95 89
R16 | 911 26 47 32 14 13 39 17 11 | 62 72 61 73 80 91 80 73
R17E | 1553 16 21 20 16 14 17 12 7 | 94 94 95 88 88 92 95 91
R18E | 780 12 12 20 8 20 20 16 7 | 125 128 128 125 127 129 132 127
R19E | 893 62 76 40 31 34 46 37 19 | 71 74 43 40 53 38 61 39
R20E | 1015 37 42 64 65 89 48 30 25 | 72 66 39 63 115 47 64 57
R21E | 872 16 18 33 20 34 7 14 10 | 168 167 160 162 172 161 169 164
R22E | 2468 26 24 25 18 11 19 20 9 | 112 111 51 105 143 112 110 110
R23E | 597 26 29 20 38 32 14 14 11 | 215 215 217 229 224 223 222 220
R24 | 1022 29 61 30 23 42 32 32 14 | --- --- --- --- --- --- --- 0
XR26E | ---- 19 60 --- --- --- --- 11 15 | 81 115 --- --- --- --- 90 84
------+----------------------------------------------+------------------------------------------
RMS | 1148 26 31 27 31 30 25 18 |T 88 92 74 76 94 88 89 83
WRMS | 1148 20 22 27 23 16 25 18 |NE 72 75 58 56 74 74 73 67
MEDI | 911 17 21 22 23 19 19 14 |MD 78 79 61 63 86 90 80 72
Table 3.2100.1 GPS week: 2100 Day: 1 MJD: 58945
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1352 32 32 31 79 47 34 23 18 | 68 76 58 72 99 68 60 63
R02 | 1480 9 8 11 12 19 16 19 6 | 45 43 42 42 37 38 51 42
R03 | 509 12 10 15 34 11 22 13 8 | 61 61 48 42 51 64 60 54
XR04 | 1003 17 18 23 42 --- 15 24 12 | 72 74 59 51 --- 71 73 64
R05 | 825 9 16 17 35 16 14 18 8 | 51 58 47 48 51 52 53 49
R07 | 665 9 14 21 33 16 22 13 8 | 67 72 60 49 74 75 70 65
R08 | 656 16 23 17 15 29 18 22 9 | 67 75 53 55 74 63 55 59
R09 | 1323 17 22 8 12 17 12 14 6 | 36 39 34 38 42 35 31 34
R11 | 2482 4 12 17 8 13 18 9 5 | 39 43 39 40 43 50 41 41
R12 | 978 13 34 10 28 31 16 11 8 | 53 74 58 50 74 52 46 53
R13 | 1676 35 45 24 51 44 20 17 14 | 66 72 50 41 83 60 53 55
R14 | 719 15 21 16 16 18 13 13 6 | 52 54 43 47 53 51 46 47
R15 | 542 8 13 19 28 10 11 30 9 | 59 60 52 49 59 55 71 57
R16 | 787 25 22 28 19 42 32 24 13 | 44 45 47 47 49 58 49 46
R17E | 2080 16 20 22 17 19 17 9 7 | 86 84 87 87 81 89 84 84
R18E | 495 7 14 18 11 15 21 12 6 | 94 92 93 93 91 98 89 92
R19E | 837 72 70 42 29 43 56 32 21 | 49 48 45 40 49 49 33 32
R20E | 1160 31 33 58 63 88 43 33 23 | 61 69 39 62 94 42 54 49
R21E | 1270 12 16 26 18 25 18 15 8 | 153 154 146 150 151 148 152 149
R22E | 2461 20 25 24 15 15 20 15 8 | 100 104 37 96 100 101 100 100
R23E | 510 21 32 23 31 31 23 15 10 | 185 184 185 197 190 195 191 189
R24 | 856 32 49 42 19 37 52 27 16 | --- --- --- --- --- --- --- 0
XR26E | ---- 25 38 --- --- --- --- 18 22 | 58 77 --- --- --- --- 72 65
------+----------------------------------------------+------------------------------------------
RMS | 1276 25 29 26 32 33 27 20 |T 71 75 62 66 77 72 69 67
WRMS | 1276 24 27 26 24 15 24 20 |NE 55 60 49 47 60 56 54 52
MEDI | 856 16 22 21 19 19 18 17 |MD 61 72 50 49 74 60 55 55
Table 3.2100.2 GPS week: 2100 Day: 2 MJD: 58946
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1618 39 39 34 69 17 29 18 16 | 80 85 55 46 61 63 63 57
R02 | 1525 9 15 30 18 13 15 27 9 | 48 43 44 45 41 38 62 44
