[IGSREPORT-29321] Wk 2260 IGLOS Final Orbits
acc
acc at igs.org
Mon May 22 06:52:58 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2260 (Apr 30, 2023 - May 06, 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 2.2260.
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:
igl2260[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2260 in the SP3 format.
igl22607.sum Combination Report for GPS Week 2260.
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. 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.
3. 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).
4. 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
5. 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 | -0.2 ns
1 | -1.0 ns
2 | 1.7 ns
3 | 0.2 ns
4 | 0.0 ns
5 | -0.8 ns
6 | 0.7 ns
6. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ALL | R01
0 | ESA | R20 R22
1 | ESA | R20 R22
2 | ESA | R20 R22
3 | ESA | R20 R22
4 | ALL | R25
4 | ESA | R20 R22
5 | ALL | R25
5 | ESA | R22
6 | ALL | R25
6 | ESA | R20 R22
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 1.2260, 1a.2260).
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 2.2260.0-6)
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 3.2260.0-6).
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 2260 summary. (Apr 30, 2023 - May 06, 2023)
Table 1.2260.a GPS week : 2260 MJD: 60064.0-60070.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 0 -20 29 .01 17 15 | 40471 615 3444 8880
| 1 0 1 9 8 22 .05 | 1893 2210
esa n/a| 0 0 3 -11 14 -33 -.04 46 25 | -2677 1542 3386 8573
| 1 1 1 9 12 18 .04 | 9990 1785
gfz n/a| 0 0 -5 17 -11 -31 -.04 22 16 | 0 402 3408 8730
| 1 1 2 14 13 17 .05 | 0 2075
grg n/a| 0 0 1 -9 38 31 .10 24 18 | -293 334 3434 8178
| 2 1 2 17 8 35 .04 | 406 1968
iac n/a| -1 0 -5 -1 3 -18 -.19 26 23 | 1887 -281 3409 9255
| 2 1 3 22 44 66 .07 | 675 911
Table 1.2260.b GPS week : 2260 MJD: 60064.0-60070.0
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 | --- 17 14 17 17 17 17 |
R02 | 8 6 9 7 7 8 7 |
R03 | 9 7 7 7 8 8 7 |
R04 | 8 7 9 6 9 8 10 |
R05 | 10 7 7 6 6 8 9 |
R07 | 8 8 6 6 8 10 9 |
R08 | 8 9 6 7 6 8 8 |
R09 | 8 9 8 8 8 9 9 |
R11 | 8 8 7 6 6 8 8 |
R12 | 13 8 10 10 11 13 12 |
R13 | 20 19 17 15 19 24 23 |
R14 | 12 12 10 9 9 8 9 |
R15 | 9 12 10 9 9 11 9 |
R16 | 19 21 19 21 21 22 15 |
R17 | 7 7 10 10 8 8 10 |
R18 | 9 8 10 8 10 11 8 |
R19 | 21 20 22 24 25 25 29 |
R20 | 24 16 18 25 27 44 24 |
R21 | 11 10 7 8 12 10 10 |
R22 | 23 13 18 19 29 23 15 |
R24 | 11 9 7 9 10 10 12 |
R25 | 0 0 0 --- --- --- --- |
Table 1.2260.c GPS week : 2260 MJD: 60064.0-60070.0
