[IGSREPORT-29872] Wk 2311 IGLOS Final Orbits
acc
acc at igs.org
Tue May 14 00:30:02 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2311 (Apr 21, 2024 - Apr 27, 2024)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.2311.
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:
igl2311[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2311 in the SP3 format.
igl23117.sum Combination Report for GPS Week 2311.
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 | 3.2 ns
1 | 5.8 ns
2 | 4.3 ns
3 | 4.5 ns
4 | 3.1 ns
5 | 4.4 ns
6 | 4.7 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 | ALL | R26
1 | ESA | R20
2 | ALL | R26
2 | ESA | R20
3 | ESA | R20
4 | ESA | R20
5 | ESA | R20
6 | ESA | R20
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2311, 1a.2311).
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 2.2311.0-6)
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 3.2311.0-6).
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 2311 summary. (Apr 21, 2024 - Apr 27, 2024)
Table 1.2311.a GPS week : 2311 MJD: 60421.0-60427.0
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 3 -12 -11 60 .06 19 16 | 3106 646 3468 15138
| 0 0 2 7 7 31 .03 | 2595 1890
esa n/a| 0 -1 2 -15 -5 -7 -.02 43 24 | 4195 2173 3245 7613
| 1 1 1 19 14 42 .03 | 6553 1915
gfz n/a| 1 0 -1 26 11 -22 .02 21 17 | 0 730 3233 7036
| 1 0 2 13 14 25 .05 | 0 1635
grg n/a| 1 0 4 -21 -12 25 .23 27 21 | 1647 641 3480 14841
| 1 2 1 29 17 37 .05 | 2448 1589
iac n/a| 0 1 -5 3 19 -5 -.09 21 19 | 4087 -161 3430 14572
| 1 1 4 20 16 52 .04 | 2777 1419
jgx n/a| 0 -1 -5 14 27 -75 -.21 32 29 | 7376 967 3294 7371
| 1 1 3 15 18 41 .02 | 1820 1879
Table 1.2311.b GPS week : 2311 MJD: 60421.0-60427.0
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 12 12 11 12 17 16 |
R02 | 7 7 6 7 9 7 8 |
R03 | 6 6 6 6 7 9 8 |
R04 | 7 7 7 8 7 6 7 |
R05 | 9 10 6 8 7 8 7 |
R07 | 7 7 9 7 8 7 6 |
R08 | 7 6 10 7 7 7 7 |
R09 | 7 6 8 7 8 6 6 |
R11 | 6 8 6 7 7 7 6 |
R12 | 9 8 6 12 7 8 7 |
R13 | 18 20 22 18 19 15 14 |
R14 | 7 7 6 10 7 8 7 |
R15 | 8 8 6 9 8 8 8 |
R16 | 8 8 8 10 9 8 7 |
R17 | 7 7 11 9 10 7 8 |
R18 | 8 10 8 7 7 8 8 |
R19 | 20 19 22 20 19 18 18 |
R20 | 28 24 23 26 31 28 22 |
R21 | 11 7 9 7 9 10 9 |
R22 | 6 6 8 7 7 8 6 |
R24 | 9 10 8 9 8 11 8 |
R25 | 11 14 12 14 11 10 8 |
R26 | 24 --- --- 25 32 32 36 |
Table 1.2311.c GPS week : 2311 MJD: 60421.0-60427.0
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 2311 0 | -18 55 137 1170 895 8004 79.8 1489 1489 | 3206 0
