[IGSREPORT-28705] Wk 2210 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 6 05:48:32 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2210 (May 15, 2022 - May 21, 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 2.2210.
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:
igl2210[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2210 in the SP3 format.
igl22107.sum Combination Report for GPS Week 2210.
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 | 1.2 ns
1 | 1.4 ns
2 | 0.1 ns
3 | -2.2 ns
4 | 1.7 ns
5 | -7.6 ns
6 | 0.8 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 1.2210, 1a.2210).
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 2.2210.0-6)
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 3.2210.0-6).
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 2210 summary. (May 15, 2022 - May 21, 2022)
Table 1.2210.a GPS week : 2210 MJD: 59714.0-59720.0
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 1 0 -8 -13 11 .10 21 17 | 34391 543 3326 8696
| 0 1 1 15 17 23 .02 | 3469 2470
emx n/a| 0 2 0 55 12 -4 -.12 49 35 | -5536 671 3271 8425
| 2 2 4 21 37 40 .05 | 11898 1629
esx n/a| 1 0 0 44 6 -17 -.09 38 26 | 4264 1168 3271 11450
| 1 1 2 20 33 14 .03 | 11643 2245
gfz n/a| 0 0 0 -6 4 -4 -.02 30 17 | 0 486 3276 8310
| 0 1 1 23 23 21 .04 | 0 2710
grg n/a| 2 0 8 -26 22 4 .23 38 27 | -1135 519 3270 8082
| 0 1 5 20 22 70 .05 | 2819 2511
iac n/a| 0 -3 -9 -38 -5 28 -.16 32 29 | 1517 -258 3264 9157
| 1 1 3 56 54 54 .05 | 3310 1386
Table 1.2210.b GPS week : 2210 MJD: 59714.0-59720.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 13 15 15 13 15 17 14 |
R02 | 9 8 9 6 6 7 8 |
R03 | 5 7 9 9 6 8 5 |
R04 | 11 9 8 8 8 11 9 |
R05 | 7 8 8 14 10 11 9 |
R07 | 8 7 6 6 6 9 9 |
R08 | 8 8 6 7 8 9 8 |
R09 | 8 7 10 8 8 9 7 |
R11 | 11 9 10 9 8 10 9 |
R12 | 8 9 9 7 8 7 9 |
R13 | 20 17 19 15 18 17 21 |
R14 | 9 11 9 9 9 8 7 |
R15 | 10 10 8 7 9 8 8 |
R17 | 7 10 9 12 10 8 8 |
R18 | 9 9 8 9 11 11 9 |
R19 | 30 28 22 26 24 25 26 |
R20 | 25 28 28 28 29 26 29 |
R21 | 8 8 9 9 8 9 8 |
R22 | 33 34 42 32 32 31 29 |
R24 | 11 10 13 13 13 13 12 |
Table 1.2210.c GPS week : 2210 MJD: 59714.0-59720.0
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 2210 0 | 22 1 144 848 242 6954 81.5 1706 1706 | 1200 0
brd 2210 1 | 61 40 209 108 985 -2144 82.1 1915 1915 | 1374 0
brd 2210 2 | -84 -74 149 -798 2622 -1057 84.1 1846 1846 | 74 0
brd 2210 3 | -43 -18 118 830 77 1958 82.5 2083 2083 | -2238 0
brd 2210 4 | -25 -94 114 1977 -838 2765 84.3 2121 2121 | 1716 0
brd 2210 5 | 19 -64 77 -590 -1565 2672 84.2 1918 1918 | -7554 0
brd 2210 6 | 89 70 102 -2540 -276 8007 83.0 1837 1837 | 766 0
-------------+------------------------------------------------------------+----------------
