[IGSREPORT-29380] Wk 2266 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 30 07:11:30 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2266 (Jun 11, 2023 - Jun 17, 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 2.2266.
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:
igl2266[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2266 in the SP3 format.
igl22667.sum Combination Report for GPS Week 2266.
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 | -8.1 ns
1 | -8.3 ns
2 | -15.1 ns
3 | -11.0 ns
4 | -13.2 ns
5 | -8.2 ns
6 | -11.0 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
----+--------+---------------
1 | 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 1.2266, 1a.2266).
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 2.2266.0-6)
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 3.2266.0-6).
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 2266 summary. (Jun 11, 2023 - Jun 17, 2023)
Table 1.2266.a GPS week : 2266 MJD: 60106.0-60112.0
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 -24 12 .04 19 15 | 18007 -170 3001 8715
| 0 1 1 11 13 19 .04 | 1387 1712
esa n/a| -1 0 0 -7 -7 -16 -.21 39 25 | -12130 739 2972 8306
| 0 0 1 11 8 23 .02 | 10618 1747
gfz n/a| 0 1 2 32 4 5 -.18 22 16 | 0 -267 2966 8165
| 1 1 0 9 15 20 .02 | 0 2075
grg n/a| 3 0 -2 -21 25 -15 .29 22 19 | -10683 -378 2966 7739
| 1 1 2 18 9 28 .02 | 2152 2003
iac n/a| 0 1 -1 -1 7 -50 -.22 24 22 | -8280 -371 2955 8688
| 1 1 2 26 26 56 .05 | 2182 1030
Table 1.2266.b GPS week : 2266 MJD: 60106.0-60112.0
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 24 22 22 20 23 24 |
R02 | 8 6 7 7 9 8 7 |
R03 | 8 10 9 6 7 9 8 |
R04 | 7 12 9 8 9 7 9 |
R05 | 6 8 8 10 8 8 7 |
R07 | 7 9 8 9 9 8 7 |
R08 | 8 13 14 10 10 11 12 |
R09 | 10 7 8 9 11 13 9 |
R11 | 5 7 7 8 6 7 8 |
R12 | 8 7 11 11 8 7 7 |
R13 | 17 15 20 17 17 23 23 |
R14 | 8 9 7 7 5 6 6 |
R15 | 6 6 7 7 7 8 8 |
R16 | 24 21 21 19 20 23 24 |
R17 | 6 6 6 6 5 7 6 |
R18 | 6 8 10 10 8 8 11 |
R19 | 25 26 28 25 23 27 26 |
R20 | 32 25 33 37 36 31 35 |
R21 | 5 7 7 9 8 9 7 |
R22 | 13 7 6 10 10 6 10 |
R24 | 9 7 9 11 9 9 6 |
R25 | 10 11 9 11 7 16 10 |
Table 1.2266.c GPS week : 2266 MJD: 60106.0-60112.0
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 2266 0 | -18 12 347 -604 1083 1992 82.2 1532 1532 | -8080 0
brd 2266 1 | -55 -55 318 -1048 1497 3595 80.5 1132 1132 | -8347 0
brd 2266 2 | -54 -69 306 -1092 -888 -3201 80.9 1075 1075 | -15061 0
brd 2266 3 | -29 -27 284 177 -1222 -4999 80.7 1151 1151 | -10965 0
brd 2266 4 | 3 -44 305 540 -1018 -1810 82.1 1330 1330 | -13171 0
