[IGSREPORT-29480] Wk 2275 IGLOS Final Orbits
acc
acc at igs.org
Tue Sep 5 00:01:04 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2275 (Aug 13, 2023 - Aug 19, 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 2.2275.
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:
igl2275[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2275 in the SP3 format.
igl22757.sum Combination Report for GPS Week 2275.
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 | -11.3 ns
1 | -11.5 ns
2 | -14.5 ns
3 | -12.7 ns
4 | -13.5 ns
5 | -10.8 ns
6 | -14.9 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 1.2275, 1a.2275).
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 2.2275.0-6)
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 3.2275.0-6).
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 2275 summary. (Aug 13, 2023 - Aug 19, 2023)
Table 1.2275.a GPS week : 2275 MJD: 60169.0-60175.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 1 -29 20 .03 18 15 | 17869 -814 3009 8853
| 1 0 1 14 17 15 .03 | 2187 1371
esa n/a| -2 0 4 0 5 13 -.21 33 24 | -11690 -100 3007 7921
| 1 2 2 10 14 20 .04 | 11236 1391
gfz n/a| 0 0 -4 20 5 -3 -.22 25 16 | 0 -902 2968 8118
| 1 0 1 14 9 19 .05 | 0 1527
grg n/a| 2 0 -1 -25 18 -46 .36 28 19 | -12311 -1161 2969 7665
| 1 2 1 19 25 37 .02 | 1634 1819
iac n/a| 0 1 -15 1 -2 3 -1.43 40 40 | -10423 -613 2990 8816
| 2 2 11 33 27 99 1.45 | 1579 1109
jgx n/a| 0 0 4 8 -5 46 -.20 32 32 | 18539 -1137 2981 8062
| 1 1 3 26 17 22 .08 | 1676 1766
Table 1.2275.b GPS week : 2275 MJD: 60169.0-60175.0
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 | 24 25 26 28 26 24 31 |
R02 | 9 7 7 10 9 8 8 |
R03 | 12 9 8 7 9 10 9 |
R04 | 8 9 8 8 7 8 8 |
R05 | 8 8 12 7 7 9 9 |
R07 | 9 9 9 11 10 9 9 |
R08 | 8 8 10 8 8 10 8 |
R09 | 8 11 8 8 10 7 7 |
R11 | 9 9 8 7 6 8 8 |
R12 | 11 8 10 9 7 8 8 |
R13 | 18 18 14 21 19 18 19 |
R14 | 9 7 8 7 5 7 8 |
R15 | 8 8 9 10 10 10 10 |
R16 | 11 12 10 9 10 9 10 |
R17 | 9 15 16 12 10 9 8 |
R18 | 11 11 12 16 12 8 8 |
R19 | 27 26 28 16 16 24 22 |
R20 | 34 36 40 36 41 41 42 |
R21 | 10 8 13 25 9 9 10 |
R22 | 9 8 8 8 10 16 8 |
R24 | 9 17 22 9 11 10 9 |
R25 | 14 11 18 14 17 16 19 |
Table 1.2275.c GPS week : 2275 MJD: 60169.0-60175.0
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 2275 0 | 80 -6 102 -930 1603 6948 79.0 1869 1869 | -11297 0
brd 2275 1 | -20 8 115 -1472 1272 5455 81.1 1396 1396 | -11462 0
brd 2275 2 | -38 -13 58 -785 559 1986 78.9 1423 1423 | -14515 0
brd 2275 3 | -57 -22 72 -1400 -1187 803 79.9 3667 3667 | -12745 0
brd 2275 4 | 60 -73 62 641 332 -690 79.4 1518 1518 | -13507 0
brd 2275 5 | -22 28 100 -111 -504 493 80.3 1454 1454 | -10765 0
brd 2275 6 | -42 33 227 1158 -1623 -706 80.1 1566 1566 | -14908 0
-------------+------------------------------------------------------------+----------------
