[IGSREPORT-27020] Wk 2085 IGLOS Final Orbits
acc
acc at igs.org
Sat Jan 11 17:15:38 PST 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2085 (Dec 22, 2019 - Dec 28, 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 2.2085.
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:
igl2085[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2085 in the SP3 format.
igl20857.sum Combination Report for GPS Week 2085.
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 | -3.4 ns
1 | -4.5 ns
2 | -5.8 ns
3 | -5.0 ns
4 | -5.3 ns
5 | -5.0 ns
6 | -4.2 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 1.2085, 1a.2085).
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 2.2085.0-6)
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 3.2085.0-6).
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 2085 summary. (Dec 22, 2019 - Dec 28, 2019)
Table 1.2085.a GPS week : 2085 MJD: 58839.0-58845.0
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 18 24 56 .09 26 23 | 7147807 7694 715498 719152
| 0 1 1 21 17 20 .03 | 4871044 8208
cof n/a| 0 0 0 19 32 55 .09 28 25 | 7147806 7705 715495 719131
| 1 1 1 14 14 30 .04 | 4871045 8217
emx n/a| 1 -1 -5 75 21 -16 .09 29 29 | -6762 -222 3047 8237
| 1 0 2 17 13 42 .04 | 7403 1322
esx n/a| 0 0 0 7 -5 6 .11 25 22 | -5123 -1560 3188 14647
| 0 1 1 13 14 28 .03 | 8392 1590
gfz n/a| 0 0 3 -5 -15 18 .13 27 18 | 0 -157 3051 8055
| 1 1 2 13 11 34 .04 | 0 1265
grg n/a| 1 0 -2 -75 -18 -93 -.36 27 22 | -3516 -145 3203 12375
| 1 0 1 26 20 75 .04 | 3339 1400
iac n/a| -2 0 5 -4 -5 41 -.12 31 27 | 7141304 625 574598 718876
| 1 1 2 20 22 58 .04 | 4882150 4630
mcc n/a| 4 2 15 -43 -30 -724 -.01 246 246 | --- --- --- ---
| 12 10 31 96 111 772 .65 | --- ---
Table 1.2085.b GPS week : 2085 MJD: 58839.0-58845.0
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 18 19 19 18 20 |
R02 | 7 6 7 7 6 9 7 |
R03 | 7 7 8 6 6 7 7 |
R04 | --- --- --- --- --- 0 24 |
R05 | 10 9 10 9 9 9 8 |
R07 | 6 8 8 8 8 8 10 |
R08 | 5 8 10 6 8 8 7 |
R09 | 7 8 7 6 7 7 12 |
R11 | 7 8 8 6 7 6 7 |
R12 | 8 8 9 10 9 8 8 |
R13 | 9 9 9 12 8 10 8 |
R14 | 7 8 9 7 10 10 9 |
R15 | 7 8 9 8 10 9 8 |
R16 | 12 11 10 9 12 12 16 |
R17 | 12 10 10 11 13 12 11 |
R18 | 8 8 8 7 6 5 6 |
R19 | 29 32 34 32 30 33 30 |
R20 | 17 16 22 21 18 19 16 |
R21 | 11 11 12 10 12 11 10 |
R22 | 10 11 11 11 10 12 10 |
R23 | 10 11 10 9 10 11 10 |
R26 | 17 14 15 31 25 18 15 |
Table 1.2085.c GPS week : 2085 MJD: 58839.0-58845.0
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 2085 0 | -51 46 191 -1002 -504 -1302 83.3 1447 1447 | -3357 0
