[IGSREPORT-29648] Wk 2291 IGLOS Final Orbits
acc
acc at igs.org
Sun Dec 24 08:52:50 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2291 (Dec 03, 2023 - Dec 09, 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 2.2291.
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:
igl2291[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2291 in the SP3 format.
igl22917.sum Combination Report for GPS Week 2291.
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).
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.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 | -0.5 ns
1 | -1.0 ns
2 | 0.3 ns
3 | -1.5 ns
4 | -1.0 ns
5 | 0.8 ns
6 | -24.8 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 1.2291, 1a.2291).
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 2.2291.0-6)
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 3.2291.0-6).
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 2291 summary. (Dec 03, 2023 - Dec 09, 2023)
Table 1.2291.a GPS week : 2291 MJD: 60281.0-60287.0
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 2 -1 2 -17 59 .16 25 19 | 39014 -3281 3586 13744
| 0 1 3 16 11 23 .03 | 8294 7477
esa n/a| 0 1 0 -33 4 -19 -.14 31 20 | 9592 -3990 3585 12243
| 0 0 2 17 14 20 .03 | 15402 7528
gfz n/a| 0 1 -3 9 13 -7 -.02 19 14 | 0 -3267 3517 13382
| 0 1 1 20 13 27 .02 | 0 7618
grg n/a| 1 -4 2 8 -12 2 .31 33 24 | -2554 -3244 3516 13097
| 0 1 1 21 14 25 .06 | 5430 7618
iac n/a| 0 0 -7 0 16 -15 -.12 23 19 | -1628 -1445 3582 14034
| 0 2 2 16 37 65 .03 | 7906 3057
jgx n/a| 0 1 4 9 1 -13 -.18 22 21 | 41051 -3295 3514 13448
| 1 1 3 16 20 43 .04 | 7787 7831
Table 1.2291.b GPS week : 2291 MJD: 60281.0-60287.0
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 | 18 16 18 16 19 17 20 |
R02 | 10 6 6 8 9 8 9 |
R03 | 8 5 7 8 8 8 9 |
R04 | 10 8 9 7 7 10 10 |
R05 | 7 7 6 5 6 7 7 |
R07 | 10 10 9 10 10 8 9 |
R08 | 6 7 9 7 6 9 7 |
R09 | 6 7 8 8 7 8 8 |
R11 | 6 7 7 7 6 7 6 |
R12 | 6 9 8 8 8 9 9 |
R13 | 19 18 16 17 16 17 20 |
R14 | 7 7 7 6 7 7 8 |
R15 | 9 8 10 8 8 9 8 |
R16 | 9 9 9 9 6 8 8 |
R17 | 9 11 8 7 6 9 8 |
R18 | 10 8 9 8 7 8 9 |
R19 | 28 24 25 27 24 24 25 |
R20 | 31 29 30 35 35 35 32 |
R21 | 8 9 6 7 8 7 9 |
R22 | 8 8 7 8 6 7 6 |
R24 | 11 10 9 9 9 8 9 |
R25 | 12 12 0 0 --- --- 0 |
R26 | 25 40 27 26 --- 0 0 |
Table 1.2291.c GPS week : 2291 MJD: 60281.0-60287.0
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 2291 0 | 12 3 -108 -554 487 -2087 81.7 1297 1297 | -502 0
