[IGSREPORT-28842] Wk 2220 IGLOS Final Orbits
acc
acc at igs.org
Sat Aug 13 10:10:15 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2220 (Jul 24, 2022 - Jul 30, 2022)
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 2.2220.
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:
igl2220[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2220 in the SP3 format.
igl22207.sum Combination Report for GPS Week 2220.
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.
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 | 1.3 ns
1 | -1.6 ns
2 | 0.9 ns
3 | -1.4 ns
4 | -1.4 ns
5 | 1.5 ns
6 | -0.8 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 | EMX | R19
2 | EMX | R19
3 | EMX | R19
4 | EMX | R19
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 1.2220, 1a.2220).
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 2.2220.0-6)
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 3.2220.0-6).
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 2220 summary. (Jul 24, 2022 - Jul 30, 2022)
Table 1.2220.a GPS week : 2220 MJD: 59784.0-59790.0
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 1 -4 -25 18 .09 23 16 | 36449 -1008 3357 8851
| 1 0 1 17 9 21 .04 | 1185 2686
emx n/a| 0 0 3 26 -13 -24 -.15 46 28 | -8211 -1053 3371 8675
| 0 1 2 17 19 23 .06 | 12401 1959
esx n/a| 0 1 0 -9 8 0 -.08 29 24 | -8225 44 3347 11789
| 1 1 0 10 7 31 .03 | 5743 2465
gfz n/a| 1 0 -1 0 5 3 -.06 23 15 | 0 -845 3385 8694
| 1 1 1 17 13 30 .06 | 0 2818
grg n/a| 2 -1 0 14 15 -23 .36 26 20 | 148 -969 3357 8347
| 0 2 2 23 9 24 .02 | 229 2551
iac n/a| -1 0 1 -4 9 19 -.15 23 22 | 2522 -1419 3349 9431
| 1 1 2 30 35 74 .06 | 953 1396
Table 1.2220.b GPS week : 2220 MJD: 59784.0-59790.0
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 | 17 17 19 17 17 24 23 |
R02 | 8 6 7 9 8 8 9 |
R03 | 7 7 8 7 7 7 9 |
R04 | 8 9 8 11 10 8 9 |
R05 | 7 9 8 8 7 9 9 |
R07 | 7 8 8 6 6 7 9 |
R08 | 6 7 8 7 7 7 8 |
R09 | 8 6 8 9 7 7 7 |
R11 | 7 7 8 9 10 10 9 |
R12 | 6 6 6 7 7 8 7 |
R13 | 13 13 12 13 13 15 16 |
R14 | 6 5 8 7 6 7 6 |
R15 | 6 6 7 7 6 6 8 |
R17 | 6 7 7 6 7 8 7 |
R18 | 9 8 8 8 9 8 7 |
R19 | 26 29 28 26 26 27 23 |
R20 | 21 22 24 23 24 20 24 |
R21 | 8 8 7 9 7 8 8 |
R24 | 8 9 10 9 9 10 9 |
Table 1.2220.c GPS week : 2220 MJD: 59784.0-59790.0
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 2220 0 | 17 29 236 -685 764 7400 85.1 1860 1860 | 1323 0
brd 2220 1 | 123 10 183 -1268 82 6407 83.8 2367 2367 | -1574 0
brd 2220 2 | 0 -16 98 587 656 5826 82.6 2045 2045 | 948 0
brd 2220 3 | -38 36 124 -810 -840 5220 82.2 1892 1892 | -1441 0
brd 2220 4 | -117 21 48 -1611 275 8007 85.4 1574 1574 | -1381 0
