[IGSREPORT-30002] Wk 2323 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 2 07:41:21 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2323 (Jul 14, 2024 - Jul 20, 2024)
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 2.2323.
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:
igl2323[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2323 in the SP3 format.
igl23237.sum Combination Report for GPS Week 2323.
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.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
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 | 11.0 ns
1 | 12.4 ns
2 | 7.5 ns
3 | 11.4 ns
4 | 9.8 ns
5 | 9.2 ns
6 | 8.1 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
4 | JGX | R20
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 1.2323, 1a.2323).
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 2.2323.0-6)
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 3.2323.0-6).
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 2323 summary. (Jul 14, 2024 - Jul 20, 2024)
Table 1.2323.a GPS week : 2323 MJD: 60505.0-60511.0
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 0 -22 -17 50 .12 23 17 | -4715 -210 3248 17347
| 1 1 2 20 18 31 .06 | 2502 1904
esa n/a| 0 -1 4 -9 14 33 -.10 32 21 | 9606 627 2879 7163
| 1 1 2 17 11 48 .07 | 6776 1936
gfz n/a| 0 0 2 11 28 19 -.04 28 17 | 0 -3 2929 8124
| 1 1 3 13 11 54 .08 | 0 1864
grg n/a| 1 0 4 0 10 -49 .46 27 20 | 7030 -286 3309 17269
| 1 1 0 36 18 78 .09 | 1443 1801
iac n/a| 0 1 -4 -8 -14 -25 -.17 17 14 | 9469 -1341 3209 16711
| 1 0 1 12 14 64 .07 | 2001 1036
jgx n/a| 1 0 -1 19 -9 -17 -.20 30 27 | 772 -5 2879 8221
| 1 0 2 19 12 54 .07 | 1950 1748
Table 1.2323.b GPS week : 2323 MJD: 60505.0-60511.0
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 14 15 14 17 17 15 |
R02 | 6 5 6 7 8 6 7 |
R03 | 6 7 7 7 7 6 6 |
R04 | 6 6 7 7 7 8 10 |
R05 | 6 7 6 7 7 8 8 |
R07 | 6 7 6 6 6 8 7 |
R08 | 7 6 7 8 5 8 8 |
R09 | 6 6 7 6 6 7 5 |
R11 | 6 7 7 5 6 8 7 |
R12 | 7 8 7 6 6 7 6 |
R13 | 14 16 18 14 14 15 17 |
R14 | 6 6 6 6 4 6 6 |
R15 | 6 5 6 7 6 7 5 |
R16 | 6 7 7 10 10 8 7 |
R17 | 7 7 7 7 6 8 8 |
R18 | 8 8 8 8 8 10 9 |
R19 | 23 21 18 17 16 17 19 |
R20 | 32 33 28 32 30 30 27 |
R21 | 7 7 8 7 8 10 7 |
R22 | 7 7 7 6 9 9 8 |
R24 | 7 7 8 8 7 10 9 |
R25 | 11 12 8 9 12 13 10 |
R26 | 36 37 38 36 35 39 40 |
Table 1.2323.c GPS week : 2323 MJD: 60505.0-60511.0
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 2323 0 | 34 35 -39 -1746 1156 3801 80.8 1802 1802 | 10995 0
brd 2323 1 | -49 -53 36 -1175 142 3863 81.9 1752 1752 | 12413 0
brd 2323 2 | 133 17 97 -10 1786 -1145 79.6 1607 1607 | 7508 0
brd 2323 3 | 17 80 104 -1563 712 -5558 79.0 1537 1537 | 11358 0
brd 2323 4 | 1 80 42 -2270 1417 -6226 79.1 1557 1557 | 9759 0
brd 2323 5 | -24 -1 198 1384 -761 2117 81.5 1776 1776 | 9212 0
brd 2323 6 | -5 59 207 22 923 1834 81.3 1859 1859 | 8062 0
