[IGSREPORT-28686] Wk 2209 IGLOS Final Orbits
acc
acc at igs.org
Fri May 27 06:37:47 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2209 (May 08, 2022 - May 14, 2022)
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 2.2209.
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:
igl2209[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2209 in the SP3 format.
igl22097.sum Combination Report for GPS Week 2209.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -0.2 ns
1 | -0.4 ns
2 | 0.3 ns
3 | 0.4 ns
4 | -0.4 ns
5 | -0.1 ns
6 | -7.0 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 1.2209, 1a.2209).
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 2.2209.0-6)
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 3.2209.0-6).
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 2209 summary. (May 08, 2022 - May 14, 2022)
Table 1.2209.a GPS week : 2209 MJD: 59707.0-59713.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -4 19 -24 13 .13 23 19 | 646581 9343 103443 291710
| 1 0 3 14 22 34 .04 | 1100133 24206
emx n/a| 0 2 2 34 4 -2 -.02 48 34 | 96 -280 3381 8488
| 1 2 2 27 32 49 .08 | 6433 911
esx n/a| 0 0 2 24 38 -55 -.07 37 25 | -28 271 3512 11061
| 1 1 2 13 19 41 .01 | 13732 1361
gfz n/a| 0 0 0 -18 -2 5 .00 32 16 | 0 -284 3532 8488
| 1 1 2 22 21 41 .03 | 0 938
grg n/a| 1 0 9 -48 25 29 .23 33 23 | -963 -429 3432 8084
| 1 1 1 23 22 76 .07 | 2791 1026
iac n/a| 0 -1 -6 2 -8 -11 -.20 22 20 | 583844 9148 98335 291970
| 1 1 2 14 33 41 .06 | 1044642 21643
Table 1.2209.b GPS week : 2209 MJD: 59707.0-59713.0
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 12 12 13 13 15 11 |
R02 | 9 6 7 7 6 7 9 |
R03 | 9 8 7 6 7 6 6 |
R04 | 10 9 8 9 7 12 11 |
R05 | 8 9 7 9 9 9 8 |
R07 | 7 7 8 6 6 8 8 |
R08 | 9 7 6 7 6 6 9 |
R09 | 6 6 7 8 7 7 7 |
R11 | 7 9 8 7 8 9 10 |
R12 | 8 7 6 8 7 7 8 |
R13 | 16 22 15 13 13 15 15 |
R14 | 13 25 99 20 19 8 11 |
R15 | 7 8 7 7 8 10 7 |
R17 | 7 9 8 8 7 8 8 |
R18 | 8 11 11 10 9 10 7 |
R19 | 28 26 28 25 23 26 25 |
R20 | 25 27 27 28 25 29 24 |
R21 | 8 9 10 11 9 9 9 |
R22 | 32 33 39 34 26 29 33 |
R24 | 9 12 11 12 11 12 13 |
Table 1.2209.c GPS week : 2209 MJD: 59707.0-59713.0
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 2209 0 | 12 13 41 562 553 8495 82.5 1495 1495 | -206 0
brd 2209 1 | 30 -63 92 1768 -488 2090 83.0 1172 1172 | -432 0
brd 2209 2 | 78 -13 178 -513 71 2463 81.8 1171 1171 | 326 0
brd 2209 3 | 120 -9 95 999 -819 1260 81.9 1444 1444 | 392 0
brd 2209 4 | -27 -23 80 -2252 -1658 -2366 83.6 1330 1330 | -381 0
brd 2209 5 | -78 75 155 -1332 -1352 -3041 81.3 1411 1411 | -68 0
brd 2209 6 | 38 48 158 568 587 7436 80.8 1583 1583 | -7016 0
-------------+------------------------------------------------------------+----------------