brd 2210 mean| 5 -20 130 -23 178 2736 83.1 1918 1918 | -666 0
brd 2210 sdev| 60 61 42 1458 1348 3750 1.1 144 144 | 3312 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 2.2210.0 GPS week: 2210 Day: 0 MJD: 59714
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 2 0 -29 -10 17 .10 19 14 | 32141 1863 3432 8544
emx n/a| 0 2 7 35 34 -21 -.11 44 29 | -19245 1920 3419 8305
esx n/a| 2 2 3 44 49 -45 -.07 41 25 | -4959 2896 3444 11762
gfz n/a| 0 -1 0 10 2 -21 .00 32 17 | 0 2285 3478 7982
grg n/a| 1 -1 4 -58 40 99 .24 40 31 | -120 2211 3419 8232
iac n/a| 0 -4 -9 29 -96 -17 -.18 33 29 | 1838 955 3428 9089
Table 2.2210.1 GPS week: 2210 Day: 1 MJD: 59715
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 9 -16 -8 .09 23 17 | 35110 2310 3370 9095
emx n/a| 0 3 0 29 21 -8 -.12 50 32 | 4266 1570 3306 8851
esx n/a| 1 0 2 36 49 -24 -.11 40 27 | -5434 2273 3306 11977
gfz n/a| -1 1 0 17 -5 19 .01 28 17 | 0 2845 3254 8768
grg n/a| 3 0 11 -24 -23 95 .16 39 26 | 285 1963 3293 8578
iac n/a| 0 -2 -15 -78 -19 1 -.12 33 30 | 4231 -1415 3319 9687
Table 2.2210.2 GPS week: 2210 Day: 2 MJD: 59716
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -3 3 16 18 .08 22 17 | 36735 1422 3431 8821
emx n/a| -1 2 0 53 -58 16 -.06 48 36 | 12576 1383 3346 8547
esx n/a| 0 0 0 41 -3 -5 -.09 38 23 | 19716 1693 3361 11994
gfz n/a| 0 1 2 5 -37 -2 -.03 28 17 | 0 915 3301 8637
grg n/a| 2 0 10 -38 20 2 .23 53 25 | -867 1251 3396 8172
iac n/a| -3 -5 -8 -91 78 52 -.16 35 31 | 2372 718 3352 9323
Table 2.2210.3 GPS week: 2210 Day: 3 MJD: 59717
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 2 0 1 -1 -28 .10 20 18 | 36135 -4588 3303 8216
emx n/a| 0 -1 -4 63 -11 16 -.20 46 38 | -16656 -2645 3290 8076
esx n/a| 0 1 -2 72 0 -3 -.05 31 29 | 12677 -3232 3236 10510
gfz n/a| 0 1 0 0 24 -30 -.08 27 19 | 0 -5098 3262 7624
grg n/a| 2 0 14 -39 32 7 .24 33 22 | -131 -4745 3207 7340
iac n/a| 0 -1 -9 -77 -4 119 -.18 36 31 | 899 -2090 3218 8666
Table 2.2210.4 GPS week: 2210 Day: 4 MJD: 59718
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 -30 -35 44 .10 23 17 | 35227 2561 3329 8693
emx n/a| 0 3 1 91 12 2 -.11 49 40 | -11889 1497 3234 8328
esx n/a| 2 -2 -1 54 -31 -12 -.10 37 28 | 15907 3486 3242 10931
gfz n/a| 0 0 -1 -36 20 -9 -.06 29 20 | 0 2268 3272 8243
grg n/a| 1 0 2 -4 39 -75 .26 34 29 | 157 2511 3268 8004
iac n/a| 0 -3 -11 -49 25 67 -.11 33 30 | 2737 1675 3243 9166
Table 2.2210.5 GPS week: 2210 Day: 5 MJD: 59719
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 -7 -31 23 .14 22 20 | 27615 -217 3159 8511
emx n/a| 0 0 0 42 35 47 -.07 48 33 | -9734 -321 3101 8193
esx n/a| 1 0 -1 7 -29 -6 -.13 39 24 | -9112 194 3090 11451