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 2260 0 | -26 -98 188 1275 -133 -2984 80.3 1522 1522 | -188 0
brd 2260 1 | 32 63 177 261 74 -832 80.6 1527 1527 | -1018 0
brd 2260 2 | -54 63 257 -774 2092 4480 81.2 1331 1331 | 1668 0
brd 2260 3 | 11 56 119 -313 1795 7033 81.3 1747 1747 | 178 0
brd 2260 4 | -88 -84 146 126 365 4371 81.4 1732 1732 | 16 0
brd 2260 5 | 12 25 201 753 245 -257 80.7 1620 1620 | -839 0
brd 2260 6 | -47 -65 221 -403 -524 1358 79.1 1691 1691 | 684 0
-------------+------------------------------------------------------------+----------------
brd 2260 mean| -23 -5 187 131 559 1881 80.7 1595 1595 | 71 0
brd 2260 sdev| 43 74 46 709 991 3544 .8 147 147 | 914 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 2.2260.0 GPS week: 2260 Day: 0 MJD: 60064
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 16 -10 76 .02 18 15 | 37269 2269 3636 9128
esa n/a| 2 -1 5 0 9 -22 -.09 51 27 | -20871 2667 3663 8744
gfz n/a| 2 1 -7 17 -10 -28 .03 22 14 | 0 1101 3652 8605
grg n/a| -2 1 2 -33 54 -29 .09 24 18 | -1134 1594 3629 8031
iac n/a| 0 0 -6 -12 -76 -79 -.28 23 20 | 1412 -138 3575 9122
Table 2.2260.1 GPS week: 2260 Day: 1 MJD: 60065
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 1 -3 -14 28 .01 14 12 | 39148 -2125 3539 8914
esa n/a| 3 -2 5 -22 0 -58 -.07 45 28 | -6200 -396 3192 7889
gfz n/a| 1 0 -4 9 4 -3 -.02 21 19 | 0 -2551 3514 8263
grg n/a| -3 -2 0 10 29 11 .11 23 16 | 53 -2545 3608 7743
iac n/a| -1 0 -12 -6 -5 78 -.27 26 22 | 1186 -2090 3521 8803
Table 2.2260.2 GPS week: 2260 Day: 2 MJD: 60066
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 9 -11 17 -.01 16 14 | 39389 3869 3441 8504
esa n/a| 1 1 2 -21 8 -41 -.05 48 23 | -3371 4525 3386 7380
gfz n/a| 0 2 -2 18 -35 -31 -.02 22 16 | 0 3606 3348 8353
grg n/a| 1 -2 -3 4 36 56 .11 19 14 | -47 3198 3378 7560
iac n/a| 0 0 -3 -14 21 13 -.17 24 22 | 2177 932 3381 8974
Table 2.2260.3 GPS week: 2260 Day: 3 MJD: 60067
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 0 -30 23 -.06 16 15 | 42212 -225 3137 8628
esa n/a| 0 0 2 -9 33 -14 -.05 46 23 | 329 1195 3122 8258
gfz n/a| 0 0 -3 31 0 -51 -.01 23 15 | 0 343 3109 8472
grg n/a| 1 0 0 -33 42 17 .10 20 15 | -31 -17 3110 7927
iac n/a| 1 -1 -3 27 26 -89 -.11 26 21 | 2160 -351 3124 8989
Table 2.2260.4 GPS week: 2260 Day: 4 MJD: 60068
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 -6 -27 18 -.02 18 15 | 42037 66 3215 8888
esa n/a| -1 0 4 -19 29 -49 .01 48 24 | 2967 670 3306 9186
gfz n/a| -2 0 -2 36 -7 -27 -.02 22 12 | 0 -452 3247 9304
grg n/a| 3 0 1 -12 32 81 .07 26 20 | -235 -152 3306 8839
iac n/a| -3 0 -1 0 -17 -29 -.15 29 26 | 2006 -180 3297 9796
