[IGSREPORT-28727] Wk 2212 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 17 05:41:14 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2212 (May 29, 2022 - Jun 04, 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 2.2212.
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:
igl2212[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2212 in the SP3 format.
igl22127.sum Combination Report for GPS Week 2212.
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 | -9.0 ns
1 | -4.7 ns
2 | -0.3 ns
3 | 0.5 ns
4 | -8.0 ns
5 | 0.3 ns
6 | 0.1 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
----+--------+---------------
6 | GFZ | R22
6 | GRG | R22
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 1.2212, 1a.2212).
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 2.2212.0-6)
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 3.2212.0-6).
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 2212 summary. (May 29, 2022 - Jun 04, 2022)
Table 1.2212.a GPS week : 2212 MJD: 59728.0-59734.0
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 -2 -3 -36 7 .13 20 15 | 31552 -160 3374 8814
| 0 0 1 11 9 21 .03 | 4081 2449
emx n/a| -1 0 -9 37 4 -55 -.09 51 35 | -9058 177 3324 8487
| 2 1 3 22 28 30 .04 | 9227 1388
esx n/a| 0 1 0 29 33 -7 -.11 40 25 | -2816 293 3327 11502
| 1 1 2 22 19 38 .03 | 11136 2263
gfz n/a| 0 0 5 -26 6 13 -.07 28 18 | 0 -324 3357 8425
| 1 1 2 29 19 19 .03 | 0 2406
grg n/a| 2 0 4 -14 19 -3 .28 33 28 | -3051 -319 3313 8072
| 2 1 4 22 36 42 .05 | 3647 2318
iac n/a| 0 0 -4 7 8 23 -.20 28 25 | -958 -308 3323 9229
| 2 3 2 21 26 33 .03 | 4315 1209
Table 1.2212.b GPS week : 2212 MJD: 59728.0-59734.0
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 | 15 15 17 19 18 16 17 |
R02 | 7 6 8 7 6 7 6 |
R03 | 7 8 6 9 9 7 6 |
R04 | 8 14 14 13 10 9 8 |
R05 | 8 8 6 9 8 8 9 |
R07 | 7 7 9 7 6 8 6 |
R08 | 7 7 6 7 7 7 6 |
R09 | 9 9 9 9 9 8 8 |
R11 | 9 9 8 8 11 10 10 |
R12 | 7 10 10 9 7 7 8 |
R13 | 20 18 21 18 15 19 19 |
R14 | 8 8 8 9 9 8 7 |
R15 | 8 7 11 11 7 9 8 |
R17 | 9 8 7 7 10 10 8 |
R18 | 9 9 7 7 7 10 9 |
R19 | 24 25 27 27 27 28 25 |
R20 | 28 24 26 27 23 25 30 |
R21 | 9 10 7 8 9 10 8 |
R22 | 27 29 28 34 29 27 39 |
R24 | 11 11 11 13 11 10 9 |
Table 1.2212.c GPS week : 2212 MJD: 59728.0-59734.0
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 2212 0 | 52 -33 166 -1361 1388 8882 81.5 1779 1779 | -8981 0
brd 2212 1 | 95 18 219 1486 739 6265 82.7 1719 1719 | -4695 0
brd 2212 2 | -124 82 242 546 607 8167 84.7 1940 1940 | -341 0
brd 2212 3 | 111 -84 213 2259 -3192 5197 84.2 1901 1901 | 471 0
brd 2212 4 | -86 -82 37 660 -1414 7620 82.0 1959 1959 | -7987 0
brd 2212 5 | -26 1 197 -706 -1690 -597 82.8 1897 1897 | 318 0
brd 2212 6 | 7 -36 153 -1732 656 593 81.9 1656 1656 | 56 0