brd 2291 1 | 24 -12 -58 245 -965 -3257 80.3 1384 1384 | -987 0
brd 2291 2 | 59 -41 -30 2327 478 694 80.1 1505 1505 | 343 0
brd 2291 3 | 9 12 -73 2097 744 2235 78.8 1652 1652 | -1487 0
brd 2291 4 | 33 34 -68 -983 1370 6820 78.3 1362 1362 | -973 0
brd 2291 5 | -44 61 -66 458 257 -3462 81.6 1308 1308 | 842 0
brd 2291 6 | 1 -32 -55 -125 639 102 81.2 1331 1331 | -24837 0
-------------+------------------------------------------------------------+----------------
brd 2291 mean| 13 3 -65 494 430 149 80.3 1405 1405 | -3943 0
brd 2291 sdev| 32 36 23 1268 708 3623 1.3 128 128 | 9248 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 2.2291.0 GPS week: 2291 Day: 0 MJD: 60281
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 2 -28 60 .10 19 15 | 39199 -491 3460 16308
esa n/a| 0 1 3 -6 10 -27 -.16 33 24 | 26050 -1535 3456 14950
gfz n/a| 0 1 -1 38 7 -1 -.05 22 17 | 0 206 3068 14725
grg n/a| 0 -6 3 -27 0 -20 .24 29 28 | -671 225 3069 14372
iac n/a| -1 2 -8 -10 13 -32 -.16 20 18 | 133 -293 3462 16164
jgx n/a| -1 3 0 -4 28 12 -.23 28 28 | 42654 5 3053 14722
Table 2.2291.1 GPS week: 2291 Day: 1 MJD: 60282
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 0 12 -22 84 .17 25 19 | 40418 -1951 2939 16421
esa n/a| 0 1 3 -29 -4 -40 -.19 29 23 | 24103 -2422 2924 13095
gfz n/a| 0 0 -4 1 12 -36 -.04 19 13 | 0 -1669 2873 16131
grg n/a| 0 -4 1 -16 -16 -7 .29 25 21 | -155 -1917 2885 15764
iac n/a| 0 1 -4 12 -29 84 -.08 21 16 | 505 -1312 2927 16679
jgx n/a| 1 2 2 32 21 4 -.23 23 23 | 43065 -2463 2909 15767
Table 2.2291.2 GPS week: 2291 Day: 2 MJD: 60283
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 3 3 -4 -31 49 .17 26 17 | 41785 2180 2724 15344
esa n/a| 1 1 -1 -32 13 -28 -.13 27 18 | 9619 1558 2714 12812
gfz n/a| 0 1 -4 15 9 -42 -.00 18 12 | 0 1851 2721 15266
grg n/a| 0 -3 3 12 -12 3 .30 30 24 | -841 2051 2700 14997
iac n/a| -1 0 -8 -13 -2 -128 -.12 27 21 | 1827 338 2722 15950
jgx n/a| 0 0 3 -6 -1 28 -.17 20 18 | 43987 1222 2637 15318
Table 2.2291.3 GPS week: 2291 Day: 3 MJD: 60284
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 3 1 -13 3 56 .13 25 19 | 43514 -3083 2892 16092
esa n/a| 1 1 1 -31 21 -37 -.16 33 17 | 19092 -3116 2879 13915
gfz n/a| 0 0 -4 0 16 -22 -.02 19 12 | 0 -2514 2874 16075
grg n/a| 1 -4 0 27 -22 -23 .42 34 22 | -464 -2597 2895 15746
iac n/a| 0 0 -10 21 26 -45 -.12 27 23 | 1363 -1394 2889 16622
jgx n/a| 0 2 4 16 -15 26 -.14 19 19 | 44816 -2146 2832 16322
Table 2.2291.4 GPS week: 2291 Day: 4 MJD: 60285