brd 2275 mean| -5 -6 105 -414 64 2041 79.8 1841 1841 | -12742 0
brd 2275 sdev| 53 36 57 1014 1216 3018 .8 820 820 | 1635 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 2.2275.0 GPS week: 2275 Day: 0 MJD: 60169
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 1 20 -11 28 .01 21 17 | 20394 -1015 3045 9216
esa n/a| -2 0 3 6 16 14 -.23 33 24 | -7914 -155 3046 7219
gfz n/a| 0 0 -4 0 4 -5 -.24 22 16 | 0 -1253 3075 8585
grg n/a| 4 0 1 -14 -6 -27 .35 21 18 | -10759 -1520 3070 8159
iac n/a| -1 0 -6 5 24 83 -.39 27 22 | -9179 -1636 3033 9187
jgx n/a| 0 -1 9 -40 6 48 -.30 33 33 | 19833 -1644 3142 8224
Table 2.2275.1 GPS week: 2275 Day: 1 MJD: 60170
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 -2 -27 19 .04 18 14 | 20506 -1944 2875 8639
esa n/a| -5 -3 8 3 14 19 -.19 37 25 | -7138 -1397 2882 7068
gfz n/a| 0 0 0 20 -10 -2 -.28 23 18 | 0 -1674 2907 7595
grg n/a| 4 1 -3 -21 34 -43 .36 24 19 | -10497 -2090 2912 7390
iac n/a| 2 0 -10 42 -10 5 -.24 27 24 | -9331 677 2874 8390
jgx n/a| 0 0 5 21 6 63 -.22 33 33 | 20467 -1430 2764 7583
Table 2.2275.2 GPS week: 2275 Day: 2 MJD: 60171
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 3 -35 11 .06 19 15 | 16095 -2840 3510 9269
esa n/a| 0 -3 5 11 19 -5 -.19 35 23 | -32472 -2572 3506 11116
gfz n/a| 0 1 -4 14 17 -15 -.17 24 13 | 0 -3437 3410 9184
grg n/a| 1 2 0 -59 -17 4 .39 33 22 | -12642 -4108 3378 8883
iac n/a| 0 0 -3 -13 15 -3 -.20 28 25 | -11634 -2338 3490 9642
jgx n/a| 2 0 1 -13 -39 55 -.13 30 30 | 17332 -3943 3440 9202
Table 2.2275.3 GPS week: 2275 Day: 3 MJD: 60172
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 -22 -38 36 .08 17 13 | 16809 1117 3635 8791
esa n/a| -2 0 1 -1 9 -5 -.15 31 18 | -14218 977 3635 7982
gfz n/a| 0 1 -5 47 12 17 -.27 24 15 | 0 1190 3371 8214
grg n/a| 3 -2 -1 -25 11 -103 .39 36 23 | -13808 1744 3448 7809
iac n/a| 0 3 -7 -64 -33 58 -.23 24 23 | -10392 -217 3625 8867
jgx n/a| 2 0 1 20 -15 68 -.07 35 35 | 17223 1898 3428 8359
Table 2.2275.4 GPS week: 2275 Day: 4 MJD: 60173
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 17 -10 13 -.01 16 14 | 15793 -2 2901 9312
esa n/a| -1 0 4 6 -15 31 -.24 31 23 | -7163 942 2902 6453
gfz n/a| 0 0 -4 19 -4 -35 -.22 29 14 | 0 429 2949 8718
grg n/a| 2 0 -2 -39 27 -16 .33 24 18 | -13500 -291 2922 7934
iac n/a| 0 2 -32 1 34 -195 -2.86 61 62 | -11396 -270 2864 9132
jgx n/a| 0 1 2 34 -10 56 -.21 32 32 | 17596 -680 2998 8551
Table 2.2275.5 GPS week: 2275 Day: 5 MJD: 60174
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 0 -2 -59 39 .03 17 15 | 19583 293 2586 9022
esa n/a| 0 2 5 -19 -12 -2 -.26 32 29 | 3762 1006 2585 8530
gfz n/a| 0 0 -6 21 8 -5 -.25 30 19 | 0 -202 2617 7825
grg n/a| 0 -2 -1 4 56 -57 .34 25 15 | -10683 -266 2615 7274
iac n/a| 0 -2 -25 9 -26 -23 -3.18 58 62 | -8302 -1018 2553 8898
jgx n/a| 0 2 3 20 1 27 -.17 34 33 | 20581 -346 2631 7858