brd 2209 mean| 25 4 114 -28 -443 2333 82.1 1372 1372 | -1055 0
brd 2209 sdev| 65 46 50 1406 891 4400 1.0 157 157 | 2648 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 2.2209.0 GPS week: 2209 Day: 0 MJD: 59707
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 -6 24 -48 34 .06 22 16 | 35480 54 3577 7426
emx n/a| 2 4 0 57 31 23 -.02 53 33 | -4606 490 3556 7245
esx n/a| 0 1 4 13 39 -6 -.06 37 20 | 9625 -739 3551 9895
gfz n/a| 1 0 2 11 0 53 -.02 32 14 | 0 -1088 3587 7095
grg n/a| 0 -4 13 -55 51 0 .29 37 22 | -6 -748 3552 6804
iac n/a| 0 0 -9 -13 -21 -63 -.13 24 22 | 2198 -305 3538 7817
Table 2.2209.1 GPS week: 2209 Day: 1 MJD: 59708
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 -9 25 -7 32 .13 28 22 | 34444 -262 4366 8478
emx n/a| 0 5 -1 23 -7 49 .04 49 37 | 2870 -1738 3771 8176
esx n/a| 0 0 0 26 0 -113 -.07 37 28 | -8598 1442 4302 10888
gfz n/a| 0 0 -1 -21 -27 -11 .01 37 16 | 0 -300 4156 7768
grg n/a| 3 -2 10 -89 30 77 .14 35 24 | 86 -1132 3722 7765
iac n/a| -2 -1 -1 7 19 -12 -.17 23 22 | 728 990 4275 8786
Table 2.2209.2 GPS week: 2209 Day: 2 MJD: 59709
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 -6 17 -51 19 .10 22 20 | 1613641 64151 701631 999999
emx n/a| 1 1 1 7 -41 33 -.02 47 30 | 9236 -1364 2896 8910
esx n/a| 0 -1 0 19 33 -45 -.07 28 18 | -13266 2002 3277 11771
gfz n/a| 2 -1 0 -25 -13 2 -.02 29 14 | 0 681 3309 9281
grg n/a| 1 0 7 -57 33 72 .17 26 20 | -289 695 3284 9116
iac n/a| -2 0 -3 25 45 -52 -.29 22 20 | 1502129 58125 666301 999999
Table 2.2209.3 GPS week: 2209 Day: 3 MJD: 59710
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 -2 0 0 -14 .19 24 17 | 2753043 2848 4476 999999
emx n/a| 0 0 6 35 -20 -18 .06 52 42 | -417 332 3561 9547
esx n/a| -1 1 0 29 46 -6 -.08 43 33 | 15459 416 3565 11796
gfz n/a| 0 0 -4 -8 7 -43 .03 29 14 | 0 594 3662 9761
grg n/a| 2 0 10 -21 23 106 .16 35 25 | -71 411 3594 9068
iac n/a| 2 -2 -4 -7 -30 -14 -.26 22 19 | 2584059 3679 4385 999999
Table 2.2209.4 GPS week: 2209 Day: 4 MJD: 59711
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 0 0 -30 65 .16 20 17 | 32675 -1678 3499 8390
emx n/a| 0 0 4 1 27 -29 .02 46 33 | 3502 -186 3423 8321
esx n/a| 1 -2 3 51 65 -99 -.09 41 29 | -2235 -2088 3454 10305
gfz n/a| 0 -1 0 1 38 -37 .02 35 21 | 0 -1932 3512 8173
grg n/a| 2 0 9 -56 -19 -111 .33 32 25 | 775 -2228 3439 7391
iac n/a| 1 0 -9 15 -2 41 -.20 15 13 | 1000 -636 3435 8827
Table 2.2209.5 GPS week: 2209 Day: 5 MJD: 59712
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 -1 25 -36 -25 .10 25 20 | 32589 -390 3281 8749
emx n/a| 0 3 3 81 51 21 -.18 49 29 | 1048 -17 3243 8638
esx n/a| 2 0 3 9 40 -46 -.06 39 29 | 15904 209 3228 11664
gfz n/a| 0 0 1 -32 0 13 .04 32 19 | 0 -72 3268 8648