brd 2085 1 | 50 -8 111 -267 1288 -1333 85.2 1444 1444 | -4506 0
brd 2085 2 | -38 14 142 -949 1138 -688 83.4 1533 1533 | -5811 0
brd 2085 3 | 1 33 136 514 644 -1042 83.2 1548 1548 | -5049 0
brd 2085 4 | 71 64 110 -1046 2301 -3335 82.0 1645 1645 | -5272 0
brd 2085 5 | -3 46 156 -769 1135 -2041 81.7 1531 1531 | -4980 0
brd 2085 6 | 23 54 92 -639 2289 -3409 82.7 1481 1481 | -4184 0
-------------+------------------------------------------------------------+----------------
brd 2085 mean| 7 35 134 -594 1184 -1878 83.1 1518 1518 | -4737 0
brd 2085 sdev| 44 25 33 557 968 1098 1.2 69 69 | 802 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 2.2085.0 GPS week: 2085 Day: 0 MJD: 58839
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 -9 0 63 .12 24 23 | 14992 2009 4941 21367
cof n/a| 0 0 -1 12 53 57 .12 27 27 | 14981 2021 4939 21358
emx n/a| 0 0 -9 56 16 -55 .15 26 26 | -9512 1825 2936 7825
esx n/a| 0 0 0 18 0 64 .13 25 23 | -12150 1313 2924 10018
gfz n/a| -3 0 5 -6 -28 63 .16 28 16 | 0 1887 2926 7646
grg n/a| 0 0 -2 -57 -6 -139 -.41 21 18 | -4431 2043 2933 6897
iac n/a| 0 -1 5 23 -41 70 -.09 29 25 | -6681 333 4773 20016
mcc n/a| -6 2 -9 -68 -40 650 -1.26 343 343 | --- --- --- ---
Table 2.2085.1 GPS week: 2085 Day: 1 MJD: 58840
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 31 54 80 .10 24 22 | 19667 908 3554 12702
cof n/a| 1 0 2 14 49 26 .07 28 25 | 19671 880 3537 12565
emx n/a| 0 -1 -8 59 33 -81 .09 25 25 | -7439 1222 2880 9186
esx n/a| 0 0 -2 -12 -28 7 .11 24 20 | -6430 -993 2868 11332
gfz n/a| 0 0 4 -12 -22 32 .12 28 19 | 0 1048 2889 8956
grg n/a| 0 2 0 -36 -24 -153 -.41 30 24 | -5002 983 2865 8301
iac n/a| -4 -1 10 -20 -4 140 -.06 32 27 | -4184 38 3438 12125
mcc n/a| -12 -4 48 125 163 -1185 .64 274 274 | --- --- --- ---
Table 2.2085.2 GPS week: 2085 Day: 2 MJD: 58841
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 11 37 78 .06 25 22 | 9999999 19311 999999 999999
cof n/a| -1 0 1 17 21 114 .04 29 25 | 9999999 19313 999999 999999
emx n/a| 2 0 -7 95 -2 -14 .05 30 30 | 1812 -1639 2899 8175
esx n/a| 0 1 0 17 -2 3 .05 26 22 | 8404 -3274 2912 10236
gfz n/a| 1 -1 1 -2 -21 60 .12 30 20 | 0 -1730 2921 8020
grg n/a| 2 0 -2 -80 -48 -189 -.38 31 25 | -4610 -2191 2920 7583
iac n/a| -4 0 5 -25 8 48 -.09 31 27 | 9999999 -5072 999999 999999
mcc n/a| 2 -14 58 -96 -144 -1431 -.03 236 236 | --- --- --- ---
Table 2.2085.3 GPS week: 2085 Day: 3 MJD: 58842
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 -5 26 43 .08 28 25 | 9999999 -3320 999999 999999