-------------+------------------------------------------------------------+----------------
brd 2323 mean| 15 31 92 -765 767 -187 80.5 1698 1698 | 9901 0
brd 2323 sdev| 58 48 88 1280 853 4241 1.2 128 128 | 1790 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 2.2323.0 GPS week: 2323 Day: 0 MJD: 60505
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 6 -27 -5 .10 23 17 | -5956 707 3263 12331
esa n/a| -2 -2 0 -26 20 -27 -.14 31 18 | 20000 1613 3170 8782
gfz n/a| 0 0 -1 1 35 6 .01 27 14 | 0 1094 3220 8852
grg n/a| 3 0 5 -23 33 -56 .29 25 20 | 8939 707 3323 12103
iac n/a| -1 1 -3 -13 -27 87 -.13 17 13 | 11654 -1000 3250 11883
jgx n/a| 2 0 1 -8 -30 -57 -.17 32 32 | -1977 887 3260 8965
Table 2.2323.1 GPS week: 2323 Day: 1 MJD: 60506
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 -22 -20 47 .10 23 16 | -4506 1838 3648 16858
esa n/a| 0 -4 7 7 6 82 -.21 35 20 | 14425 2513 3401 8303
gfz n/a| 2 0 2 27 21 59 -.06 33 18 | 0 2410 3478 9327
grg n/a| 1 2 4 -31 6 -82 .46 26 22 | 8569 1548 3708 16824
iac n/a| -1 1 -6 -13 -2 -42 -.08 15 13 | 11668 21 3609 16152
jgx n/a| 0 0 -2 33 -12 -4 -.18 29 29 | 963 1898 3408 9586
Table 2.2323.2 GPS week: 2323 Day: 2 MJD: 60507
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 -21 -3 87 .08 24 19 | -7744 -3566 3322 20160
esa n/a| 0 -2 5 3 26 77 -.06 32 21 | 13822 -2366 2692 6978
gfz n/a| 0 -2 7 24 49 35 .01 31 20 | 0 -2938 2737 8259
grg n/a| 1 0 4 -27 37 -60 .41 28 22 | 5593 -3427 3427 20254
iac n/a| 0 1 -3 3 -29 -39 -.16 13 12 | 6797 -2744 3272 19360
jgx n/a| 1 0 -3 -4 -21 -18 -.08 26 25 | -1618 -2714 2628 8278
Table 2.2323.3 GPS week: 2323 Day: 3 MJD: 60508
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 -20 4 36 .10 19 16 | -6209 1258 3523 23585
esa n/a| 0 0 4 11 2 -7 -.10 30 20 | 8908 2798 2607 6876
gfz n/a| 0 -2 4 21 23 -59 .03 25 16 | 0 1344 2628 7079
grg n/a| 2 1 5 -7 10 46 .47 28 21 | 6318 803 3595 24042
iac n/a| 0 2 -6 -8 -30 18 -.19 17 14 | 8666 -513 3457 22657
jgx n/a| 0 0 -2 12 -6 -75 -.19 33 32 | 1066 1433 2573 7371
Table 2.2323.4 GPS week: 2323 Day: 4 MJD: 60509
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 -53 -8 49 .17 21 18 | -5946 -1573 3310 27124
esa n/a| 1 -1 4 -6 22 58 -.14 32 20 | 2894 -750 2709 6227
gfz n/a| 0 0 1 11 12 25 -.20 22 15 | 0 -1405 2739 6622
grg n/a| 0 0 4 -10 -12 25 .47 24 18 | 5190 -1798 3376 27660
iac n/a| -3 0 -3 11 -12 -65 -.12 18 15 | 7454 -2674 3253 26191
jgx n/a| 2 0 -5 34 6 -48 -.19 37 23 | 1868 -1429 2712 6898
Table 2.2323.5 GPS week: 2323 Day: 5 MJD: 60510
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 2 -40 -17 82 .24 24 17 | -1471 769 2756 10137
esa n/a| 0 0 5 -26 24 -15 -.07 30 22 | 1504 1336 2705 6102
gfz n/a| 1 0 -1 -7 30 -35 -.10 30 20 | 0 540 2768 8198
grg n/a| 5 0 2 51 -2 -25 .57 28 19 | 7738 951 2793 9499
iac n/a| 0 2 -5 -24 3 -18 -.29 19 17 | 11017 -1351 2737 10033
jgx n/a| 0 0 -2 42 -6 -5 -.25 28 27 | 1581 1058 2685 8307