grg n/a| 0 0 8 -37 21 77 .26 32 23 | 13 -286 3238 8088
iac n/a| -2 -4 -6 -10 -13 -24 -.14 21 19 | 2061 492 3225 9198
Table 2.2209.6 GPS week: 2209 Day: 6 MJD: 59713
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 2 -2 39 2 -20 .13 21 18 | 24201 681 3272 8932
emx n/a| -2 1 3 36 -6 -93 -.06 43 33 | -10960 521 3217 8580
esx n/a| 2 0 4 25 44 -69 -.08 36 22 | -17089 661 3209 11108
gfz n/a| 0 -2 -3 -56 -20 61 -.02 32 16 | 0 128 3235 8696
grg n/a| 0 0 8 -24 39 -12 .25 32 21 | -7249 280 3197 8357
iac n/a| 0 -2 -7 -3 -57 44 -.21 27 24 | -5263 1696 3187 9169
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 3.2209.0 GPS week: 2209 Day: 0 MJD: 59707
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 940 36 20 25 42 44 24 15 | 82 70 71 83 52 55 66
R02 | 3879 22 24 15 13 13 27 9 | 42 41 55 54 52 60 49
R03 | 816 13 18 15 9 11 34 8 | 49 54 54 59 65 76 58
XR04 | 757 12 20 26 --- 22 16 9 | 50 56 41 --- 41 52 47
R05 | 632 13 16 28 12 17 18 8 | 42 53 50 48 54 56 46
R07 | 1053 11 15 20 14 15 17 7 | 57 59 59 69 66 75 63
R08 | 1887 11 11 12 22 30 30 9 | 47 49 48 53 62 51 48
R09E | 1779 12 24 10 15 13 11 6 | 41 40 38 43 38 42 40
XR11E | 2370 --- 14 8 13 17 14 7 | --- 27 30 34 28 32 29
R12E | 714 11 28 10 21 19 14 7 | 81 74 85 89 86 85 82
R13E | 1022 21 44 35 57 23 32 16 | 90 93 97 116 102 88 93
R14E | 1800 14 19 23 16 63 20 12 | 93 86 74 81 117 77 85
R15E | 1294 8 28 12 12 15 16 6 | 89 88 87 94 93 85 88
R17 | 1227 16 30 13 9 17 13 7 | 58 39 45 50 55 48 49
R18 | 675 13 42 16 15 18 11 8 | 60 31 60 47 62 45 50
R19 | 1355 23 160 40 56 62 39 28 | 79 49 34 98 65 72 61
R20 | 886 35 92 81 45 57 32 25 | 96 48 34 102 102 62 66
R21 | 1040 14 37 15 12 12 21 8 | 51 25 33 49 48 48 43
R22 | 1519 50 59 108 77 92 20 31 | 48 71 98 53 48 44 40
R24 | 982 13 48 18 10 15 21 9 | 78 59 71 74 78 75 72
------+-----------------------------------------+-------------------------------------
RMS | 1495 22 53 37 32 37 24 |T 64 55 58 68 65 61 58
WRMS | 1495 16 33 20 14 22 22 |NE 59 50 53 64 60 58 54
MEDI | 1040 13 24 16 15 17 20 |MD 58 53 54 59 62 56 50
Table 3.2209.1 GPS week: 2209 Day: 1 MJD: 59708
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 818 33 26 20 24 36 22 12 | 47 41 46 51 21 48 39
R02 | 1765 16 18 13 12 11 14 6 | 26 31 32 41 39 44 34
R03 | 960 19 22 8 8 11 25 7 | 30 30 42 44 49 57 42
XR04 | 591 7 11 25 --- 12 24 9 | 30 35 23 --- 39 55 35
R05 | 704 15 16 24 13 15 24 8 | 25 30 30 27 40 45 30
R07 | 1244 11 13 20 12 10 19 6 | 37 34 30 38 37 43 35
R08 | 743 11 11 16 14 20 15 6 | 30 28 24 36 34 23 26
R09E | 2360 15 19 11 15 14 9 6 | 31 28 40 38 32 29 31
XR11E | 2057 --- 17 15 15 26 14 9 | --- 22 23 27 32 23 19
R12E | 708 10 23 13 15 18 13 6 | 54 54 56 61 62 57 56
