[IGSREPORT-25163] Wk 1939 IGLOS Final Orbits
acc
acc at igs.org
Sun Mar 26 06:04:06 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1939 (Mar 05, 2017 - Mar 11, 2017)
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 2.1939.
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:
igl1939[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1939 in the SP3 format.
igl19397.sum Combination Report for GPS Week 1939.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -7.3 ns
1 | -10.2 ns
2 | -9.7 ns
3 | -8.6 ns
4 | -9.1 ns
5 | -9.4 ns
6 | -12.3 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 1.1939, 1a.1939).
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 2.1939.0-6)
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 3.1939.0-6).
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 1939 summary. (Mar 05, 2017 - Mar 11, 2017)
Table 1.1939.a GPS week : 1939 MJD: 57817.0-57823.0
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| -2 0 -3 -26 -2 9 .10 31 30 | -11045 83 3060 11412
| 1 0 2 13 19 39 .03 | 828 1641
cof n/a| -3 1 -6 -22 2 -15 .07 36 33 | -11050 88 3063 11412
| 1 1 2 21 37 36 .07 | 828 1636
emx n/a| 0 -1 6 2 -39 -46 .13 23 23 | -14984 921 3033 10478
| 0 1 2 40 34 30 .03 | 12558 1262
esx n/a| 0 0 -1 21 1 -9 .14 16 15 | -12744 -628 3051 13308
| 1 1 1 9 17 28 .01 | 15411 1885
gfz n/a| -1 0 3 -2 24 -4 -.02 24 22 | 0 250 3032 10773
| 1 0 1 15 20 33 .08 | 0 1557
grg n/a| 0 1 2 -61 33 24 -.32 33 28 | -159053 288155 3083 11188
| 1 1 7 22 30 55 .05 | 255726 493473
iac n/a| 0 0 -5 19 -1 21 -.15 20 20 | -8969 277 3048 10602
| 1 0 1 34 43 36 .03 | 1477 936
mcc n/a| 2 1 -6 -17 24 -245 -.60 124 124 | --- --- --- ---
| 3 7 15 129 104 515 .48 | --- ---
Table 1.1939.b GPS week : 1939 MJD: 57817.0-57823.0
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 | 12 14 10 10 11 11 16 |
R02 | 7 8 7 8 7 8 9 |
R03 | 10 9 10 10 9 8 10 |
R04 | 7 8 8 8 9 7 8 |
R05 | 14 12 13 13 13 13 14 |
R07 | 10 9 9 10 10 8 10 |
R08 | 7 9 11 7 8 8 9 |
R09 | 7 8 8 9 9 9 7 |
R10 | 7 8 9 10 7 8 8 |
R11 | 9 9 8 8 9 7 10 |
R13 | 8 9 9 9 8 9 7 |
R14 | 14 13 12 12 14 16 13 |
R15 | 9 9 11 12 10 10 8 |
R16 | 14 13 12 13 13 14 15 |
R17 | 8 9 8 9 7 7 7 |
R18 | 8 9 7 7 6 7 7 |
R19 | 13 11 11 11 10 9 12 |
R20 | 18 14 14 18 14 13 13 |
R21 | 7 10 10 9 8 9 8 |
R22 | 8 7 10 10 9 9 11 |
R23 | 8 8 7 9 8 9 6 |
