[IGSREPORT-25452] Wk 1960 IGLOS Final Orbits
acc
acc at igs.org
Sun Aug 20 04:34:09 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1960 (Jul 30, 2017 - Aug 05, 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 2.1960.
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:
igl1960[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1960 in the SP3 format.
igl19607.sum Combination Report for GPS Week 1960.
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 | -1.8 ns
1 | 1.6 ns
2 | 2.1 ns
3 | -1.2 ns
4 | -1.1 ns
5 | 0.7 ns
6 | -1.6 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 1.1960, 1a.1960).
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 2.1960.0-6)
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 3.1960.0-6).
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 1960 summary. (Jul 30, 2017 - Aug 05, 2017)
Table 1.1960.a GPS week : 1960 MJD: 57964.0-57970.0
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 7 -28 5 32 .09 35 35 | 7704 -1482 3029 10660
| 1 1 2 33 15 47 .06 | 2922 2611
cof n/a| -1 2 7 -24 19 44 .12 37 36 | 7702 -1492 3030 10662
| 2 1 2 38 17 36 .04 | 2920 2616
emx n/a| -1 0 3 1 -30 61 .08 23 23 | -2603 -1409 3044 9781
| 1 1 3 20 23 24 .05 | 8630 1591
esx n/a| 0 0 -2 0 18 -22 .17 18 16 | -7789 -1829 3042 12711
| 0 1 1 24 18 17 .04 | 9613 3483
gfz n/a| -1 0 -4 -34 35 18 .11 26 23 | 0 -1764 3041 10473
| 1 1 2 16 35 21 .05 | 0 2333
grg n/a| 0 0 0 -36 8 -151 -.38 31 29 | 513 -1398 3032 9892
| 2 0 8 23 17 56 .04 | 1321 2461
iac n/a| 1 0 -3 57 -22 44 -.15 21 22 | 1309 -910 3043 9775
| 1 1 1 31 41 46 .05 | 1550 1118
mcc n/a| 1 -2 17 145 -11 185 -.28 120 120 | --- --- --- ---
| 5 6 7 86 111 329 .23 | --- ---
Table 1.1960.b GPS week : 1960 MJD: 57964.0-57970.0
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 13 16 13 14 16 17 |
R02 | 11 11 11 10 11 11 11 |
R03 | 10 9 10 10 11 10 10 |
R04 | 7 8 9 7 10 8 8 |
R05 | 13 12 14 14 14 13 12 |
R06 | 12 12 11 10 10 10 10 |
R07 | 10 9 7 10 10 10 9 |
R08 | 7 9 9 6 9 7 11 |
R09 | 8 12 12 10 7 7 7 |
R10 | 7 12 14 8 10 7 8 |
R11 | 8 7 9 7 6 7 8 |
R13 | 7 10 9 7 9 9 8 |
R15 | 9 12 11 12 9 9 9 |
R16 | 12 13 10 11 12 13 14 |
R17 | 10 12 11 10 10 9 9 |
R18 | 9 8 10 10 9 12 10 |
R19 | 16 17 14 13 13 14 14 |
R20 | 15 18 14 11 13 12 14 |
R21 | 12 11 13 12 11 11 11 |
R22 | 13 12 10 11 11 10 10 |
R23 | 8 9 9 10 10 7 11 |
R24 | 15 13 18 16 17 19 19 |
R26 | 13 35 18 16 20 13 14 |
Table 1.1960.c GPS week : 1960 MJD: 57964.0-57970.0
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 1960 0 | 16 -22 231 -327 -428 -996 84.5 1659 1659 | -1811 0
