[IGSREPORT-28964] Wk 2229 IGLOS Final Orbits
acc
acc at igs.org
Sat Oct 15 10:24:56 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2229 (Sep 25, 2022 - Oct 01, 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 2.2229.
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:
igl2229[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2229 in the SP3 format.
igl22297.sum Combination Report for GPS Week 2229.
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 | 1.0 ns
2 | -2.0 ns
3 | 0.2 ns
4 | 0.1 ns
5 | -7.7 ns
6 | -0.9 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 1.2229, 1a.2229).
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 2.2229.0-6)
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 3.2229.0-6).
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 2229 summary. (Sep 25, 2022 - Oct 01, 2022)
Table 1.2229.a GPS week : 2229 MJD: 59847.0-59853.0
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 2 -15 -13 39 .13 21 14 | 32798 -1699 3102 8430
| 1 1 1 15 21 26 .04 | 3637 2104
emx n/a| -1 0 0 10 -45 0 -.13 34 25 | -3403 -1243 3101 8440
| 0 1 1 26 28 44 .05 | 8197 1491
esx n/a| 0 1 0 28 -9 21 -.11 24 18 | 7504 -1006 3105 11474
| 2 2 2 15 15 19 .03 | 7824 2371
gfz n/a| 0 1 -1 18 0 29 .01 28 15 | 0 -1444 3151 8308
| 0 0 2 33 20 22 .07 | 0 2175
grg n/a| 3 -3 5 -18 67 -135 .22 30 22 | -788 -1565 3104 7819
| 1 0 3 20 14 38 .04 | 2666 2193
iac n/a| 0 0 -8 -8 20 -4 -.22 31 28 | 2043 -995 3156 10231
| 1 1 2 31 46 52 .08 | 2556 841
Table 1.2229.b GPS week : 2229 MJD: 59847.0-59853.0
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 | 14 15 13 15 16 15 14 |
R02 | 7 6 8 9 9 8 7 |
R03 | 6 6 7 7 8 9 9 |
R04 | 9 9 6 5 11 9 7 |
R05 | 10 8 8 8 8 9 9 |
R07 | 7 7 7 7 7 6 5 |
R08 | 13 11 7 9 10 9 10 |
R09 | 11 10 11 10 13 12 13 |
R11 | 8 9 9 10 8 9 9 |
R12 | 7 8 7 7 8 9 8 |
R13 | 15 16 17 17 15 17 16 |
R14 | 9 9 10 7 7 7 8 |
R15 | 9 6 9 9 9 9 6 |
R17 | 7 7 8 7 7 7 8 |
R18 | 7 8 9 7 7 8 8 |
R19 | 21 20 20 24 26 20 22 |
R20 | 27 30 34 27 27 27 28 |
R21 | 10 8 8 8 7 9 8 |
R24 | 8 10 9 9 9 6 9 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2229.c GPS week : 2229 MJD: 59847.0-59853.0
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 2229 0 | 13 45 71 -342 1563 1990 81.6 1376 1376 | -179 0
brd 2229 1 | -13 -48 73 -330 -2152 -4651 80.8 1304 1304 | 993 0
brd 2229 2 | 48 24 26 -1435 -1773 -8866 79.7 1434 1434 | -2003 0
brd 2229 3 | 27 78 -78 -1735 -945 -9942 82.6 1740 1740 | 178 0
brd 2229 4 | -68 -25 -47 -839 -841 -1140 80.9 2133 2133 | 106 0
brd 2229 5 | 67 37 16 -277 545 -1084 80.5 1661 1661 | -7735 0
brd 2229 6 | 54 -17 -13 2216 921 6576 84.0 1783 1783 | -884 0