brd 2311 1 | -43 -55 49 780 975 3939 82.0 1877 1877 | 5784 0
brd 2311 2 | 22 79 145 -183 -101 3375 82.0 2143 2143 | 4336 0
brd 2311 3 | 60 24 183 2227 -1074 1097 80.3 1890 1890 | 4493 0
brd 2311 4 | -129 15 171 -2459 -1788 1257 80.5 1872 1872 | 3119 0
brd 2311 5 | 38 111 267 129 -209 5388 81.1 2147 2147 | 4418 0
brd 2311 6 | 10 -69 122 33 2715 10350 80.9 2371 2371 | 4661 0
-------------+------------------------------------------------------------+----------------
brd 2311 mean| -8 22 153 242 201 4772 81.0 1969 1969 | 4288 0
brd 2311 sdev| 63 66 66 1450 1485 3426 .8 282 282 | 910 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 2.2311.0 GPS week: 2311 Day: 0 MJD: 60421
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 2 -6 -1 80 .07 18 17 | 558 272 2940 7683
esa n/a| -1 -3 3 -49 15 -91 -.04 37 23 | 6124 1712 2946 7900
gfz n/a| 2 0 -4 40 7 -61 .05 25 23 | 0 466 2989 6945
grg n/a| 0 2 1 1 -28 65 .26 25 18 | 2783 462 3005 6719
iac n/a| -1 0 -8 2 38 0 -.13 21 18 | 4808 -1076 2885 7747
jgx n/a| 1 0 0 -4 8 -59 -.22 31 30 | 3398 448 2966 7197
Table 2.2311.1 GPS week: 2311 Day: 1 MJD: 60422
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 -2 -16 75 .06 18 14 | 4499 3344 3369 8961
esa n/a| 0 -1 1 -22 -23 -22 -.06 50 24 | 13979 4660 3348 8218
gfz n/a| 1 -1 1 28 33 -39 .06 21 15 | 0 2581 3382 8321
grg n/a| 0 0 4 -6 -9 30 .24 25 20 | 4169 2777 3380 7897
iac n/a| -1 1 -7 13 25 -61 -.07 20 21 | 7131 980 3355 9082
jgx n/a| -1 0 -7 9 4 -6 -.21 31 33 | 7249 3366 3498 8983
Table 2.2311.2 GPS week: 2311 Day: 2 MJD: 60423
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 -23 -14 17 .03 19 15 | 5246 555 3232 7544
esa n/a| 1 -2 3 -6 -20 -3 .01 47 23 | 9859 2103 3239 8096
gfz n/a| 1 0 0 39 3 11 .00 21 15 | 0 747 3242 6883
grg n/a| 1 0 3 -12 3 18 .15 26 19 | 3738 834 3244 6670
iac n/a| -1 3 -6 -11 33 -13 -.08 27 18 | 5656 -463 3253 7539
jgx n/a| 0 -3 -7 10 38 -51 -.22 34 32 | 7911 885 3242 7092
Table 2.2311.3 GPS week: 2311 Day: 3 MJD: 60424
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 5 -14 -9 48 .04 15 14 | 1625 1314 3536 22966
esa n/a| 0 -1 4 0 5 -4 -.04 42 24 | 4822 2996 2956 5857
gfz n/a| 2 0 -2 15 -2 -33 .07 22 15 | 0 1481 2994 5600
grg n/a| 2 -1 3 -78 13 10 .18 34 23 | -710 945 3615 23619
iac n/a| -1 0 -10 35 1 32 -.11 22 20 | 1378 1484 3453 21409
jgx n/a| 0 -1 -8 6 20 -76 -.20 41 38 | 8538 1411 3047 5781
Table 2.2311.4 GPS week: 2311 Day: 4 MJD: 60425
