[IGSREPORT-25411] Wk 1957 IGLOS Final Orbits
acc
acc at igs.org
Fri Jul 28 06:18:00 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1957 (Jul 09, 2017 - Jul 15, 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 2.1957.
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:
igl1957[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1957 in the SP3 format.
igl19577.sum Combination Report for GPS Week 1957.
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 | -6.1 ns
1 | 0.7 ns
2 | -2.6 ns
3 | -2.7 ns
4 | -4.6 ns
5 | 7.4 ns
6 | 8.6 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 1.1957, 1a.1957).
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 2.1957.0-6)
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 3.1957.0-6).
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 1957 summary. (Jul 09, 2017 - Jul 15, 2017)
Table 1.1957.a GPS week : 1957 MJD: 57943.0-57949.0
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 1 -1 -28 -2 22 .12 31 31 | -6624 794 3389 11049
| 1 0 1 21 13 16 .03 | 8654 1278
cof n/a| 0 1 -3 -16 9 28 .14 35 33 | -6615 778 3388 11048
| 1 1 2 13 16 34 .06 | 8657 1267
emx n/a| -1 0 7 2 -28 72 .06 20 20 | -1565 328 3403 10300
| 0 1 3 19 23 34 .05 | 16130 1137
esx n/a| 0 0 0 35 28 -26 .13 18 16 | -2432 -346 3405 12841
| 0 1 1 15 12 19 .04 | 12746 1189
gfz n/a| 0 0 3 -11 60 11 .02 21 17 | 0 958 3404 10637
| 1 0 1 15 19 22 .05 | 0 1152
grg n/a| 0 0 -2 -63 16 -43 -.40 30 27 | -628 1091 3399 10156
| 2 1 5 25 20 72 .07 | 5689 1246
iac n/a| 1 0 -4 14 -46 -31 -.05 18 18 | 470 -631 3806 11154
| 0 0 1 23 36 31 .02 | 6147 763
mcc n/a| 4 1 -13 54 -28 221 -.22 141 141 | --- --- --- ---
| 5 9 18 47 103 666 .43 | --- ---
Table 1.1957.b GPS week : 1957 MJD: 57943.0-57949.0
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 | 7 8 13 9 9 10 11 |
R02 | 7 7 8 7 6 8 7 |
R03 | 6 6 6 6 5 6 6 |
R04 | 7 6 8 6 7 5 6 |
R05 | 13 15 16 14 14 13 14 |
R06 | 10 7 8 8 9 12 8 |
R07 | 7 7 6 6 5 6 7 |
R08 | 7 7 7 6 7 7 6 |
R09 | 7 8 8 8 8 8 12 |
R10 | 9 8 8 9 8 9 8 |
R11 | 7 7 7 6 7 7 9 |
R13 | 8 7 8 9 7 8 9 |
R15 | 8 10 8 7 10 9 8 |
R16 | 14 11 12 14 12 12 9 |
R17 | 10 8 10 11 10 10 11 |
R18 | 9 8 9 7 9 8 9 |
R19 | 15 16 15 15 13 15 17 |
R20 | 13 13 16 17 18 17 17 |
R21 | 11 10 11 12 11 11 12 |
R22 | 11 12 11 11 12 10 11 |
R23 | 8 10 9 11 11 9 9 |
R24 | 14 16 14 13 13 17 14 |
R26 | 17 18 18 15 15 18 22 |
Table 1.1957.c GPS week : 1957 MJD: 57943.0-57949.0
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 1957 0 | -29 17 90 274 -1721 4359 83.7 1451 1451 | -6081 0
brd 1957 1 | 78 -73 190 149 -495 2197 81.0 1077 1077 | 732 0