R03 | 776 12 11 19 32 17 19 26 9 | 63 61 45 40 51 63 77 55
XR04 | 587 15 23 19 43 --- 17 21 12 | 68 68 66 44 --- 66 77 62
R05 | 522 15 15 14 27 15 16 19 8 | 55 45 44 35 54 52 56 48
R07 | 587 25 23 16 40 8 27 16 10 | 66 65 51 35 54 69 45 51
R08 | 756 27 28 14 9 19 11 14 7 | 58 58 46 42 36 42 39 42
R09 | 2123 11 11 14 15 14 19 13 6 | 16 18 18 25 30 30 32 23
R11 | 1154 6 13 17 5 12 18 16 6 | 42 43 33 40 49 45 38 40
R12 | 939 18 18 21 30 16 15 15 8 | 63 62 50 46 67 51 55 55
R13 | 2820 36 36 43 63 52 31 35 20 | 74 80 77 54 101 93 96 82
R14 | 1895 14 23 19 15 11 16 14 6 | 56 60 47 43 49 60 56 51
R15 | 692 8 13 11 21 8 20 17 6 | 72 74 65 59 67 76 70 67
R16 | 745 33 21 54 20 39 58 32 18 | 67 84 82 68 66 75 75 69
R17E | 1296 19 14 29 21 19 27 41 12 | 107 110 107 99 107 111 112 105
R18E | 657 34 15 25 15 18 25 17 10 | 174 193 191 186 190 196 194 188
R19E | 1075 65 54 41 32 24 68 37 20 | 52 46 29 46 46 51 41 29
R20E | 1093 23 41 69 77 90 43 44 28 | 39 59 51 41 96 24 47 41
R21E | 1872 19 18 33 23 13 24 33 11 | 175 175 169 163 161 171 163 166
R22E | 2322 19 18 26 15 20 23 21 9 | 119 119 62 117 138 135 119 122
R23E | 560 30 32 36 29 19 46 12 13 | 206 204 207 219 218 230 216 215
R24 | 1434 53 53 58 19 25 49 29 18 | --- --- --- --- --- --- --- 0
XR26E | ---- 32 89 --- --- --- --- 27 30 | 86 117 --- --- --- --- 100 91
------+----------------------------------------------+------------------------------------------
RMS | 1410 29 27 33 34 29 32 26 |T 81 84 73 71 84 82 83 77
WRMS | 1410 21 22 33 27 13 28 26 |NE 59 60 51 44 55 58 60 53
MEDI | 1075 19 21 25 21 17 23 21 |MD 66 65 51 46 61 63 63 55
Table 3.2100.3 GPS week: 2100 Day: 3 MJD: 58947
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1727 41 44 28 90 19 15 22 18 | 87 93 57 43 64 67 71 60
R02 | 1100 9 19 26 12 8 11 28 7 | 56 65 33 48 51 51 54 47
R03 | 793 10 13 27 29 14 11 28 8 | 73 74 48 48 72 67 83 64
XR04 | 539 14 11 28 42 --- 13 34 13 | 73 72 71 43 --- 62 88 65
R05 | 576 14 15 12 22 13 12 36 8 | 54 64 48 50 56 47 78 52
R07 | 1004 15 19 12 29 13 13 13 7 | 72 78 58 44 62 64 67 61
R08 | 564 12 11 13 23 19 11 15 7 | 61 66 53 46 66 48 47 53
R09 | 1748 16 18 14 11 17 19 22 7 | 23 28 23 26 27 22 34 22
R11 | 851 6 12 19 12 20 14 14 6 | 45 48 43 46 54 55 43 47
R12 | 725 19 12 28 29 20 11 22 9 | 56 54 48 41 53 51 59 49
R13 | 2051 26 35 30 64 47 68 51 22 | 83 89 68 60 94 67 102 75
R14 | 2674 13 15 20 25 12 14 9 7 | 54 55 42 54 57 55 51 51
R15 | 920 12 13 12 29 17 17 25 8 | 66 65 55 49 59 68 80 62
R16 | 1093 32 31 49 32 30 32 28 15 | 58 57 46 62 61 62 73 56
R17E | 571 18 21 43 25 14 22 58 14 | 96 99 97 96 98 92 109 95
R18E | 752 43 29 37 18 37 30 35 15 | 181 184 182 174 169 186 167 174
R19E | 916 57 51 33 41 28 35 33 17 | 90 91 60 68 73 60 47 61
R20E | 2341 29 36 69 77 93 39 33 27 | 53 43 57 56 102 72 52 54
R21E | 1693 18 23 31 25 15 28 71 15 | 164 166 156 158 154 155 176 157
R22E | 1857 20 22 31 20 20 26 22 10 | 138 137 100 124 193 134 136 133