brd 2220 5 | -92 4 76 944 -510 6373 84.0 1446 1446 | 1496 0
brd 2220 6 | -29 -36 158 3049 -2434 2025 82.4 1489 1489 | -824 0
-------------+------------------------------------------------------------+----------------
brd 2220 mean| -19 7 132 29 -286 5894 83.6 1810 1810 | -207 0
brd 2220 sdev| 79 25 65 1625 1111 1943 1.3 333 333 | 1397 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 2.2220.0 GPS week: 2220 Day: 0 MJD: 59784
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 0 6 -19 35 .12 24 16 | 35605 1714 3162 7885
emx n/a| 0 2 3 16 -10 -35 -.09 42 28 | -2402 676 3173 7741
esx n/a| 2 0 0 -21 5 50 -.13 25 19 | -1071 2640 3138 11310
gfz n/a| 0 0 -2 5 10 19 -.07 26 18 | 0 2297 3134 7543
grg n/a| 2 0 0 -2 16 -32 .32 21 16 | 506 1602 3150 7344
iac n/a| -1 -3 2 18 5 -39 -.20 19 18 | 3978 -1007 3131 8483
Table 2.2220.1 GPS week: 2220 Day: 1 MJD: 59785
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 0 -11 -11 23 .06 21 15 | 36365 -3760 3866 10068
emx n/a| 0 0 4 43 -19 -8 -.08 47 26 | 5701 -2199 3894 9915
esx n/a| 0 0 0 1 0 2 -.09 30 23 | -14408 -2856 3897 13150
gfz n/a| 1 0 0 -12 28 -18 .01 25 15 | 0 -3823 3861 9857
grg n/a| 2 -2 -2 5 29 4 .36 24 17 | 42 -3580 3883 9379
iac n/a| -3 0 1 19 -57 -24 -.20 21 19 | 1832 -3329 3886 10679
Table 2.2220.2 GPS week: 2220 Day: 2 MJD: 59786
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 0 -6 -33 17 .09 23 16 | 37125 701 3756 8395
emx n/a| -1 0 1 39 14 -48 -.16 49 26 | -15393 400 3758 8170
esx n/a| 0 0 0 -2 0 -34 -.06 29 34 | -7555 1979 3723 11254
gfz n/a| 2 0 0 -5 -1 -6 -.14 22 16 | 0 1262 3794 8090
grg n/a| 2 0 0 15 7 -4 .39 25 21 | 266 1000 3734 7844
iac n/a| -4 0 2 -40 36 80 -.13 27 26 | 2777 598 3728 8888
Table 2.2220.3 GPS week: 2220 Day: 3 MJD: 59787
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 -7 -30 -3 .08 21 17 | 36075 -3814 3015 9102
emx n/a| 0 2 4 6 -2 -24 -.27 47 28 | 9732 -3777 3035 8814
esx n/a| -1 1 0 -9 21 -24 -.07 30 25 | -11039 -2568 3007 11555
gfz n/a| 2 -1 -4 -18 -10 22 -.10 22 14 | 0 -3323 3060 9063
grg n/a| 3 -2 0 -4 19 -27 .38 22 20 | 147 -3408 3017 8486
iac n/a| -1 2 4 35 -2 103 -.16 27 27 | 1388 -2761 3004 9641
Table 2.2220.4 GPS week: 2220 Day: 4 MJD: 59788
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 2 -26 -17 28 .06 20 17 | 35128 -2468 3488 8953
emx n/a| 0 0 7 12 -36 18 -.17 52 31 | -16432 -2921 3531 8817
esx n/a| -1 1 -1 0 4 30 -.08 27 21 | 79 -1150 3467 12012
gfz n/a| 3 1 -1 36 0 49 -.05 20 12 | 0 -2375 3554 8964
grg n/a| 2 -4 0 64 21 -69 .39 32 26 | -236 -2278 3459 8504
iac n/a| 0 0 -2 -43 8 -96 -.03 23 23 | 1601 -1521 3482 9533
Table 2.2220.5 GPS week: 2220 Day: 5 MJD: 59789
