[IGSREPORT-29963] Wk 2319 IGLOS Final Orbits
acc
acc at igs.org
Mon Jul 8 12:20:03 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2319 (Jun 16, 2024 - Jun 22, 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 2.2319.
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:
igl2319[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2319 in the SP3 format.
igl23197.sum Combination Report for GPS Week 2319.
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 | 8.5 ns
1 | 6.2 ns
2 | 9.5 ns
3 | 11.4 ns
4 | 5.8 ns
5 | 9.1 ns
6 | 3.1 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2319, 1a.2319).
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 2.2319.0-6)
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 3.2319.0-6).
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 2319 summary. (Jun 16, 2024 - Jun 22, 2024)
Table 1.2319.a GPS week : 2319 MJD: 60477.0-60483.0
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 6 4 -33 31 .08 22 16 | 17677 -540 10610 99981
| 1 1 2 9 17 20 .03 | 30141 2153
esa n/a| 0 0 1 -9 -12 5 -.12 31 21 | 5484 410 3552 9328
| 0 0 1 18 13 18 .03 | 4381 2101
gfz n/a| 0 0 1 36 -2 7 -.09 22 16 | 0 -413 3474 7853
| 1 1 2 14 18 35 .05 | 0 1864
grg n/a| 2 0 4 -46 8 -9 .39 31 22 | 25721 -473 10891 100490
| 1 1 3 19 13 42 .04 | 31294 1798
jgx n/a| 0 0 -15 -2 54 -41 -.16 26 25 | 2692 -462 3538 8096
| 1 1 2 16 10 45 .03 | 1529 1750
Table 1.2319.b GPS week : 2319 MJD: 60477.0-60483.0
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 | 21 18 20 22 22 28 21 |
R02 | 8 8 7 7 10 8 12 |
R03 | 7 10 7 8 9 10 12 |
R04 | 6 9 10 9 7 12 10 |
R05 | 7 7 8 9 7 7 10 |
R07 | 9 11 10 7 7 10 13 |
R08 | 7 9 10 9 9 10 14 |
R09 | 8 7 8 7 8 7 7 |
R11 | 8 7 7 7 7 8 6 |
R12 | 6 6 8 6 8 8 8 |
R13 | 19 17 23 18 16 14 19 |
R14 | 5 7 6 6 7 8 7 |
R15 | 11 8 6 6 6 6 6 |
R16 | 9 8 9 9 10 9 6 |
R17 | 5 7 9 6 8 6 7 |
R18 | 12 9 10 9 8 10 11 |
R19 | 19 25 26 29 22 22 25 |
R20 | 31 30 28 34 30 34 35 |
R21 | 7 6 7 7 6 7 7 |
R22 | 8 7 8 6 6 6 6 |
R24 | 9 9 11 11 9 8 7 |
R25 | 12 11 11 17 11 12 9 |
R26 | 13 29 16 17 11 21 38 |
Table 1.2319.c GPS week : 2319 MJD: 60477.0-60483.0
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 2319 0 | 87 -62 263 -153 953 6957 80.9 1921 1921 | 8534 0
brd 2319 1 | 61 160 192 -1361 4506 3408 82.2 1888 1888 | 6187 0
brd 2319 2 | -47 79 209 411 1774 -3070 79.7 1647 1647 | 9477 0
brd 2319 3 | 44 -83 171 -293 1561 3498 80.9 1813 1813 | 11438 0
brd 2319 4 | -153 119 211 -2779 -569 -1375 79.3 1650 1650 | 5807 0
brd 2319 5 | 23 -30 243 -728 -1641 -6704 78.4 1572 1572 | 9112 0
brd 2319 6 | -9 -50 235 162 -1885 -5109 82.0 1901 1901 | 3093 0