Table 2.2323.6 GPS week: 2323 Day: 6 MJD: 60511
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 1 -1 -4 -51 57 .06 25 16 | -1173 -908 2918 11238
esa n/a| 0 -2 4 -27 -1 67 .00 32 28 | 5691 -751 2874 6879
gfz n/a| 1 0 1 3 30 101 .01 25 17 | 0 -1070 2937 8536
grg n/a| 0 0 3 51 -2 -191 .51 27 20 | 6867 -792 2946 10507
iac n/a| 1 1 -6 -18 -4 -115 -.21 18 16 | 9028 -1131 2885 10705
jgx n/a| -1 0 2 24 1 88 -.31 22 20 | 3523 -1172 2887 8146
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 3.2323.0 GPS week: 2323 Day: 0 MJD: 60505
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1086 30 38 38 24 20 49 14 | 77 82 95 85 75 87 79
XR02E | 1232 6 11 9 15 14 --- 6 | 48 46 47 48 47 --- 46
R03E | 2333 17 13 10 19 10 11 6 | 44 51 51 53 49 43 47
R04E | 2258 15 11 11 20 13 12 6 | 119 120 123 122 112 114 118
R05E | 1495 13 13 12 15 16 13 6 | 122 119 118 125 110 116 117
R07E | 1213 13 14 11 16 7 12 5 | 115 119 116 117 110 113 114
R08E | 1356 11 16 12 20 14 12 6 | 124 126 122 127 123 125 124
R09 | 1462 11 13 10 20 8 16 6 | 27 26 28 30 20 30 23
R11 | 864 19 8 15 8 9 11 5 | 41 36 37 37 35 33 35
R12 | 905 17 12 16 19 17 14 7 | 70 63 61 69 58 70 63
R13 | 2158 26 15 21 47 18 46 13 | 62 54 65 57 41 43 50
R14 | 2321 9 6 19 13 17 8 6 | 49 49 49 48 53 45 48
R15 | 1222 13 14 12 10 11 14 5 | 55 58 62 62 60 51 57
R16 | 1467 15 17 17 8 10 10 6 | 55 65 65 56 60 59 58
R17 | 1460 13 11 19 21 10 19 7 | 63 53 64 51 57 51 55
R18 | 1145 6 23 14 16 14 26 7 | 80 86 83 85 76 74 79
R19 | 1375 44 71 75 26 26 59 23 | 112 62 141 96 100 61 93
R20 | 2987 58 98 67 70 42 96 32 | 119 54 113 83 95 54 81
R21 | 783 15 11 15 17 14 15 6 | 58 53 55 53 50 45 51
R22 | 3599 15 12 14 17 16 9 6 | 83 84 78 90 84 73 81
R24 | 1563 22 13 9 14 11 22 7 | 56 53 45 53 48 50 48
XR25 |11904 11 16 --- --- 15 --- 10 | 28 33 --- --- 35 --- 30
XR26E | 8133 45 --- --- 42 58 --- 36 | 43 --- --- 41 33 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1802 23 31 27 25 17 32 |T 71 67 77 72 66 66 66
WRMS | 1802 17 18 14 20 13 32 |NE 63 55 67 62 58 52 56
MEDI | 1462 15 13 14 17 14 14 |MD 62 54 65 57 58 54 57
Table 3.2323.1 GPS week: 2323 Day: 1 MJD: 60506
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 856 24 53 40 18 21 34 14 | 60 59 82 58 65 54 57
XR02E | 1003 9 9 12 12 8 --- 5 | 28 30 30 34 29 --- 28
R03E | 1736 9 13 17 18 15 14 6 | 43 40 48 50 47 42 43
R04E | 2175 10 12 18 14 12 14 6 | 72 72 76 79 76 74 74
R05E | 1357 17 14 15 16 12 15 6 | 78 68 75 76 71 67 72
R07E | 1105 14 15 27 16 11 12 7 | 66 68 66 76 65 66 66
R08E | 879 10 15 14 13 11 12 5 | 86 87 98 95 94 90 91
R09 | 1839 11 11 13 15 16 10 6 | 22 16 29 18 27 25 20
R11 | 1139 15 15 17 11 12 18 6 | 20 23 24 21 21 23 18
R12 | 1094 21 12 20 15 20 15 8 | 63 56 57 62 51 57 55
R13 | 2269 25 22 43 64 22 30 16 | 30 34 25 39 31 27 23
R14 | 1769 8 9 15 17 14 11 6 | 26 29 27 26 32 20 24
R15 | 1368 8 10 13 11 13 12 5 | 32 43 44 40 34 40 36
