[IGSREPORT-28647] Wk 2206 IGLOS Final Orbits
acc
acc at igs.org
Mon May 9 00:45:24 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2206 (Apr 17, 2022 - Apr 23, 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 2.2206.
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:
igl2206[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2206 in the SP3 format.
igl22067.sum Combination Report for GPS Week 2206.
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 | -7.4 ns
1 | 2.0 ns
2 | -0.5 ns
3 | 0.9 ns
4 | 0.3 ns
5 | 0.4 ns
6 | -0.7 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 1.2206, 1a.2206).
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 2.2206.0-6)
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 3.2206.0-6).
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 2206 summary. (Apr 17, 2022 - Apr 23, 2022)
Table 1.2206.a GPS week : 2206 MJD: 59686.0-59692.0
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 0 -1 -6 -26 21 .19 25 18 | 37355 557 3377 8449
| 0 1 2 15 22 9 .04 | 4389 2027
emx n/a| 1 1 12 27 3 -22 .03 38 31 | -3983 797 3350 8347
| 2 2 3 25 28 32 .06 | 4420 1536
esx n/a| 0 0 0 -6 20 -1 -.10 28 19 | -3351 764 3317 8379
| 1 1 2 19 20 39 .07 | 7184 1862
gfz n/a| 1 0 0 -13 9 -13 -.12 34 17 | 0 479 3344 8008
| 1 1 2 16 23 44 .06 | 0 1797
grg n/a| 0 -2 -7 -4 17 23 .18 30 23 | -994 366 3380 7622
| 2 1 3 10 37 26 .09 | 2711 1967
iac n/a| -4 0 0 13 -16 -3 -.32 31 28 | 1368 -116 3320 8857
| 1 3 1 24 40 100 .10 | 2935 1213
Table 1.2206.b GPS week : 2206 MJD: 59686.0-59692.0
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 | 19 17 19 13 12 14 13 |
R02 | 9 9 10 6 8 13 7 |
R03 | 8 9 9 5 6 7 6 |
R04 | 8 10 12 12 8 7 11 |
R05 | 8 9 9 10 9 9 10 |
R07 | 6 7 6 7 7 6 7 |
R08 | 6 9 8 8 8 10 9 |
R09 | 9 10 10 12 9 9 9 |
R11 | 15 15 11 10 11 23 10 |
R12 | 10 10 10 9 10 9 9 |
R13 | 17 15 16 19 20 18 17 |
R14 | 10 8 10 10 10 10 7 |
R15 | 8 10 7 8 10 12 8 |
R17 | 9 8 9 9 9 7 9 |
R18 | 9 11 9 7 8 11 11 |
R19 | 19 24 20 23 25 27 25 |
R20 | 21 23 28 29 29 21 23 |
R21 | 10 12 10 12 9 9 10 |
R22 | 27 27 27 29 29 30 30 |
R24 | 9 10 10 12 10 10 10 |
Table 1.2206.c GPS week : 2206 MJD: 59686.0-59692.0
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 2206 0 | 84 92 151 -965 -48 -4326 81.9 1676 1676 | -7378 0
brd 2206 1 | -60 13 106 1157 -3319 -3523 82.8 1543 1543 | 1990 0
brd 2206 2 | 41 -79 124 724 -910 -3652 81.7 1627 1627 | -474 0
brd 2206 3 | 16 -77 284 389 -565 461 81.8 1725 1725 | 919 0
brd 2206 4 | 48 63 201 -210 687 6168 83.4 1528 1528 | 290 0
brd 2206 5 | 4 106 205 304 420 11050 82.4 1389 1389 | 443 0
brd 2206 6 | -131 -39 103 -785 -565 9645 82.9 1579 1579 | -745 0
-------------+------------------------------------------------------------+----------------