gfz n/a| 0 1 -3 -44 31 -16 -.06 32 20 | 0 -369 3129 8051
grg n/a| 1 1 2 -18 13 -68 .29 36 30 | -7470 -279 3057 8095
iac n/a| 0 -4 -3 52 19 14 -.11 27 25 | -5504 -946 3082 8915
Table 2.2210.6 GPS week: 2210 Day: 6 MJD: 59720
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 1 -3 -7 -14 13 .08 19 13 | 37779 453 3262 8992
emx n/a| -5 3 -5 70 55 -82 -.19 56 34 | 1928 1297 3201 8679
esx n/a| 0 0 -3 57 12 -21 -.06 41 23 | 1055 872 3218 11529
gfz n/a| 0 0 0 0 0 27 .04 30 12 | 0 558 3237 8871
grg n/a| 1 -1 13 -1 34 -29 .18 31 25 | 201 723 3253 8156
iac n/a| 1 -1 -7 -55 -37 -36 -.24 31 28 | 4047 -703 3208 9255
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 3.2210.0 GPS week: 2210 Day: 0 MJD: 59714
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 675 19 18 34 36 42 19 13 | 85 73 64 77 69 75 72
R02 | 3083 9 14 17 17 15 40 8 | 61 55 66 66 61 53 59
R03 | 706 7 9 11 9 14 16 5 | 61 64 69 70 69 66 65
XR04 | 638 17 21 14 --- 21 38 11 | 58 59 48 --- 50 46 50
R05 | 908 13 18 15 14 11 25 7 | 39 50 51 53 50 44 44
R07 | 844 11 14 17 21 15 27 8 | 62 62 66 75 70 73 66
R08E | 667 12 21 15 11 12 30 7 | 56 53 67 67 71 70 62
R09E | 4249 13 15 11 22 22 22 8 | 63 61 62 67 61 63 61
XR11E | 3739 --- 16 21 14 28 25 10 | --- 48 50 53 52 46 48
R12E | 846 9 29 14 20 16 24 8 | 30 32 35 30 34 50 32
R13E | 743 22 31 32 58 68 53 19 | 49 56 45 64 97 78 54
R14E | 1912 11 22 29 14 21 26 9 | 37 39 34 32 43 49 35
R15 | 1332 14 29 15 29 13 30 9 | 45 41 40 48 46 44 41
R17 | 1144 9 31 13 11 18 16 7 | 54 32 44 53 54 58 49
R18 | 1060 11 37 21 11 16 24 8 | 43 26 53 48 48 50 42
R19 | 890 39 119 38 43 100 64 29 | 78 49 46 78 73 69 59
R20 | 1791 30 91 79 58 48 39 25 | 86 22 35 93 97 87 64
R21 | 1043 10 33 12 13 16 18 7 | 38 21 32 34 41 41 32
R22 | 2694 38 55 132 68 84 41 32 | 52 56 98 63 62 76 48
R24 | 635 14 44 22 17 13 34 10 | 60 36 53 65 70 72 57
------+-----------------------------------------+-------------------------------------
RMS | 1706 19 44 41 32 40 33 |T 55 46 52 59 60 60 52
WRMS | 1706 14 29 25 17 31 29 |NE 58 46 54 63 61 61 53
MEDI | 908 13 22 17 17 16 26 |MD 56 49 50 64 61 58 50
Table 3.2210.1 GPS week: 2210 Day: 1 MJD: 59715
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 533 30 22 25 43 31 39 15 | 64 56 57 72 49 68 58
R02 | 4038 5 13 22 14 23 22 7 | 43 34 55 46 37 40 41
R03 | 869 8 8 11 17 15 31 7 | 44 47 46 53 46 25 42
XR04 | 550 17 15 12 --- 14 27 9 | 42 43 34 --- 37 31 36
R05 | 983 18 23 18 11 18 16 7 | 28 38 36 33 37 32 28
R07 | 1563 9 14 18 16 12 23 7 | 41 43 41 46 40 33 38
R08E | 1140 13 20 19 13 22 25 8 | 38 44 46 43 56 31 39
R09E | 4142 12 13 12 17 17 20 6 | 48 48 47 50 43 49 46
XR11E | 4079 --- 14 14 12 23 22 8 | --- 39 35 35 39 40 35
