[IGSREPORT-28661] [Wk 2207 IGLOS Final Orbits]
acc
acc at igs.org
Mon May 16 07:47:14 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2207 (Apr 24, 2022 - Apr 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 2.2207.
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:
igl2207[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2207 in the SP3 format.
igl22077.sum Combination Report for GPS Week 2207.
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 | 0.9 ns
1 | 0.4 ns
2 | -0.5 ns
3 | -1.5 ns
4 | -0.0 ns
5 | 0.1 ns
6 | 1.4 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 1.2207, 1a.2207).
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 2.2207.0-6)
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 3.2207.0-6).
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 2207 summary. (Apr 24, 2022 - Apr 30, 2022)
Table 1.2207.a GPS week : 2207 MJD: 59693.0-59699.0
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 0 16 -23 18 .19 27 20 | 36952 61 3560 9145
| 0 0 2 11 18 19 .05 | 1833 2125
emx n/a| 0 1 13 12 7 17 .07 41 31 | -2907 567 3546 8995
| 2 1 2 18 22 38 .08 | 9589 1302
esx n/a| 0 0 3 11 10 -22 -.08 33 22 | -342 118 3518 10507
| 2 2 1 20 18 42 .06 | 10476 2039
gfz n/a| 1 0 1 -18 -1 -22 -.12 36 17 | 0 -264 3526 8766
| 1 2 1 15 10 23 .05 | 0 1780
grg n/a| 0 0 -6 -19 23 30 .24 29 23 | 81 -189 3514 8376
| 1 2 2 23 20 91 .08 | 298 1829
iac n/a| -1 -1 -4 18 -7 -3 -.28 26 24 | 2089 0 3517 9510
| 1 2 3 41 43 59 .14 | 666 1278
Table 1.2207.b GPS week : 2207 MJD: 59693.0-59699.0
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 15 13 16 13 15 12 |
R02 | 8 7 7 6 10 8 8 |
R03 | 9 7 8 5 9 9 7 |
R04 | 8 9 12 10 10 10 7 |
R05 | 9 8 10 9 10 10 10 |
R07 | 6 7 6 5 9 7 8 |
R08 | 8 7 9 8 9 6 10 |
R09 | 8 10 9 8 8 8 9 |
R11 | 13 11 11 9 10 15 9 |
R12 | 7 10 11 10 10 9 10 |
R13 | 15 13 14 17 20 16 14 |
R14 | 9 10 8 10 10 8 10 |
R15 | 9 9 8 9 10 10 11 |
R17 | 8 7 9 9 8 9 9 |
R18 | 9 12 9 8 10 9 12 |
R19 | 25 26 27 24 22 24 26 |
R20 | 24 25 21 26 26 24 22 |
R21 | 9 9 8 9 9 8 9 |
R22 | 30 27 30 29 33 34 34 |
R24 | 9 10 8 11 12 12 10 |
Table 1.2207.c GPS week : 2207 MJD: 59693.0-59699.0
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 2207 0 | 110 -67 172 -234 -749 9355 82.8 1493 1493 | 935 0
brd 2207 1 | 67 -37 113 -1140 973 12260 82.9 1571 1571 | 412 0
brd 2207 2 | 43 4 59 -2554 346 8709 82.5 1668 1668 | -521 0
brd 2207 3 | 4 -5 37 -865 1586 3869 82.4 1448 1448 | -1489 0
brd 2207 4 | 54 0 128 -215 1692 2653 81.2 1517 1517 | -13 0
brd 2207 5 | -45 91 162 1643 1832 4950 83.4 1787 1787 | 147 0
brd 2207 6 | -75 88 182 35 -175 4468 83.2 1779 1779 | 1445 0
-------------+------------------------------------------------------------+----------------