-------------+------------------------------------------------------------+----------------
brd 2229 mean| 18 13 6 -392 -383 -2445 81.4 1632 1632 | -1360 0
brd 2229 sdev| 46 45 57 1285 1410 5872 1.4 288 288 | 2964 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 2.2229.0 GPS week: 2229 Day: 0 MJD: 59847
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 5 -22 -42 40 .09 20 14 | 35143 -1046 2639 8264
emx n/a| -1 -1 -1 -9 -74 27 -.16 32 27 | -5212 -406 2619 8133
esx n/a| 0 3 3 24 -10 36 -.10 21 19 | 1195 -579 2626 11675
gfz n/a| 0 1 -4 18 -1 17 .03 27 14 | 0 -873 2662 7974
grg n/a| 0 -3 0 13 71 -161 .20 36 19 | 49 -777 2620 7495
iac n/a| 1 0 -6 3 50 23 -.11 28 25 | 2827 -639 2759 10054
Table 2.2229.1 GPS week: 2229 Day: 1 MJD: 59848
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 4 -16 -37 62 .11 24 16 | 36551 464 2663 8063
emx n/a| -1 -1 2 21 -55 -51 -.17 30 26 | -8676 -43 2663 8033
esx n/a| -2 5 0 29 15 24 -.08 23 21 | 13494 1321 2663 11381
gfz n/a| 0 1 0 -31 9 55 .00 25 18 | 0 1027 2691 7896
grg n/a| 1 -3 0 -22 62 -87 .23 30 22 | 392 746 2664 7303
iac n/a| 0 0 -6 48 13 -71 -.18 32 29 | 4346 -145 2733 9728
Table 2.2229.2 GPS week: 2229 Day: 2 MJD: 59849
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 2 -3 -3 43 .12 27 15 | 35705 -5672 2716 8489
emx n/a| -1 3 0 26 -6 -2 -.17 34 26 | -17363 -4323 2712 8545
esx n/a| -2 3 -3 23 8 27 -.09 23 18 | 3993 -5495 2709 11129
gfz n/a| -1 1 -1 -21 -26 46 .01 27 15 | 0 -5672 2748 8547
grg n/a| 3 -4 7 7 67 -168 .18 26 21 | 637 -5834 2697 7661
iac n/a| 0 0 -9 -2 -45 16 -.30 40 31 | 2528 -2750 2792 10189
Table 2.2229.3 GPS week: 2229 Day: 3 MJD: 59850
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 -2 48 .11 19 12 | 32933 -1323 3921 8713
emx n/a| -2 3 2 -20 -82 -12 -.16 37 26 | 7972 -1212 3915 8644
esx n/a| -1 1 0 49 -16 21 -.16 27 19 | 1455 -599 3934 11761
gfz n/a| 0 0 -1 28 -25 -2 .13 27 12 | 0 -296 3968 8473
grg n/a| 6 -3 4 -31 47 -157 .19 29 22 | 421 -621 3937 8190
iac n/a| -3 0 -8 -49 83 58 -.27 30 28 | 2810 -496 3903 10618
Table 2.2229.4 GPS week: 2229 Day: 4 MJD: 59851
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 3 -5 -25 63 .11 20 15 | 32595 323 3421 9200
emx n/a| -1 0 0 57 -37 51 -.09 34 24 | 2546 45 3432 9140
esx n/a| 1 0 0 0 -10 -3 -.10 23 17 | 22208 1369 3434 12753
gfz n/a| 0 1 2 28 2 43 -.08 34 17 | 0 -100 3479 9199
grg n/a| 2 -2 6 -25 86 -172 .27 29 22 | -249 94 3433 8693
iac n/a| -1 2 -13 -37 46 -21 -.15 33 30 | 3566 -853 3448 10900
Table 2.2229.5 GPS week: 2229 Day: 5 MJD: 59852
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 0 -16 0 -15 .16 18 14 | 25946 -2902 2943 8165
