[IGSREPORT-29466] Wk 2274 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 25 06:23:04 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2274 (Aug 06, 2023 - Aug 12, 2023)
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 2.2274.
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:
igl2274[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2274 in the SP3 format.
igl22747.sum Combination Report for GPS Week 2274.
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 | 0.7 ns
1 | 0.7 ns
2 | -0.2 ns
3 | -16.4 ns
4 | -1.2 ns
5 | -0.8 ns
6 | -11.6 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 1.2274, 1a.2274).
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 2.2274.0-6)
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 3.2274.0-6).
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 2274 summary. (Aug 06, 2023 - Aug 12, 2023)
Table 1.2274.a GPS week : 2274 MJD: 60162.0-60168.0
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| -2 0 -2 -3 -31 27 .04 20 16 | 30171 -1045 2934 8791
| 0 0 1 17 10 20 .05 | 7290 1562
esa n/a| -1 -1 3 -2 3 11 -.28 34 21 | -5834 -183 2964 7101
| 0 1 1 13 3 22 .05 | 8298 1781
gfz n/a| 0 0 -2 25 9 -4 -.23 23 15 | 0 -1013 2952 8442
| 0 0 1 10 16 15 .04 | 0 1466
grg n/a| 4 0 1 -17 22 -38 .31 23 19 | -3775 -990 2947 7836
| 1 1 1 13 13 33 .03 | 6396 1372
jgx n/a| -1 0 7 21 2 -65 -.22 32 32 | 30567 -1041 2965 8405
| 1 1 2 19 16 56 .05 | 7077 1566
Table 1.2274.b GPS week : 2274 MJD: 60162.0-60168.0
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 26 27 24 29 27 |
R02 | 9 7 6 8 6 11 9 |
R03 | 10 9 8 9 7 9 10 |
R04 | 10 8 10 7 7 9 10 |
R05 | 9 8 8 9 10 9 10 |
R07 | 9 9 10 10 10 10 8 |
R08 | 7 8 11 9 12 11 11 |
R09 | 8 10 10 11 9 10 7 |
R11 | 6 8 7 6 7 8 8 |
R12 | 8 8 6 6 6 8 7 |
R13 | 17 19 20 22 20 16 21 |
R14 | 9 8 7 7 4 7 6 |
R15 | 8 7 9 11 8 10 8 |
R16 | 11 10 9 12 11 14 10 |
R17 | 8 9 11 11 14 9 10 |
R18 | 10 10 9 11 9 11 10 |
R19 | 25 26 22 19 22 24 33 |
R20 | 33 40 36 35 35 40 42 |
R21 | 7 10 9 10 9 12 10 |
R22 | 12 10 7 12 11 10 13 |
R24 | 10 9 9 9 9 10 9 |
R25 | 13 0 12 15 14 18 13 |
Table 1.2274.c GPS week : 2274 MJD: 60162.0-60168.0
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 2274 0 | -31 -61 213 973 -453 1698 79.9 1476 1476 | 699 0
brd 2274 1 | 30 -24 190 -192 -458 3131 81.5 1718 1718 | 728 0
brd 2274 2 | 16 100 294 -3376 -761 6639 82.3 2003 2003 | -242 0
brd 2274 3 | 18 -30 311 -942 7267 12880 83.9 1968 1968 | -16359 0
brd 2274 4 | 35 33 185 -100 3992 783 80.4 1600 1600 | -1242 0
brd 2274 5 | 28 92 112 -123 1462 4807 80.9 1676 1676 | -806 0