-------------+------------------------------------------------------------+----------------
brd 2212 mean| 4 -19 175 164 -414 5161 82.8 1835 1835 | -3022 0
brd 2212 sdev| 89 59 68 1483 1688 3745 1.2 117 117 | 4142 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 2.2212.0 GPS week: 2212 Day: 0 MJD: 59728
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 0 -39 22 .13 21 14 | 27878 -4047 3087 8329
emx n/a| -4 0 -4 75 34 -83 -.11 46 32 | -6543 -2068 3073 8057
esx n/a| 0 0 -1 42 47 -27 -.11 40 23 | 5429 -3412 3073 10671
gfz n/a| 2 -1 4 -70 13 18 -.00 25 16 | 0 -3610 3076 7805
grg n/a| -1 0 3 -15 -35 6 .33 36 30 | -7177 -3743 3072 7678
iac n/a| 0 5 -2 37 4 24 -.23 28 25 | -6672 -1085 3068 8719
Table 2.2212.1 GPS week: 2212 Day: 1 MJD: 59729
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 -1 -1 -24 13 .17 20 14 | 26646 3617 3355 8653
emx n/a| -4 0 -4 34 10 -46 -.01 43 31 | -5998 2025 3289 8508
esx n/a| 2 0 0 72 9 29 -.13 36 25 | -11213 3646 3302 11715
gfz n/a| 2 -2 1 -8 1 25 -.10 28 19 | 0 4128 3319 8435
grg n/a| 2 -1 2 -48 -20 -63 .29 36 24 | -6603 3480 3291 8022
iac n/a| -4 -1 -4 -24 56 24 -.21 28 25 | -4321 1961 3298 9149
Table 2.2212.2 GPS week: 2212 Day: 2 MJD: 59730
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 8 -25 23 .14 21 15 | 34850 -872 3402 9335
emx n/a| -1 3 -8 30 -26 -40 -.08 50 32 | 7415 -237 3357 8866
esx n/a| 0 0 1 20 39 -46 -.04 42 27 | -1557 -826 3368 12017
gfz n/a| 1 0 2 -24 -15 20 -.10 25 17 | 0 -883 3368 8843
grg n/a| 1 0 1 -17 12 47 .21 33 24 | -1 -975 3327 8371
iac n/a| 4 -2 -4 15 19 32 -.22 31 26 | 2662 -1503 3358 9727
Table 2.2212.3 GPS week: 2212 Day: 3 MJD: 59731
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 -6 -27 -46 34 .14 21 17 | 35279 1175 4131 9311
emx n/a| 0 -1 -13 7 43 -89 -.07 57 43 | -11797 972 4041 8887
esx n/a| 0 2 -2 15 50 -33 -.10 44 22 | -11219 1616 4061 12118
gfz n/a| 0 2 8 -38 -16 29 -.09 29 15 | 0 90 4131 8815
grg n/a| 3 -1 13 15 29 -37 .23 35 26 | -84 434 4053 8825
iac n/a| 0 3 -7 14 -24 12 -.17 31 29 | 2367 328 4056 9816
Table 2.2212.4 GPS week: 2212 Day: 4 MJD: 59732
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 -2 4 -44 -11 .10 19 15 | 27129 -1873 3086 9003
emx n/a| 3 0 -14 26 9 -15 -.10 56 36 | -22537 -969 3038 8581
esx n/a| -1 4 -2 30 54 -17 -.10 43 27 | -10266 -995 3043 12164
gfz n/a| -1 2 5 -52 2 -5 -.09 27 20 | 0 -2137 3080 8499
grg n/a| 4 1 7 3 48 52 .28 28 26 | -7056 -2305 3029 8357
iac n/a| 0 -1 -1 24 1 -7 -.22 26 25 | -5540 -1382 3028 9374
Table 2.2212.5 GPS week: 2212 Day: 5 MJD: 59733
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 -3 -28 -23 .10 19 13 | 34268 -153 3281 8794
emx n/a| 0 -1 -11 58 -5 -26 -.12 51 35 | -14942 361 3245 8561
esx n/a| -1 0 2 5 10 60 -.11 42 28 | 18144 815 3228 10784
