[IGSREPORT-28900] Wk 2224 IGLOS Final Orbits
acc
acc at igs.org
Mon Sep 12 23:45:50 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2224 (Aug 21, 2022 - Aug 27, 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 2.2224.
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:
igl2224[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2224 in the SP3 format.
igl22247.sum Combination Report for GPS Week 2224.
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 | -5.9 ns
1 | -5.2 ns
2 | 1.0 ns
3 | -1.9 ns
4 | 0.8 ns
5 | -0.9 ns
6 | 0.0 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 1.2224, 1a.2224).
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 2.2224.0-6)
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 3.2224.0-6).
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 2224 summary. (Aug 21, 2022 - Aug 27, 2022)
Table 1.2224.a GPS week : 2224 MJD: 59812.0-59818.0
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 -1 -12 -20 13 .12 26 21 | 29322 -260 3190 8580
| 1 0 2 18 18 29 .06 | 3899 1963
emx n/a| -2 0 15 16 -24 -14 -.00 41 33 | -2038 -323 3202 8568
| 1 1 1 22 20 60 .05 | 11640 1778
esx n/a| 0 0 6 16 21 7 -.12 27 19 | -5851 132 3188 11700
| 1 0 1 16 12 20 .04 | 9386 2120
gfz n/a| 0 0 -4 0 1 15 -.10 28 17 | 0 -283 3253 8387
| 1 1 1 12 23 51 .09 | 0 2236
grg n/a| 3 -1 -4 -8 38 -13 .40 23 19 | -1716 -353 3183 8095
| 1 1 2 23 6 29 .02 | 2940 2002
iac n/a| 0 0 -3 1 -24 -8 -.28 23 22 | 1400 -820 3310 10071
| 1 2 3 25 26 57 .14 | 2893 1654
Table 1.2224.b GPS week : 2224 MJD: 59812.0-59818.0
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 | 20 21 21 21 24 22 21 |
R02 | 8 8 8 8 10 10 8 |
R03 | 9 8 10 8 10 11 10 |
R04 | 10 11 8 8 10 10 8 |
R05 | 10 10 9 10 10 10 11 |
R07 | 8 9 8 9 8 8 8 |
R08 | 8 10 8 9 8 10 8 |
R09 | 8 8 10 10 9 8 7 |
R11 | 8 7 7 9 9 10 12 |
R12 | 8 7 6 7 6 7 9 |
R13 | 17 14 16 13 13 15 10 |
R14 | 7 5 7 7 5 6 7 |
R15 | 6 7 7 7 8 6 7 |
R17 | 9 9 8 10 8 9 10 |
R18 | 8 8 9 9 8 8 9 |
R19 | 24 20 16 18 24 26 24 |
R20 | 25 22 24 23 23 23 26 |
R21 | 9 11 10 10 10 10 9 |
R24 | 11 10 11 10 10 10 9 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2224.c GPS week : 2224 MJD: 59812.0-59818.0
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 2224 0 | -63 48 37 58 -1649 982 79.9 1607 1607 | -5868 0
brd 2224 1 | -18 11 144 -290 -86 2384 82.2 1579 1579 | -5208 0
brd 2224 2 | 58 -72 44 1139 852 7282 80.1 1711 1711 | 1043 0
brd 2224 3 | 53 -48 55 820 485 4515 80.5 1568 1568 | -1932 0
brd 2224 4 | 5 66 48 -231 433 2161 81.0 1531 1531 | 826 0
brd 2224 5 | 18 47 43 -42 686 4414 79.8 1370 1370 | -929 0
brd 2224 6 | -43 44 -6 -255 -483 9628 80.7 1217 1217 | 24 0