brd 1960 1 | 51 6 204 -587 512 -1174 83.6 1261 1261 | 1552 0
brd 1960 2 | -56 59 213 1012 -94 -293 83.1 1311 1311 | 2131 0
brd 1960 3 | -25 47 150 -389 -2515 3401 83.0 1348 1348 | -1166 0
brd 1960 4 | -31 15 125 -676 -1654 4655 83.6 1127 1127 | -1060 0
brd 1960 5 | 53 -25 145 -972 210 4398 81.8 1094 1094 | 661 0
brd 1960 6 | 33 41 175 1085 1844 2691 82.4 1175 1175 | -1573 0
-------------+------------------------------------------------------------+----------------
brd 1960 mean| 6 17 178 -122 -303 1811 83.1 1282 1282 | -180 0
brd 1960 sdev| 43 33 39 827 1432 2559 .9 190 190 | 1601 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 2.1960.0 GPS week: 1960 Day: 0 MJD: 57964
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 8 -68 -3 15 .14 34 36 | 9288 -3902 3174 9861
cof n/a| 0 4 8 -30 13 45 .14 32 35 | 9298 -3931 3167 9860
emx n/a| 0 0 7 21 -2 48 .17 22 22 | 7431 -2830 3190 8892
esx n/a| 0 -1 0 41 -1 -44 .13 19 16 | -13450 -1571 3175 11928
gfz n/a| -2 3 0 -31 21 36 .08 26 26 | 0 -4011 3179 9661
grg n/a| 0 1 -11 -37 15 -145 -.43 27 24 | 65 -3694 3174 8713
iac n/a| 0 0 0 5 -5 43 -.11 20 20 | 546 -2216 3187 9049
mcc n/a| -6 -5 25 234 19 -138 .06 119 119 | --- --- --- ---
Table 2.1960.1 GPS week: 1960 Day: 1 MJD: 57965
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 11 -44 2 118 .13 35 36 | 9206 2887 3355 11340
cof n/a| 1 3 12 -73 37 106 .16 41 40 | 9200 2867 3352 11341
emx n/a| -2 -1 6 14 -1 29 .06 21 22 | -2224 1499 3363 10434
esx n/a| 0 -1 0 -32 6 3 .17 20 18 | -4239 1171 3378 13058
gfz n/a| -2 0 -4 -39 69 32 .09 26 24 | 0 2226 3374 11085
grg n/a| 1 0 -5 -74 -8 -240 -.34 33 32 | 165 2865 3367 10387
iac n/a| 0 1 -6 107 -1 39 -.20 23 23 | 2161 672 3372 10348
mcc n/a| 6 3 22 131 -1 54 -.46 111 111 | --- --- --- ---
Table 2.1960.2 GPS week: 1960 Day: 2 MJD: 57966
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 -3 7 -31 16 25 .13 35 34 | 12897 -3057 2849 11140
cof n/a| 0 0 5 -28 10 73 .12 36 34 | 12890 -3057 2856 11141
emx n/a| -1 -3 1 8 -29 55 .11 21 21 | -8363 -1834 2873 10342
esx n/a| 0 0 -1 -25 -5 -14 .19 21 19 | -9846 -4388 2851 13344
gfz n/a| -2 0 -6 -9 26 36 .09 26 20 | 0 -2709 2867 10974
grg n/a| 1 0 0 -37 5 -198 -.45 33 32 | 3473 -2659 2855 10250
iac n/a| 3 1 -3 66 -5 39 -.21 25 24 | 4157 -939 2870 10374
mcc n/a| -1 4 3 -5 -20 238 -.35 106 106 | --- --- --- ---
Table 2.1960.3 GPS week: 1960 Day: 3 MJD: 57967
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 6 -67 -3 69 .13 34 34 | 6704 -2594 2899 10421
cof n/a| 0 1 4 -47 2 33 .12 36 36 | 6696 -2596 2900 10421
emx n/a| -1 -1 3 2 -52 105 .09 21 21 | 3280 -2465 2907 9479