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 2 -2 -8 -18 71 .18 29 23 | 42171 -1069 3601 14476
esa n/a| 0 1 1 -45 -1 -17 -.09 31 17 | -8632 -2017 3578 13982
gfz n/a| 1 1 -2 34 22 25 -.03 17 11 | 0 -1613 3572 14276
grg n/a| 1 -3 4 22 4 5 .30 39 23 | -573 -1368 3580 14084
iac n/a| 0 1 -4 -4 -10 16 -.10 20 19 | 610 -1834 3587 15119
jgx n/a| 0 0 4 -6 -10 -36 -.13 18 18 | 42785 -1079 3632 14485
Table 2.2291.5 GPS week: 2291 Day: 5 MJD: 60286
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 -5 -5 -10 13 .17 27 21 | 45272 1190 4954 9483
esa n/a| 0 0 -2 -25 13 10 -.14 34 21 | 10113 265 4968 9047
gfz n/a| 1 3 0 -10 -6 -1 -.00 17 13 | 0 1032 4958 9380
grg n/a| 2 -4 5 27 -35 51 .32 35 25 | -315 1001 4895 9412
iac n/a| 0 -2 -6 -24 85 -9 -.11 22 20 | 3534 2069 4963 9963
jgx n/a| 0 0 5 8 15 -46 -.19 19 19 | 46402 2046 4950 9616
Table 2.2291.6 GPS week: 2291 Day: 6 MJD: 60287
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 -4 35 -15 80 .17 26 21 | 20745 -19749 4538 8090
esa n/a| 0 0 -2 -63 -22 6 -.12 29 20 | -13196 -20665 4581 7904
gfz n/a| 0 0 -3 -13 36 26 -.03 20 19 | 0 -20168 4557 7823
grg n/a| 2 -5 2 11 -1 7 .27 36 24 | -14859 -20109 4591 7306
iac n/a| 0 -3 -10 13 32 9 -.13 24 19 | -19373 -7694 4528 7742
jgx n/a| 0 0 9 27 -25 -86 -.16 22 22 | 23649 -20651 4585 7911
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 3.2291.0 GPS week: 2291 Day: 0 MJD: 60281
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1076 48 33 15 26 16 43 18 | 101 56 65 63 77 55 67
R02 | 1221 7 35 17 17 14 12 9 | 66 88 63 63 72 67 68
R03 | 775 9 15 16 16 18 20 7 | 91 80 97 97 96 78 88
R04 | 594 19 10 14 11 20 32 9 | 101 83 95 88 80 69 88
R05 | 928 12 13 16 14 18 17 7 | 91 95 103 93 84 84 93
R07 | 941 17 13 25 24 11 16 9 | 102 83 100 84 92 83 91
R08 | 1390 12 11 8 15 18 15 6 | 81 81 83 88 94 81 82
R09 | 1729 11 16 11 10 14 9 6 | 50 56 55 49 50 49 51
R11 | 2550 11 12 14 10 12 9 5 | 36 45 50 48 43 40 42
R12 | 920 8 10 11 14 31 13 5 | 69 69 68 60 67 54 64
R13 | 448 32 31 37 20 26 62 19 | 90 60 102 74 81 43 77
R14 | 633 9 14 13 12 17 20 7 | 57 66 64 57 61 47 58
R15 | 1052 18 12 13 20 14 18 8 | 73 56 61 60 60 50 60
R16 | 1377 16 14 22 17 19 18 9 | 72 56 74 58 70 50 61
XR17 | 771 11 18 19 14 14 --- 9 | 25 28 28 27 24 --- 25
R18 | 713 9 19 18 20 13 27 9 | 33 37 38 37 29 35 34
R19 | 2269 28 68 38 79 29 58 27 | 32 27 36 26 24 48 29
R20 | 1168 27 104 54 68 41 40 30 | 45 39 77 48 41 52 47
R21 | 1376 8 19 24 9 10 18 8 | 27 24 38 33 25 27 27
R22 | 1769 11 17 13 21 11 15 7 | 44 37 46 48 45 43 42