R23E | 666 20 20 21 39 18 20 29 10 | 185 188 185 192 190 182 195 187
R24 | 630 39 46 68 27 33 39 54 19 | --- --- --- --- --- --- --- 0
XR26E | ---- 36 76 --- --- --- --- 56 44 | 65 135 --- --- --- --- 118 79
------+----------------------------------------------+------------------------------------------
RMS | 1355 26 27 34 38 30 27 34 |T 83 88 72 72 87 79 87 77
WRMS | 1355 20 21 34 29 18 21 34 |NE 61 64 49 47 59 56 66 54
MEDI | 916 18 20 28 27 19 17 28 |MD 66 72 57 50 64 64 73 61
Table 3.2100.4 GPS week: 2100 Day: 4 MJD: 58948
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1460 46 48 32 84 40 15 17 19 | 86 88 60 37 43 60 69 57
R02 | 886 17 22 18 23 9 14 13 7 | 48 56 32 34 43 46 41 40
R03 | 567 9 10 24 30 23 18 16 9 | 60 64 42 44 80 77 63 62
XR04 | 831 10 20 29 34 --- 21 28 12 | 71 83 74 58 --- 78 84 72
R05 | 852 19 10 20 38 42 15 27 12 | 49 56 48 49 78 53 65 52
R07 | 1239 15 14 21 21 19 17 12 7 | 74 76 66 69 95 89 87 80
R08 | 850 8 11 16 15 22 10 18 6 | 58 62 50 59 73 56 45 56
R09 | 1896 10 11 12 18 18 24 16 7 | 21 22 23 24 28 26 30 22
R11 | 961 9 13 14 11 8 16 13 5 | 38 37 32 34 39 29 40 34
R12 | 745 11 30 38 21 29 10 12 9 | 58 74 33 49 71 50 55 52
R13 | 2048 22 31 49 53 27 60 42 19 | 75 77 52 58 93 93 87 77
R14 | 2620 15 18 13 16 21 11 12 6 | 47 50 35 45 51 38 38 41
R15 | 1126 11 11 15 34 16 9 29 8 | 64 65 63 52 74 68 88 68
R16 | 1040 18 21 39 33 33 28 37 14 | 55 58 46 49 62 52 79 56
R17E | 1782 20 14 35 18 15 12 21 9 | 86 86 90 85 92 87 87 86
R18E | 754 17 10 29 12 15 15 12 7 | 135 133 141 137 138 128 138 135
R19E | 826 43 77 47 54 32 39 53 20 | 85 107 88 94 92 101 106 88
R20E | 3264 38 54 57 59 93 47 43 25 | 65 102 62 82 116 75 78 70
R21E | 1600 11 12 35 19 11 17 24 9 | 124 125 125 124 122 116 125 121
R22E | 1579 21 18 30 18 14 31 36 11 | 171 193 69 174 367 175 160 166
R23E | 912 11 21 24 31 25 19 22 9 | 241 236 235 247 238 244 235 239
XR24 | 1388 28 27 65 35 61 --- 34 23 | --- --- --- --- --- --- --- 0
XR26E | ---- 18 116 --- --- --- --- 28 22 | 90 112 --- --- --- --- 85 86
------+----------------------------------------------+------------------------------------------
RMS | 1511 21 29 31 35 31 25 27 |T 81 89 69 76 99 82 85 80
WRMS | 1511 15 18 32 26 16 19 27 |NE 57 62 46 47 63 58 62 54
MEDI | 1040 17 18 29 23 22 17 22 |MD 65 76 60 58 78 75 79 68
Table 3.2100.5 GPS week: 2100 Day: 5 MJD: 58949
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1086 44 42 36 79 20 25 18 17 | 80 79 57 39 51 69 67 58
R02 | 1163 20 12 17 16 16 12 16 7 | 46 40 37 34 32 45 31 36
R03 | 661 9 6 22 29 9 31 12 8 | 58 55 39 38 51 75 44 52
XR04 | 888 19 16 25 25 --- 20 22 11 | 54 53 48 52 --- 73 66 58
R05 | 1045 16 8 21 21 20 18 32 9 | 44 46 43 55 54 38 62 46
R07 | 1023 11 12 16 29 14 12 9 7 | 63 64 59 48 69 62 60 61
R08 | 612 9 11 24 20 15 11 14 7 | 56 60 50 50 68 66 68 61
R09 | 1281 11 12 18 10 16 12 10 6 | 15 13 25 29 29 21 27 21
R11 | 1044 7 9 15 7 12 16 16 5 | 34 33 26 33 31 26 36 29
