[IGSREPORT-29759] Wk 2301 IGLOS Final Orbits
acc
acc at igs.org
Mon Mar 4 01:57:35 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2301 (Feb 11, 2024 - Feb 17, 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 2.2301.
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:
igl2301[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2301 in the SP3 format.
igl23017.sum Combination Report for GPS Week 2301.
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).
The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 | -0.5 ns
1 | -5.7 ns
2 | -3.9 ns
3 | -4.4 ns
4 | -6.2 ns
5 | -5.1 ns
6 | -1.7 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
----+--------+---------------
0 | ALL | R26
1 | ALL | R26
2 | ALL | R26
3 | ALL | R26
4 | ALL | R26
5 | ALL | R26
6 | ALL | R26
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 1.2301, 1a.2301).
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 2.2301.0-6)
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 3.2301.0-6).
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 2301 summary. (Feb 11, 2024 - Feb 17, 2024)
Table 1.2301.a GPS week : 2301 MJD: 60351.0-60357.0
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 1 -2 -12 84 .11 22 16 | 11148 -608 3168 6925
| 0 1 1 16 8 31 .04 | 1824 1947
esa n/a| 0 1 0 -29 -14 -22 -.17 29 22 | -4967 -551 3163 7291
| 0 1 2 13 10 23 .04 | 3422 2028
gfz n/a| 0 0 4 33 21 -11 -.03 26 17 | 0 -615 3169 6881
| 1 1 1 11 12 28 .04 | 0 1781
grg n/a| 1 -3 -4 -5 -9 38 .33 25 18 | -3690 -699 3168 6325
| 1 1 1 11 15 80 .04 | 1647 1932
iac n/a| -1 0 -1 19 37 -40 -.25 24 20 | -1856 -368 3163 7235
| 1 0 4 24 17 42 .07 | 2086 598
jgx n/a| -1 0 -3 4 22 -138 -.25 29 29 | 12364 -164 3146 6953
| 1 1 1 20 12 89 .04 | 1981 1917
Table 1.2301.b GPS week : 2301 MJD: 60351.0-60357.0
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 19 19 17 18 18 20 |
R02 | 9 6 7 7 8 8 10 |
R03 | 9 9 9 10 11 9 9 |
R04 | 8 10 9 9 11 12 10 |
R05 | 9 8 9 8 8 9 10 |
R07 | 9 10 8 9 10 8 8 |
R08 | 9 8 7 9 10 11 7 |
R09 | 7 6 7 7 7 8 8 |
R11 | 8 10 7 9 9 7 6 |
R12 | 8 9 8 8 10 11 9 |
R13 | 20 21 15 19 17 20 18 |
R14 | 6 6 7 10 8 7 7 |
R15 | 11 9 8 8 9 11 9 |
R16 | 9 12 9 9 10 9 10 |
R17 | 9 13 8 9 10 15 12 |
R18 | 8 8 7 8 9 9 9 |
R19 | 24 22 20 18 20 19 16 |
R20 | 31 26 26 36 44 41 32 |
R21 | 7 7 10 9 8 8 8 |
R22 | 7 8 8 8 8 8 7 |
R24 | 11 12 9 9 8 10 11 |
Table 1.2301.c GPS week : 2301 MJD: 60351.0-60357.0
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 2301 0 | 47 105 151 -500 180 4989 77.8 1348 1348 | -525 0
brd 2301 1 | 38 77 221 -766 -1176 1715 78.8 1662 1662 | -5697 0
brd 2301 2 | -23 -37 183 1123 759 102 78.6 1867 1867 | -3941 0
brd 2301 3 | -62 101 179 -597 1302 765 79.7 1657 1657 | -4407 0
brd 2301 4 | 12 39 132 1432 2684 1024 79.5 1320 1320 | -6233 0