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 -21 -14 72 .13 20 15 | 1690 -2993 4239 24974
esa n/a| 0 0 0 -16 -7 41 -.04 41 23 | -1509 -1577 3849 7439
gfz n/a| 1 0 1 18 28 -2 -.06 21 16 | 0 -2506 3791 7344
grg n/a| 2 -2 7 4 -6 76 .30 28 22 | -1107 -2417 4226 25395
iac n/a| 1 1 -7 1 -6 -73 -.02 18 17 | 1319 -2734 4178 23240
jgx n/a| 1 -1 -6 23 27 -95 -.22 32 24 | 8668 -2615 3947 7798
Table 2.2311.5 GPS week: 2311 Day: 5 MJD: 60426
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 3 -11 -2 102 .05 21 17 | 792 848 3427 25301
esa n/a| -1 0 -1 11 4 18 -.00 44 26 | -4919 3111 2848 7584
gfz n/a| 0 0 -1 37 13 0 -.02 21 20 | 0 424 2821 6524
grg n/a| 3 0 3 -40 -28 -37 .24 22 19 | -974 275 3499 25813
iac n/a| -1 1 -1 -28 26 -3 -.15 22 20 | 1075 448 3358 23597
jgx n/a| -1 -2 -6 15 52 -124 -.17 32 26 | 7706 853 2934 6841
Table 2.2311.6 GPS week: 2311 Day: 6 MJD: 60427
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 -9 -22 24 .04 20 17 | 7332 1183 3534 8541
esa n/a| 0 -2 2 -26 -11 8 .01 42 25 | 1012 2206 3530 8203
gfz n/a| 0 0 -1 4 -3 -28 .03 18 13 | 0 1922 3412 7638
grg n/a| 1 4 3 -20 -33 19 .26 29 28 | 3630 1612 3397 7776
iac n/a| 1 0 2 10 16 78 -.09 20 20 | 7243 234 3528 9395
jgx n/a| 0 -1 -4 43 44 -117 -.20 24 19 | 8164 2425 3425 7908
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 3.2311.0 GPS week: 2311 Day: 0 MJD: 60421
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 931 31 39 22 33 15 33 13 | 62 46 60 61 55 53 53
R02 | 756 11 18 13 17 9 25 7 | 41 47 45 45 45 34 41
R03 | 878 9 16 20 9 16 12 6 | 46 54 57 52 54 46 49
R04 | 1133 19 13 21 7 14 9 7 | 46 39 38 38 26 33 35
R05 | 969 16 13 17 13 34 19 9 | 39 39 32 33 54 29 35
XR07 | 1430 8 13 11 16 --- --- 7 | 53 55 54 63 --- --- 55
R08 | 2213 9 16 11 14 17 19 6 | 44 47 50 50 57 38 47
R09E | 2511 15 8 17 18 10 17 6 | 60 67 65 67 61 65 63
R11E | 1410 12 9 11 13 10 17 5 | 55 51 45 49 49 45 48
R12E | 758 12 20 13 21 31 14 9 | 179 181 182 172 172 170 176
R13E | 2248 22 42 64 29 27 44 17 | 54 46 86 64 57 57 50
R14E | 1111 6 21 18 21 10 14 6 | 42 36 37 44 37 40 37
R15E | 1341 12 11 13 22 19 21 7 | 66 57 58 71 50 68 60
R16E | 995 12 16 23 19 15 22 8 | 19 25 24 25 19 26 17
XR17 | 1976 7 9 6 23 19 --- 7 | 69 64 71 70 79 --- 69
R18 | 904 14 20 14 11 15 28 7 | 55 67 65 58 69 45 59
R19 | 1320 37 58 38 49 25 64 20 | 76 68 92 81 77 56 71
R20 | 1847 34 122 28 66 46 65 27 | 127 64 154 153 143 91 131
R21 | 1585 9 34 29 13 21 35 10 | 75 65 96 82 85 62 77
R22 | 2432 13 11 20 10 10 11 6 | 41 46 46 51 50 45 44