brd 2274 6 | -40 68 45 -639 1458 8772 78.2 1928 1928 | -11623 0
-------------+------------------------------------------------------------+----------------
brd 2274 mean| 8 25 193 -628 1786 5530 81.0 1767 1767 | -4120 0
brd 2274 sdev| 31 64 93 1350 2934 4267 1.8 202 202 | 6917 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 2.2274.0 GPS week: 2274 Day: 0 MJD: 60162
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 -3 33 -36 36 .06 19 16 | 34781 822 3393 8930
esa n/a| -2 -1 3 -15 4 17 -.28 33 23 | -8651 2232 3570 8775
gfz n/a| 0 1 -1 13 3 -20 -.25 20 15 | 0 799 3444 8814
grg n/a| 4 0 0 -30 11 -16 .27 20 18 | 231 730 3446 8379
jgx n/a| 0 0 8 39 -5 -90 -.16 34 34 | 33909 1324 3401 8849
Table 2.2274.1 GPS week: 2274 Day: 1 MJD: 60163
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 -4 -12 -31 18 .09 16 15 | 36448 977 2966 8867
esa n/a| -1 -3 1 14 7 23 -.28 39 22 | 4001 1273 3018 8015
gfz n/a| 0 0 0 34 -17 -8 -.28 22 13 | 0 654 3000 8580
grg n/a| 3 0 0 -20 49 -3 .31 25 20 | 103 674 3011 7999
jgx n/a| -1 1 6 42 6 -117 -.21 31 31 | 36686 715 3066 8720
Table 2.2274.2 GPS week: 2274 Day: 2 MJD: 60164
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 -1 -11 28 .04 19 15 | 35353 -231 3050 9038
esa n/a| -1 -1 2 -14 0 -23 -.26 33 17 | 1928 1051 3044 6748
gfz n/a| 0 1 -3 23 9 -24 -.22 22 12 | 0 -182 3097 8926
grg n/a| 5 0 3 -21 14 -15 .37 24 19 | -345 -282 3092 8306
jgx n/a| 0 0 8 14 26 -117 -.24 37 37 | 36492 -748 3115 9016
Table 2.2274.3 GPS week: 2274 Day: 3 MJD: 60165
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 -3 -2 -27 52 .11 22 18 | 18257 -2930 2960 8814
esa n/a| -2 -1 2 -9 2 5 -.34 32 20 | -20640 -2200 2970 7968
gfz n/a| 0 0 -1 41 15 -3 -.26 23 19 | 0 -2286 2945 8523
grg n/a| 2 0 1 -29 21 -65 .33 22 18 | -15157 -2644 2950 7676
jgx n/a| -2 1 5 -14 -7 -88 -.24 33 33 | 19138 -2665 2967 8247
Table 2.2274.4 GPS week: 2274 Day: 4 MJD: 60166
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 -18 -45 -10 -.00 20 17 | 32932 -2283 2728 8392
esa n/a| 0 0 1 -6 -3 43 -.36 32 22 | -2652 -1649 2733 6675
gfz n/a| 0 0 0 28 20 13 -.20 24 14 | 0 -2592 2722 7892
grg n/a| 2 -2 0 -5 18 -56 .31 20 16 | -331 -1879 2702 7478
jgx n/a| 0 0 3 14 -23 -62 -.32 32 32 | 33007 -2163 2784 7967
Table 2.2274.5 GPS week: 2274 Day: 5 MJD: 60167
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 -15 -38 27 -.01 22 17 | 32101 -1640 2639 9175
esa n/a| -2 -1 4 18 5 22 -.26 32 22 | -4778 11 2617 5986
gfz n/a| 0 0 -5 17 34 17 -.18 25 15 | 0 -1048 2663 8356
grg n/a| 3 -3 4 -20 13 -93 .32 26 20 | -196 -1348 2667 7683