R24 | 581 15 15 10 36 14 22 10 | 32 37 31 36 26 27 30
XR25 | 7375 9 14 --- --- 24 --- 11 | 9999 21 --- --- 1 --- 9999
XR26 |14393 21 --- 28 --- 86 --- 24 | 1 --- 34 --- 1 --- 1
------+-----------------------------------------+-------------------------------------
RMS | 1296 19 33 22 29 20 28 |T 59 55 64 58 54 54 55
WRMS | 1296 15 24 17 28 18 28 |NE 59 55 64 58 54 54 55
MEDI | 1076 12 15 16 17 17 18 |MD 57 56 63 58 60 50 58
Table 3.2291.1 GPS week: 2291 Day: 1 MJD: 60282
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1234 48 21 14 30 17 40 16 | 68 41 47 48 54 36 46
R02 | 743 5 20 11 8 11 9 5 | 52 63 51 61 50 50 54
R03 | 865 8 9 6 12 14 11 4 | 67 68 72 78 71 70 70
R04 | 671 21 12 15 11 13 21 8 | 72 61 84 66 58 56 68
R05 | 826 14 12 10 13 17 15 6 | 76 69 73 72 58 70 71
R07 | 1134 14 18 22 20 16 17 9 | 73 61 80 65 69 66 68
R08 | 1363 17 13 16 8 14 16 7 | 62 52 72 57 62 54 59
R09 | 939 14 18 11 13 11 10 6 | 55 59 61 58 48 52 56
R11 | 1910 14 16 11 12 13 11 6 | 40 48 48 46 43 45 45
R12 | 1294 17 22 23 11 18 9 8 | 57 61 47 54 48 46 51
R13 | 878 25 26 32 33 25 51 17 | 71 55 88 75 68 47 66
R14 | 1252 11 13 9 14 14 16 6 | 50 57 57 58 48 46 52
R15 | 1432 16 15 12 11 8 19 7 | 58 53 61 58 54 46 54
R16 | 2195 21 15 16 17 21 20 9 | 59 57 61 56 60 48 54
XR17 | 577 12 15 18 23 21 --- 10 | 31 37 40 40 32 --- 34
R18 | 1585 12 23 12 15 12 17 8 | 43 48 52 48 36 45 46
R19 | 1884 56 55 31 61 31 30 23 | 39 53 51 50 35 54 47
R20 | 2036 57 89 47 50 61 45 29 | 56 55 60 61 40 66 52
R21 | 1667 8 25 17 21 15 19 9 | 33 29 42 38 31 36 34
R22 | 1539 14 16 15 19 16 14 8 | 37 34 41 44 37 38 37
R24 | 652 10 25 8 31 8 19 10 | 31 38 34 36 31 31 32
XR25 | 9646 11 11 --- --- 31 --- 11 | 1 19 --- --- 1 --- 1
XR26 |12652 44 --- 36 --- 89 --- 40 | 1 --- 42 --- 1 --- 1
------+-----------------------------------------+-------------------------------------
RMS | 1384 25 29 19 25 21 23 |T 49 50 57 55 45 50 47
WRMS | 1384 19 23 13 21 16 23 |NE 49 50 57 55 45 50 47
MEDI | 1294 14 16 15 15 16 17 |MD 55 53 52 57 48 47 52
Table 3.2291.2 GPS week: 2291 Day: 2 MJD: 60283
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 779 49 36 25 28 21 37 18 | 73 37 69 46 63 42 50
R02 | 769 6 12 13 13 22 15 6 | 49 54 56 56 50 43 51
R03 | 1121 8 11 8 26 17 12 7 | 69 64 63 87 77 62 67
R04 | 592 18 17 14 21 16 14 8 | 60 61 51 45 57 49 51
R05 | 928 10 8 9 18 16 10 5 | 61 59 60 49 63 51 56
R07 | 1086 22 9 17 23 20 13 8 | 82 71 75 63 81 63 70
