[IGSREPORT-30253] Wk 2345 IGLOS Final Orbits
acc
acc at igs.org
Fri Jan 3 08:58:55 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2345 (Dec 15, 2024 - Dec 21, 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 2.2345.
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:
igl2345[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2345 in the SP3 format.
igl23457.sum Combination Report for GPS Week 2345.
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 | -3.6 ns
1 | -8.6 ns
2 | -8.2 ns
3 | -7.0 ns
4 | 2.0 ns
5 | -2.0 ns
6 | 1.0 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 1.2345, 1a.2345).
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 2.2345.0-6)
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 3.2345.0-6).
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 2345 summary. (Dec 15, 2024 - Dec 21, 2024)
Table 1.2345.a GPS week : 2345 MJD: 60659.0-60665.0
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 8 -17 53 .18 19 16 | 11289 -809 6142 36742
| 0 0 3 16 11 15 .06 | 15225 1959
esa n/a| 0 0 1 0 3 4 -.13 35 28 | -6102 -1566 3433 8334
| 0 1 2 7 19 24 .05 | 2703 2048
gfz n/a| 0 0 1 10 4 9 .01 23 17 | 0 -782 3428 8179
| 1 2 1 22 11 41 .03 | 0 2012
grg n/a| 0 0 7 -42 -23 -42 .32 32 23 | 18 -749 6143 36463
| 1 1 2 16 21 48 .06 | 15715 1991
iac n/a| 0 0 -3 7 21 -30 -.12 19 17 | 1808 -123 6150 36620
| 0 1 3 17 20 40 .04 | 15323 1296
jgx n/a| 0 1 0 -9 -6 1 -.18 21 21 | 9106 -714 3398 8242
| 1 0 2 12 12 28 .03 | 2598 1891
Table 1.2345.b GPS week : 2345 MJD: 60659.0-60665.0
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 16 13 12 14 16 16 |
R02 | 6 8 11 13 6 6 6 |
R03 | 8 10 16 8 7 7 7 |
R04 | 8 9 11 12 8 8 7 |
R05 | 9 8 9 11 9 6 6 |
R07 | 9 9 17 12 7 8 7 |
R08 | 8 11 12 6 8 6 7 |
R09 | 7 6 8 5 8 6 6 |
R11 | 7 6 5 9 6 11 6 |
R12 | 7 6 7 6 5 7 7 |
R14 | 8 7 7 6 5 7 6 |
R15 | 7 8 7 7 6 7 7 |
R16 | 7 8 8 8 7 8 8 |
R17 | 7 6 8 7 8 8 7 |
R18 | 8 8 8 7 6 7 10 |
R19 | 20 17 18 21 19 21 18 |
R20 | 27 21 24 22 25 24 22 |
R21 | 6 8 8 9 10 11 8 |
R22 | 6 6 10 7 7 6 6 |
R24 | 9 10 9 10 10 9 9 |
R26 | 33 35 47 28 31 27 29 |
Table 1.2345.c GPS week : 2345 MJD: 60659.0-60665.0
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 2345 0 | -117 -15 -72 489 1937 -1898 80.3 1750 1750 | -3592 0
brd 2345 1 | 7 35 50 642 1798 -2628 78.8 1743 1743 | -8561 0
brd 2345 2 | 19 -36 -31 45 1111 -963 78.7 1977 1977 | -8164 0
brd 2345 3 | 14 136 98 -3957 640 -2307 80.5 1705 1705 | -7019 0
brd 2345 4 | 32 55 37 -542 -43 -312 80.9 1802 1802 | 2028 0
brd 2345 5 | 56 17 -20 -1796 -135 -324 82.4 1599 1599 | -2015 0
brd 2345 6 | 11 19 21 -876 -1276 -1016 82.8 1658 1658 | 1027 0
-------------+------------------------------------------------------------+----------------
