[IGSREPORT-28490] Wk 2195 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 18 02:33:20 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2195 (Jan 30, 2022 - Feb 05, 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 2.2195.
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:
igl2195[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2195 in the SP3 format.
igl21957.sum Combination Report for GPS Week 2195.
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 | 0.6 ns
1 | -0.6 ns
2 | -2.6 ns
3 | -1.8 ns
4 | -3.9 ns
5 | -2.5 ns
6 | -2.1 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 1.2195, 1a.2195).
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 2.2195.0-6)
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 3.2195.0-6).
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 2195 summary. (Jan 30, 2022 - Feb 05, 2022)
Table 1.2195.a GPS week : 2195 MJD: 59609.0-59615.0
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 -4 -13 59 .16 24 19 | 14806 -46 2854 7995
| 0 1 1 17 12 19 .04 | 945 1896
emx n/a| 0 1 0 23 17 -19 -.10 45 34 | -5829 582 2850 8109
| 1 1 1 29 37 59 .09 | 10335 1269
esx n/a| 0 1 0 14 -22 -21 -.14 39 32 | 7015 -734 2860 8733
| 0 1 2 32 14 15 .05 | 7037 1659
gfz n/a| 0 0 4 -4 -11 -29 -.05 27 17 | 0 249 2847 7751
| 1 1 1 22 17 24 .05 | 0 1825
grg n/a| 1 -3 -7 -26 19 10 .29 34 26 | -2044 232 2855 7510
| 1 0 3 21 25 51 .05 | 738 1711
iac n/a| 0 1 -3 13 36 -12 -.26 34 32 | 14 -153 2850 8558
| 2 2 2 36 27 116 .13 | 1303 1142
mcc n/a| 1 1 -6 4 -37 585 -.76 145 145 | --- --- --- ---
| 2 4 17 89 69 804 .40 | --- ---
Table 1.2195.b GPS week : 2195 MJD: 59609.0-59615.0
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 26 24 19 16 21 21 |
R02 | 7 9 9 9 8 9 7 |
R03 | 9 10 10 9 9 8 7 |
R04 | 13 10 12 10 8 8 9 |
R05 | 10 10 8 10 10 8 10 |
R07 | 8 8 10 9 8 7 7 |
R08 | 9 8 10 9 9 10 8 |
R09 | 8 9 11 10 7 8 8 |
R11 | 14 9 9 8 9 11 10 |
R12 | 12 10 8 8 7 9 8 |
R13 | 15 18 13 13 17 14 13 |
R14 | 7 6 9 7 7 8 7 |
R15 | 8 7 7 6 7 7 8 |
R17 | 11 11 11 9 11 9 7 |
R18 | 9 9 10 9 10 11 11 |
R19 | 24 26 27 25 23 23 18 |
R20 | 26 29 32 29 33 29 29 |
R21 | 12 13 9 10 14 13 7 |
R22 | 27 22 19 27 30 32 22 |
R24 | 15 15 16 15 14 13 14 |
Table 1.2195.c GPS week : 2195 MJD: 59609.0-59615.0
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 2195 0 | 42 46 -145 -1909 476 -13450 81.6 1241 1241 | 635 0
brd 2195 1 | -13 74 -78 -1634 -417 -6588 81.3 1123 1123 | -565 0
brd 2195 2 | -35 -43 -23 -2594 -320 -8661 82.5 1104 1104 | -2648 0
brd 2195 3 | 127 -43 112 -664 -102 -3298 81.4 1409 1409 | -1802 0