Table 2.2260.5 GPS week: 2260 Day: 5 MJD: 60069
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 -8 -27 8 .05 19 18 | 41308 -1669 3835 8814
esa n/a| -1 -2 4 -7 12 -39 .00 39 22 | -3521 -327 3782 8993
gfz n/a| 0 0 -9 10 -8 -23 -.10 26 17 | 0 -1295 3766 8916
grg n/a| 0 2 3 1 33 46 .06 30 23 | -449 -1408 3789 8275
iac n/a| -5 2 -3 -32 10 -71 -.15 30 27 | 1208 -317 3792 9310
Table 2.2260.6 GPS week: 2260 Day: 6 MJD: 60070
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -1 -3 -21 33 .10 21 17 | 41939 2122 3308 9286
esa n/a| 0 0 1 1 6 -10 -.04 48 27 | 11928 2461 3252 9561
gfz n/a| 0 1 -5 -5 -21 -54 -.12 20 15 | 0 2063 3220 9203
grg n/a| -1 -1 5 -3 40 36 .17 27 20 | -212 1669 3221 8875
iac n/a| 0 0 -4 30 68 50 -.22 24 23 | 3063 172 3179 9796
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 3.2260.0 GPS week: 2260 Day: 0 MJD: 60064
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R02 | 807 9 14 14 19 16 8 | 59 60 56 65 64 58
R03 | 700 18 11 11 22 15 9 | 60 66 70 79 68 67
R04 | 552 15 9 14 14 18 7 | 55 46 46 50 45 49
R05 | 1177 21 12 13 18 23 9 | 50 44 42 47 48 44
R07 | 1130 16 13 13 12 15 8 | 57 63 66 59 57 59
R08 | 1331 14 16 11 15 22 8 | 49 61 60 55 57 54
R09E | 3178 13 10 12 21 15 8 | 44 45 42 40 45 41
R11E | 1228 12 16 10 16 16 8 | 29 40 37 31 34 31
R12E | 3661 12 17 19 38 22 12 | 86 95 91 99 107 90
R13E | 1082 25 37 37 38 31 20 | 55 56 69 66 64 55
R14E | 733 7 22 19 33 12 12 | 107 95 99 114 100 101
R15E | 1954 10 17 12 23 18 9 | 77 75 77 75 77 74
R16E | 941 23 30 47 24 19 18 | 100 85 108 97 94 95
R17 | 734 8 15 13 13 22 7 | 68 59 70 67 70 65
R18 | 623 13 12 18 19 13 9 | 55 63 63 57 60 58
R19 | 648 42 35 20 39 36 20 | 86 55 90 75 67 74
R20 | 913 28 205 40 35 57 24 | 124 71 143 127 109 127
R21 | 813 13 24 18 18 10 10 | 65 47 72 66 71 62
XR22 | 1693 --- 351 19 27 16 23 | --- 136 55 68 62 58
R24 | 1958 10 25 22 12 16 10 | 70 57 75 72 70 67
XR25 | 9706 4 --- --- --- 26 0 | 257 --- --- --- 227 33
------+------------------------------------+--------------------------------
RMS | 1521 18 51 22 24 23 |T 77 65 70 70 75 64
WRMS | 1521 15 27 14 18 20 |NE 80 62 69 68 75 62
MEDI | 1082 13 16 14 19 18 |MD 65 60 69 67 64 59
Table 3.2260.1 GPS week: 2260 Day: 1 MJD: 60065
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1367 31 38 21 25 53 17 | 53 88 84 70 51 70
R02 | 460 5 13 8 13 18 5 | 31 39 26 36 35 31
R03 | 1037 10 12 7 18 15 7 | 33 31 36 44 41 35
R04 | 558 10 7 17 12 23 7 | 28 39 41 35 31 32
R05 | 1422 10 12 11 15 14 7 | 28 30 24 22 26 25
R07 | 1129 7 12 17 19 16 8 | 34 34 29 34 24 31
