[IGSREPORT-29748] Wk 2300 IGLOS Final Orbits
acc
acc at igs.org
Mon Feb 26 03:52:03 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2300 (Feb 04, 2024 - Feb 10, 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 2.2300.
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:
igl2300[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2300 in the SP3 format.
igl23007.sum Combination Report for GPS Week 2300.
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 | -10.3 ns
1 | -7.8 ns
2 | -6.2 ns
3 | -8.5 ns
4 | -3.6 ns
5 | -2.7 ns
6 | -0.9 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 | COD | R26
0 | ESA | R26
0 | GFZ | R26
0 | GRG | R26
0 | IAC | R26
0 | JGX | R26
1 | COD | R26
1 | ESA | R26
1 | GFZ | R26
1 | GRG | R26
1 | IAC | R26
1 | JGX | R26
2 | COD | R26
2 | ESA | R26
2 | GFZ | R26
2 | GRG | R26
2 | IAC | R26
2 | JGX | R26
3 | COD | R26
3 | ESA | R26
3 | GFZ | R26
3 | GRG | R26
3 | IAC | R26
3 | JGX | R26
4 | COD | R26
4 | ESA | R26
4 | GFZ | R26
4 | GRG | R26
4 | IAC | R26
4 | JGX | R26
5 | COD | R26
5 | ESA | R26
5 | GFZ | R26
5 | GRG | R26
5 | IAC | R26
5 | JGX | R26
6 | COD | R26
6 | ESA | R26
6 | GFZ | R26
6 | GRG | R26
6 | IAC | R26
6 | JGX | 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 1.2300, 1a.2300).
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 2.2300.0-6)
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 3.2300.0-6).
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 2300 summary. (Feb 04, 2024 - Feb 10, 2024)
Table 1.2300.a GPS week : 2300 MJD: 60344.0-60350.0
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 1 5 -20 -7 54 .12 24 18 | 11472 -1787 3042 7517
| 1 0 1 11 14 41 .04 | 1352 2173
esa n/a| 0 1 -1 -22 -15 -40 -.18 29 20 | -3623 -1623 3030 7703
| 0 1 1 17 14 26 .03 | 4439 2272
gfz n/a| 0 1 5 39 4 -32 -.08 30 17 | 0 -1760 3068 7092
| 1 1 2 12 10 26 .04 | 0 2486
grg n/a| 3 -2 -5 9 3 55 .36 31 21 | -4962 -1741 3056 6675
| 1 0 1 25 24 27 .04 | 3364 2356
jgx n/a| 0 0 -3 1 12 -37 -.16 29 28 | 13225 -1456 3041 7172
| 1 0 2 20 15 68 .05 | 875 2039
Table 1.2300.b GPS week : 2300 MJD: 60344.0-60350.0
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 | 21 21 17 18 18 22 22 |
R02 | 9 6 8 7 8 10 9 |
R03 | 9 10 11 10 9 9 10 |
R04 | 9 9 9 11 12 9 8 |
R05 | 9 7 7 8 9 9 9 |
R07 | 8 8 9 10 10 9 11 |
R08 | 8 7 9 9 11 9 10 |
R09 | 11 11 9 9 9 7 7 |
R11 | 10 6 10 9 8 9 8 |
R12 | 7 9 9 11 11 8 8 |
R13 | 22 14 18 16 20 21 20 |
R14 | 6 6 8 8 6 7 10 |
R15 | 7 9 12 8 8 11 10 |
R16 | 12 8 8 9 9 10 11 |
R17 | 25 9 9 10 11 15 10 |
R18 | 9 16 8 8 8 9 9 |
R19 | 24 22 17 22 19 15 16 |
R20 | 44 39 38 44 46 33 31 |
R21 | 13 16 8 8 9 8 7 |
R22 | 9 9 8 10 8 8 7 |
R24 | 21 12 8 9 10 11 9 |