R13E | 876 32 56 36 83 38 38 22 | 68 80 77 108 80 82 75
XR14E | 3221 22 --- 30 75 --- 32 25 | 57 --- 65 96 --- 48 54
R15E | 584 11 32 14 24 14 13 8 | 93 98 97 104 99 96 96
R17 | 1772 22 30 14 13 21 18 8 | 36 31 35 36 38 39 33
R18 | 746 25 32 19 15 12 35 11 | 40 18 29 29 37 31 26
R19 | 601 40 115 28 57 73 26 25 | 50 63 32 41 46 26 28
R20 | 1680 55 83 82 53 63 29 27 | 59 27 53 59 63 23 34
R21 | 619 15 41 19 14 16 15 9 | 33 25 25 31 36 33 28
R22 | 771 63 78 101 82 81 28 32 | 36 58 56 38 48 42 28
R24 | 1004 11 59 26 18 18 23 12 | 56 58 62 58 64 58 57
------+-----------------------------------------+-------------------------------------
RMS | 1172 28 49 37 37 35 23 |T 44 41 43 50 47 45 40
WRMS | 1172 22 37 28 16 24 22 |NE 38 36 37 40 42 40 33
MEDI | 818 16 26 19 15 18 22 |MD 37 31 35 41 39 43 34
Table 3.2209.2 GPS week: 2209 Day: 2 MJD: 59709
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 731 29 30 32 14 24 20 11 | 52 62 42 56 47 47 46
R02 | 1387 18 11 11 13 14 19 6 | 34 30 30 27 33 36 29
R03 | 899 16 18 12 15 12 16 6 | 34 36 51 52 40 50 43
XR04 | 1187 13 17 17 --- 18 16 8 | 35 38 30 --- 25 40 31
R05 | 708 15 14 10 10 22 18 7 | 32 33 35 34 26 39 31
R07 | 1385 11 10 15 13 10 29 7 | 39 44 41 45 44 58 44
R08 | 626 9 10 9 14 14 18 5 | 33 37 35 38 40 48 37
R09E | 2434 13 17 11 16 17 15 6 | 31 34 27 37 35 34 31
XR11E | 2196 --- 13 13 14 22 17 8 | --- 25 24 25 30 22 22
R12E | 1039 10 20 11 11 15 12 5 | 42 31 39 40 43 41 38
R13E | 1215 17 45 30 32 35 42 15 | 38 45 50 54 54 43 40
XR14E | 6491 93 --- --- --- --- 104 99 | 214 --- --- --- --- 53 130
R15E | 658 13 30 13 15 13 17 7 | 40 38 37 43 40 45 39
R17 | 1322 18 26 11 16 22 17 8 | 43 29 35 31 35 39 33
R18 | 899 27 24 28 25 17 18 10 | 42 27 43 39 43 27 32
R19 | 691 36 116 40 83 61 36 27 | 60 44 51 98 49 54 52
R20 | 942 52 103 80 48 52 24 27 | 78 49 46 77 70 36 49
R21 | 612 14 46 20 10 17 21 9 | 37 28 25 32 45 39 32
XR22 | 774 54 --- 107 86 89 22 38 | 61 --- 67 38 43 49 39
R24 | 1622 21 58 18 18 14 13 10 | 54 44 41 54 47 45 45
------+-----------------------------------------+-------------------------------------
RMS | 1170 22 47 28 29 26 22 |T 52 37 39 45 41 42 42
WRMS | 1170 20 30 18 14 20 20 |NE 45 38 40 47 41 43 38
MEDI | 942 17 20 15 15 17 18 |MD 40 36 39 39 43 41 38
Table 3.2209.3 GPS week: 2209 Day: 3 MJD: 59710
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 691 31 25 42 25 29 23 13 | 66 58 58 55 61 57 56
R02 | 2009 11 11 16 14 21 13 6 | 36 34 36 39 50 42 37
R03 | 602 10 10 16 11 13 13 5 | 39 43 54 48 49 42 44
XR04 | 1102 11 15 11 --- 32 13 8 | 42 44 40 --- 38 48 40
R05 | 812 18 13 20 14 26 24 9 | 35 47 52 45 35 58 42
R07 | 1647 8 7 20 12 13 10 5 | 55 57 46 55 58 56 53