-------------+------------------------------------------------------------+----------------
brd 2319 mean| 1 18 218 -677 671 -342 80.5 1770 1770 | 7664 0
brd 2319 sdev| 81 98 31 1095 2243 5062 1.4 144 144 | 2796 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 2.2319.0 GPS week: 2319 Day: 0 MJD: 60477
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 1 9 7 -46 47 .08 24 18 | 62636 542 30863 324054
esa n/a| -1 0 2 10 -37 29 -.08 24 18 | 11209 1220 2870 9940
gfz n/a| -1 -1 0 43 19 44 -.08 18 15 | 0 -404 2821 7730
grg n/a| 1 1 6 -85 14 -34 .41 31 25 | 71913 46 32228 331025
jgx n/a| 3 0 -16 23 45 -71 -.20 26 26 | 3313 -380 2901 8091
Table 2.2319.1 GPS week: 2319 Day: 1 MJD: 60478
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 1 1 -12 -34 29 .08 20 15 | 60910 -2097 25229 324113
esa n/a| 0 0 4 -10 -1 1 -.14 29 21 | 7591 -545 3648 10340
gfz n/a| 0 0 0 36 -2 19 -.11 24 17 | 0 -1964 3696 6958
grg n/a| 2 0 6 -39 1 38 .38 23 17 | 70953 -2329 26279 330942
jgx n/a| 0 -1 -14 14 72 -99 -.16 27 27 | 301 -1632 3867 7450
Table 2.2319.2 GPS week: 2319 Day: 2 MJD: 60479
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 6 13 -18 50 .05 18 18 | 498 -1137 2952 7843
esa n/a| 0 0 1 -1 -10 25 -.15 36 25 | 8953 -215 2976 8382
gfz n/a| 0 1 1 37 -12 54 -.09 22 20 | 0 -1025 2978 6961
grg n/a| 2 0 1 -54 -11 -60 .41 29 19 | 9661 -950 2962 7034
jgx n/a| 0 0 -13 -8 57 -82 -.14 27 27 | 1661 -1070 3034 7216
Table 2.2319.3 GPS week: 2319 Day: 3 MJD: 60480
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 4 12 -47 15 .05 19 15 | 954 2066 3821 8354
esa n/a| -1 0 1 3 -12 5 -.15 34 22 | 2774 3234 3858 6982
gfz n/a| 0 0 4 5 20 0 -.14 23 17 | 0 2067 3909 7399
grg n/a| 3 0 3 -41 7 -27 .40 31 20 | 9989 1657 3930 7812
jgx n/a| 0 -2 -19 -8 63 -36 -.13 29 27 | 3939 2231 3958 7624
Table 2.2319.4 GPS week: 2319 Day: 4 MJD: 60481
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 7 -5 -3 -6 .08 21 15 | -1587 -1218 3910 9215
esa n/a| -1 0 0 2 -7 9 -.12 30 19 | 7361 -624 3953 8586
gfz n/a| 1 0 0 42 -32 6 -.14 20 13 | 0 -1208 3969 8083
grg n/a| 3 3 8 -47 29 5 .44 26 21 | 5848 -1114 3925 8464
jgx n/a| 0 0 -17 -1 49 17 -.13 25 25 | 1646 -1757 4000 7950
Table 2.2319.5 GPS week: 2319 Day: 5 MJD: 60482
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 -2 9 3 -51 42 .12 28 17 | 1040 1882 3611 9589
esa n/a| -1 -1 2 -35 -21 -16 -.12 31 24 | -159 2638 3632 8293
gfz n/a| 0 0 -3 39 -9 -43 -.09 20 15 | 0 2183 3588 7428
grg n/a| 4 0 7 -20 19 52 .39 36 27 | 7572 1976 3529 7839
jgx n/a| 0 0 -12 -26 47 -29 -.15 23 23 | 4637 1642 3609 7601
Table 2.2319.6 GPS week: 2319 Day: 6 MJD: 60483