R16 | 1769 10 21 17 21 11 16 7 | 34 48 44 30 45 29 37
R17 | 1290 14 11 20 24 8 17 7 | 53 51 57 51 47 59 51
R18 | 1281 5 30 23 16 11 18 7 | 76 75 91 76 64 72 73
R19 | 1575 50 77 53 46 20 37 21 | 70 62 93 79 66 62 67
R20 | 1736 64 105 104 49 24 98 32 | 75 50 112 73 63 42 59
R21 | 733 17 13 11 18 7 25 7 | 61 53 55 58 54 48 53
R22 | 3910 14 13 16 14 9 21 6 | 77 79 74 87 76 69 75
R24 | 2289 20 21 14 15 11 17 7 | 48 45 44 48 41 43 43
XR25 |14285 19 21 --- --- 13 --- 12 | 24 39 --- --- 36 --- 31
XR26E |10401 39 --- --- 56 56 --- 36 | 41 --- --- 37 25 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1751 23 35 33 26 15 29 |T 51 51 59 55 50 50 49
WRMS | 1751 16 20 18 22 13 29 |NE 47 46 55 50 45 44 44
MEDI | 1575 14 14 17 16 12 16 |MD 53 50 57 51 47 48 51
Table 3.2323.2 GPS week: 2323 Day: 2 MJD: 60507
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1049 32 56 34 21 19 38 15 | 59 67 67 60 55 56 53
XR02E | 760 8 15 14 12 10 --- 6 | 40 37 43 43 35 --- 37
R03E | 1221 13 14 21 30 9 10 7 | 74 82 75 73 75 75 74
R04E | 1625 14 12 19 16 12 19 6 | 45 46 48 54 49 49 47
R05E | 1667 10 11 18 17 11 14 6 | 45 50 52 54 51 45 49
R07E | 1079 10 15 15 13 10 14 5 | 49 50 48 55 42 47 46
R08E | 1239 10 15 19 17 13 14 6 | 54 54 50 58 54 49 52
R09 | 2408 13 9 25 22 12 12 7 | 30 34 33 39 20 34 27
R11 | 1262 17 11 15 14 9 21 6 | 31 25 23 29 31 28 25
R12 | 1133 11 17 24 14 15 15 7 | 50 57 57 51 41 53 47
R13 | 1601 45 19 32 73 16 43 17 | 60 42 48 27 36 40 36
R14 | 1023 9 16 16 12 9 15 5 | 34 45 48 35 32 45 36
R15 | 674 9 11 25 10 8 16 6 | 41 46 53 38 40 37 39
R16 | 948 18 18 22 15 9 16 7 | 41 60 56 45 56 53 50
R17 | 1491 19 15 14 15 6 17 6 | 52 43 43 40 43 35 41
R18 | 1514 14 25 23 18 8 19 7 | 69 73 63 63 65 77 67
R19 | 1278 33 61 59 44 23 34 18 | 61 40 57 62 53 43 47
R20 | 1204 67 96 78 59 21 69 28 | 94 57 94 56 52 61 57
R21 | 631 16 18 22 13 11 22 7 | 51 54 44 51 50 42 47
R22 | 3215 13 15 30 15 11 10 7 | 71 69 71 79 77 72 72
R24 | 2985 12 26 20 15 13 15 7 | 47 54 44 55 44 43 45
XR25 |16786 11 14 --- --- 8 --- 7 | 28 33 --- --- 24 --- 26
XR26E |11546 47 --- --- 63 51 --- 37 | 42 --- --- 39 34 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1606 24 32 31 28 13 26 |T 50 50 53 50 46 49 45
WRMS | 1606 19 21 20 22 12 25 |NE 50 48 52 47 44 47 44
MEDI | 1262 13 15 22 15 11 16 |MD 49 50 50 51 44 45 47
Table 3.2323.3 GPS week: 2323 Day: 3 MJD: 60508
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1345 22 43 42 18 23 28 13 | 78 88 109 86 99 84 88
XR02E | 1510 11 19 14 14 11 --- 6 | 43 40 39 44 31 --- 36
R03E | 1129 11 13 15 17 17 20 7 | 69 75 72 71 69 82 71
R04E | 1327 9 12 13 24 13 15 6 | 41 41 39 53 42 35 40
R05E | 1420 9 16 18 25 10 11 6 | 43 42 48 40 44 33 40
R07E | 1244 12 16 10 17 11 8 5 | 42 46 47 53 38 39 42
R08E | 1125 15 17 9 14 21 18 7 | 57 59 57 72 68 55 60
R09 | 1641 13 7 13 25 10 13 6 | 23 20 22 34 20 21 20
R11 | 806 7 8 12 14 11 13 4 | 33 33 38 35 33 33 33