brd 1957 2 | -20 22 139 65 -385 3257 83.0 1532 1532 | -2617 0
brd 1957 3 | -8 -10 97 -137 192 2880 84.1 1504 1504 | -2686 0
brd 1957 4 | -14 -3 223 138 -378 954 84.2 1224 1224 | -4590 0
brd 1957 5 | 34 -2 191 282 -1185 -607 83.6 1314 1314 | 7428 0
brd 1957 6 | -11 4 259 -21 -837 -166 85.3 1239 1239 | 8561 0
-------------+------------------------------------------------------------+----------------
brd 1957 mean| 4 -6 169 107 -687 1839 83.6 1334 1334 | 106 0
brd 1957 sdev| 38 31 63 152 624 1842 1.3 168 168 | 5788 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 2.1957.0 GPS week: 1957 Day: 0 MJD: 57943
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 2 -2 -2 .14 31 33 | -16596 386 2721 9807
cof n/a| 0 0 0 -8 17 17 .05 34 36 | -16586 358 2725 9803
emx n/a| -1 0 13 -3 -28 78 .15 21 21 | -12415 -3 2737 8882
esx n/a| 0 1 -3 49 29 -29 .08 17 16 | -16609 -583 2729 11583
gfz n/a| 3 -2 5 -3 70 20 -.00 22 21 | 0 181 2740 9435
grg n/a| -2 0 -11 -11 -9 -57 -.32 26 23 | -6411 647 2721 9213
iac n/a| 0 -1 -2 -17 -44 -31 -.01 17 17 | -5519 354 2743 8983
mcc n/a| 6 -3 -12 -20 -75 1667 .43 167 167 | --- --- --- ---
Table 2.1957.1 GPS week: 1957 Day: 1 MJD: 57944
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 -47 10 24 .08 32 31 | -12045 2223 3102 11934
cof n/a| 0 3 -5 -28 7 -11 .08 33 31 | -12027 2190 3109 11941
emx n/a| 0 0 8 0 -42 20 .00 19 20 | -9104 1683 3116 11092
esx n/a| -1 -1 0 21 34 -30 .19 17 16 | 10633 702 3126 13047
gfz n/a| 1 0 3 -13 73 22 .02 21 14 | 0 2724 3128 11368
grg n/a| -4 0 -4 -76 11 74 -.49 28 25 | -1588 2447 3111 10942
iac n/a| 0 0 -3 46 -58 -28 -.04 19 20 | -4195 -1666 5902 17996
mcc n/a| 9 -14 -24 77 61 -5 -.13 127 127 | --- --- --- ---
Table 2.1957.2 GPS week: 1957 Day: 2 MJD: 57945
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 -14 -16 27 .11 30 32 | -11470 1451 2955 11615
cof n/a| 0 0 -5 -7 33 13 .14 35 34 | -11471 1438 2962 11612
emx n/a| -1 1 6 8 -19 90 .04 21 21 | 20659 323 2960 10804
esx n/a| 0 0 2 23 51 -59 .15 17 15 | -13258 -861 2961 13652
gfz n/a| 2 0 4 -19 38 -5 .04 21 18 | 0 630 2933 11151
grg n/a| -1 0 -2 -80 28 -13 -.47 32 28 | -3227 1018 2967 10825
iac n/a| 1 -1 -6 14 -53 -1 -.07 18 18 | -1285 -986 2964 10590
mcc n/a| 5 4 -19 117 30 24 -.98 123 123 | --- --- --- ---
Table 2.1957.3 GPS week: 1957 Day: 3 MJD: 57946
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 -8 -12 46 .11 30 31 | -9091 1474 3556 11198
cof n/a| 2 0 -3 5 -10 45 .15 35 34 | -9090 1478 3551 11195
emx n/a| -1 0 7 0 -46 43 .02 20 20 | -18876 1210 3582 10736
esx n/a| 0 1 2 19 20 2 .10 21 16 | 7298 1040 3572 13137
