[IGSREPORT-30010] Wk 2324 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 9 01:01:04 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2324 (Jul 21, 2024 - Jul 27, 2024)
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 2.2324.
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:
igl2324[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2324 in the SP3 format.
igl23247.sum Combination Report for GPS Week 2324.
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).
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 | 6.0 ns
1 | 8.5 ns
2 | 6.7 ns
3 | 5.6 ns
4 | 6.9 ns
5 | 8.1 ns
6 | 7.4 ns
5. 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
----+--------+---------------
4 | GFZ | 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 1.2324, 1a.2324).
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 2.2324.0-6)
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 3.2324.0-6).
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 2324 summary. (Jul 21, 2024 - Jul 27, 2024)
Table 1.2324.a GPS week : 2324 MJD: 60512.0-60518.0
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 -6 -27 29 .20 22 19 | -1386 -371 3423 11592
| 0 0 1 12 30 24 .07 | 1798 1905
esa n/a| -1 -1 1 -12 11 27 -.21 29 22 | 5747 152 3393 7592
| 0 1 2 10 9 25 .09 | 5672 2077
gfz n/a| 0 0 0 29 23 5 -.10 29 17 | 0 -450 3453 8175
| 1 0 0 15 18 29 .14 | 0 1989
grg n/a| 2 0 4 -10 28 -31 .52 30 23 | 5463 -566 3477 11218
| 2 1 2 24 25 52 .08 | 734 1916
iac n/a| 0 1 -5 -1 -6 -48 -.14 18 17 | 7576 -938 3401 11093
| 2 1 2 24 22 30 .19 | 944 801
jgx n/a| 0 -1 3 13 -10 55 -.18 26 26 | 3111 -466 3382 8348
| 1 1 1 14 25 75 .16 | 1966 2309
Table 1.2324.b GPS week : 2324 MJD: 60512.0-60518.0
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 | 15 18 18 20 15 18 18 |
R02 | 7 8 7 16 12 8 9 |
R03 | 6 9 14 12 9 7 8 |
R04 | 7 7 6 13 8 7 8 |
R05 | 7 8 7 14 9 8 7 |
R07 | 8 12 9 12 7 8 8 |
R08 | 8 8 10 14 8 8 8 |
R09 | 6 8 7 7 8 7 7 |
R11 | 9 7 7 7 6 6 7 |
R12 | 7 9 9 6 6 5 7 |
R13 | 14 12 15 15 14 12 14 |
R14 | 7 9 6 6 7 6 6 |
R15 | 7 6 7 8 8 8 7 |
R16 | 8 8 9 9 10 8 9 |
R17 | 8 7 8 7 5 7 7 |
R18 | 8 9 9 7 6 8 9 |
R19 | 22 23 19 17 17 17 17 |
R20 | 32 30 26 28 31 28 25 |
R21 | 8 7 7 9 9 7 10 |
R22 | 7 8 7 8 7 8 8 |
R24 | 9 8 8 8 8 8 9 |
R25 | 14 10 12 14 13 10 12 |
R26 | 37 33 43 36 37 35 36 |
Table 1.2324.c GPS week : 2324 MJD: 60512.0-60518.0
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 2324 0 | -25 34 -4 -335 3132 6780 81.2 1365 1365 | 5991 0
brd 2324 1 | -74 -28 160 -1763 1322 3076 80.3 1397 1397 | 8450 0
brd 2324 2 | 46 13 206 -1129 173 -3660 78.2 1714 1714 | 6719 0
brd 2324 3 | -60 -19 150 -13 -1004 -3563 80.7 1903 1903 | 5587 0
brd 2324 4 | -75 4 181 -422 1541 -9215 82.5 1566 1566 | 6894 0
brd 2324 5 | -23 28 148 -744 523 2977 79.4 1586 1586 | 8066 0
brd 2324 6 | -48 -13 198 -459 1768 1795 81.5 1454 1454 | 7386 0
-------------+------------------------------------------------------------+----------------