cof n/a| 0 0 0 -1 23 24 .11 30 26 | 9999999 -3298 999999 999999
emx n/a| 0 -1 -5 57 29 -3 .04 32 32 | -14616 -360 3000 7704
esx n/a| 0 1 0 12 -18 -1 .06 22 18 | -17884 -1006 2995 9911
gfz n/a| 0 0 1 15 2 -3 .13 26 19 | 0 -380 2998 7553
grg n/a| 3 0 -2 -54 -43 -86 -.36 28 23 | -5004 -1 2998 7256
iac n/a| -2 0 5 -19 27 29 -.15 29 25 | 9999999 2144 999999 999999
mcc n/a| 13 17 17 4 -134 -1561 .70 258 258 | --- --- --- ---
Table 2.2085.4 GPS week: 2085 Day: 4 MJD: 58843
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 16 21 65 .08 27 23 | 9999999 9298 999999 999999
cof n/a| -1 0 -2 19 18 64 .08 29 24 | 9999999 9324 999999 999999
emx n/a| 1 -1 -4 83 28 -21 .12 32 32 | -11494 -1212 2879 8989
esx n/a| 0 0 1 -9 -10 -2 .12 25 24 | -1405 -2319 2885 10661
gfz n/a| 0 0 4 -26 -23 -20 .07 23 17 | 0 -523 2887 8742
grg n/a| 1 0 -5 -93 -5 -91 -.31 28 21 | -5189 -275 2895 8113
iac n/a| -2 1 3 19 7 56 -.15 31 27 | 9999999 -3852 999999 999999
mcc n/a| 9 14 -32 -184 -112 -762 .18 230 230 | --- --- --- ---
Table 2.2085.5 GPS week: 2085 Day: 5 MJD: 58844
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 2 -2 50 10 26 .05 26 23 | 9999999 10151 999999 999999
cof n/a| -1 0 -1 36 31 51 .07 28 26 | 9999999 10123 999999 999999
emx n/a| 2 0 -2 83 30 17 .05 31 31 | 5191 -1315 3358 8507
esx n/a| -1 -2 1 1 9 4 .14 27 26 | -1696 -3221 3364 10308
gfz n/a| 0 0 2 6 -17 12 .19 31 21 | 0 -1303 3370 8336
grg n/a| 0 0 -3 -104 5 -21 -.35 26 23 | -4404 -1363 3384 7904
iac n/a| 0 0 5 3 -13 -24 -.12 30 27 | 9999999 1657 999999 999999
mcc n/a| 23 3 12 -69 33 -551 -.17 186 186 | --- --- --- ---
Table 2.2085.6 GPS week: 2085 Day: 6 MJD: 58845
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 -1 34 24 38 .13 28 24 | 9999999 15504 999999 999999
cof n/a| 0 2 -2 40 25 47 .16 27 24 | 9999999 15577 999999 999999
emx n/a| 3 -2 -1 95 12 45 .09 31 31 | -11276 -75 3379 7279
esx n/a| 0 -2 1 20 10 -31 .12 25 22 | -4705 -1423 4371 40063
gfz n/a| -1 2 0 -9 -1 -16 .12 25 15 | 0 -104 3368 7136
grg n/a| 1 0 0 -103 -7 25 -.33 24 19 | 4025 -215 4430 40577
iac n/a| -3 0 1 -11 -21 -30 -.19 33 28 | 9999999 9130 13984 999999
mcc n/a| 1 1 15 -15 20 -228 -.12 197 197 | --- --- --- ---
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 3.2085.0 GPS week: 2085 Day: 0 MJD: 58839
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 800 39 45 48 53 16 22 26 --- 16 | 88 94 87 44 62 43 43 --- 55
R02 | 1138 14 18 16 11 15 14 16 286 6 | 48 49 48 41 42 37 36 124 40