gfz n/a| -1 0 5 14 26 27 -.06 32 19 | 0 202 3290 8605
grg n/a| 4 0 4 0 39 -17 .30 33 31 | -208 346 3222 7855
iac n/a| 0 2 -7 -16 19 -8 -.16 26 22 | 2151 -111 3236 9161
Table 2.2212.6 GPS week: 2212 Day: 6 MJD: 59734
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 -4 -45 -8 .16 18 15 | 34818 1028 3276 8279
emx n/a| -1 -1 -7 28 -32 -87 -.15 55 36 | -9004 1157 3228 7951
esx n/a| 1 0 -1 22 20 -14 -.14 35 23 | -9034 1207 3218 11047
gfz n/a| -1 1 8 -7 34 -22 -.08 29 18 | 0 -60 3236 7975
grg n/a| 4 1 2 -37 66 -9 .32 29 32 | -232 528 3203 7399
iac n/a| -2 -2 -6 3 -14 90 -.22 23 20 | 2642 -370 3223 8658
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 3.2212.0 GPS week: 2212 Day: 0 MJD: 59728
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 763 30 31 51 24 36 31 15 | 93 64 46 81 83 71 73
R02 | 2827 10 19 11 15 12 21 6 | 61 50 57 70 57 64 60
R03 | 680 8 17 14 14 13 28 7 | 68 62 74 79 72 62 69
XR04 | 547 14 14 11 --- 12 26 8 | 74 72 68 --- 64 72 69
R05M | 971 17 17 19 11 13 26 8 | 72 71 69 70 77 84 72
R07 | 986 8 12 15 13 25 22 7 | 62 54 61 71 60 66 62
R08 | 1081 9 15 12 11 21 21 6 | 64 60 66 77 79 78 70
R09E | 4932 14 22 12 14 21 32 8 | 47 47 51 51 45 64 49
XR11E | 2161 --- 17 13 16 15 26 9 | --- 40 34 34 41 45 36
R12E | 721 7 24 16 12 14 23 7 | 72 76 72 73 79 73 72
R13E | 1910 28 59 40 61 42 39 20 | 52 58 52 95 63 69 58
R14E | 942 13 27 20 16 12 19 8 | 57 57 50 58 62 66 57
R15E | 1474 12 28 15 22 18 16 8 | 55 56 62 67 72 60 60
R17 | 1435 7 40 14 19 20 19 9 | 54 38 48 56 52 60 51
R18M | 749 7 24 17 11 32 32 9 | 46 34 49 43 36 62 43
R19M | 739 30 115 50 39 52 33 23 | 84 24 45 86 76 80 67
R20 | 1975 34 96 109 27 59 50 28 | 99 85 68 104 103 101 87
R21 | 830 13 32 20 11 27 22 9 | 48 34 38 40 53 53 43
R22 | 2161 51 38 89 46 93 36 27 | 36 40 63 477 354 34 21
R24M | 902 21 54 12 23 17 20 11 | 62 40 52 68 71 65 59
------+-----------------------------------------+-------------------------------------
RMS | 1778 21 46 40 25 36 28 |T 63 53 56 89 79 66 58
WRMS | 1778 14 32 23 16 30 25 |NE 62 55 60 121 99 65 59
MEDI | 971 13 24 15 16 20 26 |MD 62 54 52 70 64 65 60
Table 3.2212.1 GPS week: 2212 Day: 1 MJD: 59729
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 1009 27 29 48 32 37 30 15 | 67 52 40 53 64 64 55
R02 | 1404 8 16 9 10 13 21 5 | 44 37 42 37 44 58 43
R03 | 621 8 11 14 21 15 32 8 | 47 41 50 57 48 26 43
XR04 | 511 23 24 10 --- 18 47 13 | 51 52 48 --- 42 62 46
R05M | 715 10 21 16 23 21 15 8 | 57 61 56 54 62 53 54
R07 | 1447 9 13 15 20 10 17 6 | 42 38 44 50 45 44 43
R08 | 659 11 19 14 15 19 17 6 | 46 43 52 52 56 58 49
R09E | 5108 15 19 14 15 25 30 8 | 53 53 61 59 53 69 55
XR11E | 2286 --- 13 9 12 24 25 9 | --- 43 46 48 47 54 46