brd 2324 mean| -37 2 148 -695 1064 -258 80.5 1569 1569 | 7013 0
brd 2324 sdev| 42 24 71 585 1318 5447 1.4 190 190 | 1040 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 2.2324.0 GPS week: 2324 Day: 0 MJD: 60512
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 0 1 -16 -27 1 .06 22 18 | -3771 -2450 3671 10012
esa n/a| -2 0 -1 -6 -5 16 -.22 35 23 | 967 -2062 3696 7410
gfz n/a| 0 0 0 25 7 6 -.21 24 16 | 0 -3176 3713 7264
grg n/a| 3 -2 7 14 4 -98 .46 28 23 | 5989 -3137 3655 9074
iac n/a| 0 3 -6 -31 15 -16 .07 18 15 | 6534 -1983 3658 9492
jgx n/a| 0 -2 3 16 5 116 -.45 34 33 | 939 -4122 3639 7368
Table 2.2324.1 GPS week: 2324 Day: 1 MJD: 60513
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 14 -54 17 .20 22 16 | -3078 3313 3289 10730
esa n/a| -1 -4 4 -23 11 38 -.21 30 26 | 4287 4418 3299 7894
gfz n/a| 0 0 -1 19 53 32 -.24 32 17 | 0 3266 3412 8256
grg n/a| 0 1 4 -19 38 -31 .59 30 26 | 5341 3072 3370 10428
iac n/a| 2 1 -6 -14 -23 -98 -.04 21 20 | 8468 274 3276 10229
jgx n/a| 0 -3 3 27 18 162 -.35 30 30 | 1410 3467 3318 8366
Table 2.2324.2 GPS week: 2324 Day: 2 MJD: 60514
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 -22 -23 17 .27 22 18 | -1406 663 3483 11613
esa n/a| 0 -3 0 -16 19 -12 -.33 32 21 | 14989 228 3460 8950
gfz n/a| 0 0 0 31 1 30 -.13 25 16 | 0 59 3525 8920
grg n/a| 3 1 1 20 2 -77 .67 34 22 | 5034 28 3597 11307
iac n/a| 0 1 -3 -5 17 -39 -.06 20 19 | 7895 -375 3468 11239
jgx n/a| 1 -3 2 -4 -27 90 -.15 26 25 | 3031 637 3524 9254
Table 2.2324.3 GPS week: 2324 Day: 3 MJD: 60515
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 -10 -61 11 .25 20 20 | -2454 -363 3138 11623
esa n/a| 0 -2 3 -7 22 16 -.05 30 21 | 4878 539 3078 7791
gfz n/a| 2 0 0 31 41 -27 .16 33 17 | 0 -557 3126 8852
grg n/a| -1 1 4 3 71 -49 .52 45 24 | 4056 -636 3197 11491
iac n/a| 2 1 -6 23 -21 -68 -.45 23 22 | 5963 -347 3100 11230
jgx n/a| 1 -1 5 -9 19 66 -.09 24 24 | 1343 -195 2962 8868
Table 2.2324.4 GPS week: 2324 Day: 4 MJD: 60516
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 3 33 66 .21 20 20 | 40 -1420 3484 11391
esa n/a| -1 0 0 3 15 32 -.22 23 19 | -2085 -691 3407 7601
gfz n/a| 3 -1 0 42 16 -44 -.18 24 16 | 0 -956 3462 7615
grg n/a| 5 0 0 -22 44 0 .47 26 23 | 5695 -1370 3495 11030
iac n/a| -3 1 -1 -1 -21 -17 -.03 14 14 | 8262 -1542 3447 10789
jgx n/a| 0 0 1 14 -46 17 -.14 19 18 | 4329 -823 3348 7738
Table 2.2324.5 GPS week: 2324 Day: 5 MJD: 60517
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 -14 -23 45 .17 23 19 | -106 -700 3518 12560
esa n/a| 0 0 0 -26 8 27 -.29 29 26 | 10072 -168 3482 6587
gfz n/a| 0 0 0 3 22 16 -.13 32 19 | 0 1 3539 7960
grg n/a| 3 -2 4 -47 32 60 .52 24 22 | 6021 -302 3586 12374
iac n/a| -1 1 -4 38 -31 -65 -.16 14 13 | 7910 -1289 3500 12031
jgx n/a| 2 0 3 26 -10 -32 -.07 26 26 | 4713 -440 3494 8233
Table 2.2324.6 GPS week: 2324 Day: 6 MJD: 60518