gfz n/a| 0 -1 5 17 29 10 .10 20 16 | 0 1520 3604 10922
grg n/a| 0 -1 -4 -57 16 -23 -.33 27 25 | -3761 2141 3568 10467
iac n/a| 2 -1 -5 14 14 -76 -.02 18 18 | -1337 145 3576 10253
mcc n/a| 9 3 -20 24 91 -66 -.07 137 137 | --- --- --- ---
Table 2.1957.4 GPS week: 1957 Day: 4 MJD: 57947
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 -34 -18 28 .11 33 33 | -7923 -1428 4142 11762
cof n/a| 0 2 0 -33 -1 49 .12 38 35 | -7922 -1417 4133 11751
emx n/a| -1 0 9 -12 -63 54 .02 20 20 | -14087 -1489 4154 11110
esx n/a| 0 0 0 30 22 -22 .10 18 16 | -16637 -2114 4154 14195
gfz n/a| -1 0 2 -27 54 -4 .03 23 16 | 0 -617 4162 10943
grg n/a| -2 2 -4 -71 35 -28 -.37 30 31 | -4280 -948 4155 10626
iac n/a| 2 0 -6 32 -15 -43 -.06 16 16 | -2767 -1142 4154 10966
mcc n/a| -5 2 -35 96 -2 -215 -.31 155 155 | --- --- --- ---
Table 2.1957.5 GPS week: 1957 Day: 5 MJD: 57948
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -3 -53 11 6 .16 31 29 | 4592 -208 3504 10301
cof n/a| -1 0 -2 -27 23 -1 .20 37 30 | 4607 -226 3496 10298
emx n/a| -2 2 3 -20 0 104 .06 20 20 | 18447 -644 3511 9519
esx n/a| 0 -1 1 47 15 -37 .11 17 14 | 11013 -1311 3515 11922
gfz n/a| 0 0 3 -11 73 -15 -.07 21 20 | 0 334 3508 10130
grg n/a| 1 -1 2 -89 41 -100 -.37 33 29 | 7392 165 3512 9174
iac n/a| 1 0 -6 24 -91 15 -.06 19 19 | 9227 -1042 3524 9421
mcc n/a| 6 1 21 22 -196 -217 -.04 154 154 | --- --- --- ---
Table 2.1957.6 GPS week: 1957 Day: 6 MJD: 57949
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 -3 -46 10 28 .14 32 27 | 6163 1664 3743 10732
cof n/a| 0 2 -3 -18 -3 87 .21 35 28 | 6179 1627 3746 10740
emx n/a| 0 0 4 41 -1 115 .09 19 19 | 4418 1219 3763 9959
esx n/a| 0 0 0 58 21 -9 .16 20 17 | 536 700 3780 12356
gfz n/a| -1 0 1 -25 80 49 -.02 20 18 | 0 1935 3756 10512
grg n/a| 2 0 4 -56 -8 -155 -.44 31 26 | 7474 2167 3762 9850
iac n/a| 2 0 -4 -13 -79 -54 -.07 21 21 | 9166 -86 3781 9872
mcc n/a| 0 17 -3 61 -109 363 -.47 124 124 | --- --- --- ---
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 3.1957.0 GPS week: 1957 Day: 0 MJD: 57943
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 | 1152 14 19 17 20 16 12 12 --- 7 | 59 61 53 44 60 62 55 --- 52
R02 | 748 11 17 18 14 10 16 16 275 6 | 58 59 61 51 54 46 41 279 50
R03 | 517 8 8 15 11 10 14 17 96 6 | 54 54 59 58 54 47 47 98 52
R04 | 656 9 12 16 19 10 13 14 --- 6 | 54 53 59 51 48 41 54 --- 50
R05 | 737 37 41 22 20 21 46 24 --- 12 | 55 50 67 56 61 43 58 --- 54
R06 | 1932 22 19 23 28 27 19 14 --- 10 | 31 31 35 42 38 33 29 --- 30
R07 | 790 13 14 15 9 21 14 13 162 6 | 62 60 67 61 61 60 60 95 60
