[IGSREPORT-29460] Wk 2273 IGLOS Final Orbits
acc
acc at igs.org
Mon Aug 21 04:25:56 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2273 (Jul 30, 2023 - Aug 05, 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 2.2273.
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:
igl2273[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2273 in the SP3 format.
igl22737.sum Combination Report for GPS Week 2273.
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 | -17.0 ns
1 | -0.2 ns
2 | -0.1 ns
3 | -16.1 ns
4 | -0.1 ns
5 | 0.1 ns
6 | -18.0 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2273, 1a.2273).
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 2.2273.0-6)
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 3.2273.0-6).
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 2273 summary. (Jul 30, 2023 - Aug 05, 2023)
Table 1.2273.a GPS week : 2273 MJD: 60155.0-60161.0
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 -1 -2 -20 25 .03 20 17 | 29813 -1087 3079 8635
| 1 0 2 20 10 28 .05 | 9207 1785
esa n/a| -1 -1 1 -4 3 26 -.28 33 21 | -4914 -128 3081 7790
| 1 1 2 13 12 17 .09 | 9001 2054
gfz n/a| 0 1 0 11 10 24 -.19 22 15 | 0 -929 3083 8156
| 0 1 1 12 8 24 .05 | 0 1742
grg n/a| 2 0 0 -9 6 -76 .40 27 19 | -6966 -1073 3084 7711
| 1 1 3 13 10 25 .04 | 8605 1850
jgx n/a| 0 0 5 38 17 69 -.34 34 34 | 30186 -1179 3082 8151
| 1 1 4 16 13 74 .11 | 9356 1967
Table 1.2273.b GPS week : 2273 MJD: 60155.0-60161.0
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 | 18 19 23 23 29 24 24 |
R02 | 6 7 8 9 10 20 15 |
R03 | 7 7 9 10 12 17 11 |
R04 | 8 8 8 8 8 17 11 |
R05 | 8 8 10 9 8 16 14 |
R07 | 8 8 10 9 11 20 9 |
R08 | 8 8 7 11 10 26 11 |
R09 | 8 7 11 8 7 5 7 |
R11 | 8 7 8 7 10 8 9 |
R12 | 6 13 7 8 9 7 10 |
R13 | 14 20 17 18 21 18 15 |
R14 | 6 7 6 7 7 7 6 |
R15 | 9 9 10 10 10 10 6 |
R16 | 12 12 10 11 12 11 10 |
R17 | 11 12 7 7 10 8 9 |
R18 | 12 9 10 11 13 14 10 |
R19 | 31 24 25 26 29 30 28 |
R20 | 37 33 33 36 42 38 36 |
R21 | 8 11 11 10 12 9 11 |
R22 | 7 8 9 8 10 9 9 |
R24 | 8 9 9 10 10 9 8 |
R25 | 9 11 14 15 13 0 15 |
Table 1.2273.c GPS week : 2273 MJD: 60155.0-60161.0
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 2273 0 | 16 19 178 1208 2222 4915 80.9 1550 1550 | -17031 0
brd 2273 1 | -46 14 239 -145 1758 1979 80.4 1478 1478 | -171 0
brd 2273 2 | -16 -66 171 677 1391 10730 80.4 2011 2011 | -73 0
brd 2273 3 | 34 58 236 -1853 -1235 4275 79.1 1987 1987 | -16059 0
brd 2273 4 | 13 40 156 -851 -2282 6006 76.2 1656 1656 | -50 0
brd 2273 5 | -24 35 138 1179 -265 509 79.4 1733 1733 | 144 0