brd 2206 mean| 0 11 168 87 -614 2260 82.4 1581 1581 | -707 0
brd 2206 sdev| 73 78 66 779 1322 6609 .7 110 110 | 3076 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 2.2206.0 GPS week: 2206 Day: 0 MJD: 59686
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 -17 5 21 .23 22 15 | 28052 -334 3144 8602
emx n/a| 5 -3 6 47 -9 -58 .04 38 29 | -2335 -400 3137 8574
esx n/a| -1 -1 0 -16 -4 -61 -.13 26 17 | -7093 401 3087 7390
gfz n/a| -1 0 2 1 35 -16 -.20 33 16 | 0 196 3114 7848
grg n/a| 0 -1 -4 4 -20 40 .29 29 23 | -7128 -813 3348 7918
iac n/a| -6 6 0 7 -16 14 -.39 30 27 | -4943 -2013 3087 9036
Table 2.2206.1 GPS week: 2206 Day: 1 MJD: 59687
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 -5 -39 31 .24 24 21 | 38427 3634 3233 8378
emx n/a| 2 3 13 12 3 -45 .12 36 30 | -5388 2078 3088 8182
esx n/a| 0 0 3 -14 45 -18 -.21 26 20 | -1440 4087 3160 8426
gfz n/a| 3 0 3 -28 40 -66 -.09 31 17 | 0 3267 3197 8152
grg n/a| -2 0 -11 -19 -2 75 .12 23 19 | 56 3469 3368 7639
iac n/a| -5 -3 -2 49 -83 20 -.34 32 31 | 3980 1950 3158 8726
Table 2.2206.2 GPS week: 2206 Day: 2 MJD: 59688
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 -23 -52 36 .17 27 20 | 36577 -717 3016 8296
emx n/a| 0 2 13 47 31 -51 -.09 36 32 | 2708 840 2999 8236
esx n/a| 0 2 -4 -37 43 -17 -.12 23 18 | -4055 -854 2943 7820
gfz n/a| 0 0 -3 0 21 -10 -.12 31 18 | 0 -867 2894 7912
grg n/a| 0 -3 -3 -5 -27 2 .15 27 20 | -76 -770 2851 7202
iac n/a| -4 1 0 5 39 55 -.18 31 28 | 1063 218 2930 8719
Table 2.2206.3 GPS week: 2206 Day: 3 MJD: 59689
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 21 -54 15 .15 24 16 | 37479 1982 3168 9290
emx n/a| 0 0 12 -8 42 1 .03 41 29 | -1510 2203 3189 9314
esx n/a| 2 0 0 3 20 2 -.02 28 22 | 8509 1160 3105 8670
gfz n/a| 0 0 -2 -37 6 39 -.08 38 17 | 0 1812 3127 9046
grg n/a| -2 -2 -6 -1 43 9 .07 32 22 | -97 1915 3110 8575
iac n/a| -2 -2 0 38 -51 -155 -.31 34 29 | 2931 218 3125 9793
Table 2.2206.4 GPS week: 2206 Day: 4 MJD: 59690
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 -10 -10 10 .17 26 18 | 39782 867 3365 9032
emx n/a| 0 0 16 64 14 18 .05 36 30 | -4606 1575 3351 8875
esx n/a| 1 3 1 2 14 32 -.03 28 18 | -791 1279 3270 8586
gfz n/a| 3 -1 -2 4 -19 -27 -.16 36 18 | 0 644 3298 8492
grg n/a| -1 -4 -12 7 11 17 .20 31 22 | 106 485 3317 7984
iac n/a| -2 3 3 -23 -2 -40 -.47 39 30 | 2604 -396 3298 9352
Table 2.2206.5 GPS week: 2206 Day: 5 MJD: 59691
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 -12 -16 12 .15 26 17 | 40092 1128 3716 7647
emx n/a| 0 1 10 11 -34 -36 .03 41 32 | -11743 1350 3699 7437
esx n/a| 1 0 2 26 25 -10 -.07 30 19 | -3230 1064 3685 7679
gfz n/a| 0 -1 0 -7 -5 -63 -.03 33 15 | 0 630 3745 7245
grg n/a| 2 -3 -4 1 51 -1 .32 38 29 | -222 798 3699 6920