R25 | 17 14 12 14 0 --- --- |
Table 1.2300.c GPS week : 2300 MJD: 60344.0-60350.0
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 2300 0 | 1 102 109 -2120 1353 -5098 80.1 1651 1651 | -10328 0
brd 2300 1 | 39 -30 28 -445 -825 -6694 80.6 1628 1628 | -7810 0
brd 2300 2 | -31 5 108 -143 -1283 -6444 78.6 1730 1730 | -6161 0
brd 2300 3 | 0 71 75 -1182 -1475 -1167 78.5 1619 1619 | -8460 0
brd 2300 4 | 44 -8 82 -1164 -1448 -5196 80.1 1611 1611 | -3598 0
brd 2300 5 | 1 19 103 -912 -837 -1054 78.5 1883 1883 | -2735 0
brd 2300 6 | 28 55 124 -1560 2957 4006 81.1 3231 3231 | -905 0
-------------+------------------------------------------------------------+----------------
brd 2300 mean| 11 30 90 -1075 -222 -3092 79.6 1907 1907 | -5713 0
brd 2300 sdev| 26 47 31 663 1709 3892 1.1 591 591 | 3413 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 2.2300.0 GPS week: 2300 Day: 0 MJD: 60344
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 8 -1 -15 126 .16 26 20 | 12734 -938 2791 8768
esa n/a| 0 0 -3 -48 -33 0 -.14 37 26 | -7812 -766 2782 7885
gfz n/a| -3 0 3 20 18 -46 -.08 34 18 | 0 -1000 2836 8171
grg n/a| 6 -2 -4 14 43 36 .28 35 24 | -9932 -956 2819 7531
jgx n/a| -2 0 -6 19 -5 -133 -.17 27 26 | 13865 -199 2791 7857
Table 2.2300.1 GPS week: 2300 Day: 1 MJD: 60345
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 6 -27 -14 79 .13 27 19 | 13317 -5659 3362 8164
esa n/a| 0 2 -1 -35 -13 -34 -.19 32 21 | -4669 -5538 3344 8070
gfz n/a| 0 3 9 31 -3 -33 -.02 33 18 | 0 -5914 3401 7660
grg n/a| 2 -3 -8 14 32 101 .39 28 19 | -4939 -5865 3415 7248
jgx n/a| -2 0 -3 5 -5 -92 -.25 24 24 | 14738 -4617 3115 7595
Table 2.2300.2 GPS week: 2300 Day: 2 MJD: 60346
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 7 -23 -6 58 .12 23 18 | 10300 1093 3109 7252
esa n/a| -1 1 0 -28 -25 -31 -.18 27 20 | -8246 1686 3101 6749
gfz n/a| -1 3 3 42 16 -12 -.14 31 18 | 0 2185 3156 6606
grg n/a| 3 -3 -6 -7 4 53 .40 23 17 | -7231 1920 3121 6129
jgx n/a| 0 0 0 10 10 -79 -.16 28 28 | 12850 1749 3194 6762
Table 2.2300.3 GPS week: 2300 Day: 3 MJD: 60347
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 4 -27 -6 43 .15 23 19 | 9370 -1595 3003 8784
esa n/a| -1 0 0 -15 2 -62 -.16 26 18 | -2514 -2361 2995 8189
gfz n/a| 0 0 3 55 -7 1 -.05 29 19 | 0 -2658 3061 7871
grg n/a| 2 -3 -5 -19 -23 20 .34 42 22 | -7352 -2436 3054 7391
jgx n/a| -1 0 -1 19 16 -35 -.20 27 28 | 11957 -1994 3060 8098
Table 2.2300.4 GPS week: 2300 Day: 4 MJD: 60348
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 -21 14 34 .15 25 21 | 11825 -3042 3022 6945
esa n/a| -1 1 -1 -17 -23 -28 -.23 25 18 | 3906 -2192 2989 9005
gfz n/a| 1 1 4 53 7 -10 -.07 29 15 | 0 -2292 3009 6849