brd 2273 6 | -3 34 231 -186 -256 2636 77.2 1687 1687 | -18044 0
-------------+------------------------------------------------------------+----------------
brd 2273 mean| -3 19 193 3 190 4435 79.1 1728 1728 | -7326 0
brd 2273 sdev| 27 40 41 1119 1662 3342 1.8 203 203 | 9109 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 2.2273.0 GPS week: 2273 Day: 0 MJD: 60155
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 -41 -26 3 -.01 17 15 | 20103 270 2933 8701
esa n/a| -1 -4 4 0 7 39 -.19 36 18 | -16627 1438 3033 6860
gfz n/a| 0 1 -1 17 16 42 -.20 21 15 | 0 69 2929 8278
grg n/a| 1 1 0 13 -2 -64 .37 23 17 | -16930 -149 2918 7933
jgx n/a| 0 0 0 45 13 -5 -.30 33 33 | 20275 394 2851 8608
Table 2.2273.1 GPS week: 2273 Day: 1 MJD: 60156
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 0 14 -6 38 .00 18 17 | 37540 -123 3268 8170
esa n/a| 0 -1 1 0 14 19 -.27 32 20 | -8920 1172 3247 6628
gfz n/a| 0 0 -1 -6 0 35 -.25 22 15 | 0 -267 3306 7780
grg n/a| 3 0 -3 -13 1 -95 .39 21 17 | -298 -56 3311 7362
jgx n/a| 0 0 3 47 16 72 -.30 31 31 | 37953 -403 3325 7841
Table 2.2273.2 GPS week: 2273 Day: 2 MJD: 60157
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 0 -11 -14 29 .04 19 16 | 37616 -1143 2768 8489
esa n/a| 0 -1 -1 -12 -10 35 -.25 31 21 | -2992 251 2744 7511
gfz n/a| 0 0 -1 10 12 67 -.15 21 13 | 0 -1027 2782 8096
grg n/a| 2 0 0 -3 13 -126 .40 23 19 | 296 -1095 2768 7867
jgx n/a| 2 2 6 7 36 157 -.50 38 38 | 37416 -1865 2799 8248
Table 2.2273.3 GPS week: 2273 Day: 3 MJD: 60158
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 -4 -17 54 .01 21 17 | 20684 -1347 3383 7450
esa n/a| 0 0 0 4 -13 -2 -.36 32 22 | -8657 -1416 3376 7290
gfz n/a| 0 2 0 12 26 5 -.21 23 17 | 0 -955 3388 7392
grg n/a| 2 -1 0 -20 -7 -59 .38 20 17 | -15379 -1406 3388 6813
jgx n/a| 0 0 4 34 2 153 -.43 36 36 | 20696 -890 3391 7249
Table 2.2273.4 GPS week: 2273 Day: 4 MJD: 60159
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 14 -10 62 -.04 24 17 | 36636 251 3310 8067
esa n/a| 0 -1 2 -8 21 28 -.41 32 23 | 1071 1300 3301 6672
gfz n/a| 1 3 0 16 3 9 -.22 29 17 | 0 -75 3345 7499
grg n/a| 2 -2 2 -10 2 -68 .48 27 20 | -297 334 3340 7004
jgx n/a| 0 1 1 33 30 114 -.34 35 35 | 37542 -254 3355 7231
Table 2.2273.5 GPS week: 2273 Day: 5 MJD: 60160
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 -4 12 -32 -8 .11 25 18 | 36940 -653 2584 9572
esa n/a| -1 -1 -1 -29 -1 15 -.17 36 22 | 11173 584 2585 11444
gfz n/a| 0 0 -2 -2 6 -1 -.10 18 12 | 0 441 2572 8629
grg n/a| 1 0 7 -4 19 -56 .40 50 27 | -11 -113 2642 7886
jgx n/a| 0 0 8 57 1 2 -.15 28 26 | 37818 82 2552 8368
Table 2.2273.6 GPS week: 2273 Day: 6 MJD: 60161