R03M | 719 10 9 12 17 13 18 24 437 7 | 57 57 60 48 56 52 52 385 52
R05 | 901 25 31 18 22 24 18 18 --- 9 | 55 63 53 49 57 46 36 --- 47
R07 | 601 14 19 11 12 10 15 20 468 6 | 71 74 67 68 68 66 58 181 65
R08 | 765 9 11 8 10 12 12 10 --- 4 | 65 67 60 68 64 65 53 --- 62
R09E | 3788 14 10 17 11 18 19 13 --- 7 | 22 24 30 27 41 30 28 --- 24
R11E | 557 11 11 22 10 10 15 18 214 6 | 100 99 106 97 101 98 99 119 100
R12E | 847 15 18 21 15 9 13 32 --- 8 | 63 63 65 66 60 67 56 --- 62
R13E | 1543 13 11 28 15 22 18 16 --- 8 | 86 85 88 78 78 86 81 --- 82
R14E | 604 12 13 20 17 18 13 15 --- 7 | 124 122 127 126 127 122 127 --- 125
R15E | 1022 9 15 23 11 22 14 14 --- 7 | 80 82 82 78 84 83 79 --- 80
R16E | 1161 17 19 30 12 41 30 27 --- 12 | 37 41 41 43 65 38 35 --- 38
R17M | 858 19 20 23 22 26 22 42 --- 11 | 76 77 47 48 79 71 34 --- 59
R18 | 645 13 13 18 24 13 15 17 --- 7 | 56 56 42 56 57 45 51 --- 50
R19 | 1318 59 61 60 65 81 33 81 --- 28 | 108 105 42 73 133 97 25 --- 70
R20M | 1781 38 44 37 21 44 51 27 --- 17 | 69 68 38 44 71 70 32 --- 49
R21M | 1393 22 27 17 23 32 12 30 226 10 | 67 70 48 46 70 63 33 184 53
R22 | 2786 24 26 20 27 14 21 25 --- 10 | 66 68 44 44 59 68 38 --- 52
R23 | 1173 28 34 15 30 14 14 24 --- 10 | 37 35 38 61 43 36 55 --- 42
XR26M | 4467 14 46 --- --- --- --- 19 --- 17 | 48 86 --- --- --- --- 37 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1447 24 26 26 25 28 21 29 343 |T 67 70 60 60 70 64 51 198 59
WRMS | 1447 23 27 26 23 16 18 25 343 |NE 63 64 49 57 65 57 44 152 53
MEDI | 1022 14 19 20 17 16 15 20 286 |MD 66 68 48 49 64 65 43 181 53
Table 3.2085.1 GPS week: 2085 Day: 1 MJD: 58840
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 456 47 57 45 40 38 38 32 --- 18 | 61 68 60 36 51 36 31 --- 42
R02 | 969 10 18 9 8 19 16 21 129 6 | 39 47 39 39 50 33 25 108 37
R03M | 807 10 13 12 5 13 18 32 500 7 | 46 50 47 48 48 52 35 286 45
R05 | 1469 18 22 17 19 15 21 26 --- 8 | 38 41 44 46 43 28 25 --- 36
R07 | 1263 13 12 13 13 14 21 26 175 7 | 59 56 55 58 54 62 49 60 56
R08 | 825 16 20 11 17 17 18 22 --- 7 | 48 53 50 56 41 58 31 --- 47
R09E | 4286 14 12 17 12 22 12 24 --- 7 | 35 35 45 43 59 40 32 --- 37
R11E | 952 13 18 26 11 16 17 17 252 7 | 87 91 98 91 90 91 86 95 90
R12E | 987 20 19 26 13 16 12 20 --- 8 | 58 62 62 63 60 60 56 --- 58
R13E | 1480 11 18 20 18 27 25 12 --- 8 | 57 60 55 58 57 59 57 --- 55
R14E | 684 12 13 23 23 11 9 15 --- 7 | 99 102 103 105 105 101 99 --- 101
R15E | 684 11 11 26 10 17 24 19 --- 8 | 77 79 74 72 76 82 67 --- 73
R16E | 1103 17 25 23 15 44 23 19 --- 11 | 29 37 25 44 62 37 29 --- 33
