[IGSREPORT-30083] Wk 2330 IGLOS Final Orbits
acc
acc at igs.org
Fri Sep 20 03:30:23 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2330 (Sep 01, 2024 - Sep 07, 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 2.2330.
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:
igl2330[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2330 in the SP3 format.
igl23307.sum Combination Report for GPS Week 2330.
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 | 6.7 ns
1 | 6.4 ns
2 | 4.8 ns
3 | 5.6 ns
4 | 7.5 ns
5 | 4.7 ns
6 | 4.5 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
----+--------+---------------
1 | IAC | R20
2 | IAC | R20 R21
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 1.2330, 1a.2330).
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 2.2330.0-6)
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 3.2330.0-6).
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 2330 summary. (Sep 01, 2024 - Sep 07, 2024)
Table 1.2330.a GPS week : 2330 MJD: 60554.0-60560.0
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| 0 -1 3 -27 -12 55 .09 17 13 | -829 -520 3704 16385
| 1 0 1 8 19 32 .03 | 1526 2557
esa n/a| 0 -1 0 7 -19 2 -.10 23 15 | 8517 -336 3049 7428
| 1 1 1 13 9 26 .03 | 6220 2090
gfz n/a| 0 0 0 46 28 -7 -.01 23 14 | 0 -239 3079 8088
| 1 1 1 8 12 26 .05 | 0 2584
grg n/a| 1 1 1 -22 -10 -51 .40 23 17 | 2926 -535 3777 16242
| 0 1 2 20 21 37 .03 | 1241 2674
iac n/a| 0 0 -6 30 44 -47 -.21 295 38 | 5137 -642 3683 15488
| 1 1 2 29 25 58 .07 | 1480 1017
jgx n/a| 0 0 -1 -46 -31 18 -.20 29 29 | 4135 -341 3077 8155
| 1 0 1 17 23 19 .05 | 1427 2492
Table 1.2330.b GPS week : 2330 MJD: 60554.0-60560.0
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 | 13 13 14 14 12 11 11 |
R02 | 7 7 10 8 7 7 8 |
R03 | 6 6 6 5 9 8 7 |
R04 | 8 7 7 6 8 5 7 |
R05 | 7 8 6 6 7 6 6 |
R07 | 7 8 6 5 7 6 7 |
R08 | 7 6 8 6 7 6 6 |
R09 | 7 6 7 7 7 7 6 |
R11 | 7 9 7 7 6 6 7 |
R12 | 10 7 6 6 8 9 7 |
R14 | 6 6 6 5 6 6 6 |
R15 | 9 8 9 8 6 6 6 |
R16 | 7 7 6 8 8 8 8 |
R17 | 7 7 7 7 6 7 6 |
R18 | 7 6 6 7 7 7 7 |
R19 | 22 17 18 23 21 22 20 |
R20 | 27 27 27 24 28 33 29 |
R21 | 6 15 7 5 6 7 6 |
R22 | 6 7 7 6 7 6 7 |
R24 | 7 7 9 7 7 7 9 |
R25 | 9 11 10 8 10 8 10 |
R26 | 31 31 30 27 30 39 36 |
Table 1.2330.c GPS week : 2330 MJD: 60554.0-60560.0
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 2330 0 | 29 -42 -8 199 578 -4593 80.3 1848 1848 | 6685 0
brd 2330 1 | -9 -80 45 793 1416 -6504 80.1 1619 1619 | 6441 0
brd 2330 2 | 58 94 92 634 350 -5522 81.3 1357 1357 | 4779 0
brd 2330 3 | 12 70 111 -1548 -365 -7481 81.1 1457 1457 | 5622 0
brd 2330 4 | -10 11 36 -1120 1350 -8371 79.9 1526 1526 | 7527 0
brd 2330 5 | -17 17 106 -1143 910 -5804 78.9 1587 1587 | 4730 0
brd 2330 6 | -37 -3 87 -356 -357 -8541 80.3 1810 1810 | 4475 0
-------------+------------------------------------------------------------+----------------