-------------+------------------------------------------------------------+----------------
brd 2224 mean| 1 14 52 171 33 4480 80.6 1511 1511 | -1720 0
brd 2224 sdev| 46 53 45 573 873 3064 .8 165 165 | 2804 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 2.2224.0 GPS week: 2224 Day: 0 MJD: 59812
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| -3 0 -1 -11 -8 37 .19 26 26 | 23404 630 2777 8354
emx n/a| -3 0 12 35 -22 46 .01 48 36 | -17196 -429 2792 8323
esx n/a| 0 0 3 7 -1 2 -.11 28 17 | -6148 732 2783 11361
gfz n/a| 0 0 -3 -5 -37 45 -.17 22 14 | 0 278 2837 8247
grg n/a| 3 0 -2 -6 37 12 .42 27 21 | -5960 66 2775 7841
iac n/a| 1 0 -4 9 11 -73 -.15 23 21 | -2550 -256 2912 10072
Table 2.2224.1 GPS week: 2224 Day: 1 MJD: 59813
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 -1 -47 -35 4 .14 24 17 | 24114 926 2976 8004
emx n/a| 0 -2 14 -4 -38 -28 .07 39 32 | -121 1147 2983 8021
esx n/a| -1 1 6 30 30 21 -.07 25 16 | -17922 2329 2981 11305
gfz n/a| 0 2 -4 2 17 29 .04 24 16 | 0 891 3041 7531
grg n/a| 4 0 -3 32 47 -41 .41 24 19 | -6051 1219 2986 7462
iac n/a| -2 -2 -7 15 -61 2 -.51 24 24 | -2671 807 3158 9781
Table 2.2224.2 GPS week: 2224 Day: 2 MJD: 59814
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 -18 -19 -42 .16 24 18 | 31303 1107 3233 8378
emx n/a| -4 0 18 -10 -8 -111 .01 42 34 | 10758 1158 3231 8286
esx n/a| -1 0 6 11 25 -15 -.13 27 18 | -3894 1821 3225 11711
gfz n/a| 0 0 -4 20 28 -60 -.00 26 16 | 0 1765 3249 8086
grg n/a| 2 0 -3 -14 35 30 .43 23 20 | 301 1148 3212 7488
iac n/a| -1 3 -5 10 -43 87 -.43 21 21 | 4750 -1325 3425 11193
Table 2.2224.3 GPS week: 2224 Day: 3 MJD: 59815
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 -18 -31 6 .14 24 17 | 31371 -3550 3421 7977
emx n/a| 0 -2 16 45 0 -75 -.05 38 33 | -3302 -1651 3431 7970
esx n/a| 1 0 7 3 13 -21 -.18 27 20 | 6397 -3253 3417 11505
gfz n/a| 0 0 -2 8 23 -26 -.22 31 22 | 0 -3695 3500 7874
grg n/a| 2 -1 -8 -2 28 4 .41 21 20 | -392 -3331 3407 7756
iac n/a| -2 -1 1 13 -10 40 -.16 21 20 | 2052 -3270 3417 8667
Table 2.2224.4 GPS week: 2224 Day: 4 MJD: 59816
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 -6 10 11 14 .11 30 21 | 31203 1859 3658 8884
emx n/a| -2 0 14 12 -9 34 .06 36 31 | -18062 1904 3646 8963
esx n/a| -1 0 7 18 21 10 -.13 25 17 | -15191 1869 3633 12285
gfz n/a| 3 1 -6 -8 -11 97 -.12 36 17 | 0 2344 3731 8633
grg n/a| 1 -3 -3 2 33 -27 .38 23 21 | -233 1987 3646 8700
iac n/a| 0 0 -2 -44 -46 -61 -.20 21 21 | 2002 1592 3638 9664
Table 2.2224.5 GPS week: 2224 Day: 5 MJD: 59817
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| -3 0 -2 3 -16 47 .03 27 21 | 33310 -2157 3130 9466
