[IGSREPORT-30078] Wk 2329 IGLOS Final Orbits
acc
acc at igs.org
Mon Sep 16 00:15:32 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2329 (Aug 25, 2024 - Aug 31, 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 2.2329.
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:
igl2329[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2329 in the SP3 format.
igl23297.sum Combination Report for GPS Week 2329.
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 | 6.4 ns
1 | 6.4 ns
2 | 8.6 ns
3 | 7.9 ns
4 | 7.8 ns
5 | 6.9 ns
6 | 7.0 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 1.2329, 1a.2329).
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 2.2329.0-6)
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 3.2329.0-6).
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 2329 summary. (Aug 25, 2024 - Aug 31, 2024)
Table 1.2329.a GPS week : 2329 MJD: 60547.0-60553.0
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 5 -12 -15 53 .11 20 12 | -511 -614 3544 15481
| 0 0 1 7 4 17 .02 | 614 1707
esa n/a| 0 -1 1 2 -8 7 -.14 22 15 | 8897 9 3017 7624
| 1 0 1 3 8 21 .03 | 5038 1608
gfz n/a| 0 0 0 45 27 -14 .00 26 15 | 0 -328 3050 7825
| 0 0 1 11 18 14 .06 | 0 1409
grg n/a| 1 1 1 -25 -12 -19 .42 25 16 | 4702 -617 3604 15175
| 0 0 4 18 16 67 .03 | 456 1597
iac n/a| 0 0 -8 28 25 -31 -.16 23 17 | 6708 -504 3524 14579
| 1 2 2 17 28 41 .04 | 442 1281
jgx n/a| 0 0 0 -31 -8 -18 -.21 28 29 | 4166 -426 3065 8114
| 1 0 2 20 19 64 .04 | 373 1384
Table 1.2329.b GPS week : 2329 MJD: 60547.0-60553.0
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 | 16 15 19 16 14 14 13 |
R02 | 6 7 7 5 5 6 7 |
R03 | 7 7 7 7 7 6 6 |
R04 | 7 7 7 7 7 6 7 |
R05 | 6 7 5 6 7 7 7 |
R07 | 8 7 8 7 6 6 9 |
R08 | 9 9 6 9 8 7 7 |
R09 | 7 7 6 7 6 6 6 |
R11 | 7 6 7 6 5 7 7 |
R12 | 7 7 6 5 6 5 8 |
R14 | 6 6 5 6 6 6 6 |
R15 | 7 8 7 7 8 6 5 |
R16 | 8 7 7 5 8 9 9 |
R17 | 6 8 8 6 6 6 6 |
R18 | 7 6 8 9 7 8 6 |
R19 | 21 15 16 23 23 24 28 |
R20 | 32 28 23 30 33 27 31 |
R21 | 6 7 7 5 6 6 6 |
R22 | 7 7 7 6 6 7 7 |
R24 | 7 9 8 7 8 9 9 |
R25 | 9 11 12 10 9 9 12 |
R26 | 30 32 30 24 27 33 35 |
Table 1.2329.c GPS week : 2329 MJD: 60547.0-60553.0
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 2329 0 | -27 -3 141 -651 2548 -2194 80.8 1392 1392 | 6445 0
brd 2329 1 | 5 0 75 2377 1591 -872 80.7 1057 1057 | 6428 0
brd 2329 2 | 25 116 78 963 342 565 79.1 1528 1528 | 8560 0
brd 2329 3 | -147 49 -4 -195 1550 13 80.5 1602 1602 | 7873 0
brd 2329 4 | -165 40 -19 -1430 767 276 82.2 1442 1442 | 7799 0
brd 2329 5 | -77 21 -46 -2806 1621 286 81.8 1490 1490 | 6880 0
brd 2329 6 | -40 -35 8 -243 -472 -2518 82.2 1579 1579 | 7023 0
-------------+------------------------------------------------------------+----------------
brd 2329 mean| -60 27 33 -283 1135 -634 81.0 1441 1441 | 7286 0