R24 | 17 16 17 14 15 15 20 |
Table 1.1939.c GPS week : 1939 MJD: 57817.0-57823.0
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 1939 0 | -10 -12 -33 34 640 786 85.1 957 957 | -7264 0
brd 1939 1 | 10 -10 -24 157 250 2149 84.6 998 998 | -10202 0
brd 1939 2 | 7 15 -66 894 791 632 85.2 990 990 | -9680 0
brd 1939 3 | -25 31 -27 -137 -240 1376 84.4 982 982 | -8639 0
brd 1939 4 | -11 26 22 -226 -1720 835 85.3 1118 1118 | -9084 0
brd 1939 5 | 0 40 -18 -665 -290 1631 84.4 1255 1255 | -9417 0
brd 1939 6 | 27 -23 21 44 -587 26 84.5 1211 1211 | -12309 0
-------------+------------------------------------------------------------+----------------
brd 1939 mean| 0 9 -18 14 -165 1062 84.8 1073 1073 | -9513 0
brd 1939 sdev| 17 25 31 472 851 705 .4 121 121 | 1545 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 2.1939.0 GPS week: 1939 Day: 0 MJD: 57817
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 -6 -34 25 28 .06 35 30 | -12355 2522 2823 11536
cof n/a| -2 2 -8 -16 66 -30 -.02 41 36 | -12365 2532 2828 11535
emx n/a| 0 0 4 44 -46 -84 .19 22 22 | -21497 2997 2811 10526
esx n/a| 0 1 -3 8 27 31 .14 18 14 | -7837 1687 2826 13380
gfz n/a| -1 0 3 -11 55 13 .08 24 23 | 0 2236 2818 10946
grg n/a| 0 0 5 -67 46 -93 -.35 31 25 | -8731 2652 2828 11016
iac n/a| 0 0 -2 1 -40 42 -.20 21 21 | -7489 1570 2835 10758
mcc n/a| -3 0 7 -61 89 583 -.67 120 120 | --- --- --- ---
Table 2.1939.1 GPS week: 1939 Day: 1 MJD: 57818
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| -4 0 -4 -30 16 64 .12 34 33 | -11916 -2155 2859 11188
cof n/a| -2 0 -4 -34 36 44 .16 37 36 | -11919 -2143 2865 11187
emx n/a| -1 0 2 71 -30 -31 .16 21 21 | -19883 -564 2836 10242
esx n/a| 1 0 -2 22 22 -7 .14 16 16 | -14607 -2277 2843 13087
gfz n/a| 1 0 3 13 12 51 -.03 23 20 | 0 -2257 2834 10466
grg n/a| -2 0 15 -76 29 23 -.25 35 29 | -9278 -1637 2814 10882
iac n/a| 0 1 -4 -40 -44 -38 -.16 19 19 | -8898 -1301 2829 10328
mcc n/a| 3 10 -21 -265 -42 123 -1.07 121 121 | --- --- --- ---
Table 2.1939.2 GPS week: 1939 Day: 2 MJD: 57819
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 0 -5 -3 -24 9 .11 30 30 | -10914 979 3118 11182
cof n/a| -3 2 -4 3 -27 1 .09 32 30 | -10913 966 3124 11184
emx n/a| 0 -1 5 -2 -86 -70 .10 24 24 | -25811 1637 3109 10560
esx n/a| 0 1 1 28 3 -17 .13 14 13 | 9888 201 3104 13162
gfz n/a| 0 0 3 15 -6 11 -.13 25 24 | 0 351 3099 10669