esx n/a| 0 1 -2 -2 32 -40 .24 18 16 | -433 -769 2910 12403
gfz n/a| -2 0 -4 -56 -21 26 .12 27 23 | 0 -2822 2897 10270
grg n/a| 1 0 -3 -15 23 -127 -.37 27 25 | 139 -2326 2904 9916
iac n/a| 1 1 -3 65 1 -7 -.16 19 20 | -634 46 2895 9501
mcc n/a| 1 -5 12 88 -231 874 -.40 112 112 | --- --- --- ---
Table 2.1960.4 GPS week: 1960 Day: 4 MJD: 57968
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 5 8 -15 -11 .07 37 33 | 4551 -1347 2976 10675
cof n/a| -1 0 8 -18 10 32 .16 38 34 | 4559 -1377 2981 10683
emx n/a| -3 0 1 12 -24 75 .09 25 25 | -15724 -1326 2984 10008
esx n/a| 0 0 -4 -1 35 -29 .17 14 14 | 7032 -1214 2974 12658
gfz n/a| 0 0 -6 -48 46 -22 .06 25 25 | 0 -2188 2989 10551
grg n/a| 2 -1 8 -57 25 -161 -.38 30 31 | -410 -1404 2975 10000
iac n/a| 1 1 -3 72 -104 124 -.09 23 24 | 370 -1316 3001 9790
mcc n/a| 7 -2 20 241 -45 222 -.56 107 107 | --- --- --- ---
Table 2.1960.5 GPS week: 1960 Day: 5 MJD: 57969
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 4 14 25 -16 -.02 37 34 | 5464 1272 2705 11424
cof n/a| -4 3 3 53 10 -11 .04 40 36 | 5452 1296 2707 11427
emx n/a| 0 0 3 -36 -40 68 .05 23 23 | -8483 -145 2723 10468
esx n/a| 0 1 -3 10 39 -4 .14 16 15 | -22695 2121 2753 13445
gfz n/a| 0 0 -5 -37 85 20 .22 24 26 | 0 731 2722 11153
grg n/a| -4 0 7 -11 -21 -70 -.35 35 32 | -26 999 2714 11336
iac n/a| 0 0 -3 35 -52 -8 -.18 19 19 | 1705 -336 2725 10473
mcc n/a| 5 -1 17 144 104 24 -.22 127 127 | --- --- --- ---
Table 2.1960.6 GPS week: 1960 Day: 6 MJD: 57970
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 -2 5 -12 20 27 .06 36 34 | 5820 -3638 3246 9761
cof n/a| -3 0 8 -22 50 32 .12 37 34 | 5825 -3651 3251 9761
emx n/a| 0 1 -2 -12 -60 51 .03 25 25 | 5857 -2762 3268 8845
esx n/a| 1 0 -3 8 22 -25 .14 18 15 | -10896 -8159 3253 12143
gfz n/a| 0 -1 -7 -18 19 2 .12 26 18 | 0 -3575 3261 9619
grg n/a| 0 0 9 -20 20 -112 -.35 30 26 | 185 -3569 3240 8648
iac n/a| 2 -1 -2 52 7 78 -.10 21 21 | 863 -2285 3256 8896
mcc n/a| -3 -14 21 181 91 20 -.02 159 159 | --- --- --- ---
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 3.1960.0 GPS week: 1960 Day: 0 MJD: 57964
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 | 1024 57 27 22 42 22 36 12 --- 15 | 85 80 51 32 37 64 40 --- 42
R02 | 718 31 34 26 16 29 18 23 134 10 | 76 77 66 42 35 53 40 41 48
R03 | 1398 16 16 24 13 28 28 22 144 10 | 73 73 68 64 48 67 54 30 60
R04 | 836 21 17 15 8 12 22 11 --- 6 | 71 65 62 52 53 53 44 --- 53
R05 | 965 36 20 26 31 15 40 19 --- 13 | 73 69 60 68 49 57 46 --- 57
R06 | 1121 23 20 15 25 16 43 23 --- 11 | 38 39 34 53 45 25 44 --- 37
R07 | 543 27 31 24 10 34 13 22 108 9 | 73 74 64 56 43 55 35 103 52