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 1 1 2 -35 -1 .09 19 16 | 19176 -4869 3308 10002
esa n/a| -3 1 5 13 6 52 -.32 35 23 | -9450 -4231 3284 8126
gfz n/a| -1 1 0 31 9 14 -.22 22 16 | 0 -4692 3263 9420
grg n/a| 5 -2 -1 -29 19 -61 .37 26 19 | -16145 -5029 3222 9114
jgx n/a| -1 0 11 45 24 -11 -.33 39 37 | 19604 -5319 3303 9513
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 3.2273.0 GPS week: 2273 Day: 0 MJD: 60155
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1449 22 48 37 19 36 18 | 59 70 77 56 57 59
R02E | 1361 7 14 11 9 --- 6 | 40 44 41 46 --- 41
R03E | 2069 10 14 12 13 12 7 | 112 115 111 119 115 113
R04E | 2888 9 14 12 17 15 7 | 77 80 78 83 79 79
R05E | 1720 11 15 13 14 20 7 | 123 115 120 122 130 120
R07E | 686 12 16 13 12 19 7 | 156 162 158 157 163 157
R08E | 1244 7 14 18 16 20 8 | 49 48 57 55 47 51
R09 | 1585 16 10 12 14 16 8 | 32 30 36 40 32 33
R11 | 1439 9 12 12 17 19 7 | 28 27 29 37 35 28
R12 | 816 8 9 12 9 13 5 | 30 33 33 34 32 30
R13 | 980 15 26 18 34 66 13 | 32 32 33 30 48 28
R14 | 586 9 8 13 9 13 6 | 34 30 38 32 32 33
R15 | 1026 12 11 23 11 14 9 | 43 43 41 42 40 40
R16 | 1189 21 25 21 12 13 11 | 41 53 53 46 42 44
R17 | 888 16 15 11 27 --- 10 | 90 79 90 91 --- 88
R18 | 1394 13 32 15 20 15 11 | 98 102 96 102 97 97
R19 | 1087 30 87 49 52 49 31 | 114 88 127 111 88 106
R20 | 1434 42 111 44 55 93 36 | 118 70 125 106 84 98
R21 | 1573 13 14 15 12 25 8 | 106 98 102 101 93 101
R22 | 2786 12 12 8 16 11 7 | 88 92 89 89 86 88
R24 | 1907 7 16 13 15 9 7 | 63 67 69 66 60 65
XR25 |23988 6 13 --- --- --- 9 | 48 49 --- --- --- 49
------+------------------------------------+--------------------------------
RMS | 1549 17 36 21 23 33 |T 71 69 76 74 71 70
WRMS | 1549 15 18 15 17 33 |NE 64 59 68 66 59 61
MEDI | 1394 12 14 13 15 16 |MD 59 67 77 66 60 59
Table 3.2273.1 GPS week: 2273 Day: 1 MJD: 60156
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 879 31 55 28 14 37 19 | 62 68 74 58 57 60
R02E | 936 9 12 15 9 --- 6 | 35 33 40 41 --- 36
R03E | 2508 11 14 10 12 25 7 | 134 128 124 130 130 129
R04E | 2900 8 11 14 18 23 7 | 85 83 84 88 79 84
R05E | 1228 9 14 15 16 19 8 | 128 127 124 125 123 126
R07E | 983 12 18 9 13 11 7 | 154 152 154 160 145 155
R08E | 873 8 16 15 14 20 7 | 40 45 42 51 46 42
R09 | 746 8 10 16 11 12 7 | 26 27 32 26 22 26
R11 | 1320 15 16 8 7 11 7 | 19 16 17 20 19 15
R12 | 842 22 19 26 16 13 12 | 18 34 41 19 19 21
R13 | 1264 37 32 30 38 56 20 | 39 38 40 17 32 22
R14 | 705 5 10 15 13 16 6 | 19 18 23 19 21 17
R15 | 561 18 10 18 11 11 9 | 24 29 30 26 24 24
R16 | 832 13 26 15 25 18 11 | 26 45 36 37 32 30