brd 2301 5 | 36 -69 203 2045 -598 -2358 81.0 1234 1234 | -5113 0
brd 2301 6 | 47 119 218 -967 -1570 -2875 81.9 1432 1432 | -1652 0
-------------+------------------------------------------------------------+----------------
brd 2301 mean| 13 47 184 252 225 480 79.6 1502 1502 | -3938 0
brd 2301 sdev| 42 74 33 1236 1492 2635 1.4 229 229 | 2114 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 2.2301.0 GPS week: 2301 Day: 0 MJD: 60351
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 23 -15 117 .16 25 18 | 11707 3143 2828 7891
esa n/a| 1 0 0 -38 -18 9 -.17 30 21 | -7159 3498 2808 7964
gfz n/a| 0 1 5 27 13 -12 -.10 24 14 | 0 2972 2806 7857
grg n/a| 0 0 -4 12 1 -114 .33 22 20 | -2397 3241 2829 7175
iac n/a| 0 0 2 49 26 -42 -.24 22 20 | 1507 192 2806 8235
jgx n/a| 0 0 -5 -20 33 30 -.20 29 28 | 13345 3406 2844 8019
Table 2.2301.1 GPS week: 2301 Day: 1 MJD: 60352
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 1 -21 68 .12 20 15 | 10696 950 3492 6745
esa n/a| 0 3 0 -44 -12 -7 -.18 30 21 | -9225 680 3490 8330
gfz n/a| -1 0 5 50 22 -58 -.02 24 20 | 0 466 3510 6751
grg n/a| 3 -2 -6 -16 16 60 .32 25 20 | -5870 328 3480 6114
iac n/a| -3 2 0 17 25 -73 -.28 21 18 | -2831 -1137 3505 6955
jgx n/a| -3 2 -4 -9 2 -68 -.24 27 25 | 11378 806 3564 6902
Table 2.2301.2 GPS week: 2301 Day: 2 MJD: 60353
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 -13 -18 61 .14 21 14 | 13653 -1342 3200 6730
esa n/a| 0 0 -2 -36 -5 -44 -.13 28 29 | -7869 -1252 3191 6533
gfz n/a| 1 2 5 48 4 -7 -.06 20 17 | 0 -947 3185 6690
grg n/a| 1 -5 -1 3 -8 103 .31 23 19 | -3406 -1126 3192 5972
iac n/a| -1 0 0 -17 46 -32 -.19 24 20 | -1843 -690 3178 7039
jgx n/a| 0 -1 -3 -15 27 -167 -.31 24 24 | 14375 -916 3179 6832
Table 2.2301.3 GPS week: 2301 Day: 3 MJD: 60354
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 -28 -4 47 .05 22 16 | 13089 -1727 3124 6975
esa n/a| 0 0 0 -27 -37 -60 -.13 27 25 | -734 -1912 3127 7152
gfz n/a| 0 0 3 35 28 -5 -.04 28 17 | 0 -1596 3147 6918
grg n/a| 3 -3 -5 -13 -16 132 .36 23 18 | -3435 -2121 3131 6353
iac n/a| -1 0 0 0 67 -97 -.24 24 22 | -1739 -1019 3121 7418
jgx n/a| -1 0 0 15 25 -147 -.22 29 30 | 15067 -1141 3169 7159
Table 2.2301.4 GPS week: 2301 Day: 4 MJD: 60355
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 -7 -2 135 .06 24 21 | 10353 -2074 2904 6705
esa n/a| 0 2 4 -6 -9 -27 -.15 28 20 | -4087 -2353 2893 7510
gfz n/a| -1 0 2 26 11 -20 .01 34 18 | 0 -1828 2907 6561
grg n/a| 0 -1 -4 -19 -27 59 .31 26 17 | -5226 -2232 2918 6142
iac n/a| -2 0 -1 9 48 10 -.21 24 19 | -4308 -271 2921 7064
jgx n/a| 0 -1 -2 25 38 -212 -.29 32 33 | 12145 -2220 2926 6843
Table 2.2301.5 GPS week: 2301 Day: 5 MJD: 60356
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 8 -3 87 .12 23 18 | 8341 -2012 3351 6741
esa n/a| 0 0 -1 -37 -10 -17 -.23 30 18 | -475 -970 3355 6717