R08 | 563 19 15 16 12 16 12 18 --- 7 | 76 76 69 58 61 58 50 --- 59
R09E | 3592 13 12 21 11 21 19 13 --- 7 | 47 45 50 42 43 42 45 --- 43
R10E | 843 19 16 15 12 16 17 11 --- 6 | 82 81 75 77 71 78 81 --- 76
R11E | 702 13 15 19 9 20 25 17 65 8 | 70 72 71 67 66 76 64 78 67
R13E | 2094 15 14 13 17 21 19 11 --- 7 | 131 133 122 137 118 137 131 --- 129
R15E | 4854 21 25 20 13 25 20 17 --- 8 | 53 57 43 47 49 49 52 --- 46
R16E | 2220 23 37 26 28 28 28 26 --- 12 | 84 104 78 93 93 95 86 --- 86
R17 | 671 41 41 17 10 29 18 16 --- 9 | 72 73 50 48 34 47 34 --- 44
R18 | 813 34 33 14 13 27 25 14 --- 9 | 59 61 40 46 26 40 31 --- 37
R19 | 939 73 77 27 23 37 18 29 --- 15 | 88 94 59 63 44 60 43 --- 53
R20 | 1106 53 50 35 17 29 41 24 --- 14 | 87 84 50 48 32 59 33 --- 44
R21 | 697 43 37 24 14 32 25 23 129 11 | 81 80 59 57 45 58 45 104 54
R22 | 555 48 47 27 10 39 21 30 --- 13 | 79 78 57 50 41 61 37 --- 49
R23 | 700 10 15 17 22 11 22 12 --- 7 | 34 36 35 50 37 35 37 --- 36
R24 | 1428 26 23 26 30 37 40 32 --- 14 | 38 49 34 61 43 50 38 --- 37
XR26 | ---- 18 93 --- --- --- --- 9 --- 13 | 35 89 --- --- --- --- 20 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1659 34 32 22 19 26 27 20 119 |T 69 73 58 59 50 59 49 71 53
WRMS | 1659 36 35 22 16 26 24 20 119 |NE 66 70 53 53 42 52 39 69 46
MEDI | 843 23 25 21 13 25 22 18 129 |MD 73 74 59 53 44 57 44 78 49
Table 3.1960.1 GPS week: 1960 Day: 1 MJD: 57965
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 | 741 55 83 19 29 26 17 19 --- 12 | 64 89 42 40 40 33 31 --- 34
R02 | 568 35 37 29 15 13 26 26 123 11 | 54 54 47 35 37 21 18 19 31
R03 | 925 24 28 22 7 19 18 23 126 8 | 48 53 44 35 33 39 34 23 36
R04 | 602 18 22 17 6 23 19 23 --- 8 | 45 50 49 43 33 50 29 --- 40
R05 | 669 34 49 26 16 19 32 29 --- 11 | 47 59 48 44 45 49 24 --- 39
R06 | 800 22 29 19 35 11 38 18 --- 11 | 27 28 38 54 29 16 28 --- 32
R07 | 597 33 33 16 9 22 14 24 78 8 | 54 54 41 38 40 44 23 70 36
R08 | 581 22 30 23 8 21 31 15 --- 9 | 52 63 52 42 36 38 31 --- 39
R09E | 3118 20 12 24 13 19 53 20 --- 11 | 84 94 97 92 95 92 95 --- 91
R10E | 835 25 20 15 19 26 14 46 --- 11 | 98 99 96 100 94 95 110 --- 97
R11E | 908 18 15 18 12 19 17 14 105 7 | 96 96 90 95 84 94 106 85 94
R13E | 1793 12 13 17 21 22 44 13 --- 10 | 109 109 104 110 102 123 110 --- 108
R15E | 2140 29 40 24 30 22 29 20 --- 11 | 102 109 99 112 101 121 110 --- 106
R16E | 2242 22 37 25 21 24 49 23 --- 12 | 69 84 58 64 62 74 57 --- 57
R17 | 654 46 48 21 11 38 16 18 --- 11 | 41 41 28 23 27 28 21 --- 23
R18 | 671 28 27 12 12 29 15 16 --- 8 | 35 33 28 31 23 33 22 --- 26
