[IGSREPORT-29363] Wk 2264 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 19 06:01:13 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2264 (May 28, 2023 - Jun 03, 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 2.2264.
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:
igl2264[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2264 in the SP3 format.
igl22647.sum Combination Report for GPS Week 2264.
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 | -13.6 ns
1 | -11.8 ns
2 | -13.7 ns
3 | -6.3 ns
4 | -5.9 ns
5 | -8.0 ns
6 | -10.7 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 | ESA | R20
2 | ALL | R24
2 | ESA | R20
2 | GRG | R09
3 | ALL | R24
3 | ESA | R20
4 | ESA | R20
6 | ESA | R20
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 1.2264, 1a.2264).
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 2.2264.0-6)
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 3.2264.0-6).
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 2264 summary. (May 28, 2023 - Jun 03, 2023)
Table 1.2264.a GPS week : 2264 MJD: 60092.0-60098.0
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 -7 -11 16 .06 18 15 | 15536 -793 3126 8868
| 0 0 1 16 13 11 .03 | 1701 2719
esa n/a| 0 0 0 -16 6 -31 -.18 43 25 | -12005 -628 3446 8845
| 0 0 2 13 16 15 .02 | 9312 2693
gfz n/a| 0 0 2 17 -12 -15 -.17 23 14 | 0 -1213 3432 9315
| 0 1 1 11 15 17 .03 | 0 3036
grg n/a| 3 0 -1 0 23 -12 .26 477 18 | -9848 -1383 3633 9013
| 0 1 2 27 16 17 .04 | 2405 2844
iac n/a| -1 0 0 6 -1 -35 -.25 23 23 | -8476 -342 3441 10071
| 0 1 2 33 34 66 .04 | 2793 1396
Table 1.2264.b GPS week : 2264 MJD: 60092.0-60098.0
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 | 23 19 16 21 22 21 23 |
R02 | 7 6 7 8 8 8 8 |
R03 | 6 9 7 7 8 7 6 |
R04 | 10 9 8 6 10 10 8 |
R05 | 7 14 8 7 8 8 7 |
R07 | 6 7 6 9 7 8 8 |
R08 | 8 7 7 10 9 6 6 |
R09 | 9 9 13 11 13 10 10 |
R11 | 7 9 9 8 8 10 8 |
R12 | 7 12 11 10 7 7 8 |
R13 | 22 23 24 28 24 21 18 |
R14 | 8 6 8 7 9 7 7 |
R15 | 10 8 8 7 7 6 6 |
R16 | 21 19 21 22 24 21 22 |
R17 | 7 6 7 5 7 6 6 |
R18 | 9 9 11 10 8 7 6 |
R19 | 24 28 24 23 25 20 25 |
R20 | 15 41 37 25 22 35 21 |
R21 | 8 10 8 9 8 6 7 |
R22 | 7 12 8 11 8 12 8 |
R24 | 12 0 --- --- 9 7 10 |
R25 | 11 13 14 18 0 19 11 |
Table 1.2264.c GPS week : 2264 MJD: 60092.0-60098.0
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 2264 0 | -31 -61 218 -322 2403 898 80.6 1610 1610 | -13566 0
brd 2264 1 | 52 -81 275 2384 1860 -2430 80.0 1246 1246 | -11779 0
brd 2264 2 | -50 -31 188 443 -398 -3191 80.7 1402 1402 | -13730 0
brd 2264 3 | 105 1 219 -1117 728 1656 80.5 1561 1561 | -6255 0