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 -3 -35 51 .23 27 21 | 1073 -1640 3382 13219
esa n/a| 0 -1 4 -10 6 71 -.17 27 20 | 7122 -1197 3335 6916
gfz n/a| 0 0 0 51 22 22 .01 29 18 | 0 -1788 3400 8358
grg n/a| 2 -1 5 -22 8 -23 .43 23 21 | 6109 -1621 3445 12823
iac n/a| 0 0 -6 -21 18 -31 -.34 17 16 | 8000 -1308 3360 12644
jgx n/a| 0 0 3 23 -30 -34 -.03 24 23 | 6012 -1787 3394 8612
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 3.2324.0 GPS week: 2324 Day: 0 MJD: 60512
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 697 38 40 32 25 26 44 15 | 69 54 70 70 65 62 59
XR02E |17062 9 13 12 14 18 --- 7 | 37 43 43 54 42 --- 41
R03E | 998 10 14 12 18 10 14 5 | 92 95 95 105 93 96 95
R04E | 1581 12 15 19 14 14 10 6 | 58 56 60 66 57 54 57
R05E | 1263 10 17 18 15 15 15 7 | 88 83 85 92 93 77 86
R07E | 1235 14 16 23 15 12 29 8 | 111 108 108 109 107 103 107
R08E | 1821 18 11 11 22 16 24 7 | 136 138 139 135 127 140 134
R09 | 1553 10 12 8 10 10 23 5 | 32 33 33 35 36 35 33
R11 | 1185 17 18 16 18 26 17 8 | 30 47 39 28 40 37 33
R12 | 855 11 14 13 20 16 12 6 | 25 38 34 31 35 39 30
R13 | 1100 19 35 9 45 21 54 14 | 28 35 37 38 26 46 31
R14 | 1174 12 11 17 14 17 15 6 | 22 25 22 21 38 29 25
R15 | 1905 11 13 16 11 13 21 6 | 25 41 35 26 35 40 31
R16 | 1237 25 20 16 11 13 11 7 | 26 55 48 34 39 43 37
R17 | 1188 22 18 14 22 13 19 8 | 126 123 117 111 111 109 115
R18 | 1211 8 28 12 20 10 19 7 | 131 146 134 132 129 96 132
R19 | 1835 45 70 55 36 33 56 22 | 139 106 161 120 136 108 128
R20 | 1529 48 111 66 83 28 96 32 | 136 107 133 97 107 95 107
R21 | 937 18 17 15 17 14 22 7 | 76 64 70 65 65 56 65
R22 | 1962 16 14 9 19 12 19 6 | 105 112 115 125 117 108 113
R24 | 1100 22 12 11 29 15 19 8 | 109 115 108 101 118 105 109
XR25 |17122 14 24 --- --- 20 --- 14 | 62 70 --- --- 65 --- 64
XR26E |22894 44 --- --- 50 57 --- 36 | 45 --- --- 41 42 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1364 22 35 24 28 18 34 |T 74 77 80 74 74 73 72
WRMS | 1364 18 23 16 23 15 33 |NE 71 74 77 68 73 67 70
MEDI | 1237 16 16 15 18 15 19 |MD 69 64 70 66 65 62 64
Table 3.2324.1 GPS week: 2324 Day: 1 MJD: 60513
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 985 47 26 44 60 25 37 18 | 62 42 73 76 59 35 50
XR02E | 975 11 10 16 18 19 --- 7 | 44 43 46 46 36 --- 40
R03E | 1777 18 11 14 20 26 19 8 | 120 124 128 128 114 126 121
R04E | 1200 12 11 19 23 11 18 7 | 35 34 39 38 32 38 33
R05E | 1145 17 17 14 22 17 19 8 | 94 94 87 79 74 83 83
R07E | 1088 17 29 15 15 37 27 11 | 121 121 117 113 103 121 114
R08E | 1080 13 16 12 15 17 26 7 | 111 104 109 108 107 107 107
R09 | 1904 24 17 8 14 13 21 7 | 25 31 32 36 21 33 25
R11 | 919 15 11 11 14 21 16 7 | 22 31 27 24 28 33 24
R12 | 683 11 20 22 29 13 22 8 | 21 37 40 25 23 25 23
R13 | 1290 20 25 17 51 16 28 12 | 19 40 35 24 17 34 21
R14 | 1051 12 15 32 14 20 17 8 | 21 25 34 25 24 31 19
R15 | 2166 10 15 13 13 14 17 6 | 24 28 18 31 23 27 20
R16 | 909 17 17 23 15 17 15 8 | 23 40 41 30 15 38 26