iac n/a| -4 -2 0 0 10 159 -.32 30 28 | 2321 106 3683 7998
Table 2.2206.6 GPS week: 2206 Day: 6 MJD: 59692
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 3 -17 20 .20 25 17 | 41082 -2655 3999 7902
emx n/a| 1 3 13 20 -21 12 .01 41 34 | -5008 -2067 3989 7816
esx n/a| -2 0 3 -10 -5 60 -.09 33 21 | -15363 -1787 3970 10087
gfz n/a| 1 2 1 -24 -11 47 -.15 34 16 | 0 -2329 4035 7363
grg n/a| 0 -1 -9 -16 68 21 .13 29 24 | 398 -2519 3973 7118
iac n/a| -2 -1 -1 15 -7 -77 -.19 25 24 | 1624 -900 3959 8375
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 3.2206.0 GPS week: 2206 Day: 0 MJD: 59686
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1484 39 43 47 46 41 32 18 | 142 155 186 178 147 141 156
R02 | 2964 12 14 20 19 22 25 8 | 34 38 39 40 28 33 30
R03 | 904 11 21 11 12 11 30 7 | 42 43 43 49 51 65 46
XR04 | 1036 9 15 10 --- 14 25 7 | 44 39 43 --- 35 54 41
R05 | 514 18 15 14 17 16 22 7 | 33 37 45 46 37 35 36
R07 | 727 8 10 14 13 11 18 5 | 56 59 59 65 60 60 59
R08 | 1118 10 12 13 18 13 18 6 | 52 52 49 56 51 50 50
R09 | 3887 13 15 12 20 25 33 9 | 64 65 72 68 59 80 66
XR11 | 2145 --- --- 21 14 27 37 14 | --- --- 41 35 50 44 40
R12 | 1108 10 48 16 16 15 26 10 | 90 49 80 90 87 92 81
R13 | 1987 34 46 33 31 32 46 16 | 124 77 85 118 106 79 97
R14 | 1519 12 27 23 16 24 28 9 | 109 88 122 110 93 102 105
R15 | 1125 8 31 12 12 24 22 8 | 108 89 105 99 115 109 104
R17E | 1640 17 26 9 23 22 19 8 | 71 63 69 70 74 70 68
R18E | 628 13 23 18 14 19 27 8 | 78 73 78 74 74 66 72
R19E | 1573 27 62 35 60 38 38 19 | 62 92 101 94 79 76 77
R20E | 1435 41 58 56 56 32 35 21 | 52 60 76 79 57 51 51
R21E | 838 19 30 18 12 22 26 9 | 50 35 45 47 53 36 43
R22E | 1998 34 78 44 82 72 47 26 | 73 75 102 95 69 96 79
R24E | 726 13 28 13 15 22 29 9 | 94 108 97 92 110 95 97
------+-----------------------------------------+-------------------------------------
RMS | 1676 22 38 26 33 29 30 |T 72 68 76 79 71 71 69
WRMS | 1676 15 29 17 16 23 27 |NE 74 65 74 79 70 72 70
MEDI | 1125 13 27 16 17 22 27 |MD 64 63 72 74 60 66 66
Table 3.2206.1 GPS week: 2206 Day: 1 MJD: 59687
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1368 47 25 48 36 33 13 16 | 114 124 147 134 130 118 126
R02 | 1357 19 25 13 14 14 33 9 | 20 22 28 28 24 32 20
R03 | 873 14 16 20 17 9 35 8 | 25 24 29 38 27 48 28
XR04 | 836 21 11 22 --- 11 31 10 | 28 21 23 --- 27 48 25
R05 | 1219 21 23 14 15 13 32 9 | 18 24 41 41 28 52 28
R07 | 658 8 10 23 8 9 27 7 | 36 40 39 40 33 47 37
R08 | 919 12 13 22 26 20 21 9 | 34 37 53 42 32 24 35
R09 | 3436 15 16 22 17 29 30 10 | 51 60 54 50 48 43 48
XR11 | 3002 --- --- 25 9 19 43 14 | --- --- 48 41 35 44 38
R12 | 1107 19 49 16 16 18 14 10 | 65 34 59 55 60 57 54