R19 | 777 63 67 31 29 53 28 19 --- 16 | 46 53 33 39 37 41 27 --- 30
R20 | 1202 61 67 27 28 29 73 22 --- 18 | 62 70 32 42 38 49 25 --- 31
R21 | 920 44 49 18 11 26 22 23 115 10 | 52 58 38 45 38 45 38 79 39
R22 | 613 48 44 22 12 35 24 25 --- 12 | 44 41 31 27 26 42 25 --- 28
R23 | 633 9 12 14 27 19 29 14 --- 9 | 21 24 20 30 19 25 22 --- 19
R24 | 1571 33 44 19 21 24 50 32 --- 13 | 38 56 27 44 43 31 23 --- 28
XR26 | ---- 42 195 --- --- --- --- 28 --- 34 | 60 177 --- --- --- --- 21 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1260 35 41 21 20 26 33 23 111 |T 58 69 51 53 49 53 44 55 47
WRMS | 1260 36 40 22 18 24 32 23 111 |NE 46 59 37 38 34 36 26 47 31
MEDI | 777 29 37 19 15 22 26 22 115 |MD 52 58 42 42 38 42 28 70 36
Table 3.1960.2 GPS week: 1960 Day: 2 MJD: 57966
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 | 563 71 65 20 21 40 35 34 --- 16 | 83 79 49 37 31 57 32 --- 40
R02 | 727 32 34 28 21 25 21 22 146 11 | 63 67 56 46 41 40 36 49 44
R03 | 854 18 21 25 19 16 29 16 115 9 | 59 55 57 49 43 37 57 29 49
R04 | 718 27 26 20 13 20 23 13 --- 8 | 63 57 47 46 45 66 43 --- 48
R05 | 583 36 41 22 28 26 34 37 --- 13 | 59 63 41 59 34 42 35 --- 39
R06 | 799 27 29 21 23 21 33 27 --- 11 | 33 39 41 40 29 25 44 --- 31
R07 | 668 21 26 11 13 18 16 15 70 7 | 65 65 54 66 55 60 51 35 57
R08 | 713 22 16 10 16 21 19 28 --- 8 | 70 65 58 63 49 70 44 --- 57
R09E | 3605 29 29 31 18 22 36 26 --- 12 | 92 102 116 99 106 84 106 --- 100
R10E | 1338 21 20 25 25 20 45 40 --- 13 | 96 107 101 107 101 116 69 --- 95
R11E | 1700 12 16 15 14 16 32 27 94 9 | 68 71 63 73 66 83 62 76 67
R13E | 887 19 16 16 22 18 30 14 --- 9 | 71 70 58 83 60 76 65 --- 68
R15E | 1437 21 15 17 27 22 36 25 --- 11 | 87 85 91 98 105 105 111 --- 98
R16E | 2047 23 28 17 19 23 29 27 --- 10 | 76 71 59 67 67 60 68 --- 62
R17 | 830 44 47 23 10 27 14 23 --- 10 | 63 66 53 49 35 45 36 --- 45
R18 | 545 35 33 16 20 22 17 20 --- 9 | 52 54 40 56 37 28 27 --- 38
R19 | 747 53 44 29 18 45 27 19 --- 14 | 58 54 47 40 27 46 34 --- 39
R20 | 1590 52 78 20 19 36 40 16 --- 13 | 60 79 31 35 27 35 26 --- 27
R21 | 801 41 41 16 16 33 45 25 90 12 | 70 69 57 56 54 68 53 70 55
R22 | 749 41 47 10 10 22 27 24 --- 10 | 66 72 53 52 53 69 43 --- 53
R23 | 823 12 17 20 24 16 30 14 --- 9 | 32 36 37 44 40 43 33 --- 35
R24 | 1757 37 23 28 41 38 65 25 --- 17 | 34 42 35 63 43 45 33 --- 35
XR26 | ---- 21 88 --- --- --- --- 15 --- 18 | 23 104 --- --- --- --- 29 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1310 35 36 21 21 26 33 25 106 |T 62 68 56 60 52 59 49 51 52
WRMS | 1310 34 34 21 19 20 32 24 106 |NE 56 62 47 50 40 48 38 45 42