R12E | 1609 10 33 14 16 21 26 8 | 23 25 26 19 32 33 22
R13E | 690 34 28 30 51 24 45 17 | 40 48 52 95 79 76 56
R14E | 1458 16 32 12 15 24 45 11 | 33 34 41 42 50 59 38
R15 | 2184 11 32 12 25 18 33 9 | 33 35 34 35 37 43 33
R17 | 640 9 33 23 13 16 36 9 | 31 26 22 30 30 48 28
R18 | 1226 15 38 16 17 15 16 8 | 35 20 26 33 37 30 27
R19 | 949 34 137 35 37 84 46 28 | 32 51 30 37 35 52 26
R20 | 1517 40 101 90 27 71 48 28 | 53 39 34 38 70 43 32
R21 | 991 9 30 16 11 15 27 8 | 26 20 26 26 29 36 24
R22 | 2948 50 69 120 67 95 39 34 | 46 57 65 48 63 53 43
R24 | 1422 13 45 25 19 23 15 10 | 37 36 54 46 53 40 41
------+-----------------------------------------+-------------------------------------
RMS | 1914 23 50 40 28 39 33 |T 38 39 40 43 44 43 36
WRMS | 1914 17 32 27 17 26 30 |NE 39 38 40 41 42 41 35
MEDI | 1226 13 28 18 17 21 27 |MD 38 39 36 42 39 40 36
Table 3.2210.2 GPS week: 2210 Day: 2 MJD: 59716
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 895 36 33 30 28 28 39 14 | 72 61 51 74 50 76 62
R02 | 2843 16 16 9 24 13 28 8 | 52 47 53 68 54 59 54
R03 | 665 14 15 16 12 17 40 9 | 52 55 64 67 60 68 58
XR04 | 770 13 8 11 --- 14 27 7 | 53 43 45 --- 57 45 47
R05 | 761 15 19 19 15 15 27 8 | 39 39 40 42 49 47 38
R07 | 1926 10 15 7 14 16 16 5 | 49 48 51 57 50 48 49
R08E | 658 6 11 7 7 12 25 5 | 43 40 45 43 46 35 41
R09E | 5483 14 18 17 16 28 35 9 | 33 29 36 33 33 51 32
XR11E | 4030 --- 10 9 17 23 34 10 | --- 31 32 40 50 28 34
R12E | 1540 14 30 23 18 13 19 8 | 31 33 43 34 33 31 30
R13E | 742 29 57 36 36 63 44 18 | 31 56 40 65 61 43 31
R14E | 828 15 28 10 16 27 25 8 | 28 35 32 36 44 42 31
R15 | 2311 11 30 13 14 20 21 7 | 29 30 28 25 33 31 26
R17 | 547 9 34 16 15 16 29 8 | 37 27 34 43 45 56 37
R18 | 854 15 34 14 10 17 24 8 | 45 23 41 33 39 31 34
R19 | 786 36 104 25 29 73 26 21 | 72 68 41 55 43 39 47
R20 | 927 45 106 87 41 58 29 28 | 66 52 38 58 68 42 40
R21 | 1424 13 29 19 13 19 31 9 | 31 26 26 29 31 31 25
R22 | 1564 39 78 111 76 182 79 42 | 53 76 79 73 66 98 56
R24 | 1129 12 52 20 32 21 38 13 | 44 32 45 54 44 58 42
------+-----------------------------------------+-------------------------------------
RMS | 1845 22 48 38 28 53 35 |T 45 42 43 48 47 47 40
WRMS | 1845 17 36 23 17 25 31 |NE 49 44 45 52 49 52 43
MEDI | 895 14 29 16 16 19 28 |MD 44 39 41 43 46 43 38
Table 3.2210.3 GPS week: 2210 Day: 3 MJD: 59717
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 888 25 28 38 18 25 26 12 | 76 65 58 78 86 63 68
R02 | 3093 8 12 12 12 15 19 5 | 53 55 53 63 58 63 56
R03 | 680 21 16 17 23 15 22 8 | 53 54 72 81 66 74 65
XR04 | 662 15 18 10 --- 16 24 8 | 50 49 41 --- 46 38 44
R05 | 821 28 22 13 14 60 26 13 | 44 43 40 49 67 64 44
R07 | 866 8 17 11 12 10 22 5 | 58 48 62 63 63 53 58