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 1 8 11 -30 38 .12 23 17 | -708 -3818 3885 16704
esa n/a| 0 0 2 -32 0 -16 -.10 33 21 | 662 -2834 3931 12778
gfz n/a| 1 -1 4 51 -1 -26 -.00 25 13 | 0 -2545 3359 10412
grg n/a| 0 0 -1 -40 0 -39 .32 43 29 | 4117 -2600 3387 10319
jgx n/a| 0 1 -14 -9 45 10 -.19 23 23 | 3350 -2272 3401 10742
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 3.2319.0 GPS week: 2319 Day: 0 MJD: 60477
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1511 44 39 41 37 43 20 | 72 48 65 49 34 45
R02 | 2047 17 14 9 22 17 8 | 100 105 97 89 55 95
R03 | 1297 10 13 15 12 16 7 | 75 60 75 70 55 66
R04 | 797 12 12 10 14 10 5 | 93 89 89 83 68 87
R05 | 710 13 13 13 16 10 6 | 67 71 62 74 56 64
R07 | 2156 21 22 17 17 13 9 | 92 66 89 82 64 78
R08E | 2154 12 15 16 15 11 7 | 91 76 100 92 80 87
R09 | 2149 19 14 15 19 12 8 | 29 25 34 36 27 27
R11 | 3101 15 21 14 17 13 8 | 26 23 29 26 26 22
R12 | 1192 12 10 14 13 12 6 | 58 61 57 61 56 57
R13 | 1421 31 29 16 59 51 19 | 73 44 56 50 50 53
R14 | 921 8 13 9 5 9 4 | 46 55 45 47 44 46
R15 | 1178 20 21 27 23 15 11 | 67 75 54 69 61 62
R16 | 1108 16 19 17 22 16 9 | 68 82 82 64 67 72
R17 | 1960 10 12 9 12 9 5 | 74 68 74 71 67 70
XR18 | 1196 17 26 23 10 --- 12 | 56 69 53 58 --- 57
R19 | 2771 44 45 25 48 21 18 | 111 68 117 104 89 96
R20 | 3646 58 58 25 87 73 30 | 115 66 112 111 79 92
R21 | 1400 12 13 17 13 12 7 | 74 65 79 70 67 71
R22 | 2480 15 10 11 20 18 7 | 38 42 46 44 38 40
R24 | 1068 23 14 16 16 18 8 | 78 67 66 72 61 67
XR25 |11061 11 11 --- --- --- 11 | 21 27 --- --- --- 24
XR26E | 7997 13 --- --- 11 --- 12 | 58 --- --- 60 --- 58
------+------------------------------------+--------------------------------
RMS | 1921 24 24 18 31 26 |T 68 61 70 67 57 62
WRMS | 1921 18 18 15 25 26 |NE 68 61 69 67 57 62
MEDI | 1511 15 14 16 16 13 |MD 72 66 66 69 56 64
Table 3.2319.1 GPS week: 2319 Day: 1 MJD: 60478
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1611 33 38 46 23 35 17 | 46 37 62 45 30 38
R02 | 2441 11 18 12 12 20 7 | 76 83 70 71 51 73
R03 | 1102 13 12 26 14 28 9 | 52 44 60 55 32 46
XR04 | 865 13 16 15 18 --- 9 | 77 78 65 69 --- 71
R05 | 2287 9 9 16 13 15 6 | 43 45 41 47 43 42
R07 | 1349 9 21 37 21 13 10 | 61 54 86 64 56 62
R08E | 1983 9 24 25 16 12 8 | 64 57 76 69 60 63
R09 | 1864 13 17 12 13 11 6 | 17 27 27 19 23 18
R11 | 2281 12 11 18 13 13 6 | 20 26 26 29 24 22
R12 | 1337 12 14 11 7 15 6 | 52 54 54 48 48 50
XR13 | 1552 31 34 22 29 --- 17 | 55 41 41 37 --- 45
R14 | 1485 6 20 14 11 11 6 | 35 50 32 38 43 38
R15 | 1192 13 14 25 16 7 8 | 59 63 45 59 57 56
R16 | 1021 14 22 17 13 9 7 | 55 69 59 54 63 58
R17 | 1453 8 12 18 14 18 7 | 37 31 38 42 29 34