emx n/a| -1 0 1 -8 -15 48 -.10 37 24 | -3220 -1495 2952 8300
esx n/a| 1 -2 1 36 -25 49 -.15 26 16 | 2359 -2433 2950 10518
gfz n/a| 0 3 -3 63 29 37 .04 26 17 | 0 -2326 3000 8030
grg n/a| 4 -3 9 -35 83 -113 .21 29 22 | -6798 -2349 2961 7665
iac n/a| -1 -2 -7 -14 -34 -75 -.33 30 28 | -3434 -897 2989 10259
Table 2.2229.6 GPS week: 2229 Day: 6 MJD: 59853
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 -45 15 31 .21 21 15 | 30714 -1743 3417 8117
emx n/a| -3 0 0 4 -44 -58 -.03 32 24 | 126 -1271 3414 8287
esx n/a| 2 0 2 35 -26 -4 -.08 26 15 | 7825 -632 3421 11103
gfz n/a| 0 2 -1 41 18 5 -.03 28 15 | 0 -1874 3512 8040
grg n/a| 3 -4 5 -33 56 -84 .30 30 22 | 27 -2220 3417 7731
iac n/a| 0 0 -6 -10 26 36 -.22 25 24 | 1658 -1185 3470 9873
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 3.2229.0 GPS week: 2229 Day: 0 MJD: 59847
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 696 33 27 38 21 22 34 13 | 110 80 64 94 100 95 90
R02 | 678 10 22 12 11 13 18 6 | 57 46 58 61 64 68 58
R03 | 501 6 21 14 6 17 11 5 | 68 56 72 72 78 75 69
XR04 | 1076 16 14 11 --- 13 28 8 | 83 82 79 --- 77 79 80
R05M | 1967 24 24 20 27 13 19 10 | 69 52 70 61 59 65 62
R07M | 563 13 21 20 11 13 14 7 | 66 51 69 69 67 63 64
R08M | 974 22 32 11 19 18 55 12 | 61 58 76 93 76 114 77
R09M | 609 19 19 17 20 39 28 10 | 58 56 59 58 28 61 51
R11M | 2337 11 20 24 8 19 23 8 | 17 25 41 31 31 18 23
R12 | 938 9 25 14 17 15 15 7 | 59 47 64 65 59 56 57
R13M | 627 25 47 34 28 27 34 14 | 94 58 60 70 85 95 76
R14M | 566 10 35 19 14 21 17 8 | 51 34 64 54 71 54 54
R15M | 607 8 19 11 16 23 38 9 | 69 53 65 72 87 67 67
R17E | 1572 8 23 12 15 15 14 6 | 54 52 56 58 63 62 56
R18E | 1162 10 15 16 18 21 17 7 | 80 79 87 83 90 82 83
R19E | 1913 26 73 26 62 54 46 21 | 68 69 65 79 97 97 72
R20E | 1284 45 41 35 65 117 32 26 | 90 74 69 79 156 82 79
R21E | 1201 13 34 16 30 16 20 9 | 71 65 67 79 76 68 69
R24E | 3058 10 29 17 12 20 10 7 | 43 39 42 46 50 42 42
XR25 |27293 --- --- --- --- --- 5 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1375 20 32 21 27 36 28 |T 66 56 64 68 74 70 64
WRMS | 1375 14 27 19 14 19 25 |NE 66 57 68 66 69 69 66
MEDI | 974 13 24 17 17 19 19 |MD 68 56 65 69 76 68 67
Table 3.2229.1 GPS week: 2229 Day: 1 MJD: 59848
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 772 27 30 44 26 19 48 14 | 76 46 39 79 65 71 60
R02 | 636 7 12 12 18 10 17 6 | 41 35 42 32 40 36 36
R03 | 523 6 14 16 10 12 12 5 | 46 36 44 48 47 44 44
XR04 | 588 12 14 12 --- 12 36 9 | 62 55 55 --- 58 49 55
R05M | 1178 22 14 13 19 12 25 8 | 47 40 43 42 44 38 39
R07M | 589 9 20 16 13 18 16 7 | 42 29 36 49 50 41 40
R08M | 1131 19 19 10 16 13 57 11 | 53 49 58 64 65 81 58