brd 2207 mean| 22 10 122 -475 786 6609 82.6 1608 1608 | 130 0
brd 2207 sdev| 65 59 56 1277 1005 3520 .7 137 137 | 959 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 2.2207.0 GPS week: 2207 Day: 0 MJD: 59693
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -4 16 -21 -8 .25 27 18 | 39750 1625 3879 8989
emx n/a| -1 1 11 6 -17 49 .17 37 33 | 140 1416 3866 8934
esx n/a| 0 0 1 -6 5 46 -.08 30 21 | -17606 1786 3802 10983
gfz n/a| 1 3 2 -40 -2 9 -.10 39 20 | 0 1435 3870 8685
grg n/a| 4 -5 -6 -12 53 -49 .34 28 22 | 166 1448 3832 8380
iac n/a| -1 -1 -1 42 -20 -22 -.43 26 22 | 2203 1548 3830 9490
Table 2.2207.1 GPS week: 2207 Day: 1 MJD: 59694
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 -3 3 -33 23 .22 29 20 | 38661 344 4066 9272
emx n/a| -3 -1 10 -9 28 37 .09 39 32 | -13879 642 4090 9267
esx n/a| 0 -1 0 12 -6 -15 .01 29 20 | 13083 -735 4039 9311
gfz n/a| 0 1 0 -8 7 -20 -.08 34 20 | 0 -496 4083 8946
grg n/a| 0 0 -3 -15 16 -65 .31 28 22 | 225 -243 4005 8537
iac n/a| 0 2 0 41 -25 61 -.49 25 23 | 2961 -497 4027 9709
Table 2.2207.2 GPS week: 2207 Day: 2 MJD: 59695
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 30 -4 12 .16 29 22 | 37961 -2691 3359 10299
emx n/a| 1 2 15 22 19 -6 .02 44 29 | -10451 -1216 3321 10193
esx n/a| 0 -3 5 13 24 -69 -.18 33 24 | -321 -2462 3389 12369
gfz n/a| 2 0 2 -23 1 -26 -.15 34 16 | 0 -2373 3446 9853
grg n/a| -1 1 -5 -46 11 15 .20 23 18 | 465 -2585 3414 9564
iac n/a| -1 -1 -4 61 -14 87 -.21 25 22 | 1676 -1516 3383 10744
Table 2.2207.3 GPS week: 2207 Day: 3 MJD: 59696
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 17 -12 43 .13 27 20 | 35795 -2968 3465 9001
emx n/a| -1 3 15 13 40 45 -.03 39 29 | 5850 -1329 3468 8937
esx n/a| 0 0 3 -11 5 17 -.05 31 20 | 12002 -2376 3402 7844
gfz n/a| 0 0 0 7 -4 -2 -.15 39 16 | 0 -2443 3436 9022
grg n/a| 0 0 -4 -22 21 -23 .23 26 18 | -295 -2364 3384 8178
iac n/a| 1 -2 -7 -29 -52 -73 -.23 27 23 | 1326 -1547 3403 9224
Table 2.2207.4 GPS week: 2207 Day: 4 MJD: 59697
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 34 -10 40 .13 27 24 | 34848 1210 3645 9474
emx n/a| 1 3 13 -13 5 55 .03 37 30 | 9008 1722 3656 9265
esx n/a| 4 -2 2 51 5 -50 -.07 36 21 | -3607 1330 3587 11206
gfz n/a| 2 -3 0 -17 -9 -64 -.15 44 14 | 0 -192 3375 8874
grg n/a| -1 -2 -4 23 41 37 .32 32 25 | -335 780 3576 8306
iac n/a| -3 0 -7 -48 -47 -61 -.10 25 23 | 1289 714 3597 9629
Table 2.2207.5 GPS week: 2207 Day: 5 MJD: 59698
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 0 9 -22 14 .21 23 19 | 36036 304 3110 8293
emx n/a| 1 1 14 35 -6 -30 .17 43 33 | -13664 1194 3070 8018
esx n/a| -1 0 5 4 -8 -32 -.08 36 23 | -1667 530 3066 10905
gfz n/a| 2 -1 1 -20 -16 -30 -.20 34 17 | 0 -141 3086 7656