gfz n/a| -1 1 5 29 34 38 -.04 27 17 | 0 -1982 3353 6742
grg n/a| 1 -3 -2 -4 -6 24 .26 27 16 | -4424 -1585 3351 6216
iac n/a| 0 0 -3 41 23 -66 -.21 24 17 | -3870 422 3349 7004
jgx n/a| 0 0 -3 33 9 -211 -.24 35 36 | 9833 -1623 3360 6784
Table 2.2301.6 GPS week: 2301 Day: 6 MJD: 60357
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 0 1 -20 73 .10 17 14 | 10201 -1195 3277 6690
esa n/a| 0 2 0 -14 -8 -11 -.22 28 19 | -5226 -1553 3283 6833
gfz n/a| -1 0 5 18 34 -12 .02 27 17 | 0 -1390 3280 6652
grg n/a| 2 -5 -3 -2 -26 3 .39 27 19 | -1078 -1398 3275 6307
iac n/a| -2 1 -10 35 22 16 -.39 29 22 | 87 -79 3265 6930
jgx n/a| -1 -1 -2 1 23 -193 -.26 29 26 | 10409 537 2984 6137
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 3.2301.0 GPS week: 2301 Day: 0 MJD: 60351
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 727 46 66 19 27 21 22 19 | 138 77 117 115 101 88 106
R02 | 2860 11 18 14 18 18 25 8 | 79 91 77 84 77 68 79
R03 | 1899 10 17 23 10 13 26 9 | 103 94 109 103 97 83 98
R04 | 1392 18 17 12 15 22 20 8 | 100 93 107 102 96 90 98
R05 | 1107 18 9 16 14 12 24 8 | 93 87 89 89 87 84 87
R07 | 1254 20 20 11 15 37 21 8 | 93 85 90 94 106 77 87
R08 | 773 18 17 12 18 13 21 8 | 89 88 85 92 91 76 85
R09 | 1129 14 13 11 11 25 13 6 | 40 38 37 38 40 33 38
R11 | 686 22 12 12 12 9 16 7 | 49 50 52 56 51 59 51
R12 | 1368 21 17 10 14 12 11 7 | 28 42 39 30 27 29 32
R13 | 558 28 21 25 52 11 58 19 | 48 44 45 34 38 26 36
R14 | 1275 7 22 8 9 10 12 6 | 28 46 30 31 27 26 31
R15 | 895 13 17 26 10 26 38 11 | 43 56 67 53 41 32 49
R16 | 615 16 25 14 16 12 21 9 | 56 67 61 43 45 41 53
XR17 | 2685 9 19 12 19 21 --- 9 | 102 90 98 104 90 --- 100
R18E | 782 10 17 19 20 22 12 8 | 78 81 83 85 80 72 79
R19E | 1775 40 49 57 37 31 45 23 | 99 90 115 95 83 92 92
R20E | 1467 67 75 60 34 51 65 30 | 101 98 120 87 96 86 90
R21E | 974 9 18 14 15 20 15 7 | 34 34 37 41 38 36 34
R22E | 895 18 11 12 16 18 10 7 | 33 41 38 39 39 44 37
R24E | 2070 13 28 15 28 14 18 10 | 126 126 122 127 123 132 125
------+-----------------------------------------+-------------------------------------
RMS | 1348 25 30 24 22 22 29 |T 74 72 77 73 70 63 70
WRMS | 1348 18 21 14 20 20 28 |NE 72 69 73 71 67 58 68
MEDI | 1129 18 18 14 16 18 21 |MD 79 81 83 85 80 68 79
Table 3.2301.1 GPS week: 2301 Day: 1 MJD: 60352
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 595 36 68 26 20 17 22 19 | 94 44 93 75 79 65 74
R02 | 2645 9 14 9 13 19 16 6 | 59 63 61 62 55 52 59
R03 | 923 11 18 15 18 16 22 8 | 73 65 66 80 59 58 68
R04 | 1671 10 23 24 16 20 26 10 | 67 72 83 70 66 58 69
R05 | 1975 9 19 15 18 13 13 7 | 58 65 61 58 58 59 58
R07 | 1115 8 22 24 22 20 23 10 | 63 56 84 76 77 52 65
R08 | 917 9 16 13 17 22 24 8 | 58 60 67 71 72 45 59
R09 | 1404 9 14 11 16 10 11 6 | 33 33 34 32 29 36 33
R11 | 939 16 10 25 22 11 18 9 | 44 54 52 65 51 58 52