grg n/a| 2 -3 -8 -4 -9 40 .36 38 20 | -2596 -2225 3000 6531
jgx n/a| 0 0 0 6 8 -9 -.07 34 35 | 13103 -2786 3037 6952
Table 2.2300.5 GPS week: 2300 Day: 5 MJD: 60349
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 5 -8 6 -8 .09 21 17 | 11221 -2188 3128 6916
esa n/a| 0 2 -3 3 -18 -47 -.20 27 19 | -6144 -2229 3127 6199
gfz n/a| -1 0 6 41 -2 -72 -.07 27 18 | 0 -2378 3142 6749
grg n/a| 2 -2 -5 10 -9 80 .39 26 19 | -1870 -2088 3105 6334
jgx n/a| 1 -1 -5 -23 21 50 -.13 31 27 | 12862 -1844 3183 7047
Table 2.2300.6 GPS week: 2300 Day: 6 MJD: 60350
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 5 -32 -28 51 .06 22 16 | 11537 -185 2881 5791
esa n/a| -1 1 -3 -13 7 -80 -.16 29 19 | 114 36 2875 7829
gfz n/a| 0 1 4 31 3 -55 -.10 24 16 | 0 -264 2874 5739
grg n/a| 2 -2 -2 58 -12 53 .37 26 26 | -815 -539 2884 5561
jgx n/a| 0 -1 -6 -30 39 38 -.17 27 26 | 13201 -503 2909 5898
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 3.2300.0 GPS week: 2300 Day: 0 MJD: 60344
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 699 42 77 28 15 21 21 | 112 56 96 83 62 77
R02M | 592 11 27 16 18 15 9 | 78 77 74 79 64 73
R03 | 2230 13 19 17 19 20 9 | 78 59 72 77 53 67
R04 | 966 14 15 15 20 25 9 | 77 80 82 79 72 76
R05 | 1943 10 13 25 18 18 9 | 60 58 72 57 51 58
R07 | 1385 11 17 17 14 16 7 | 74 64 78 74 55 68
R08 | 1659 15 18 13 19 17 8 | 70 70 73 83 59 69
R09M | 1829 17 22 19 24 29 11 | 44 47 43 46 36 40
R11M | 1419 12 13 23 32 13 9 | 36 39 44 50 36 39
R12M | 663 12 10 13 17 13 6 | 44 44 46 37 48 42
R13M | 1572 29 23 14 71 57 21 | 63 57 53 41 44 50
R14 | 2959 8 14 12 14 10 5 | 44 54 50 44 45 46
R15 | 1548 15 14 15 12 14 7 | 48 54 55 48 41 48
R16 | 1221 19 23 28 13 30 11 | 59 78 78 72 58 66
XR17 | 1141 25 19 34 76 --- 24 | 95 92 99 120 --- 96
R18E | 759 16 19 15 28 11 9 | 44 50 52 53 42 45
R19E | 1417 64 47 30 38 49 24 | 156 129 145 149 134 138
R20E | 1636 50 117 125 59 59 43 | 110 69 167 84 98 94
R21E | 802 11 18 14 47 24 12 | 68 63 70 92 69 69
R22E | 3272 18 16 23 16 11 8 | 62 64 69 72 60 63
R24E | 1330 33 30 32 81 17 21 | 116 133 127 139 114 121
XR25 |14014 13 21 --- --- --- 17 | 38 28 --- --- --- 35
------+------------------------------------+--------------------------------
RMS | 1650 26 37 34 35 27 |T 71 66 78 75 62 67
WRMS | 1650 20 26 18 24 26 |NE 68 63 75 73 55 64
MEDI | 1417 15 19 17 19 17 |MD 63 59 72 74 55 66
Table 3.2300.1 GPS week: 2300 Day: 1 MJD: 60345
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 967 50 59 43 11 31 21 | 78 44 79 52 38 51
R02M | 937 6 13 17 11 12 6 | 72 68 70 76 62 69
R03 | 2206 19 17 16 19 26 10 | 64 50 55 67 39 53
R04 | 999 13 12 12 17 26 8 | 63 54 61 64 50 57
R05 | 1531 13 14 16 11 17 7 | 47 44 48 45 36 42