R08E | 967 16 19 12 17 12 17 7 | 44 47 58 64 63 51 53
R09E | 6422 13 16 12 14 12 37 8 | 26 32 28 27 26 41 26
XR11E | 3872 --- 20 17 15 21 12 8 | --- 28 31 39 44 31 33
R12E | 1923 10 31 11 14 10 23 7 | 29 34 30 28 29 32 27
R13E | 1041 22 52 32 31 28 41 14 | 50 52 66 60 51 63 50
R14E | 990 13 22 19 18 19 30 8 | 35 33 42 40 34 46 34
R15 | 2381 12 29 13 13 12 20 7 | 36 33 31 28 29 26 28
R17 | 726 12 42 12 27 17 53 11 | 40 30 33 48 45 42 35
R18 | 731 8 30 24 12 22 21 8 | 30 24 41 29 40 38 31
R19 | 815 33 122 33 52 68 64 26 | 62 52 42 80 52 56 49
XR20 | 1372 27 --- 100 31 49 40 28 | 78 --- 41 81 82 91 64
R21 | 1668 13 35 20 14 24 25 9 | 38 21 26 35 42 39 30
R22 | 1600 35 70 101 72 75 71 32 | 56 60 46 51 80 78 38
R24 | 896 23 64 17 21 21 34 13 | 33 37 33 41 36 48 30
------+-----------------------------------------+-------------------------------------
RMS | 2082 20 46 31 27 33 36 |T 46 41 43 51 51 51 43
WRMS | 2082 18 38 29 19 22 31 |NE 50 43 44 55 56 55 45
MEDI | 967 15 28 17 17 19 25 |MD 44 43 41 49 46 48 38
Table 3.2210.4 GPS week: 2210 Day: 4 MJD: 59718
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 545 38 33 34 23 39 35 15 | 71 61 62 58 43 52 55
R02 | 3265 11 19 13 10 11 20 6 | 48 43 55 52 52 47 49
R03 | 627 13 11 8 6 17 22 6 | 54 58 58 58 66 59 57
XR04 | 544 13 15 15 --- 13 24 8 | 52 56 59 --- 49 41 50
R05 | 692 22 13 26 21 21 26 10 | 36 52 66 63 37 49 49
R07 | 1836 10 17 11 11 9 23 6 | 58 51 54 64 62 62 58
R08E | 1814 8 20 7 11 10 39 8 | 48 40 42 46 50 68 47
R09E | 6633 13 18 11 17 21 27 8 | 25 31 31 29 30 45 28
XR11E | 3975 --- 14 12 10 22 15 7 | --- 25 24 23 30 28 23
R12E | 2139 15 26 17 14 15 23 8 | 26 25 25 28 31 41 26
R13E | 1063 34 59 26 57 28 36 18 | 43 46 42 62 47 44 37
R14E | 1014 13 21 17 14 25 25 8 | 30 32 35 33 35 39 29
R15 | 2076 16 28 17 16 18 23 8 | 33 34 38 34 31 37 31
R17 | 721 13 33 15 10 13 42 9 | 38 33 42 37 42 37 35
R18 | 714 11 43 20 21 31 30 11 | 36 23 37 50 53 37 37
R19 | 861 35 101 43 44 62 47 23 | 54 48 46 68 53 47 46
R20 | 997 30 95 101 44 51 53 28 | 73 46 33 86 90 104 66
R21 | 1566 13 34 18 10 22 15 8 | 39 21 29 36 41 36 32
R22 | 947 50 82 86 73 88 41 31 | 81 84 106 110 77 88 83
R24 | 1129 16 68 24 13 19 38 13 | 50 49 43 42 57 63 47
------+-----------------------------------------+-------------------------------------
RMS | 2120 23 49 37 29 34 33 |T 47 42 46 51 48 51 44
WRMS | 2120 17 40 28 20 29 30 |NE 51 47 52 58 53 54 49
MEDI | 1014 13 26 17 14 21 26 |MD 48 43 42 50 47 45 46
Table 3.2210.5 GPS week: 2210 Day: 5 MJD: 59719
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 698 40 33 59 34 22 21 16 | 51 45 44 43 49 33 37
R02 | 2120 10 20 12 9 16 21 6 | 41 33 36 41 51 45 40
R03 | 736 12 12 15 9 24 25 7 | 40 38 38 39 58 49 41