R09M | 916 17 22 19 20 26 34 10 | 45 43 51 52 29 54 43
R11M | 2305 13 21 15 17 34 17 9 | 12 22 31 29 35 22 17
R12 | 1187 10 22 18 18 16 21 8 | 52 34 45 55 49 41 45
R13M | 644 25 52 40 20 42 39 16 | 96 77 70 89 73 96 80
R14M | 1246 16 33 22 10 8 31 9 | 130 114 123 129 130 126 125
R15M | 799 8 22 11 8 18 12 6 | 56 43 48 49 63 48 51
R17E | 1470 8 26 12 16 15 17 7 | 30 32 32 31 38 35 30
R18E | 1305 8 19 16 17 27 19 8 | 56 61 61 55 54 59 56
R19E | 1396 28 63 30 64 41 34 20 | 52 51 44 96 82 66 58
R20E | 1365 79 39 48 54 89 68 29 | 51 71 84 100 121 128 79
R21E | 928 6 31 13 18 13 17 7 | 64 64 68 68 61 59 64
R24E | 2760 16 37 13 15 22 24 9 | 33 34 34 30 34 41 30
XR25 |28285 --- --- --- --- --- 6 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1304 24 30 23 25 30 32 |T 54 49 53 60 59 59 53
WRMS | 1304 16 26 21 18 22 29 |NE 50 40 46 45 48 42 45
MEDI | 1131 13 22 16 17 18 21 |MD 52 43 45 52 54 49 51
Table 3.2229.2 GPS week: 2229 Day: 2 MJD: 59849
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 680 29 33 30 22 21 35 12 | 97 80 74 89 85 103 85
R02 | 931 8 24 10 12 16 32 7 | 48 38 46 51 55 55 47
R03 | 670 10 14 11 13 18 22 6 | 64 56 66 65 68 73 64
XR04 | 931 9 9 10 --- 12 21 6 | 69 67 64 --- 65 64 65
R05M | 1880 12 16 20 12 17 29 8 | 62 58 72 65 65 60 63
R07M | 652 9 23 16 13 16 17 7 | 53 44 55 57 56 54 52
R08M | 1987 11 21 14 16 16 16 7 | 94 92 109 106 97 106 100
R09M | 1991 14 22 17 16 37 32 10 | 52 52 59 61 30 71 50
R11M | 2210 17 23 12 19 24 22 8 | 19 27 28 27 34 29 20
R12 | 917 10 29 16 13 13 19 7 | 58 47 51 63 62 62 56
R13M | 727 26 38 40 31 46 46 16 | 111 78 88 116 112 99 99
R14M | 1487 20 28 15 26 10 25 9 | 301 302 298 301 298 288 298
R15M | 798 12 24 12 16 26 32 9 | 75 69 78 76 95 94 79
R17E | 1664 13 27 13 14 21 15 7 | 31 27 32 28 42 33 30
R18E | 1010 10 23 14 20 28 25 9 | 56 55 55 46 70 52 54
R19E | 1263 35 79 31 44 42 43 20 | 65 100 81 89 77 76 74
R20E | 2253 92 55 55 74 39 125 33 | 48 74 91 128 89 172 76
R21E | 725 8 30 11 23 11 21 8 | 50 56 49 65 56 50 53
R24E | 1799 10 35 14 17 23 23 9 | 31 31 32 39 42 46 33
XR25 |21052 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1433 27 34 23 27 26 40 |T 72 71 75 81 78 83 73
WRMS | 1433 15 26 18 15 21 31 |NE 59 52 56 59 62 63 58
MEDI | 1010 12 24 14 16 21 23 |MD 58 56 64 65 65 64 63
Table 3.2229.3 GPS week: 2229 Day: 3 MJD: 59850
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 627 21 38 44 28 33 44 15 | 102 77 77 97 93 118 93
R02 | 1209 6 27 11 8 16 44 9 | 50 32 57 50 44 92 52
R03 | 965 8 15 8 13 16 26 6 | 62 50 57 51 67 54 56
XR04 | 757 4 16 9 --- 13 11 5 | 63 64 63 --- 59 72 63
R05M | 1876 11 16 26 16 13 16 7 | 53 50 69 57 60 50 55