brd 2330 mean| 3 9 67 -362 554 -6688 80.3 1600 1600 | 5751 0
brd 2330 sdev| 32 60 43 933 732 1497 .8 178 178 | 1164 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 2.2330.0 GPS week: 2330 Day: 0 MJD: 60554
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 4 -30 16 63 .12 16 14 | -728 -962 2913 12265
esa n/a| 0 -3 0 25 -36 -40 -.13 23 16 | 11820 -604 2693 6783
gfz n/a| 1 0 0 53 27 -39 .02 27 15 | 0 -838 2739 6756
grg n/a| 1 3 0 -17 -15 -22 .40 27 16 | 5000 -1133 2955 11908
iac n/a| -1 0 -7 4 70 -35 -.21 22 18 | 6753 -754 2870 11494
jgx n/a| 1 0 -1 -58 -54 22 -.23 26 26 | 3394 -782 2746 6946
Table 2.2330.1 GPS week: 2330 Day: 1 MJD: 60555
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 -29 -33 32 .07 17 13 | -1809 3229 4109 16546
esa n/a| 1 -1 1 13 -17 22 -.14 25 18 | -395 2794 3180 8412
gfz n/a| 0 -2 1 40 30 -33 -.07 18 15 | 0 3921 3153 8279
grg n/a| 1 2 5 -47 -17 -69 .39 22 16 | 1610 3620 4174 16440
iac n/a| 0 0 -10 89 70 3 -.11 40 17 | 5853 309 4098 15665
jgx n/a| 0 0 -2 -62 -16 30 -.25 26 26 | 2977 3655 3141 8309
Table 2.2330.2 GPS week: 2330 Day: 2 MJD: 60556
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 2 -19 -35 119 .05 18 13 | 390 -3013 3296 15762
esa n/a| 1 -3 1 5 -14 16 -.08 21 15 | 9955 -2762 2958 5738
gfz n/a| 0 0 0 32 16 23 -.05 20 13 | 0 -2863 2986 6999
grg n/a| 2 0 2 -39 -33 -77 .45 23 20 | 3337 -3237 3325 15590
iac n/a| -1 1 -6 40 58 -136 -.14 1915 159 | 5052 -1532 3276 14831
jgx n/a| 0 0 -2 -52 11 50 -.15 28 28 | 6224 -2846 2972 6897
Table 2.2330.3 GPS week: 2330 Day: 3 MJD: 60557
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 3 -16 -3 55 .08 17 11 | -2431 491 3553 16689
esa n/a| 0 -2 -2 -17 -18 -8 -.11 22 17 | 11833 -125 2783 7059
gfz n/a| -1 0 -1 43 10 -34 -.08 24 14 | 0 -242 2803 8684
grg n/a| 1 0 2 -30 7 11 .39 18 14 | 2244 207 3623 16723
iac n/a| 1 3 -2 32 40 -87 -.27 26 20 | 3480 633 3531 15801
jgx n/a| 0 0 0 -18 -30 5 -.25 28 29 | 2847 -229 2836 8717
Table 2.2330.4 GPS week: 2330 Day: 4 MJD: 60558
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 3 -32 -8 45 .09 16 11 | 843 1795 3936 16272
esa n/a| 0 -1 0 19 -29 -19 -.07 22 14 | 11447 2021 3427 8312
gfz n/a| 0 1 1 47 30 8 .00 26 14 | 0 2579 3479 8209
grg n/a| 0 1 0 -11 28 -37 .36 24 18 | 3585 1812 4047 16065
iac n/a| 1 0 -5 24 6 -88 -.30 23 18 | 6942 -7 3907 15357
jgx n/a| 0 0 -3 -60 -36 24 -.13 30 30 | 5458 2268 3421 8286
Table 2.2330.5 GPS week: 2330 Day: 5 MJD: 60559
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 5 -22 3 60 .06 20 14 | 709 -3972 4387 17700
esa n/a| 0 1 0 3 -8 14 -.11 21 12 | 15164 -2256 3433 7995
gfz n/a| -1 0 1 53 39 9 .06 24 16 | 0 -2637 3474 8446
grg n/a| 1 1 -1 -20 -25 -95 .41 26 19 | 3216 -3949 4512 17507
iac n/a| -1 0 -9 21 16 -4 -.24 24 19 | 4697 -2182 4391 16664
jgx n/a| 2 1 -1 -39 -36 -8 -.22 34 36 | 5148 -2899 3533 8623