brd 2195 4 | -5 -6 83 1008 -263 8326 81.5 1813 1813 | -3912 0
brd 2195 5 | 30 25 169 -1645 76 -2205 78.8 1627 1627 | -2481 0
brd 2195 6 | -17 22 104 1456 1078 -7991 81.4 1570 1570 | -2090 0
-------------+------------------------------------------------------------+----------------
brd 2195 mean| 18 10 31 -854 75 -4838 81.2 1412 1412 | -1837 0
brd 2195 sdev| 55 44 115 1539 534 6884 1.1 270 270 | 1481 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 2.2195.0 GPS week: 2195 Day: 0 MJD: 59609
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 8 -7 70 .11 22 19 | 12915 2073 2638 7731
emx n/a| 0 -1 -2 46 91 45 -.01 47 37 | -1076 1850 2651 7802
esx n/a| -1 2 1 73 6 -37 -.11 40 37 | 5105 1066 2635 7247
gfz n/a| -1 2 4 -5 -15 -19 -.07 22 16 | 0 2131 2642 7287
grg n/a| 3 -3 -9 -52 0 -87 .24 28 23 | -579 2137 2647 7355
iac n/a| -2 4 -3 -13 -20 100 -.55 46 43 | 2145 -473 2641 8374
mcc n/a| -1 3 1 66 -57 -176 -.57 193 193 | --- --- --- ---
Table 2.2195.1 GPS week: 2195 Day: 1 MJD: 59610
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 -15 5 59 .15 24 18 | 14751 1963 2699 7533
emx n/a| 0 0 -1 45 19 3 -.08 41 32 | -14782 1441 2700 7524
esx n/a| -1 2 2 17 -15 -39 -.07 36 33 | 14597 1088 2723 9686
gfz n/a| -1 0 4 -34 -16 -48 -.01 29 21 | 0 2107 2714 7248
grg n/a| 1 -2 -4 -53 -13 3 .30 38 28 | -1804 1987 2711 6954
iac n/a| 3 -2 -10 84 57 35 -.23 37 34 | 1416 -55 2713 8156
mcc n/a| 3 -2 -20 123 40 1125 -.34 215 215 | --- --- --- ---
Table 2.2195.2 GPS week: 2195 Day: 2 MJD: 59611
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 7 -36 46 .14 27 18 | 15647 -2102 2649 7928
emx n/a| 3 4 0 -13 20 25 -.05 43 30 | 1380 -693 2640 7851
esx n/a| -1 2 1 2 -23 -13 -.17 35 30 | 11946 -2454 2648 9643
gfz n/a| -1 0 5 6 4 -55 -.06 29 14 | 0 -1171 2637 7386
grg n/a| 0 -4 -10 -33 12 4 .24 31 26 | -2157 -1100 2669 7181
iac n/a| -2 3 -3 21 45 -40 -.15 35 38 | -441 -1097 2643 8321
mcc n/a| 0 0 -38 24 -158 2133 -.73 82 82 | --- --- --- ---
Table 2.2195.3 GPS week: 2195 Day: 3 MJD: 59612
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 22 -10 64 .15 22 19 | 15308 1476 2844 9115
emx n/a| 0 0 0 0 25 -55 -.05 44 33 | -17086 2170 2831 9133
esx n/a| -1 2 -2 27 -35 -15 -.16 40 34 | 12506 334 2866 9580
gfz n/a| 0 1 3 -31 -41 -36 -.11 26 14 | 0 1908 2784 8968
grg n/a| 1 -2 -6 -3 18 26 .22 32 28 | -2561 1526 2856 8339
iac n/a| 4 0 -2 -25 62 9 -.23 36 32 | -531 956 2848 9643
mcc n/a| -3 5 0 -22 13 562 -.80 150 150 | --- --- --- ---
Table 2.2195.4 GPS week: 2195 Day: 4 MJD: 59613
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 -8 -12 86 .20 22 19 | 15619 -2131 2992 8693