R07 | 1376 11 10 17 17 16 7 | 55 50 52 55 43 49
R08 | 900 12 12 20 11 12 7 | 48 50 47 46 44 45
XR09M | 1569 19 20 20 15 --- 10 | 34 46 39 40 --- 38
R11M | 1366 11 10 15 13 13 6 | 33 37 37 45 35 35
R12M | 792 14 10 23 15 20 8 | 29 32 40 29 21 28
R13M | 1760 19 16 14 41 36 14 | 45 40 50 51 44 43
R14 | 1780 11 12 11 10 11 5 | 31 33 28 35 26 28
R15 | 983 17 12 23 21 12 8 | 31 32 30 40 26 27
R16 | 990 21 18 16 11 9 8 | 37 50 46 41 42 40
XR17 | 1251 14 14 14 17 --- 8 | 82 84 83 86 --- 82
R18E | 634 10 33 19 59 15 16 | 60 56 60 87 57 58
R19E | 1592 55 40 36 47 37 22 | 125 110 120 120 107 112
R20E | 2476 65 102 111 37 50 38 | 91 56 131 88 65 72
R21E | 956 20 18 20 57 24 15 | 61 56 60 97 46 59
R22E | 3232 17 12 20 23 18 9 | 60 62 66 71 64 63
R24E | 2549 31 19 24 18 19 11 | 103 105 104 103 105 102
XR25 |13456 14 13 --- --- --- 14 | 37 33 --- --- --- 37
------+------------------------------------+--------------------------------
RMS | 1628 27 32 33 28 24 |T 58 54 62 63 50 54
WRMS | 1628 19 21 18 19 24 |NE 52 47 52 53 38 46
MEDI | 1366 14 14 19 17 18 |MD 55 50 55 55 44 49
Table 3.2300.2 GPS week: 2300 Day: 2 MJD: 60346
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1198 30 51 34 15 32 17 | 77 34 81 74 45 59
R02M | 610 12 15 20 16 16 8 | 60 74 73 57 64 64
R03 | 715 19 17 19 15 32 10 | 65 48 62 58 42 53
R04 | 1404 12 21 13 17 21 8 | 71 68 69 77 65 69
R05 | 1046 11 11 14 13 21 7 | 61 51 58 65 42 55
R07 | 1975 20 15 13 15 23 9 | 75 59 60 61 52 60
R08 | 810 15 13 19 19 16 8 | 58 52 50 55 47 51
R09M | 1470 17 19 17 14 16 8 | 37 46 44 41 38 38
R11M | 899 16 13 14 28 23 10 | 24 32 29 43 20 24
R12M | 713 25 10 14 19 15 9 | 33 29 28 24 17 24
R13M | 2151 25 12 42 54 31 18 | 53 46 50 33 38 41
R14 | 1098 9 11 28 17 11 8 | 34 40 59 31 36 38
R15 | 746 23 23 14 20 31 11 | 33 37 31 38 21 27
R16 | 1030 16 19 11 15 18 8 | 43 55 48 44 48 45
XR17 | 1380 15 15 15 18 --- 9 | 82 75 79 86 --- 80
R18E | 490 9 21 13 17 10 7 | 25 31 25 35 23 25
R19E | 1849 28 33 37 32 35 16 | 156 147 159 146 141 148
R20E | 3711 66 84 102 39 82 38 | 114 97 129 101 96 94
R21E | 1301 10 16 21 14 17 8 | 37 30 42 41 27 33
R22E | 3591 12 14 18 18 12 7 | 113 118 120 115 114 115
R24E | 2633 18 17 17 15 13 8 | 71 67 65 79 70 69
XR25 |13531 11 13 --- --- --- 12 | 59 51 --- --- --- 58
------+------------------------------------+--------------------------------
RMS | 1729 23 27 31 23 28 |T 62 58 64 62 52 57
WRMS | 1729 18 20 18 17 28 |NE 59 51 59 58 44 54
MEDI | 1198 16 15 17 17 18 |MD 59 51 59 57 42 53
Table 3.2300.3 GPS week: 2300 Day: 3 MJD: 60347
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 683 40 45 29 25 27 17 | 79 37 61 62 41 49
R02M | 862 8 13 16 20 17 7 | 58 60 50 68 49 55