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 0 27 -39 45 .06 28 18 | 36104 2740 2926 8715
emx n/a| -2 0 3 18 -39 -22 -.12 46 33 | -21140 1333 2912 8563
esx n/a| 0 3 0 -7 15 -3 -.05 31 20 | -13489 2996 2908 11579
gfz n/a| 3 -1 -1 -7 -5 -46 .02 19 14 | 0 2715 2955 8628
grg n/a| 1 1 0 18 12 -9 .35 31 23 | 73 2433 2957 8171
iac n/a| -1 -3 0 -14 53 38 -.16 21 19 | 3287 -69 2926 9332
Table 2.2220.6 GPS week: 2220 Day: 6 MJD: 59790
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 1 -12 -27 -17 .16 21 15 | 38742 -2172 3286 8841
emx n/a| 0 0 0 50 0 -49 -.15 38 24 | -17549 -886 3295 8707
esx n/a| -2 2 0 -23 12 -23 -.08 31 24 | -10094 -733 3293 11663
gfz n/a| 1 -2 -2 4 18 6 -.11 26 16 | 0 -2674 3343 8713
grg n/a| 1 0 4 2 0 -27 .36 28 20 | 244 -2554 3299 8706
iac n/a| 0 -1 0 -7 24 75 -.19 23 21 | 2792 -1845 3286 9465
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 3.2220.0 GPS week: 2220 Day: 0 MJD: 59784
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1377 26 52 33 59 31 25 16 | 68 65 72 78 76 66 66
R02E | 4592 15 24 14 24 12 18 8 | 58 57 60 52 63 58 57
R03E | 3103 12 34 13 14 13 16 7 | 78 82 84 82 84 79 80
XR04E | 2849 8 29 16 --- 12 15 7 | 51 47 48 --- 55 51 49
R05E | 1718 12 33 12 15 11 18 7 | 89 94 87 86 89 89 88
R07E | 1891 9 27 14 12 15 18 7 | 72 68 74 72 72 61 69
R08E | 1345 9 22 16 11 16 12 6 | 68 60 68 72 70 63 66
R09 | 1273 19 15 15 15 19 20 8 | 48 44 42 39 36 43 39
R11 | 2449 17 18 17 14 11 13 6 | 30 34 24 25 25 26 24
R12 | 674 17 12 15 14 9 13 6 | 43 43 48 48 43 38 42
R13 | 842 25 24 28 33 41 15 13 | 57 47 35 43 41 48 43
R14 | 820 10 13 11 12 15 12 5 | 44 40 48 49 48 46 44
R15 | 1008 11 11 11 19 9 18 6 | 59 56 54 57 51 55 53
R17 | 1835 10 29 11 10 11 14 6 | 67 45 60 63 65 65 61
R18 | 853 9 20 31 22 10 13 8 | 47 42 63 46 52 46 48
R19 | 1125 47 122 64 52 41 26 25 | 115 60 66 116 102 101 93
R20 | 1484 66 76 42 35 34 35 21 | 105 51 73 91 78 60 72
R21 | 1235 18 18 10 15 13 29 8 | 62 45 55 62 57 54 54
R24 | 1314 12 43 14 15 15 14 8 | 76 53 68 74 74 60 68
------+-----------------------------------------+-------------------------------------
RMS | 1859 24 42 25 26 21 19 |T 65 54 59 64 62 58 58
WRMS | 1859 16 28 19 18 16 18 |NE 62 46 53 59 56 53 53
MEDI | 1345 12 24 15 15 13 16 |MD 62 51 60 62 63 58 57
Table 3.2220.1 GPS week: 2220 Day: 1 MJD: 59785
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 986 24 47 36 55 38 29 17 | 52 52 60 70 75 47 55
R02E | 7579 8 21 11 10 11 17 5 | 39 41 43 44 47 40 40
R03E | 1507 9 29 14 11 10 17 6 | 54 60 58 62 62 50 56
XR04E | 3565 8 32 14 --- 17 16 8 | 36 36 37 --- 38 34 34
R05E | 3595 12 33 18 23 14 14 8 | 65 67 58 62 70 72 64