emx n/a| -1 2 1 18 -24 -8 -.12 47 36 | -18061 58 2881 8987
esx n/a| 0 0 0 22 -34 -10 -.20 45 36 | 1507 -2646 2991 9176
gfz n/a| -2 2 7 -7 13 19 -.13 30 18 | 0 -2481 2944 8856
grg n/a| 0 -3 -13 -22 53 74 .29 39 25 | -2738 -2377 2969 8243
iac n/a| 0 -1 -3 -11 37 -238 -.16 31 27 | -798 -1985 2972 9215
mcc n/a| 3 7 12 -19 -50 20 -.61 114 114 | --- --- --- ---
Table 2.2195.5 GPS week: 2195 Day: 5 MJD: 59614
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 -28 -21 22 .21 25 17 | 14438 -86 3383 7695
emx n/a| 0 2 0 4 -4 -133 -.28 46 36 | 4068 359 3453 8038
esx n/a| 0 0 4 -26 -31 -35 -.18 42 31 | 8625 -358 3381 8171
gfz n/a| 0 0 3 25 -14 -33 -.01 28 22 | 0 -320 3422 7523
grg n/a| 1 -4 -5 -19 53 50 .34 37 25 | -2578 -36 3366 7379
iac n/a| -1 2 -1 16 28 99 -.27 32 28 | -1569 1275 3370 8303
mcc n/a| 3 -5 2 -163 24 341 -.69 114 114 | --- --- --- ---
Table 2.2195.6 GPS week: 2195 Day: 6 MJD: 59615
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 -14 -12 63 .18 24 21 | 14967 -1519 2774 7272
emx n/a| 0 1 1 65 -3 -12 -.13 49 36 | 4752 -1109 2796 7431
esx n/a| 0 1 -2 -11 -24 0 -.08 35 22 | -5176 -2170 2776 7631
gfz n/a| 0 0 4 16 -9 -29 .01 25 15 | 0 -427 2786 6995
grg n/a| 2 -3 -4 1 14 -1 .36 32 25 | -1891 -507 2770 7121
iac n/a| 0 0 -2 24 47 -55 -.24 22 21 | -118 303 2768 7896
mcc n/a| 4 1 -3 19 -72 94 -1.61 144 144 | --- --- --- ---
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 3.2195.0 GPS week: 2195 Day: 0 MJD: 59609
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 879 37 49 25 33 36 47 --- 16 | 112 100 96 109 119 109 --- 105
R02E | 1538 9 27 14 10 8 34 --- 7 | 42 43 44 42 42 46 --- 41
R03E | 813 13 32 12 13 14 41 --- 8 | 52 52 55 52 53 56 --- 51
XR04E | 864 10 35 10 --- 22 56 133 12 | 35 42 32 --- 32 59 77 34
R05E | 1407 14 38 14 11 14 47 112 9 | 58 55 48 49 51 56 56 51
R07E | 1405 11 29 13 14 14 30 --- 7 | 65 55 65 66 67 68 --- 63
R08E | 1444 8 32 10 17 19 32 --- 8 | 34 37 30 33 34 51 --- 32
R09 | 1826 19 18 10 16 11 34 --- 8 | 28 38 32 46 41 49 --- 34
XR11 | 2397 19 --- 37 16 33 41 --- 14 | 37 --- 46 44 42 59 --- 37
R12 | 696 16 27 31 12 8 66 282 11 | 61 53 53 52 52 75 166 52
R13 | 1002 24 33 27 40 34 47 --- 15 | 63 63 58 62 54 55 --- 56
R14 | 550 8 18 14 12 17 31 --- 7 | 50 42 52 45 39 63 --- 44
R15 | 850 15 18 15 12 12 41 246 8 | 58 57 48 51 47 71 144 52
R17 | 650 9 34 18 13 29 51 --- 10 | 55 37 43 54 59 68 --- 51
R18 | 1374 11 32 19 11 14 39 --- 8 | 41 32 46 45 52 56 --- 41
R19 | 1585 46 91 67 30 54 47 --- 23 | 84 41 29 84 85 87 --- 67
R20 | 1328 30 104 92 37 45 45 --- 25 | 92 36 42 101 98 100 --- 76