grg n/a| 0 0 1 -37 -14 24 -.28 35 27 | -501803 948663 3218 11129
iac n/a| 1 0 -5 3 51 34 -.12 19 19 | -8764 78 3097 10446
mcc n/a| 1 0 -31 -40 94 -837 -1.21 158 158 | --- --- --- ---
Table 2.1939.3 GPS week: 1939 Day: 3 MJD: 57820
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 -1 -20 -18 -31 .09 30 30 | -10669 1022 2873 12672
cof n/a| -4 2 -4 -4 -32 -75 .16 33 32 | -10682 1049 2871 12673
emx n/a| -1 -4 7 -11 -54 -73 .11 24 24 | 7419 856 2846 11031
esx n/a| 0 1 -2 14 -19 -6 .13 18 18 | -13181 -3827 2861 14576
gfz n/a| -2 1 3 5 12 -26 .10 23 22 | 0 1321 2833 12024
grg n/a| 0 1 -2 -23 76 53 -.29 36 31 | -563191 1068811 2855 12803
iac n/a| 0 0 -4 25 48 16 -.14 17 17 | -7977 -85 2852 11899
mcc n/a| 8 0 0 71 77 -804 -.14 116 116 | --- --- --- ---
Table 2.1939.4 GPS week: 1939 Day: 4 MJD: 57821
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| -3 -1 -4 -20 -10 -49 .15 29 28 | -10049 -434 3565 11389
cof n/a| -4 0 -10 -16 -14 -33 .06 35 32 | -10049 -439 3561 11386
emx n/a| -1 -1 10 -34 -11 -44 .11 23 23 | -14507 1388 3480 10492
esx n/a| 0 0 0 17 -16 9 .16 15 14 | -32864 737 3572 13269
gfz n/a| -2 0 3 0 36 -10 -.01 22 24 | 0 744 3481 10763
grg n/a| 2 0 0 -89 19 46 -.39 31 30 | -9412 -13 3605 11421
iac n/a| 2 0 -5 62 26 18 -.16 18 18 | -8926 1009 3570 10480
mcc n/a| 3 12 9 -29 153 -526 .06 115 115 | --- --- --- ---
Table 2.1939.5 GPS week: 1939 Day: 5 MJD: 57822
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| -5 0 -7 -47 8 7 .09 32 31 | -11074 347 3192 11038
cof n/a| -6 0 -6 -59 11 -10 -.00 38 34 | -11069 327 3195 11042
emx n/a| -1 -2 8 -40 -63 -15 .13 22 22 | -3897 724 3174 9991
esx n/a| 0 0 -1 20 -2 -12 .15 15 13 | -23 -10 3159 12746
gfz n/a| 0 0 2 -19 27 -17 -.07 22 19 | 0 744 3183 10269
grg n/a| 1 3 2 -67 60 35 -.34 31 25 | -9487 199 3209 10755
iac n/a| 1 0 -6 50 -10 1 -.14 19 19 | -8635 776 3171 10074
mcc n/a| 0 -7 0 119 -124 -176 -.85 111 111 | --- --- --- ---
Table 2.1939.6 GPS week: 1939 Day: 6 MJD: 57823
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 -27 -15 38 .08 29 27 | -10344 -1700 2992 10882
cof n/a| -1 0 -3 -33 -24 -2 .07 35 32 | -10356 -1672 2997 10881
emx n/a| -1 -1 8 -12 16 -8 .10 21 21 | -26717 -586 2979 10509
esx n/a| 3 0 -2 36 -4 -61 .16 17 16 | -30589 -907 2992 12938
gfz n/a| -1 -1 5 -23 36 -52 -.05 29 26 | 0 -1389 2980 10275