R17 | 1023 12 15 18 30 --- 11 | 66 62 72 81 --- 69
R18 | 1273 9 23 14 16 26 9 | 73 66 63 69 74 67
R19 | 1179 17 64 45 36 52 24 | 72 67 67 64 59 64
R20 | 1488 45 91 47 41 74 32 | 60 47 60 46 47 44
R21 | 1295 9 22 25 20 29 11 | 70 71 83 72 66 72
R22 | 2865 12 9 15 15 14 7 | 61 62 63 62 57 61
R24 | 2008 13 18 12 17 15 8 | 41 44 39 44 45 40
XR25 |22596 7 14 --- --- --- 10 | 26 35 --- --- --- 28
------+------------------------------------+--------------------------------
RMS | 1478 18 32 22 21 31 |T 58 58 62 59 57 56
WRMS | 1478 17 20 15 17 31 |NE 42 44 47 43 39 40
MEDI | 1179 12 16 15 16 19 |MD 41 45 60 51 47 42
Table 3.2273.2 GPS week: 2273 Day: 2 MJD: 60157
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1250 33 54 39 29 38 22 | 76 77 103 87 82 81
R02E | 1033 8 20 15 12 --- 8 | 37 37 38 43 --- 36
R03E | 2887 20 14 15 13 21 9 | 90 78 75 83 72 81
R04E | 3453 15 15 11 12 28 7 | 105 117 107 109 125 108
R05E | 1319 14 11 11 25 21 9 | 95 89 91 80 86 88
R07E | 1109 16 15 15 18 25 9 | 107 96 99 102 96 100
R08E | 2409 9 16 10 14 17 7 | 45 47 55 53 44 48
R09 | 735 13 16 20 23 15 10 | 22 23 28 33 22 22
R11 | 1596 16 13 11 9 14 7 | 21 25 31 27 27 24
R12 | 1211 10 13 9 16 18 7 | 19 20 19 20 22 17
R13 | 2069 18 30 22 44 47 17 | 26 39 28 22 27 22
R14 | 584 8 10 9 11 10 5 | 22 24 20 25 20 21
R15 | 1060 17 19 16 14 22 9 | 28 24 34 27 27 26
R16 | 1449 22 15 14 14 15 9 | 28 34 30 25 33 25
R17 | 1168 13 14 8 14 --- 7 | 71 68 74 67 --- 69
R18 | 1011 11 20 11 24 25 10 | 91 94 92 97 99 92
R19 | 1649 25 62 47 29 49 24 | 81 59 106 65 72 76
R20 | 4729 40 91 45 50 120 33 | 79 62 98 63 86 70
R21 | 1123 17 18 17 21 31 10 | 84 81 86 90 87 84
R22 | 2983 16 10 9 22 23 8 | 73 72 68 79 78 72
R24 | 1779 19 15 11 14 17 8 | 34 37 38 49 33 37
XR25 |13701 9 18 --- --- --- 13 | 28 31 --- --- --- 28
------+------------------------------------+--------------------------------
RMS | 2010 19 31 21 23 38 |T 57 56 62 59 59 55
WRMS | 2010 16 21 13 19 38 |NE 47 46 53 49 48 45
MEDI | 1319 16 15 14 16 22 |MD 45 47 68 63 72 48
Table 3.2273.3 GPS week: 2273 Day: 3 MJD: 60158
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1243 33 51 41 30 34 22 | 87 112 105 86 97 91
R02E | 955 9 15 18 18 --- 9 | 40 42 51 50 --- 43
R03E | 2172 11 15 18 19 30 9 | 188 188 193 190 195 189
R04E | 1885 15 17 12 12 34 8 | 117 124 120 124 124 120
R05E | 1977 17 12 10 16 27 8 | 142 137 142 148 155 142
R07E | 842 18 11 15 16 27 9 | 198 198 202 207 194 201
R08E | 1797 15 23 20 16 20 10 | 40 27 37 42 28 33
R09 | 565 13 9 11 19 17 8 | 18 18 21 23 19 17
R11 | 1333 10 14 12 9 14 6 | 18 25 23 18 23 18