R21 | 759 10 49 25 23 15 45 124 11 | 44 28 36 61 57 71 71 47
R22 | 890 40 36 99 39 63 70 --- 26 | 32 39 103 70 48 69 --- 41
R24 | 2010 26 74 30 10 17 56 133 14 | 70 41 59 78 76 99 86 68
------+----------------------------------------------+------------------------------------------
RMS | 1240 22 47 40 22 28 46 193 |T 55 46 50 60 57 68 100 52
WRMS | 1240 19 37 37 16 23 43 193 |NE 55 42 49 61 57 70 116 51
MEDI | 1002 14 33 18 14 17 45 133 |MD 52 42 46 52 52 63 77 51
Table 3.2195.1 GPS week: 2195 Day: 1 MJD: 59610
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 940 44 41 35 48 98 65 --- 25 | 120 112 139 142 162 154 --- 130
R02E | 1398 15 28 18 15 9 30 --- 8 | 22 17 19 20 23 35 --- 18
R03E | 620 12 29 11 14 13 43 --- 9 | 49 44 48 46 54 45 --- 45
XR04E | 986 9 30 13 --- 16 35 169 10 | 30 32 28 --- 31 45 44 29
R05E | 1690 10 34 12 18 20 33 70 9 | 32 35 37 41 38 48 70 35
R07E | 1121 9 26 14 18 14 29 --- 8 | 49 51 47 47 50 60 --- 48
R08E | 1368 9 23 15 20 21 20 --- 8 | 24 26 25 22 33 39 --- 23
R09 | 977 13 21 17 17 13 38 --- 9 | 23 40 29 36 37 42 --- 29
R11 | 2562 15 19 22 19 17 33 --- 9 | 23 20 28 33 25 46 --- 24
R12 | 602 20 19 23 15 21 28 417 9 | 37 28 40 39 37 38 220 32
R13 | 462 29 24 37 27 62 50 --- 17 | 49 48 35 45 57 39 --- 41
R14 | 617 11 10 12 11 14 23 --- 6 | 34 31 38 29 26 37 --- 31
R15 | 756 8 11 11 7 19 28 177 6 | 37 36 46 38 27 57 123 37
R17 | 934 12 38 20 19 24 35 --- 10 | 30 22 27 44 42 48 --- 32
R18 | 1019 9 40 19 12 13 19 --- 8 | 31 34 31 27 30 33 --- 27
R19 | 951 51 101 66 37 56 32 --- 26 | 77 44 35 73 68 50 --- 53
R20 | 931 41 77 86 68 54 50 --- 28 | 56 45 35 66 49 49 --- 42
R21 | 661 18 45 19 35 23 33 112 13 | 31 26 34 47 49 39 33 32
R22 | 689 36 19 80 44 54 41 --- 22 | 36 42 61 43 45 56 --- 34
R24 | 1037 19 56 28 19 25 47 96 14 | 44 34 34 45 38 59 90 39
------+----------------------------------------------+------------------------------------------
RMS | 1122 24 41 36 29 38 37 215 |T 41 38 40 46 46 50 96 39
WRMS | 1122 18 32 33 21 28 34 215 |NE 39 34 36 43 40 45 116 34
MEDI | 940 13 28 19 19 20 33 112 |MD 34 34 35 43 38 45 70 32
Table 3.2195.2 GPS week: 2195 Day: 2 MJD: 59611
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1133 56 27 32 56 71 51 --- 23 | 71 69 74 101 107 76 --- 73
R02E | 1358 12 26 15 13 19 33 --- 8 | 31 25 40 35 35 52 --- 32
R03E | 907 14 26 28 17 16 29 --- 9 | 50 45 62 48 57 53 --- 49
XR04E | 906 14 26 28 --- 15 30 168 11 | 34 33 42 --- 39 44 28 33
R05E | 1779 16 29 11 12 13 16 46 7 | 43 34 43 38 43 50 69 39
R07E | 1419 19 19 26 27 10 25 --- 10 | 64 63 65 75 67 67 --- 65