grg n/a| 0 2 -8 -71 13 80 -.35 34 26 | -11472 -1584 3056 10314
iac n/a| -1 1 -8 34 -43 77 -.14 25 25 | -12095 -103 2986 10234
mcc n/a| 3 -6 -5 82 -77 -79 -.34 131 131 | --- --- --- ---
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 3.1939.0 GPS week: 1939 Day: 0 MJD: 57817
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 497 68 73 22 11 28 19 20 --- 12 | 4 5 2 4 5 3 2 --- 3
R02 | 691 22 19 16 15 16 14 10 123 6 | 2 4 3 3 4 3 3 2 2
R03 | 1213 40 40 18 7 29 24 14 135 9 | 3 4 3 3 4 7 3 1 2
R04 | 1640 36 41 12 10 21 12 12 --- 7 | 2 3 2 2 2 4 2 --- 2
R05 | 643 50 52 27 18 34 30 35 --- 13 | 4 10 3 5 7 6 3 --- 3
R07 | 681 48 51 16 9 26 23 13 155 9 | 2 4 3 3 3 3 3 2 2
R08 | 824 27 21 12 10 22 15 9 --- 6 | 2 5 2 2 3 3 3 --- 2
XR09 | 1177 20 24 14 12 14 --- 13 --- 7 | 1 2 2 2 3 --- 2 --- 1
R10 | 636 21 32 14 15 23 12 13 --- 7 | 2 4 2 5 3 2 2 --- 2
R11 | 530 33 35 11 12 17 25 21 101 8 | 2 2 2 2 2 4 2 2 2
R13 | 1027 29 32 15 11 27 16 14 --- 8 | 2 3 2 3 5 2 2 --- 2
R14 | 884 24 30 27 31 23 34 37 --- 13 | 2 9 6 6 9 3 3 --- 4
R15 | 1038 25 23 22 21 23 12 16 --- 9 | 2 4 3 3 3 1 2 --- 2
R16 | 554 45 66 21 36 20 48 20 --- 14 | 2 9 2 4 5 2 3 --- 2
R17 | 900 25 27 17 14 16 16 18 --- 7 | 1 2 2 4 4 3 1 --- 2
R18 | 1897 23 27 15 13 25 15 21 --- 8 | 1 2 2 1 5 3 2 --- 2
R19 | 708 55 66 36 14 33 18 25 --- 13 | 1 7 3 6 4 3 2 --- 3
R20 | 622 22 28 43 25 22 80 12 --- 17 | 3 9 4 5 5 5 2 --- 3
R21 | 782 24 31 11 10 15 13 18 65 6 | 1 3 1 2 3 3 2 1 1
R22 | 1373 28 37 11 9 18 20 19 --- 7 | 1 3 2 4 3 3 1 --- 1
R23 | 737 15 18 20 11 15 26 10 --- 7 | 1 2 1 2 1 4 2 --- 1
R24 | 747 28 53 36 29 28 65 38 --- 17 | 4 6 2 4 5 5 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 957 35 41 22 18 24 31 21 120 |T 2 4 2 3 4 3 2 1 2
WRMS | 957 30 36 22 14 23 25 21 120 |NE 2 4 2 3 4 3 2 1 2
MEDI | 747 27 32 16 12 22 19 16 123 |MD 2 4 2 3 4 3 2 2 2
Table 3.1939.1 GPS week: 1939 Day: 1 MJD: 57818
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 912 69 75 27 11 35 28 18 --- 13 | 3 6 4 5 6 5 2 --- 3
R02 | 586 21 25 17 18 20 20 9 77 7 | 2 4 3 5 4 3 2 1 2
R03 | 1151 43 60 13 13 23 28 12 75 9 | 3 5 3 5 4 6 3 2 3
R04 | 1734 41 39 15 7 21 20 11 --- 8 | 2 3 3 3 2 3 3 --- 2
R05 | 764 35 44 21 20 39 21 28 --- 12 | 3 9 3 5 8 6 3 --- 2
R07 | 1541 45 50 14 11 25 22 13 163 9 | 3 5 3 6 5 4 4 2 3
R08 | 858 33 38 13 8 24 38 11 --- 8 | 2 5 2 3 3 3 2 --- 2