R12 | 747 13 22 24 12 13 13 8 | 20 24 27 18 21 16 17
R13 | 732 24 23 27 65 14 56 21 | 39 38 33 34 29 25 31
R14 | 1800 7 10 9 11 10 19 5 | 22 25 24 27 21 19 21
R15 | 885 18 26 12 13 12 19 9 | 25 32 30 30 24 20 24
R16 | 1291 16 27 21 20 18 33 11 | 38 59 51 35 30 35 40
XR17 | 1703 12 27 17 33 28 --- 13 | 105 105 112 103 97 --- 106
R18E | 430 10 18 17 20 19 10 7 | 63 70 80 64 60 65 67
R19E | 1484 44 39 35 41 44 53 21 | 75 73 68 71 60 78 65
R20E | 4595 43 72 56 34 50 44 25 | 87 102 108 98 82 108 93
R21E | 733 9 15 20 14 15 12 7 | 28 24 34 39 27 24 28
R22E | 1254 17 9 16 18 18 13 7 | 27 30 31 36 33 35 29
R24E | 1730 18 27 23 29 18 15 11 | 83 88 88 96 84 84 85
------+-----------------------------------------+-------------------------------------
RMS | 1662 20 30 24 25 21 27 |T 55 56 61 59 53 49 54
WRMS | 1662 15 21 20 20 18 25 |NE 53 53 58 55 51 42 51
MEDI | 1254 12 22 20 18 18 19 |MD 58 59 61 64 58 52 59
Table 3.2301.2 GPS week: 2301 Day: 2 MJD: 60353
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 995 32 63 35 18 17 35 19 | 102 47 111 90 80 63 84
R02 | 2907 9 14 17 14 19 14 7 | 57 68 72 72 59 57 64
R03 | 597 8 19 9 22 15 23 8 | 82 74 85 96 74 70 81
R04 | 1835 10 23 13 21 15 20 9 | 86 78 84 95 80 73 82
R05 | 2222 6 17 23 15 13 25 9 | 82 85 96 87 75 73 84
R07 | 901 16 13 14 13 17 19 7 | 82 67 70 75 66 64 71
R08 | 1083 13 10 15 10 18 17 6 | 72 64 64 70 61 62 66
R09 | 1149 11 11 12 17 15 14 6 | 32 33 29 34 36 24 30
R11 | 942 13 13 12 11 20 17 6 | 35 44 45 34 44 36 37
R12 | 642 16 12 19 15 12 18 8 | 29 29 29 24 24 29 26
R13 | 846 16 21 15 47 16 39 14 | 53 39 46 50 43 33 43
R14 | 902 9 10 18 15 13 14 6 | 31 36 41 23 35 24 30
R15 | 1185 15 12 13 15 9 23 8 | 30 26 28 32 25 22 25
R16 | 2070 14 24 13 21 14 12 8 | 37 48 37 25 26 31 33
XR17 | 2368 8 16 9 21 14 --- 8 | 45 51 49 40 44 --- 44
R18E | 704 6 18 13 14 16 12 6 | 75 72 80 76 75 77 75
R19E | 1536 45 42 29 42 54 33 19 | 44 47 48 35 38 41 34
R20E | 5639 53 70 44 34 69 58 26 | 60 73 99 76 69 63 66
R21E | 728 12 23 12 25 16 22 9 | 28 28 24 36 29 27 24
R22E | 667 19 15 14 19 16 12 8 | 18 26 21 37 25 21 21
R24E | 2040 13 22 20 22 15 13 9 | 82 80 68 88 78 78 77
------+-----------------------------------------+-------------------------------------
RMS | 1867 21 28 20 23 24 24 |T 55 53 58 56 51 48 52
WRMS | 1867 14 29 17 19 20 24 |NE 57 52 59 56 51 47 53
MEDI | 1083 13 17 14 18 16 18 |MD 53 48 49 50 44 41 44
Table 3.2301.3 GPS week: 2301 Day: 3 MJD: 60354
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1397 45 46 22 18 14 20 16 | 116 49 87 90 81 77 83
R02 | 2536 10 14 16 9 20 15 6 | 60 72 71 65 58 60 65
R03 | 833 16 23 21 12 15 19 9 | 83 59 84 80 66 66 74
R04 | 938 13 21 21 19 17 18 9 | 79 64 86 93 90 77 80
R05 | 1215 13 16 24 11 24 14 8 | 77 69 92 85 95 76 79
R07 | 749 13 19 12 19 17 19 8 | 85 76 73 85 66 71 77