R08E | 718 16 25 20 13 17 39 --- 9 | 37 38 38 36 43 38 --- 35
R09 | 1089 25 19 14 11 14 52 --- 11 | 38 52 44 54 56 57 --- 45
R11 | 1767 10 9 28 18 19 25 --- 8 | 56 22 58 52 55 62 --- 54
R12 | 1144 18 16 10 15 13 29 --- 7 | 55 47 50 47 48 53 --- 47
R13 | 901 21 15 30 17 53 20 --- 13 | 54 45 45 39 44 51 --- 43
R14 | 544 13 14 9 8 21 42 --- 8 | 43 44 43 41 49 43 --- 40
R15 | 1156 8 12 13 13 10 28 119 6 | 38 37 47 42 40 33 96 38
R17 | 934 15 27 12 12 15 49 --- 10 | 44 35 42 50 39 47 --- 39
R18 | 830 10 37 10 23 16 31 --- 9 | 40 34 35 50 44 42 --- 37
R19 | 995 55 107 63 32 52 43 --- 27 | 77 31 33 65 55 63 --- 49
R20 | 887 53 95 80 86 58 44 --- 32 | 65 46 37 94 53 82 --- 54
R21 | 521 12 36 20 12 25 14 94 9 | 43 36 37 45 50 35 41 39
R22 | 693 29 25 78 27 35 26 --- 18 | 35 34 53 38 53 48 --- 33
R24 | 1155 24 69 32 26 14 33 46 15 | 59 62 48 65 56 49 85 52
------+----------------------------------------------+------------------------------------------
RMS | 1103 27 43 35 29 31 35 82 |T 48 41 46 53 51 52 63 44
WRMS | 1103 18 30 30 14 26 38 82 |NE 49 40 44 52 49 51 74 43
MEDI | 934 16 26 20 17 16 30 94 |MD 43 37 43 48 49 50 69 40
Table 3.2195.3 GPS week: 2195 Day: 3 MJD: 59612
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 681 39 49 43 44 44 42 --- 19 | 77 82 83 88 91 74 --- 76
R02E | 2964 14 29 12 13 19 35 --- 9 | 40 32 33 42 44 53 --- 38
R03E | 1367 11 27 16 19 13 36 --- 9 | 40 36 38 43 48 44 --- 38
XR04E | 1843 11 27 18 --- 23 23 70 10 | 30 27 34 --- 36 33 35 28
R05E | 1121 10 28 18 17 22 39 99 9 | 37 34 39 37 43 54 71 36
R07E | 794 14 20 19 18 25 29 --- 9 | 42 36 41 43 53 47 --- 40
R08E | 3022 15 29 17 13 28 28 --- 9 | 31 34 35 28 46 40 --- 32
R09 | 1020 26 11 18 11 13 41 --- 9 | 14 31 37 28 22 58 --- 24
R11 | 1244 11 13 16 13 10 40 --- 8 | 34 16 23 29 27 37 --- 26
R12 | 1266 13 16 19 16 10 27 277 7 | 52 47 42 53 50 33 255 45
R13 | 937 27 24 33 21 45 17 --- 13 | 55 46 36 40 39 46 --- 42
R14 | 781 12 7 17 13 14 24 --- 6 | 42 34 34 39 39 29 --- 34
R15 | 986 11 11 18 8 15 22 95 6 | 46 35 33 37 50 36 81 38
R17 | 677 9 39 21 15 19 27 --- 9 | 45 25 33 50 49 54 --- 42
R18 | 653 12 34 12 9 28 19 --- 8 | 40 24 43 45 55 51 --- 40
R19 | 1470 41 105 50 23 72 30 --- 24 | 55 43 27 47 66 56 --- 40
R20 | 1538 36 94 93 64 46 60 --- 29 | 77 53 40 91 64 101 --- 65
R21 | 661 11 42 24 21 22 18 63 10 | 38 27 34 52 57 52 45 42
R22 | 1042 27 45 108 54 44 77 --- 27 | 48 42 64 58 36 90 --- 37
R24 | 1411 27 61 32 9 42 21 112 14 | 56 25 31 44 69 56 84 44
------+----------------------------------------------+------------------------------------------