R08 | 1604 18 13 19 9 15 9 | 29 43 43 32 32 35
R09E | 2631 13 14 17 17 17 9 | 39 50 39 50 40 41
R11E | 1479 11 14 15 16 16 8 | 23 31 35 25 24 26
R12E | 2956 11 14 15 17 28 8 | 70 69 72 68 58 68
R13E | 837 23 40 39 31 50 19 | 50 51 68 54 53 48
R14E | 2134 7 25 13 32 15 11 | 53 57 56 58 55 52
R15E | 1635 11 22 16 34 25 12 | 58 53 70 83 55 63
R16E | 1233 19 39 52 35 21 21 | 55 57 67 64 58 55
R17 | 884 7 18 8 12 16 6 | 35 28 28 42 33 32
R18 | 532 13 15 14 13 17 8 | 36 41 28 45 37 35
R19 | 521 22 47 17 46 20 19 | 52 44 53 60 48 50
R20 | 1250 16 175 26 25 49 15 | 58 48 58 66 51 59
R21 | 620 8 26 20 11 16 9 | 46 40 54 49 51 47
XR22 | 1065 --- 361 11 14 36 12 | --- 100 37 41 44 36
R24 | 2583 8 16 21 16 22 9 | 33 30 36 41 32 32
XR25 | 8078 2 --- --- --- 30 0 | 292 --- --- --- 246 19
------+------------------------------------+--------------------------------
RMS | 1526 14 45 21 23 26 |T 54 47 46 48 51 41
WRMS | 1526 12 28 19 16 22 |NE 56 45 41 44 52 37
MEDI | 1233 11 16 17 17 18 |MD 39 43 41 45 41 35
Table 3.2260.2 GPS week: 2260 Day: 2 MJD: 60066
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1225 24 32 22 20 21 14 | 65 57 69 64 64 49
R02 | 498 8 11 19 21 32 9 | 50 54 59 52 70 51
R03 | 802 12 11 16 10 17 7 | 53 59 61 58 68 57
R04 | 690 11 22 13 13 14 8 | 50 39 44 50 46 45
R05 | 1186 14 13 12 9 13 7 | 47 40 43 42 38 42
R07 | 764 7 11 10 10 13 5 | 50 44 44 46 49 46
R08 | 1329 12 7 10 9 19 5 | 44 42 43 47 48 43
R09E | 2516 9 15 17 12 17 7 | 61 61 70 53 65 61
R11E | 2064 9 13 15 10 26 6 | 46 51 52 44 55 47
R12E | 791 11 19 15 22 25 10 | 93 99 95 83 80 91
R13E | 948 25 35 37 18 49 16 | 46 51 72 61 53 51
R14E | 1523 9 21 8 24 14 9 | 32 38 35 43 32 33
R15E | 1436 10 19 14 25 19 10 | 45 55 51 42 49 45
R16E | 1233 20 31 51 23 21 19 | 34 56 53 41 35 40
R17 | 1008 8 23 24 9 12 9 | 57 55 72 65 61 61
R18 | 552 15 15 20 15 15 9 | 56 56 60 69 54 58
R19 | 544 37 39 27 45 16 22 | 68 54 69 64 55 61
R20 | 2273 21 193 30 23 49 17 | 88 66 110 95 72 95
R21 | 654 8 18 12 10 31 7 | 54 52 58 56 67 54
XR22 | 1282 --- 359 18 18 31 18 | --- 152 48 61 50 53
R24 | 1888 11 12 12 11 18 6 | 60 55 55 60 55 57
XR25 | 7206 2 --- --- --- 16 0 | 234 --- --- --- 164 35
------+------------------------------------+--------------------------------
RMS | 1331 16 48 22 19 24 |T 63 58 60 56 60 53
WRMS | 1331 14 23 16 14 22 |NE 69 58 59 59 64 53
MEDI | 1186 11 19 16 15 18 |MD 53 55 58 56 55 51
Table 3.2260.3 GPS week: 2260 Day: 3 MJD: 60067
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 991 33 41 23 17 27 17 | 67 35 54 49 55 40
R02 | 766 10 12 16 9 38 7 | 42 51 58 44 69 48
R03 | 990 12 9 15 11 13 7 | 55 60 68 63 65 61