R12 | 884 11 23 12 8 13 15 6 | 42 38 35 41 42 47 39
R13 | 627 27 19 21 60 13 39 14 | 47 35 36 42 37 35 36
R14 | 1246 7 7 15 12 15 13 5 | 34 42 43 43 45 36 39
R15 | 827 12 14 19 11 12 20 6 | 44 47 54 46 45 40 44
R16 | 913 17 29 32 20 14 9 9 | 45 68 68 42 44 49 49
R17 | 1698 13 16 15 18 12 18 6 | 74 68 71 61 58 60 64
R18 | 1444 8 27 24 16 11 14 7 | 76 88 78 70 69 78 74
R19 | 1188 34 54 44 30 28 39 17 | 82 58 83 70 65 52 63
R20 | 2424 47 90 63 78 38 118 32 | 99 56 117 82 61 64 73
R21 | 734 15 17 15 21 14 16 7 | 48 34 46 55 47 34 42
R22 | 2983 15 10 13 17 8 16 6 | 45 47 54 62 52 50 50
R24 | 2880 13 23 15 17 21 21 8 | 40 38 33 45 38 43 36
XR25 |15476 15 13 --- --- 10 --- 9 | 31 39 --- --- 46 --- 38
XR26E |12323 37 --- --- 51 59 --- 35 | 29 --- --- 41 41 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1537 18 30 25 28 17 33 |T 50 50 56 54 49 48 48
WRMS | 1537 16 20 16 21 14 32 |NE 50 47 55 52 46 45 46
MEDI | 1327 13 16 15 17 13 16 |MD 44 42 48 46 45 43 42
Table 3.2323.4 GPS week: 2323 Day: 4 MJD: 60509
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1393 35 61 36 23 41 14 16 | 84 118 108 84 76 83 87
XR02E | 1048 8 19 12 17 18 --- 7 | 39 39 40 43 35 --- 37
R03E | 1729 12 20 14 14 17 14 7 | 69 67 73 75 69 64 68
R04E | 1014 14 13 17 13 10 18 6 | 44 45 46 48 40 44 42
R05E | 1626 13 16 9 25 14 16 7 | 47 53 47 62 46 41 47
R07E | 1365 10 9 11 15 13 12 5 | 49 47 49 54 43 45 46
R08E | 991 14 15 9 11 10 10 5 | 54 57 51 60 51 57 53
R09 | 1510 11 11 13 17 13 11 5 | 28 29 21 28 29 34 25
R11 | 881 11 15 13 9 11 15 5 | 31 35 26 36 30 21 27
R12 | 855 10 10 17 16 11 15 6 | 51 48 46 49 53 44 47
R13 | 848 32 22 21 43 12 43 14 | 46 29 34 29 41 37 32
R14 | 883 8 12 9 9 8 10 4 | 25 32 19 29 19 22 22
R15 | 803 12 14 17 9 14 15 6 | 36 27 32 31 34 24 28
R16 | 1522 21 19 28 11 30 16 10 | 36 42 55 33 29 35 33
R17 | 1370 18 14 9 14 14 14 6 | 60 46 43 54 54 52 50
R18 | 1377 13 30 17 12 14 17 8 | 85 91 84 78 86 78 82
R19 | 1371 45 49 34 36 26 30 16 | 83 61 81 70 66 87 71
R20 | 2655 41 95 57 65 28 147 29 | 95 69 133 109 81 60 102
R21 | 878 15 19 23 16 10 17 7 | 68 54 65 54 63 54 59
R22 | 3637 20 18 16 32 11 12 8 | 83 83 84 105 83 78 84
R24 | 1438 15 23 12 18 13 13 7 | 54 58 55 60 49 49 52
XR25 |15504 19 13 --- --- 15 --- 11 | 18 23 --- --- 34 --- 24
XR26E |12346 36 --- --- 43 63 --- 35 | 29 --- --- 28 35 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 1557 21 32 22 24 18 37 |T 52 52 56 55 49 50 49
WRMS | 1557 18 20 15 18 15 23 |NE 53 48 55 54 50 48 49
MEDI | 1371 14 16 16 16 14 15 |MD 49 47 49 54 46 45 47
Table 3.2323.5 GPS week: 2323 Day: 5 MJD: 60510
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1719 32 38 46 30 37 37 16 | 103 98 129 103 85 107 99
XR02E | 928 9 17 9 9 10 --- 5 | 33 31 30 38 28 --- 30
R03E | 1720 14 14 16 16 12 12 6 | 68 68 70 70 66 63 66
R04E | 1344 9 20 18 20 19 16 7 | 80 71 79 88 84 77 79
R05E | 1265 13 12 26 17 14 23 8 | 79 67 76 80 73 73 73