brd 2266 5 | 74 36 312 -977 849 -2299 80.9 1437 1437 | -8166 0
brd 2266 6 | 40 -14 272 1210 -107 -130 82.4 1249 1249 | -10953 0
-------------+------------------------------------------------------------+----------------
brd 2266 mean| -5 -23 306 -256 27 -978 81.4 1272 1272 | -10677 0
brd 2266 sdev| 48 37 24 907 1115 2999 .8 169 169 | 2710 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 2.2266.0 GPS week: 2266 Day: 0 MJD: 60106
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 -14 -7 26 .07 19 14 | 18819 1549 2812 9495
esa n/a| 0 1 0 -14 -13 -25 -.19 38 23 | -2043 2919 2795 8150
gfz n/a| 0 0 1 21 -12 4 -.16 19 12 | 0 1678 2778 8125
grg n/a| 4 0 -2 -3 19 -10 .29 22 18 | -9061 1437 2793 7722
iac n/a| -1 -1 -2 -1 17 7 -.19 23 21 | -6864 787 2773 9078
Table 2.2266.1 GPS week: 2266 Day: 1 MJD: 60107
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 -7 -21 18 .04 22 17 | 19417 2144 2987 9544
esa n/a| -2 0 0 0 -9 -45 -.21 42 21 | -12866 1928 2945 8681
gfz n/a| 0 0 3 24 -8 -7 -.15 20 15 | 0 1725 2965 8637
grg n/a| 4 0 -4 -7 28 -11 .30 21 19 | -9412 1366 2931 8199
iac n/a| -1 2 0 -32 34 -42 -.20 21 18 | -6369 -235 2919 9221
Table 2.2266.2 GPS week: 2266 Day: 2 MJD: 60108
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 0 -30 -24 -10 .09 19 15 | 16913 -1855 3076 8473
esa n/a| -2 0 0 -19 -12 -32 -.20 38 22 | -30945 -1243 3032 10052
gfz n/a| 1 0 1 43 29 3 -.20 20 11 | 0 -2498 2999 7712
grg n/a| 5 2 0 0 19 18 .31 28 26 | -14079 -2496 3053 6991
iac n/a| 1 1 -5 20 -4 -134 -.16 26 25 | -11544 -2386 3021 8161
Table 2.2266.3 GPS week: 2266 Day: 3 MJD: 60109
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 1 -6 -24 36 .08 18 13 | 19508 -1386 3375 9482
esa n/a| -3 0 0 -12 2 -11 -.22 39 22 | -1081 -435 3322 7977
gfz n/a| 0 1 1 22 12 0 -.19 22 15 | 0 -1567 3353 9029
grg n/a| 4 0 -2 -23 16 -54 .30 24 19 | -10323 -1757 3311 8572
iac n/a| -2 1 0 -1 -44 -54 -.24 24 20 | -8336 -499 3296 9325
Table 2.2266.4 GPS week: 2266 Day: 4 MJD: 60110
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 0 -20 20 .01 17 13 | 16247 -2007 3251 8703
esa n/a| -1 0 2 -13 1 -26 -.22 38 26 | -8055 -766 3191 8563
gfz n/a| 0 2 2 35 15 -25 -.17 24 20 | 0 -2442 3209 8529
grg n/a| 2 0 -5 -30 18 20 .25 20 19 | -12015 -2506 3234 8504
iac n/a| 0 2 -3 -12 10 31 -.32 27 23 | -10712 -130 3188 8917
Table 2.2266.5 GPS week: 2266 Day: 5 MJD: 60111
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 -1 -1 -52 11 -.01 21 15 | 18567 -644 2661 7517
esa n/a| 0 0 0 -1 -3 9 -.26 37 30 | -9234 20 2680 7329