R04 | 880 10 14 10 9 16 6 | 43 40 38 47 40 42
R05 | 973 10 7 11 7 23 5 | 41 41 37 41 55 39
R07 | 864 10 11 9 11 31 6 | 44 48 47 49 53 46
R08 | 734 9 15 11 14 19 7 | 40 40 43 46 40 41
R09E | 3211 10 16 16 11 11 7 | 21 26 28 17 32 20
R11E | 2844 8 11 11 11 14 6 | 26 31 33 27 34 28
R12E | 1221 15 18 12 20 30 9 | 79 82 83 100 77 85
R13E | 1132 18 30 27 30 65 15 | 51 66 69 56 70 56
R14E | 857 9 20 9 23 15 9 | 38 44 37 43 42 37
R15E | 2538 13 15 10 19 13 8 | 52 53 63 71 57 58
R16E | 1044 20 39 53 25 21 20 | 35 54 51 41 32 38
R17 | 1216 8 21 19 22 11 10 | 40 42 49 40 41 40
R18 | 608 14 16 13 10 11 7 | 35 43 46 46 41 41
R19 | 511 33 43 36 49 21 23 | 58 41 66 58 40 51
R20 | 4727 22 181 51 30 39 25 | 95 68 88 96 67 90
R21 | 664 8 25 12 10 26 8 | 40 32 43 44 44 38
XR22 | 2477 --- 362 18 19 38 19 | --- 155 39 71 37 53
R24 | 1051 13 20 17 14 19 9 | 40 28 44 41 41 36
------+------------------------------------+--------------------------------
RMS | 1746 16 46 23 20 26 |T 47 51 51 51 49 47
WRMS | 1746 15 23 15 14 21 |NE 49 51 51 52 49 47
MEDI | 991 10 18 15 14 21 |MD 41 43 47 46 42 41
Table 3.2260.4 GPS week: 2260 Day: 4 MJD: 60068
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 709 28 37 26 20 27 16 | 61 39 56 51 40 48
R02 | 701 8 15 9 11 27 6 | 38 39 42 39 57 38
R03 | 813 15 14 4 14 13 7 | 42 59 49 52 56 48
R04 | 869 13 14 11 24 14 9 | 40 46 47 29 44 39
R05 | 1032 10 9 10 13 23 6 | 34 35 33 28 45 31
R07 | 1274 10 9 10 22 29 7 | 38 41 41 55 53 42
R08 | 631 10 11 8 11 18 6 | 39 45 40 42 40 40
R09E | 4023 11 12 11 21 50 8 | 30 30 36 44 52 31
R11E | 3646 11 10 13 8 19 6 | 20 32 31 28 22 26
R12E | 1615 13 13 16 30 20 10 | 65 65 64 64 56 62
R13E | 1115 23 38 37 34 65 19 | 47 68 61 54 103 50
R14E | 630 11 20 10 20 17 9 | 41 46 39 39 41 39
R15E | 2606 8 14 13 25 17 8 | 54 53 57 57 55 53
R16E | 849 24 26 55 25 25 20 | 38 35 64 47 43 42
R17 | 1744 8 18 11 15 10 7 | 36 28 37 39 31 33
R18 | 548 10 22 14 23 16 10 | 38 45 34 36 32 35
R19 | 1000 46 30 28 62 27 24 | 52 44 56 53 38 45
R20 | 2778 21 194 47 44 40 27 | 82 62 70 89 56 78
R21 | 639 11 34 13 17 29 11 | 42 35 37 44 47 38
XR22 | 3465 --- 364 23 34 15 28 | --- 118 39 71 38 50
R24 | 870 13 20 18 17 36 10 | 41 33 47 34 56 38
------+------------------------------------+--------------------------------
RMS | 1732 18 48 22 26 29 |T 62 47 46 47 67 43
WRMS | 1732 15 24 12 20 26 |NE 72 47 44 47 73 43
MEDI | 1000 11 18 13 21 23 |MD 41 44 42 44 45 40
Table 3.2260.5 GPS week: 2260 Day: 5 MJD: 60069
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 584 21 40 17 37 25 16 | 42 30 32 37 24 28