R12E | 889 20 26 24 22 16 21 9 | 82 77 84 88 82 83 81
R13E | 1186 33 49 37 47 31 39 17 | 71 69 68 100 64 86 73
R14E | 900 12 22 15 15 20 23 7 | 65 62 76 77 79 82 72
R15E | 1128 9 27 16 21 12 10 7 | 66 61 64 79 81 67 69
R17 | 1200 11 33 13 15 15 16 7 | 27 25 25 29 29 30 23
R18M | 649 11 29 17 17 18 32 9 | 30 29 40 27 40 39 30
R19M | 715 32 111 39 31 77 49 25 | 58 46 35 41 75 55 42
R20 | 1200 26 79 81 55 47 25 23 | 48 48 48 68 43 39 41
R21 | 1053 14 32 16 12 19 33 9 | 29 22 24 27 30 33 24
R22 | 3112 46 51 94 55 95 33 28 | 52 46 43 269 207 50 38
R24M | 1338 11 44 16 15 26 35 11 | 34 34 34 30 47 47 31
------+-----------------------------------------+-------------------------------------
RMS | 1719 20 43 36 28 36 28 |T 51 46 49 65 61 54 47
WRMS | 1719 14 31 25 19 24 25 |NE 42 39 41 73 60 44 38
MEDI | 1053 12 26 16 20 19 25 |MD 51 46 46 53 48 54 43
Table 3.2212.2 GPS week: 2212 Day: 2 MJD: 59730
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 627 34 32 56 26 41 36 17 | 77 45 39 71 52 77 61
R02 | 866 9 24 13 20 11 28 8 | 49 41 49 66 55 61 53
R03 | 1331 8 11 15 10 13 21 6 | 58 55 67 62 62 55 59
XR04 | 547 22 22 11 --- 15 52 13 | 57 55 57 --- 44 43 47
R05M | 800 11 13 13 15 14 16 6 | 49 44 54 56 57 48 50
R07 | 745 8 21 15 25 24 20 8 | 50 39 47 60 58 60 52
R08 | 799 11 18 10 14 11 11 5 | 47 45 59 60 55 55 52
R09E | 5475 22 15 11 21 20 23 9 | 34 44 40 46 48 55 40
XR11E | 3366 --- 23 13 10 17 20 8 | --- 48 40 42 41 55 43
R12E | 803 14 40 17 16 26 22 9 | 126 122 126 129 138 134 127
R13E | 1215 48 48 40 41 51 47 20 | 104 101 120 115 124 106 107
R14E | 1443 11 23 19 16 18 21 7 | 58 53 60 59 65 60 57
R15E | 1264 7 28 18 14 22 48 10 | 107 98 111 107 104 108 105
R17 | 1505 8 30 12 13 12 21 7 | 32 30 34 33 37 40 32
R18M | 1515 16 23 13 12 13 22 7 | 61 56 67 66 60 76 63
R19M | 787 23 144 53 21 70 54 27 | 55 32 38 60 72 69 48
R20 | 1125 25 89 94 44 55 40 25 | 60 38 36 73 80 64 54
R21 | 1326 8 31 12 13 17 17 7 | 35 28 38 40 39 29 33
R22 | 4178 35 53 114 55 59 39 27 | 24 50 64 452 365 41 30
R24M | 1243 10 54 18 19 15 28 10 | 43 37 51 55 55 55 46
------+-----------------------------------------+-------------------------------------
RMS | 1940 21 50 42 25 33 31 |T 59 53 59 86 80 64 57
WRMS | 1940 15 32 27 17 24 26 |NE 45 42 50 105 88 49 45
MEDI | 1215 11 24 15 16 17 22 |MD 55 45 51 60 57 55 52
Table 3.2212.3 GPS week: 2212 Day: 3 MJD: 59731
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 864 40 43 53 47 35 28 18 | 81 42 33 83 51 62 59
R02 | 961 7 22 13 20 15 22 7 | 55 37 52 70 55 67 56
R03 | 1733 13 21 13 17 28 29 9 | 57 52 62 79 88 65 66
XR04 | 633 21 25 12 --- 11 49 13 | 51 48 43 --- 51 26 42
R05M | 1236 14 25 17 19 15 34 9 | 45 46 56 61 56 32 46
R07 | 943 7 16 15 15 17 23 6 | 50 45 49 58 73 58 54