brd 2329 sdev| 73 48 66 1656 996 1263 1.1 184 184 | 807 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 2.2329.0 GPS week: 2329 Day: 0 MJD: 60547
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 4 -23 -16 52 .13 21 12 | 755 -2289 3936 16246
esa n/a| 1 -1 0 7 0 20 -.18 25 17 | 6582 -1584 3174 7010
gfz n/a| 0 1 1 42 9 -28 -.04 25 14 | 0 -1311 3204 6921
grg n/a| 2 2 7 -10 -28 64 .40 25 16 | 4431 -2412 4022 16283
iac n/a| 0 0 -8 11 31 -10 -.19 26 16 | 6732 -2142 3885 15229
jgx n/a| -1 -1 -4 -6 29 -110 -.22 25 25 | 4934 -1125 3233 7451
Table 2.2329.1 GPS week: 2329 Day: 1 MJD: 60548
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 3 -19 -16 72 .14 25 14 | -306 -3145 3991 16643
esa n/a| 1 -1 0 0 -19 25 -.11 16 13 | 16192 -2511 3414 7493
gfz n/a| -1 0 0 63 44 -21 -.01 20 15 | 0 -2546 3448 6909
grg n/a| 2 2 6 -50 -2 54 .41 24 16 | 4730 -2840 4031 16507
iac n/a| 0 0 -8 22 -7 -26 -.19 20 16 | 6018 -1565 3945 15628
jgx n/a| 0 0 -2 -33 -4 -74 -.20 26 26 | 4193 -2492 3466 7234
Table 2.2329.2 GPS week: 2329 Day: 2 MJD: 60549
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 4 -3 -23 71 .12 19 12 | -963 1561 3408 14923
esa n/a| 0 -1 2 -1 -2 -18 -.17 15 12 | 12586 2162 2996 7727
gfz n/a| 0 0 0 46 60 -27 .00 22 16 | 0 1702 3024 8638
grg n/a| 1 1 4 -34 -22 -2 .41 19 14 | 5341 1277 3436 14456
iac n/a| 0 4 -13 35 3 40 -.10 21 18 | 7437 772 3413 14270
jgx n/a| -1 0 -2 -33 -7 -71 -.27 25 25 | 4083 1761 3041 8694
Table 2.2329.3 GPS week: 2329 Day: 3 MJD: 60550
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 6 -11 -9 51 .07 19 12 | -840 -783 3563 16039
esa n/a| -1 0 1 0 -11 -4 -.12 22 16 | 11582 81 2991 8753
gfz n/a| 0 1 0 35 25 -11 .02 27 13 | 0 -307 3027 8512
grg n/a| 0 2 -4 -33 -29 -53 .42 24 19 | 5147 -840 3645 15517
iac n/a| 0 -2 -11 44 73 -52 -.17 24 20 | 6647 -502 3554 15131
jgx n/a| -1 1 2 -14 -26 29 -.20 29 30 | 3777 -256 3068 8833
Table 2.2329.4 GPS week: 2329 Day: 4 MJD: 60551
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 -5 -11 49 .09 18 12 | -994 175 3612 15227
esa n/a| 0 0 0 1 -19 40 -.17 23 15 | 6035 910 3155 7074
gfz n/a| 0 0 -1 43 27 8 .06 26 15 | 0 498 3194 7532
grg n/a| 0 1 0 -39 0 -109 .39 25 13 | 4895 34 3674 14861
iac n/a| 0 0 -8 53 51 -75 -.20 28 20 | 7004 -577 3599 14301
jgx n/a| 0 0 0 -34 -17 37 -.19 32 32 | 3897 220 3178 7848
Table 2.2329.5 GPS week: 2329 Day: 5 MJD: 60552
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 4 -17 -17 54 .10 16 11 | -774 -888 3247 15720
esa n/a| 0 0 2 4 0 4 -.16 26 16 | 866 -80 2867 8576
gfz n/a| 0 0 -1 30 8 -1 .07 23 15 | 0 -934 2912 8259
grg n/a| 2 0 0 3 -18 -88 .41 27 15 | 4191 -682 3302 15377
iac n/a| 1 0 -6 6 5 -15 -.15 20 15 | 6689 -1042 3234 14705
jgx n/a| 1 -1 1 -69 -2 9 -.26 32 32 | 4225 -1411 2923 8554