R17 | 892 16 11 15 21 10 19 7 | 114 110 110 109 110 107 109
XR18 | 1330 13 24 13 24 16 --- 9 | 119 130 128 116 119 --- 121
R19 | 1027 40 53 82 46 28 45 22 | 103 86 139 100 108 97 101
R20 | 1407 44 94 71 57 41 80 29 | 86 81 103 81 102 68 84
R21 | 925 13 16 21 15 12 19 7 | 58 56 49 62 58 54 54
R22 | 2952 14 16 23 20 10 22 8 | 116 118 124 139 125 126 123
R24 | 1107 12 20 16 21 15 23 8 | 89 96 94 89 94 92 91
XR25 |12612 13 17 --- --- 11 --- 10 | 71 79 --- --- 76 --- 75
XR26E |23375 40 --- --- 37 57 --- 33 | 44 --- --- 51 50 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1397 22 30 32 29 21 30 |T 67 70 74 69 66 67 65
WRMS | 1397 16 26 17 26 20 30 |NE 60 65 69 63 62 58 61
MEDI | 1107 15 17 16 20 17 21 |MD 62 56 73 62 59 54 54
Table 3.2324.2 GPS week: 2324 Day: 2 MJD: 60514
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1281 29 49 52 47 19 47 18 | 54 44 78 85 39 42 46
XR02E | 993 9 14 9 23 14 --- 7 | 62 68 62 67 62 --- 62
R03E | 2039 11 15 12 54 43 24 13 | 100 104 107 120 104 95 101
R04E | 1608 13 10 9 19 13 15 6 | 54 53 48 57 56 50 52
R05E | 1123 16 13 19 15 13 16 7 | 85 75 77 83 80 70 77
R07E | 1216 15 18 16 38 16 17 9 | 86 89 87 85 86 84 84
R08E | 1314 13 18 22 36 25 16 10 | 134 126 136 149 132 133 133
R09 | 3398 12 15 18 19 9 15 6 | 24 24 33 26 21 27 22
R11 | 1884 19 18 14 14 10 12 6 | 16 26 29 25 21 18 19
R12 | 742 17 22 28 20 12 17 8 | 22 40 43 22 24 22 24
R13 | 1094 26 23 22 68 16 45 15 | 26 37 29 23 28 44 23
R14 | 1731 12 10 12 16 6 16 5 | 14 19 20 20 12 23 13
R15 | 1079 15 14 15 15 19 11 7 | 18 27 26 21 22 25 18
R16 | 1035 22 24 23 18 8 17 8 | 16 52 45 23 28 32 30
R17 | 841 18 17 18 25 9 20 8 | 68 66 72 79 65 59 66
XR18 | 1349 13 25 17 23 8 --- 8 | 96 100 92 120 98 --- 99
R19 | 1614 43 53 45 41 32 36 18 | 82 82 89 75 65 68 72
R20 | 1415 51 96 53 58 35 56 26 | 90 71 55 67 76 75 65
R21 | 1439 19 14 10 11 9 22 6 | 63 67 60 71 58 55 60
R22 | 3569 15 18 8 14 17 18 7 | 71 83 83 78 75 75 76
R24 | 844 12 22 11 25 11 21 7 | 81 80 78 94 77 77 78
XR25 |14813 17 21 --- --- 12 --- 11 | 31 37 --- --- 33 --- 32
XR26E |14730 39 --- --- 93 57 --- 43 | 53 --- --- 73 58 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 1713 22 32 25 34 20 26 |T 58 62 64 66 57 56 56
WRMS | 1713 18 21 16 22 19 25 |NE 47 54 53 53 46 46 46
MEDI | 1349 16 18 17 23 13 17 |MD 62 66 62 71 58 55 60
Table 3.2324.3 GPS week: 2324 Day: 3 MJD: 60515
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1999 45 54 64 21 29 41 20 | 69 45 85 54 38 33 43
XR02E | 826 12 12 20 83 23 --- 15 | 77 77 83 127 75 --- 80
R03E | 2034 13 17 26 46 32 22 11 | 90 93 96 119 71 90 87
R04E | 1180 18 12 15 70 26 24 12 | 48 48 51 69 62 45 47
R05E | 818 18 11 20 92 22 13 14 | 64 63 66 94 67 57 59
R07E | 1211 13 21 20 69 22 14 11 | 73 75 72 97 76 72 72
R08E | 1695 13 21 24 67 40 26 14 | 115 125 125 125 113 122 116
R09 | 3794 12 12 21 16 12 14 6 | 20 29 37 28 27 25 24
R11 | 1972 17 18 7 11 13 21 7 | 24 31 27 27 33 29 24