emx n/a| -4 0 16 0 -33 -1 -.05 40 33 | 6424 -2854 3182 9466
esx n/a| -1 1 5 0 35 33 -.09 29 22 | 5438 -1761 3149 12635
gfz n/a| 0 0 -4 -8 -3 -7 -.07 30 15 | 0 -2515 3215 9531
grg n/a| 5 -3 -3 -36 43 -24 .38 24 18 | 89 -2387 3138 8936
iac n/a| 0 3 -3 27 -17 -11 -.23 23 23 | 3430 -1566 3143 10062
Table 2.2224.6 GPS week: 2224 Day: 6 MJD: 59818
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 -8 -41 27 .04 26 26 | 30550 -638 3137 9000
emx n/a| -4 2 15 36 -56 34 -.06 41 32 | 7230 -1542 3153 8953
esx n/a| -1 0 7 45 26 22 -.14 29 21 | -9638 -808 3132 11098
gfz n/a| 2 0 -7 -15 -3 31 -.12 30 15 | 0 -1052 3203 8813
grg n/a| 4 -3 -3 -36 43 -47 .38 22 17 | 230 -1179 3117 8486
iac n/a| -2 4 -4 -23 -4 -42 -.27 26 25 | 2791 -1726 3483 11064
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 3.2224.0 GPS week: 2224 Day: 0 MJD: 59812
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 538 62 59 55 34 19 23 19 | 104 83 77 79 80 63 71
R02 | 2485 11 42 8 13 14 21 8 | 67 37 60 67 64 66 60
R03 | 2210 19 37 14 12 19 23 9 | 68 32 48 61 61 61 55
XR04 | 1029 14 30 14 --- 22 19 9 | 61 39 58 --- 61 63 56
R05 | 1256 12 44 19 12 19 26 9 | 63 30 47 59 62 66 55
R07 | 683 21 34 16 10 18 14 8 | 74 37 56 61 70 61 60
R08 | 713 14 38 11 15 16 13 7 | 67 39 59 72 79 73 66
R09 | 758 11 13 7 15 30 15 7 | 28 34 26 31 28 33 26
R11 | 3216 16 10 17 16 13 22 7 | 22 29 24 28 24 23 20
R12 | 1809 14 20 18 15 16 20 7 | 38 42 40 36 31 38 32
R13 | 1292 16 52 43 17 58 30 16 | 49 60 38 53 58 46 44
R14 | 1523 8 11 16 19 16 11 6 | 37 45 38 46 35 44 39
R15 | 1742 11 9 10 10 13 15 5 | 42 40 40 42 44 41 40
R17 | 1042 18 33 16 19 25 15 9 | 132 119 124 130 114 123 123
R18 | 1458 13 27 17 10 20 20 7 | 127 120 141 135 128 128 130
R19 | 1132 55 96 49 47 39 44 23 | 121 110 97 125 122 103 107
R20 | 1546 46 110 59 49 54 27 24 | 125 110 85 131 109 89 100
R21 | 789 18 33 11 15 17 28 9 | 103 81 91 105 104 89 95
R24 | 1959 20 51 12 20 16 27 10 | 87 64 79 85 85 69 77
XR25 |16096 --- --- --- --- --- 5 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1607 26 48 28 22 27 23 |T 74 60 64 74 71 67 66
WRMS | 1607 26 36 17 14 21 21 |NE 74 60 64 74 71 67 66
MEDI | 1292 16 34 16 15 19 20 |MD 67 42 58 61 64 63 60
Table 3.2224.1 GPS week: 2224 Day: 1 MJD: 59813
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 770 62 55 59 31 24 40 21 | 88 70 74 80 65 63 66
R02 | 1914 10 33 9 19 13 25 8 | 56 35 52 66 60 47 53
R03 | 1065 15 40 12 12 15 15 8 | 50 27 38 47 53 43 43
XR04 | 838 16 30 15 --- 21 26 10 | 55 39 47 --- 46 65 49
R05 | 889 16 38 13 22 21 25 10 | 57 29 37 52 41 56 44
R07 | 1116 15 34 19 15 14 19 8 | 55 34 42 56 54 46 47