R08 | 1242 6 8 8 9 14 29 13 --- 6 | 48 52 52 47 55 53 51 --- 49
R09E | 3543 11 14 19 6 12 24 18 --- 7 | 46 47 51 53 52 55 52 --- 50
R10E | 1615 18 18 17 14 21 28 16 --- 8 | 40 41 39 39 35 44 32 --- 35
R11E | 914 10 17 16 15 15 21 11 115 6 | 35 37 36 39 41 37 34 110 36
R13E | 2118 24 16 15 13 12 26 16 --- 8 | 71 68 67 64 61 64 57 --- 62
R15E | 2852 18 23 22 18 18 17 11 --- 7 | 40 44 42 36 37 39 37 --- 36
R16E | 853 16 20 42 17 30 49 23 --- 14 | 38 45 37 44 50 31 34 --- 34
R17 | 1014 44 47 19 13 25 18 16 --- 10 | 85 88 52 53 40 51 43 --- 50
R18 | 576 39 39 19 11 24 16 10 --- 9 | 93 95 70 76 62 75 68 --- 72
R19 | 853 73 83 21 13 37 25 25 --- 15 | 107 113 51 43 32 60 35 --- 47
R20 | 1392 45 58 24 21 22 34 24 --- 12 | 91 104 54 72 58 71 63 --- 63
R21 | 999 41 47 26 16 30 15 14 127 10 | 81 84 52 48 32 47 45 88 47
R22 | 708 54 50 19 14 24 19 10 --- 11 | 81 80 41 40 29 45 38 --- 41
R23 | 581 20 19 19 17 10 28 14 --- 8 | 47 46 45 66 50 44 62 --- 51
R24 | 1438 30 25 27 31 34 39 22 --- 13 | 59 63 70 76 59 56 64 --- 61
XR26 | ---- 23 149 --- --- --- --- 12 --- 16 | 33 97 --- --- --- --- 35 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1450 31 34 21 17 22 26 17 167 |T 59 64 52 52 48 50 47 134 48
WRMS | 1450 33 36 21 16 21 23 17 167 |NE 64 70 55 55 49 52 49 140 50
MEDI | 914 20 19 19 14 21 19 14 127 |MD 55 59 52 51 50 47 47 98 50
Table 3.1957.1 GPS week: 1957 Day: 1 MJD: 57944
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 | 878 14 22 22 10 13 22 17 --- 7 | 44 54 44 49 51 34 35 --- 40
R02 | 547 15 13 14 12 10 18 22 205 7 | 41 39 42 40 39 31 24 184 35
XR03 | ---- 10 11 8 13 11 --- 14 115 6 | 38 39 41 41 39 --- 28 31 36
R04 | ---- 8 12 10 14 7 25 9 --- 6 | 35 30 34 42 36 20 32 --- 33
R05 | 536 43 37 26 18 30 55 29 --- 14 | 30 36 38 37 54 47 48 --- 38
R06 | 1722 12 15 11 17 18 23 14 --- 7 | 19 25 24 37 30 32 24 --- 24
R07 | 1025 19 15 10 15 14 17 15 109 6 | 40 43 49 60 57 38 43 72 48
R08 | 812 6 15 6 18 12 28 18 --- 7 | 35 35 37 32 32 48 36 --- 32
R09E | ---- 14 13 16 13 18 26 12 --- 7 | 31 37 39 41 39 45 45 --- 37
R10E | ---- 13 17 20 12 13 25 17 --- 7 | 36 37 39 37 37 41 29 --- 33
R11E | 1628 11 21 13 17 16 18 11 76 6 | 21 25 25 27 25 20 21 90 20
R13E | ---- 13 14 15 13 11 18 18 --- 6 | 57 56 57 57 56 73 54 --- 56
R15E | ---- 24 26 20 25 21 20 19 --- 9 | 38 41 36 35 37 36 36 --- 32
R16E | ---- 26 39 23 20 28 23 25 --- 10 | 24 45 40 29 39 22 33 --- 26
R17 | ---- 34 32 20 7 21 12 13 --- 8 | 49 47 37 38 35 39 33 --- 35
R18 | ---- 32 39 13 11 22 14 10 --- 7 | 60 65 51 49 43 51 47 --- 48
R19 | ---- 79 79 25 13 38 29 27 --- 16 | 77 76 39 32 25 38 31 --- 32