brd 2345 mean| 3 30 11 -856 575 -1350 80.6 1747 1747 | -3756 0
brd 2345 sdev| 55 55 57 1605 1151 934 1.6 120 120 | 4331 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 2.2345.0 GPS week: 2345 Day: 0 MJD: 60659
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 3 19 -7 79 .12 17 14 | 6419 2350 2944 11046
esa n/a| 0 2 4 -9 -21 26 -.12 39 22 | -9800 1793 2914 10399
gfz n/a| 1 2 0 -13 7 30 -.02 23 16 | 0 2457 2920 8321
grg n/a| 0 0 5 -33 -44 -18 .31 29 23 | -6802 2562 2928 10746
iac n/a| 0 -2 -9 20 42 -87 -.10 15 15 | -3836 1139 2930 10651
jgx n/a| -3 1 4 -24 -11 26 -.22 25 25 | 9338 2460 2928 8396
Table 2.2345.1 GPS week: 2345 Day: 1 MJD: 60660
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 3 -6 -27 42 .22 21 18 | 5380 -3513 4136 11233
esa n/a| 1 0 2 7 0 7 -.08 34 22 | -8270 -4517 4175 8257
gfz n/a| 0 -2 3 1 0 -58 -.00 22 14 | 0 -3355 4148 8682
grg n/a| 0 3 3 -66 -22 -39 .35 40 25 | -8411 -3528 4194 10897
iac n/a| 0 0 -2 6 35 3 -.08 15 14 | -6923 -1169 4126 10791
jgx n/a| -1 1 -2 -19 -17 12 -.15 18 18 | 7495 -3320 4130 8906
Table 2.2345.2 GPS week: 2345 Day: 2 MJD: 60661
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 -3 13 -35 30 .27 24 19 | 1935 50 3483 11130
esa n/a| 0 2 0 3 -14 24 -.10 32 25 | -6489 -214 3494 8134
gfz n/a| -1 1 3 49 7 3 -.01 20 19 | 0 515 3511 8800
grg n/a| 0 0 9 -35 -38 30 .19 48 27 | -9589 -177 3450 10889
iac n/a| 0 -2 0 -25 24 -31 -.06 22 22 | -7129 -735 3469 10838
jgx n/a| 1 0 -3 -16 8 -18 -.12 19 19 | 5514 79 3498 8804
Table 2.2345.3 GPS week: 2345 Day: 3 MJD: 60662
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 -3 27 -15 49 .20 18 15 | 4378 -2605 3402 11508
esa n/a| -1 0 3 0 -8 17 -.09 35 28 | -6535 -3385 3405 7964
gfz n/a| 1 1 2 16 24 11 -.01 24 17 | 0 -2733 3412 9207
grg n/a| 2 -1 9 -66 -7 -127 .38 30 19 | -7525 -2416 3397 11111
iac n/a| 0 -2 -6 0 35 -7 -.14 22 20 | -5527 -1779 3386 11167
jgx n/a| -1 0 -3 -2 -26 19 -.17 18 18 | 7805 -2325 3326 9088
Table 2.2345.4 GPS week: 2345 Day: 4 MJD: 60663
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 12 -5 51 .16 17 14 | 45513 223 22375 193359
esa n/a| 0 0 1 2 33 2 -.17 39 39 | -1751 -1580 3416 9253
gfz n/a| 0 0 1 -16 -10 60 -.00 19 18 | 0 79 3350 7046
grg n/a| 1 0 7 -37 16 -62 .31 27 26 | 34810 505 22384 193405
iac n/a| 1 0 -3 27 8 -20 -.13 17 15 | 35840 1427 22492 194407
jgx n/a| 0 0 -1 9 1 -44 -.20 25 25 | 13775 200 3314 7130
Table 2.2345.5 GPS week: 2345 Day: 5 MJD: 60664
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 12 -22 62 .18 19 16 | 7814 -1619 3103 8100
esa n/a| 0 0 1 7 16 1 -.20 37 32 | -6258 -1692 3062 6554
gfz n/a| 2 -3 1 16 12 45 .06 31 19 | 0 -1753 3076 6863
grg n/a| 0 0 9 -31 -41 -54 .34 25 20 | -2098 -1414 3105 7791
iac n/a| 0 0 -3 4 -16 -84 -.17 18 16 | -1150 1062 3093 8116