grg n/a| 0 -2 -8 -22 31 116 .19 28 23 | 288 -589 3043 7532
iac n/a| -1 0 -1 16 56 -13 -.25 30 28 | 2521 -105 3050 8685
Table 2.2207.6 GPS week: 2207 Day: 6 MJD: 59699
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 7 -60 0 .19 28 19 | 35615 2603 3401 8691
emx n/a| -1 2 14 30 -17 -32 .07 45 29 | 2645 1542 3356 8351
esx n/a| 2 4 3 16 44 -56 -.10 34 24 | -4281 2753 3347 10933
gfz n/a| 0 -2 1 -28 15 -21 -.04 29 17 | 0 2356 3389 8328
grg n/a| -1 1 -9 -43 -7 184 .11 36 29 | 58 2227 3345 8135
iac n/a| -3 -5 -7 42 49 -2 -.22 25 24 | 2647 1399 3335 9094
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 3.2207.0 GPS week: 2207 Day: 0 MJD: 59693
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1031 34 63 36 13 41 24 16 | 26 67 55 35 38 27 32
R02 | 1362 12 8 13 26 11 28 8 | 26 31 24 27 23 37 24
R03 | 631 13 21 20 20 19 24 8 | 37 35 47 40 49 38 38
XR04 | 1597 10 9 16 --- 19 18 7 | 33 34 30 --- 28 39 30
R05 | 700 13 16 28 15 19 26 9 | 28 32 53 42 39 36 34
R07 | 900 8 14 15 14 10 12 5 | 41 36 47 47 41 50 42
R08 | 784 12 13 19 17 22 24 8 | 28 25 29 35 35 33 26
R09 | 4042 14 16 17 15 17 24 8 | 71 79 76 75 76 84 75
XR11 | 2612 --- --- 8 25 21 26 12 | --- --- 40 34 42 36 35
R12 | 1868 11 27 16 11 10 17 7 | 82 66 83 78 79 70 75
R13 | 1062 25 42 39 32 27 31 14 | 69 48 49 65 61 57 54
R14 | 671 11 22 23 14 20 25 9 | 58 50 73 64 59 64 59
R15 | 854 13 33 9 24 20 18 8 | 73 62 69 80 76 65 69
R17E | 1875 17 29 12 17 21 13 8 | 86 57 73 79 77 67 73
R18E | 1393 16 30 23 20 22 14 9 | 76 58 80 67 78 74 71
R19E | 1734 25 73 35 106 38 39 24 | 65 33 66 126 72 68 65
R20E | 954 72 50 53 49 36 41 23 | 110 39 55 96 83 68 68
R21E | 1438 24 34 10 17 14 16 9 | 112 90 93 103 104 102 100
R22E | 764 58 60 73 90 67 39 29 | 64 94 138 62 95 109 88
R24E | 841 14 33 12 16 21 15 8 | 84 58 79 88 76 80 77
------+-----------------------------------------+-------------------------------------
RMS | 1493 27 37 30 39 28 25 |T 61 52 62 65 61 60 56
WRMS | 1493 18 33 21 20 22 22 |NE 47 47 51 51 49 48 45
MEDI | 1031 14 29 17 17 20 24 |MD 65 50 55 65 61 64 59
Table 3.2207.1 GPS week: 2207 Day: 1 MJD: 59694
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 638 31 30 46 24 31 30 15 | 23 29 56 35 29 34 28
R02 | 3583 16 14 11 21 17 15 7 | 24 23 20 21 18 26 17
R03 | 938 7 13 14 8 21 22 7 | 25 23 27 20 25 22 20
XR04 | 1611 16 6 24 --- 7 22 8 | 18 18 27 --- 21 35 18
R05 | 754 27 16 16 11 12 13 7 | 21 20 32 24 22 32 19
R07 | 630 12 11 15 11 14 23 7 | 23 28 27 24 28 41 26
R08 | 920 12 13 13 17 9 22 6 | 19 25 32 33 20 36 22
R09 | 3059 15 16 13 25 25 31 10 | 54 57 54 61 55 53 52
XR11 | 3049 --- --- 15 13 23 21 10 | --- --- 35 38 33 28 29
R12 | 1905 19 35 14 22 22 20 9 | 79 60 76 84 72 68 72