Table 2.2330.6 GPS week: 2330 Day: 6 MJD: 60560
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 2 -39 -26 16 .13 17 12 | -2778 -1212 3739 19463
esa n/a| -1 0 0 5 -11 35 -.09 25 14 | -200 -1421 2871 7701
gfz n/a| 2 0 3 53 46 11 .02 24 14 | 0 -1596 2924 9245
grg n/a| 1 0 1 13 -14 -69 .36 24 18 | 1492 -1070 3807 19462
iac n/a| -1 1 -5 0 45 19 -.23 20 17 | 3184 -962 3713 18607
jgx n/a| 0 0 -1 -29 -55 5 -.18 31 31 | 2897 -1558 2894 9307
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 3.2330.0 GPS week: 2330 Day: 0 MJD: 60554
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 602 25 38 25 24 23 30 12 | 105 68 97 105 99 79 91
R02M | 702 11 13 13 9 14 30 7 | 67 64 59 64 74 43 62
R03 | 1233 10 11 11 13 13 23 6 | 66 60 60 71 66 51 62
R04 | 1037 10 17 14 20 22 25 8 | 77 73 65 67 79 57 69
R05M | 1248 14 8 17 9 18 17 6 | 58 60 65 66 75 54 62
R07 | 1471 14 16 15 15 22 16 7 | 74 59 63 63 74 53 64
R08 | 868 18 11 16 13 19 17 7 | 67 72 83 81 87 66 74
R09 | 2964 10 15 14 19 20 12 7 | 42 46 41 40 44 48 41
R11 | 1333 15 17 10 15 14 13 6 | 29 33 34 32 31 35 30
R12M | 605 18 20 25 27 14 21 9 | 44 44 63 68 53 50 51
R14M | 1166 7 10 16 10 20 15 6 | 52 54 47 54 62 44 51
R15 | 881 16 20 17 11 23 29 9 | 80 71 81 85 80 65 76
R16 | 814 13 19 11 17 14 13 6 | 70 73 67 56 65 61 65
R17E | 584 11 13 13 21 12 20 6 | 57 60 55 64 55 60 57
R18E | 878 11 17 16 18 18 17 7 | 45 46 41 51 48 46 44
R19E | 2558 29 44 42 65 55 55 21 | 120 119 127 146 129 137 123
R20E | 3745 32 63 90 70 36 60 27 | 78 79 113 81 9999 80 68
R21E | 868 11 17 12 13 13 14 6 | 50 52 52 61 64 49 52
R22E | 4738 13 6 9 15 16 12 5 | 34 35 36 43 43 34 36
R24E | 1331 13 15 15 19 18 17 7 | 128 126 130 138 129 138 130
XR25E |13862 12 12 --- --- 13 --- 9 | 42 47 --- --- 41 --- 42
XR26 |15435 33 --- --- 23 68 --- 31 | 82 --- --- 86 123 --- 90
------+-----------------------------------------+-------------------------------------
RMS | 1848 16 23 27 27 22 26 |T 66 63 68 72 72 62 65
WRMS | 1848 14 16 15 16 18 26 |NE 69 61 65 68 74 57 66
MEDI | 1166 13 16 15 17 18 17 |MD 66 60 63 66 66 53 62
Table 3.2330.1 GPS week: 2330 Day: 1 MJD: 60555
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 768 21 47 21 31 21 28 13 | 61 49 70 65 59 53 57
R02M | 787 9 18 11 12 20 19 6 | 49 51 43 45 56 45 46
R03 | 1350 9 16 11 16 13 19 6 | 46 40 41 49 45 38 42
R04 | 1233 13 14 14 15 17 19 7 | 54 52 46 54 56 47 50
R05M | 1263 9 20 15 15 24 20 7 | 44 56 46 44 58 40 46
R07 | 1910 15 10 20 17 11 23 7 | 54 49 64 52 44 48 51
R08 | 841 14 15 12 12 16 13 6 | 44 41 52 52 51 46 47
R09 | 2565 12 13 16 9 10 13 5 | 25 26 36 29 26 28 26
R11 | 667 18 21 15 20 19 22 8 | 26 34 29 25 24 32 24
R12M | 628 9 21 14 12 21 8 6 | 45 46 47 47 54 40 45
R14M | 1204 10 11 13 17 16 16 6 | 42 45 55 58 48 39 46
R15 | 801 13 18 16 14 20 19 7 | 50 49 56 57 54 42 50
R16 | 915 18 13 14 12 15 11 6 | 53 67 72 68 53 61 61