XR09 | 1684 23 23 18 13 17 --- 11 --- 8 | 1 3 2 2 3 --- 3 --- 1
R10 | 999 18 25 16 20 16 27 8 --- 8 | 2 4 4 7 5 4 2 --- 3
R11 | 624 34 39 15 8 22 28 17 159 8 | 2 3 3 2 3 7 2 2 2
R13 | 754 29 27 18 11 22 37 17 --- 9 | 2 3 2 3 5 4 2 --- 2
R14 | 1254 27 31 18 21 20 42 38 --- 12 | 2 10 6 6 8 4 3 --- 3
R15 | 743 30 35 21 20 13 17 18 --- 9 | 3 4 3 4 5 3 3 --- 2
R16 | 695 27 19 28 28 17 53 16 --- 12 | 3 9 3 4 6 3 3 --- 2
R17 | 940 26 27 14 14 25 26 17 --- 8 | 1 2 2 4 5 3 1 --- 2
R18 | 1313 20 23 17 17 20 29 16 --- 8 | 1 3 3 4 5 5 2 --- 2
R19 | 1174 47 42 30 15 25 15 20 --- 11 | 1 5 3 5 5 3 1 --- 3
R20 | 584 20 23 29 24 23 62 20 --- 13 | 3 10 4 7 8 6 3 --- 4
R21 | 581 33 30 22 12 17 23 27 99 10 | 1 5 2 7 4 3 3 1 3
R22 | 970 26 22 12 10 13 20 17 --- 7 | 1 4 2 4 4 3 1 --- 2
R23 | 1009 11 11 19 18 16 22 10 --- 7 | 1 3 3 4 2 5 2 --- 1
R24 | 727 35 37 38 17 28 80 23 --- 16 | 4 5 3 5 6 9 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 998 34 37 21 16 23 35 19 121 |T 2 5 3 4 4 4 2 1 2
WRMS | 998 33 36 21 16 20 29 19 121 |NE 2 5 3 4 4 4 2 1 2
MEDI | 912 29 30 18 14 21 27 17 99 |MD 2 4 3 4 5 4 2 2 2
Table 3.1939.2 GPS week: 1939 Day: 2 MJD: 57819
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 633 44 40 21 7 25 26 13 --- 9 | 3 6 3 5 6 5 2 --- 3
R02 | 801 23 23 17 9 22 22 12 49 7 | 2 4 3 4 3 2 2 4 2
R03 | 568 37 29 23 16 26 18 12 75 9 | 2 4 3 5 3 2 2 3 3
R04 | 1558 36 32 18 10 22 19 9 --- 8 | 2 5 3 3 4 2 2 --- 2
R05 | 780 21 23 17 20 33 57 28 --- 13 | 4 10 2 4 10 3 3 --- 2
R07 | 1070 39 40 12 8 33 22 12 183 9 | 2 4 3 5 5 3 3 11 3
R08 | 1451 28 31 17 10 25 54 15 --- 10 | 3 5 3 4 3 5 3 --- 3
XR09 | 2001 18 23 23 8 13 --- 14 --- 7 | 1 3 2 2 2 --- 2 --- 2
R10 | 826 20 22 19 18 27 16 14 --- 8 | 2 4 3 6 6 3 2 --- 3
R11 | 928 27 27 12 9 28 15 15 234 7 | 2 3 3 4 4 7 1 18 2
R13 | 982 30 27 15 12 22 23 18 --- 8 | 2 4 2 5 5 5 2 --- 3
R14 | 1258 28 27 20 14 28 43 26 --- 11 | 2 7 5 6 9 2 3 --- 3
R15 | 1083 37 42 25 19 39 22 12 --- 11 | 2 4 2 4 5 3 2 --- 2
R16 | 577 25 48 31 24 16 33 23 --- 11 | 2 8 4 10 7 3 3 --- 4
R17 | 903 21 22 16 11 25 28 12 --- 8 | 1 2 2 4 4 3 1 --- 2
R18 | 1020 22 22 18 8 18 12 11 --- 6 | 1 2 2 3 4 3 1 --- 2
R19 | 1399 42 39 22 21 19 26 17 --- 10 | 1 2 3 8 6 3 1 --- 3
R20 | 928 31 34 44 11 18 68 18 --- 14 | 3 8 5 6 9 7 1 --- 4
R21 | 522 28 28 24 13 23 27 23 167 9 | 1 4 2 6 4 5 2 7 3