brd 2264 4 | -14 84 205 -2136 -2347 -1842 80.6 1501 1501 | -5878 0
brd 2264 5 | 14 42 152 11 -2737 -7742 81.1 1441 1441 | -8019 0
brd 2264 6 | -22 -22 272 -767 -1647 -8326 80.8 1595 1595 | -10662 0
-------------+------------------------------------------------------------+----------------
brd 2264 mean| 7 -9 218 -214 -305 -2996 80.6 1479 1479 | -9984 0
brd 2264 sdev| 54 57 44 1417 2040 3860 .3 128 128 | 3295 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 2.2264.0 GPS week: 2264 Day: 0 MJD: 60092
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 -22 -11 14 .07 17 13 | 16426 -1456 3576 8704
esa n/a| -2 -1 3 -25 -5 -35 -.16 45 26 | -28595 -908 3519 8510
gfz n/a| 0 0 0 29 -14 -32 -.16 21 12 | 0 -1361 3548 8192
grg n/a| 2 1 -1 23 48 -25 .29 23 19 | -12803 -1874 3532 7860
iac n/a| 0 -1 -1 2 -30 33 -.20 19 17 | -12153 754 3506 8775
Table 2.2264.1 GPS week: 2264 Day: 1 MJD: 60093
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 -15 -17 31 .02 20 16 | 15301 -907 3133 8597
esa n/a| 0 0 2 -17 -8 -9 -.16 37 25 | -21255 -707 3098 10308
gfz n/a| -1 1 0 1 -7 -22 -.18 26 15 | 0 12 3009 7795
grg n/a| 1 0 -1 46 22 -38 .20 26 21 | -11796 -373 2997 7373
iac n/a| -2 0 0 8 -6 -40 -.21 22 21 | -10436 31 3081 8510
Table 2.2264.2 GPS week: 2264 Day: 2 MJD: 60094
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 -8 -28 14 .11 19 14 | 14189 -4051 2880 9265
esa n/a| -1 0 -2 -30 -13 -29 -.17 47 23 | -6079 -4304 3090 6425
gfz n/a| -1 -1 4 28 4 -9 -.12 22 14 | 0 -5364 3091 8221
grg n/a| 1 1 -2 -6 34 4 .27 3202 20 | -11677 -5033 3982 7939
iac n/a| -1 -2 -2 -49 32 -131 -.27 22 24 | -10897 -1887 3107 9219
Table 2.2264.3 GPS week: 2264 Day: 3 MJD: 60095
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 23 -12 24 .08 19 15 | 16575 219 2655 8889
esa n/a| 0 -1 -2 -26 19 -58 -.22 49 25 | -2749 -205 3599 11436
gfz n/a| -1 0 3 23 -2 -7 -.18 23 15 | 0 -1656 3611 11979
grg n/a| 3 2 2 -31 11 -9 .23 24 16 | -6851 -2146 3887 11890
iac n/a| -2 0 0 4 37 -7 -.26 23 25 | -5962 -386 3589 12601
Table 2.2264.4 GPS week: 2264 Day: 4 MJD: 60096
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 0 3 15 0 .08 20 17 | 16030 4448 3050 8974
esa n/a| 0 0 1 6 3 -19 -.16 44 28 | -7992 4656 3847 10973
gfz n/a| 0 1 0 9 -34 -29 -.18 22 14 | 0 4544 3813 11248
grg n/a| 3 -1 0 -30 -4 12 .27 25 17 | -9117 4220 4013 11060
iac n/a| -1 -1 -1 28 -7 17 -.21 21 24 | -5646 1976 3848 11850
Table 2.2264.5 GPS week: 2264 Day: 5 MJD: 60097
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 -10 -16 5 .06 14 12 | 17668 -2986 3054 8605