R07M | 708 9 15 23 8 15 14 6 | 59 48 49 55 63 61 55
R08M | 2187 10 22 14 23 14 32 8 | 133 131 129 144 134 139 134
R09M | 2705 17 18 23 17 38 16 10 | 60 57 59 59 30 47 50
R11M | 1722 13 17 22 29 31 18 10 | 18 29 26 34 28 26 19
R12 | 1117 7 23 9 8 16 26 6 | 48 33 46 47 40 63 45
R13M | 849 33 42 47 25 50 23 16 | 101 78 69 93 88 83 84
R14M | 1213 11 23 18 16 11 16 7 | 447 442 440 439 447 443 443
R15M | 915 8 28 19 16 21 31 9 | 60 47 52 68 75 85 63
R17E | 787 7 22 10 12 14 23 6 | 54 54 52 58 58 50 53
R18E | 1960 12 25 11 17 15 18 7 | 48 46 51 56 53 50 49
R19E | 1816 33 91 44 55 55 50 23 | 55 60 58 80 73 61 53
R20E | 4165 50 76 57 72 61 53 27 | 65 57 74 74 81 84 61
R21E | 680 10 26 18 19 10 19 7 | 66 61 63 70 76 80 68
R24E | 1667 14 34 13 19 21 21 9 | 41 49 43 49 56 40 43
XR25 |15979 --- --- --- --- --- 9 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1740 19 37 27 27 29 30 |T 83 77 80 87 85 89 81
WRMS | 1740 12 26 19 12 22 28 |NE 55 44 55 49 52 70 54
MEDI | 1209 11 23 18 17 16 21 |MD 60 54 58 58 63 63 55
Table 3.2229.4 GPS week: 2229 Day: 4 MJD: 59851
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 894 31 26 36 40 33 45 15 | 92 84 82 75 101 108 86
R02 | 1532 13 25 11 8 12 45 9 | 45 43 51 47 49 75 49
R03 | 709 6 19 14 13 14 38 8 | 52 47 59 46 49 89 55
XR04 | 769 7 12 15 --- 21 49 11 | 68 70 78 --- 67 69 69
R05M | 1305 18 18 16 13 16 18 7 | 44 48 55 50 50 63 49
R07M | 675 13 15 15 15 15 13 6 | 56 42 50 42 56 57 50
R08M | 2347 19 22 7 15 12 52 10 | 181 183 182 178 186 200 183
R09M | 3478 23 17 25 13 54 18 12 | 71 63 70 64 32 59 57
R11M | 1225 14 20 16 16 23 13 7 | 18 26 23 25 32 23 17
R12 | 1673 18 20 14 12 9 30 7 | 50 41 47 49 55 67 48
R13M | 713 28 40 33 26 36 39 15 | 85 80 79 73 95 94 81
R14M | 1102 5 26 15 11 12 14 6 | 592 598 599 593 589 602 595
R15M | 579 10 25 10 20 29 25 8 | 53 38 51 69 77 40 54
R17E | 697 7 28 10 12 19 14 6 | 38 32 36 42 49 36 37
R18E | 2669 12 23 12 12 17 23 7 | 49 46 53 51 54 61 50
R19E | 1865 36 68 34 102 56 44 26 | 57 74 87 144 69 67 68
R20E | 5458 33 80 56 77 55 64 26 | 52 45 71 80 75 74 51
R21E | 888 14 23 13 12 17 18 7 | 57 56 65 64 64 56 59
R24E | 3233 17 29 14 25 15 15 8 | 40 32 43 50 41 40 38
XR25 |14815 --- --- --- --- --- 9 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 2133 20 34 23 34 29 33 |T 89 86 93 96 94 98 89
WRMS | 2133 15 24 17 17 22 30 |NE 53 50 58 47 55 75 55
MEDI | 1225 14 23 15 13 17 23 |MD 53 47 59 51 56 67 54
Table 3.2229.5 GPS week: 2229 Day: 5 MJD: 59852
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 775 31 24 49 27 28 22 14 | 114 128 116 108 121 106 112
R02 | 1331 11 21 14 18 13 30 7 | 41 36 47 54 49 58 45