R13 | 911 36 38 23 28 22 28 13 | 60 47 44 50 50 52 45
R14 | 924 12 26 26 20 15 27 9 | 48 37 63 54 52 57 50
R15 | 877 11 33 12 18 16 22 8 | 60 47 53 58 56 60 54
R17E | 1428 19 27 10 12 12 14 7 | 49 35 44 39 44 37 40
R18E | 909 10 39 24 18 32 27 11 | 60 45 61 57 61 65 56
R19E | 1438 37 82 36 91 53 45 26 | 36 44 63 82 62 39 44
R20E | 1868 65 64 72 62 34 20 25 | 62 40 52 62 51 42 39
R21E | 1528 18 34 14 13 15 21 8 | 81 70 69 78 81 83 76
R22E | 915 66 73 53 64 69 32 26 | 63 90 72 81 77 68 68
R24E | 1200 21 33 10 21 21 20 9 | 46 35 41 48 41 44 40
------+-----------------------------------------+-------------------------------------
RMS | 1571 29 39 29 34 28 25 |T 44 40 47 49 44 46 40
WRMS | 1571 20 32 20 20 22 23 |NE 37 34 42 41 37 41 34
MEDI | 938 18 30 15 20 21 22 |MD 48 37 44 50 44 41 40
Table 3.2207.2 GPS week: 2207 Day: 2 MJD: 59695
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 851 26 23 43 29 26 17 12 | 40 34 56 40 32 29 34
R02 | 4439 16 22 13 11 12 17 6 | 17 21 30 24 26 30 20
R03 | 776 16 15 23 23 9 21 8 | 26 23 40 28 35 38 28
XR04 | 1849 22 15 14 --- 9 39 11 | 28 30 32 --- 28 47 26
R05 | 896 30 24 28 27 10 18 10 | 23 21 56 53 31 38 31
R07 | 1694 9 11 20 13 10 16 6 | 32 34 40 36 30 38 32
R08 | 1134 14 14 12 13 15 35 9 | 22 28 30 29 21 44 25
R09 | 2636 16 25 13 20 17 23 8 | 43 47 51 61 55 60 50
XR11 | 3002 --- --- 20 15 14 25 11 | --- --- 29 26 26 43 27
R12 | 1339 32 36 20 13 22 21 11 | 79 68 70 58 60 52 61
R13 | 779 48 35 28 24 19 32 14 | 51 32 35 31 39 43 29
R14 | 1695 14 22 20 11 19 16 7 | 63 53 66 55 66 51 58
R15 | 716 6 38 11 10 16 23 8 | 69 57 77 66 74 73 70
R17E | 802 15 33 15 30 16 17 9 | 66 46 48 74 52 56 56
R18E | 496 14 32 22 13 19 20 9 | 56 56 66 62 66 64 60
R19E | 841 34 111 51 85 43 40 27 | 54 49 56 106 65 65 58
R20E | 2478 59 63 66 39 24 24 20 | 82 41 33 66 66 60 56
R21E | 1442 19 30 15 15 11 15 7 | 77 63 60 70 73 74 69
R22E | 721 56 88 79 86 54 45 30 | 59 118 120 78 82 82 79
R24E | 995 16 40 12 16 11 16 8 | 65 44 56 62 59 65 59
------+-----------------------------------------+-------------------------------------
RMS | 1667 29 44 33 34 23 25 |T 50 45 52 53 49 52 46
WRMS | 1667 22 29 24 16 18 22 |NE 41 37 47 42 40 45 37
MEDI | 995 16 30 20 16 16 21 |MD 54 44 51 58 52 51 50
Table 3.2207.3 GPS week: 2207 Day: 3 MJD: 59696
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1255 20 17 47 44 40 29 15 | 20 24 44 36 33 30 19
R02 | 3364 9 12 9 23 13 16 6 | 13 19 22 25 17 29 16
R03 | 611 9 13 9 13 11 13 5 | 23 23 23 24 28 18 21
XR04 | 1171 25 20 18 --- 14 20 10 | 25 27 24 --- 19 29 20
R05 | 1066 18 14 23 26 8 21 8 | 21 24 45 44 30 36 28
R07 | 1423 5 11 7 9 11 17 4 | 25 31 27 24 25 18 22