R08 | 1046 12 11 9 14 18 20 6 | 45 45 45 48 51 51 46
R09E | 3021 17 15 13 21 19 11 7 | 32 34 46 54 35 38 38
XR11E | 2682 --- 14 12 15 15 12 6 | --- 28 30 31 30 25 26
R12E | 2470 7 28 18 14 24 13 7 | 41 31 46 50 58 43 43
R13E | 1527 25 44 24 37 22 25 13 | 42 42 53 66 46 49 44
XR14E | 3158 19 --- --- --- --- 20 20 | 55 --- --- --- --- 51 49
R15E | 1483 13 26 13 11 19 11 6 | 77 70 70 76 68 69 71
R17 | 898 15 29 13 19 15 12 7 | 46 33 36 47 44 34 38
R18 | 868 10 34 22 19 36 15 10 | 45 28 50 47 37 37 37
R19 | 758 32 112 44 58 57 37 24 | 60 39 58 90 60 65 58
R20 | 1006 44 95 108 41 53 28 27 | 100 34 41 95 103 83 73
R21 | 752 9 45 23 11 17 29 10 | 49 27 39 49 49 66 47
R22 | 845 55 111 107 68 88 43 34 | 65 89 82 51 38 51 42
R24 | 1369 23 56 21 20 18 16 11 | 48 28 28 45 39 35 35
------+-----------------------------------------+-------------------------------------
RMS | 1443 24 52 43 29 35 22 |T 51 42 47 55 49 50 45
WRMS | 1443 17 42 33 14 25 19 |NE 52 43 47 54 50 51 46
MEDI | 1046 15 26 20 15 21 15 |MD 46 39 46 49 49 49 43
Table 3.2209.4 GPS week: 2209 Day: 4 MJD: 59711
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 724 26 19 44 33 37 12 12 | 50 41 46 46 62 37 40
R02 | 1426 9 8 11 18 20 11 5 | 33 35 35 35 44 35 33
R03 | 649 7 14 17 15 31 13 7 | 34 39 34 31 60 35 34
XR04 | 734 10 13 14 --- 18 13 6 | 36 36 38 --- 33 40 36
R05 | 962 22 16 25 24 17 15 8 | 30 38 58 58 33 45 40
R07 | 2091 7 12 11 22 16 14 6 | 45 43 47 63 45 47 47
R08 | 678 8 9 16 20 16 12 6 | 47 48 52 53 56 34 44
R09E | 2669 15 16 14 20 19 11 7 | 21 24 28 30 23 26 21
XR11E | 2957 --- 15 18 12 19 12 7 | --- 18 29 27 27 20 20
R12E | 1214 9 30 21 15 14 12 7 | 42 41 55 49 54 41 44
R13E | 904 18 38 34 48 31 20 13 | 49 50 65 78 66 46 52
XR14E | 1523 17 74 --- 30 --- 18 18 | 64 80 --- 65 --- 53 57
R15E | 938 10 29 21 22 17 11 7 | 74 64 90 84 84 72 75
R17 | 650 10 30 14 22 14 9 7 | 39 35 41 52 50 41 40
R18 | 666 15 38 21 23 20 14 9 | 35 32 47 58 51 53 42
R19 | 688 28 112 50 64 58 16 23 | 54 42 41 73 51 45 41
R20 | 1367 32 86 101 58 35 29 24 | 85 55 42 112 98 88 78
R21 | 1402 17 30 30 15 14 11 8 | 48 34 35 42 48 41 41
R22 | 2328 40 69 96 78 76 20 26 | 43 64 66 47 37 32 33
R24 | 668 17 59 20 11 22 11 10 | 69 51 55 60 73 63 61
------+-----------------------------------------+-------------------------------------
RMS | 1330 20 46 41 35 32 15 |T 47 43 47 55 52 44 43
WRMS | 1330 17 33 29 21 25 13 |NE 46 42 45 56 52 45 43
MEDI | 938 15 29 21 22 19 12 |MD 45 41 46 53 51 41 41
Table 3.2209.5 GPS week: 2209 Day: 5 MJD: 59712
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 555 31 21 41 38 43 26 15 | 41 43 55 53 27 32 35
R02 | 1124 10 15 19 14 17 19 7 | 27 22 26 35 32 29 25
R03 | 594 8 13 9 12 12 18 5 | 28 30 28 31 28 38 28