R08 | 1105 15 20 14 21 21 20 9 | 78 82 74 76 71 70 75
R09 | 815 8 9 12 17 13 21 7 | 23 28 29 27 22 23 22
R11 | 878 11 10 19 18 19 28 9 | 23 37 39 24 34 41 28
R12 | 954 16 10 16 19 11 17 8 | 22 16 16 19 17 17 13
R13 | 799 34 17 26 50 16 52 19 | 63 35 48 43 36 33 43
R14 | 678 8 21 22 23 11 15 9 | 31 49 48 21 36 32 34
R15 | 1596 19 14 17 13 12 16 8 | 35 22 28 24 26 24 24
R16 | 2403 18 15 15 17 13 22 9 | 35 36 37 30 31 23 29
XR17 | 2228 9 17 11 18 21 --- 8 | 74 62 69 75 80 --- 71
R18E | 655 12 15 19 15 27 17 8 | 79 75 85 91 61 82 81
R19E | 1605 39 33 34 37 44 27 17 | 40 60 61 39 28 46 40
R20E | 4973 39 80 91 47 59 89 35 | 104 127 133 101 108 110 105
R21E | 625 12 17 21 15 20 25 9 | 26 28 39 32 36 36 27
R22E | 657 18 15 13 21 25 14 8 | 21 23 24 43 30 26 25
R24E | 1167 20 21 16 15 22 12 8 | 54 74 71 54 56 63 61
------+-----------------------------------------+-------------------------------------
RMS | 1657 22 27 28 23 24 29 |T 57 54 61 57 53 52 54
WRMS | 1657 16 25 17 18 22 30 |NE 58 50 58 55 53 49 53
MEDI | 954 15 17 19 18 19 19 |MD 60 59 69 54 56 46 61
Table 3.2301.4 GPS week: 2301 Day: 4 MJD: 60355
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 978 52 35 26 19 21 30 17 | 105 47 53 73 60 56 65
R02 | 1431 10 17 13 10 11 25 8 | 62 68 49 56 56 50 56
R03 | 1162 17 24 31 11 33 26 11 | 87 77 102 80 110 74 82
R04 | 648 18 27 22 17 31 20 10 | 77 59 78 85 99 74 73
R05 | 931 12 14 14 15 11 19 7 | 80 70 66 82 77 70 73
R07 | 785 20 13 18 20 19 28 10 | 77 67 62 75 72 47 65
R08 | 1118 18 22 17 15 16 22 9 | 68 84 73 68 76 65 70
R09 | 1236 17 12 9 14 11 15 7 | 33 34 32 37 32 33 33
R11 | 754 18 11 26 9 12 18 8 | 42 56 64 56 45 49 52
R12 | 852 22 12 20 21 14 17 9 | 31 20 26 20 24 23 19
R13 | 1175 29 9 29 40 16 54 17 | 43 31 35 28 34 28 29
R14 | 741 14 8 14 16 14 23 7 | 35 23 35 25 35 26 26
R15 | 923 21 11 17 16 15 24 9 | 40 25 27 34 36 25 29
R16 | 2743 25 18 19 9 14 21 9 | 43 41 33 29 29 34 33
XR17 | 1457 12 17 16 21 13 --- 10 | 52 54 46 63 42 --- 50
R18E | 1069 10 17 23 22 22 16 9 | 56 57 61 46 52 54 52
R19E | 979 29 37 53 39 37 34 19 | 57 66 96 62 40 53 59
R20E | 3180 50 96 114 76 71 95 43 | 97 104 165 106 100 98 95
R21E | 519 10 16 21 17 10 17 8 | 23 27 36 30 27 30 26
R22E | 932 15 10 17 22 11 17 8 | 30 32 36 40 30 40 31
R24E | 930 13 16 19 17 16 15 8 | 83 92 88 87 91 89 86
------+-----------------------------------------+-------------------------------------
RMS | 1320 24 28 34 26 24 32 |T 58 54 60 56 55 50 52
WRMS | 1320 21 20 18 17 19 33 |NE 58 50 52 54 55 46 50
MEDI | 978 18 16 19 17 15 21 |MD 56 56 53 56 45 49 52
Table 3.2301.5 GPS week: 2301 Day: 5 MJD: 60356
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1259 50 34 22 22 27 39 18 | 92 59 61 71 75 52 66
R02 | 551 11 21 14 13 12 20 8 | 60 71 55 60 56 50 58
R03 | 1243 16 20 14 17 24 23 9 | 81 69 73 81 86 66 74