R08 | 991 13 13 21 12 22 19 8 | 62 61 80 68 81 60 66
R09 | 827 12 16 14 17 23 15 7 | 33 39 39 33 46 34 33
R11 | 1239 17 13 11 13 15 10 6 | 42 53 55 47 40 44 47
R12 | 1893 10 19 13 14 15 20 8 | 59 63 59 62 62 45 56
XR13 | 676 30 28 13 38 19 --- 15 | 74 50 64 49 54 --- 59
R14 | 832 9 15 11 17 11 13 6 | 52 63 59 62 49 46 55
R15 | 2221 13 20 25 10 25 23 10 | 62 61 80 67 47 52 64
R16 | 2533 24 18 13 10 10 19 9 | 61 57 61 51 54 42 53
XR17 | 510 10 16 8 21 14 --- 8 | 17 17 18 25 18 --- 15
R18 | 1418 9 29 14 19 12 14 8 | 18 22 23 22 16 19 17
R19 | 1514 43 59 40 75 38 27 24 | 33 36 29 29 24 27 22
R20 | 3134 77 70 27 76 79 47 30 | 45 52 55 47 19 71 43
R21 | 1471 11 12 7 18 26 11 6 | 21 19 24 24 27 19 19
R22 | 1437 14 12 13 22 23 9 7 | 50 58 52 56 53 51 52
R24 | 997 19 17 11 25 12 13 8 | 26 21 22 28 17 15 18
XR25 | 8848 5 --- --- --- --- --- 0 | 1 --- --- --- --- --- 1
XR26 |10112 32 --- 22 --- 83 --- 27 | 1 --- 29 --- 1 --- 1
------+-----------------------------------------+-------------------------------------
RMS | 1505 26 27 18 30 27 20 |T 45 48 51 48 45 43 42
WRMS | 1505 17 18 12 24 21 18 |NE 45 48 51 48 45 43 42
MEDI | 1121 13 16 13 19 19 14 |MD 50 54 55 49 49 45 51
Table 3.2291.3 GPS week: 2291 Day: 3 MJD: 60284
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1209 43 34 22 23 29 28 15 | 75 36 66 44 65 33 48
R02 | 708 13 11 20 19 25 10 7 | 51 51 70 45 37 48 53
R03 | 813 14 19 10 20 24 17 8 | 68 46 64 77 77 51 60
R04 | 892 19 9 13 13 14 8 6 | 61 44 44 59 55 44 48
R05 | 915 8 15 9 15 13 7 5 | 50 58 45 49 49 47 48
R07 | 1508 20 16 18 24 17 17 9 | 77 56 78 59 77 53 65
R08 | 818 14 15 16 15 45 11 7 | 69 74 65 65 103 60 65
R09 | 590 14 24 12 20 36 9 7 | 27 36 34 18 52 28 26
R11 | 970 11 15 13 23 7 10 7 | 24 35 25 35 27 22 25
R12 | 1689 11 15 14 23 19 15 7 | 54 56 59 40 61 42 49
XR13 | 4514 25 19 19 51 20 --- 17 | 88 75 82 49 77 --- 73
R14 | 704 11 16 11 13 13 8 6 | 58 71 66 65 64 57 62
R15 | 2339 17 16 11 16 12 19 8 | 73 67 63 70 60 49 62
R16 | 1310 16 25 15 11 19 21 9 | 70 68 74 69 60 54 65
XR17 | 527 5 17 11 11 12 --- 6 | 19 17 20 22 16 --- 16
R18 | 535 14 20 8 20 16 19 8 | 21 18 22 24 17 20 18
R19 | 3022 54 57 22 90 33 44 26 | 40 50 61 29 41 56 43
R20 | 4220 60 109 59 95 69 33 35 | 43 93 93 33 33 53 55
R21 | 1771 14 10 10 15 13 14 6 | 22 21 26 27 16 20 20
R22 | 1365 24 11 13 13 19 9 7 | 16 28 33 23 23 25 22
R24 | 745 17 13 11 18 13 22 8 | 24 20 17 24 22 21 17
XR25 |13630 4 --- --- --- --- --- 0 | 1 --- --- --- --- --- 1