XR04 | 813 27 26 16 --- 17 29 12 | 34 31 19 --- 27 37 23
R05 | 1338 20 20 20 17 19 20 8 | 25 35 39 30 37 31 26
R07 | 1011 16 18 13 12 17 25 8 | 38 36 50 46 34 55 43
R08 | 810 12 8 19 21 10 8 6 | 37 36 40 46 33 35 36
R09E | 3069 14 16 17 12 16 12 6 | 21 22 31 25 21 29 23
XR11E | 2804 --- 16 10 12 26 20 9 | --- 23 23 24 26 27 21
R12E | 1107 6 23 14 15 17 13 6 | 66 57 66 65 69 63 63
R13E | 913 32 38 35 46 28 25 15 | 52 52 63 71 60 62 53
R14E | 1319 14 21 21 16 16 13 7 | 65 49 58 52 47 54 58
R15E | 1087 16 23 20 27 15 23 9 | 108 102 115 119 116 94 106
R17 | 682 16 35 14 10 13 10 7 | 42 22 33 32 35 38 34
R18 | 957 12 24 27 25 14 28 10 | 36 31 44 45 36 29 33
R19 | 1372 43 126 38 54 63 24 26 | 46 44 47 46 46 45 33
R20 | 1976 45 101 102 59 56 30 29 | 85 78 61 88 83 49 62
R21 | 910 18 30 26 8 24 18 9 | 41 30 32 32 54 33 35
R22 | 2525 50 70 93 69 74 29 28 | 35 45 44 44 39 51 31
R24 | 1291 18 66 17 25 13 12 12 | 58 40 45 56 56 42 48
------+-----------------------------------------+-------------------------------------
RMS | 1411 25 49 39 32 32 21 |T 46 41 45 49 45 43 40
WRMS | 1411 20 29 29 19 23 19 |NE 40 37 40 44 40 38 35
MEDI | 1087 16 23 19 17 17 20 |MD 41 36 44 46 36 38 34
Table 3.2209.6 GPS week: 2209 Day: 6 MJD: 59713
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 689 19 18 25 18 37 21 10 | 76 66 59 69 62 57 63
R02 | 929 17 13 18 13 14 34 9 | 47 42 49 48 52 51 44
R03 | 622 11 9 10 10 9 24 6 | 44 50 52 50 55 60 49
XR04 | 930 19 22 16 --- 14 31 10 | 48 49 36 --- 40 44 38
R05 | 649 16 22 16 17 14 17 7 | 37 45 43 44 43 45 38
R07 | 830 14 18 14 9 14 26 7 | 60 63 72 71 62 78 66
R08 | 544 15 18 16 22 22 28 9 | 56 50 64 69 58 61 57
R09E | 4564 16 15 9 24 12 15 7 | 32 30 35 45 31 36 33
XR11E | 3857 --- 12 18 9 27 23 9 | --- 26 26 29 31 33 26
R12E | 1544 9 30 14 17 15 19 7 | 83 80 80 79 86 85 81
R13E | 576 24 35 25 47 46 23 15 | 71 81 75 75 93 83 74
R14E | 2283 13 31 23 16 28 33 10 | 91 70 69 74 61 80 84
R15E | 1454 12 28 12 17 14 14 7 | 106 110 106 109 104 103 105
R17 | 1357 15 33 15 15 14 14 8 | 62 32 46 56 55 47 50
R18 | 683 8 26 20 13 15 7 6 | 52 34 58 50 45 41 46
R19 | 1176 40 104 32 55 59 44 24 | 72 48 49 102 76 68 63
R20 | 2074 40 76 81 40 49 17 23 | 115 67 69 122 122 88 92
R21 | 1013 16 30 21 16 18 15 8 | 67 36 45 59 70 62 58
R22 | 1292 36 76 109 87 75 51 33 | 47 66 98 56 47 55 41
R24 | 612 16 56 16 15 18 39 12 | 82 54 65 76 71 89 72
------+-----------------------------------------+-------------------------------------
RMS | 1582 21 43 36 32 32 27 |T 65 54 59 67 63 63 59
WRMS | 1582 18 33 22 16 21 24 |NE 61 50 57 67 61 60 55
MEDI | 930 16 26 16 17 15 23 |MD 62 50 58 69 58 60 57
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