R08 | 872 19 12 22 13 13 22 8 | 21 22 26 27 17 31 19
R09 | 3048 13 17 11 21 21 24 8 | 22 35 35 45 26 38 29
XR11 | 2583 --- --- 9 21 13 20 9 | --- --- 23 27 13 29 18
R12 | 1337 22 38 19 12 21 18 10 | 64 38 51 52 59 52 50
R13 | 1066 36 54 26 48 36 32 17 | 58 39 46 75 57 44 43
R14 | 1080 14 27 26 10 22 22 9 | 39 20 41 34 48 22 31
R15 | 760 12 32 12 17 21 26 9 | 42 37 47 48 52 57 44
R17E | 574 17 35 18 26 13 15 9 | 62 35 49 68 50 61 53
R18E | 1078 14 20 26 11 13 23 8 | 44 39 53 45 48 36 42
R19E | 1033 44 85 41 63 47 35 23 | 52 45 55 77 52 67 45
R20E | 1092 53 81 67 62 34 50 25 | 93 78 43 92 88 50 64
R21E | 1031 15 30 14 22 13 24 8 | 76 55 66 79 76 72 70
R22E | 1165 66 36 68 103 49 48 28 | 46 66 105 70 74 115 72
R24E | 656 18 44 17 31 11 19 10 | 66 42 52 79 61 68 60
------+-----------------------------------------+-------------------------------------
RMS | 1448 27 39 31 39 26 27 |T 42 36 43 51 43 45 38
WRMS | 1448 20 29 20 16 18 23 |NE 31 28 34 38 32 33 27
MEDI | 1078 18 27 18 22 13 22 |MD 42 35 44 45 48 36 31
Table 3.2207.4 GPS week: 2207 Day: 4 MJD: 59697
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 2857 20 23 43 29 32 15 12 | 25 30 31 37 35 22 24
R02 | 1240 14 11 20 12 24 34 9 | 19 19 17 25 21 45 19
R03 | 547 16 14 16 11 29 22 8 | 15 18 21 24 33 24 19
XR04 | 661 10 14 27 --- 20 20 9 | 17 20 25 --- 19 28 17
R05 | 1184 18 23 26 27 18 20 9 | 20 23 47 50 21 32 25
R07 | 727 16 14 12 14 20 29 8 | 24 22 29 25 29 41 26
R08 | 1334 14 8 21 24 22 22 8 | 18 19 20 16 22 32 15
R09 | 3662 12 12 18 15 27 16 7 | 49 54 55 55 64 60 53
XR11 | 2051 --- --- 7 20 19 18 9 | --- --- 25 30 27 32 25
R12 | 1378 20 31 15 17 24 15 9 | 76 63 65 72 66 66 66
R13 | 702 31 63 52 66 22 24 20 | 63 38 37 82 51 53 41
R14 | 1191 15 20 30 17 22 24 9 | 61 52 66 55 67 43 54
R15 | 901 8 40 16 21 17 17 9 | 70 53 66 74 78 69 67
R17E | 906 19 32 11 10 11 16 8 | 51 33 41 44 48 48 43
R18E | 1381 16 21 19 11 20 31 9 | 60 56 63 60 63 72 60
R19E | 923 39 74 38 58 63 21 22 | 47 38 42 57 49 49 37
R20E | 679 55 67 76 62 42 44 26 | 72 67 69 81 67 56 57
R21E | 1594 22 29 15 15 23 17 9 | 65 47 53 66 69 51 56
R22E | 1229 54 41 86 133 69 34 32 | 36 56 88 73 76 73 52
R24E | 1251 26 39 15 27 17 22 11 | 52 30 41 53 48 33 40
------+-----------------------------------------+-------------------------------------
RMS | 1517 26 37 36 44 32 25 |T 44 38 45 51 47 46 39
WRMS | 1517 24 30 21 14 25 23 |NE 38 34 38 45 41 42 34
MEDI | 1191 18 23 19 20 22 21 |MD 49 38 41 55 48 45 40
Table 3.2207.5 GPS week: 2207 Day: 5 MJD: 59698
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 3004 30 17 36 30 34 39 14 | 23 23 36 43 22 36 21
R02 | 1483 8 9 25 13 15 31 8 | 21 23 25 19 16 37 18
R03 | 545 14 18 14 11 23 34 9 | 25 25 18 18 33 32 21