R17M | 464 21 27 21 20 25 15 35 --- 10 | 45 50 31 34 46 38 32 --- 36
R18 | 904 13 9 20 13 19 11 21 --- 7 | 34 36 32 44 47 44 40 --- 39
R19 | 1277 57 60 53 72 81 84 87 --- 32 | 61 69 30 63 72 82 26 --- 42
R20M | 1479 33 43 37 14 24 59 41 --- 16 | 30 46 21 30 38 36 16 --- 26
R21M | 1500 30 27 16 20 20 14 37 124 10 | 36 37 31 24 32 24 20 109 25
R22 | 1328 25 24 17 24 13 31 30 --- 10 | 37 36 25 28 33 47 22 --- 29
R23 | 1408 26 33 11 33 21 24 20 --- 11 | 28 30 31 38 31 19 33 --- 26
XR26M | 4199 8 101 --- --- --- --- 19 --- 13 | 30 101 --- --- --- --- 30 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1443 24 28 25 24 28 30 32 274 |T 49 56 47 51 54 51 40 131 45
WRMS | 1443 22 25 25 20 19 24 27 274 |NE 43 46 38 46 46 46 31 84 39
MEDI | 1103 16 20 20 15 19 18 22 175 |MD 45 50 44 44 50 44 32 108 39
Table 3.2085.2 GPS week: 2085 Day: 2 MJD: 58841
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 492 45 48 39 28 34 56 28 --- 17 | 70 71 58 48 42 33 31 --- 44
R02 | 755 11 14 11 15 20 12 24 151 7 | 40 39 36 51 54 39 21 60 40
R03M | 822 15 22 21 12 15 19 23 428 8 | 52 58 51 44 46 60 33 159 45
R05 | 1389 25 19 24 22 15 19 21 --- 9 | 48 43 46 36 38 32 27 --- 35
R07 | 2040 12 14 17 21 15 20 22 124 8 | 59 62 59 56 67 62 57 90 58
R08 | 502 13 12 18 18 21 30 32 --- 10 | 57 56 55 66 63 77 45 --- 59
R09E | 4752 9 9 21 13 17 21 13 --- 7 | 45 47 47 38 48 51 41 --- 44
R11E | 1617 13 13 27 8 12 24 18 208 8 | 59 56 60 59 57 71 61 68 59
R12E | 1010 23 25 29 13 19 18 17 --- 9 | 50 51 43 45 53 46 44 --- 44
R13E | 1601 14 16 28 11 22 17 24 --- 8 | 85 87 88 84 90 88 80 --- 84
R14E | 1124 21 12 26 19 14 17 14 --- 8 | 66 66 64 66 59 68 63 --- 62
R15E | 682 20 17 24 12 23 17 14 --- 8 | 52 52 49 53 58 61 55 --- 53
R16E | 581 19 31 26 17 23 23 20 --- 9 | 24 31 27 39 48 30 34 --- 28
R17M | 424 23 21 23 15 24 14 35 --- 10 | 54 53 37 43 55 41 28 --- 42
R18 | 1087 21 22 24 21 11 15 13 --- 8 | 55 60 43 45 52 42 47 --- 46
R19 | 668 61 70 57 82 99 64 83 --- 34 | 77 81 50 67 109 69 31 --- 56
R20M | 776 37 48 66 26 28 75 45 --- 21 | 61 69 31 46 58 78 28 --- 45
R21M | 814 20 23 19 17 26 26 44 122 11 | 49 50 34 35 57 52 23 76 40
R22 | 799 27 29 22 22 19 23 33 --- 11 | 51 54 43 39 47 56 29 --- 41
R23 | 2138 16 30 14 33 14 22 21 --- 9 | 34 31 36 42 23 33 36 --- 30
XR26M | 3582 12 99 --- --- --- --- 17 --- 14 | 28 105 --- --- --- --- 26 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1532 25 29 30 26 30 31 31 236 |T 53 58 47 50 56 54 40 90 46