R07E | 2846 9 30 11 14 11 23 7 | 43 48 39 46 50 38 42
R08E | 994 9 27 17 13 8 17 7 | 68 59 71 69 71 62 66
R09 | 832 11 17 14 12 16 13 6 | 32 33 30 36 19 24 27
R11 | 2174 7 11 15 14 21 19 6 | 17 26 31 21 21 18 19
R12 | 675 10 13 18 11 17 10 6 | 28 27 37 31 29 31 28
R13 | 688 20 21 26 31 46 17 12 | 46 39 45 40 27 44 38
R14 | 833 9 9 14 9 13 14 5 | 31 31 35 35 38 37 32
R15 | 913 9 13 20 13 14 12 6 | 34 39 38 39 43 38 36
R17 | 1177 10 27 13 14 21 11 7 | 36 34 38 40 51 34 36
R18 | 876 10 18 28 18 11 15 7 | 31 24 35 28 40 29 28
R19 | 1291 55 164 94 36 55 21 28 | 78 42 35 77 59 73 66
R20 | 1282 50 53 47 61 36 44 22 | 57 62 45 71 40 34 46
R21 | 1197 12 21 10 15 13 32 8 | 34 24 34 35 37 32 30
R24 | 1834 20 36 11 11 15 20 8 | 43 38 39 39 45 44 39
------+-----------------------------------------+-------------------------------------
RMS | 2367 21 47 30 25 24 21 |T 43 41 42 46 45 41 41
WRMS | 2367 15 26 23 15 17 19 |NE 38 34 36 41 37 36 35
MEDI | 1197 10 27 15 14 15 17 |MD 39 39 38 40 43 38 38
Table 3.2220.2 GPS week: 2220 Day: 2 MJD: 59786
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 805 39 43 39 47 28 48 18 | 40 40 45 70 58 59 42
R02E | 4092 8 24 15 11 15 21 7 | 39 43 37 39 45 40 38
R03E | 1367 12 26 13 19 13 17 7 | 55 46 52 45 61 61 52
XR04E | 4471 8 28 11 --- 12 19 8 | 36 32 35 --- 41 45 36
R05E | 2725 10 29 15 12 17 17 7 | 52 46 59 62 64 65 57
R07E | 3650 7 33 12 19 9 21 8 | 37 40 34 43 38 37 36
R08E | 995 14 29 15 9 16 25 8 | 58 56 49 51 61 43 51
R09 | 1258 11 22 21 17 13 24 8 | 42 46 47 38 48 47 42
R11 | 2454 18 16 20 11 15 17 7 | 20 26 32 23 19 19 17
R12 | 646 11 8 13 13 20 12 6 | 28 25 27 30 24 32 24
R13 | 683 21 14 21 14 49 31 12 | 57 36 42 46 31 64 43
R14 | 966 11 19 14 11 13 33 7 | 35 34 40 33 37 52 35
R15 | 975 10 15 7 11 17 26 6 | 43 41 39 36 33 50 38
R17 | 1009 10 23 17 11 15 23 7 | 44 36 41 47 42 50 42
R18 | 1059 10 23 28 10 17 17 8 | 36 28 45 35 35 32 33
R19 | 1603 51 173 82 31 54 41 27 | 80 50 35 59 60 84 61
R20 | 2437 56 62 53 55 46 39 23 | 78 69 62 81 68 50 65
R21 | 894 7 27 10 17 11 16 6 | 38 27 33 42 42 42 36
R24 | 3536 22 26 8 13 23 33 9 | 57 52 46 44 56 40 47
------+-----------------------------------------+-------------------------------------
RMS | 2046 23 49 29 22 25 27 |T 46 40 42 45 45 48 41
WRMS | 2046 16 26 34 16 21 26 |NE 46 39 40 42 41 46 40
MEDI | 1258 11 26 15 13 16 23 |MD 42 40 41 43 42 47 42
Table 3.2220.3 GPS week: 2220 Day: 3 MJD: 59787
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1108 37 46 30 46 29 41 17 | 36 32 49 62 58 43 40
R02E | 2425 11 22 21 14 15 32 8 | 49 45 58 53 55 41 49
R03E | 1084 11 24 16 17 13 20 7 | 47 50 48 51 51 47 47