RMS | 1409 22 44 40 26 32 36 150 |T 44 36 39 47 49 52 95 40
WRMS | 1409 19 33 34 14 28 32 150 |NE 46 34 36 47 47 53 116 39
MEDI | 1042 13 28 18 16 22 28 95 |MD 42 34 35 43 48 51 71 38
Table 3.2195.4 GPS week: 2195 Day: 4 MJD: 59613
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 859 23 53 41 38 33 29 --- 15 | 52 49 59 69 70 60 --- 54
R02E | 4391 7 20 17 24 18 23 --- 8 | 41 36 46 49 44 38 --- 40
R03E | 1172 12 29 14 16 23 29 --- 9 | 41 39 37 35 48 34 --- 36
XR04E | 1918 10 25 13 --- 15 15 62 7 | 34 33 34 --- 37 38 39 32
R05E | 1384 12 29 13 18 17 40 97 10 | 33 32 33 37 36 43 41 30
R07E | 1887 10 27 11 14 13 28 --- 7 | 62 65 58 63 58 46 --- 58
R08E | 1368 14 32 16 19 19 15 --- 8 | 32 33 40 39 34 35 --- 32
R09 | 996 15 16 10 14 18 21 --- 7 | 43 44 37 47 44 44 --- 41
XR11 | 1082 9 --- 19 15 12 28 --- 8 | 49 --- 54 52 49 49 --- 48
R12 | 1797 12 13 22 13 15 22 165 7 | 44 44 41 50 51 57 135 46
R13 | 839 24 36 32 29 69 25 --- 16 | 43 46 26 31 30 29 --- 31
R14 | 832 9 12 10 16 14 27 --- 7 | 40 36 36 31 39 46 --- 36
R15 | 625 7 10 19 15 14 26 78 7 | 37 38 31 31 44 48 82 35
R17 | 961 12 46 19 18 18 36 --- 11 | 46 30 36 40 52 70 --- 43
R18 | 1065 19 35 10 24 25 19 --- 10 | 37 32 37 55 54 41 --- 40
R19 | 1287 51 81 42 28 68 41 --- 23 | 59 33 34 57 58 61 --- 44
R20 | 3692 45 109 113 73 56 54 --- 33 | 73 40 57 100 65 86 --- 63
R21 | 1039 12 48 36 33 17 42 99 14 | 50 43 43 68 46 73 24 51
R22 | 1646 31 52 121 49 96 40 --- 30 | 52 44 65 73 89 69 --- 49
R24 | 1807 18 63 30 27 28 22 112 13 | 55 31 35 60 56 39 75 45
------+----------------------------------------------+------------------------------------------
RMS | 1813 22 47 45 30 39 31 114 |T 46 39 41 51 50 50 66 42
WRMS | 1813 19 36 36 18 25 27 114 |NE 48 38 40 53 52 54 79 44
MEDI | 1172 12 32 19 19 18 27 97 |MD 43 38 37 50 48 46 41 41
Table 3.2195.5 GPS week: 2195 Day: 5 MJD: 59614
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 941 32 63 45 55 46 41 --- 20 | 72 60 88 104 94 90 --- 81
R02E | 3561 17 27 12 11 22 31 --- 9 | 39 41 47 45 49 51 --- 43
R03E | 721 10 26 19 15 17 15 --- 7 | 48 43 62 54 56 61 --- 52
XR04E | 1115 7 26 16 --- 11 18 67 7 | 31 23 32 --- 37 36 43 30
R05E | 724 15 22 18 12 12 28 89 8 | 36 29 38 39 49 58 36 39
R07E | 1612 11 27 15 17 11 14 --- 7 | 56 53 56 55 56 65 --- 55
R08E | 2228 21 30 16 28 16 23 --- 10 | 46 39 38 38 47 44 --- 40
R09 | 721 10 13 22 14 23 26 --- 8 | 48 46 56 54 44 55 --- 47
XR11 | 798 13 --- 25 12 20 38 --- 11 | 57 --- 54 66 39 71 --- 55
R12 | 803 12 21 23 14 21 30 97 9 | 41 44 37 33 36 59 57 38