R03 | 577 6 21 11 17 17 41 8 | 45 37 48 45 54 74 48
XR04 | 1321 10 14 15 --- 12 35 9 | 51 47 51 --- 48 38 46
R05M | 1031 13 23 23 17 13 30 8 | 45 57 60 59 42 36 48
R07M | 570 5 16 12 13 12 21 5 | 51 42 49 57 51 43 48
R08M | 631 17 23 12 22 14 30 8 | 239 235 241 236 240 247 239
R09M | 3482 25 20 20 17 44 32 12 | 69 76 74 69 41 70 64
R11M | 923 17 15 21 13 28 19 8 | 46 56 68 58 83 59 59
R12 | 1633 6 31 20 15 10 39 9 | 35 31 40 48 42 56 38
R13M | 1048 33 33 36 27 58 30 16 | 118 95 107 113 125 106 109
R14M | 755 8 24 8 17 14 22 7 | 767 774 774 780 776 770 773
R15M | 480 13 23 20 16 22 23 8 | 62 60 49 51 71 72 59
R17E | 664 6 25 11 17 14 18 6 | 54 56 58 57 64 60 57
R18E | 2247 12 21 17 20 23 20 8 | 63 63 66 59 69 57 62
R19E | 1869 21 90 30 44 52 30 20 | 35 69 57 74 55 37 44
R20E | 1919 35 88 57 74 54 60 27 | 60 67 85 80 85 70 59
R21E | 1080 10 27 26 13 23 21 8 | 56 54 74 62 62 51 58
R24E | 3709 12 26 10 12 11 13 6 | 61 61 65 63 64 54 61
XR25 |15214 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1660 18 37 26 26 29 30 |T 105 107 112 115 112 108 106
WRMS | 1660 14 24 16 17 22 28 |NE 43 37 46 49 48 56 44
MEDI | 1048 12 23 20 17 17 23 |MD 56 60 65 59 64 59 59
Table 3.2229.6 GPS week: 2229 Day: 6 MJD: 59853
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 1029 21 26 47 22 36 21 13 | 154 138 144 148 154 156 147
R02 | 1573 7 12 14 12 18 29 7 | 53 44 54 54 51 68 52
R03 | 752 6 16 9 14 10 42 8 | 62 53 64 57 58 89 63
XR04 | 1416 6 14 17 --- 13 16 6 | 72 63 69 --- 64 81 69
R05M | 950 15 17 18 19 23 22 8 | 78 63 83 82 69 73 74
R07M | 615 9 10 8 10 18 11 5 | 76 67 68 71 83 72 72
R08M | 2270 19 21 15 24 24 27 9 | 283 285 288 296 288 292 288
R09M | 3372 26 19 17 18 54 21 12 | 68 69 70 66 35 68 60
R11M | 1113 20 15 17 16 35 18 9 | 26 33 38 31 42 27 29
R12 | 1326 12 24 13 9 12 27 7 | 55 36 51 51 55 55 49
R13M | 977 30 48 31 27 49 21 15 | 194 190 183 190 188 195 188
R14M | 1398 8 31 10 13 19 16 7 | 941 938 940 936 937 932 938
R15M | 632 9 21 12 11 13 15 6 | 85 75 83 87 101 90 86
R17E | 982 13 21 14 17 11 25 7 | 51 46 58 55 64 56 54
R18E | 2417 12 18 21 17 14 17 7 | 46 47 60 51 57 51 50
R19E | 1508 26 72 39 62 56 31 21 | 63 63 63 96 80 66 64
R20E | 2307 60 71 70 69 49 46 27 | 62 46 89 93 85 70 62
R21E | 1681 10 25 16 14 17 18 7 | 61 49 60 67 75 60 61
R24E | 3433 13 28 13 29 12 25 9 | 49 45 48 53 57 45 48
XR25 |16519 --- --- --- --- --- 5 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1783 21 32 26 28 30 25 |T 130 123 132 138 133 134 129
WRMS | 1783 15 24 15 15 22 24 |NE 60 49 59 54 57 73 58
MEDI | 1398 13 21 16 17 18 21 |MD 63 63 68 67 69 70 63
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