Table 2.2329.6 GPS week: 2329 Day: 6 MJD: 60553
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 -7 -15 20 .12 19 12 | -459 1065 3057 13571
esa n/a| 0 -1 1 6 -9 -12 -.08 25 16 | 8439 1090 2525 6741
gfz n/a| 1 0 0 55 18 -22 -.09 39 15 | 0 599 2545 8004
grg n/a| 2 1 0 -17 13 -1 .48 28 19 | 4179 1141 3124 13228
iac n/a| 2 3 -6 24 21 -77 -.15 19 17 | 6434 1528 3040 12793
jgx n/a| 0 0 0 -26 -28 49 -.15 29 29 | 4053 317 2548 8187
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 3.2329.0 GPS week: 2329 Day: 0 MJD: 60547
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 | ---- 12 --- --- 20 --- --- 16 | 146 --- --- 140 --- --- 139
R02 | 843 6 15 21 10 11 16 6 | 99 99 109 102 102 89 100
R03 | 720 12 11 10 13 13 27 6 | 97 92 92 97 99 79 92
R04 | 1495 8 17 13 15 12 22 6 | 95 95 89 91 93 91 91
R05 | 761 13 9 14 10 15 14 5 | 89 90 90 95 102 90 92
R07 | 1347 22 13 13 14 14 28 8 | 101 82 95 94 95 74 90
R08 | 815 13 30 11 11 33 10 9 | 96 92 110 108 124 102 104
R09 | 1650 10 11 22 15 10 17 6 | 40 48 43 46 46 44 43
R11 | 1147 17 11 11 23 11 20 7 | 29 37 32 40 33 42 33
R12 | 754 7 17 12 16 19 13 6 | 60 51 53 66 69 60 58
R14 | 855 13 13 12 15 13 11 5 | 102 94 97 105 90 98 97
R15 | 1009 12 20 11 19 9 20 7 | 61 45 56 64 51 49 53
R16 | 923 15 18 16 14 19 25 8 | 69 67 75 75 64 59 67
R17E | 2330 10 13 14 18 12 14 6 | 86 82 88 96 83 84 86
R18E | 2194 7 20 14 18 12 14 6 | 81 81 75 85 83 79 80
R19E | 1592 40 42 64 42 34 50 20 | 94 97 119 94 93 90 92
R20E | 2406 62 74 65 77 87 59 32 | 146 127 124 102 146 105 112
R21E | 952 12 13 13 15 8 19 6 | 73 69 75 74 69 65 70
XR22E | 1768 16 7 14 16 10 --- 6 | 56 62 70 71 58 --- 62
R24E | 1288 14 13 14 18 20 17 7 | 95 96 101 106 93 89 96
XR25E |12879 11 14 --- --- 14 --- 9 | 69 71 --- --- 72 --- 71
XR26 | 7460 35 --- --- 30 57 --- 29 | 39 --- --- 57 82 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 1392 21 25 25 25 26 25 |T 82 78 83 86 83 77 80
WRMS | 1392 12 17 14 16 16 25 |NE 80 74 78 84 80 73 79
MEDI | 1288 12 13 14 16 13 17 |MD 86 82 89 94 83 79 86
Table 3.2329.1 GPS week: 2329 Day: 1 MJD: 60548
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 |11869 13 --- --- 16 --- --- 15 | 79 --- --- 86 --- --- 85
R02 | 924 12 10 18 10 9 31 7 | 62 67 75 68 66 50 65
R03 | 787 12 9 11 13 15 30 7 | 63 57 61 55 60 43 56
R04 | 1035 12 13 10 19 10 19 6 | 62 59 61 58 58 60 58
R05 | 712 6 11 8 14 21 21 6 | 59 55 54 48 65 50 54
R07 | 872 11 16 13 16 11 19 6 | 70 58 69 68 67 57 64
R08 | 868 10 17 10 26 23 29 9 | 68 58 71 73 77 58 66
R09 | 1447 12 13 20 10 16 13 6 | 38 42 45 46 36 37 39
R11 | 1101 19 9 14 9 8 12 5 | 39 42 37 36 39 40 38
R12 | 1022 13 20 14 16 14 12 7 | 50 45 45 49 48 46 45
R14 | 678 7 11 9 11 18 15 5 | 86 80 83 88 75 79 81
R15 | 632 17 20 13 22 12 16 7 | 50 42 45 52 42 39 43