esa n/a| 0 -1 1 -3 31 -41 -.21 39 24 | -8159 -1924 3286 8381
gfz n/a| 0 1 2 6 -2 18 -.21 24 15 | 0 -2930 3268 8823
grg n/a| 2 -2 -4 -4 27 -18 .27 23 17 | -6793 -2749 3304 8492
iac n/a| 0 -1 4 -9 20 -120 -.32 26 22 | -5446 -1749 3281 9773
Table 2.2264.6 GPS week: 2264 Day: 6 MJD: 60098
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 -20 -6 29 .04 16 14 | 12564 -823 3537 9047
esa n/a| 0 0 0 -19 16 -28 -.17 43 23 | -9208 -1004 3684 5884
gfz n/a| 0 0 2 21 -31 -25 -.16 23 15 | 0 -1738 3688 8951
grg n/a| 4 0 -4 3 28 -13 .29 20 14 | -9905 -1729 3721 8479
iac n/a| -2 0 3 60 -55 0 -.26 25 26 | -8797 -1133 3681 9773
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 3.2264.0 GPS week: 2264 Day: 0 MJD: 60092
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1040 35 72 18 25 21 23 | 102 42 86 92 87 81
R02 | 831 7 16 10 16 15 7 | 73 60 70 78 78 70
R03 | 1079 7 13 8 13 10 6 | 78 75 70 83 74 76
R04 | 772 12 12 11 26 17 9 | 76 73 66 61 63 68
R05 | 2243 13 12 8 13 17 6 | 71 68 67 61 65 66
R07 | 1599 12 11 11 8 25 6 | 78 77 86 83 100 80
R08 | 816 14 14 12 15 24 8 | 72 75 84 83 85 78
R09 | 1513 13 17 17 14 16 9 | 49 55 46 9999 53 48
R11 | 2160 12 10 11 10 14 6 | 135 137 127 134 134 133
R12 | 1461 8 19 10 11 10 7 | 59 75 61 67 64 63
R13 | 1368 15 47 51 32 21 22 | 88 57 113 63 77 79
R14 | 1182 11 14 11 16 14 7 | 59 67 63 66 68 62
R15 | 1084 14 19 9 24 13 9 | 66 65 54 55 62 58
R16 | 898 23 29 51 28 30 20 | 64 55 70 60 63 61
R17 | 1431 8 9 14 16 16 7 | 30 27 28 30 30 27
R18 | 696 11 24 8 19 13 9 | 29 27 27 32 21 26
R19 | 892 35 42 22 64 29 24 | 48 50 63 52 44 50
R20 | 1691 18 162 24 20 28 15 | 75 58 86 76 75 74
R21 | 730 9 19 12 17 18 8 | 38 34 39 45 36 38
XR22 | 2200 --- 11 8 8 26 6 | --- 47 52 59 39 52
R24 | 4353 28 21 16 14 18 12 | 40 26 9999 28 32 9999
XR25 |12167 9 13 --- --- 29 11 | 46 47 --- --- 44 45
------+------------------------------------+--------------------------------
RMS | 1609 17 45 21 23 19 |T 65 58 67 65 63 63
WRMS | 1609 13 26 12 19 17 |NE 65 58 67 65 63 63
MEDI | 1182 12 16 11 16 17 |MD 66 57 66 61 63 63
Table 3.2264.1 GPS week: 2264 Day: 1 MJD: 60093
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1454 30 51 20 26 27 18 | 73 47 67 57 71 61
R02 | 939 7 10 8 14 11 5 | 51 48 53 61 51 53
R03 | 880 12 12 20 12 31 8 | 61 57 45 57 46 54
R04 | 628 14 13 17 14 22 8 | 62 64 47 50 51 55
R05 | 1189 21 15 35 17 13 13 | 60 71 92 61 68 68
R07 | 997 8 14 11 13 27 6 | 65 62 72 70 81 67
R08 | 1130 13 8 13 11 28 7 | 58 68 75 68 80 66
R09 | 1909 10 15 22 10 14 8 | 46 52 44 9999 46 45
R11 | 2442 10 10 22 17 17 9 | 115 116 112 116 107 114