XR18 | 1272 13 18 16 12 --- 8 | 29 29 22 41 --- 28
R19 | 2587 35 77 37 52 39 24 | 57 53 63 60 44 51
R20 | 2370 52 66 36 61 81 30 | 74 65 58 58 58 59
R21 | 1547 12 12 9 10 12 5 | 41 34 40 39 40 38
R22 | 3143 13 11 13 15 13 6 | 21 26 30 27 28 23
R24 | 1246 15 10 26 15 22 9 | 40 38 51 35 30 36
XR25 |13443 8 13 --- --- --- 10 | 17 20 --- --- --- 16
XR26E | 9971 24 --- --- 33 --- 28 | 52 --- --- 69 --- 57
------+------------------------------------+--------------------------------
RMS | 1888 20 29 24 23 27 |T 46 46 49 48 42 44
WRMS | 1888 15 21 17 17 27 |NE 45 46 47 46 41 43
MEDI | 1552 13 16 18 14 13 |MD 52 44 51 47 43 45
Table 3.2319.2 GPS week: 2319 Day: 2 MJD: 60479
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1987 27 45 45 37 40 19 | 53 34 61 49 37 39
R02 | 2558 12 14 12 13 16 6 | 78 79 70 73 61 72
R03 | 889 11 14 10 13 23 7 | 61 54 55 66 42 55
R04 | 1205 15 16 19 18 26 9 | 66 68 75 69 81 67
R05 | 2775 16 15 13 14 20 8 | 59 62 54 60 51 55
R07 | 1671 16 16 21 14 25 9 | 72 60 75 66 52 65
R08E | 1700 12 21 28 14 21 10 | 75 70 98 86 74 80
R09 | 1888 12 19 19 13 11 7 | 25 27 35 21 28 24
R11 | 1948 16 11 11 20 10 7 | 23 30 30 34 29 25
R12 | 1028 12 16 19 12 14 7 | 49 45 47 52 49 46
R13 | 1385 41 38 23 62 62 23 | 63 30 49 46 39 43
R14 | 1160 9 7 13 11 12 5 | 38 38 47 47 45 42
R15 | 955 7 13 10 12 17 6 | 52 57 54 52 61 54
R16 | 1255 17 24 14 16 11 8 | 58 52 49 57 52 52
R17 | 1414 11 8 25 15 23 9 | 51 52 61 55 45 51
XR18 | 1589 7 30 14 14 --- 9 | 44 53 42 47 --- 44
R19 | 1128 21 90 20 65 45 25 | 86 55 88 98 89 81
R20 | 1339 26 104 42 60 38 28 | 67 43 86 90 77 70
R21 | 1390 13 11 10 12 22 7 | 50 49 53 56 46 49
R22 | 1826 13 16 19 14 10 7 | 36 34 37 45 34 34
R24 | 1903 22 14 19 20 25 10 | 55 52 56 48 41 48
XR25 |16879 7 16 --- --- --- 11 | 19 25 --- --- --- 21
XR26 |10921 13 --- --- 19 --- 15 | 35 --- --- 43 --- 36
------+------------------------------------+--------------------------------
RMS | 1647 18 36 22 29 27 |T 52 48 58 57 51 50
WRMS | 1647 18 25 20 19 27 |NE 52 48 55 56 51 49
MEDI | 1589 13 16 19 14 21 |MD 53 52 54 52 46 49
Table 3.2319.3 GPS week: 2319 Day: 3 MJD: 60480
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 2365 33 42 55 39 41 21 | 59 58 84 52 45 54
R02 | 2291 11 11 15 16 19 7 | 71 69 80 77 36 70
R03 | 726 18 12 9 15 21 7 | 67 54 55 62 41 56
R04 | 1665 12 10 20 12 26 8 | 69 62 68 68 62 64
R05 | 3365 11 10 19 21 27 9 | 59 60 65 63 44 56
R07 | 1833 11 11 11 12 17 6 | 74 64 68 67 61 67
R08E | 1070 9 19 18 17 22 8 | 77 69 90 85 61 77
R09 | 2156 9 19 15 13 10 7 | 21 32 30 34 34 27
R11 | 1766 9 17 16 14 16 7 | 23 36 37 26 29 27
R12 | 1099 7 13 11 14 15 6 | 36 38 36 40 31 34