R17E | 758 11 14 14 20 9 19 6 | 46 42 54 51 47 44 46
R18E | 953 8 15 15 17 13 15 6 | 31 31 27 34 32 27 28
R19E | 1431 39 36 27 36 28 55 16 | 148 168 160 161 161 167 158
R20E | 3250 37 64 45 54 157 67 26 | 70 99 80 81 9999 87 72
XR21E | 9176 24 --- 28 21 47 19 15 | 53 --- 53 69 105 51 58
R22E | 3672 14 13 17 18 14 16 7 | 42 43 49 49 48 43 44
R24E | 1156 12 15 12 19 15 16 6 | 96 100 99 108 108 96 100
XR25E |11597 11 19 --- --- 17 --- 11 | 54 53 --- --- 62 --- 55
XR26 |13845 36 --- --- 28 60 --- 30 | 62 --- --- 84 94 --- 76
------+-----------------------------------------+-------------------------------------
RMS | 1618 17 25 18 22 40 26 |T 54 57 58 61 61 53 55
WRMS | 1618 13 18 15 16 17 26 |NE 47 45 51 53 50 43 48
MEDI | 1204 13 15 15 17 17 19 |MD 49 49 52 52 54 44 47
Table 3.2330.2 GPS week: 2330 Day: 2 MJD: 60556
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1142 25 33 23 28 17 53 13 | 71 55 79 70 74 65 68
XR02M | 1503 18 14 15 34 18 --- 10 | 51 55 50 89 65 --- 60
R03 | 881 12 11 8 13 10 20 5 | 54 57 50 54 47 47 50
R04 | 937 17 14 13 12 13 18 6 | 66 59 56 62 54 54 57
R05M | 626 10 12 14 13 14 16 6 | 61 59 49 47 57 48 53
R07 | 1183 9 12 8 16 12 22 6 | 61 52 62 63 63 49 58
R08 | 716 15 15 15 25 14 19 7 | 55 54 69 61 62 53 58
R09 | 1753 14 14 11 17 17 11 6 | 25 23 30 23 26 25 22
R11 | 955 12 15 15 21 16 7 6 | 23 31 32 19 21 25 23
R12M | 1344 12 13 7 11 12 24 6 | 48 54 49 55 50 37 48
R14M | 851 10 9 15 13 12 13 5 | 48 46 49 54 35 38 44
R15 | 748 14 21 12 25 17 23 8 | 63 54 64 73 53 41 57
R16 | 761 12 14 17 13 16 7 6 | 50 53 57 51 44 50 49
R17E | 750 11 13 21 18 13 15 7 | 66 70 71 69 64 72 67
R18E | 1002 8 13 12 17 9 14 5 | 37 38 43 42 36 43 38
R19E | 1512 33 28 44 38 32 61 17 | 82 75 101 79 81 78 78
R20E | 2386 45 58 48 57 8344 64 27 | 79 98 92 81 9999 91 75
R21E | 1361 12 13 16 13 206 12 6 | 52 67 57 58 173 54 51
R22E | 3056 15 8 10 16 19 14 6 | 38 44 43 49 53 39 43
R24E | 1137 21 21 16 18 16 24 8 | 124 134 126 127 116 143 127
XR25E |11872 15 10 --- --- 16 --- 10 | 42 40 --- --- 44 --- 41
XR26 |13149 33 --- --- 32 54 --- 29 | 65 --- --- 47 85 --- 64
------+-----------------------------------------+-------------------------------------
RMS | 1356 18 21 20 23 1914 28 |T 57 58 61 60 62 55 55
WRMS | 1356 13 15 13 20 159 28 |NE 53 48 55 52 52 45 50
MEDI | 1137 14 14 15 17 16 18 |MD 54 54 56 58 54 49 53
Table 3.2330.3 GPS week: 2330 Day: 3 MJD: 60557
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 968 22 40 22 29 18 49 13 | 92 63 101 94 92 86 87
R02M | 2059 12 17 20 12 34 9 8 | 57 61 65 65 79 58 61
R03 | 1627 10 7 10 12 13 17 5 | 59 62 66 68 63 54 62
R04 | 1734 11 9 13 8 11 22 5 | 66 63 63 64 59 49 61
R05M | 680 9 10 10 9 22 16 5 | 75 71 67 75 71 65 70
R07 | 552 11 12 11 9 11 16 5 | 68 72 70 68 67 59 67
R08 | 565 9 10 13 11 16 18 5 | 62 64 75 72 72 59 66
R09 | 797 12 13 18 16 16 16 6 | 30 36 31 42 33 33 32