MEDI | 801 27 29 20 19 22 30 24 94 |MD 63 67 53 56 43 57 43 49 48
Table 3.1960.3 GPS week: 1960 Day: 3 MJD: 57967
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 | 596 63 68 23 8 23 37 25 --- 13 | 69 73 25 34 31 50 21 --- 29
R02 | 910 37 39 24 12 22 17 23 175 9 | 63 64 46 37 22 41 22 93 35
R03 | 1026 22 27 28 12 31 13 19 116 9 | 56 62 56 40 40 47 34 28 42
R04 | 630 26 35 19 10 20 8 15 --- 7 | 50 57 47 36 26 34 27 --- 34
R05 | 545 53 46 25 22 28 32 29 --- 13 | 57 51 49 37 48 46 35 --- 38
R06 | 895 30 43 14 21 18 23 24 --- 9 | 17 23 40 41 38 20 39 --- 30
R07 | 1358 28 23 21 18 26 24 13 84 9 | 61 58 56 39 41 58 40 60 45
R08 | 527 19 26 10 12 16 18 12 --- 6 | 56 63 46 52 36 36 36 --- 43
R09E | 3586 18 19 19 18 27 31 16 --- 9 | 53 51 50 60 55 58 58 --- 53
R10E | 1345 24 20 21 16 17 18 14 --- 8 | 76 69 62 78 69 70 75 --- 70
R11E | 1000 18 19 13 10 19 19 10 56 6 | 86 84 73 82 74 84 80 123 79
R13E | 1402 17 20 13 16 17 17 7 --- 6 | 62 64 63 67 57 61 57 --- 61
R15E | 2174 18 32 24 29 25 39 15 --- 11 | 67 74 65 65 52 77 60 --- 63
R16E | 1675 27 33 18 18 24 37 21 --- 10 | 77 84 58 67 62 47 64 --- 60
R17 | 640 40 42 21 10 34 20 19 --- 10 | 58 61 41 41 23 35 26 --- 34
R18 | 596 34 39 19 16 30 15 19 --- 9 | 52 57 39 36 21 27 28 --- 31
R19 | 627 50 54 22 20 36 32 23 --- 13 | 70 76 43 40 31 62 30 --- 41
R20 | 1865 26 26 23 20 28 32 21 --- 11 | 41 46 42 42 32 31 27 --- 31
R21 | 696 42 43 22 14 39 21 25 90 11 | 57 57 40 37 24 40 28 36 32
R22 | 641 45 41 18 12 40 21 18 --- 11 | 68 64 45 36 26 48 32 --- 37
R23 | 1353 16 13 25 28 10 15 16 --- 9 | 29 35 27 57 37 36 40 --- 37
R24 | 1251 34 32 26 24 38 61 25 --- 15 | 51 52 34 50 32 38 34 --- 35
XR26 | ---- 22 63 --- --- --- --- 11 --- 15 | 22 69 --- --- --- --- 32 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1347 34 36 21 18 27 27 19 111 |T 56 60 47 48 39 47 40 68 42
WRMS | 1347 34 36 21 16 23 25 20 111 |NE 51 56 42 40 31 40 31 54 35
MEDI | 910 27 33 21 16 25 21 19 90 |MD 57 62 46 41 36 46 34 60 37
Table 3.1960.4 GPS week: 1960 Day: 4 MJD: 57968
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 | 670 71 59 38 10 20 32 22 --- 14 | 83 81 43 39 44 63 40 --- 42
R02 | 497 45 41 24 12 21 20 26 111 10 | 68 65 49 37 34 53 26 70 39
R03 | 1109 33 29 27 13 33 21 26 116 11 | 62 60 56 46 49 52 37 37 44
R04 | 580 35 27 27 12 11 31 20 --- 10 | 59 49 53 45 44 64 27 --- 44
R05 | 1432 46 53 27 11 20 51 39 --- 14 | 56 62 52 56 48 59 29 --- 47
R06 | 824 27 24 19 24 13 25 14 --- 9 | 29 34 28 45 35 19 27 --- 30
R07 | 1567 27 32 22 10 30 26 28 132 10 | 58 62 49 46 39 58 33 38 42
R08 | 818 26 26 16 16 19 29 7 --- 8 | 64 66 59 44 49 74 52 --- 53