R20 | ---- 49 45 24 18 29 31 29 --- 13 | 69 66 60 66 55 52 48 --- 54
R21 | ---- 43 42 17 11 25 23 18 67 10 | 54 55 39 37 29 37 33 79 35
R22 | 770 53 58 17 19 32 17 15 --- 11 | 52 57 30 38 30 31 30 --- 31
R23 | ---- 15 14 28 26 11 19 17 --- 9 | 37 45 37 55 47 37 47 --- 43
R24 | ---- 31 29 28 27 27 65 30 --- 15 | 50 63 49 65 58 49 60 --- 52
XR26 | 5219 22 52 --- --- --- --- 13 --- 17 | 19 54 --- --- --- --- 28 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS | 1077 32 33 19 17 21 28 19 126 |T 41 46 40 42 40 39 36 91 36
WRMS | 1077 31 31 20 16 14 25 20 126 |NE 44 48 40 44 41 38 36 91 37
MEDI | 878 19 22 17 14 18 23 17 109 |MD 38 45 39 38 39 38 33 79 35
Table 3.1957.2 GPS week: 1957 Day: 2 MJD: 57945
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 | 1225 17 22 41 16 15 44 28 --- 12 | 51 50 29 39 48 71 51 --- 41
R02 | 698 16 21 13 21 9 30 14 164 7 | 50 56 46 60 50 47 39 103 47
R03 | 669 10 9 13 11 11 23 12 116 6 | 50 53 51 59 63 50 51 39 53
R04 | 552 9 12 14 11 13 32 18 --- 7 | 47 50 51 51 47 71 41 --- 48
R05 | 1073 44 45 32 23 24 64 23 --- 15 | 38 35 57 58 52 45 48 --- 47
R06 | 1400 12 18 15 19 13 30 17 --- 8 | 28 34 34 41 36 24 28 --- 29
R07 | 773 10 12 16 9 13 22 14 129 6 | 54 56 52 58 59 42 50 69 52
R08 | 496 9 12 8 13 16 23 16 --- 6 | 40 40 44 51 48 35 35 --- 41
R09E | 3308 14 20 18 15 15 27 13 --- 7 | 22 23 26 43 35 50 26 --- 31
R10E | 1130 18 21 20 18 18 19 15 --- 8 | 41 49 40 49 39 43 38 --- 39
R11E | 760 11 18 17 14 17 16 13 122 6 | 29 32 28 39 41 35 31 73 32
R13E | 1435 13 28 16 14 18 27 19 --- 8 | 51 53 50 50 52 55 44 --- 48
R15E | 4035 19 22 13 16 21 24 17 --- 8 | 36 38 30 39 43 39 35 --- 34
R16E | 944 19 52 24 24 22 56 19 --- 12 | 37 64 29 42 39 38 33 --- 29
R17 | 1107 38 42 16 10 23 19 17 --- 9 | 65 68 47 43 32 53 42 --- 44
R18 | 560 25 26 13 12 27 21 17 --- 8 | 104 106 91 100 92 103 97 --- 96
R19 | 1866 67 73 24 12 35 14 23 --- 14 | 84 91 50 49 25 40 35 --- 43
R20 | 2122 54 55 37 25 32 43 23 --- 15 | 71 73 32 53 52 53 43 --- 41
R21 | 824 50 52 14 15 25 15 18 65 11 | 68 69 39 40 25 37 30 52 36
R22 | 824 48 52 12 16 22 20 18 --- 10 | 62 66 30 41 26 28 31 --- 32
R23 | 728 22 18 26 28 10 18 12 --- 9 | 38 44 37 63 45 39 53 --- 47
R24 | 1218 31 33 30 23 30 50 25 --- 13 | 66 70 50 62 35 52 68 --- 52
XR26 | ---- 24 47 --- --- --- --- 12 --- 18 | 26 62 --- --- --- --- 42 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1532 30 35 21 17 21 32 18 123 |T 50 55 42 51 44 47 43 67 43
WRMS | 1532 32 34 21 15 18 28 18 123 |NE 55 60 46 54 45 49 46 65 46
MEDI | 944 19 22 16 15 18 23 17 122 |MD 50 53 40 49 43 43 41 69 41