R13 | 1772 34 45 38 28 18 28 14 | 100 66 81 96 108 84 88
R14 | 1821 11 28 20 16 15 21 8 | 97 93 107 96 105 78 96
R15 | 1133 10 29 18 22 21 28 9 | 85 68 78 66 84 101 80
R17E | 1572 19 30 13 12 12 21 8 | 66 53 65 61 61 69 61
R18E | 856 12 37 20 24 30 27 11 | 138 139 148 147 139 118 138
R19E | 1997 24 78 32 79 48 45 23 | 50 55 48 86 60 60 49
R20E | 1649 53 53 53 67 26 48 22 | 54 48 62 83 57 42 48
R21E | 1468 15 37 17 15 21 52 12 | 56 50 50 61 58 68 53
XR22E | 2777 51 --- 52 69 52 34 26 | 88 --- 114 111 106 115 101
R24E | 617 12 38 13 16 21 33 10 | 91 83 94 100 98 93 91
------+-----------------------------------------+-------------------------------------
RMS | 1543 24 36 26 31 23 32 |T 64 57 68 72 66 67 62
WRMS | 1543 21 30 20 17 19 31 |NE 56 51 60 60 57 59 54
MEDI | 1357 19 28 20 17 19 30 |MD 56 50 54 61 58 57 49
Table 3.2206.2 GPS week: 2206 Day: 2 MJD: 59688
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 893 37 31 43 41 53 37 18 | 73 72 57 61 61 81 61
R02 | 1445 15 20 15 22 11 44 10 | 25 27 32 36 21 42 24
R03 | 603 11 16 16 23 15 31 8 | 27 35 31 36 31 28 27
XR04 | 867 13 12 22 --- --- 29 11 | 33 29 30 --- --- 36 26
R05 | 1744 19 21 19 16 11 30 8 | 29 28 44 41 36 36 32
R07 | 1137 9 10 14 11 13 23 6 | 39 37 35 34 40 50 37
R08 | 874 17 10 16 27 15 18 8 | 37 37 32 46 34 38 35
R09 | 3618 16 18 20 23 30 23 10 | 94 99 95 113 94 92 96
XR11 | 3596 --- --- 17 20 18 23 11 | --- --- 56 52 52 51 52
R12 | 1720 21 42 20 12 15 21 10 | 76 33 57 68 69 54 59
R13 | 2175 41 44 33 33 38 19 16 | 86 41 53 71 64 70 60
R14 | 1205 9 26 28 24 17 21 9 | 76 71 80 64 73 79 72
R15 | 1308 12 25 10 11 18 19 7 | 88 75 88 90 83 76 83
R17E | 821 16 31 13 18 16 24 8 | 44 29 37 43 48 45 39
R18E | 673 12 23 23 16 20 23 9 | 91 87 97 99 95 90 92
R19E | 1143 31 80 26 40 40 49 20 | 89 106 95 106 111 78 91
XR20E | 1364 45 78 43 63 --- 54 27 | 63 78 65 66 --- 61 53
R21E | 1019 19 28 14 15 20 38 10 | 50 36 49 57 57 51 47
R22E | 2787 71 65 35 81 55 51 27 | 61 99 97 102 105 114 85
R24E | 1193 15 36 9 28 17 23 9 | 139 132 140 141 140 131 136
------+-----------------------------------------+-------------------------------------
RMS | 1626 27 36 23 31 27 31 |T 64 60 63 69 67 65 60
WRMS | 1626 20 32 18 18 20 28 |NE 56 48 53 59 54 56 51
MEDI | 1193 16 26 19 23 17 23 |MD 63 41 56 64 61 54 53
Table 3.2206.3 GPS week: 2206 Day: 3 MJD: 59689
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 795 28 19 34 35 33 19 13 | 64 60 49 56 65 54 55
R02 | 1152 8 12 16 7 14 14 5 | 28 30 30 30 34 35 29
R03 | 561 9 12 10 12 10 15 5 | 30 30 35 37 32 39 31
XR04 | 818 22 19 15 --- 29 29 11 | 33 32 30 --- 31 35 25
R05 | 2162 12 26 26 25 13 34 10 | 22 29 44 45 32 33 27
R07 | 1547 10 18 9 15 21 21 7 | 40 39 46 52 55 38 43
R08 | 1020 17 14 16 18 19 22 8 | 41 39 45 38 34 49 39