R07E | 2244 12 18 15 27 17 15 8 | 79 82 77 74 76 77 76
R08E | 1091 11 15 20 21 19 12 7 | 80 74 75 81 78 74 76
XR09 | 1546 9 10 17 19 15 --- 7 | 13 12 20 22 13 --- 10
R11 | 1212 15 15 19 20 17 15 7 | 26 31 31 28 21 29 23
R12 | 696 10 15 15 15 21 15 7 | 31 28 34 22 38 23 27
R13 | 1343 26 18 23 52 17 53 15 | 38 47 33 31 49 46 37
R14 | 1576 9 12 9 12 16 14 5 | 30 25 25 31 37 22 27
R15 | 1360 9 24 11 23 13 12 7 | 30 26 28 43 39 27 30
R16 | 1307 15 18 19 12 23 11 7 | 30 36 35 34 28 34 28
R17 | 1509 19 14 8 18 20 23 8 | 56 50 53 57 55 42 50
R18 | 1055 14 36 36 13 16 6 9 | 45 51 42 50 50 38 43
R19 | 853 36 57 50 30 20 26 16 | 67 59 83 65 55 56 59
R20 | 4454 72 86 78 60 24 79 30 | 85 39 85 62 46 47 52
R21 | 769 21 17 23 32 12 27 10 | 51 47 52 49 45 35 43
R22 | 2931 17 18 19 33 17 10 8 | 46 48 51 46 45 44 44
R24 | 1201 11 22 33 26 15 25 9 | 54 65 69 64 58 51 56
XR25 |21123 20 14 --- --- 16 --- 12 | 16 36 --- --- 37 --- 28
XR26E |18832 43 --- --- 50 65 --- 38 | 29 --- --- 42 27 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 1776 24 30 30 28 19 28 |T 50 49 56 53 49 50 47
WRMS | 1776 17 22 20 19 17 27 |NE 41 40 45 43 41 38 37
MEDI | 1344 14 17 19 20 17 15 |MD 46 47 52 49 46 46 43
Table 3.2323.6 GPS week: 2323 Day: 6 MJD: 60511
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1919 48 30 30 25 27 27 14 | 68 66 76 70 62 72 64
XR02E | 1126 10 10 17 19 9 --- 6 | 34 31 37 42 34 --- 33
R03E | 811 11 14 12 13 16 13 6 | 76 81 75 75 75 76 75
R04E | 2160 20 25 21 25 22 16 9 | 88 91 98 92 93 95 91
R05E | 1488 13 13 25 17 16 16 7 | 92 91 100 96 84 91 91
R07E | 1450 13 14 22 18 13 15 7 | 80 85 77 87 77 86 80
R08E | 2112 9 10 11 29 22 20 8 | 85 82 83 83 88 88 84
R09 | 1047 9 8 16 9 13 12 5 | 29 28 34 37 27 26 28
R11 | 1713 13 14 14 15 11 18 6 | 37 31 37 40 34 30 33
R12 | 649 9 12 13 15 18 14 6 | 52 49 54 53 48 46 49
R13 | 1020 18 12 24 66 15 55 16 | 57 56 49 50 58 61 53
R14 | 1422 9 19 14 12 11 10 5 | 42 45 41 44 44 41 42
R15 | 2290 11 14 11 16 10 7 5 | 50 47 47 57 53 43 48
R16 | 1834 17 11 20 15 16 10 7 | 50 52 56 53 42 47 46
R17 | 1856 20 15 18 20 7 20 7 | 81 67 75 69 73 63 70
R18 | 1092 12 37 15 18 18 14 9 | 69 83 57 63 62 60 63
R19 | 1436 41 78 37 43 14 34 19 | 107 51 108 100 85 65 82
R20 | 4086 69 94 73 39 41 37 27 | 131 80 149 100 83 84 95
R21 | 850 17 17 19 15 7 20 7 | 86 76 85 79 76 64 76
R22 | 3056 15 18 12 24 14 17 7 | 81 82 76 87 82 75 79
R24 | 1305 24 19 18 30 10 14 8 | 87 89 83 92 87 79 84
XR25 |22742 9 18 --- --- 14 --- 10 | 39 45 --- --- 43 --- 40
XR26E |20802 44 --- --- 58 64 --- 40 | 60 --- --- 58 52 --- 52
------+-----------------------------------------+-------------------------------------
RMS | 1858 25 32 25 27 18 22 |T 68 64 71 69 63 64 63
WRMS | 1858 16 28 17 20 16 20 |NE 66 58 67 66 59 56 59
MEDI | 1488 13 14 18 18 14 16 |MD 69 66 75 69 62 64 64
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