jgx n/a| -2 2 11 28 19 -17 -.20 31 31 | 32835 -1294 2660 8293
Table 2.2274.6 GPS week: 2274 Day: 6 MJD: 60168
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 -9 -29 39 .01 21 16 | 21331 -2030 2807 8323
esa n/a| -1 0 6 -2 5 -8 -.19 37 23 | -10051 -2003 2801 5546
gfz n/a| -1 0 -4 15 0 -6 -.22 27 18 | 0 -2437 2797 8006
grg n/a| 5 0 0 7 25 -18 .28 27 20 | -10731 -2181 2767 7331
jgx n/a| -2 0 9 23 1 34 -.17 29 29 | 21902 -2458 2768 7748
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 3.2274.0 GPS week: 2274 Day: 0 MJD: 60162
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1748 31 60 27 14 60 19 | 93 38 85 60 45 67
R02 | 588 11 11 19 17 24 9 | 88 85 78 92 79 85
R03 | 1383 16 18 16 19 22 10 | 69 50 63 57 45 59
R04 | 997 17 12 15 20 24 9 | 66 54 54 54 41 55
R05 | 1431 15 17 10 18 19 9 | 67 52 51 62 52 59
R07 | 892 9 22 14 12 34 8 | 77 64 76 71 57 72
R08 | 1900 11 11 11 13 19 6 | 67 58 66 58 47 61
R09 | 2739 16 5 16 10 14 7 | 29 28 22 30 22 26
R11 | 1163 12 15 7 7 10 6 | 31 38 35 33 32 33
R12 | 821 13 18 10 10 14 7 | 27 37 36 32 32 31
R13 | 976 22 34 26 32 49 16 | 47 45 45 52 35 45
R14 | 906 12 7 20 14 20 8 | 25 24 29 28 33 24
R15 | 1799 14 14 15 9 14 7 | 27 42 45 32 41 35
R16 | 974 20 20 18 17 14 10 | 38 62 58 39 43 46
R17 | 799 14 11 11 15 --- 7 | 190 189 187 181 --- 186
R18 | 820 14 20 13 19 21 9 | 129 144 134 129 131 132
R19 | 735 31 65 44 33 58 25 | 150 124 162 127 123 140
R20 | 1313 38 98 46 41 85 32 | 121 91 141 113 99 110
R21 | 1232 11 11 11 14 27 7 | 104 100 104 96 87 100
R22 | 3301 20 23 13 24 13 11 | 30 37 45 46 35 36
R24 | 1230 15 20 15 19 21 10 | 45 50 47 45 38 43
XR25 |13891 10 15 --- --- --- 12 | 40 53 --- --- --- 45
------+------------------------------------+--------------------------------
RMS | 1476 19 33 20 20 34 |T 70 66 74 68 55 67
WRMS | 1476 16 23 15 18 34 |NE 70 66 74 68 55 67
MEDI | 1163 14 17 15 17 21 |MD 66 52 58 57 43 55
Table 3.2274.1 GPS week: 2274 Day: 1 MJD: 60163
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1352 28 68 29 20 51 21 | 65 29 59 50 29 51
R02 | 1169 11 12 9 15 26 7 | 59 56 49 56 54 54
R03 | 2294 13 14 13 23 22 9 | 51 45 45 41 39 44
R04 | 1189 12 11 9 21 23 8 | 49 47 43 44 44 44
R05 | 3095 9 14 9 20 31 7 | 47 42 34 42 38 41
R07 | 1448 13 23 15 15 17 9 | 48 47 47 54 49 47
R08 | 711 11 18 11 12 23 7 | 47 42 45 52 37 46
R09 | 2279 17 19 14 18 17 10 | 27 28 21 22 21 21
R11 | 1809 13 18 13 8 15 7 | 18 30 24 23 21 21
R12 | 584 14 11 15 11 12 7 | 18 27 34 25 21 23
R13 | 1432 18 40 23 51 46 19 | 20 38 27 42 27 24
R14 | 792 13 17 14 10 14 7 | 18 17 20 16 16 14