R08 | 1343 11 39 15 25 15 26 9 | 46 30 40 61 52 58 47
R09 | 935 18 19 12 16 22 14 7 | 33 32 32 32 25 26 25
R11 | 2460 14 9 17 13 10 21 6 | 19 21 28 21 22 21 18
R12 | 1497 9 12 13 15 13 22 6 | 29 26 35 31 33 32 28
R13 | 2343 29 20 30 24 46 19 13 | 37 27 35 42 31 35 30
R14 | 1017 9 11 13 8 12 12 5 | 21 24 18 22 24 24 19
R15 | 1524 9 13 21 13 12 17 6 | 24 28 23 28 23 25 21
R17 | 826 17 38 11 17 19 22 9 | 116 106 109 112 115 119 112
R18 | 1619 10 30 15 14 16 18 7 | 120 113 122 124 119 120 120
R19 | 1572 24 80 41 51 42 33 20 | 116 129 120 115 120 119 116
R20 | 2088 49 74 49 53 47 28 22 | 88 99 96 89 88 73 83
R21 | 882 22 36 10 19 26 31 10 | 66 53 61 61 81 51 61
R24 | 2583 19 31 18 12 13 33 9 | 57 52 54 50 57 51 51
XR25 |17467 --- --- --- --- --- 10 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1578 24 39 25 24 24 24 |T 59 51 55 60 58 56 54
WRMS | 1578 17 32 16 16 19 24 |NE 59 51 55 60 58 56 54
MEDI | 1343 16 33 15 16 16 22 |MD 55 34 42 52 53 51 47
Table 3.2224.2 GPS week: 2224 Day: 2 MJD: 59814
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 970 58 61 71 28 25 15 21 | 78 39 58 64 55 45 47
R02 | 2883 8 32 13 16 17 20 8 | 56 50 55 52 69 56 55
R03 | 792 16 35 12 23 11 27 9 | 59 34 51 64 60 36 50
XR04 | 1179 12 30 16 --- 10 15 8 | 53 31 54 --- 52 51 49
R05 | 812 17 33 13 12 27 23 9 | 56 25 40 46 38 67 45
R07 | 1565 15 32 15 15 19 16 8 | 64 39 51 61 64 61 57
R08 | 1828 8 38 16 13 18 18 8 | 53 28 47 54 66 63 52
R09 | 723 18 19 15 13 19 33 9 | 25 14 26 26 30 36 19
R11 | 997 12 20 14 14 17 17 7 | 17 21 25 22 29 33 19
R12 | 905 12 15 10 10 18 12 6 | 31 35 31 30 37 27 29
R13 | 2424 24 22 45 29 46 27 15 | 35 43 39 45 40 44 36
R14 | 965 15 20 15 10 14 14 6 | 29 34 29 25 32 28 25
R15 | 807 12 14 14 17 15 20 7 | 29 31 24 36 24 39 26
R17 | 767 17 34 11 17 19 14 8 | 55 47 52 53 59 56 53
R18 | 1063 12 34 17 14 19 25 9 | 66 73 76 67 83 71 71
R19 | 1659 27 58 27 57 20 22 16 | 59 55 63 85 65 63 61
R20 | 3416 54 104 49 61 38 17 24 | 71 87 63 91 70 57 66
R21 | 1101 18 34 13 21 30 22 10 | 65 48 63 65 66 65 61
R24 | 3029 11 54 16 19 18 26 10 | 48 37 49 53 65 58 51
XR25 |13843 --- --- --- --- --- 9 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1710 24 42 27 26 23 21 |T 49 40 47 52 52 50 45
WRMS | 1710 18 34 18 16 20 21 |NE 49 40 47 52 52 50 45
MEDI | 1063 15 33 15 16 19 18 |MD 55 37 51 53 59 56 50
Table 3.2224.3 GPS week: 2224 Day: 3 MJD: 59815
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 770 53 58 70 49 20 23 21 | 112 63 48 108 93 74 78
R02 | 2591 12 37 15 25 12 9 8 | 81 57 71 90 80 73 75
R03 | 658 15 36 11 12 13 17 7 | 77 49 66 69 77 64 68