Table 2.2275.6 GPS week: 2275 Day: 6 MJD: 60175
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 0 -23 -3 .01 20 14 | 15903 -1311 2514 7724
esa n/a| -2 0 5 -3 3 45 -.24 31 27 | -16691 495 2496 7080
gfz n/a| 2 1 -5 19 12 23 -.14 22 13 | 0 -1369 2449 6711
grg n/a| 1 -3 0 -25 21 -79 .38 30 17 | -14290 -1602 2439 6212
iac n/a| -4 1 -25 27 -24 100 -2.90 57 60 | -12727 509 2495 7596
jgx n/a| 0 3 7 16 11 4 -.27 27 27 | 16746 -1818 2466 6660
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 3.2275.0 GPS week: 2275 Day: 0 MJD: 60169
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1984 33 74 28 17 19 29 23 | 100 36 94 79 76 48 75
R02 | 825 12 12 16 21 20 19 9 | 57 48 62 52 66 39 53
R03 | 3183 13 19 24 22 22 34 11 | 62 39 61 54 62 31 52
R04 | 2071 14 12 12 14 12 25 7 | 61 50 52 57 59 42 54
R05 | 1426 12 12 10 18 15 12 8 | 57 55 59 61 68 48 57
R07 | 1665 16 15 13 15 19 23 8 | 79 58 68 70 81 50 68
R08 | 1612 11 17 11 14 17 34 7 | 67 55 65 59 68 41 60
R09 | 641 11 15 12 15 25 --- 8 | 34 42 35 34 38 --- 34
R11 | 775 12 22 10 14 29 17 8 | 39 56 47 43 50 38 44
R12 | 831 17 15 21 17 20 16 10 | 31 33 32 36 31 32 30
R13 | 1012 33 42 21 25 26 57 17 | 61 37 35 43 38 54 42
R14 | 1785 9 14 18 15 26 13 8 | 33 32 41 36 45 31 35
R15 | 1065 14 8 15 12 17 27 7 | 44 50 55 50 51 36 48
R16 | 896 29 13 19 8 26 15 11 | 49 47 47 38 51 48 42
R17 | 1531 15 14 14 19 18 --- 9 | 127 125 130 123 125 --- 126
R18E | 1397 16 22 12 24 17 14 11 | 123 130 121 132 127 122 125
R19E | 3800 38 61 51 35 63 71 27 | 106 55 117 70 52 43 86
R20 | 3816 40 91 55 48 51 65 34 | 110 62 121 86 93 83 89
R21E | 602 13 13 16 22 27 18 9 | 169 162 164 167 163 163 165
R22E | 2101 13 17 9 17 14 20 8 | 39 48 42 46 41 46 41
R24E | 976 15 16 13 16 20 21 9 | 92 94 91 98 89 83 92
XR25 |15641 11 15 --- --- 45 --- 13 | 39 39 --- --- 31 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1868 21 33 22 21 27 33 |T 71 61 73 68 68 56 66
WRMS | 1868 17 24 16 18 22 33 |NE 61 50 62 57 60 44 55
MEDI | 1426 14 15 15 17 20 21 |MD 61 50 61 57 59 46 53
Table 3.2275.1 GPS week: 2275 Day: 1 MJD: 60170
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1941 25 89 28 12 31 51 24 | 81 46 77 74 51 45 68
R02 | 648 8 9 13 14 24 20 6 | 52 51 47 53 54 38 49
R03 | 2943 16 18 6 17 12 21 8 | 54 42 44 47 48 39 45
R04 | 1659 13 12 11 20 25 23 8 | 53 43 49 48 56 42 47
R05 | 1101 10 17 15 12 22 17 7 | 43 42 47 49 43 37 44
R07 | 907 8 27 16 11 31 34 9 | 59 48 70 67 66 42 61
R08 | 979 10 21 10 11 13 33 7 | 55 43 54 54 44 33 51
R09 | 1315 16 17 20 19 26 --- 10 | 34 43 39 43 37 --- 37
R11 | 769 17 11 19 9 17 15 8 | 36 46 42 48 43 34 40
R12 | 787 10 20 9 13 15 23 7 | 28 39 39 31 32 28 32
R13 | 968 24 32 24 41 17 46 17 | 46 41 44 41 39 41 41
R14 | 1338 5 9 15 13 16 16 6 | 28 36 28 35 26 27 29
R15 | 795 12 22 12 12 16 11 8 | 32 50 48 40 39 41 40