R12 | 1010 13 21 16 31 18 12 | 52 61 53 72 59 56
R13 | 1628 25 45 54 32 25 22 | 67 64 97 51 62 64
R14 | 1352 7 13 10 11 16 6 | 47 49 47 50 52 47
R15 | 1120 9 14 12 17 14 7 | 51 51 48 46 52 47
R16 | 874 19 27 55 24 26 19 | 48 44 38 47 43 42
R17 | 1111 11 10 10 9 20 5 | 22 17 18 19 15 18
R18 | 622 12 22 16 11 16 9 | 21 21 28 22 19 19
R19 | 621 47 50 20 64 27 27 | 33 46 46 44 30 39
R20 | 1407 42 124 48 59 35 40 | 45 35 47 32 30 44
R21 | 719 10 25 16 18 18 10 | 22 20 25 34 24 23
XR22 | 2806 --- 18 16 13 32 11 | --- 24 32 37 28 29
XR24 |10526 --- --- 3 --- 7157 0 | --- --- 9999 --- 73 9999
XR25 |11263 10 17 --- --- 28 13 | 24 28 --- --- 24 23
------+------------------------------------+--------------------------------
RMS | 1246 20 37 26 26 22 |T 51 49 54 52 50 49
WRMS | 1246 16 25 15 21 21 |NE 51 49 54 52 50 49
MEDI | 1120 12 15 16 14 22 |MD 51 49 47 50 51 47
Table 3.2264.2 GPS week: 2264 Day: 2 MJD: 60094
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1986 28 41 21 19 22 16 | 87 66 82 65 68 74
R02 | 729 8 8 13 14 17 6 | 65 64 72 63 66 65
R03 | 739 10 10 7 16 26 6 | 71 62 65 70 56 67
R04 | 525 17 12 13 7 32 7 | 73 61 61 71 46 66
R05 | 961 14 17 14 8 16 8 | 65 71 61 65 64 64
R07 | 787 7 10 9 12 30 5 | 77 70 77 75 90 74
R08 | 1049 8 9 15 14 31 7 | 71 72 77 79 93 73
R09 | 1980 15 24 15 >>>> 18 12 | 52 57 60 9999 61 54
R11 | 2937 15 14 14 17 15 8 | 102 97 100 95 103 98
R12 | 1253 10 18 15 26 11 10 | 57 66 67 49 53 57
R13 | 932 36 44 35 51 17 24 | 91 60 95 87 62 77
R14 | 974 14 16 12 13 9 8 | 61 63 69 65 61 63
R15 | 1569 9 15 14 16 14 8 | 61 57 70 59 66 60
R16 | 1589 22 33 56 23 20 20 | 58 53 71 60 57 57
R17 | 838 13 9 12 8 35 6 | 36 36 42 37 36 36
R18 | 561 11 28 13 21 13 10 | 33 35 38 44 30 35
R19 | 1796 23 54 40 51 22 24 | 47 34 58 48 43 43
R20 | 1907 48 177 19 75 27 37 | 78 83 58 49 62 59
R21 | 747 6 20 13 10 24 7 | 36 39 37 45 36 38
XR22 | 3103 --- 10 11 11 16 8 | --- 56 66 57 57 58
XR25 |13383 11 17 --- --- 20 14 | 57 64 --- --- 60 58
------+------------------------------------+--------------------------------
RMS | 1401 19 47 22 3202 22 |T 63 60 66 62 60 60
WRMS | 1401 14 23 14 20 24 |NE 63 60 66 62 60 60
MEDI | 1049 13 17 14 16 20 |MD 61 62 66 63 60 60
Table 3.2264.3 GPS week: 2264 Day: 3 MJD: 60095
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1658 28 66 19 29 24 21 | 83 32 69 76 71 65
R02 | 683 15 12 9 15 25 7 | 59 59 69 79 78 66
R03 | 695 10 14 9 16 8 7 | 66 69 70 76 68 69
R04 | 596 8 9 13 10 34 6 | 55 57 55 59 34 55
R05 | 574 13 14 13 8 20 7 | 49 53 49 55 50 50
R07 | 910 8 16 22 16 18 9 | 68 66 88 65 80 71