R13 | 1368 26 31 17 46 59 18 | 71 49 57 52 55 57
R14 | 2074 9 7 11 13 14 5 | 45 44 42 51 34 43
R15 | 1068 11 11 10 10 11 5 | 53 44 44 54 38 47
R16 | 1178 14 20 17 14 22 8 | 54 45 41 54 59 49
R17 | 1994 9 13 10 8 15 5 | 55 47 56 55 50 52
XR18 | 1666 12 25 11 13 --- 9 | 42 55 41 47 --- 45
R19 | 1743 28 77 41 86 44 28 | 94 49 97 104 75 83
R20 | 948 43 106 47 73 64 33 | 92 64 99 104 97 85
R21 | 1148 13 11 17 12 15 7 | 58 50 51 60 55 54
R22 | 2088 12 10 11 9 14 5 | 28 35 36 38 35 32
R24 | 2114 29 15 13 17 23 10 | 63 46 48 50 42 49
XR25 |14274 13 22 --- --- --- 17 | 36 25 --- --- --- 30
XR26 |12289 13 --- --- 20 --- 16 | 37 --- --- 53 --- 43
------+------------------------------------+--------------------------------
RMS | 1813 19 34 23 31 29 |T 55 49 58 58 49 52
WRMS | 1813 15 22 17 20 27 |NE 55 48 55 58 48 51
MEDI | 1766 12 13 15 14 19 |MD 58 49 55 54 44 52
Table 3.2319.4 GPS week: 2319 Day: 4 MJD: 60481
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1231 45 42 27 44 54 21 | 132 144 137 159 148 139
R02 | 1522 11 15 29 23 14 10 | 71 69 96 65 47 73
R03 | 816 11 17 19 16 22 8 | 49 34 54 54 28 43
R04 | 1297 11 13 14 13 12 6 | 75 76 78 77 80 77
R05 | 2751 10 11 13 12 20 6 | 41 40 43 53 36 41
R07 | 1380 15 10 9 11 20 7 | 54 42 42 56 36 45
R08E | 1021 10 19 23 13 20 8 | 56 49 70 69 56 58
R09 | 1343 13 12 11 22 16 7 | 22 21 26 31 25 22
R11 | 1535 12 16 10 17 16 7 | 25 31 26 23 29 23
R12 | 1127 11 20 11 19 17 7 | 50 48 44 58 43 46
R13 | 1724 25 21 26 47 29 15 | 63 48 68 41 47 52
R14 | 2641 10 16 16 14 13 7 | 47 52 40 52 43 44
R15 | 1394 12 10 7 8 16 5 | 59 50 57 60 48 54
R16 | 882 22 26 15 11 19 9 | 65 44 48 55 59 52
R17 | 1451 7 13 19 9 21 7 | 29 23 36 31 23 27
XR18 | 2079 13 20 8 12 --- 8 | 28 32 30 27 --- 27
R19 | 2566 39 58 36 50 38 22 | 48 43 61 54 50 47
R20 | 1371 46 96 41 57 53 30 | 77 59 77 66 58 63
R21 | 1588 11 12 10 12 12 5 | 36 37 33 38 32 34
R22 | 1614 12 15 7 14 9 6 | 26 25 27 44 32 28
R24 | 1987 18 18 12 10 24 8 | 35 27 35 37 23 30
XR25 |19384 9 11 --- --- --- 10 | 20 22 --- --- --- 18
XR26E |17155 11 --- --- 11 --- 11 | 50 --- --- 54 --- 52
------+------------------------------------+--------------------------------
RMS | 1650 21 30 20 26 25 |T 50 46 53 54 47 47
WRMS | 1650 15 19 13 21 25 |NE 46 41 48 48 41 42
MEDI | 1522 12 16 14 13 19 |MD 49 42 44 54 43 45
Table 3.2319.5 GPS week: 2319 Day: 5 MJD: 60482
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 1126 83 17 37 86 30 27 | 153 132 150 164 143 141
XR02 | 1796 15 9 15 15 --- 8 | 88 76 75 76 --- 77
R03 | 759 12 14 23 27 23 10 | 53 42 60 60 35 47
R04 | 978 12 12 8 51 23 11 | 90 90 90 79 91 87