R09 | 4143 14 19 15 20 30 47 11 | 70 69 76 63 58 104 70
XR11 | 3821 --- --- 13 12 24 19 10 | --- --- 59 60 45 65 57
R12 | 1928 14 40 12 15 15 27 9 | 72 35 63 73 70 60 63
R13 | 1598 33 62 45 45 40 29 18 | 106 50 62 108 100 75 81
R14 | 1039 12 28 25 21 23 24 9 | 101 94 119 106 107 112 106
R15 | 1590 9 34 10 20 15 18 8 | 74 49 69 82 70 60 68
R17E | 703 21 30 11 14 16 18 8 | 46 32 38 40 43 41 37
R18E | 626 8 23 18 9 17 19 7 | 54 36 59 55 54 51 51
R19E | 641 30 84 36 63 61 40 23 | 114 124 133 140 116 120 119
R20E | 1894 57 89 51 66 48 83 29 | 116 187 153 152 136 92 127
R21E | 832 20 29 16 22 31 38 11 | 41 24 34 44 53 37 33
R22E | 2084 45 42 64 101 66 52 28 | 43 55 78 74 79 78 52
R24E | 2483 12 52 16 21 35 18 11 | 68 64 67 70 76 65 65
------+-----------------------------------------+-------------------------------------
RMS | 1724 24 41 28 38 32 34 |T 61 56 64 69 64 62 58
WRMS | 1724 16 29 22 17 22 29 |NE 56 46 55 62 56 58 53
MEDI | 1152 14 28 16 20 23 22 |MD 54 39 59 60 55 54 52
Table 3.2206.4 GPS week: 2206 Day: 4 MJD: 59690
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 634 26 14 29 26 29 29 12 | 83 98 100 109 96 105 95
R02 | 1077 11 12 21 19 16 24 7 | 38 40 37 51 59 57 43
R03 | 993 11 15 13 15 12 13 6 | 33 42 45 31 38 35 35
XR04 | 526 11 9 13 --- 12 28 7 | 38 37 44 --- 28 27 33
R05 | 2478 17 24 18 22 11 31 9 | 28 34 44 45 35 46 33
R07 | 1420 7 9 13 13 22 18 6 | 46 47 61 55 36 49 48
R08 | 711 11 16 12 29 14 20 7 | 48 46 50 59 32 52 45
R09 | 3536 16 27 14 17 23 19 8 | 121 132 125 126 101 124 120
XR11 | 2681 --- --- 9 20 20 24 10 | --- --- 70 61 56 67 59
R12 | 1151 24 32 14 10 21 28 10 | 73 39 61 52 65 49 56
R13 | 1186 43 55 39 52 36 34 19 | 85 36 52 94 72 58 60
R14 | 682 13 33 22 20 18 30 10 | 83 65 95 90 80 85 82
R15 | 2076 8 38 10 16 17 38 10 | 93 68 94 91 102 111 92
R17E | 718 20 27 13 14 17 25 8 | 48 38 45 46 44 33 40
R18E | 809 11 21 19 24 16 16 8 | 50 44 59 51 52 51 50
R19E | 842 36 77 32 77 55 55 24 | 125 129 120 153 149 134 129
R20E | 1944 61 55 33 60 51 115 28 | 98 86 87 97 98 137 87
R21E | 658 25 23 14 9 21 27 9 | 41 30 33 33 40 34 32
R22E | 1868 43 46 81 80 75 36 28 | 75 67 103 72 72 71 67
R24E | 1093 12 38 12 22 24 16 9 | 80 82 83 83 89 78 81
------+-----------------------------------------+-------------------------------------
RMS | 1527 26 36 28 36 31 39 |T 67 61 70 73 67 70 64
WRMS | 1527 18 29 18 18 22 30 |NE 64 57 67 72 61 66 61
MEDI | 1077 16 27 14 20 20 27 |MD 73 46 61 61 59 57 56
Table 3.2206.5 GPS week: 2206 Day: 5 MJD: 59691
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1411 37 16 22 36 40 32 14 | 57 57 84 72 52 64 61
R02 | 1006 14 9 21 26 64 26 13 | 32 25 37 36 63 37 32
R03 | 470 13 20 9 16 19 21 7 | 28 22 32 39 40 37 31