R24 | 638 12 31 16 13 19 30 9 | 77 66 83 79 82 62 75
XR25 |13879 15 13 --- --- 18 --- 11 | 33 35 --- --- 39 --- 33
XR26 | 9257 24 --- --- 25 49 --- 24 | 51 --- --- 48 80 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 1488 18 37 25 25 21 31 |T 61 57 68 66 65 56 59
WRMS | 1488 17 23 23 18 18 30 |NE 58 53 67 64 66 49 57
MEDI | 1341 12 16 17 17 17 21 |MD 54 51 58 58 55 46 50
Table 3.2311.1 GPS week: 2311 Day: 1 MJD: 60422
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1693 23 24 22 41 16 29 11 | 35 40 50 50 32 32 37
R02 | 1440 9 8 15 25 13 18 6 | 25 27 31 41 28 28 26
R03 | 2062 11 14 13 10 13 10 5 | 29 39 40 29 31 30 32
R04 | 910 23 9 9 7 22 14 7 | 32 31 30 27 23 21 26
R05 | 834 11 15 12 16 39 27 9 | 22 37 28 25 45 28 26
XR07 | 1170 9 13 13 9 17 --- 6 | 39 35 45 40 52 --- 38
R08 | 2306 6 9 11 17 13 21 5 | 37 31 36 34 35 28 32
R09E | 4401 13 9 11 15 13 17 6 | 58 60 58 59 59 59 57
R11E | 1664 16 8 25 18 10 19 7 | 44 34 35 50 44 29 37
R12E | 1257 15 11 19 30 14 15 8 | 128 135 129 132 124 123 128
XR13E | 1638 34 34 53 43 37 --- 20 | 41 57 86 39 69 --- 48
R14E | 1115 11 18 14 22 11 13 7 | 31 37 25 31 28 32 27
R15E | 2387 11 15 12 24 17 19 7 | 48 50 42 46 43 51 44
R16E | 1251 11 16 28 17 19 15 8 | 28 35 37 28 28 31 28
XR17 | 1162 7 16 9 16 19 --- 7 | 38 36 38 37 45 --- 36
R18 | 642 15 25 19 15 25 34 10 | 30 41 26 28 47 22 29
R19 | 1720 40 40 35 48 30 63 19 | 54 34 46 36 35 51 37
R20 | 1323 34 197 38 47 32 85 23 | 61 62 74 70 79 54 64
R21 | 1689 11 11 15 16 15 25 7 | 39 41 38 32 40 34 35
R22 | 2590 12 9 19 13 15 13 6 | 25 28 37 31 27 27 27
R24 | 675 12 29 27 13 21 20 9 | 43 46 55 39 48 39 43
XR25 |15210 20 22 --- --- 15 --- 14 | 33 22 --- --- 32 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1877 18 50 21 25 20 31 |T 41 43 46 42 45 39 40
WRMS | 1877 14 24 15 20 21 33 |NE 35 36 41 36 40 32 34
MEDI | 1440 12 15 15 17 16 19 |MD 37 37 38 36 43 31 35
Table 3.2311.2 GPS week: 2311 Day: 2 MJD: 60423
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1003 20 25 23 44 17 27 11 | 45 38 41 53 50 35 42
R02 | 1007 12 13 12 10 13 10 5 | 35 33 31 34 38 40 33
R03 | 1286 13 11 9 11 16 16 5 | 32 34 41 40 39 32 35
R04 | 1491 19 7 8 13 16 19 6 | 31 31 31 33 25 27 28
R05 | 826 10 8 14 13 13 18 5 | 22 25 28 24 17 24 20
XR07 | 1044 22 15 15 9 23 --- 9 | 36 56 53 44 43 --- 48
R08 | 2556 18 11 23 20 14 36 9 | 36 54 66 56 49 39 49
R09E | 5380 18 13 21 15 12 19 7 | 52 59 54 55 50 58 53
R11E | 2785 13 12 12 13 9 16 5 | 30 29 32 29 26 25 27