R03 | 816 16 24 15 18 20 9 | 61 45 61 62 46 52
R04 | 744 21 19 20 17 25 10 | 56 44 48 57 34 45
R05 | 626 15 16 11 13 21 8 | 63 47 58 58 41 52
R07 | 1189 17 15 19 25 26 10 | 60 62 69 69 46 58
R08 | 884 20 17 10 17 22 9 | 54 59 59 63 48 54
R09M | 1341 19 12 17 21 15 8 | 31 34 36 34 41 32
R11M | 675 15 11 22 17 23 9 | 30 41 51 40 29 36
R12M | 641 23 15 17 29 23 10 | 40 38 37 22 23 30
R13M | 2368 27 8 25 55 35 15 | 52 41 47 35 31 40
R14 | 1675 10 13 23 16 9 7 | 44 42 58 52 42 46
R15 | 656 16 18 20 17 9 8 | 40 37 51 48 38 40
R16 | 517 20 23 13 17 14 9 | 53 59 52 58 53 52
XR17 | 1254 16 15 13 22 --- 9 | 71 70 69 71 --- 69
R18E | 559 9 13 20 18 14 7 | 30 35 32 41 31 30
R19E | 2378 31 22 36 93 26 22 | 136 141 146 180 133 140
R20E | 3041 59 78 95 127 84 43 | 86 96 112 119 77 79
R21E | 1165 12 16 15 17 14 7 | 39 33 39 42 33 35
R22E | 3506 12 18 24 30 14 9 | 76 74 80 78 73 74
R24E | 2602 12 23 17 22 16 9 | 76 82 80 82 75 77
XR25 |19236 13 14 --- --- --- 14 | 54 37 --- --- --- 50
------+------------------------------------+--------------------------------
RMS | 1619 23 26 29 42 27 |T 58 55 61 63 49 54
WRMS | 1619 19 18 19 22 28 |NE 57 49 58 60 43 51
MEDI | 884 16 16 19 20 20 |MD 54 44 58 58 41 50
Table 3.2300.4 GPS week: 2300 Day: 4 MJD: 60348
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 909 49 34 21 29 38 18 | 72 34 50 44 30 40
R02M | 1904 8 19 15 13 21 8 | 63 77 65 69 66 67
R03 | 609 12 18 16 20 26 9 | 63 51 64 71 56 58
R04 | 1250 23 24 22 16 33 12 | 63 65 76 66 64 64
R05 | 1878 15 18 17 19 24 9 | 48 35 44 56 37 41
R07 | 983 18 20 12 17 31 10 | 57 39 50 58 31 45
R08 | 727 26 18 16 15 26 10 | 57 48 63 48 44 51
R09M | 2121 21 19 10 15 16 8 | 46 46 43 45 40 43
R11M | 690 12 13 11 22 24 8 | 25 27 24 31 31 23
R12M | 664 18 15 20 32 23 10 | 34 41 46 23 28 33
R13M | 2460 39 14 25 43 74 20 | 50 37 49 28 31 34
R14 | 833 12 9 11 13 14 6 | 40 35 34 33 34 34
R15 | 681 13 13 16 16 23 8 | 41 39 45 37 30 37
R16 | 663 15 17 20 14 20 8 | 43 56 60 55 38 49
XR17 | 1011 12 18 15 29 --- 10 | 109 103 106 117 --- 108
R18E | 659 12 16 19 13 16 8 | 25 31 27 34 29 26
R19E | 1921 41 21 31 61 32 19 | 151 159 161 137 155 151
R20E | 3013 54 81 105 129 88 46 | 89 132 140 110 103 99
R21E | 1137 9 16 13 22 24 8 | 29 28 30 38 27 27
R22E | 1918 17 15 13 19 14 8 | 57 58 59 56 57 56
R24E | 3044 19 16 14 31 15 9 | 57 54 55 56 47 51
XR25 |25719 4 --- --- --- --- 0 | 44 --- --- --- --- 40
------+------------------------------------+--------------------------------
RMS | 1611 25 25 29 38 34 |T 57 56 61 57 48 53
WRMS | 1611 21 18 15 20 35 |NE 57 50 59 58 40 51
MEDI | 1011 15 18 16 19 24 |MD 50 46 50 55 37 43
Table 3.2300.5 GPS week: 2300 Day: 5 MJD: 60349