R16 | 799 21 23 20 18 18 25 12 | 35 63 64 40 37 33 47
R17 | 1591 20 20 19 37 41 --- 14 | 93 95 95 104 96 --- 93
R18E | 1390 14 24 10 26 23 24 11 | 96 104 98 100 106 98 97
R19E | 1609 26 65 49 40 64 --- 25 | 72 55 99 61 37 --- 69
R20 | 1810 42 102 63 43 35 78 36 | 72 33 93 79 62 47 65
R21E | 727 12 17 12 15 30 19 8 | 132 130 133 126 124 125 130
R22E | 1733 12 14 9 17 18 20 7 | 24 32 29 38 30 35 28
R24E | 1240 20 22 22 44 29 36 16 | 98 104 102 123 95 91 102
XR25 |12693 8 15 --- --- 28 --- 11 | 38 42 --- --- 38 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1396 18 37 23 24 27 33 |T 57 55 63 61 54 48 57
WRMS | 1396 14 25 18 19 24 33 |NE 49 47 55 53 47 37 48
MEDI | 1240 13 20 15 17 23 23 |MD 52 43 49 49 43 39 47
Table 3.2275.2 GPS week: 2275 Day: 2 MJD: 60171
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1300 32 81 29 20 27 55 26 | 85 33 81 66 40 28 63
R02 | 831 6 18 14 12 22 36 7 | 46 36 53 49 52 28 45
R03 | 3013 12 15 16 13 22 29 8 | 51 38 46 47 50 28 44
R04 | 1738 11 8 11 21 22 24 7 | 48 41 47 41 43 39 44
R05 | 1062 15 16 25 27 21 23 12 | 35 45 60 40 47 28 42
R07 | 637 11 21 12 14 19 23 8 | 60 51 69 70 69 50 61
R08 | 894 12 22 20 10 19 29 9 | 49 47 67 60 55 41 54
R09 | 728 11 10 10 19 19 20 7 | 23 28 28 21 33 21 22
R11 | 1029 16 16 11 11 32 20 8 | 28 32 34 26 36 35 27
R12 | 1782 14 20 14 18 16 14 9 | 22 33 32 30 27 20 25
R13 | 1373 14 29 17 37 30 50 14 | 25 28 41 35 38 27 28
R14 | 1307 7 12 15 18 13 14 7 | 25 26 35 21 25 26 25
R15 | 857 6 12 17 21 15 11 8 | 35 39 28 43 31 38 34
R16 | 750 19 26 11 12 16 21 10 | 36 59 46 41 41 38 43
R17 | 1647 21 14 15 52 49 --- 16 | 163 160 161 162 162 --- 160
R18E | 1088 16 22 15 27 14 18 11 | 130 140 132 147 127 129 135
R19E | 1413 25 52 60 51 52 --- 27 | 49 55 93 48 35 --- 56
R20 | 1735 54 102 55 66 39 60 40 | 81 62 76 59 64 63 57
R21E | 827 10 22 15 42 20 23 13 | 194 194 190 210 199 195 195
R22E | 2052 12 15 9 18 25 19 7 | 28 32 28 38 40 35 29
R24E | 1492 22 18 27 76 40 19 22 | 147 143 142 158 129 135 143
XR25 |17333 13 22 --- --- 20 --- 17 | 23 48 --- --- 33 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1422 19 35 24 33 28 30 |T 62 62 70 67 62 52 61
WRMS | 1422 15 23 13 22 25 30 |NE 49 47 56 50 49 34 47
MEDI | 1300 13 18 15 20 21 23 |MD 46 41 53 47 41 35 44
Table 3.2275.3 GPS week: 2275 Day: 3 MJD: 60172
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 946 29 87 32 25 16 56 27 | 91 38 96 86 74 36 73
R02 | 984 5 20 22 15 14 34 9 | 57 42 63 54 49 33 53
R03 | 1909 11 16 10 9 27 37 7 | 58 39 45 54 62 33 49
R04 | 975 14 9 11 17 21 25 7 | 53 41 40 39 43 32 43
R05 | 1597 8 9 10 19 31 14 6 | 47 42 44 47 51 42 44
R07 | 1036 16 25 12 23 20 24 11 | 72 58 67 60 54 56 63
R08 | 1469 9 18 13 16 11 20 8 | 55 50 64 62 55 43 56
R09 | 1023 14 13 13 17 16 9 8 | 18 17 15 15 26 13 14