WRMS | 1532 22 25 30 22 20 25 27 236 |NE 52 53 46 50 56 51 36 75 45
MEDI | 822 20 22 24 17 19 20 22 151 |MD 52 56 46 45 54 52 34 76 44
Table 3.2085.3 GPS week: 2085 Day: 3 MJD: 58842
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 485 50 61 59 41 31 39 22 --- 18 | 73 82 76 34 47 33 36 --- 42
R02 | 1625 11 17 16 11 13 16 18 210 6 | 40 42 43 39 31 30 29 74 33
R03M | 750 14 19 16 13 8 8 21 398 6 | 54 55 50 44 51 51 39 116 47
R05 | 657 24 22 19 19 16 20 20 --- 8 | 47 50 46 42 44 50 28 --- 40
R07 | 2610 13 14 20 17 13 17 19 308 7 | 55 55 57 49 53 48 39 210 48
R08 | 833 11 14 11 16 7 12 15 --- 5 | 54 55 52 58 55 54 55 --- 54
R09E | 4371 13 14 16 8 15 12 14 --- 5 | 32 36 27 36 42 33 29 --- 32
R11E | 1578 8 7 22 7 10 17 16 161 6 | 45 42 41 44 40 46 44 79 42
R12E | 766 27 26 29 13 15 19 23 --- 9 | 46 48 34 35 44 38 33 --- 36
R13E | 1818 19 22 38 17 31 27 24 --- 11 | 62 63 62 68 80 70 62 --- 65
R14E | 1489 21 17 26 11 12 12 12 --- 7 | 41 39 36 38 38 35 28 --- 34
R15E | 655 14 17 27 9 17 11 22 --- 7 | 60 63 61 65 73 66 52 --- 62
R16E | 705 17 23 27 15 20 22 24 --- 9 | 29 36 30 28 42 42 31 --- 30
R17M | 660 31 38 18 17 19 14 36 --- 10 | 63 65 41 40 53 45 29 --- 43
R18 | 1575 15 14 20 12 17 17 13 --- 7 | 41 39 29 39 39 43 34 --- 36
R19 | 463 70 70 67 65 82 66 74 --- 31 | 85 85 40 38 96 73 33 --- 47
R20M | 780 41 41 59 25 34 68 46 --- 20 | 73 75 40 38 72 75 30 --- 52
R21M | 780 23 23 19 13 16 24 41 98 10 | 57 58 45 47 49 54 25 55 45
R22 | 668 23 20 20 19 17 24 37 --- 10 | 60 57 44 37 51 58 24 --- 44
R23 | 1758 29 26 23 21 13 12 13 --- 8 | 23 30 32 47 40 32 36 --- 34
XR26M | 4225 27 49 --- --- --- --- 33 --- 30 | 47 61 --- --- --- --- 32 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1547 28 30 32 22 26 28 29 258 |T 51 54 44 43 52 48 35 106 42
WRMS | 1547 25 26 32 18 19 23 25 258 |NE 50 51 42 43 51 48 34 142 42
MEDI | 780 21 22 20 15 16 17 22 210 |MD 54 55 41 39 47 46 33 79 42
Table 3.2085.4 GPS week: 2085 Day: 4 MJD: 58843
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 795 50 50 60 53 23 35 21 --- 19 | 71 68 69 30 43 37 30 --- 37
R02 | 2789 11 12 18 13 12 16 16 286 6 | 39 40 41 34 33 34 26 145 32
R03M | 719 9 6 11 15 10 12 22 338 6 | 55 54 51 55 51 51 42 68 50
R05 | 707 18 25 21 29 15 22 14 --- 9 | 51 55 47 30 47 51 37 --- 40
R07 | 1484 15 10 20 15 17 19 18 --- 7 | 56 52 55 50 46 59 44 --- 49
R08 | 853 15 19 20 18 20 14 13 --- 7 | 56 63 41 57 54 49 49 --- 50
R09E | 4694 18 19 17 7 15 22 15 --- 7 | 55 60 41 59 51 65 56 --- 57
R11E | 1137 9 10 22 11 13 18 12 98 6 | 80 80 79 74 83 89 76 172 80