XR04 | 616 20 16 17 --- 13 34 11 | 43 43 37 --- 39 39 37
R05 | 725 21 26 28 29 18 25 11 | 29 45 53 52 26 31 33
R07 | 1295 13 13 20 9 14 32 8 | 45 43 44 42 45 57 44
R08E | 1291 13 25 11 23 20 30 9 | 37 33 38 53 36 56 41
R09E | 6210 19 16 13 24 17 21 8 | 56 51 52 55 47 47 50
XR11E | 3914 --- 16 15 11 19 32 10 | --- 37 40 40 35 42 35
R12E | 2210 9 30 15 14 11 19 7 | 32 36 28 30 27 39 29
R13E | 1173 31 48 35 49 30 29 16 | 64 63 75 84 61 65 65
R14E | 954 13 25 15 18 11 22 8 | 38 35 41 40 31 39 34
R15 | 661 16 27 20 12 17 13 7 | 37 34 40 36 32 37 34
R17 | 859 7 32 9 15 17 20 7 | 31 27 31 33 45 31 30
R18 | 910 18 38 31 16 15 22 10 | 24 28 37 29 37 26 23
R19 | 1431 19 128 49 47 56 41 25 | 42 52 41 51 45 48 35
R20 | 1768 29 92 89 51 56 42 26 | 58 56 34 76 65 57 52
R21 | 872 10 33 17 14 28 18 8 | 31 33 31 35 43 25 29
R22 | 913 53 37 90 77 104 37 31 | 43 70 50 47 44 73 40
R24 | 1514 13 63 23 12 23 30 12 | 41 25 34 32 52 43 36
------+-----------------------------------------+-------------------------------------
RMS | 1917 22 48 39 32 35 27 |T 41 41 41 45 43 44 38
WRMS | 1917 20 33 24 20 30 25 |NE 39 40 39 42 45 42 36
MEDI | 954 16 27 17 16 18 25 |MD 41 37 38 41 44 42 36
Table 3.2210.6 GPS week: 2210 Day: 6 MJD: 59720
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 702 22 26 46 27 38 25 14 | 89 76 59 81 79 64 74
R02 | 3350 9 24 23 16 14 19 7 | 62 47 57 71 75 69 63
R03 | 693 7 21 14 9 12 10 5 | 63 59 69 69 72 62 65
XR04 | 892 14 14 17 --- 10 31 9 | 60 55 49 --- 54 35 50
R05 | 754 17 18 24 18 11 27 8 | 40 53 57 54 43 42 44
R07 | 891 12 17 17 10 12 43 9 | 68 65 67 77 75 90 73
R08E | 842 13 21 16 11 16 28 7 | 63 52 59 71 71 78 65
R09E | 5468 13 17 12 17 17 21 7 | 65 61 65 66 66 77 66
XR11E | 3493 --- 15 11 15 20 21 8 | --- 46 50 52 49 44 48
R12E | 1885 10 27 16 11 15 35 8 | 29 30 32 32 37 48 31
R13E | 703 30 56 33 73 32 41 20 | 42 53 51 87 54 55 48
R14E | 974 10 19 19 16 15 16 7 | 30 33 42 37 34 40 33
R15 | 640 10 30 20 17 11 19 7 | 35 35 31 32 33 33 31
R17 | 677 11 35 9 10 14 28 7 | 39 20 34 40 43 47 37
R18 | 791 8 34 17 20 19 23 8 | 34 19 48 41 43 49 37
R19 | 985 26 150 45 40 41 52 25 | 77 40 39 82 72 74 59
R20 | 1781 36 127 104 49 49 31 29 | 113 91 58 114 116 95 90
R21 | 656 14 27 19 10 19 26 8 | 51 28 39 47 58 41 44
R22 | 2110 33 36 100 63 90 51 29 | 59 47 73 60 59 65 45
R24 | 1006 12 70 28 13 20 27 12 | 56 44 48 57 65 68 54
------+-----------------------------------------+-------------------------------------
RMS | 1836 19 56 41 30 31 31 |T 56 47 51 61 59 58 52
WRMS | 1836 13 34 23 12 25 28 |NE 60 48 52 63 63 59 54
MEDI | 891 13 26 19 16 16 27 |MD 59 47 50 60 58 55 48
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