R08 | 1152 9 15 16 9 14 30 7 | 50 44 47 56 62 70 53
R09E | 5836 17 18 19 18 12 32 9 | 25 32 43 35 33 45 31
XR11E | 3950 --- 18 9 13 19 18 7 | --- 23 27 33 34 28 27
R12E | 685 15 38 16 16 21 26 9 | 95 93 101 103 111 102 99
R13E | 1241 22 64 38 55 41 24 18 | 48 33 41 74 49 56 44
R14E | 2869 12 31 14 10 33 15 8 | 53 50 58 59 85 58 58
R15E | 1011 11 24 14 15 23 48 10 | 109 108 117 116 126 90 109
R17 | 970 12 31 16 8 12 18 7 | 46 28 34 42 46 46 40
R18M | 1474 11 30 17 11 17 17 7 | 101 108 110 106 102 103 104
R19M | 1029 31 153 38 26 75 45 26 | 59 47 34 55 49 73 47
R20 | 1011 36 97 98 34 60 48 27 | 76 33 43 55 77 78 54
R21 | 1142 11 31 13 15 15 22 7 | 35 25 30 24 36 38 29
R22 | 1906 41 85 127 75 72 37 33 | 34 50 57 383 333 32 23
R24M | 1085 10 74 21 12 26 27 12 | 68 42 63 69 76 74 65
------+-----------------------------------------+-------------------------------------
RMS | 1901 21 57 44 29 35 31 |T 59 49 55 82 79 60 55
WRMS | 1901 17 43 22 15 26 29 |NE 50 40 46 95 91 53 46
MEDI | 1085 13 30 16 16 19 27 |MD 53 44 47 61 56 58 53
Table 3.2212.4 GPS week: 2212 Day: 4 MJD: 59732
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 1328 34 38 71 34 22 32 17 | 67 32 27 60 45 72 49
R02 | 1370 5 24 11 18 11 14 6 | 48 32 50 63 45 55 49
R03 | 2061 17 23 12 22 11 31 8 | 52 42 57 75 55 78 59
XR04 | 1059 20 14 16 --- 12 29 10 | 55 48 49 --- 51 59 52
R05M | 1850 13 26 16 13 8 30 8 | 56 48 58 62 57 78 58
R07 | 1112 9 15 11 17 11 13 5 | 49 45 52 57 57 55 51
R08 | 2177 16 16 11 16 17 15 7 | 47 44 53 59 63 62 54
R09E | 5249 16 18 19 15 22 24 8 | 34 33 38 37 27 39 31
XR11E | 5045 --- 20 15 23 30 16 11 | --- 31 36 40 44 25 30
R12E | 749 9 28 12 12 15 19 6 | 75 65 75 78 78 76 74
R13E | 992 24 57 36 49 19 22 15 | 56 56 54 86 57 50 55
R14E | 2959 13 33 22 17 22 18 8 | 54 33 61 64 58 57 54
R15E | 1165 11 26 14 15 16 14 6 | 181 177 181 191 192 174 183
R17 | 1319 8 42 16 17 15 39 10 | 47 41 46 50 48 63 47
R18M | 1313 10 40 12 9 13 19 7 | 153 143 147 150 140 156 149
R19M | 1154 39 157 41 29 70 31 26 | 61 71 40 57 49 49 48
R20 | 1475 25 97 93 34 39 36 23 | 61 43 48 65 58 56 52
R21 | 1327 7 47 19 9 13 29 8 | 40 28 39 36 44 49 38
R22 | 1287 23 64 116 66 67 31 28 | 40 41 36 284 190 44 30
R24M | 1461 17 61 16 9 11 30 10 | 51 42 40 42 51 53 44
------+-----------------------------------------+-------------------------------------
RMS | 1958 19 56 43 27 28 26 |T 64 54 59 81 70 67 60
WRMS | 1958 15 36 27 20 26 25 |NE 48 40 47 86 67 57 48
MEDI | 1327 16 28 16 17 15 24 |MD 54 42 49 62 55 56 51
Table 3.2212.5 GPS week: 2212 Day: 5 MJD: 59733
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 484 33 45 61 29 27 15 16 | 54 44 41 50 62 52 47
R02 | 2578 11 21 13 16 13 19 6 | 52 40 38 51 49 41 45
R03 | 959 5 19 13 17 20 18 6 | 50 36 53 57 60 42 49