Table 3.1957.3 GPS week: 1957 Day: 3 MJD: 57946
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 | 853 14 20 24 20 11 29 15 --- 9 | 50 58 40 43 48 62 41 --- 44
R02 | 579 19 18 18 23 10 8 12 139 7 | 49 41 45 39 51 46 52 78 44
R03 | 647 12 13 12 14 15 11 12 114 5 | 46 45 46 56 57 43 46 62 48
R04 | 866 9 11 10 13 12 14 18 --- 6 | 44 44 46 46 51 42 31 --- 42
R05 | 790 26 26 15 38 13 60 23 --- 14 | 42 52 71 65 63 26 59 --- 53
R06 | 946 10 13 19 9 14 14 26 --- 7 | 25 28 29 30 33 26 17 --- 22
R07 | 694 15 15 16 10 5 11 12 183 5 | 48 51 54 48 53 47 45 95 48
R08 | 739 6 9 12 12 11 21 13 --- 6 | 47 45 50 55 48 54 43 --- 48
R09E | 3862 16 16 18 10 16 28 17 --- 8 | 28 28 32 40 34 55 31 --- 33
R10E | 1031 18 19 23 18 19 31 15 --- 9 | 46 45 53 47 46 59 43 --- 46
R11E | 868 14 32 15 12 14 18 9 155 6 | 33 37 26 27 29 29 28 110 25
R13E | 2038 15 22 16 17 13 32 19 --- 8 | 32 38 35 40 33 45 28 --- 32
R15E | 3382 15 29 20 17 16 12 15 --- 7 | 32 36 26 30 28 33 25 --- 26
R16E | 1203 12 22 26 45 33 29 22 --- 13 | 31 39 36 58 46 45 32 --- 32
R17 | 1231 50 55 20 12 26 10 12 --- 10 | 76 81 43 37 31 42 38 --- 40
R18 | 711 27 28 13 9 19 13 12 --- 7 | 68 68 49 58 55 62 55 --- 56
R19 | 703 63 61 26 27 28 26 23 --- 15 | 100 103 59 54 42 58 41 --- 53
R20 | 1494 57 75 28 20 40 52 21 --- 16 | 78 98 41 59 46 61 45 --- 46
R21 | 1060 51 59 20 9 26 19 20 61 11 | 83 88 48 47 34 54 42 41 47
R22 | 659 51 51 16 12 23 22 18 --- 11 | 77 75 40 44 31 50 32 --- 41
R23 | 1427 21 23 22 30 15 27 21 --- 10 | 32 32 33 59 44 24 49 --- 39
R24 | 1678 19 46 35 26 18 39 30 --- 13 | 63 90 69 56 54 40 66 --- 54
XR26 | ---- 19 40 --- --- --- --- 10 --- 14 | 33 43 --- --- --- --- 34 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1503 30 35 20 21 20 27 18 137 |T 50 55 44 47 43 45 40 77 41
WRMS | 1503 31 34 20 16 16 25 18 137 |NE 56 61 47 49 46 46 43 69 44
MEDI | 868 18 23 18 14 15 21 17 139 |MD 46 45 43 47 46 45 41 78 44
Table 3.1957.4 GPS week: 1957 Day: 4 MJD: 57947
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 | 494 19 14 22 24 14 20 8 --- 8 | 46 43 49 32 40 47 32 --- 36
R02 | 644 14 23 10 13 11 17 11 106 5 | 44 53 44 39 47 55 49 60 44
R03 | 636 9 12 9 10 13 20 9 112 5 | 42 43 45 37 45 53 41 69 41
R04 | 773 10 14 9 16 19 24 16 --- 7 | 45 49 42 43 52 28 33 --- 39
R05 | 565 46 37 28 29 17 51 17 --- 13 | 41 53 58 57 50 39 53 --- 48
R06 | 604 24 30 21 10 14 33 22 --- 9 | 26 30 29 29 28 33 22 --- 24
R07 | 784 13 15 6 11 7 16 12 254 5 | 47 47 49 53 51 46 41 172 47
R08 | 572 12 11 14 13 17 22 14 --- 6 | 41 46 50 48 54 30 35 --- 43
R09E | 2989 19 23 15 16 14 33 10 --- 7 | 30 33 30 45 41 50 35 --- 36