XR26 | 6284 30 --- 22 --- 65 --- 25 | 1 --- 43 --- 1 --- 1
------+-----------------------------------------+-------------------------------------
RMS | 1651 25 33 19 34 27 19 |T 44 48 52 44 46 41 40
WRMS | 1651 19 17 12 22 23 19 |NE 44 48 52 44 46 41 40
MEDI | 1209 14 16 13 19 19 15 |MD 50 50 59 44 49 47 48
Table 3.2291.4 GPS week: 2291 Day: 4 MJD: 60285
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 565 68 19 25 40 15 33 19 | 81 55 40 34 48 52 45
R02 | 1065 11 22 13 30 16 14 8 | 53 55 55 34 47 38 45
R03 | 1785 7 15 19 11 14 15 7 | 69 55 75 64 70 62 65
R04 | 775 23 12 9 11 21 13 7 | 63 45 54 50 58 45 50
R05 | 892 12 12 9 22 11 9 6 | 49 62 55 69 52 52 55
R07 | 1191 22 18 17 12 12 21 9 | 76 58 71 66 66 53 63
R08 | 1448 13 10 11 17 27 11 6 | 63 57 60 63 75 51 58
R09 | 1094 20 12 10 17 26 11 7 | 47 54 57 46 45 48 50
R11 | 1276 11 9 14 19 15 9 6 | 41 42 52 49 43 41 44
R12 | 1416 13 17 11 20 26 14 7 | 57 59 51 48 67 52 52
R13 | 829 46 21 21 30 17 35 15 | 86 55 70 57 60 64 60
R14 | 865 14 20 9 18 10 7 6 | 61 78 69 64 65 62 66
R15 | 1507 24 9 12 16 11 14 7 | 76 60 67 57 62 55 62
R16 | 801 19 15 8 13 17 8 6 | 65 66 59 56 55 53 58
XR17 | 1214 9 14 10 10 25 --- 6 | 28 28 33 27 31 --- 28
R18 | 873 15 15 6 17 17 16 7 | 34 32 34 27 30 25 28
R19 | 2645 47 69 16 90 31 25 24 | 28 49 49 38 35 24 32
R20 | 2544 58 101 52 121 42 31 35 | 35 73 71 47 49 57 43
R21 | 1272 16 15 8 23 13 18 8 | 27 28 28 34 31 30 27
R22 | 1230 13 8 11 19 18 8 6 | 41 50 46 51 45 49 46
R24 | 984 22 20 11 28 13 16 9 | 27 36 33 30 32 30 28
------+-----------------------------------------+-------------------------------------
RMS | 1361 29 31 17 39 20 18 |T 52 52 53 48 48 47 47
WRMS | 1361 23 17 11 23 19 18 |NE 52 52 53 48 48 47 47
MEDI | 1191 16 15 11 19 17 14 |MD 53 55 55 49 48 51 50
Table 3.2291.5 GPS week: 2291 Day: 5 MJD: 60286
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 628 59 35 17 21 15 28 17 | 69 28 44 40 31 27 36
R02 | 915 10 25 15 17 19 8 7 | 49 58 45 45 58 49 47
R03 | 1076 11 11 16 18 23 14 7 | 58 51 58 49 62 45 51
R04 | 613 33 11 13 19 14 18 10 | 64 43 52 42 47 33 44
R05 | 1277 15 7 10 14 12 16 6 | 52 47 50 38 47 39 44
R07 | 1340 18 10 15 15 18 17 7 | 59 54 56 58 55 46 53
R08 | 1931 14 10 21 15 16 17 8 | 50 46 65 55 45 43 51
R09 | 1631 19 13 12 21 22 12 7 | 36 45 44 36 42 34 37
R11 | 1840 12 12 14 20 19 10 7 | 32 36 30 37 34 36 32
R12 | 1482 13 24 20 23 18 9 9 | 59 60 43 41 57 42 46
R13 | 1387 47 21 19 39 23 34 16 | 75 61 59 53 66 56 60
R14 | 1139 8 12 15 12 13 15 6 | 53 56 60 55 61 45 53