gfz n/a| -2 3 2 42 4 36 -.19 26 20 | 0 -986 2668 7608
grg n/a| 2 -3 0 -34 41 -41 .30 19 17 | -7823 -880 2661 7347
iac n/a| 0 1 -2 42 27 -94 -.24 24 23 | -5761 -656 2664 8178
Table 2.2266.6 GPS week: 2266 Day: 6 MJD: 60112
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 0 6 -20 -16 .01 19 15 | 16580 1004 2845 7793
esa n/a| -1 0 2 11 -18 19 -.19 38 30 | -20686 2754 2840 7390
gfz n/a| 0 1 3 40 -11 23 -.22 24 18 | 0 2221 2792 7516
grg n/a| 2 -1 -4 -48 32 -29 .28 23 17 | -12073 2186 2784 6840
iac n/a| 0 -1 3 -26 14 -66 -.20 23 22 | -8376 518 2828 7939
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 3.2266.0 GPS week: 2266 Day: 0 MJD: 60106
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1136 42 70 25 24 18 22 | 106 42 81 74 71 78
R02 | 637 7 21 9 18 11 7 | 76 61 77 79 74 74
R03 | 852 15 13 11 10 23 7 | 83 66 70 78 85 74
R04 | 901 12 9 11 10 14 6 | 84 74 77 83 73 79
R05 | 806 10 10 8 13 14 6 | 81 77 76 70 69 75
R07 | 869 7 21 7 13 10 6 | 84 66 81 86 85 80
R08 | 1482 6 22 9 17 34 7 | 79 68 89 93 97 83
R09 | 2924 11 25 11 21 19 9 | 53 59 61 55 52 55
R11 | 1662 8 10 8 7 22 5 | 31 36 35 35 35 33
R12 | 587 8 22 8 14 16 7 | 53 70 52 51 49 53
R13 | 1194 24 37 25 35 30 17 | 89 51 83 64 79 73
R14 | 632 13 16 11 12 14 7 | 62 71 60 57 69 60
R15 | 1278 8 11 10 13 15 6 | 79 74 72 74 73 74
R16 | 784 26 39 57 33 25 24 | 77 79 90 73 86 78
R17 | 1329 11 10 12 8 13 6 | 28 28 29 30 28 28
R18 | 668 8 17 5 8 25 5 | 25 26 23 29 28 24
R19 | 2236 38 64 24 50 29 24 | 29 25 31 29 26 24
R20 | 3846 32 117 33 43 51 32 | 43 77 33 30 29 35
R21 | 809 6 13 8 10 11 5 | 36 33 32 38 36 33
XR22 | 1133 --- 14 19 19 19 13 | --- 32 28 32 27 29
R24 | 1305 13 14 10 20 28 8 | 42 40 37 43 35 38
XR25 | 9706 6 14 --- --- 15 10 | 28 33 --- --- 37 29
------+------------------------------------+--------------------------------
RMS | 1532 19 38 19 22 23 |T 60 54 57 57 56 54
WRMS | 1532 14 23 12 18 21 |NE 60 54 57 57 56 54
MEDI | 1133 11 16 11 14 18 |MD 62 59 61 57 52 55
Table 3.2266.1 GPS week: 2266 Day: 1 MJD: 60107
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1158 45 63 22 24 21 23 | 78 31 56 65 65 54
R02 | 710 8 13 10 11 14 6 | 59 50 60 59 60 57
R03 | 783 12 16 20 17 12 9 | 63 62 84 72 68 70
R04 | 1004 20 10 14 30 12 11 | 65 48 63 53 58 55
R05 | 1533 19 9 14 11 12 8 | 64 53 45 52 49 52
R07 | 786 12 19 17 13 21 9 | 62 52 71 64 73 62
R08 | 925 20 27 14 26 11 12 | 56 49 68 83 57 63
R09 | 1984 12 12 11 11 24 6 | 44 47 50 48 48 47
R11 | 1187 11 8 16 9 12 6 | 16 21 24 18 22 17
R12 | 716 9 14 11 11 14 6 | 36 43 34 40 30 37
R13 | 590 25 32 20 21 25 14 | 62 45 60 41 49 49