R08 | 806 9 25 15 18 15 9 | 70 57 82 79 72 72
R09 | 1990 17 30 13 12 25 10 | 24 43 35 9999 29 29
R11 | 2616 13 11 17 15 28 8 | 40 46 51 40 62 42
R12 | 1576 16 15 21 17 15 10 | 53 57 43 64 58 52
R13 | 726 41 55 43 52 31 27 | 90 46 84 65 67 68
R14 | 819 10 14 11 12 21 6 | 46 59 56 57 54 53
R15 | 941 9 13 8 13 13 6 | 53 52 56 62 55 55
R16 | 1364 19 34 59 26 18 21 | 61 56 72 53 56 58
R17 | 663 7 12 7 10 35 5 | 24 23 20 25 29 21
R18 | 677 12 22 21 9 13 9 | 22 24 23 27 22 21
R19 | 2516 33 53 34 43 33 23 | 37 25 49 38 36 32
R20 | 3879 33 175 23 45 18 24 | 72 46 73 55 61 65
R21 | 944 7 25 14 11 27 8 | 33 30 33 41 35 33
XR22 | 3626 --- 13 12 17 13 10 | --- 35 41 45 37 39
XR25 |15878 12 24 --- --- 23 17 | 28 43 --- --- 37 30
------+------------------------------------+--------------------------------
RMS | 1560 19 49 23 24 23 |T 51 46 55 55 51 49
WRMS | 1560 15 25 15 16 25 |NE 51 46 55 55 51 49
MEDI | 941 12 16 14 15 21 |MD 53 46 55 55 54 53
Table 3.2264.4 GPS week: 2264 Day: 4 MJD: 60096
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 724 38 52 22 36 16 22 | 89 40 61 64 62 62
R02 | 826 12 11 12 15 23 7 | 64 58 66 72 70 64
R03 | 647 9 12 14 19 16 8 | 67 64 56 78 69 65
R04 | 564 17 15 14 23 21 10 | 61 60 50 54 42 54
R05 | 693 15 11 13 13 28 7 | 59 59 57 56 39 57
R07 | 925 9 19 8 12 12 7 | 74 63 78 75 67 72
R08 | 1471 19 11 15 13 15 8 | 69 83 90 75 72 78
R09 | 2049 23 15 24 21 21 12 | 43 48 55 9999 45 42
R11 | 1662 14 9 13 16 19 7 | 93 86 87 91 98 89
R12 | 2042 6 16 10 15 23 7 | 54 54 50 62 71 53
R13 | 794 34 53 38 40 18 24 | 78 34 72 64 64 59
R14 | 947 16 14 16 14 13 9 | 43 57 61 55 53 52
R15 | 684 7 10 15 13 17 7 | 53 51 41 59 41 49
R16 | 1173 26 36 63 29 30 24 | 60 51 64 48 64 53
R17 | 524 9 17 11 8 16 7 | 22 23 22 25 16 21
R18 | 568 16 13 9 17 13 8 | 23 19 21 23 16 19
R19 | 1691 30 48 18 65 27 25 | 39 47 37 54 31 37
R20 | 4251 33 165 26 34 25 22 | 61 51 65 59 48 60
R21 | 894 14 16 12 14 31 8 | 22 26 27 34 19 24
XR22 | 6612 --- 12 7 13 34 8 | --- 31 36 38 25 34
R24 | 1656 17 18 14 8 17 8 | 33 33 9999 32 29 9999
XR25 |18265 2 --- --- --- 25 0 | 35 --- --- --- 37 35
------+------------------------------------+--------------------------------
RMS | 1500 20 44 22 25 21 |T 54 49 54 55 49 51
WRMS | 1500 17 28 14 17 24 |NE 54 49 54 55 49 51
MEDI | 925 16 15 14 15 19 |MD 59 51 56 56 45 53
Table 3.2264.5 GPS week: 2264 Day: 5 MJD: 60097
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 701 28 54 33 35 35 20 | 73 40 69 49 65 60
R02 | 610 8 18 13 14 17 7 | 54 37 55 40 57 47
R03 | 751 6 18 12 14 14 7 | 53 41 57 60 60 53
R04 | 753 16 16 18 13 25 9 | 52 53 43 52 44 48