R12E | 772 9 15 12 13 19 16 6 | 89 86 88 86 85 85 86
R13E | 1338 45 27 40 32 85 46 21 | 46 44 65 44 117 47 52
R14E | 1250 10 17 14 14 14 12 6 | 32 41 35 37 37 32 33
R15E | 2074 9 16 11 16 16 13 6 | 42 47 44 46 46 52 44
R16E | 1012 16 20 14 27 20 12 8 | 41 33 37 42 31 37 33
XR17 | 1082 13 29 21 12 22 --- 10 | 52 44 66 56 64 --- 55
R18 | 883 11 15 15 19 15 30 7 | 40 48 50 37 46 33 41
R19 | 1818 30 49 34 71 28 78 22 | 62 36 64 72 50 36 50
R20 | 3796 32 189 42 36 37 83 23 | 93 44 137 117 128 76 109
R21 | 931 9 23 21 17 15 32 9 | 50 39 59 53 48 40 48
R22 | 2618 16 13 8 16 27 28 8 | 36 34 36 45 47 30 35
R24 | 1383 13 27 10 19 21 17 8 | 48 51 44 57 53 43 47
XR25 |13209 20 14 --- --- 16 --- 12 | 26 25 --- --- 25 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2143 19 47 21 26 27 34 |T 45 42 52 51 51 41 45
WRMS | 2143 15 23 15 19 18 32 |NE 44 39 53 52 49 37 44
MEDI | 1286 13 15 14 16 16 19 |MD 41 39 44 45 47 37 42
Table 3.2311.3 GPS week: 2311 Day: 3 MJD: 60424
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 953 20 22 16 43 14 29 10 | 59 48 58 54 58 42 54
R02 | 1035 7 16 13 17 13 29 6 | 48 47 50 41 44 30 43
R03 | 961 10 11 11 16 10 18 5 | 44 46 46 49 43 38 43
R04 | 1658 20 13 21 15 16 13 8 | 35 34 31 28 26 22 26
R05 | 726 14 14 11 14 25 20 7 | 35 33 28 35 30 33 27
R07 | 888 14 17 8 29 17 15 7 | 47 49 50 65 44 24 50
R08 | 1352 8 14 10 10 15 32 6 | 37 46 44 40 44 30 40
R09E | 3764 14 11 24 15 12 12 7 | 46 49 52 48 43 49 46
R11E | 2698 11 16 15 20 17 14 6 | 27 27 32 32 28 26 26
R12E | 1075 13 16 21 50 42 16 12 | 107 106 117 114 81 103 103
R13E | 1700 26 24 42 47 24 80 17 | 49 49 76 37 55 53 49
R14E | 1014 14 16 13 53 10 18 9 | 37 46 37 67 36 39 38
R15E | 1680 8 16 15 54 12 15 9 | 33 34 35 70 40 36 35
R16E | 1070 11 31 20 33 24 17 10 | 33 53 40 59 31 41 36
XR17 | 1018 13 24 12 20 22 --- 9 | 55 48 57 72 72 --- 58
R18 | 806 12 12 11 13 12 28 6 | 47 52 56 55 56 37 50
R19 | 2192 21 42 38 66 35 80 20 | 64 65 88 79 66 53 64
R20 | 3870 25 169 47 38 36 114 26 | 91 46 130 122 127 68 105
R21 | 1216 7 15 19 11 15 30 7 | 52 45 60 56 59 49 52
R22 | 2682 14 18 11 16 14 11 6 | 32 35 49 51 45 50 40
R24 | 1741 11 24 12 19 29 24 9 | 55 54 59 70 75 51 59
XR25 |13963 19 11 --- --- 26 --- 14 | 27 30 --- --- 44 --- 29
XR26 | 9646 20 --- --- 43 45 --- 24 | 39 --- --- 40 77 --- 67
------+-----------------------------------------+-------------------------------------
RMS | 1890 15 42 22 34 22 41 |T 47 47 56 58 53 43 49