XR04E | 4276 15 27 14 --- 19 34 10 | 34 30 37 --- 45 34 32
R05E | 1922 12 27 13 13 14 25 7 | 34 32 42 39 44 41 37
R07E | 2331 10 25 13 12 12 14 6 | 35 30 31 34 43 42 34
R08E | 1946 11 26 11 13 9 24 7 | 56 54 59 64 63 63 59
R09 | 1071 13 27 20 15 16 34 9 | 30 34 46 40 30 62 36
R11 | 2619 19 24 27 13 12 13 8 | 18 25 37 26 17 17 18
R12 | 644 9 12 20 16 17 21 7 | 27 26 36 34 21 31 25
R13 | 657 13 35 16 23 44 25 12 | 43 72 55 44 32 44 43
R14 | 994 7 13 18 15 14 24 7 | 34 29 44 31 32 42 33
R15 | 962 8 14 16 9 15 31 7 | 43 40 43 41 36 52 40
R17 | 1028 9 25 11 13 13 17 6 | 52 39 50 54 56 49 50
R18 | 1302 8 22 22 12 15 27 7 | 38 28 52 51 48 38 42
R19 | 1482 38 156 89 21 47 32 25 | 98 45 41 90 108 89 85
R20 | 3979 55 59 58 58 37 26 23 | 82 40 46 88 73 44 62
R21 | 1087 10 33 11 13 7 38 8 | 52 33 52 57 58 78 53
R24 | 3238 23 37 11 7 18 24 9 | 51 45 51 46 52 35 45
------+-----------------------------------------+-------------------------------------
RMS | 1892 21 47 30 22 22 27 |T 45 38 46 50 48 46 43
WRMS | 1892 17 28 25 14 20 27 |NE 47 38 46 50 46 48 44
MEDI | 1302 11 26 16 13 15 25 |MD 43 34 46 46 48 43 42
Table 3.2220.4 GPS week: 2220 Day: 4 MJD: 59788
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 2031 25 42 25 39 60 47 17 | 47 53 59 67 70 63 51
R02E | 2156 12 22 11 19 14 31 8 | 51 48 47 45 54 46 45
R03E | 688 12 27 13 14 15 16 7 | 61 67 65 61 72 71 64
XR04E | 3094 9 26 12 --- 19 30 9 | 37 36 39 --- 40 43 37
R05E | 1509 10 24 14 13 13 24 7 | 54 58 52 54 61 64 55
R07E | 1055 8 26 10 12 16 15 6 | 42 41 42 42 44 49 41
R08E | 1076 6 28 13 12 20 16 6 | 45 40 44 49 56 44 45
R09 | 1653 10 17 12 13 29 19 7 | 37 42 44 37 60 56 42
R11 | 2931 20 19 23 22 31 17 10 | 26 25 32 34 23 33 25
R12 | 676 16 15 15 14 13 22 7 | 30 33 35 33 32 32 28
R13 | 755 13 56 15 17 52 24 12 | 39 57 37 43 36 44 36
R14 | 969 10 15 13 9 21 12 6 | 29 31 37 33 25 39 31
R15 | 1362 11 14 14 9 17 16 6 | 48 42 39 46 49 41 43
R17 | 1061 15 27 13 11 18 19 7 | 53 43 41 51 45 50 45
R18 | 1296 14 21 23 11 21 27 8 | 38 32 48 39 42 43 39
R19 | 1798 47 169 79 24 65 16 26 | 80 49 44 74 95 69 66
R20 | 1364 46 80 61 45 56 27 23 | 83 62 55 84 80 83 69
R21 | 1355 9 32 7 15 12 16 6 | 48 36 44 49 46 46 44
R24 | 2426 16 49 9 10 23 18 9 | 59 50 61 55 61 59 56
------+-----------------------------------------+-------------------------------------
RMS | 1573 20 52 27 20 32 23 |T 47 44 45 49 52 51 45
WRMS | 1573 17 31 21 12 26 23 |NE 47 41 43 48 49 49 43
MEDI | 1362 12 26 13 13 20 19 |MD 47 42 44 46 49 46 44
Table 3.2220.5 GPS week: 2220 Day: 5 MJD: 59789
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1034 72 57 68 33 63 27 23 | 144 51 47 77 127 86 82