XR04 | 462 12 16 15 --- 26 24 9 | 20 24 22 --- 28 34 20
R05 | 1298 23 21 27 20 14 28 10 | 22 24 49 44 41 32 30
R07 | 1130 12 13 11 20 16 23 7 | 17 18 30 27 23 29 20
R08 | 1006 7 16 11 20 10 11 5 | 19 19 20 23 17 18 16
R09 | 4035 14 22 12 19 24 19 8 | 67 71 73 78 67 72 69
XR11 | 1845 --- 61 23 15 20 17 14 | --- 28 38 36 36 37 34
R12 | 1826 18 33 12 13 22 22 9 | 55 44 49 49 56 56 50
R13 | 797 31 46 46 42 22 26 16 | 60 49 45 66 58 51 49
R14 | 1165 9 22 24 13 14 23 8 | 56 47 74 59 56 64 58
R15 | 1546 18 47 13 11 19 18 9 | 80 58 74 73 68 73 70
R17E | 783 17 35 12 14 19 26 9 | 48 31 38 44 52 39 42
R18E | 936 15 28 13 14 13 30 8 | 49 50 48 48 56 62 50
R19E | 2475 32 102 32 61 52 36 24 | 51 49 46 70 59 53 49
R20E | 939 44 84 64 49 35 36 23 | 53 44 41 65 63 48 45
R21E | 2037 13 30 16 15 15 20 8 | 58 47 51 55 62 60 54
R22E | 879 43 65 108 95 69 50 33 | 37 65 97 60 52 51 42
R24E | 2128 18 40 20 21 19 40 12 | 48 38 43 51 49 45 42
------+-----------------------------------------+-------------------------------------
RMS | 1786 23 43 36 34 28 30 |T 42 38 45 48 45 46 40
WRMS | 1786 19 33 23 17 23 28 |NE 38 34 42 44 40 43 36
MEDI | 1165 17 28 16 19 19 26 |MD 48 38 43 49 52 45 42
Table 3.2207.6 GPS week: 2207 Day: 6 MJD: 59699
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 2001 34 21 25 25 26 21 12 | 26 24 47 43 29 29 27
R02 | 2078 14 12 7 15 15 28 7 | 20 25 29 30 24 38 25
R03 | 1253 10 14 14 14 16 23 7 | 24 23 24 26 32 26 22
XR04 | 622 9 14 9 --- 17 20 7 | 22 26 23 --- 26 24 20
R05 | 1158 18 21 25 19 21 21 9 | 21 25 52 47 42 32 32
R07 | 1537 10 12 23 12 18 20 7 | 31 30 36 35 25 31 29
R08 | 540 8 14 28 23 19 32 10 | 21 21 32 36 20 32 20
R09 | 3787 22 24 12 17 24 23 9 | 98 101 103 104 102 96 99
XR11 | 2563 --- 25 19 8 16 20 9 | --- 21 33 32 31 38 32
R12 | 1464 13 29 17 20 38 22 10 | 82 72 76 81 68 69 73
R13 | 700 31 47 33 24 26 27 14 | 73 49 43 66 60 51 52
R14 | 1063 11 21 25 22 29 26 10 | 79 63 92 78 75 75 76
R15 | 1861 16 39 18 23 40 16 11 | 94 77 94 102 101 89 91
R17E | 561 17 30 11 14 14 25 8 | 66 45 57 58 61 61 57
R18E | 1116 21 27 30 19 46 19 12 | 67 56 65 54 79 57 59
R19E | 2170 38 121 24 50 73 38 26 | 49 41 48 100 75 53 52
R20E | 1692 36 77 68 37 34 31 21 | 93 35 27 90 87 70 61
R21E | 2068 18 34 17 12 12 18 8 | 85 62 67 79 81 83 76
R22E | 1432 80 61 94 78 86 34 33 | 45 83 141 61 90 86 73
R24E | 2461 11 43 9 21 21 21 9 | 74 57 68 83 81 71 71
------+-----------------------------------------+-------------------------------------
RMS | 1779 28 45 34 29 36 25 |T 56 46 57 63 59 55 52
WRMS | 1779 19 29 24 17 29 24 |NE 49 42 52 56 48 48 46
MEDI | 1464 17 25 19 20 21 22 |MD 66 41 48 61 61 53 52
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