R05 | 1275 10 14 14 18 16 7 | 48 51 56 56 49 50
R07 | 1388 12 19 15 28 23 9 | 55 50 56 69 39 51
R08E | 907 14 19 21 24 18 9 | 62 55 67 85 52 62
R09 | 1623 13 16 10 18 7 6 | 29 34 36 35 31 30
R11 | 1303 15 13 21 12 12 8 | 24 30 33 25 28 24
R12 | 1336 11 18 9 19 21 8 | 47 52 41 45 43 43
R13 | 1099 24 17 16 42 35 13 | 52 48 47 40 39 43
R14 | 2405 13 26 17 13 6 8 | 38 50 26 35 35 34
R15 | 1554 10 15 9 18 11 6 | 57 66 51 49 62 56
R16 | 1820 18 26 16 9 15 9 | 61 60 56 61 51 55
R17 | 1094 10 14 7 12 12 5 | 38 35 32 41 32 33
XR18 | 1875 13 22 11 24 --- 10 | 35 37 38 33 --- 34
R19 | 3155 35 59 35 64 25 21 | 40 34 45 39 35 36
R20 | 1132 64 100 45 61 60 33 | 52 60 52 39 39 39
R21 | 1159 14 13 8 16 14 6 | 41 40 42 44 43 40
R22 | 2520 10 9 12 14 10 5 | 53 55 57 63 48 54
R24 | 875 18 11 10 14 20 7 | 42 38 38 42 34 37
XR25 |17598 12 12 --- --- --- 12 | 23 27 --- --- --- 24
XR26E |16969 17 --- --- 26 --- 21 | 37 --- --- 47 --- 36
------+------------------------------------+--------------------------------
RMS | 1571 28 31 20 36 23 |T 52 52 54 55 48 49
WRMS | 1571 17 24 15 27 23 |NE 48 48 49 49 43 44
MEDI | 1336 13 15 15 18 18 |MD 48 50 51 45 39 43
Table 3.2319.6 GPS week: 2319 Day: 6 MJD: 60483
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 973 56 42 28 36 42 21 | 102 97 93 71 81 84
XR02 | 2557 14 15 13 41 --- 11 | 85 77 80 89 --- 79
R03 | 1761 24 14 12 58 12 12 | 58 40 44 50 30 39
R04 | 2629 14 13 11 38 22 9 | 55 49 44 72 47 48
R05 | 1190 13 12 10 50 17 10 | 61 67 64 74 66 63
R07 | 1204 14 16 17 68 9 12 | 68 56 62 101 52 61
R08E | 968 17 16 23 71 14 14 | 87 79 93 127 71 85
R09 | 1716 13 14 13 23 10 7 | 30 25 35 29 29 27
R11 | 2368 11 8 10 20 13 6 | 32 31 32 32 31 30
R12 | 1114 17 15 18 11 7 7 | 63 72 63 66 60 64
R13 | 969 30 20 18 69 48 18 | 79 64 74 59 45 63
R14 | 1967 8 19 9 14 14 6 | 56 70 59 57 53 58
R15 | 1470 14 10 9 19 9 6 | 82 82 79 71 76 78
R16 | 2196 12 9 10 18 8 5 | 89 86 77 77 84 83
R17 | 1814 10 9 13 15 21 7 | 45 38 41 46 30 38
XR18 | 1477 18 24 13 16 --- 10 | 33 40 34 35 --- 33
R19 | 3546 33 71 47 75 25 25 | 75 53 91 75 67 70
R20 | 2948 45 105 74 62 48 34 | 100 44 112 91 66 77
R21 | 1469 11 10 15 12 20 7 | 50 43 53 53 42 46
R22 | 2047 13 9 11 12 12 5 | 48 55 55 62 52 53
R24 | 1164 14 10 13 15 12 6 | 48 46 46 54 42 44
XR25 |16640 9 8 --- --- --- 9 | 21 22 --- --- --- 21
XR26 |15844 23 --- --- 60 --- 38 | 51 --- --- 85 --- 54
------+------------------------------------+--------------------------------
RMS | 1900 23 33 25 43 23 |T 61 56 63 67 53 56
WRMS | 1900 17 21 13 29 23 |NE 58 53 60 62 51 53
MEDI | 1761 14 14 13 23 14 |MD 58 53 62 66 52 58
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