XR04 | 676 13 18 14 --- 21 19 8 | 45 37 47 --- 38 54 44
R05M | 1467 15 19 15 14 21 18 7 | 48 36 42 44 37 45 40
R07 | 704 8 20 13 21 12 28 7 | 40 31 42 46 46 40 39
R08 | 1630 12 21 10 11 16 21 6 | 40 34 45 48 50 58 45
R09E | 4445 12 17 12 18 23 20 7 | 32 36 37 38 44 40 35
XR11E | 4628 --- 21 13 21 28 16 10 | --- 31 34 41 32 31 31
R12E | 900 9 25 15 24 13 9 7 | 68 64 60 70 67 66 65
R13E | 630 15 49 51 67 35 38 18 | 45 38 37 90 52 73 50
R14E | 3806 12 35 20 15 20 11 8 | 40 25 46 42 48 37 38
R15E | 1967 8 30 12 23 28 25 9 | 229 230 224 218 222 239 227
R17 | 1182 7 43 18 13 16 31 9 | 30 25 22 33 38 41 30
R18M | 1010 7 43 17 18 27 24 9 | 177 179 168 171 191 177 176
R19M | 879 41 131 48 35 88 52 28 | 59 55 51 71 46 39 49
R20 | 1467 26 99 95 35 46 41 24 | 44 26 30 44 44 50 36
R21 | 716 12 47 25 16 15 23 9 | 29 24 24 36 32 36 28
R22 | 2312 33 38 101 84 59 27 27 | 43 59 66 926 786 41 44
R24M | 1046 14 52 19 17 20 11 9 | 41 40 36 43 43 34 37
------+-----------------------------------------+-------------------------------------
RMS | 1896 19 51 42 32 33 26 |T 61 54 57 111 99 61 57
WRMS | 1896 13 35 28 19 31 22 |NE 41 34 40 155 127 44 40
MEDI | 1046 12 30 15 18 21 20 |MD 45 36 42 48 46 41 44
Table 3.2212.6 GPS week: 2212 Day: 6 MJD: 59734
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 656 38 42 56 29 26 22 16 | 91 46 42 77 71 67 66
R02 | 3548 12 21 12 12 12 10 5 | 66 47 52 67 63 53 59
R03 | 750 6 18 13 7 20 12 5 | 65 55 63 72 75 58 64
XR04 | 774 13 14 12 --- 19 18 7 | 68 63 65 --- 54 56 61
R05M | 1319 14 28 22 22 19 23 9 | 61 59 61 67 58 65 60
R07 | 922 9 21 11 17 12 13 5 | 62 48 59 68 70 54 61
R08 | 1027 8 25 9 21 12 12 6 | 58 46 64 75 72 70 64
R09E | 3698 14 18 9 17 25 21 8 | 49 43 53 51 49 64 50
XR11E | 3689 --- 14 13 14 28 19 9 | --- 40 35 38 37 40 36
R12E | 934 13 34 11 21 16 17 7 | 74 68 75 85 78 82 76
R13E | 633 33 57 46 59 33 29 18 | 67 45 53 94 56 71 60
R14E | 2071 12 27 11 16 20 13 7 | 64 51 70 76 71 72 67
R15E | 1914 11 27 11 22 23 16 7 | 248 251 255 255 255 249 251
R17 | 807 8 42 14 13 9 23 7 | 63 41 57 63 67 71 61
R18M | 1094 8 39 14 13 19 30 9 | 229 227 237 231 228 231 230
R19M | 845 29 133 57 39 69 41 25 | 99 53 71 102 90 98 85
R20 | 1254 27 123 101 69 66 37 30 | 102 61 43 125 113 109 90
R21 | 840 8 37 16 12 11 23 7 | 51 36 43 45 50 60 48
XR22 | 9791 19 --- --- 3925 2959 56 38 | 49 --- --- 9999 9999 43 51
R24M | 1273 11 56 15 12 20 12 8 | 98 67 90 93 103 89 92
------+-----------------------------------------+-------------------------------------
RMS | 1655 18 55 35 29 29 23 |T 87 70 78 93 87 85 81
WRMS | 1655 15 36 23 18 32 20 |NE 64 49 55 73 70 63 62
MEDI | 1027 12 28 13 17 20 19 |MD 66 51 61 75 71 67 61
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