XR04 | 725 13 32 13 --- 15 12 8 | 71 47 62 --- 77 63 65
R05 | 882 18 46 21 16 16 20 10 | 78 54 70 72 75 74 69
R07 | 1252 19 32 18 9 18 24 9 | 73 50 58 66 66 66 62
R08 | 742 13 31 18 15 20 16 8 | 75 53 62 63 81 69 68
R09 | 1177 15 37 16 20 20 25 9 | 47 47 57 53 53 54 49
R11 | 939 18 15 19 9 26 17 8 | 42 43 47 41 34 41 36
R12 | 1385 14 14 15 22 15 13 7 | 45 47 57 43 46 50 46
R13 | 752 22 19 37 26 35 23 13 | 65 71 54 69 54 64 60
R14 | 1333 9 17 11 26 11 15 6 | 45 51 46 57 45 48 45
R15 | 1238 10 16 20 16 13 17 7 | 50 53 53 58 56 57 53
R17 | 598 16 30 11 15 21 30 9 | 65 53 58 56 62 71 60
R18 | 785 12 21 25 18 15 20 8 | 66 63 78 63 75 66 68
R19 | 968 46 60 28 50 24 32 17 | 67 64 51 65 65 61 56
R20 | 3034 48 69 48 81 42 27 23 | 80 58 58 98 63 56 61
R21 | 956 15 37 19 27 21 18 10 | 76 67 67 86 75 80 73
R24 | 3674 9 46 14 26 16 16 9 | 56 50 58 66 62 47 54
XR25 |21786 --- --- --- --- --- 3 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1567 24 38 27 31 21 21 |T 66 54 59 67 65 62 60
WRMS | 1567 17 33 20 22 20 20 |NE 66 54 59 67 65 62 60
MEDI | 956 15 32 18 20 18 17 |MD 67 53 58 65 65 64 61
Table 3.2224.4 GPS week: 2224 Day: 4 MJD: 59816
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1239 63 61 64 67 26 22 23 | 106 38 39 107 85 52 62
R02 | 2228 14 37 12 22 21 24 9 | 68 44 59 74 82 58 63
R03 | 900 18 39 13 20 20 16 9 | 77 43 59 77 78 71 66
XR04 | 1526 14 39 17 --- 17 15 10 | 61 46 68 --- 77 60 62
R05 | 1486 23 32 17 16 15 25 9 | 66 36 49 49 57 44 48
R07 | 545 23 23 8 17 16 15 7 | 63 35 49 51 53 53 49
R08 | 1026 12 29 12 14 18 23 8 | 59 34 50 51 56 62 52
R09 | 1228 14 28 10 20 20 25 8 | 29 37 29 29 30 40 28
R11 | 1431 18 14 13 15 31 21 9 | 20 21 25 27 45 32 23
R12 | 1741 11 10 14 17 9 15 6 | 29 27 33 36 28 29 28
R13 | 713 20 19 33 34 35 28 13 | 32 36 45 42 25 53 35
R14 | 882 8 15 8 15 10 11 5 | 29 30 32 28 32 27 28
R15 | 1139 13 18 12 14 19 28 8 | 30 32 35 40 36 50 35
R17 | 686 12 30 8 18 15 15 7 | 71 64 65 73 71 66 66
R18 | 889 19 21 24 12 15 14 8 | 74 74 86 80 82 80 79
R19 | 1215 67 78 36 73 35 31 23 | 80 67 62 95 75 70 63
R20 | 2719 60 55 43 87 40 20 23 | 77 66 44 86 58 45 51
R21 | 772 22 30 9 24 27 18 9 | 62 49 53 62 66 56 55
R24 | 3376 17 29 19 15 21 23 9 | 46 38 43 37 53 43 40
XR25 | ---- --- --- --- --- --- 5 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1530 30 36 25 36 23 21 |T 56 43 48 58 57 52 49
WRMS | 1530 21 31 17 17 21 21 |NE 56 43 48 58 57 52 49
MEDI | 1215 18 29 13 17 20 20 |MD 62 38 49 51 57 53 51
Table 3.2224.5 GPS week: 2224 Day: 5 MJD: 59817
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1286 52 65 73 31 23 29 21 | 84 32 29 67 62 70 52