jgx n/a| 0 1 0 3 5 31 -.18 20 20 | 9594 -1445 3036 6811
Table 2.2345.6 GPS week: 2345 Day: 6 MJD: 60665
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 -3 -20 -7 61 .08 17 15 | 7585 -552 3555 10824
esa n/a| 0 0 -1 -9 16 -46 -.16 33 24 | -3614 -1371 3571 7782
gfz n/a| 1 0 0 21 -6 -27 .04 22 16 | 0 -687 3581 8337
grg n/a| 0 1 6 -27 -26 -24 .33 23 18 | -257 -777 3543 10407
iac n/a| 0 0 1 19 16 14 -.16 19 17 | 1381 -807 3555 10375
jgx n/a| 0 1 0 -14 -2 -19 -.19 20 20 | 10222 -647 3556 8561
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 3.2345.0 GPS week: 2345 Day: 0 MJD: 60659
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 589 22 34 30 52 19 38 14 | 104 106 105 130 93 104 102
R02E | 772 10 18 10 19 10 13 5 | 59 59 58 64 56 13 57
R03E | 667 20 15 19 9 17 16 7 | 141 139 143 143 142 135 140
R04E | 1681 23 19 18 11 18 16 8 | 217 221 221 216 205 215 214
R05E | 990 11 15 13 33 18 22 8 | 173 161 172 170 179 163 172
R07E | 769 13 24 24 12 12 27 8 | 181 180 187 190 181 179 182
R08E | 597 10 17 19 20 18 14 7 | 108 110 113 115 109 109 109
R09 | 903 8 15 16 23 13 22 7 | 37 43 49 39 35 48 39
R11 | 856 13 20 14 17 10 17 6 | 35 41 38 34 31 34 33
R12 | 1922 15 22 6 23 10 17 7 | 75 72 70 63 74 66 70
R14 | 621 10 13 17 9 21 24 7 | 59 57 55 51 71 47 57
R15 | 1751 14 25 11 13 14 22 7 | 81 66 72 75 81 68 74
R16 | 810 17 21 11 11 16 15 7 | 79 62 69 71 67 58 67
R17 | 792 12 16 19 9 6 30 7 | 59 46 60 64 57 39 54
R18 | 512 12 10 18 18 13 29 7 | 47 53 56 63 52 33 49
R19 | 3028 26 95 19 63 18 37 19 | 92 59 84 95 89 78 78
R20 | 5666 28 118 69 73 26 52 27 | 114 67 139 123 117 96 108
R21 | 561 13 22 10 11 11 14 6 | 70 51 71 68 69 58 65
R22 | 1299 12 17 13 11 14 15 6 | 34 31 33 40 38 27 31
R24 | 1249 21 25 24 14 9 22 8 | 72 49 73 75 67 56 65
XR26E |13877 42 --- --- 43 52 --- 33 | 36 --- --- 52 37 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1749 17 39 23 29 15 25 |T 89 83 93 92 88 81 85
WRMS | 1749 14 22 16 23 15 25 |NE 65 53 66 66 65 54 60
MEDI | 856 13 19 17 17 14 22 |MD 75 59 71 71 71 58 67
Table 3.2345.1 GPS week: 2345 Day: 1 MJD: 60660
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 539 36 25 44 78 17 23 16 | 89 101 101 111 85 85 88
XR02E | 722 17 14 14 29 13 --- 8 | 44 51 51 54 48 --- 47
R03E | 1559 17 21 19 43 23 17 10 | 153 144 141 140 143 139 141
R04E | 1595 30 21 20 31 12 16 9 | 192 182 190 182 178 184 184
R05E | 1730 9 18 19 32 21 13 8 | 162 161 164 167 165 156 162
R07E | 1138 13 23 17 38 16 21 9 | 185 176 186 184 183 175 181
R08E | 893 18 24 29 47 11 20 10 | 111 115 124 119 105 104 109
R09 | 893 11 16 14 19 9 14 5 | 29 33 31 35 28 36 29
R11 | 703 11 14 10 28 14 10 6 | 29 30 27 32 26 28 26
R12 | 571 11 17 10 25 11 10 5 | 62 65 65 62 72 67 66
R14 | 753 12 8 18 19 16 13 6 | 47 50 45 40 62 45 49