R14 | 1038 13 16 16 16 18 8 | 45 50 42 34 53 41
R15 | 1155 12 11 9 9 11 6 | 58 49 48 52 54 51
R16 | 729 27 28 53 24 29 20 | 54 54 53 54 55 52
R17 | 1288 6 14 7 13 14 6 | 21 21 17 25 22 18
R18 | 768 14 21 8 10 11 8 | 17 27 22 25 20 19
R19 | 1444 48 45 19 58 19 25 | 27 25 31 27 31 27
R20 | 1989 34 155 42 26 54 25 | 33 60 45 24 27 29
R21 | 678 13 12 9 9 19 6 | 25 20 23 26 20 21
XR22 | 956 --- 10 12 8 17 7 | --- 23 22 24 24 21
R24 | 649 12 9 13 14 20 7 | 31 28 29 25 25 25
XR25 |18766 9 12 --- --- 28 10 | 36 37 --- --- 38 36
------+------------------------------------+--------------------------------
RMS | 1131 22 42 20 21 21 |T 45 40 45 43 43 41
WRMS | 1131 17 21 15 19 18 |NE 45 40 45 43 43 41
MEDI | 956 13 14 14 13 17 |MD 45 45 45 41 48 41
Table 3.2266.2 GPS week: 2266 Day: 2 MJD: 60108
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 691 30 74 18 28 38 22 | 82 37 78 74 44 68
R02 | 702 10 16 10 14 34 7 | 58 47 50 71 80 56
R03 | 912 11 16 14 21 25 9 | 66 57 53 76 74 61
R04 | 1270 16 15 8 24 20 9 | 69 72 64 59 52 64
R05 | 1934 11 12 15 17 16 8 | 57 50 62 55 44 56
R07 | 658 9 23 13 11 11 8 | 65 57 80 80 67 71
R08 | 856 21 20 24 27 16 13 | 61 69 91 90 64 77
R09 | 1576 14 11 12 12 15 7 | 33 42 46 43 35 39
R11 | 975 11 14 11 15 10 7 | 21 24 34 36 29 27
R12 | 961 12 23 23 12 21 10 | 42 57 33 49 43 41
R13 | 1328 23 47 31 39 18 19 | 73 47 82 58 60 65
R14 | 1312 6 15 6 19 21 6 | 50 56 51 42 51 48
R15 | 826 13 10 9 18 13 7 | 65 60 58 59 63 60
R16 | 717 21 26 52 33 24 21 | 64 59 70 72 69 65
R17 | 757 6 8 11 15 18 6 | 27 22 26 30 24 25
R18 | 609 11 29 7 21 21 9 | 21 25 22 27 26 19
R19 | 1401 39 50 26 77 41 28 | 54 39 52 34 33 44
R20 | 1456 38 119 25 40 57 33 | 37 49 48 34 26 33
R21 | 616 12 16 9 10 28 7 | 24 21 23 29 25 22
XR22 | 1286 --- 6 7 11 21 6 | --- 18 22 28 22 22
R24 | 579 18 22 9 15 25 9 | 28 24 22 30 30 23
XR25 |16799 6 12 --- --- 26 9 | 31 34 --- --- 41 32
------+------------------------------------+--------------------------------
RMS | 1075 19 38 20 28 26 |T 48 43 50 51 45 46
WRMS | 1075 15 22 11 26 25 |NE 48 43 50 51 45 46
MEDI | 912 12 16 12 18 21 |MD 54 47 51 49 43 44
Table 3.2266.3 GPS week: 2266 Day: 3 MJD: 60109
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 549 35 59 25 35 24 22 | 88 56 82 51 63 68
R02 | 649 9 12 14 11 22 7 | 68 62 76 75 70 70
R03 | 768 9 12 8 13 19 6 | 75 68 70 80 81 73
R04 | 893 15 10 13 15 20 8 | 70 65 57 59 57 63
R05 | 775 9 8 20 26 17 10 | 66 64 75 50 68 62
R07 | 1801 13 19 19 13 17 9 | 73 58 58 75 74 66
R08 | 1177 10 25 21 10 16 9 | 78 68 98 86 81 83