R12 | 797 11 9 37 36 15 10 28 10 | 53 48 44 48 59 53 66 52
R13 | 949 24 33 50 59 24 37 36 16 | 72 85 54 55 90 85 92 76
R14 | 1235 15 19 16 13 13 13 10 6 | 44 53 37 48 49 37 38 42
R15 | 1229 15 19 16 19 9 20 22 7 | 55 61 53 55 53 52 59 53
R16 | 1617 27 23 42 34 23 28 26 13 | 49 62 88 77 89 62 84 71
R17E | 2085 15 10 26 23 12 18 13 8 | 75 75 74 81 75 69 73 73
R18E | 1200 9 9 23 10 10 21 8 6 | 85 87 86 85 89 85 85 86
R19E | 562 40 31 61 55 28 48 72 22 | 86 93 67 55 78 53 107 69
R20E | 2477 36 75 87 60 52 66 70 27 | 70 84 82 59 100 67 92 68
R21E | 2180 12 20 35 18 17 24 15 9 | 99 103 96 99 106 97 100 99
XR22E |17275 25 339 --- --- 1708 32 17 18 | 116 298 --- --- 9999 117 119 114
R23E | 924 21 15 26 24 25 25 15 10 | 160 165 161 168 171 171 165 165
XR24 | 6265 --- --- --- --- --- --- 2 0 | --- --- --- --- --- --- --- 0
XR26E | ---- 23 48 --- --- --- --- 37 30 | 50 55 --- --- --- --- 63 52
------+----------------------------------------------+------------------------------------------
RMS | 1323 21 25 36 35 21 27 29 |T 66 77 61 60 70 67 72 65
WRMS | 1323 16 16 28 27 13 23 29 |NE 51 53 47 47 55 54 57 51
MEDI | 1086 15 15 24 23 16 20 16 |MD 56 61 53 52 68 66 66 58
Table 3.2100.6 GPS week: 2100 Day: 6 MJD: 58950
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1149 40 46 42 78 15 12 16 16 | 111 119 90 43 82 86 79 81
R02 | 1076 17 22 21 13 14 12 22 7 | 60 63 47 47 52 56 46 50
R03 | 665 14 17 16 38 9 15 10 8 | 79 80 56 48 74 87 72 69
XR04 | 979 13 13 21 46 --- 15 28 13 | 77 80 65 51 --- 90 98 76
R05 | 953 18 18 20 27 19 12 22 9 | 56 56 46 50 61 63 68 56
R07 | 1290 11 13 15 19 15 17 15 7 | 86 87 72 65 89 89 80 81
R08 | 518 14 14 16 16 19 26 14 8 | 75 74 63 66 69 87 79 72
R09 | 1639 16 22 14 14 17 24 13 7 | 25 24 29 29 36 28 32 27
R11 | 1401 7 12 15 8 10 20 7 5 | 48 52 43 51 55 52 49 49
R12 | 800 12 23 19 24 9 14 16 7 | 73 77 60 58 72 65 75 66
R13 | 1727 24 22 31 70 34 40 33 17 | 96 98 85 55 102 107 111 93
R14 | 868 10 11 26 19 12 21 9 7 | 66 70 44 57 66 73 61 61
R15 | 896 12 8 22 32 13 26 13 8 | 85 86 74 65 83 99 93 83
R16 | 1536 21 21 34 27 34 52 25 14 | 66 70 73 76 86 82 89 76
R17E | 2029 14 14 28 21 12 15 11 7 | 73 72 80 73 76 74 73 73
R18E | 876 8 11 20 13 15 17 10 6 | 100 101 103 97 96 106 100 99
R19E | 988 51 39 47 26 39 48 35 19 | 66 64 61 63 65 55 52 54
R20E | 1437 39 47 59 37 72 75 42 25 | 70 71 76 82 98 72 62 67
R21E | 1796 14 18 30 21 19 24 10 8 | 108 103 104 105 100 111 103 104
R23E | 2005 19 27 25 29 21 21 16 9 | 175 178 174 174 181 180 173 175
XR24 | 9245 4 10 --- --- --- --- --- 0 | --- --- --- --- --- --- --- 0
XR26E | ---- 21 36 --- --- --- --- 21 21 | 59 69 --- --- --- --- 64 61
------+----------------------------------------------+------------------------------------------
RMS | 1320 22 24 29 33 26 30 20 |T 80 82 72 70 99 85 81 77
WRMS | 1320 16 19 29 28 15 24 20 |NE 71 74 60 54 71 76 73 67
MEDI | 1149 14 18 21 24 15 20 16 |MD 73 74 65 63 76 86 75 72
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