R11 | 967 12 13 10 10 20 20 6 | 27 23 24 25 35 25 23
R12 | 1673 16 16 16 13 12 11 9 | 31 31 33 31 25 30 28
R13 | 2084 21 30 35 63 19 83 21 | 36 32 46 42 37 47 34
R14 | 1550 9 11 16 13 16 15 7 | 30 30 41 33 30 28 33
R15 | 995 13 18 18 24 13 12 10 | 36 36 46 43 33 33 37
R16 | 693 11 20 8 21 14 14 8 | 41 56 47 33 50 48 44
R17 | 1103 8 18 19 37 23 --- 11 | 102 96 104 98 111 --- 98
R18E | 860 9 25 13 57 20 15 15 | 130 131 130 128 128 125 127
R19E | 1537 20 28 26 40 41 31 16 | 45 57 60 60 38 45 46
R20 | 3674 43 75 65 68 59 85 35 | 92 73 114 49 53 45 73
R21E | 677 14 18 46 86 24 28 25 | 216 219 232 228 207 222 219
R22E |15419 12 10 13 19 20 15 7 | 40 42 50 52 39 43 43
R24E | 1071 13 19 13 17 18 19 8 | 91 93 99 84 81 88 90
XR25 |12541 10 18 --- --- 18 --- 14 | 41 54 --- --- 40 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 3667 17 31 24 36 24 35 |T 64 59 69 63 60 53 60
WRMS | 3667 13 18 15 23 23 35 |NE 52 44 55 48 48 36 47
MEDI | 1071 12 18 13 19 19 20 |MD 47 42 50 52 49 42 44
Table 3.2275.4 GPS week: 2275 Day: 4 MJD: 60173
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1209 30 84 32 21 88 35 26 | 95 47 96 77 147 58 77
R02 | 667 11 19 18 12 64 28 8 | 55 49 71 64 107 39 58
R03 | 1275 10 21 18 16 75 24 9 | 61 48 68 54 120 43 57
R04 | 702 10 15 8 13 73 32 6 | 61 55 51 62 116 42 56
R05 | 1583 11 9 12 15 95 15 7 | 54 48 45 46 125 47 47
R07 | 895 15 24 10 18 81 28 10 | 67 48 59 59 118 41 58
R08 | 1590 9 16 13 17 57 21 8 | 57 54 65 55 102 51 57
R09 | 612 10 14 22 19 47 14 9 | 24 33 32 28 24 19 25
R11 | 1717 6 7 14 9 48 9 5 | 30 39 48 33 27 37 36
R12 | 783 7 15 15 11 44 11 7 | 26 36 29 27 80 28 26
R13 | 1913 27 34 35 35 46 49 18 | 34 39 37 34 78 21 29
R14 | 2053 7 10 8 11 36 12 5 | 24 31 28 28 70 28 27
R15 | 773 14 26 12 16 41 22 10 | 30 42 43 40 82 25 35
R16 | 673 19 19 15 16 52 17 10 | 36 43 41 27 89 34 34
R17 | 1407 11 19 13 23 38 --- 9 | 129 131 130 132 128 --- 129
R18E | 840 19 23 25 17 31 17 12 | 136 133 124 127 123 131 129
R19E | 1658 19 31 37 25 65 40 16 | 44 34 55 53 80 31 41
R20 | 3735 31 80 102 69 101 91 41 | 82 57 147 53 134 60 78
R21E | 906 13 17 14 19 35 14 9 | 184 181 178 179 182 184 180
R22E | 2126 14 12 20 23 62 16 10 | 50 51 48 71 46 47 53
R24E | 948 16 19 19 24 37 24 11 | 56 68 65 60 67 62 59
XR25 |11881 11 23 --- --- 55 --- 16 | 31 31 --- --- 21 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 1517 16 31 29 24 61 32 |T 62 59 69 62 93 51 60
WRMS | 1517 14 23 14 18 62 32 |NE 52 48 61 51 92 38 50
MEDI | 1209 11 19 15 17 52 21 |MD 54 48 55 54 89 41 53
Table 3.2275.5 GPS week: 2275 Day: 5 MJD: 60174
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1146 29 81 27 14 81 40 24 | 92 52 91 78 136 64 78
R02 | 1136 10 18 16 12 67 20 8 | 55 47 65 57 104 47 55
R03 | 1783 11 28 20 9 58 26 10 | 62 47 77 68 99 52 63
R04 | 728 11 19 10 10 59 26 7 | 65 61 65 66 96 54 63