R05 | 757 12 15 17 12 32 8 | 47 45 30 47 36 41
R07 | 857 6 20 9 19 20 7 | 63 50 59 72 70 62
R08 | 1572 11 10 9 11 27 6 | 55 60 64 60 77 59
R09 | 2411 14 26 16 13 13 9 | 34 42 37 763 36 33
R11 | 1497 12 14 21 19 21 9 | 116 111 103 112 103 110
R12 | 1687 8 12 11 17 16 7 | 56 56 57 56 57 55
R13 | 1393 23 65 33 32 44 21 | 73 41 74 51 86 60
R14 | 1470 8 15 13 13 23 7 | 44 50 36 49 57 43
R15 | 532 8 11 11 12 23 6 | 53 53 57 56 44 54
R16 | 1252 19 36 61 21 34 21 | 53 46 58 56 71 52
R17 | 607 4 18 8 11 11 5 | 20 17 18 26 21 19
R18 | 542 10 17 12 12 15 7 | 23 22 22 26 21 21
R19 | 613 24 52 12 49 20 20 | 31 32 29 35 23 30
R20 | 3949 22 124 54 49 48 35 | 38 49 45 38 37 31
R21 | 906 7 11 11 11 20 5 | 23 21 35 29 20 25
XR22 | 7512 --- 15 16 16 23 11 | --- 105 109 102 104 105
R24 | 1197 10 19 9 10 10 6 | 40 33 659 41 34 658
XR25 |13359 11 30 --- --- 36 19 | 110 114 --- --- 121 110
------+------------------------------------+--------------------------------
RMS | 1441 14 39 24 23 26 |T 52 50 81 86 56 80
WRMS | 1441 12 24 15 17 22 |NE 52 50 81 86 56 80
MEDI | 906 11 18 13 14 21 |MD 53 45 57 51 57 52
Table 3.2264.6 GPS week: 2264 Day: 6 MJD: 60098
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1326 32 73 27 20 23 22 | 112 52 108 88 102 92
R02 | 1071 7 14 18 11 14 7 | 85 74 95 83 94 84
R03 | 895 7 17 8 11 15 6 | 84 72 84 84 76 81
R04 | 588 13 10 19 10 35 8 | 82 74 64 73 58 72
R05 | 811 11 10 16 7 17 6 | 73 74 60 70 62 68
R07 | 788 9 14 13 17 24 7 | 88 79 84 95 98 87
R08 | 1232 11 15 8 9 33 6 | 83 85 92 89 104 86
R09 | 4071 12 30 16 13 18 10 | 40 50 47 811 51 43
R11 | 1794 11 12 14 14 20 7 | 144 148 143 141 136 143
R12 | 761 7 17 14 15 17 7 | 72 77 76 71 67 73
R13 | 1802 24 48 31 21 32 17 | 94 55 107 75 93 83
R14 | 1767 7 15 9 14 33 6 | 63 73 64 67 86 65
R15 | 1339 8 12 8 13 13 6 | 75 73 70 73 74 72
R16 | 1018 21 31 64 25 28 22 | 68 60 78 59 75 64
R17 | 641 8 12 10 11 12 5 | 25 19 17 25 19 20
R18 | 742 10 14 5 7 17 5 | 21 19 22 25 22 20
R19 | 1243 34 50 23 58 32 25 | 36 32 38 39 30 33
R20 | 3045 23 149 37 29 47 21 | 66 79 82 68 66 66
R21 | 1323 11 11 14 10 23 7 | 32 33 34 34 25 32
XR22 | 8575 --- 13 8 12 23 8 | --- 131 134 135 134 133
R24 | 963 14 24 13 16 19 9 | 48 41 923 37 41 922
XR25 |18079 8 15 --- --- 23 11 | 124 135 --- --- 130 127
------+------------------------------------+--------------------------------
RMS | 1595 16 43 23 20 25 |T 72 69 115 106 74 112
WRMS | 1595 14 23 15 14 26 |NE 72 69 115 106 74 112
MEDI | 1232 11 15 14 13 23 |MD 73 73 78 73 74 72
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