WRMS | 1890 14 24 15 23 20 38 |NE 47 45 57 57 56 40 50
MEDI | 1352 14 16 15 20 17 18 |MD 46 46 50 54 44 39 46
Table 3.2311.4 GPS week: 2311 Day: 4 MJD: 60425
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1039 25 18 25 39 17 31 11 | 58 53 64 41 57 39 50
R02 | 1204 11 13 20 20 17 34 9 | 45 49 53 34 49 32 41
R03 | 768 18 9 18 12 16 18 7 | 43 51 62 49 55 46 50
R04 | 1044 13 19 12 10 13 14 6 | 35 32 39 35 33 36 32
R05 | 754 16 11 12 18 18 12 6 | 33 33 33 37 25 32 28
R07 | 564 8 23 10 29 13 18 8 | 41 39 41 54 32 18 37
R08 | 810 9 16 7 20 15 19 6 | 38 33 37 48 38 27 35
R09E | 3507 15 13 20 19 17 21 7 | 41 43 57 44 43 52 44
R11E | 4080 17 11 13 17 14 14 6 | 35 29 32 31 31 30 29
R12E | 656 12 15 14 13 16 18 6 | 87 98 96 93 86 86 90
XR13E | 2130 35 28 62 28 22 --- 19 | 40 50 85 41 37 --- 40
R14E | 1892 15 19 16 13 16 14 7 | 23 32 25 32 29 29 24
R15E | 695 9 11 21 28 19 15 8 | 46 47 45 60 40 40 43
R16E | 1471 13 21 27 19 11 20 8 | 24 40 33 40 29 26 28
XR17 | 1047 10 28 14 14 26 --- 10 | 41 42 53 44 58 --- 46
R18 | 643 12 12 17 17 10 16 6 | 35 36 44 46 37 36 37
R19 | 668 57 42 31 61 22 23 18 | 60 43 64 47 61 65 51
R20 | 3745 26 164 47 68 26 110 30 | 80 57 80 100 75 42 68
R21 | 1074 13 14 14 14 25 31 8 | 40 43 46 37 52 26 39
R22 | 2637 16 11 17 14 16 11 6 | 45 48 54 56 41 48 46
R24 | 1495 9 18 16 13 25 18 7 | 38 39 41 41 42 38 37
XR25 |14418 19 12 --- --- 13 --- 10 | 31 31 --- --- 24 --- 26
XR26 |12460 41 --- --- 26 58 --- 32 | 40 --- --- 53 68 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1872 20 41 21 28 18 32 |T 43 44 51 48 45 39 41
WRMS | 1872 15 23 16 22 17 24 |NE 43 41 50 48 46 37 41
MEDI | 1074 15 15 17 18 17 18 |MD 40 42 46 44 41 36 39
Table 3.2311.5 GPS week: 2311 Day: 5 MJD: 60426
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1512 46 47 17 30 30 49 17 | 56 33 43 37 53 35 35
R02 | 1148 14 12 18 9 20 23 7 | 41 48 58 38 54 38 45
R03 | 694 21 10 15 12 33 26 9 | 37 47 55 47 61 38 46
R04 | 1159 12 13 10 8 17 17 6 | 32 27 36 29 38 22 28
R05 | 737 22 12 17 10 22 13 7 | 31 27 28 27 24 23 22
R07 | 1125 10 15 15 10 21 15 6 | 31 27 30 31 30 26 28
R08 | 1218 12 15 12 12 20 20 6 | 31 34 33 36 37 40 32
R09E | 4872 14 9 14 12 13 13 5 | 60 62 66 51 61 62 59
R11E | 4639 12 9 16 17 14 22 6 | 38 37 38 39 35 37 35
R12E | 1287 13 16 12 12 24 22 7 | 149 149 146 148 142 140 145
XR13E | 1082 22 26 41 34 22 --- 15 | 41 66 83 39 46 --- 51
R14E | 1910 12 14 18 24 15 16 7 | 26 28 32 29 31 28 25
R15E | 1024 9 15 18 18 20 23 7 | 49 59 60 46 44 63 50