R15 | 1309 23 11 17 18 14 13 7 | 61 52 55 49 62 52 55
R16 | 547 24 24 20 16 11 15 8 | 60 38 49 55 51 45 48
R17 | 868 13 14 11 16 8 14 5 | 35 32 35 44 30 31 32
R18 | 575 15 9 28 12 7 22 8 | 31 35 53 42 38 31 35
R19 | 1449 31 77 25 60 16 34 17 | 49 42 39 54 40 29 35
R20 | 5783 32 95 36 91 24 24 21 | 60 48 48 77 53 67 50
R21 | 880 24 22 18 17 13 10 7 | 44 29 24 33 26 24 25
R22 | 1764 17 16 9 17 10 14 6 | 32 29 30 34 28 30 27
R24 | 1621 18 42 13 32 15 18 9 | 50 39 45 57 50 37 44
XR26E |13635 54 --- --- 57 44 --- 35 | 54 --- --- 78 42 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 1742 21 34 22 40 15 18 |T 75 72 75 78 72 71 70
WRMS | 1742 18 22 14 25 14 18 |NE 45 40 42 47 43 40 40
MEDI | 893 17 18 18 29 14 15 |MD 54 48 49 55 51 45 48
Table 3.2345.2 GPS week: 2345 Day: 2 MJD: 60661
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 622 33 31 27 27 19 31 12 | 48 50 56 53 46 51 46
XR02E | 1060 15 15 14 48 17 --- 10 | 69 70 71 91 76 --- 71
R03E | 2161 24 16 24 94 29 21 15 | 151 141 154 149 123 144 140
R04E | 1345 26 13 12 37 33 25 11 | 192 184 181 196 170 175 180
R05E | 1552 13 9 16 40 21 19 8 | 175 147 175 179 176 168 173
R07E | 1528 22 22 36 97 31 14 16 | 209 206 207 234 202 212 207
R08E | 948 17 19 20 75 19 20 12 | 166 158 161 180 162 150 159
R09 | 1329 18 18 17 15 16 13 7 | 43 37 48 32 45 52 42
R11 | 700 12 11 8 12 10 10 4 | 29 27 31 25 28 31 28
R12 | 554 16 21 13 14 12 13 6 | 41 47 38 33 34 29 35
R14 | 970 9 11 19 23 13 12 6 | 48 51 46 31 49 43 43
R15 | 1059 23 13 11 22 10 9 6 | 69 55 51 51 53 58 55
R16 | 589 25 20 12 14 17 9 7 | 59 49 47 45 36 45 44
R17 | 970 18 17 12 23 15 17 7 | 43 35 30 47 34 28 32
R18 | 1433 12 17 14 13 15 23 7 | 31 38 31 37 34 25 29
R19 | 2835 44 73 13 50 31 31 18 | 84 44 54 77 72 52 58
R20 | 5909 50 88 35 98 34 35 24 | 96 39 59 111 74 46 62
R21 | 691 12 24 20 18 16 17 8 | 50 41 60 58 50 45 50
R22 | 2585 16 17 24 15 32 9 9 | 23 37 34 28 39 25 26
R24 | 1918 9 35 10 29 19 13 8 | 55 42 58 63 63 50 54
XR26E |14946 36 --- --- 114 63 --- 47 | 32 --- --- 118 46 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1977 24 32 20 48 22 19 |T 81 74 79 87 76 75 74
WRMS | 1977 19 25 19 27 22 19 |NE 51 41 45 49 47 40 42
MEDI | 1329 18 17 14 27 19 17 |MD 55 47 54 58 50 50 50
Table 3.2345.3 GPS week: 2345 Day: 3 MJD: 60662
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 810 24 38 28 23 23 29 12 | 44 47 46 45 38 42 38
XR02E | 1275 13 17 20 53 18 --- 13 | 50 48 42 72 58 --- 48
R03E | 1472 11 21 22 19 19 13 7 | 150 148 146 156 151 150 149
R04E | 2020 14 18 33 38 33 13 11 | 223 213 202 209 224 213 213
R05E | 958 18 14 12 53 20 12 10 | 206 251 203 189 194 203 198
R07E | 2156 20 24 31 26 36 17 11 | 233 220 225 230 228 235 229