R09 | 1890 11 24 15 9 18 8 | 29 38 34 30 32 30
R11 | 1159 12 16 12 14 18 7 | 41 40 44 50 51 42
R12 | 765 8 17 30 14 14 10 | 52 56 40 53 51 47
R13 | 1953 20 54 23 20 33 16 | 77 52 69 70 73 66
R14 | 1739 6 9 12 17 14 6 | 60 55 65 49 54 57
R15 | 987 6 16 11 17 22 7 | 55 52 56 52 49 52
R16 | 542 18 30 52 22 28 19 | 60 49 71 59 57 59
R17 | 723 9 11 10 9 14 5 | 38 34 39 41 37 37
R18 | 680 8 26 12 23 29 10 | 35 35 33 36 34 32
R19 | 1273 40 63 22 50 43 25 | 43 48 42 39 41 39
R20 | 1323 38 122 37 58 42 36 | 72 62 57 40 38 56
R21 | 606 8 24 17 10 17 8 | 37 37 42 40 38 38
XR22 | 1401 --- 20 12 9 17 9 | --- 42 49 37 28 40
R24 | 892 14 18 21 21 17 10 | 42 43 38 48 35 39
XR25 |14368 7 15 --- --- 20 10 | 30 38 --- --- 36 31
------+------------------------------------+--------------------------------
RMS | 1150 18 39 22 24 24 |T 56 51 56 53 52 52
WRMS | 1150 13 22 15 19 20 |NE 56 51 56 53 52 52
MEDI | 893 10 18 17 15 18 |MD 60 52 57 50 51 52
Table 3.2266.4 GPS week: 2266 Day: 4 MJD: 60110
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 692 30 63 19 23 33 19 | 76 43 68 55 52 59
R02 | 1040 10 15 19 18 20 9 | 63 63 75 58 58 62
R03 | 734 9 12 12 13 15 6 | 66 67 62 76 70 67
R04 | 557 16 11 15 13 14 8 | 72 64 67 72 65 69
R05 | 696 7 10 13 19 25 7 | 71 70 72 54 76 65
R07 | 2580 12 30 10 13 26 9 | 75 55 76 64 79 68
R08 | 1003 7 26 25 11 20 10 | 72 62 88 73 75 73
R09 | 2742 9 21 29 13 20 10 | 41 43 58 43 45 44
R11 | 1505 7 13 12 9 32 5 | 22 23 33 24 39 24
R12 | 644 7 20 14 11 16 7 | 37 45 27 33 35 33
R13 | 2416 24 36 33 23 39 16 | 67 48 60 56 68 55
R14 | 1602 8 11 10 8 24 5 | 47 48 52 44 54 46
R15 | 944 10 14 15 8 24 6 | 56 50 55 57 67 54
R16 | 686 23 27 55 22 30 19 | 56 54 55 68 68 56
R17 | 787 8 8 8 9 23 5 | 31 29 30 33 28 30
R18 | 663 12 19 16 9 23 8 | 25 22 26 27 24 23
R19 | 800 30 69 22 36 33 22 | 45 24 28 30 40 29
R20 | 1401 37 114 50 53 51 36 | 51 43 51 33 31 40
R21 | 839 11 17 19 11 15 8 | 28 27 33 29 27 27
XR22 | 1057 --- 14 12 14 22 9 | --- 29 36 33 36 31
R24 | 682 17 19 11 12 15 8 | 36 34 34 39 31 34
XR25 |11433 5 10 --- --- 21 7 | 37 39 --- --- 43 37
------+------------------------------------+--------------------------------
RMS | 1329 17 38 24 20 26 |T 51 44 51 47 50 46
WRMS | 1329 13 26 20 19 23 |NE 51 44 51 47 50 46
MEDI | 839 10 17 15 13 23 |MD 51 43 55 44 45 44
Table 3.2266.5 GPS week: 2266 Day: 5 MJD: 60111
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 683 45 68 25 21 34 23 | 80 50 63 60 66 60
R02 | 1734 8 18 19 11 15 8 | 65 60 80 72 64 69
R03 | 718 7 21 20 14 11 9 | 68 58 76 74 67 69