R10E | 1014 26 23 20 13 18 18 14 --- 8 | 43 43 44 34 38 41 37 --- 36
R11E | 1205 15 18 14 13 15 25 14 163 7 | 31 30 26 24 30 28 27 135 24
R13E | 1567 18 31 14 19 13 23 10 --- 7 | 26 32 31 28 27 30 29 --- 25
R15E | 2766 33 66 13 16 20 37 19 --- 9 | 33 58 29 32 32 37 29 --- 26
R16E | 1249 24 39 28 15 35 40 19 --- 11 | 25 29 44 30 47 29 23 --- 27
R17 | 791 50 57 14 11 26 17 11 --- 9 | 66 71 34 37 25 32 32 --- 33
R18 | 769 32 41 13 13 26 24 11 --- 8 | 80 83 68 65 59 76 69 --- 66
R19 | 591 66 66 19 19 30 22 18 --- 12 | 85 84 41 46 37 56 35 --- 43
R20 | 844 58 50 37 29 52 49 26 --- 18 | 95 92 43 79 72 81 57 --- 62
R21 | 845 50 48 18 12 26 22 23 79 11 | 80 79 46 53 36 54 49 62 49
R22 | 922 54 63 19 11 29 25 19 --- 11 | 74 81 46 45 34 58 37 --- 43
R23 | 1476 22 24 26 31 14 24 17 --- 10 | 35 35 34 59 44 40 51 --- 44
R24 | 750 23 31 28 23 20 56 22 --- 12 | 50 48 54 56 48 36 42 --- 44
XR26 | ---- 23 66 --- --- --- --- 8 --- 14 | 33 68 --- --- --- --- 38 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1224 33 38 20 18 23 30 16 155 |T 48 53 42 44 42 44 38 99 39
WRMS | 1224 33 35 20 16 16 31 16 155 |NE 54 59 45 48 45 47 42 90 43
MEDI | 784 23 31 15 13 17 24 14 112 |MD 43 48 44 43 41 40 37 69 41
Table 3.1957.5 GPS week: 1957 Day: 5 MJD: 57948
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 | 587 28 21 20 20 18 30 20 --- 10 | 34 33 30 33 39 39 29 --- 28
R02 | 928 16 14 15 15 21 19 15 106 7 | 43 40 32 34 39 52 32 31 34
R03 | 590 14 15 11 13 13 19 10 246 6 | 43 40 42 50 43 59 42 133 44
R04 | 668 9 9 10 8 8 21 10 --- 5 | 46 47 47 44 44 33 45 --- 43
R05 | 1044 41 37 28 19 13 58 16 --- 13 | 39 35 51 50 47 36 36 --- 42
R06 | 761 28 28 28 13 25 29 29 --- 11 | 23 28 24 35 45 19 28 --- 27
R07 | 1353 16 21 15 10 12 21 8 177 6 | 44 48 49 59 58 65 50 163 53
R08 | 1373 12 16 13 15 13 14 20 --- 7 | 37 39 41 51 45 50 37 --- 42
R09E | 1347 15 18 16 13 18 25 13 --- 7 | 33 36 31 49 41 35 37 --- 37
R10E | 905 17 28 16 14 18 33 23 --- 9 | 68 66 72 70 68 53 62 --- 65
R11E | 1334 16 17 14 11 14 20 13 95 6 | 44 45 41 49 44 36 41 114 41
R13E | 916 10 13 17 13 13 30 15 --- 7 | 41 48 42 39 38 54 34 --- 37
R15E | 4201 15 46 17 19 19 37 16 --- 9 | 42 54 45 46 41 44 36 --- 39
R16E | 1479 18 73 32 22 29 23 22 --- 11 | 32 67 39 27 45 33 25 --- 26
R17 | 603 42 46 19 10 22 14 19 --- 9 | 56 57 38 35 27 27 26 --- 32
R18 | 617 34 38 11 10 23 16 10 --- 8 | 64 68 47 52 43 49 48 --- 48
R19 | 953 71 68 15 25 27 34 18 --- 14 | 73 71 42 36 39 44 26 --- 36
R20 | 833 59 67 20 27 29 63 33 --- 16 | 77 89 59 56 46 50 54 --- 52
R21 | 1002 41 38 16 13 26 21 23 78 10 | 60 57 43 47 34 40 37 46 41