R15 | 1022 27 16 12 21 10 11 8 | 65 58 38 39 52 45 46
R16 | 799 26 15 12 13 25 12 8 | 59 47 41 46 42 40 44
XR17 | 695 17 20 11 11 15 --- 8 | 18 27 23 19 17 --- 18
R18 | 638 10 9 17 18 16 20 8 | 21 24 32 31 19 17 22
R19 | 2297 22 75 26 74 34 40 24 | 39 32 36 35 26 22 29
R20 | 1234 58 112 38 109 47 29 34 | 31 62 47 28 31 32 28
R21 | 1263 13 19 11 20 20 11 7 | 18 24 23 21 21 22 18
R22 | 1242 14 17 9 19 16 10 6 | 42 46 53 49 51 43 45
R24 | 877 24 19 10 12 26 15 8 | 30 23 19 25 22 21 19
XR26 |11934 --- --- --- 7 --- --- 0 | --- --- --- 9 --- --- 1
------+-----------------------------------------+-------------------------------------
RMS | 1307 27 34 17 35 22 19 |T 46 44 43 38 42 36 37
WRMS | 1307 21 21 13 25 20 19 |NE 46 44 43 38 42 36 37
MEDI | 1234 17 16 15 18 18 15 |MD 50 46 44 39 45 39 44
Table 3.2291.6 GPS week: 2291 Day: 6 MJD: 60287
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 658 65 29 23 37 24 35 20 | 89 42 55 53 60 47 50
R02 | 876 10 16 21 17 19 17 8 | 58 67 50 57 53 56 55
R03 | 668 18 11 18 23 24 15 8 | 78 66 83 67 84 62 70
R04 | 510 24 13 22 25 22 16 10 | 83 60 76 59 65 56 66
R05 | 885 17 8 16 12 13 15 7 | 74 65 72 63 64 60 66
R07 | 1312 13 18 22 11 14 20 9 | 87 76 94 81 84 63 79
R08 | 2770 13 13 12 21 23 11 7 | 74 72 70 82 80 62 70
R09 | 1333 15 18 17 16 15 13 8 | 46 54 46 46 51 43 45
R11 | 2017 15 12 10 12 20 11 6 | 40 43 48 45 40 42 43
R12 | 934 20 15 21 14 13 19 9 | 72 68 80 57 67 57 66
R13 | 986 47 19 30 38 22 54 20 | 99 77 99 72 76 69 84
R14 | 1202 7 13 18 26 15 13 8 | 77 88 92 69 83 69 79
R15 | 1117 18 9 12 15 10 21 8 | 96 85 83 76 84 66 81
R16 | 841 17 16 11 12 16 18 7 | 84 80 77 75 71 58 74
XR17 | 742 10 15 18 9 19 --- 8 | 26 24 26 25 24 --- 22
R18 | 601 7 26 18 15 13 15 8 | 27 30 33 34 23 25 27
R19 | 759 35 64 22 85 47 35 25 | 40 35 35 26 30 37 31
R20 | 2667 52 87 38 103 54 30 31 | 37 46 37 42 27 36 25
R21 | 1249 16 20 12 22 20 15 8 | 23 21 26 26 22 19 19
R22 | 1491 13 13 12 13 22 8 6 | 57 56 62 60 67 58 58
R24 | 652 12 22 19 22 23 12 8 | 25 32 31 29 21 22 24
XR25 | 8838 6 --- --- --- 92 --- 0 | 1 --- --- --- 1 --- 1
XR26 |16062 6 --- --- --- 26 --- 0 | 1 --- --- --- 1 --- 1
------+-----------------------------------------+-------------------------------------
RMS | 1331 26 29 20 36 24 22 |T 56 56 60 54 51 50 49
WRMS | 1331 21 20 19 24 19 22 |NE 56 56 60 54 51 50 49
MEDI | 986 15 16 18 17 20 15 |MD 58 60 62 57 60 56 55
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