R04 | 709 17 24 31 14 19 29 11 | 79 76 98 89 91 75 82
R05 | 712 10 19 24 10 13 19 8 | 71 56 80 61 58 57 65
R07 | 856 8 17 13 19 22 20 8 | 69 66 79 85 63 67 73
R08 | 1054 21 19 13 23 14 34 11 | 67 74 72 88 72 56 72
R09 | 1242 17 14 17 6 20 16 7 | 32 38 40 41 38 32 35
R11 | 981 12 15 16 9 16 18 7 | 24 28 33 25 21 33 26
R12 | 815 18 16 23 27 14 17 10 | 31 44 44 34 29 31 33
R13 | 2256 26 16 52 47 17 51 20 | 40 33 57 22 38 28 28
R14 | 599 9 17 19 6 13 15 7 | 26 37 24 25 27 29 26
R15 | 878 17 11 31 11 20 31 10 | 38 32 36 31 41 24 30
R16 | 1257 17 15 20 8 12 22 8 | 43 49 60 47 44 42 46
XR17 |11472 14 --- 21 26 32 --- 15 | 65 --- 70 78 63 --- 67
R18E | 1064 11 22 18 15 14 17 8 | 55 60 59 57 58 53 55
R19E | 1008 32 34 43 36 46 50 19 | 64 63 75 69 46 69 61
R20E | 2353 54 105 60 84 58 104 41 | 174 198 205 206 170 175 184
R21E | 516 11 19 14 12 18 24 8 | 22 25 26 34 28 34 24
R22E | 1918 18 13 14 14 18 14 7 | 31 35 39 41 41 39 34
R24E | 1253 16 18 17 28 16 20 10 | 81 84 88 106 90 91 89
------+-----------------------------------------+-------------------------------------
RMS | 1234 23 30 27 27 24 35 |T 59 59 65 64 58 55 58
WRMS | 1234 18 18 17 16 17 36 |NE 54 52 58 55 53 45 52
MEDI | 1054 17 18 19 15 18 20 |MD 60 56 60 60 56 50 58
Table 3.2301.6 GPS week: 2301 Day: 6 MJD: 60357
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1172 35 48 23 44 39 47 20 | 133 84 125 143 102 89 113
R02 | 606 11 24 15 22 19 29 10 | 83 101 85 88 86 69 84
R03 | 827 13 13 19 15 20 27 8 | 110 100 112 109 107 87 104
R04 | 1109 13 26 27 13 21 21 10 | 107 99 127 113 112 108 109
R05 | 952 15 18 26 11 22 21 9 | 94 84 104 92 101 85 91
R07 | 796 12 11 19 18 30 19 7 | 101 89 86 104 83 85 93
R08 | 817 14 17 10 13 17 14 7 | 92 93 94 99 90 82 91
XR09 | 1704 11 10 16 14 33 --- 7 | 40 39 45 45 57 --- 41
R11 | 2149 11 10 11 15 18 14 6 | 34 40 40 40 39 35 36
R12 | 658 10 20 12 19 17 23 8 | 39 53 47 36 42 38 39
R13 | 1981 12 9 42 62 38 40 17 | 57 55 76 45 64 41 51
R14 | 1257 9 10 17 14 22 17 6 | 39 44 34 30 36 30 34
R15 | 583 19 15 15 11 17 20 8 | 47 50 47 40 49 32 41
R16 | 1145 13 13 27 22 15 24 10 | 57 58 67 62 59 45 56
XR17 | 4236 10 16 24 33 17 --- 12 | 81 86 80 78 75 --- 77
R18E | 1428 8 21 19 23 15 13 8 | 65 68 68 71 69 63 66
R19E | 1810 21 29 45 27 52 39 16 | 96 96 104 78 75 89 89
R20E | 2488 42 86 69 57 68 64 31 | 146 195 158 133 144 158 151
R21E | 584 10 18 12 20 21 20 8 | 35 38 38 43 38 39 35
R22E | 2678 14 12 13 16 21 16 7 | 49 50 48 59 56 56 50
R24E | 1359 10 22 27 24 17 24 10 | 134 135 132 145 137 146 137
------+-----------------------------------------+-------------------------------------
RMS | 1432 17 28 27 27 29 29 |T 78 78 81 78 77 72 75
WRMS | 1432 14 19 17 19 22 26 |NE 74 71 77 74 73 63 70
MEDI | 1172 12 17 19 19 21 21 |MD 81 84 80 78 75 69 77
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