R22 | 700 26 27 21 14 21 14 32 --- 10 | 1 4 6 6 4 3 2 --- 2
R23 | 1008 12 14 19 12 13 23 19 --- 7 | 2 3 3 4 2 5 3 --- 1
R24 | 938 28 46 51 16 35 70 30 --- 16 | 3 7 3 5 5 8 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 990 30 32 24 14 25 35 19 157 |T 2 4 3 4 5 3 2 8 2
WRMS | 990 30 30 24 13 24 27 19 157 |NE 2 4 3 4 5 3 2 8 2
MEDI | 928 28 27 19 12 23 23 15 167 |MD 2 4 3 5 4 3 2 7 3
Table 3.1939.3 GPS week: 1939 Day: 3 MJD: 57820
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 516 41 21 17 9 23 31 11 --- 9 | 4 12 3 3 5 3 2 --- 2
R02 | 971 21 26 16 11 25 20 10 65 7 | 2 5 2 3 4 1 2 6 2
R03 | 620 42 46 18 7 29 24 8 87 9 | 2 3 3 3 3 3 2 5 2
R04 | 1155 33 42 14 14 23 20 11 --- 8 | 2 4 2 3 5 3 2 --- 2
R05 | 1005 22 29 28 17 27 51 26 --- 12 | 4 11 3 6 9 3 4 --- 3
R07 | 691 34 40 26 15 28 15 11 194 9 | 2 3 3 3 6 4 3 18 3
R08 | 1706 27 25 18 10 19 20 8 --- 7 | 2 5 4 6 3 4 2 --- 3
XR09 | 1693 21 17 22 15 11 --- 15 --- 8 | 1 4 2 6 4 --- 3 --- 3
R10 | 1114 15 18 30 28 14 22 15 --- 10 | 2 6 3 4 5 4 2 --- 2
R11 | 776 27 31 14 10 19 23 16 115 7 | 2 3 2 5 4 4 2 29 2
R13 | 903 30 32 18 13 28 19 14 --- 8 | 2 4 2 7 6 4 2 --- 3
R14 | 1264 32 32 30 22 21 25 24 --- 11 | 3 9 4 10 8 5 4 --- 5
R15 | 783 27 24 28 25 34 34 16 --- 11 | 2 5 3 5 4 3 3 --- 2
R16 | 782 24 27 30 18 21 61 16 --- 12 | 2 8 4 9 6 3 2 --- 4
R17 | 644 26 27 23 11 22 29 9 --- 8 | 1 2 4 4 5 2 1 --- 2
R18 | 682 19 29 18 8 26 21 6 --- 7 | 1 3 2 4 5 4 1 --- 2
R19 | 749 36 43 28 22 20 26 20 --- 11 | 1 4 3 7 5 2 2 --- 3
R20 | 701 49 52 44 24 24 73 28 --- 17 | 4 6 4 3 6 6 3 --- 3
R21 | 856 30 30 21 14 18 30 16 72 9 | 1 3 3 4 4 4 2 11 2
R22 | 1025 31 38 22 18 19 28 22 --- 10 | 1 5 4 5 4 5 3 --- 2
R23 | 1640 7 15 11 27 10 17 25 --- 9 | 2 4 3 3 3 6 2 --- 1
R24 | 1011 25 38 31 22 23 73 18 --- 14 | 4 11 4 13 8 7 2 --- 6
------+---------------------------------------------------+-----------------------------------------------
RMS | 982 30 33 24 18 23 36 17 116 |T 2 5 3 5 5 3 2 13 2
WRMS | 982 30 32 24 18 22 31 17 116 |NE 2 5 3 5 5 3 2 13 2
MEDI | 856 27 29 22 15 22 25 15 87 |MD 2 4 3 4 5 4 2 11 2
Table 3.1939.4 GPS week: 1939 Day: 4 MJD: 57821
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 579 51 68 17 9 25 32 14 --- 10 | 3 8 3 3 3 3 2 --- 2
R02 | 1561 20 21 16 12 14 18 12 79 6 | 3 5 3 4 6 2 2 1 3
R03 | 989 42 49 18 8 21 23 11 89 9 | 2 4 4 3 3 3 2 1 2