R15 | 954 7 9 13 14 15 6 | 15 25 21 17 26 17
R16 | 733 17 29 9 11 17 9 | 19 58 35 28 39 30
R17 | 987 14 17 9 20 --- 8 | 182 177 176 177 --- 178
R18 | 1095 7 25 17 18 14 9 | 129 131 116 131 129 125
R19 | 760 31 71 42 40 43 25 | 151 136 150 137 138 143
R20 | 1995 27 123 67 60 76 40 | 89 89 101 115 104 91
R21 | 1479 11 22 20 19 40 10 | 74 75 79 72 68 74
R22 | 3799 13 13 12 24 20 9 | 24 31 35 44 27 31
R24 | 1900 11 18 11 20 19 8 | 32 39 35 43 31 33
XR25 |13862 3 --- --- --- --- 0 | 46 --- --- --- --- 47
------+------------------------------------+--------------------------------
RMS | 1717 16 39 22 25 31 |T 55 57 56 58 47 54
WRMS | 1717 15 22 13 20 31 |NE 55 57 56 58 47 54
MEDI | 1352 13 18 13 19 20 |MD 47 42 43 44 37 44
Table 3.2274.2 GPS week: 2274 Day: 2 MJD: 60164
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1123 38 75 33 28 56 25 | 77 54 78 52 33 60
R02 | 2394 7 14 7 15 25 6 | 58 46 52 62 46 54
R03 | 1076 15 14 10 13 30 7 | 55 39 39 55 36 47
R04 | 1361 17 12 12 23 27 9 | 55 49 41 45 43 45
R05 | 3379 12 9 12 19 22 8 | 61 45 48 51 45 52
R07 | 1084 17 19 11 19 26 9 | 69 60 66 60 50 63
R08 | 1742 12 17 20 23 20 10 | 59 52 73 58 58 61
R09 | 2200 17 19 17 12 18 9 | 32 30 32 25 23 27
R11 | 2673 11 16 10 9 25 6 | 27 29 31 27 34 27
R12 | 820 8 14 8 11 14 5 | 32 37 34 34 36 33
R13 | 971 30 32 33 41 77 19 | 47 32 41 41 53 39
R14 | 699 8 9 14 12 16 6 | 31 29 29 35 35 30
R15 | 1164 10 18 15 19 26 8 | 31 33 39 27 39 31
R16 | 882 12 24 9 16 18 9 | 37 54 41 30 43 38
R17 | 1191 11 20 11 30 --- 10 | 115 114 116 111 --- 113
R18 | 1229 9 21 7 21 18 8 | 76 82 78 82 75 78
R19 | 1756 22 50 33 48 34 22 | 91 100 100 74 81 89
R20 | 3582 48 94 65 42 98 36 | 92 82 119 70 54 81
R21 | 1223 14 21 14 15 28 9 | 91 84 90 90 70 88
R22 | 4059 13 9 9 14 18 6 | 41 45 47 47 43 44
R24 | 2354 9 14 14 20 17 8 | 45 51 49 55 41 48
XR25 |14220 8 16 --- --- --- 12 | 41 40 --- --- --- 40
------+------------------------------------+--------------------------------
RMS | 2002 19 33 22 24 37 |T 57 53 59 53 46 54
WRMS | 2002 15 17 12 19 37 |NE 57 53 59 53 46 54
MEDI | 1229 12 17 12 19 25 |MD 55 46 48 52 43 47
Table 3.2274.3 GPS week: 2274 Day: 3 MJD: 60165
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 771 42 74 35 30 29 26 | 89 40 83 59 45 61
R02 | 2691 10 15 13 15 21 7 | 60 53 63 60 49 58
R03 | 1418 13 15 13 17 31 8 | 64 46 62 50 41 55
R04 | 2004 11 14 10 14 34 7 | 51 51 41 48 38 46
R05 | 2164 21 11 9 18 24 9 | 56 39 35 39 45 40
R07 | 1336 16 18 16 18 32 10 | 69 46 68 58 39 59
R08 | 1342 18 14 9 20 24 9 | 66 53 60 53 44 57
R09 | 1300 21 16 21 14 12 10 | 27 23 25 17 23 19