R12E | 1224 21 24 29 13 17 19 19 --- 8 | 48 48 41 47 48 49 42 --- 44
R13E | 2631 13 14 27 11 12 21 13 --- 7 | 89 89 88 88 90 88 86 --- 87
R14E | 1197 18 19 29 16 16 32 27 --- 10 | 79 83 81 79 86 63 96 --- 79
R15E | 649 20 16 20 17 14 26 33 --- 9 | 99 99 93 108 106 101 99 --- 100
R16E | 761 22 22 41 16 21 31 32 --- 12 | 35 45 24 43 46 52 34 --- 35
R17M | 1803 28 26 20 27 27 17 43 --- 12 | 52 51 32 35 57 48 30 --- 40
R18 | 982 13 15 15 7 11 15 11 --- 5 | 35 34 30 29 32 21 21 --- 27
R19 | 514 70 75 60 61 71 64 78 --- 30 | 77 73 42 41 80 68 38 --- 48
R20M | 947 35 53 59 23 29 51 47 --- 18 | 72 89 38 40 66 75 28 --- 51
R21M | 780 26 26 22 21 13 30 43 75 11 | 56 56 42 36 48 60 32 70 44
R22 | 719 21 22 20 20 18 15 38 --- 10 | 51 51 43 40 53 47 29 --- 43
R23 | 1026 19 18 28 30 19 11 20 --- 10 | 32 32 38 44 30 31 32 --- 31
XR26M | 3411 22 85 --- --- --- --- 26 --- 24 | 37 99 --- --- --- --- 28 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1644 27 29 32 25 23 28 31 230 |T 58 62 50 50 57 56 45 113 50
WRMS | 1644 23 24 32 24 17 21 27 230 |NE 49 50 42 40 46 45 34 145 40
MEDI | 982 19 19 21 16 16 19 21 98 |MD 55 56 42 43 51 51 37 70 44
Table 3.2085.5 GPS week: 2085 Day: 5 MJD: 58844
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 1077 48 53 48 48 25 22 38 --- 18 | 90 93 90 73 73 72 64 --- 72
R02 | 2351 17 22 23 21 18 17 13 203 8 | 31 33 31 25 26 26 20 168 22
R03M | 524 14 17 13 9 9 15 27 158 7 | 82 84 81 80 74 90 76 205 80
XR04 |10860 4 415 --- --- --- --- --- --- 0 | 95 238 --- --- --- --- --- --- 99
R05 | 967 15 20 18 22 25 12 26 --- 9 | 42 49 41 34 62 41 25 --- 39
R07 | 576 14 18 19 13 12 11 33 185 8 | 45 50 45 47 50 48 32 243 43
R08 | 984 18 23 17 17 21 12 13 --- 7 | 42 43 35 39 49 49 33 --- 39
R09E | 3820 16 16 12 11 26 9 20 --- 7 | 53 56 32 56 44 56 47 --- 53
R11E | 1262 10 11 19 10 14 11 16 257 6 | 92 94 98 90 94 90 83 212 90
R12E | 1171 20 24 26 12 19 12 13 --- 7 | 62 62 64 60 72 67 62 --- 63
R13E | 2061 17 17 30 18 31 20 16 --- 10 | 56 57 58 63 74 60 58 --- 60
R14E | 1357 25 16 24 9 31 21 15 --- 9 | 100 103 103 102 102 100 96 --- 99
R15E | 1427 16 20 20 15 20 19 30 --- 9 | 100 100 100 88 99 97 82 --- 93
R16E | 741 19 27 36 14 34 30 23 --- 12 | 46 46 38 40 67 51 39 --- 43
R17M | 2522 31 35 19 23 28 12 36 --- 11 | 46 50 39 33 47 35 27 --- 35
R18 | 1519 9 13 13 9 17 11 11 --- 5 | 38 39 33 34 30 31 35 --- 32
R19 | 524 60 64 70 77 97 71 69 --- 33 | 65 76 54 51 94 68 35 --- 51
R20M | 712 38 35 64 21 20 52 42 --- 18 | 50 40 24 33 41 52 43 --- 37