R09E | 2146 13 17 14 8 16 28 16 --- 7 | 29 32 35 31 37 42 36 --- 32
R10E | 759 14 21 20 15 17 43 12 --- 9 | 60 67 55 60 52 48 57 --- 54
R11E | 720 20 26 12 8 20 17 12 100 6 | 52 58 42 45 35 47 41 94 42
R13E | 1502 22 18 21 17 15 21 22 --- 8 | 62 58 49 63 51 60 61 --- 56
R15E | 2002 25 24 19 16 20 21 22 --- 9 | 63 67 55 58 63 58 53 --- 56
R16E | 998 23 29 35 24 23 31 22 --- 12 | 58 61 45 67 56 40 57 --- 52
R17 | 621 37 34 22 8 34 17 23 --- 10 | 54 52 46 37 32 50 28 --- 37
R18 | 840 24 27 19 11 37 19 15 --- 9 | 41 44 41 41 30 35 35 --- 35
R19 | 882 58 65 27 8 38 20 30 --- 12 | 70 69 47 40 26 43 30 --- 38
R20 | 1293 36 19 22 14 34 39 30 --- 12 | 43 51 41 42 42 31 22 --- 31
R21 | 706 50 58 28 11 28 15 23 67 11 | 64 73 44 57 41 46 41 71 46
R22 | 624 47 48 17 12 35 18 17 --- 10 | 59 61 47 49 48 50 43 --- 46
R23 | 1190 11 18 30 16 19 21 25 --- 9 | 33 30 39 44 45 45 32 --- 38
R24 | 1000 49 61 44 21 26 65 25 --- 17 | 54 81 43 54 51 36 31 --- 41
XR26 | ---- 26 96 --- --- --- --- 14 --- 19 | 47 70 --- --- --- --- 31 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1127 37 38 25 14 25 30 23 107 |T 55 58 46 47 43 48 37 62 42
WRMS | 1127 33 34 25 14 25 31 24 107 |NE 55 59 46 45 41 48 33 54 40
MEDI | 840 27 29 22 12 20 21 22 111 |MD 58 61 46 45 44 48 35 70 42
Table 3.1960.5 GPS week: 1960 Day: 5 MJD: 57969
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 | 713 76 83 16 21 27 54 25 --- 15 | 73 77 50 36 36 68 36 --- 39
R02 | 525 39 45 28 18 20 18 25 98 11 | 59 62 53 32 36 48 30 41 38
R03 | 1144 33 38 22 6 19 21 28 111 9 | 56 60 42 39 30 46 37 29 38
R04 | 959 34 44 17 9 19 11 18 --- 8 | 48 52 43 42 44 36 40 --- 40
R05 | 968 42 36 24 17 31 53 17 --- 13 | 78 80 70 64 73 80 70 --- 67
R06 | 1294 23 23 21 20 18 36 11 --- 9 | 31 31 25 35 35 30 27 --- 27
R07 | 1315 34 29 28 8 31 20 19 151 10 | 50 46 47 34 39 34 24 54 32
R08 | 548 25 27 12 12 20 16 17 --- 7 | 57 59 47 51 46 44 42 --- 46
R09E | 2647 15 15 13 9 13 23 17 --- 6 | 28 27 26 31 35 18 34 --- 26
R10E | 745 11 12 15 16 14 19 11 --- 6 | 40 39 40 47 40 35 36 --- 40
R11E | 561 17 15 14 11 13 18 19 173 6 | 80 78 79 80 83 74 91 88 81
R13E | 1017 19 22 18 14 15 37 11 --- 8 | 66 69 55 60 57 63 59 --- 57
R15E | 1205 25 25 20 20 20 24 15 --- 9 | 54 55 56 58 51 59 58 --- 55
R16E | 1225 26 35 27 26 27 33 27 --- 12 | 60 64 53 66 56 57 56 --- 54
R17 | 829 36 40 15 9 23 18 19 --- 8 | 43 45 34 39 33 35 37 --- 34
R18 | 702 21 16 14 29 28 42 18 --- 11 | 32 27 26 42 32 28 27 --- 27
R19 | 834 63 66 34 15 41 14 21 --- 14 | 58 63 53 37 20 37 31 --- 36
R20 | 955 36 54 30 21 26 42 16 --- 12 | 33 49 25 38 25 32 27 --- 24