R11 | 2871 11 10 10 10 14 6 | 24 24 24 24 24 21
R12 | 1375 11 9 8 13 21 6 | 26 28 27 26 33 25
R13 | 1115 40 42 32 38 62 22 | 46 38 31 38 38 35
R14 | 1063 9 7 15 13 14 6 | 23 27 23 29 27 24
R15 | 1282 21 17 18 17 23 10 | 30 52 56 38 35 42
R16 | 1159 25 19 19 17 12 11 | 36 62 60 35 50 45
R17 | 983 25 15 12 18 --- 10 | 77 58 64 74 --- 67
R18 | 1163 12 24 16 18 20 10 | 53 53 40 57 49 48
R19 | 3018 21 47 33 24 38 18 | 67 40 68 54 41 54
R20 | 2378 41 86 66 45 85 35 | 81 60 107 54 49 69
R21 | 790 10 23 15 20 18 10 | 76 65 79 81 63 74
R22 | 4461 19 16 16 25 18 11 | 35 39 45 51 40 40
R24 | 2089 13 20 11 17 25 9 | 29 36 25 42 26 30
XR25 |11378 11 17 --- --- --- 14 | 23 30 --- --- --- 26
------+------------------------------------+--------------------------------
RMS | 1967 22 32 23 22 33 |T 50 43 51 47 39 45
WRMS | 1967 18 20 19 18 33 |NE 50 43 51 47 39 45
MEDI | 1342 16 16 15 18 23 |MD 51 40 56 50 40 45
Table 3.2274.4 GPS week: 2274 Day: 4 MJD: 60166
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1303 41 69 28 14 41 23 | 89 29 83 67 47 67
R02 | 1794 9 9 9 10 15 5 | 57 49 47 57 48 52
R03 | 1661 12 15 10 13 24 7 | 59 45 55 54 43 53
R04 | 2013 13 11 8 11 22 6 | 53 49 45 50 36 48
R05 | 734 19 14 15 21 26 10 | 61 48 39 40 36 48
R07 | 845 19 17 6 20 24 9 | 65 55 51 51 44 54
R08 | 1236 12 18 24 27 26 12 | 63 55 80 56 46 62
R09 | 748 13 18 16 11 15 8 | 11 20 23 15 17 15
R11 | 1950 9 14 12 11 12 6 | 20 30 28 24 25 23
R12 | 1029 9 15 11 8 14 6 | 23 26 23 24 24 22
R13 | 834 36 41 34 28 55 20 | 47 29 29 28 39 32
R14 | 766 5 10 4 7 16 4 | 19 23 22 23 21 21
R15 | 634 10 13 13 16 15 7 | 21 30 27 30 33 25
R16 | 1147 24 20 15 14 15 11 | 29 53 47 34 38 37
R17 | 786 21 20 13 33 --- 13 | 190 203 198 188 --- 193
R18 | 1136 8 21 18 12 9 9 | 80 95 87 91 81 87
R19 | 2143 27 48 39 37 30 21 | 87 74 81 80 76 78
R20 | 1825 32 92 76 34 93 35 | 79 50 116 74 57 74
R21 | 924 15 15 12 17 18 8 | 71 63 71 73 61 69
R22 | 4218 15 16 19 23 20 11 | 20 28 33 43 32 28
R24 | 1532 10 18 13 20 18 9 | 35 39 32 38 25 33
XR25 |13232 10 18 --- --- --- 14 | 18 19 --- --- --- 17
------+------------------------------------+--------------------------------
RMS | 1600 20 32 24 20 32 |T 54 50 57 54 41 51
WRMS | 1600 17 22 14 16 32 |NE 54 50 57 54 41 51
MEDI | 1147 13 17 13 16 18 |MD 53 45 47 50 38 48
Table 3.2274.5 GPS week: 2274 Day: 5 MJD: 60167
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 966 33 81 45 21 48 28 | 81 27 96 71 49 65
R02 | 1419 9 12 23 24 19 10 | 47 49 61 47 37 48
R03 | 2395 15 16 9 16 25 8 | 57 44 53 50 37 50
R04 | 2077 14 17 13 16 23 8 | 53 45 55 51 41 49