XR04 | 525 9 11 12 --- 13 22 7 | 22 27 40 --- 24 26 26
R05 | 1723 16 15 16 13 13 33 8 | 18 27 34 28 32 31 20
R07 | 1378 9 9 11 14 17 15 5 | 25 27 27 35 30 29 26
R08 | 884 6 20 26 13 20 32 9 | 31 24 27 31 40 49 29
R09 | 2744 23 21 14 17 28 21 9 | 105 107 111 109 116 126 110
XR11 | 2632 --- 97 27 17 29 37 23 | --- 15 71 89 64 72 77
R12 | 1412 13 39 12 13 26 17 9 | 58 38 49 51 67 53 51
R13 | 1213 32 64 39 45 24 35 18 | 82 62 47 91 78 60 66
R14 | 832 11 28 20 17 17 31 9 | 90 87 92 80 87 102 89
R15 | 2213 11 40 13 14 25 42 11 | 71 52 73 72 80 100 73
R17E | 845 16 26 15 12 16 12 7 | 36 27 33 34 39 33 31
R18E | 712 12 25 18 14 39 34 10 | 44 42 46 48 63 45 44
R19E | 1439 50 101 33 65 68 44 26 | 68 90 70 91 73 73 67
R20E | 1053 38 69 47 47 45 38 21 | 57 49 61 66 57 52 49
R21E | 614 20 28 15 13 22 25 9 | 36 23 33 28 37 43 30
R22E | 1968 56 46 88 79 80 26 30 | 48 51 103 69 51 58 56
R24E | 775 13 39 11 20 20 28 10 | 95 102 91 90 98 95 93
------+-----------------------------------------+-------------------------------------
RMS | 1388 26 41 30 33 38 30 |T 52 47 58 61 59 59 53
WRMS | 1388 17 32 19 15 29 28 |NE 51 43 55 61 59 60 53
MEDI | 1053 14 26 16 17 24 28 |MD 48 38 47 66 57 52 49
Table 3.2206.6 GPS week: 2206 Day: 6 MJD: 59692
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1602 30 34 32 20 35 26 13 | 89 104 110 99 78 88 90
R02 | 1008 10 7 12 16 16 22 6 | 43 41 44 43 38 44 40
R03 | 646 12 11 12 15 11 16 6 | 41 42 44 46 42 45 41
XR04 | 989 14 18 27 --- 26 19 10 | 38 40 39 --- 30 34 33
R05 | 917 18 21 18 21 13 32 9 | 29 39 33 33 33 36 27
R07 | 1271 12 15 19 16 11 16 6 | 55 55 57 57 57 59 55
R08 | 1065 8 15 31 17 16 18 8 | 50 43 47 52 48 56 48
R09 | 4034 16 25 18 22 20 19 9 | 96 97 101 98 101 107 98
XR11 | 2852 --- --- 8 23 15 17 9 | --- --- 54 61 55 51 58
R12 | 1439 15 35 17 15 18 23 9 | 82 50 73 77 81 77 73
R13 | 1007 37 49 44 40 22 29 16 | 104 54 61 100 88 63 76
R14 | 992 10 24 18 12 18 16 7 | 84 73 89 82 92 94 86
R15 | 2006 15 27 9 10 15 26 8 | 101 73 92 92 97 88 90
R17E | 1329 18 28 12 16 22 21 8 | 52 32 45 52 46 47 44
R18E | 1495 19 25 26 24 20 34 11 | 60 51 64 54 59 52 55
R19E | 1844 42 90 34 72 58 34 24 | 82 100 82 113 95 91 83
R20E | 1099 48 68 65 56 42 35 23 | 81 68 83 91 80 69 70
R21E | 1200 17 34 18 23 17 16 9 | 51 24 37 51 50 42 41
R22E | 1428 52 80 88 85 65 26 30 | 53 79 124 75 69 81 70
R24E | 888 13 35 11 13 23 27 9 | 103 105 104 104 113 91 102
------+-----------------------------------------+-------------------------------------
RMS | 1578 25 41 33 34 29 25 |T 68 61 69 72 67 65 64
WRMS | 1578 17 34 21 16 24 23 |NE 67 59 64 70 64 64 62
MEDI | 1200 16 27 18 20 18 22 |MD 60 54 61 75 59 59 58
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