R12 | 917 11 13 19 22 15 7 6 | 19 24 31 26 24 21 20
R13 | 1013 26 21 25 57 25 44 14 | 34 41 50 41 30 48 36
R14 | 1791 5 14 14 11 20 9 5 | 18 25 25 24 22 16 16
R15 | 709 16 21 23 23 16 15 8 | 16 43 40 16 27 35 25
R16 | 1565 21 25 12 13 20 16 8 | 18 47 27 25 38 37 27
R17 | 879 8 18 19 18 13 15 6 | 61 54 67 64 57 50 57
R18 | 1047 7 23 12 23 15 14 7 | 61 67 64 68 72 66 63
R19 | 3572 16 49 66 43 30 26 17 | 61 75 79 62 62 60 58
R20 | 2695 41 83 87 74 31 55 27 | 87 69 117 60 61 69 68
R21 | 1663 15 18 19 29 16 21 8 | 65 58 64 69 54 44 56
R22 | 2481 17 19 18 14 19 11 7 | 39 35 41 43 39 33 35
R24 | 847 11 21 24 23 14 17 8 | 67 63 58 68 66 68 63
XR25 |14235 13 27 --- --- 20 --- 14 | 27 37 --- --- 25 --- 25
XR26E |13717 35 --- --- 55 64 --- 36 | 52 --- --- 72 53 --- 52
------+-----------------------------------------+-------------------------------------
RMS | 1902 20 30 33 45 23 24 |T 52 55 62 62 51 51 50
WRMS | 1902 20 21 17 24 22 24 |NE 41 46 51 44 42 42 39
MEDI | 1663 15 19 20 23 20 16 |MD 61 48 64 62 54 45 52
Table 3.2324.4 GPS week: 2324 Day: 4 MJD: 60516
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1687 49 51 33 21 10 28 15 | 59 41 60 38 28 24 32
XR02E | 832 20 21 19 38 20 --- 11 | 44 42 38 63 47 --- 41
R03E | 1790 11 19 24 16 9 30 8 | 68 67 74 79 69 72 69
R04E | 962 9 12 15 25 13 24 7 | 51 50 47 59 48 46 47
R05E | 954 15 9 14 38 23 17 9 | 59 53 56 74 55 48 53
R07E | 2493 15 14 16 25 9 15 7 | 72 71 75 83 69 70 71
R08E | 1569 17 22 22 28 7 17 8 | 127 135 146 134 131 136 133
R09 | 1526 17 18 18 37 9 11 8 | 29 27 28 41 27 22 23
R11 | 1809 10 23 11 13 13 6 6 | 25 39 32 27 35 31 29
R12 | 999 16 10 12 20 7 7 5 | 26 31 33 25 27 27 27
R13 | 748 30 33 21 55 9 33 13 | 30 45 44 34 25 32 31
R14 | 1840 11 18 13 16 21 11 7 | 20 28 31 27 33 25 25
R15 | 804 18 18 18 20 12 19 7 | 26 39 38 32 25 39 29
R16 | 1706 22 26 30 20 15 17 9 | 31 54 52 29 31 36 34
R17 | 1151 9 14 13 12 9 14 5 | 74 77 76 72 64 63 69
R18 | 1085 6 23 11 15 9 17 6 | 95 106 93 103 94 53 96
R19 | 2008 28 40 64 26 29 26 16 | 82 65 100 75 79 74 75
XR20 | 3261 49 82 138 65 25 --- 31 | 109 84 162 89 82 --- 82
R21 | 1371 22 12 26 19 16 15 8 | 82 76 86 76 66 66 73
R22 | 2307 15 19 12 26 15 9 7 | 100 106 104 112 99 101 102
R24 | 1479 19 19 18 20 13 16 7 | 76 88 82 86 90 84 83
XR25 |10778 14 27 --- --- 14 --- 12 | 46 63 --- --- 45 --- 50
XR26E | 9860 49 --- --- 59 51 --- 37 | 39 --- --- 37 39 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1566 20 23 24 26 14 19 |T 59 63 69 63 56 55 56
WRMS | 1566 20 19 16 23 14 18 |NE 56 61 68 59 54 50 55
MEDI | 1569 17 19 18 21 13 17 |MD 59 54 60 63 48 48 50
Table 3.2324.5 GPS week: 2324 Day: 5 MJD: 60517
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1650 41 69 44 20 25 38 18 | 64 32 70 48 57 41 46
R02E | 752 16 17 17 21 15 18 7 | 30 33 31 38 29 25 27
R03E | 905 12 17 13 10 14 23 7 | 57 57 59 66 57 59 57
R04E | 1055 15 15 15 11 12 21 6 | 37 39 42 47 36 35 37