R04 | 848 39 32 17 10 26 23 11 --- 9 | 2 3 3 4 5 4 2 --- 3
R05 | 963 23 35 26 18 22 52 29 --- 12 | 3 9 3 5 6 4 5 --- 3
R07 | 812 33 34 30 16 25 13 11 191 9 | 2 4 4 3 6 4 2 2 2
R08 | 1862 27 32 12 14 17 23 14 --- 7 | 2 6 3 6 3 3 3 --- 3
XR09 | 1962 21 21 20 18 15 --- 14 --- 9 | 1 4 2 5 4 --- 2 --- 2
R10 | 591 19 24 19 13 16 13 11 --- 6 | 2 5 2 4 4 3 1 --- 2
R11 | 719 20 21 14 21 24 17 16 93 8 | 2 3 2 5 3 3 3 1 2
R13 | 2060 25 18 14 14 22 15 13 --- 7 | 2 4 3 7 5 4 2 --- 3
R14 | 1334 32 37 40 22 23 41 32 --- 14 | 3 14 7 11 9 5 5 --- 6
R15 | 1092 23 20 18 19 22 35 13 --- 9 | 2 6 2 4 4 3 4 --- 2
R16 | 730 31 36 38 20 16 44 26 --- 13 | 2 6 3 4 6 3 3 --- 3
R17 | 789 23 28 14 10 20 13 18 --- 7 | 1 3 3 4 5 2 1 --- 2
R18 | 786 9 11 13 13 15 14 10 --- 5 | 1 3 2 3 7 6 2 --- 2
R19 | 741 23 15 25 8 33 27 18 --- 9 | 1 5 3 3 3 2 2 --- 2
R20 | 637 41 60 39 17 25 49 15 --- 13 | 3 5 3 6 7 3 4 --- 4
R21 | 1105 28 32 17 11 22 21 15 78 8 | 1 3 2 4 5 2 1 1 2
R22 | 615 29 28 16 12 23 17 23 --- 8 | 2 5 2 4 5 3 3 --- 3
R23 | 1488 13 16 23 14 22 16 11 --- 7 | 2 4 2 6 5 4 2 --- 3
R24 | 1445 31 55 29 21 20 67 28 --- 14 | 6 16 5 11 9 6 2 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1118 29 35 23 15 22 31 18 115 |T 2 5 3 4 5 3 2 1 2
WRMS | 1118 28 32 23 14 24 30 18 115 |NE 2 5 3 4 5 3 2 1 2
MEDI | 848 25 28 18 14 22 23 14 89 |MD 2 5 3 4 5 3 2 1 2
Table 3.1939.5 GPS week: 1939 Day: 5 MJD: 57822
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 728 62 68 18 10 27 21 14 --- 11 | 3 4 3 3 3 4 3 --- 2
R02 | 1365 22 26 18 17 20 16 15 89 8 | 2 5 3 7 6 4 3 1 3
R03 | 1001 41 42 13 11 16 16 17 87 8 | 3 4 4 4 5 3 3 1 2
R04 | 1163 31 38 14 10 18 15 11 --- 7 | 2 4 2 4 3 4 2 --- 2
R05 | 1009 40 44 23 15 24 36 35 --- 12 | 4 6 3 4 9 6 3 --- 3
R07 | 820 33 41 19 7 24 13 15 140 8 | 2 4 4 5 6 2 3 2 3
R08 | 1987 28 34 17 12 25 19 15 --- 8 | 2 4 3 4 3 3 2 --- 2
XR09 | 1648 22 22 22 9 23 --- 13 --- 8 | 1 4 3 4 4 --- 2 --- 2
R10 | 501 16 16 15 15 24 22 11 --- 7 | 2 6 2 4 4 2 2 --- 2
R11 | 883 26 27 13 7 18 14 12 135 6 | 2 4 2 6 6 5 2 1 3
R13 | 1400 28 34 21 10 27 23 6 --- 8 | 2 4 3 5 4 4 2 --- 3
R14 | 3026 45 65 24 36 28 55 29 --- 16 | 3 15 9 15 12 3 4 --- 8
R15 | 1109 25 32 20 12 25 32 21 --- 9 | 2 5 2 5 4 4 2 --- 2
R16 | 779 34 25 47 18 26 43 19 --- 14 | 3 3 2 4 7 2 3 --- 2
R17 | 829 15 11 12 8 16 25 18 --- 7 | 1 4 2 3 4 3 2 --- 2