R08E | 1656 9 15 17 15 16 7 5 | 97 93 92 88 98 92 93
R09 | 2816 11 18 11 12 11 8 5 | 20 23 23 18 21 20 17
R11 | 957 18 18 20 38 13 16 9 | 19 26 33 55 32 22 24
R12 | 1156 9 17 16 15 19 9 6 | 39 42 46 32 32 31 34
R14 | 696 11 21 19 13 9 9 6 | 44 63 50 41 52 49 47
R15 | 1259 16 11 10 14 18 17 6 | 61 56 49 42 63 45 51
R16 | 607 19 21 12 14 11 21 7 | 66 54 62 53 58 45 54
R17 | 805 8 22 19 17 14 16 7 | 49 36 57 57 50 39 47
R18 | 1228 10 19 14 18 15 20 7 | 31 44 37 46 37 25 33
R19 | 922 43 93 21 50 42 24 20 | 93 44 81 87 89 71 78
R20 | 2684 30 81 60 68 30 34 22 | 90 49 90 106 96 71 82
R21 | 558 9 23 13 18 27 20 8 | 51 37 52 57 61 38 48
R22 | 3796 16 7 17 15 18 9 6 | 20 20 19 32 26 16 18
R24 | 1559 11 38 27 19 13 20 9 | 55 40 65 64 59 43 53
XR26E |18882 29 --- --- 31 55 --- 28 | 28 --- --- 37 32 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1704 18 35 24 30 22 18 |T 79 77 81 81 80 76 75
WRMS | 1704 15 28 17 19 20 18 |NE 49 41 51 53 52 39 45
MEDI | 1259 14 19 19 19 18 16 |MD 51 47 52 57 58 45 48
Table 3.2345.4 GPS week: 2345 Day: 4 MJD: 60663
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1203 33 36 25 32 20 44 14 | 41 46 49 45 36 40 36
XR02E | 1302 10 12 11 17 11 --- 6 | 78 77 80 80 75 --- 77
R03E | 1512 15 14 13 15 20 15 7 | 88 87 91 91 96 82 88
R04E | 2405 15 11 18 23 16 14 7 | 191 191 199 190 196 187 192
XR05E | 2180 10 --- 24 25 11 20 9 | 219 --- 221 215 216 215 217
R07E | 1863 13 15 15 18 13 17 6 | 179 181 190 176 183 173 180
R08E | 2408 12 20 24 22 10 14 7 | 132 140 137 131 128 131 132
R09 | 3275 15 8 23 11 12 22 7 | 41 43 40 39 33 54 39
R11 | 999 13 18 13 19 10 11 6 | 32 31 40 27 26 26 28
R12 | 1363 11 11 9 10 9 13 4 | 42 39 42 43 39 46 41
R14 | 902 7 11 8 8 13 16 5 | 45 47 53 49 57 40 48
R15 | 693 12 21 10 22 7 13 6 | 60 72 56 44 57 57 56
R16 | 918 18 14 14 13 7 17 6 | 59 58 54 54 57 50 54
R17 | 1029 10 26 11 13 22 24 8 | 44 33 42 42 51 27 40
R18 | 897 11 15 8 14 15 15 5 | 32 38 32 42 38 28 33
R19 | 1955 32 92 17 58 25 37 19 | 83 38 82 94 70 73 74
R20 | 2012 25 108 50 63 34 56 24 | 69 32 77 79 74 50 63
R21 | 932 13 34 18 16 27 27 10 | 46 34 59 56 66 38 51
R22 | 3288 14 12 8 22 15 16 6 | 20 26 25 36 21 22 21
R24 | 1586 14 41 16 26 12 28 10 | 46 34 41 59 47 32 41
XR26E |15238 32 --- --- 42 53 --- 30 | 34 --- --- 48 39 --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1802 17 39 19 27 17 25 |T 75 65 80 78 76 72 75
WRMS | 1802 14 39 18 26 15 25 |NE 47 40 49 51 48 41 45
MEDI | 1512 13 15 14 19 13 17 |MD 46 43 54 54 57 50 51
Table 3.2345.5 GPS week: 2345 Day: 5 MJD: 60664
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1604 32 36 54 29 22 40 16 | 56 46 76 49 48 39 46
XR02E | 909 8 11 13 13 14 --- 6 | 56 55 52 53 54 --- 52
R03E | 1588 10 15 18 14 20 14 7 | 103 99 97 98 110 94 100