R05 | 1513 17 12 11 17 23 8 | 59 40 48 50 38 47
R07 | 821 21 14 16 17 20 10 | 63 48 48 59 43 53
R08 | 1098 15 11 14 31 22 11 | 54 52 57 44 36 50
R09 | 674 19 12 20 16 9 10 | 20 28 31 19 20 21
R11 | 1217 10 11 17 13 11 8 | 27 30 21 28 30 24
R12 | 996 9 14 14 13 13 7 | 14 30 25 17 23 19
R13 | 1281 24 24 25 35 65 16 | 25 27 31 23 24 23
R14 | 872 9 11 11 14 14 6 | 17 21 19 16 16 16
R15 | 1073 9 14 15 25 22 9 | 15 24 23 26 32 19
R16 | 952 29 21 24 16 22 13 | 20 44 48 30 35 28
R17 | 1105 17 12 14 15 --- 8 | 69 68 65 59 --- 64
R18 | 1590 7 25 22 15 11 10 | 51 63 51 53 49 53
R19 | 2843 45 44 32 40 34 23 | 68 72 78 56 58 63
R20 | 2798 53 93 68 63 74 40 | 68 58 71 50 51 49
R21 | 1092 13 20 22 28 21 12 | 60 59 70 54 51 58
R22 | 3513 14 19 12 20 13 9 | 33 39 38 40 34 34
R24 | 1107 8 15 15 24 24 9 | 37 35 43 46 25 37
XR25 |15920 14 22 --- --- --- 18 | 21 30 --- --- --- 20
------+------------------------------------+--------------------------------
RMS | 1676 22 32 25 26 31 |T 43 42 49 42 36 40
WRMS | 1676 17 22 15 20 31 |NE 43 42 49 42 36 40
MEDI | 1107 14 15 16 17 22 |MD 47 40 48 47 36 47
Table 3.2274.6 GPS week: 2274 Day: 6 MJD: 60168
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1582 37 80 36 21 40 26 | 112 45 110 88 58 88
R02 | 1032 12 12 16 17 24 8 | 70 68 79 79 56 73
R03 | 2451 15 20 14 18 34 9 | 77 59 74 65 45 69
R04 | 2452 11 14 17 22 20 9 | 71 63 72 58 51 65
XR05 | 1481 12 16 --- 13 28 9 | 71 54 --- 63 46 63
R07 | 1599 15 15 11 11 30 7 | 85 64 68 71 55 72
R08 | 1077 10 9 19 28 27 10 | 76 65 81 58 59 70
R09 | 1031 7 17 11 11 --- 6 | 24 31 30 25 --- 26
R11 | 722 12 19 10 9 11 7 | 35 35 35 34 36 33
R12 | 991 4 9 13 18 7 7 | 31 29 26 36 29 29
R13 | 1336 26 47 28 45 53 21 | 56 47 53 46 67 49
R14 | 1926 4 9 13 10 14 5 | 32 34 34 31 34 32
R15 | 893 10 14 15 16 8 8 | 32 34 31 37 37 32
R16 | 828 19 19 17 11 18 10 | 39 52 48 40 46 41
R17 | 1306 17 11 12 23 --- 9 | 108 102 102 100 --- 102
R18 | 1565 15 15 11 22 19 9 | 75 89 80 83 73 80
R19 | 4097 48 68 60 51 46 32 | 103 79 115 80 82 89
R20 | 3720 48 101 75 68 46 42 | 103 113 119 81 68 89
R21 | 776 9 21 17 23 30 10 | 94 91 103 84 76 92
R22 | 2992 19 12 28 23 20 12 | 42 48 52 52 36 43
R24 | 1073 10 18 14 22 26 9 | 56 53 59 62 46 56
XR25 |11401 8 18 --- --- --- 13 | 23 32 --- --- --- 24
------+------------------------------------+--------------------------------
RMS | 1928 21 37 27 27 29 |T 64 58 68 60 52 59
WRMS | 1928 16 23 18 20 29 |NE 64 58 68 60 52 59
MEDI | 1336 12 16 15 21 26 |MD 70 53 68 62 51 63
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