R21M | 697 27 33 20 21 15 25 34 80 11 | 87 91 83 78 85 85 74 128 81
R22 | 1064 22 23 22 16 22 24 44 --- 11 | 40 41 32 38 45 40 22 --- 34
R23 | 579 15 18 24 40 14 20 11 --- 10 | 35 33 32 56 39 32 35 --- 37
XR26M | 3002 16 70 --- --- --- --- 19 --- 18 | 23 67 --- --- --- --- 31 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1530 26 28 31 27 31 26 30 186 |T 60 70 55 56 63 59 48 191 55
WRMS | 1530 23 26 31 26 21 23 27 186 |NE 48 66 37 40 49 41 29 205 44
MEDI | 1077 17 22 20 16 20 17 23 185 |MD 50 56 41 51 62 52 39 205 43
Table 3.2085.6 GPS week: 2085 Day: 6 MJD: 58845
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 727 64 49 55 42 36 32 38 --- 20 | 101 108 95 90 104 81 78 --- 87
R02 | 1427 13 16 17 14 9 8 27 98 6 | 45 46 42 35 35 36 26 128 35
R03M | 779 14 16 14 15 17 12 25 274 7 | 145 145 143 143 146 139 137 149 141
XR04 |20304 27 36 --- --- 20 --- --- --- 23 | 58 137 --- --- 9 --- --- --- 61
R05 | 1555 13 8 16 19 19 15 24 --- 8 | 54 56 53 59 62 48 33 --- 50
R07 | 1185 23 31 25 18 15 14 39 126 10 | 67 69 68 58 70 59 43 133 59
R08 | 1357 17 17 14 15 12 18 16 --- 7 | 63 64 53 63 60 66 51 --- 59
XR09E | 2726 14 26 --- 16 --- 27 20 --- 11 | 51 57 --- 49 --- 51 64 --- 53
R11E | 634 12 12 22 13 13 13 17 283 6 | 144 145 150 147 152 160 154 153 150
R12E | 1271 17 16 19 6 23 19 15 --- 7 | 69 70 76 71 70 75 69 --- 69
R13E | 3394 11 14 24 12 22 15 12 --- 7 | 78 76 79 76 81 81 78 --- 78
R14E | 1150 17 15 24 14 14 17 38 --- 9 | 136 139 140 137 139 141 144 --- 138
R15E | 1086 20 18 22 14 14 11 18 --- 7 | 129 130 128 130 134 132 124 --- 129
R16E | 1060 28 22 33 23 26 30 66 --- 15 | 77 85 86 94 99 96 54 --- 83
R17M | 2157 21 19 19 21 16 26 39 --- 10 | 84 83 62 63 81 83 49 --- 70
R18 | 1703 17 18 10 13 11 14 9 --- 5 | 54 56 50 54 51 46 54 --- 50
R19 | 848 55 56 76 69 71 59 68 --- 30 | 111 110 48 47 129 101 34 --- 72
R20M | 1377 45 52 55 25 24 37 24 --- 16 | 79 83 44 48 71 67 37 --- 55
R21M | 872 30 22 23 16 20 12 34 118 10 | 136 134 122 125 130 131 122 142 127
R22 | 2047 25 27 20 22 19 17 34 --- 10 | 70 70 48 47 67 64 36 --- 55
R23 | 712 19 18 17 31 10 25 13 --- 9 | 43 48 41 69 51 39 55 --- 48
XR26M | 5203 13 250 --- --- --- --- 16 --- 15 | 37 212 --- --- --- --- 40 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1480 28 27 31 25 25 24 33 197 |T 83 96 80 80 87 84 70 141 77
WRMS | 1480 24 24 31 22 15 19 28 197 |NE 62 72 50 54 59 57 41 130 54
MEDI | 1271 17 18 22 16 17 17 24 126 |MD 70 83 68 63 71 75 54 142 61
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