R22 | 719 48 53 15 10 26 18 18 --- 10 | 59 64 40 43 32 29 34 --- 37
R23 | 754 23 19 15 27 15 20 13 --- 8 | 32 35 37 50 42 32 43 --- 39
R24 | 1030 16 17 41 27 34 76 26 --- 17 | 35 40 50 47 37 46 34 --- 31
XR26 | ---- 23 57 --- --- --- --- 13 --- 18 | 30 52 --- --- --- --- 32 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1314 31 37 20 17 21 33 19 154 |T 45 50 42 45 42 42 37 97 39
WRMS | 1314 29 30 20 14 20 29 19 154 |NE 46 49 42 45 41 41 37 93 38
MEDI | 916 18 28 16 13 18 21 16 106 |MD 43 48 42 47 42 40 36 114 39
Table 3.1957.6 GPS week: 1957 Day: 6 MJD: 57949
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 | 923 17 15 21 26 14 34 23 --- 10 | 59 58 50 46 57 70 53 --- 51
R02 | 1022 14 18 12 8 12 28 7 125 6 | 55 60 51 50 51 52 44 57 49
R03 | 713 7 11 17 7 11 18 10 170 5 | 56 57 58 58 59 55 53 80 56
R04 | 685 10 13 13 11 15 15 14 --- 6 | 57 56 57 57 59 52 47 --- 54
R05 | 869 32 37 16 33 17 62 20 --- 14 | 45 46 62 70 61 45 49 --- 55
R06 | 986 26 26 16 9 13 16 25 --- 8 | 30 32 32 39 39 37 36 --- 33
R07 | 1623 19 18 17 8 15 24 11 152 7 | 60 63 65 73 75 83 70 113 70
R08 | 1455 14 21 11 10 11 18 18 --- 6 | 54 58 59 59 58 60 47 --- 55
R09E | 1457 17 19 21 39 18 36 22 --- 12 | 47 44 52 47 55 56 48 --- 46
R10E | 780 20 27 18 21 13 16 20 --- 8 | 66 71 70 55 59 72 62 --- 62
R11E | 1291 18 29 17 13 24 29 11 76 8 | 58 59 55 59 52 62 49 102 53
R13E | 978 12 13 21 13 21 25 17 --- 8 | 61 66 61 64 64 62 62 --- 61
R15E | 3243 22 16 16 17 11 18 21 --- 7 | 56 54 63 56 54 60 47 --- 54
R16E | 1367 18 43 18 19 16 25 25 --- 9 | 42 57 50 45 48 47 40 --- 42
R17 | 540 46 45 19 11 26 18 22 --- 11 | 84 85 46 46 31 52 38 --- 45
R18 | 626 34 32 14 15 17 18 19 --- 8 | 91 90 66 73 62 66 67 --- 68
R19 | 638 66 66 24 27 35 48 19 --- 16 | 111 110 52 58 39 74 41 --- 53
R20 | 1464 64 77 23 28 35 53 30 --- 17 | 117 127 68 72 54 83 66 --- 70
R21 | 944 45 50 20 17 23 31 26 64 12 | 102 106 67 67 47 64 51 52 62
R22 | 763 47 40 23 8 28 19 19 --- 11 | 95 94 58 56 37 63 48 --- 55
R23 | 615 23 24 23 27 12 17 13 --- 9 | 48 47 52 82 64 56 71 --- 63
R24 | 1257 26 31 31 24 17 47 41 --- 14 | 65 69 66 70 52 61 52 --- 55
XR26 | ---- 27 130 --- --- --- --- 17 --- 22 | 49 129 --- --- --- --- 53 --- 49
------+---------------------------------------------------+-----------------------------------------------
RMS | 1239 32 35 19 20 20 31 21 124 |T 65 71 57 59 53 60 51 80 54
WRMS | 1239 27 28 19 17 18 26 21 124 |NE 69 75 56 61 52 60 52 75 55
MEDI | 944 22 27 18 15 16 24 19 125 |MD 58 60 58 58 54 60 49 80 55
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