R16 | 829 18 14 15 18 10 15 6 | 64 60 67 58 57 60 60
R17E | 1292 10 12 20 23 18 16 7 | 56 56 70 68 57 52 58
R18E | 1212 13 14 14 16 10 13 6 | 47 52 59 56 48 48 50
R19E | 1240 37 20 30 30 32 45 14 | 69 67 77 62 64 71 64
R20E | 1684 86 37 56 67 53 66 27 | 118 82 93 72 62 96 71
R21E | 1202 13 14 15 21 14 12 6 | 55 50 57 58 60 55 54
R22E | 936 16 8 15 20 12 20 6 | 52 54 56 56 54 74 54
R24E | 956 18 13 21 28 19 20 9 | 75 75 82 87 72 71 76
XR25E |11047 20 14 --- --- 11 --- 11 | 61 60 --- --- 65 --- 61
XR26 | 8583 36 --- --- 34 59 --- 32 | 36 --- --- 54 67 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1057 25 16 20 24 20 26 |T 61 58 63 61 59 57 58
WRMS | 1057 14 13 15 16 16 26 |NE 59 55 59 59 58 51 57
MEDI | 1022 13 13 14 18 14 19 |MD 61 57 61 58 60 55 58
Table 3.2329.2 GPS week: 2329 Day: 2 MJD: 60549
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 | 1656 28 45 18 31 --- --- 19 | 120 54 80 109 --- --- 102
R02 | 824 7 12 21 10 17 21 6 | 82 77 94 87 96 74 84
R03 | 1664 12 12 11 11 25 26 7 | 86 73 76 87 98 69 81
R04 | 639 15 12 10 9 24 20 7 | 85 90 88 84 70 86 84
R05 | 592 11 9 7 7 12 12 4 | 82 73 72 73 78 70 74
R07 | 1285 10 10 29 14 16 22 8 | 81 74 91 73 78 64 75
R08 | 900 10 8 9 12 19 20 6 | 80 86 87 92 94 77 85
R09 | 1499 10 7 9 12 21 13 5 | 26 31 32 31 35 30 28
R11 | 713 18 18 12 16 12 19 7 | 27 31 26 29 32 33 26
R12 | 1364 9 11 19 10 17 8 6 | 68 69 68 62 68 63 66
R14 | 1614 7 9 10 11 12 17 5 | 105 105 102 102 105 107 104
R15 | 548 11 17 11 20 17 10 6 | 52 46 55 62 59 53 53
R16 | 762 16 14 17 15 14 10 6 | 54 55 56 62 50 50 53
R17E | 1428 13 16 14 25 22 7 7 | 81 89 89 100 85 87 87
R18E | 2431 12 11 14 22 13 25 7 | 67 70 61 78 74 61 68
R19E | 1466 35 21 35 42 31 46 15 | 65 72 81 62 58 64 63
R20E | 3673 54 37 63 28 49 71 22 | 102 106 96 81 81 105 86
R21E | 1533 15 15 14 22 10 15 7 | 75 67 62 72 66 66 67
R22E | 1057 16 10 16 19 16 14 7 | 58 65 68 55 54 56 60
R24E | 1584 12 17 14 24 20 15 8 | 63 67 66 79 62 62 65
XR25E |10618 18 19 --- --- 9 --- 12 | 40 47 --- --- 37 --- 41
XR26 | 9989 27 --- --- 28 67 --- 30 | 32 --- --- 23 62 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1527 19 15 22 19 21 25 |T 69 68 72 71 68 67 67
WRMS | 1527 12 12 16 14 18 25 |NE 70 66 71 69 71 64 67
MEDI | 1428 12 12 14 16 17 17 |MD 68 70 72 73 68 64 67
Table 3.2329.3 GPS week: 2329 Day: 3 MJD: 60550
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1312 24 55 21 29 34 29 15 | 125 46 64 114 58 46 111
R02 | 761 8 9 10 18 10 16 5 | 84 89 87 98 90 78 86
R03 | 1384 9 18 13 22 13 19 7 | 91 82 90 107 99 75 89
R04 | 810 18 11 13 15 17 23 7 | 83 76 67 87 67 59 73
R05 | 539 8 11 9 15 14 22 6 | 76 71 73 84 77 59 73
R07 | 806 7 11 10 11 23 24 6 | 80 76 79 84 91 74 80
R08 | 735 11 7 19 21 37 22 9 | 75 79 78 74 108 70 79
R09 | 1164 10 10 11 22 24 15 7 | 30 35 37 25 43 28 30