R12 | 1495 16 14 13 12 22 8 | 22 28 26 25 31 22
R13 | 1929 25 35 30 33 49 17 | 24 32 34 29 35 25
R14 | 1326 11 7 13 11 20 6 | 22 20 33 22 22 24
R15 | 1345 21 21 16 12 19 10 | 23 32 36 25 21 24
R16 | 997 21 19 20 15 19 11 | 26 40 44 25 28 29
R17 | 1256 9 13 12 11 --- 6 | 72 65 74 74 --- 70
R18 | 970 12 25 23 14 23 11 | 64 71 57 57 47 60
R19 | 3545 48 66 24 33 37 25 | 95 71 90 66 72 75
R20 | 4674 36 96 67 39 108 35 | 75 35 123 67 36 72
R21 | 974 19 14 10 21 33 10 | 53 40 42 52 45 45
R22 | 3444 15 11 12 15 21 8 | 45 52 61 64 61 55
R24 | 1406 17 18 13 18 22 9 | 29 38 33 45 29 33
XR25 |20364 11 17 --- --- --- 14 | 29 27 --- --- --- 26
------+------------------------------------+--------------------------------
RMS | 1987 21 32 23 20 36 |T 64 64 73 68 66 64
WRMS | 1987 17 22 17 17 36 |NE 41 39 49 42 36 39
MEDI | 1345 15 15 15 16 23 |MD 40 40 51 52 36 43
Table 3.2273.4 GPS week: 2273 Day: 4 MJD: 60159
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 768 47 45 48 60 39 29 | 98 87 98 111 89 90
R02E | 834 13 19 22 16 --- 10 | 38 38 52 49 --- 41
R03E | 2398 18 22 24 21 28 12 | 118 138 128 118 134 123
R04E | 915 15 13 13 12 27 7 | 80 72 74 82 73 76
R05E | 2072 14 14 15 13 32 8 | 80 79 83 79 81 79
R07E | 1250 15 14 16 26 16 11 | 123 127 125 129 122 125
R08E | 2997 17 11 20 18 17 9 | 73 65 80 71 72 70
R09 | 1119 12 13 14 10 24 7 | 21 29 31 28 27 24
R11 | 796 14 14 21 16 11 9 | 14 17 25 29 16 18
R12 | 1475 17 17 12 12 15 8 | 16 40 33 19 25 23
R13 | 716 22 32 32 50 62 20 | 25 30 32 26 18 23
R14 | 1595 8 13 11 11 15 6 | 22 22 19 25 19 21
R15 | 725 17 13 22 15 16 10 | 29 31 40 31 23 30
R16 | 613 22 15 23 16 17 11 | 20 36 43 27 25 25
R17 | 877 23 10 20 10 --- 10 | 64 56 55 67 --- 58
R18 | 917 10 29 32 9 22 12 | 103 105 104 113 115 105
R19 | 1205 52 67 45 32 39 29 | 102 66 94 82 84 80
R20 | 2499 56 98 75 55 88 41 | 85 41 86 54 69 52
R21 | 837 18 16 20 27 41 12 | 81 72 80 71 86 74
R22 | 3984 12 21 18 19 17 10 | 78 73 70 85 81 75
R24 | 972 11 17 14 22 34 9 | 34 33 32 42 25 32
XR25 |19793 9 15 --- --- --- 12 | 20 33 --- --- --- 25
------+------------------------------------+--------------------------------
RMS | 1655 24 32 29 27 35 |T 60 58 65 63 62 57
WRMS | 1655 17 23 17 20 35 |NE 47 45 53 49 47 44
MEDI | 972 15 15 20 16 24 |MD 64 41 70 67 72 52
Table 3.2273.5 GPS week: 2273 Day: 5 MJD: 60160
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 908 42 62 25 34 45 23 | 102 108 114 114 107 106
R02E | 972 26 24 9 83 --- 20 | 84 79 87 135 --- 87
R03E | 1644 29 20 14 62 19 17 | 188 186 187 197 185 185
R04E | 1260 17 14 15 72 17 17 | 113 109 110 128 105 109