R02E | 1252 15 34 12 12 20 21 8 | 45 47 50 60 44 60 52
R03E | 859 7 33 14 9 8 16 6 | 60 65 61 59 62 63 60
XR04E | 2408 9 30 12 --- 19 13 8 | 32 34 35 --- 36 29 30
R05E | 1045 21 27 21 17 18 19 9 | 54 58 55 61 60 66 57
R07E | 1051 13 22 13 20 13 13 7 | 46 53 48 52 56 47 48
R08E | 1797 14 27 11 12 18 16 7 | 32 31 33 32 39 36 32
R09 | 2309 11 27 9 9 13 19 6 | 43 39 42 43 38 52 42
R11 | 2664 18 20 26 17 34 18 10 | 18 23 24 16 27 27 12
R12 | 1100 17 17 20 9 21 24 8 | 33 30 43 33 48 31 33
R13 | 1044 37 37 34 28 48 18 14 | 38 41 36 32 27 27 27
R14 | 1088 12 11 12 11 19 18 6 | 25 31 35 35 24 32 28
R15 | 989 19 12 14 8 19 9 6 | 39 33 38 35 27 33 33
R17 | 661 20 30 10 13 20 15 7 | 44 40 37 38 37 39 36
R18 | 1280 9 17 23 13 22 17 7 | 35 34 38 37 36 37 34
R19 | 2037 48 124 76 35 49 46 27 | 51 30 56 58 61 51 47
R20 | 1533 39 86 48 33 60 22 20 | 61 54 49 63 56 65 52
R21 | 770 11 35 17 16 12 17 8 | 36 31 34 42 37 37 35
R24 | 1662 21 52 11 15 17 17 9 | 46 45 46 42 50 50 44
------+-----------------------------------------+-------------------------------------
RMS | 1446 28 46 31 19 31 21 |T 46 40 42 45 46 45 41
WRMS | 1446 18 33 20 14 23 19 |NE 39 35 39 39 39 40 35
MEDI | 1100 17 30 14 13 19 18 |MD 43 39 42 42 39 39 36
Table 3.2220.6 GPS week: 2220 Day: 6 MJD: 59790
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 917 59 25 55 60 47 41 23 | 54 66 65 107 86 77 63
R02E | 2493 9 27 21 17 23 25 9 | 51 51 54 54 57 58 52
R03E | 816 9 26 34 12 17 12 8 | 75 73 89 74 74 75 75
XR04E | 1005 7 33 12 --- 14 18 8 | 41 42 36 --- 43 34 37
R05E | 1083 11 29 14 20 18 26 9 | 72 68 70 73 80 75 71
R07E | 1603 13 24 20 19 20 18 8 | 50 56 49 56 63 49 51
R08E | 1737 10 16 17 15 10 26 7 | 48 48 56 55 54 59 52
R09 | 2465 10 16 13 12 24 17 7 | 42 46 47 47 46 51 44
R11 | 2195 16 14 18 16 19 26 8 | 26 28 18 20 22 25 17
R12 | 1209 11 14 12 15 15 22 6 | 39 39 49 52 44 47 44
R13 | 859 28 23 54 24 49 28 16 | 52 46 47 48 42 41 39
R14 | 810 8 11 16 17 10 11 5 | 30 33 36 38 33 42 33
R15 | 750 15 12 20 16 16 19 7 | 57 57 49 56 42 51 50
R17 | 673 15 22 13 6 14 13 6 | 66 46 60 63 57 59 59
R18 | 1378 7 18 28 8 17 14 7 | 48 39 63 47 46 49 48
R19 | 1032 29 99 61 37 44 40 23 | 107 31 55 99 100 100 87
R20 | 1945 35 88 49 63 57 24 23 | 96 63 62 106 84 77 78
R21 | 932 10 27 15 11 17 20 7 | 64 47 59 67 60 65 60
R24 | 1732 12 45 6 19 9 9 8 | 66 39 58 62 65 55 58
------+-----------------------------------------+-------------------------------------
RMS | 1488 21 38 31 26 28 23 |T 57 48 53 62 57 57 53
WRMS | 1488 15 24 24 16 20 21 |NE 57 42 50 58 53 55 51
MEDI | 1083 11 24 18 16 17 20 |MD 52 46 55 56 57 55 52
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