R11 | 1348 17 11 12 14 14 15 6 | 16 23 23 27 24 21 17
R12 | 981 9 16 10 10 12 13 5 | 38 50 40 39 40 30 39
R14 | 1568 6 8 10 22 12 16 5 | 51 52 48 47 43 51 47
R15 | 959 9 14 7 10 24 20 6 | 44 38 40 41 52 29 39
R16 | 679 11 11 10 20 8 8 5 | 41 39 39 38 37 36 37
R17E | 1079 8 16 13 12 10 16 5 | 76 71 71 79 70 78 73
R18E | 3626 17 14 15 19 20 31 8 | 71 77 66 70 71 70 70
R19E | 1978 30 46 78 50 30 56 22 | 75 79 142 79 70 70 79
R20E | 2544 62 45 74 61 66 88 29 | 92 106 123 78 104 78 89
R21E | 2732 12 13 13 12 9 10 5 | 63 62 67 65 63 58 62
R22E | 1772 15 8 12 17 14 9 5 | 48 49 51 63 51 49 51
R24E | 1303 11 19 15 18 13 13 7 | 70 56 59 69 65 66 62
XR25E |13585 13 15 --- --- 12 --- 10 | 39 50 --- --- 44 --- 42
XR26 |12231 22 --- --- 28 49 --- 24 | 15 --- --- 27 45 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 1602 19 22 27 24 24 29 |T 62 62 67 66 64 56 61
WRMS | 1602 12 16 13 19 20 30 |NE 60 58 58 63 62 50 58
MEDI | 1303 11 13 12 18 14 16 |MD 70 62 66 70 63 59 62
Table 3.2329.4 GPS week: 2329 Day: 4 MJD: 60551
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 557 26 50 21 24 24 20 13 | 104 39 62 100 41 31 89
R02 | 903 8 11 11 9 16 16 5 | 68 63 71 72 67 60 66
R03 | 1114 10 18 10 12 13 21 6 | 76 69 75 81 70 65 72
R04 | 564 12 8 19 9 14 22 6 | 75 72 64 75 77 60 70
R05 | 576 14 11 12 13 21 18 6 | 67 70 66 81 82 60 69
R07 | 772 11 18 14 12 11 15 6 | 72 68 78 70 67 64 69
R08 | 813 6 7 16 14 32 27 8 | 62 64 75 62 85 47 65
R09 | 2821 9 13 9 14 17 11 5 | 33 41 35 28 32 43 33
R11 | 1589 12 13 8 11 11 11 5 | 19 25 21 19 16 22 17
R12 | 1143 12 12 16 8 15 19 6 | 55 59 62 61 65 47 57
R14 | 1541 7 19 14 10 15 9 6 | 87 92 83 86 87 81 85
R15 | 1681 8 9 17 22 25 28 8 | 50 51 54 45 55 40 47
R16 | 578 19 16 16 23 19 9 8 | 48 52 53 44 47 40 45
R17E | 1429 9 15 17 16 13 11 6 | 64 62 66 75 61 61 64
R18E | 1846 12 15 13 11 16 20 6 | 47 47 45 53 45 43 46
R19E | 1646 33 43 65 59 51 59 23 | 55 88 108 67 64 77 66
R20E | 2008 49 52 74 69 88 110 32 | 95 96 102 77 110 89 75
R21E | 1786 7 14 21 12 9 16 6 | 45 39 53 47 37 41 42
R22E | 1929 16 9 7 17 13 14 6 | 41 49 48 51 42 41 46
R24E | 915 19 17 17 15 18 15 7 | 57 48 53 61 56 51 53
XR25E |13090 9 14 --- --- 13 --- 8 | 40 40 --- --- 48 --- 41
XR26 |15276 17 --- --- 30 62 --- 26 | 27 --- --- 27 50 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1441 18 23 26 25 28 32 |T 58 58 63 61 59 53 56
WRMS | 1441 12 15 15 13 20 32 |NE 60 58 61 60 60 50 58
MEDI | 1429 12 14 16 14 16 16 |MD 55 59 62 62 56 47 57
Table 3.2329.5 GPS week: 2329 Day: 5 MJD: 60552
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 774 23 48 19 20 32 35 13 | 97 42 59 95 50 37 91
R02 | 884 7 11 11 14 13 17 5 | 66 67 61 69 55 55 62
R03 | 685 5 14 13 16 17 16 6 | 67 65 66 79 77 66 69
R04 | 1054 9 11 12 11 16 12 5 | 64 60 63 69 75 59 65