R18 | 938 11 19 8 14 18 25 10 --- 6 | 2 2 2 2 5 5 2 --- 2
R19 | 1097 33 32 23 10 20 17 16 --- 8 | 2 6 4 6 8 2 2 --- 3
R20 | 1145 30 36 28 26 19 50 25 --- 13 | 4 13 4 10 8 2 4 --- 5
R21 | 834 32 34 24 9 12 18 20 94 8 | 1 3 2 3 5 2 2 1 2
R22 | 647 33 40 18 7 17 12 28 --- 8 | 1 4 2 4 4 2 3 --- 2
R23 | 710 11 9 22 22 16 23 19 --- 9 | 1 4 2 7 4 2 2 --- 3
R24 | 1734 27 55 37 15 30 69 13 --- 15 | 5 17 6 7 8 5 3 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1255 32 38 22 15 22 31 19 111 |T 2 5 3 5 5 3 2 1 2
WRMS | 1255 31 34 22 13 19 25 19 111 |NE 2 5 3 5 5 3 2 1 2
MEDI | 1001 28 34 19 11 20 22 15 94 |MD 2 4 3 4 5 3 2 1 2
Table 3.1939.6 GPS week: 1939 Day: 6 MJD: 57823
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 514 53 65 30 18 26 36 48 --- 15 | 2 4 2 3 2 4 4 --- 2
R02 | 1897 17 27 23 16 26 22 13 76 8 | 3 5 3 6 4 4 4 2 2
R03 | 594 39 37 16 9 29 25 17 72 9 | 3 3 3 3 4 4 3 1 2
XR04 | 912 30 31 14 9 16 --- 14 --- 8 | 3 3 2 2 2 --- 3 --- 2
R05 | 882 39 53 22 27 31 45 34 --- 14 | 3 7 2 3 8 6 3 --- 2
R07 | 1081 33 41 16 12 33 22 19 139 9 | 3 3 3 4 5 2 2 2 2
R08 | 1216 22 28 19 14 19 30 11 --- 8 | 3 3 3 3 2 4 2 --- 2
XR09 | 2176 20 20 11 8 16 --- 12 --- 6 | 1 3 2 4 3 --- 2 --- 2
R10 | 669 19 23 18 18 22 16 8 --- 7 | 2 4 2 3 3 2 2 --- 2
R11 | 697 26 22 17 12 27 21 30 199 9 | 2 3 2 4 4 5 2 2 2
R13 | 1010 26 30 13 12 22 15 14 --- 7 | 2 3 2 3 2 3 2 --- 2
R14 | 2192 21 36 21 21 26 43 34 --- 12 | 3 9 6 11 8 3 4 --- 6
R15 | 949 21 22 18 12 26 19 16 --- 8 | 2 3 2 4 3 3 3 --- 2
R16 | 874 32 48 41 22 51 36 28 --- 15 | 3 2 2 3 6 2 3 --- 2
R17 | 533 14 20 11 9 20 13 20 --- 6 | 1 3 1 2 3 2 3 --- 2
R18 | 1549 17 18 11 12 23 18 15 --- 7 | 1 2 2 2 3 2 2 --- 1
R19 | 1926 47 55 11 19 33 29 22 --- 11 | 2 5 3 5 6 2 2 --- 3
R20 | 1429 20 21 17 32 17 54 16 --- 12 | 4 10 3 7 5 2 3 --- 3
R21 | 483 21 23 13 9 34 20 15 125 8 | 1 2 1 2 3 2 3 1 1
R22 | 1378 34 34 20 11 19 31 31 --- 10 | 1 3 1 3 3 2 2 --- 2
R23 | 539 15 15 11 13 15 21 13 --- 6 | 1 3 2 5 2 2 3 --- 2
R24 | 1542 32 42 39 17 54 84 41 --- 19 | 4 11 5 6 5 4 2 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1210 29 35 21 17 29 34 25 131 |T 2 4 2 4 3 3 2 1 2
WRMS | 1210 27 32 21 16 26 26 25 131 |NE 2 4 2 4 3 3 2 1 2
MEDI | 949 22 28 17 12 26 22 16 125 |MD 2 3 2 3 3 2 3 2 2
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