R11 | 1264 13 17 16 15 20 10 7 | 30 33 33 31 33 37 30
R12M | 2472 11 15 15 10 15 16 6 | 73 80 81 81 84 71 78
R14M | 888 5 11 8 9 14 11 4 | 55 57 46 56 51 52 52
R15 | 973 7 27 10 23 15 14 7 | 65 51 66 80 60 54 63
R16 | 876 10 19 22 15 18 15 7 | 65 66 63 70 63 66 64
R17E | 796 9 14 14 17 19 12 6 | 64 68 62 67 57 64 62
R18E | 1260 8 15 14 19 12 18 6 | 44 43 38 49 46 39 42
R19E | 741 31 36 55 42 67 72 22 | 141 180 164 167 123 170 152
R20E | 2071 48 59 68 28 55 68 24 | 76 87 114 81 9999 65 70
R21E | 886 9 11 15 10 14 13 5 | 70 64 67 73 104 64 68
R22E | 3155 13 9 15 16 14 14 6 | 61 60 63 64 63 65 61
R24E | 1358 13 19 11 11 23 15 7 | 130 142 132 137 131 139 134
XR25E |10778 9 13 --- --- 12 --- 8 | 42 50 --- --- 49 --- 46
XR26 |12008 25 --- --- 20 68 --- 27 | 44 --- --- 43 71 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1456 17 22 24 18 26 28 |T 66 70 73 73 70 67 66
WRMS | 1456 11 17 14 14 20 29 |NE 58 56 63 63 61 55 57
MEDI | 973 11 14 14 15 16 16 |MD 64 63 66 68 63 59 62
Table 3.2330.4 GPS week: 2330 Day: 4 MJD: 60558
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1584 22 30 20 32 18 39 12 | 84 65 84 79 83 86 79
R02M | 1156 7 12 10 14 25 22 6 | 52 53 54 52 69 44 53
R03 | 2108 8 11 18 20 35 17 8 | 54 56 56 52 83 63 58
R04 | 1552 12 9 8 15 19 35 7 | 68 65 57 65 67 48 61
R05M | 1489 6 13 15 13 14 27 6 | 57 56 58 60 50 40 53
R07 | 1242 17 12 13 11 13 23 6 | 66 59 48 57 64 47 57
R08 | 642 11 10 10 16 21 22 6 | 57 66 62 55 70 51 60
R09 | 1010 12 16 21 14 15 20 7 | 21 29 25 21 25 29 20
R11 | 878 13 9 15 14 17 7 5 | 14 16 26 20 20 18 15
R12M | 2266 10 15 12 26 22 13 7 | 59 53 55 75 76 60 61
R14M | 1037 8 18 11 14 19 8 6 | 49 60 48 41 33 42 45
R15 | 1149 10 13 11 14 12 13 5 | 61 49 58 62 53 53 56
R16 | 942 12 23 16 18 16 15 7 | 53 44 56 47 52 36 47
R17E | 753 8 15 13 15 11 13 5 | 73 73 78 80 78 75 75
R18E | 1382 11 15 14 16 12 18 6 | 35 37 35 41 38 34 35
R19E | 1518 35 39 53 52 37 65 20 | 67 76 111 80 78 68 75
R20E | 1611 43 60 83 56 54 83 28 | 72 89 122 77 9999 59 72
R21E | 1118 9 14 14 11 9 17 5 | 185 188 186 185 216 184 187
R22E | 2778 12 11 10 23 20 11 6 | 79 78 75 76 76 78 76
R24E | 2270 9 21 13 20 16 12 7 | 103 104 107 105 111 103 104
XR25E |17347 12 15 --- --- 12 --- 9 | 62 64 --- --- 64 --- 62
XR26 |12529 32 --- --- 24 65 --- 30 | 61 --- --- 53 70 --- 57
------+-----------------------------------------+-------------------------------------
RMS | 1526 16 22 26 24 23 30 |T 65 65 70 65 70 60 64
WRMS | 1526 11 14 14 18 18 30 |NE 53 49 52 51 58 47 51
MEDI | 1382 11 15 13 16 17 17 |MD 61 60 57 60 69 51 58
Table 3.2330.5 GPS week: 2330 Day: 5 MJD: 60559
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 745 23 20 17 29 19 40 11 | 67 60 62 69 53 55 59
R02M | 1944 9 10 13 15 21 17 6 | 43 46 49 44 56 42 45
R03 | 1634 6 13 17 22 20 25 7 | 50 44 42 66 61 37 49