R02 | 673 12 20 13 11 17 8 | 30 21 22 27 29 22
R03 | 611 10 15 16 17 14 8 | 35 27 27 37 32 28
R04 | 737 12 8 9 22 26 8 | 31 34 34 24 40 29
R05 | 981 13 14 10 16 26 7 | 28 38 32 25 36 28
R07 | 1946 11 11 13 31 28 10 | 27 36 31 52 43 33
R08 | 630 13 9 9 20 21 7 | 22 33 24 43 35 28
R09E | 3439 13 10 19 15 55 8 | 53 51 52 53 64 51
R11E | 3493 12 13 15 14 15 8 | 23 25 21 25 23 20
R12E | 1467 11 16 29 30 13 13 | 56 53 68 52 52 54
R13E | 1654 27 54 55 24 45 24 | 68 64 126 90 65 81
R14E | 797 9 15 15 16 21 8 | 46 50 42 51 49 45
R15E | 2579 12 20 17 25 19 10 | 44 43 38 45 48 39
R16E | 1311 30 32 56 27 22 22 | 40 45 83 58 47 48
R17 | 1790 10 11 12 19 39 7 | 32 32 32 30 47 30
R18 | 727 8 22 19 23 22 10 | 28 39 40 33 38 31
R19 | 798 47 42 38 43 32 25 | 35 37 48 39 35 34
R20 | 1243 25 137 41 88 58 44 | 63 40 61 86 76 44
R21 | 675 8 30 13 18 17 10 | 37 28 41 46 34 38
XR22 | 3482 --- 355 21 24 22 22 | --- 63 63 45 50 50
R24 | 1136 18 15 20 11 31 10 | 46 39 37 46 55 41
------+------------------------------------+--------------------------------
RMS | 1619 19 39 26 30 30 |T 50 39 45 44 53 38
WRMS | 1619 18 22 17 23 27 |NE 51 35 37 40 54 33
MEDI | 1136 12 16 17 22 22 |MD 37 38 38 45 43 34
Table 3.2260.6 GPS week: 2260 Day: 6 MJD: 60070
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 642 26 43 10 33 21 17 | 75 55 71 73 59 59
R02 | 558 12 8 13 14 27 7 | 51 48 53 58 60 51
R03 | 672 12 8 14 10 20 6 | 59 59 60 70 68 61
R04 | 738 24 13 15 8 17 9 | 56 44 46 41 54 46
R05 | 679 10 15 14 18 19 8 | 44 49 44 36 61 42
R07 | 2338 5 13 17 19 26 8 | 54 51 50 66 63 54
R08 | 881 15 9 11 19 21 8 | 44 53 53 64 58 52
R09E | 3365 14 11 17 14 26 8 | 79 75 73 79 71 75
R11E | 3570 13 13 12 16 18 7 | 41 52 49 38 43 44
R12E | 1293 11 14 15 34 21 11 | 63 69 68 81 61 67
R13E | 1281 41 33 31 49 40 22 | 52 72 81 83 55 63
R14E | 964 14 12 14 18 18 8 | 70 68 63 66 68 66
R15E | 2338 15 13 14 21 23 9 | 65 72 71 63 64 67
R16E | 1182 20 27 35 17 21 15 | 59 62 67 69 60 61
R17 | 1715 8 19 22 12 23 9 | 54 40 64 50 62 52
R18 | 775 11 16 11 19 32 8 | 43 54 51 45 60 47
R19 | 984 43 55 37 67 32 29 | 92 43 80 64 68 66
R20 | 2546 34 189 26 39 26 23 | 128 48 132 142 128 129
R21 | 747 18 24 9 15 19 10 | 54 42 54 56 58 50
XR22 | 3684 --- 339 13 16 13 14 | --- 108 55 60 55 55
R24 | 1418 21 26 18 16 17 12 | 71 50 67 58 64 60
------+------------------------------------+--------------------------------
RMS | 1690 21 48 20 27 24 |T 69 57 64 64 70 60
WRMS | 1690 17 27 15 20 23 |NE 74 53 62 63 75 58
MEDI | 1182 14 15 14 18 21 |MD 59 53 63 64 61 59
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