R05E | 1597 15 14 13 67 24 16 | 130 136 131 129 135 128
R07E | 886 25 20 12 82 17 20 | 171 168 158 184 166 163
R08E | 4021 24 17 23 109 21 25 | 88 87 81 138 90 85
R09 | 2773 11 7 7 9 15 5 | 24 23 22 25 19 21
R11 | 774 16 12 8 18 10 7 | 18 21 18 27 23 18
R12 | 994 7 12 9 19 17 6 | 15 20 20 27 22 16
R13 | 672 18 22 18 70 53 18 | 29 49 44 20 51 34
R14 | 1459 7 14 11 18 6 7 | 18 26 29 21 25 23
R15 | 894 24 7 15 15 24 9 | 25 26 27 22 33 23
R16 | 619 26 18 14 17 28 11 | 23 44 40 25 30 29
R17 | 819 16 12 13 15 --- 8 | 43 38 41 46 --- 40
R18 | 851 11 31 24 18 22 13 | 52 49 52 59 59 50
R19 | 586 47 82 30 44 47 30 | 75 43 60 63 59 55
R20 | 2229 56 106 39 47 37 37 | 71 63 64 52 64 52
R21 | 1326 17 17 9 23 28 9 | 60 63 57 61 58 58
R22 | 3891 15 17 8 26 13 9 | 71 77 78 70 73 72
R24 | 918 13 14 12 22 26 8 | 44 40 45 48 34 42
XR25 |16085 3 --- --- --- --- 0 | 23 --- --- --- --- 20
------+------------------------------------+--------------------------------
RMS | 1733 25 36 18 50 28 |T 66 69 69 75 70 64
WRMS | 1733 18 22 12 27 26 |NE 39 41 42 40 42 36
MEDI | 972 17 17 13 26 22 |MD 52 49 57 59 59 50
Table 3.2273.6 GPS week: 2273 Day: 6 MJD: 60161
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1716 42 59 32 34 44 24 | 106 114 112 101 96 103
R02E | 728 18 19 16 43 --- 15 | 109 118 115 129 --- 113
R03E | 822 11 25 15 27 32 11 | 132 126 125 149 128 132
R04E | 1385 9 18 14 30 36 11 | 100 106 99 98 109 98
R05E | 1347 11 21 16 41 23 14 | 110 104 102 131 108 110
R07E | 926 10 19 13 18 26 8 | 144 143 141 142 139 142
R08E | 4089 12 16 18 27 38 11 | 125 115 122 125 119 120
R09 | 2670 11 13 15 10 24 7 | 28 30 37 35 34 31
R11 | 933 12 24 12 13 18 8 | 30 29 33 33 31 29
R12 | 1043 14 13 19 18 28 9 | 34 38 42 38 35 35
R13 | 660 21 38 23 25 66 15 | 36 34 39 37 51 35
R14 | 1528 10 10 11 10 10 6 | 30 33 33 35 30 31
R15 | 1307 10 13 11 7 22 6 | 38 42 48 38 42 39
R16 | 941 20 22 13 9 29 9 | 36 54 44 38 47 38
R17 | 885 11 15 15 17 --- 8 | 58 48 56 55 --- 53
R18 | 846 14 25 12 19 22 10 | 67 78 72 78 73 71
R19 | 792 35 77 46 37 73 28 | 93 51 101 67 50 74
R20 | 1358 36 100 57 53 85 35 | 92 73 104 71 73 77
R21 | 1630 20 19 17 17 17 10 | 89 90 91 86 84 87
R22 | 3501 13 15 12 20 15 8 | 96 101 97 93 99 96
R24 | 958 12 13 12 15 26 7 | 65 65 62 70 60 64
XR25 |11750 10 20 --- --- --- 15 | 41 46 --- --- --- 41
------+------------------------------------+--------------------------------
RMS | 1686 19 35 22 26 39 |T 75 74 79 78 74 73
WRMS | 1686 16 23 16 19 37 |NE 55 54 61 55 54 53
MEDI | 1043 12 19 15 19 26 |MD 67 65 91 71 73 71
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