R05 | 1349 16 14 11 19 65 25 9 | 69 56 58 57 99 49 60
R07 | 1358 15 19 7 18 81 25 9 | 70 52 65 60 110 50 62
R08 | 1521 10 21 21 19 76 30 10 | 63 62 75 69 117 58 65
R09 | 807 9 14 12 11 59 14 6 | 32 34 38 33 52 31 33
R11 | 1197 11 18 11 13 55 15 7 | 46 56 46 56 60 46 49
R12 | 1012 13 10 13 15 48 32 7 | 35 48 50 37 90 28 40
R13 | 1158 30 40 33 23 58 61 18 | 38 37 30 41 95 29 32
R14 | 1607 10 14 11 11 53 13 6 | 36 38 41 33 89 37 36
R15 | 920 15 22 16 17 36 9 10 | 35 36 41 41 80 38 35
R16 | 734 16 18 15 14 63 20 9 | 35 44 46 45 102 42 40
R17 | 848 9 18 13 22 28 --- 9 | 92 95 92 89 99 --- 90
R18E | 818 6 22 16 12 34 16 8 | 98 102 100 100 100 98 99
R19E | 985 27 32 46 55 65 43 23 | 43 47 59 71 47 39 44
R20 | 3159 28 84 103 60 43 97 40 | 69 42 134 65 62 43 68
R21E | 813 10 17 14 18 41 14 8 | 112 115 113 107 113 107 110
R22E | 3057 17 16 27 40 65 13 15 | 80 77 80 101 84 82 81
R24E | 1144 15 20 14 16 36 17 9 | 45 55 53 56 54 47 49
XR25 |12415 10 23 --- --- 64 --- 16 | 39 42 --- --- 56 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1453 17 32 30 25 58 34 |T 59 56 67 63 88 52 58
WRMS | 1453 15 29 19 15 62 33 |NE 54 49 63 55 90 44 53
MEDI | 1144 11 19 15 16 58 20 |MD 55 48 65 60 95 47 55
Table 3.2275.6 GPS week: 2275 Day: 6 MJD: 60175
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 748 26 97 45 17 68 40 30 | 132 40 141 118 157 81 109
R02 | 791 8 14 15 14 65 18 7 | 70 61 82 76 123 57 71
R03 | 1074 9 22 9 16 68 28 8 | 79 58 82 79 131 51 75
R04 | 877 11 20 11 11 49 29 7 | 73 59 79 76 106 48 71
R05 | 1114 12 19 11 18 64 27 8 | 76 58 71 68 118 53 68
R07 | 1586 17 15 14 13 73 22 9 | 85 64 71 74 125 55 74
R08 | 997 8 17 14 15 83 20 8 | 82 74 89 86 141 66 82
R09 | 818 11 11 14 13 49 11 7 | 39 45 47 44 47 32 42
R11 | 1355 9 12 15 17 58 15 7 | 49 51 47 52 51 47 48
R12 | 721 12 16 10 17 43 16 8 | 42 44 44 48 80 42 43
R13 | 1131 17 30 31 48 62 60 18 | 62 59 63 49 101 51 56
R14 | 763 10 18 16 9 58 10 8 | 47 39 43 44 89 46 42
R15 | 752 10 14 21 21 47 12 9 | 51 47 46 57 86 51 49
R16 | 1534 20 17 15 12 74 24 9 | 54 57 50 52 100 55 51
R17 | 820 10 13 10 20 31 --- 8 | 132 125 128 137 132 --- 130
R18E | 1192 9 18 13 17 28 13 8 | 111 108 106 114 106 106 108
R19E | 1520 27 34 46 40 53 44 21 | 78 64 113 78 94 64 80
R20 | 4011 68 60 47 105 68 49 41 | 122 94 143 122 98 90 107
R21E | 842 12 19 17 18 31 11 9 | 150 144 143 151 146 147 147
R22E | 3735 10 17 11 19 48 12 8 | 68 72 64 70 70 74 66
R24E | 836 13 14 14 19 37 14 8 | 84 78 89 89 82 80 84
XR25 |12767 13 24 --- --- 51 --- 18 | 39 46 --- --- 35 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1566 20 31 22 30 57 27 |T 78 67 82 80 100 64 74
WRMS | 1566 14 27 13 17 60 27 |NE 72 60 76 73 101 55 68
MEDI | 997 11 17 14 17 53 18 |MD 73 59 79 76 100 55 71
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