R13 | 713 22 43 22 24 48 29 --- 14 | 34 38 26 24 21 44 --- 24
R14 | 894 12 16 10 10 10 32 --- 7 | 31 33 25 26 27 31 --- 25
R15 | 838 12 16 11 19 15 19 106 7 | 38 38 33 21 29 48 94 32
R17 | 501 10 37 20 15 21 23 --- 9 | 37 28 36 48 46 45 --- 39
R18 | 573 19 32 23 14 23 34 --- 10 | 31 31 39 32 42 43 --- 32
R19 | 2154 42 80 49 30 65 48 --- 23 | 38 30 47 61 41 48 --- 36
R20 | 2497 36 107 87 69 51 44 --- 29 | 41 53 50 67 40 57 --- 44
R21 | 885 12 38 39 30 15 32 148 12 | 45 35 33 46 43 51 59 40
R22 | 1560 62 47 118 27 94 49 --- 31 | 70 43 61 40 79 57 --- 38
R24 | 2758 11 62 30 22 24 20 119 12 | 43 39 43 51 50 47 50 43
------+----------------------------------------------+------------------------------------------
RMS | 1627 25 46 42 28 37 31 114 |T 44 39 45 47 46 53 56 41
WRMS | 1627 17 36 31 22 25 28 114 |NE 42 38 41 43 41 50 65 37
MEDI | 885 12 30 22 17 21 29 97 |MD 41 39 39 46 43 51 50 39
Table 3.2195.6 GPS week: 2195 Day: 6 MJD: 59615
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1228 34 68 42 54 41 40 --- 20 | 86 76 77 103 83 86 --- 81
R02E | 4322 11 35 14 11 15 12 --- 7 | 54 55 57 54 61 59 --- 55
R03E | 892 10 30 16 10 18 14 --- 7 | 45 40 49 44 53 53 --- 46
XR04E | 917 9 26 25 --- 14 13 82 8 | 39 40 39 --- 39 44 57 37
R05E | 900 17 25 18 22 16 26 108 9 | 48 45 51 52 52 53 54 47
R07E | 1109 10 28 17 10 11 21 --- 7 | 61 53 63 60 66 60 --- 60
R08E | 1831 15 33 18 17 9 16 --- 8 | 45 46 52 51 50 49 --- 47
R09 | 922 16 15 9 9 32 15 --- 7 | 51 48 44 46 41 51 --- 44
XR11 | 803 14 --- 19 16 17 30 --- 10 | 56 --- 52 62 56 69 --- 58
R12 | 668 11 14 11 13 30 23 139 8 | 59 60 56 62 46 65 71 57
R13 | 551 32 17 26 24 47 10 --- 12 | 63 52 48 50 46 50 --- 49
R14 | 617 15 19 9 13 7 22 --- 6 | 54 51 48 49 52 50 --- 49
R15 | 1076 17 26 16 11 24 12 118 7 | 61 61 46 48 51 58 148 52
R17 | 631 9 22 13 11 21 20 --- 7 | 60 41 49 64 67 75 --- 58
R18 | 836 32 41 17 20 21 14 --- 10 | 45 35 60 65 68 62 --- 54
R19 | 1006 40 84 35 29 47 17 --- 18 | 79 36 35 78 73 69 --- 60
R20 | 1251 40 126 88 58 61 31 --- 29 | 104 40 50 115 92 107 --- 85
R21 | 1363 11 31 16 11 15 15 222 7 | 56 37 41 68 64 64 77 55
R22 | 2425 45 44 85 23 60 23 --- 22 | 55 35 82 50 51 40 --- 34
R24 | 1846 12 66 31 19 27 32 99 13 | 63 30 43 67 73 72 49 57
------+----------------------------------------------+------------------------------------------
RMS | 1569 24 49 35 25 32 22 144 |T 59 46 52 62 59 61 76 54
WRMS | 1569 21 36 22 15 25 21 144 |NE 62 43 50 63 60 64 86 54
MEDI | 922 15 30 17 16 21 17 108 |MD 56 45 49 60 53 59 57 54
More information about the IGSREPORT
mailing list