R04E | 2277 13 16 30 16 15 15 7 | 170 171 175 162 171 165 168
R05E | 713 12 10 18 13 11 15 6 | 164 122 165 157 161 150 160
R07E | 1218 15 23 20 19 18 15 8 | 184 188 191 181 190 177 184
R08E | 2269 14 11 18 14 18 7 6 | 118 114 121 109 108 108 112
R09 | 1596 16 10 14 12 14 12 6 | 26 31 32 28 27 37 28
R11 | 1604 17 16 27 41 16 15 10 | 24 33 31 62 35 25 30
R12 | 2381 17 14 14 12 14 13 6 | 42 32 30 37 35 37 35
R14 | 644 9 19 24 13 18 10 6 | 43 38 60 42 48 43 44
R15 | 746 19 15 17 15 13 13 7 | 58 47 52 50 49 48 50
R16 | 1039 15 32 16 20 11 10 7 | 58 73 54 44 51 47 51
R17 | 1530 18 23 16 20 16 18 8 | 38 33 37 35 35 28 31
R18 | 640 13 18 17 15 13 16 6 | 28 29 28 32 25 26 25
R19 | 2042 36 99 57 50 22 22 21 | 54 32 96 65 52 53 55
R20 | 1862 32 90 76 58 34 45 24 | 62 34 69 40 60 54 49
R21 | 1174 13 34 23 17 27 25 10 | 36 27 51 46 52 25 37
R22 | 2391 13 15 15 14 14 11 6 | 17 25 29 28 20 19 19
R24 | 910 10 36 25 14 17 15 8 | 36 33 49 44 41 36 38
XR26E |15153 28 --- --- 39 46 --- 27 | 24 --- --- 29 24 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1599 19 37 31 25 18 20 |T 66 63 74 66 66 63 63
WRMS | 1599 16 32 19 20 16 20 |NE 40 35 47 42 40 36 37
MEDI | 1588 15 16 18 15 16 15 |MD 54 34 52 46 49 43 46
Table 3.2345.6 GPS week: 2345 Day: 6 MJD: 60665
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1830 33 36 49 38 28 32 16 | 88 84 92 86 82 78 81
XR02E | 1605 6 9 15 11 12 --- 5 | 72 74 75 76 73 --- 73
R03E | 1710 9 13 16 13 19 17 6 | 155 156 167 160 147 150 155
R04E | 1076 7 12 20 21 11 17 6 | 200 197 209 210 196 196 201
R05E | 1302 10 10 12 15 13 11 5 | 199 165 203 201 197 197 200
R07E | 1456 9 13 16 18 24 14 7 | 202 202 213 210 193 210 205
R08E | 1420 7 12 16 14 19 14 6 | 153 155 159 159 140 153 152
R09 | 1717 8 15 20 9 9 12 5 | 35 43 35 33 35 42 36
R11 | 1434 10 13 12 10 11 16 5 | 40 44 46 54 46 42 44
R12 | 2247 22 10 11 10 12 11 6 | 69 59 57 59 61 60 61
R14 | 1344 7 7 12 20 11 12 5 | 65 62 62 65 63 58 62
R15 | 964 23 17 10 16 8 16 7 | 80 64 71 64 72 69 70
R16 | 819 20 14 8 17 17 17 7 | 77 70 64 63 68 54 65
R17 | 879 12 19 14 13 18 19 7 | 62 52 54 64 69 45 57
R18 | 612 11 23 26 16 23 26 9 | 41 53 49 52 50 33 42
R19 | 2127 19 77 23 48 30 32 17 | 107 37 99 110 94 87 89
R20 | 3842 34 90 48 42 37 40 21 | 101 41 99 109 104 66 84
R21 | 931 10 32 19 20 14 12 8 | 70 50 78 81 82 60 70
R22 | 1911 12 12 11 16 16 7 5 | 23 27 31 36 31 26 27
R24 | 728 9 36 16 25 18 21 9 | 71 42 74 80 65 52 64
XR26E |13944 28 --- --- 34 56 --- 29 | 40 --- --- 50 35 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1658 17 33 22 23 19 20 |T 92 83 96 96 90 88 89
WRMS | 1658 15 24 16 18 17 20 |NE 64 49 63 66 64 53 59
MEDI | 1434 10 13 16 16 17 16 |MD 72 59 74 76 72 60 70
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