R02 | 1780 16 35 12 27 16 18 9 | 61 33 47 70 59 40 51
R03 | 1144 27 32 14 14 16 33 10 | 61 33 42 51 62 51 49
XR04 | 2107 17 31 19 --- 16 20 10 | 55 28 45 --- 58 49 46
R05 | 903 19 33 19 12 21 26 9 | 54 42 46 45 58 33 43
R07 | 546 19 32 10 14 12 18 8 | 60 34 48 46 56 50 48
R08 | 1164 15 31 12 12 21 34 10 | 57 33 43 46 48 68 48
R09 | 1114 13 23 13 18 20 12 7 | 24 27 32 32 25 28 24
R11 | 1148 23 24 28 16 20 24 10 | 21 28 45 37 14 21 22
R12 | 1114 15 14 10 14 12 21 6 | 23 17 25 23 19 28 19
R13 | 863 19 38 30 29 49 25 15 | 33 49 35 47 28 38 33
R14 | 581 10 14 14 7 11 18 5 | 24 22 36 28 23 31 25
R15 | 742 8 14 15 8 13 14 5 | 25 26 25 18 23 32 22
R17 | 845 17 32 11 24 22 17 9 | 55 56 47 54 48 50 48
R18 | 869 19 22 21 11 21 15 8 | 45 46 59 57 58 54 52
R19 | 1680 68 95 52 75 31 18 26 | 72 40 34 75 49 40 40
R20 | 3490 38 64 51 74 43 26 23 | 69 48 48 68 54 39 50
R21 | 596 19 32 14 23 15 28 9 | 80 76 80 84 76 60 74
R24 | 1706 19 30 14 15 24 24 9 | 43 38 37 36 44 42 36
XR25 |30250 --- --- --- --- --- 4 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1370 27 40 29 30 24 23 |T 49 37 42 49 45 43 41
WRMS | 1370 21 33 22 15 18 23 |NE 49 37 42 49 45 43 41
MEDI | 1114 19 32 14 15 20 20 |MD 55 33 43 46 49 40 46
Table 3.2224.6 GPS week: 2224 Day: 6 MJD: 59818
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1507 42 64 73 46 19 18 21 | 117 36 31 115 89 85 78
R02 | 1632 9 35 11 11 14 20 7 | 80 46 69 80 78 82 74
R03 | 1196 21 32 14 19 14 31 9 | 91 55 68 84 86 65 76
XR04 | 1666 14 30 11 --- 14 16 8 | 81 54 76 --- 80 68 73
R05 | 947 14 39 25 21 24 28 11 | 72 41 64 76 78 60 65
R07 | 1203 17 31 14 12 14 12 7 | 76 47 59 60 73 58 63
R08 | 1336 7 36 11 10 13 24 7 | 72 40 60 71 71 84 67
R09 | 1148 11 18 11 20 16 21 7 | 25 28 36 25 31 40 28
R11 | 508 17 21 30 19 27 41 12 | 22 30 47 33 38 35 26
R12 | 637 17 14 14 20 15 27 8 | 33 32 35 36 26 36 29
R13 | 1023 15 30 21 14 27 24 10 | 52 53 41 46 46 43 44
R14 | 726 16 19 14 19 10 15 7 | 34 38 48 49 40 49 41
R15 | 788 10 14 16 9 9 29 7 | 43 48 43 47 44 59 45
R17 | 683 18 30 9 21 25 23 9 | 80 67 69 78 68 75 71
R18 | 927 18 27 24 10 24 15 9 | 66 61 79 70 74 74 69
R19 | 1471 79 85 40 51 23 36 24 | 87 78 44 77 64 48 52
R20 | 2620 27 84 61 84 45 38 25 | 95 64 60 125 77 73 76
R21 | 527 11 31 18 21 20 23 9 | 93 76 90 106 90 85 89
R24 | 1163 18 36 17 18 22 16 9 | 64 50 56 59 65 58 56
XR25 |27941 --- --- --- --- --- 6 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1217 26 41 29 30 22 26 |T 67 49 56 68 64 61 59
WRMS | 1217 26 32 21 15 17 25 |NE 67 49 56 68 64 61 59
MEDI | 1148 17 31 16 19 19 23 |MD 72 48 59 70 71 60 65
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