R21 | 572 49 51 15 8 33 18 21 81 10 | 57 58 38 40 36 41 34 72 37
R22 | 872 50 52 14 9 28 20 16 --- 9 | 52 57 41 47 37 30 35 --- 38
R23 | 1399 13 20 11 16 19 19 10 --- 6 | 41 49 35 40 36 46 45 --- 38
R24 | 984 43 46 49 16 25 92 15 --- 19 | 60 64 36 48 50 43 36 --- 38
XR26 | ---- 18 97 --- --- --- --- 9 --- 12 | 20 122 --- --- --- --- 36 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1094 37 40 23 16 24 35 19 127 |T 51 57 44 45 42 44 41 56 40
WRMS | 1094 34 36 23 15 26 32 19 127 |NE 49 58 41 41 38 42 36 49 37
MEDI | 955 33 36 17 15 20 20 17 111 |MD 54 58 42 40 36 41 36 54 38
Table 3.1960.6 GPS week: 1960 Day: 6 MJD: 57970
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 | 904 73 70 27 18 45 36 34 --- 16 | 95 92 56 37 39 72 38 --- 44
R02 | 602 38 37 34 10 19 17 31 99 11 | 83 79 75 43 41 56 29 39 49
R03 | 2013 33 35 24 14 22 20 21 111 9 | 79 78 62 53 40 55 42 31 52
R04 | 770 34 29 16 7 16 11 23 --- 8 | 69 67 57 54 51 58 45 --- 53
R05 | 724 42 35 19 28 23 34 19 --- 12 | 94 87 87 72 80 85 78 --- 78
R06 | 967 20 23 15 28 12 25 18 --- 9 | 36 34 30 55 39 26 40 --- 37
R07 | 1186 33 39 23 10 27 14 14 170 8 | 73 78 54 49 43 51 37 84 47
R08 | 538 29 33 21 10 31 20 30 --- 10 | 71 74 56 51 44 58 42 --- 50
R09E | 2861 14 23 14 11 18 19 15 --- 6 | 47 56 51 47 54 51 59 --- 50
R10E | 810 15 15 23 19 11 19 13 --- 8 | 65 69 58 75 60 64 67 --- 65
R11E | 726 21 22 15 13 21 29 11 262 8 | 99 100 91 99 97 84 97 102 94
R13E | 1113 22 19 18 15 17 24 15 --- 8 | 79 80 64 78 63 72 73 --- 71
R15E | 1409 21 21 14 20 21 20 17 --- 8 | 70 70 62 67 60 67 63 --- 63
R16E | 1598 21 36 37 23 36 37 25 --- 13 | 77 82 62 82 66 71 74 --- 69
R17 | 787 44 44 19 10 24 12 14 --- 9 | 74 73 49 51 42 46 44 --- 47
R18 | 1149 25 22 26 15 17 23 20 --- 9 | 56 56 45 53 40 39 40 --- 43
R19 | 902 59 55 24 26 26 24 29 --- 13 | 90 91 65 56 46 54 42 --- 53
R20 | 855 43 45 33 22 34 44 15 --- 14 | 67 68 35 53 33 44 34 --- 38
R21 | 643 41 44 24 9 34 21 22 80 11 | 78 79 57 58 43 51 44 99 52
R22 | 787 46 46 15 13 29 17 20 --- 10 | 78 79 57 55 43 57 44 --- 52
R23 | 1097 13 21 17 20 29 42 16 --- 10 | 44 53 40 49 38 48 45 --- 42
R24 | 712 31 46 51 25 32 77 18 --- 19 | 58 78 52 62 51 36 43 --- 45
XR26 | ---- 21 61 --- --- --- --- 7 --- 13 | 25 68 --- --- --- --- 31 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1175 36 37 25 18 26 30 21 158 |T 69 73 57 59 50 56 50 71 53
WRMS | 1175 34 34 25 15 18 26 21 158 |NE 68 72 54 53 44 52 42 63 47
MEDI | 855 31 35 21 15 23 21 18 111 |MD 73 78 57 54 43 55 44 84 50
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