R05E | 659 18 13 18 18 13 24 7 | 50 42 46 50 41 35 41
R07E | 2468 15 10 17 28 14 17 7 | 67 62 65 72 63 63 63
R08E | 1373 13 14 31 21 8 23 8 | 122 124 129 132 123 127 124
R09 | 848 17 17 17 19 9 11 6 | 14 20 25 25 19 19 16
R11 | 1263 9 16 11 12 9 17 5 | 17 30 19 24 24 28 20
R12 | 1436 8 10 20 11 8 9 5 | 16 26 35 19 22 19 19
R13 | 907 27 22 25 44 11 32 12 | 35 44 52 29 37 49 37
R14 | 1124 11 7 17 16 12 10 5 | 16 15 22 15 17 18 14
R15 | 870 17 26 17 20 9 19 8 | 15 38 30 19 20 19 18
R16 | 1454 21 22 22 10 11 19 7 | 15 43 42 24 21 27 23
R17 | 1278 12 20 14 24 12 15 7 | 62 64 66 77 55 60 62
R18 | 1603 8 31 27 19 10 14 8 | 68 88 73 85 69 51 73
R19 | 1150 51 35 43 34 31 22 16 | 56 66 78 60 61 39 54
R20 | 3838 46 74 106 47 22 82 28 | 73 60 102 57 52 87 60
R21 | 1284 17 14 17 23 11 15 7 | 91 87 96 79 88 84 87
R22 | 2446 22 16 13 26 16 11 8 | 53 67 66 77 60 66 63
R24 | 1385 19 19 24 23 9 19 8 | 62 72 74 76 68 62 67
XR25 |10678 16 15 --- --- 11 --- 10 | 20 27 --- --- 30 --- 25
XR26E |12065 43 --- --- 52 50 --- 34 | 39 --- --- 41 45 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1585 23 29 32 24 14 26 |T 46 51 58 52 47 48 46
WRMS | 1585 19 26 18 22 13 26 |NE 40 49 55 47 42 44 42
MEDI | 1284 17 17 17 20 12 19 |MD 50 43 59 48 45 41 41
Table 3.2324.6 GPS week: 2324 Day: 6 MJD: 60518
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1773 45 62 49 23 20 38 18 | 85 34 86 74 58 38 55
R02E | 766 13 17 15 26 22 14 8 | 40 45 44 40 39 29 37
R03E | 1345 15 17 17 19 19 18 8 | 69 68 68 75 69 66 67
R04E | 1600 13 17 10 15 17 24 7 | 50 48 49 54 51 40 47
R05E | 542 18 13 11 21 15 19 7 | 54 47 47 54 53 42 48
R07E | 1933 22 8 16 21 13 19 7 | 74 69 72 73 71 68 69
R08E | 1479 19 11 19 23 11 26 8 | 128 129 133 136 129 133 130
R09 | 904 14 12 15 16 18 16 7 | 22 24 30 27 27 25 22
R11 | 1053 15 11 12 17 16 16 6 | 32 27 28 33 30 27 27
R12 | 1543 18 24 13 8 14 15 7 | 29 44 31 26 33 33 30
R13 | 591 38 21 34 42 14 39 14 | 55 45 46 55 48 58 50
R14 | 1324 11 13 19 13 13 13 6 | 28 31 37 31 31 30 28
R15 | 791 9 20 14 23 12 14 7 | 23 34 28 32 26 28 26
R16 | 901 27 19 27 9 12 14 8 | 26 45 59 32 38 34 35
R17 | 1068 17 15 9 16 13 20 6 | 91 84 87 87 81 80 83
R18 | 1666 10 28 24 17 18 17 9 | 99 120 100 112 100 64 103
R19 | 1613 44 41 54 26 28 22 16 | 105 76 124 90 86 73 87
R20 | 3131 69 68 83 37 19 53 25 | 131 83 151 89 90 90 95
R21 | 938 10 26 27 28 13 21 9 | 121 120 126 99 111 109 112
R22 | 1783 17 13 12 26 16 19 8 | 70 82 76 79 76 78 75
R24 | 1355 19 22 14 25 16 18 8 | 101 101 92 104 97 97 97
XR25 |12966 18 18 --- --- 15 --- 12 | 33 52 --- --- 45 --- 43
XR26E | 8043 52 --- --- 42 55 --- 36 | 47 --- --- 51 50 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1454 27 27 29 23 17 24 |T 65 64 72 66 62 59 61
WRMS | 1454 21 20 18 21 16 23 |NE 64 64 72 64 61 59 60
MEDI | 1355 18 17 16 21 16 19 |MD 55 48 68 55 53 58 50
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