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1270 43 58 26 31 45 21 | 85 50 77 73 45 63
R02M | 2607 13 25 12 27 24 10 | 52 55 53 46 46 47
R03 | 576 14 11 19 13 25 8 | 66 55 53 64 46 56
R04 | 1486 10 14 14 20 27 8 | 68 64 60 76 67 65
R05 | 1973 13 18 20 14 28 9 | 56 49 58 54 53 52
R07 | 875 12 19 15 15 30 9 | 59 44 47 60 35 48
R08 | 1083 14 19 13 14 26 8 | 53 49 52 54 45 50
R09M | 1510 9 17 14 9 18 7 | 34 36 38 38 40 35
R11M | 1050 12 15 21 26 16 9 | 18 20 30 33 22 20
R12M | 835 12 14 15 19 13 7 | 24 33 27 25 28 25
R13M | 1549 27 9 24 54 75 20 | 40 37 47 22 38 32
R14 | 1046 13 10 15 15 12 6 | 31 28 24 24 31 26
R15 | 1033 21 18 28 15 23 10 | 37 43 35 25 32 31
R16 | 686 18 14 24 14 23 9 | 44 46 42 38 35 39
XR17 | 2095 17 24 22 35 --- 14 | 85 85 82 70 --- 78
R18E | 530 13 16 21 18 22 9 | 31 33 30 39 33 31
R19E | 3726 27 18 33 35 31 14 | 108 108 115 112 106 107
R20E | 4787 50 77 84 59 55 33 | 88 92 124 60 69 77
R21E | 745 11 16 14 14 20 7 | 39 34 37 37 31 34
R22E | 1248 15 13 11 20 19 8 | 54 50 52 52 47 49
R24E | 2410 16 25 23 22 17 10 | 103 98 100 99 95 98
------+------------------------------------+--------------------------------
RMS | 1883 21 27 27 26 31 |T 55 52 56 52 47 50
WRMS | 1883 17 19 18 19 27 |NE 58 51 53 53 43 50
MEDI | 1248 14 17 20 19 23 |MD 53 49 52 52 40 48
Table 3.2300.6 GPS week: 2300 Day: 6 MJD: 60350
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 958 45 68 22 36 35 22 | 118 52 97 106 60 83
R02M | 2841 13 17 12 15 24 8 | 70 80 78 73 63 72
R03 | 1115 18 15 19 21 23 9 | 89 80 86 84 67 80
R04 |12421 12 12 16 20 17 7 | 93 87 89 95 97 89
R05 | 1356 15 13 18 17 25 9 | 81 69 81 76 67 74
R07 | 1140 20 21 14 24 27 10 | 72 50 59 78 42 59
R08 | 724 13 18 16 19 32 10 | 75 68 67 72 54 66
R09M | 2090 10 15 14 10 18 7 | 46 47 50 48 53 48
R11M | 1477 12 16 17 14 19 8 | 71 68 77 71 73 70
R12M | 946 10 13 13 20 18 7 | 37 40 37 28 31 33
R13M | 1250 33 26 27 48 57 19 | 56 63 64 43 48 52
R14 | 1021 10 15 18 16 32 9 | 44 48 48 39 40 42
R15 | 1159 17 23 12 15 29 9 | 53 57 45 44 38 45
R16 | 618 15 15 21 31 22 10 | 64 63 68 50 55 58
XR17 | 2400 8 20 12 24 --- 9 | 107 100 107 116 --- 107
R18E | 469 16 15 23 14 21 9 | 32 37 45 41 32 35
R19E | 2765 23 27 38 42 29 16 | 132 134 135 138 134 132
R20E | 3799 58 79 67 51 36 30 | 79 114 116 79 94 81
R21E | 764 8 15 15 18 13 7 | 45 39 43 46 40 41
R22E | 946 14 10 10 17 19 7 | 55 56 60 63 62 58
R24E | 2237 11 20 14 23 16 8 | 106 105 107 113 106 106
------+------------------------------------+--------------------------------
RMS | 3230 22 29 24 26 27 |T 72 69 74 71 62 68
WRMS | 3230 16 19 16 26 26 |NE 79 67 74 76 57 70
MEDI | 1159 14 16 16 20 23 |MD 71 63 68 72 55 66
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