R16E | 1228 11 16 22 12 21 17 7 | 21 28 26 31 23 25 21
XR17 | 703 11 18 14 10 16 --- 7 | 36 35 42 44 39 --- 38
R18 | 897 20 22 14 11 18 21 8 | 32 38 33 39 38 33 33
R19 | 1347 46 43 26 47 28 34 17 | 35 29 47 36 52 44 36
R20 | 3719 26 171 41 59 37 97 27 | 71 78 73 80 49 52 61
R21 | 816 8 23 18 24 18 31 9 | 44 38 45 56 39 37 43
R22 | 2755 16 16 25 9 19 11 7 | 42 36 40 36 39 38 36
R24 | 1011 9 30 36 10 17 30 10 | 38 36 56 49 42 37 41
XR25 |18173 12 12 --- --- 16 --- 9 | 34 32 --- --- 35 --- 31
XR26 |10867 42 --- --- 20 67 --- 32 | 59 --- --- 62 75 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 2147 21 44 21 22 22 32 |T 44 45 50 46 47 43 43
WRMS | 2147 17 26 20 19 20 26 |NE 40 37 44 43 44 35 38
MEDI | 1218 13 15 17 12 20 22 |MD 38 36 43 39 39 37 36
Table 3.2311.6 GPS week: 2311 Day: 6 MJD: 60427
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1122 52 51 28 26 25 20 16 | 80 52 67 79 78 59 66
R02 | 888 10 19 16 15 22 20 8 | 60 53 58 61 64 51 56
R03 | 954 13 16 10 14 27 18 7 | 63 64 70 69 79 61 67
R04 | 2094 10 22 7 28 18 9 7 | 54 53 46 43 51 45 46
R05 | 1599 15 12 15 18 12 20 7 | 52 42 47 42 37 32 41
R07 | 2926 14 14 7 10 18 15 6 | 57 60 67 69 55 34 62
R08 | 1126 16 13 11 25 14 10 6 | 49 55 61 66 58 50 55
R09E | 5111 14 10 15 16 12 11 6 | 55 63 70 58 60 59 60
R11E | 6130 12 10 14 15 10 14 5 | 43 44 41 42 42 38 40
R12E | 2528 12 16 14 17 21 17 7 | 176 179 178 169 168 166 173
R13E | 1853 22 38 26 32 26 36 13 | 56 65 64 62 54 68 56
R14E | 1232 15 17 11 23 11 11 6 | 55 60 54 64 51 56 55
R15E | 950 10 13 10 32 21 12 7 | 64 61 57 79 57 61 61
R16E | 1411 11 16 16 19 14 11 6 | 39 38 47 42 41 43 39
XR17 | 1046 12 17 11 23 12 --- 7 | 57 48 56 64 62 --- 55
R18 | 1030 18 17 14 28 16 16 8 | 44 50 46 57 54 39 46
R19 | 1472 37 22 20 77 33 49 18 | 71 48 72 70 63 53 57
R20 | 2095 35 162 38 49 29 62 21 | 113 56 113 131 106 57 101
R21 | 632 9 22 18 31 11 22 8 | 54 42 57 68 59 42 51
R22 | 2486 14 11 16 13 7 15 6 | 34 33 46 44 34 35 35
R24 | 742 13 20 13 16 28 16 8 | 59 51 60 59 68 49 56
XR25 |17670 9 10 --- --- 15 --- 8 | 34 27 --- --- 35 --- 31
XR26 | 9845 43 --- --- 29 67 --- 35 | 66 --- --- 71 96 --- 60
------+-----------------------------------------+-------------------------------------
RMS | 2371 20 42 18 29 20 24 |T 62 56 65 68 64 54 59
WRMS | 2371 17 25 13 28 20 19 |NE 59 48 61 66 62 46 55
MEDI | 1472 14 16 14 23 18 16 |MD 56 52 58 64 58 50 56
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