R05 | 842 11 12 15 21 18 8 6 | 54 59 60 49 65 59 56
R07 | 670 13 13 14 10 11 22 6 | 70 64 73 75 68 58 68
R08 | 1062 10 15 21 12 13 23 7 | 68 69 81 71 68 61 69
R09 | 3868 10 13 13 11 12 15 5 | 52 58 60 55 49 53 54
XR11 | 2506 12 12 14 18 16 --- 7 | 23 32 35 39 36 --- 29
R12 | 951 10 12 7 7 11 12 4 | 50 48 45 46 47 61 48
R14 | 1472 5 15 15 9 15 15 5 | 67 66 63 66 66 69 65
R15 | 825 10 9 18 14 9 20 6 | 48 51 56 47 49 45 49
R16 | 1126 21 17 11 36 12 19 9 | 67 72 64 67 66 67 65
R17E | 920 12 11 17 21 9 12 6 | 65 56 56 68 55 57 58
R18E | 1161 14 19 19 18 13 17 7 | 43 48 38 48 44 44 42
R19E | 1662 28 44 48 80 46 71 23 | 55 71 90 58 73 54 58
R20E | 2012 38 78 59 52 36 93 26 | 79 114 89 73 80 87 79
R21E | 1455 5 14 20 16 9 15 6 | 43 41 48 47 41 36 41
R22E | 2266 15 13 16 15 13 17 6 | 59 64 71 63 64 63 64
R24E | 834 21 11 14 26 15 22 8 | 88 88 91 92 87 91 88
XR25E | 7239 11 15 --- --- 12 --- 9 | 60 61 --- --- 64 --- 61
XR26 |17970 34 --- --- 39 62 --- 32 | 31 --- --- 28 57 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1490 16 26 23 27 20 32 |T 59 61 63 62 60 59 59
WRMS | 1490 11 16 15 15 15 32 |NE 58 57 60 61 59 57 58
MEDI | 1062 11 13 15 16 13 17 |MD 60 61 61 66 64 59 61
Table 3.2329.6 GPS week: 2329 Day: 6 MJD: 60553
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 894 30 46 18 20 28 19 13 | 135 50 69 126 53 49 119
R02 | 1124 5 21 19 12 15 16 6 | 86 94 78 84 90 78 85
R03 | 1313 9 11 12 18 15 18 6 | 92 90 85 90 95 83 89
R04 | 1263 9 13 21 22 12 19 7 | 93 83 100 94 98 84 91
R05 | 2019 9 14 23 12 14 15 6 | 75 83 94 87 81 80 81
R07 | 621 15 14 12 13 23 30 8 | 92 73 78 90 94 64 82
R08 | 1481 10 10 14 23 13 19 6 | 88 94 106 110 100 86 95
R09 | 2463 11 15 12 15 13 15 6 | 50 60 52 56 49 46 51
R11 | 2681 15 17 10 17 14 11 6 | 25 34 27 36 30 24 27
R12 | 1078 7 12 13 23 20 22 7 | 63 63 57 69 70 69 63
R14 | 980 5 7 19 18 19 13 6 | 89 86 85 85 93 86 87
R15 | 704 8 14 10 15 12 9 5 | 66 60 64 70 63 59 62
R16 | 1096 11 25 13 40 16 10 9 | 85 73 76 77 84 77 77
R17E | 775 8 11 16 26 10 12 6 | 77 77 79 94 76 75 78
R18E | 1044 7 20 15 14 9 16 6 | 64 66 61 73 60 60 63
R19E | 1505 52 45 118 65 38 55 28 | 88 82 139 97 73 72 74
R20E | 2106 37 69 107 63 37 96 30 | 91 96 131 91 79 109 86
R21E | 1084 7 15 14 19 15 14 6 | 51 45 55 53 54 43 49
R22E | 3245 14 7 13 22 17 15 6 | 60 62 64 69 62 52 62
R24E | 787 20 17 23 16 14 21 8 | 87 85 95 94 87 87 87
XR25E |10198 16 17 --- --- 16 --- 11 | 62 64 --- --- 67 --- 64
XR26 |16240 39 --- --- 31 69 --- 35 | 38 --- --- 39 88 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1578 19 25 39 28 19 29 |T 75 72 79 80 74 69 73
WRMS | 1578 12 16 15 19 17 29 |NE 76 72 74 79 77 68 75
MEDI | 1124 10 15 14 19 15 16 |MD 77 73 78 85 76 72 77
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