R04 | 603 11 10 14 10 30 6 | 73 68 67 79 58 72
R05 | 638 13 13 16 13 17 8 | 67 62 61 64 68 63
R07 | 1807 12 23 9 14 34 8 | 78 59 67 77 90 71
R08 | 2267 11 27 28 11 27 11 | 82 71 98 89 96 85
R09 | 3409 13 39 19 18 24 12 | 44 60 55 46 55 47
R11 | 1558 10 9 18 9 16 7 | 38 41 44 44 44 41
R12 | 679 9 13 13 9 24 6 | 48 54 46 57 45 50
R13 | 1620 28 53 40 40 28 23 | 62 51 55 58 68 53
R14 | 1080 9 14 10 8 10 5 | 50 48 42 47 44 46
R15 | 1009 10 16 15 13 14 7 | 64 67 75 73 67 69
R16 | 888 18 32 66 28 17 22 | 64 66 71 62 62 64
R17 | 1128 12 9 13 9 26 6 | 35 36 41 38 38 36
R18 | 754 10 22 12 10 22 7 | 33 35 37 37 35 35
R19 | 1538 50 76 20 35 24 26 | 53 48 44 41 39 41
R20 | 1402 38 94 56 35 41 31 | 58 40 41 54 48 45
R21 | 935 9 16 19 17 26 9 | 50 43 49 64 49 51
R22 | 1494 10 13 9 5 16 5 | 13 39 34 36 34 33
R24 | 899 15 24 11 13 14 9 | 39 46 43 39 36 39
XR25 |19866 9 23 --- --- 33 15 | 51 59 --- --- 60 52
------+------------------------------------+--------------------------------
RMS | 1437 21 37 26 19 24 |T 55 52 56 57 56 54
WRMS | 1437 15 30 20 17 23 |NE 55 52 56 57 56 54
MEDI | 1080 11 21 18 13 24 |MD 53 51 55 58 55 51
Table 3.2266.6 GPS week: 2266 Day: 6 MJD: 60112
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 822 38 68 30 26 23 23 | 103 49 92 74 79 79
R02 | 901 12 14 9 12 27 7 | 80 67 84 78 84 77
R03 | 850 12 15 16 13 9 8 | 86 80 99 96 90 90
R04 | 696 11 13 15 20 23 8 | 90 85 91 93 74 89
R05 | 808 13 11 9 15 18 7 | 82 77 77 77 78 78
R07 | 1273 13 17 7 11 32 7 | 100 74 89 91 112 90
R08 | 1332 14 16 31 14 27 11 | 100 95 130 107 122 107
R09 | 3209 13 20 14 16 15 9 | 38 44 51 39 43 40
R11 | 1637 15 12 16 9 17 7 | 35 34 32 30 30 31
R12 | 1098 10 14 12 12 19 7 | 52 58 44 52 49 50
R13 | 1225 33 52 29 44 29 22 | 85 49 67 53 74 63
R14 | 867 9 9 10 9 14 5 | 45 54 47 48 50 47
R15 | 979 9 12 16 14 15 7 | 66 65 62 67 72 64
R16 | 634 25 39 64 24 31 23 | 71 74 85 71 82 73
R17 | 947 9 7 11 14 17 6 | 40 45 44 47 38 43
R18 | 837 14 30 16 15 13 10 | 31 41 37 41 32 36
R19 | 1058 35 68 23 53 20 26 | 54 66 64 54 35 55
R20 | 1367 25 113 48 48 46 34 | 42 39 52 55 37 39
R21 | 1087 11 13 10 11 21 6 | 44 36 40 47 44 41
R22 | 1126 14 15 22 13 19 9 | 13 34 44 46 36 36
R24 | 1072 13 14 8 7 12 6 | 48 50 50 49 46 48
XR25 |17845 7 12 --- --- 18 9 | 43 41 --- --- 50 42
------+------------------------------------+--------------------------------
RMS | 1248 19 38 24 23 23 |T 61 57 65 62 61 59
WRMS | 1248 15 30 18 17 22 |NE 61 57 65 62 61 59
MEDI | 1058 13 14 16 14 19 |MD 52 50 62 54 50 50
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