R04 | 898 11 8 13 12 14 9 5 | 55 51 50 59 53 55 52
R05M | 1068 10 9 17 16 7 23 6 | 47 48 67 63 48 38 51
R07 | 794 12 10 9 14 21 16 6 | 55 52 52 57 64 52 54
R08 | 558 13 8 17 14 15 16 6 | 46 38 42 38 44 42 40
R09 | 1127 14 11 9 10 23 17 6 | 26 24 27 31 34 31 25
R11 | 801 10 11 11 15 14 20 6 | 18 22 25 19 19 27 19
R12M | 1148 18 16 17 32 21 18 9 | 66 70 70 82 68 69 69
R14M | 1116 12 10 16 11 12 8 5 | 53 47 36 43 39 47 43
R15 | 688 13 12 13 13 18 12 6 | 56 50 52 53 40 46 48
R16 | 790 19 15 15 19 20 9 7 | 46 45 51 35 34 36 40
R17E | 612 14 13 11 19 17 13 6 | 64 54 58 61 60 62 58
R18E | 795 18 15 14 13 11 20 7 | 34 39 35 50 35 43 37
R19E | 1509 27 39 44 72 49 58 21 | 68 83 95 81 81 79 75
R20E | 3771 61 69 77 55 63 118 33 | 76 98 94 90 545 95 71
R21E | 1056 8 12 23 16 14 20 7 | 245 250 249 257 240 250 246
R22E | 1983 13 9 17 16 15 13 6 | 91 99 104 101 97 98 97
R24E | 3511 11 15 17 20 16 17 7 | 117 118 116 124 119 120 118
XR25E |12171 8 11 --- --- 14 --- 8 | 76 75 --- --- 75 --- 76
XR26 |13061 49 --- --- 24 77 --- 39 | 26 --- --- 38 71 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1587 20 21 24 26 24 34 |T 64 67 68 69 88 66 63
WRMS | 1587 14 12 16 19 19 36 |NE 44 42 44 46 47 42 42
MEDI | 1068 13 12 16 16 17 17 |MD 55 51 52 59 56 47 51
Table 3.2330.6 GPS week: 2330 Day: 6 MJD: 60560
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 894 22 27 21 30 14 37 11 | 101 80 102 105 100 97 96
R02M | 1976 10 21 12 20 21 28 8 | 67 79 72 64 84 54 70
R03 | 852 8 11 11 19 12 25 6 | 79 75 73 92 87 67 78
R04 | 1046 12 13 15 12 21 24 7 | 90 80 86 90 85 68 84
R05M | 1792 9 11 14 12 17 17 6 | 94 96 90 97 101 95 95
R07 | 594 14 13 15 11 16 28 7 | 84 69 71 74 87 65 75
R08 | 748 9 7 10 23 10 17 5 | 69 69 77 83 78 66 73
R09 | 1132 13 7 9 12 9 23 5 | 53 45 45 48 46 53 47
R11 | 1092 14 13 16 11 10 24 6 | 40 41 41 38 38 52 39
R12M | 774 11 19 17 17 17 9 7 | 110 112 119 121 115 110 114
R14M | 904 8 9 13 16 10 19 5 | 65 63 67 69 65 57 64
R15 | 954 7 11 13 18 13 13 5 | 79 65 77 76 76 68 73
R16 | 707 13 18 12 28 12 26 8 | 59 54 55 43 52 39 49
R17E | 1134 9 19 11 18 11 16 6 | 77 85 76 82 76 83 79
R18E | 1575 10 19 13 24 15 15 7 | 71 70 67 81 69 74 71
R19E | 1152 29 46 51 50 44 54 20 | 78 87 117 85 83 78 82
R20E | 4823 43 80 72 55 46 92 28 | 110 121 143 116 710 108 113
R21E | 1900 9 14 14 17 12 14 6 | 252 261 251 253 244 258 251
R22E | 2182 19 9 16 18 13 18 7 | 131 128 133 130 134 127 130
R24E | 3581 21 22 18 17 16 14 8 | 153 165 160 156 159 157 157
XR25E |10278 11 17 --- --- 14 --- 10 | 99 102 --- --- 104 --- 101
XR26 | 9007 41 --- --- 28 70 --- 35 | 53 --- --- 57 100 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 1810 17 25 24 24 20 31 |T 91 92 96 93 122 88 91
WRMS | 1810 12 14 14 18 17 31 |NE 70 64 69 70 74 63 67
MEDI | 1132 11 14 14 18 14 19 |MD 79 80 77 83 85 68 78
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