[IGSREPORT-25555] Wk 1967 IGLOS Final Orbits
acc
acc at igs.org
Wed Oct 11 20:54:08 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1967 (Sep 17, 2017 - Sep 23, 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 2.1967.
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:
igl1967[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1967 in the SP3 format.
igl19677.sum Combination Report for GPS Week 1967.
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 | -0.7 ns
1 | -0.5 ns
2 | 1.5 ns
3 | -1.1 ns
4 | 0.4 ns
5 | -2.4 ns
6 | -2.0 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | IAC | R01 R14
1 | IAC | R15
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 1.1967, 1a.1967).
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 2.1967.0-6)
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 3.1967.0-6).
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 1967 summary. (Sep 17, 2017 - Sep 23, 2017)
Table 1.1967.a GPS week : 1967 MJD: 58013.0-58019.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 -1 -2 15 0 .06 27 28 | 9527 -1310 69 569
| 0 0 2 18 25 31 .04 | 1292 2412
cof n/a| 0 0 -2 3 4 3 .11 31 30 | 9507 -1302 39 560
| 0 1 2 26 17 24 .05 | 1288 2399
emx n/a| -1 1 -4 -1 -1 34 .06 26 26 | -3420 -1584 62 664
| 1 0 0 28 19 33 .04 | 10180 1383
esx n/a| 0 0 0 -14 20 -29 .23 17 15 | -2576 -58 185 2607
| 0 1 0 17 9 42 .05 | 7195 2745
gfz n/a| 0 0 -1 -12 16 46 .00 23 20 | 0 -1166 50 447
| 0 1 1 18 13 31 .06 | 0 2747
grg n/a| 0 0 8 -65 2 -90 -.45 30 29 | -128 -1117 119 2033
| 1 1 5 22 37 75 .05 | 619 2447
iac n/a| 1 0 1 62 -46 28 -.03 25 22 | 816 -1326 50 834
| 1 1 3 41 45 78 .03 | 1052 1402
mcc n/a| 3 0 35 126 -23 -190 -.25 125 125 | --- --- --- ---
| 5 6 8 62 72 637 .32 | --- ---
Table 1.1967.b GPS week : 1967 MJD: 58013.0-58019.0
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 | 11 11 11 12 10 8 11 |
R02 | 8 7 6 9 9 8 8 |
R03 | 8 8 8 9 8 7 7 |
R04 | 8 8 8 7 7 7 7 |
R05 | 12 11 10 19 13 11 13 |
R06 | 9 10 10 10 11 12 10 |
R07 | 8 7 7 8 9 7 7 |
R08 | 6 7 9 7 7 7 8 |
R09 | 8 15 15 8 8 12 6 |
R10 | 8 6 9 8 7 6 11 |
R11 | 9 8 9 7 8 10 9 |
R13 | 8 9 8 8 8 10 6 |
R14 | --- --- --- --- 0 20 29 |
R15 | 13 19 16 14 13 15 13 |
R16 | 17 19 16 14 17 17 12 |
R17 | 10 9 10 9 8 10 9 |
R18 | 9 8 8 9 11 7 8 |
R19 | 12 13 15 13 13 14 12 |
R20 | 15 13 13 14 10 15 14 |
R21 | 9 9 12 11 8 10 9 |
R22 | 9 9 9 11 12 11 10 |
R23 | 10 9 7 9 10 7 10 |
R24 | 12 14 15 16 13 15 14 |
R26 | 28 27 0 37 --- --- --- |
Table 1.1967.c GPS week : 1967 MJD: 58013.0-58019.0
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 1967 0 | 71 -11 115 394 992 3773 81.6 1791 1791 | -611 -50
brd 1967 1 | -69 -53 171 925 -1075 2375 82.8 1602 1602 | -537 11
brd 1967 2 | -36 -33 72 -542 141 1623 82.4 1363 1363 | 2345 -799
brd 1967 3 | 3 -13 74 99 624 3168 84.3 1341 1341 | -931 32
brd 1967 4 | 55 -17 1 1502 272 654 84.9 1181 1181 | 761 157
brd 1967 5 | -26 9 -59 -9 900 314 84.4 1365 1365 | -1683 -739
brd 1967 6 | -41 17 -40 567 -375 2283 84.6 1436 1436 | -1349 -698
-------------+------------------------------------------------------------+----------------
brd 1967 mean| -6 -14 47 419 211 2027 83.6 1439 1439 | -286 -298
brd 1967 sdev| 52 24 84 666 737 1259 1.3 199 199 | 1395 423
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 2.1967.0 GPS week: 1967 Day: 0 MJD: 58013
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 0 -17 12 14 .00 24 24 | 9627 -2146 66 779
cof n/a| 0 0 1 -13 -4 0 .12 28 23 | 9597 -2131 42 776
emx n/a| -2 1 -5 -29 2 15 .07 24 24 | 84 -1934 58 579
esx n/a| 0 -1 -2 -14 9 -78 .18 15 15 | 6194 -188 214 3202
gfz n/a| -1 0 0 -41 27 -11 .03 22 19 | 0 -1588 53 657
grg n/a| 0 1 10 -49 -36 17 -.37 31 31 | 497 -1746 116 2135
iac n/a| 2 0 3 102 -26 114 -.01 50 31 | 308 -516 22 601
mcc n/a| 7 3 31 161 89 756 -.60 88 88 | --- --- --- ---
Table 2.1967.1 GPS week: 1967 Day: 1 MJD: 58014
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 -19 -7 .11 25 27 | 7630 -1153 65 464
cof n/a| -1 -2 -2 -19 -21 -2 .12 29 30 | 7608 -1137 35 454
emx n/a| -2 2 -4 27 4 53 .11 27 27 | -16779 -1963 74 830
esx n/a| 0 -2 0 -2 29 -84 .18 18 17 | 3544 382 320 2821
gfz n/a| 1 0 -1 13 27 90 .03 25 20 | 0 -1023 46 472
grg n/a| 0 1 8 -104 -1 -9 -.46 35 35 | -209 -899 153 1948
iac n/a| 3 0 5 34 -51 34 -.06 18 18 | 174 -283 61 948
mcc n/a| 0 10 45 210 12 316 -.27 78 78 | --- --- --- ---
Table 2.1967.2 GPS week: 1967 Day: 2 MJD: 58015
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 -2 3 -12 8 -37 .11 30 31 | 9403 2653 77 584
cof n/a| 0 1 0 -8 12 -11 .16 32 33 | 9386 2642 52 577
emx n/a| 0 0 -3 5 1 41 .08 28 28 | -7330 337 52 576
esx n/a| 0 -2 0 -9 30 -55 .20 18 15 | -10872 5019 177 2778
gfz n/a| -1 -1 -1 -27 -6 51 .07 23 19 | 0 2947 42 491
grg n/a| 2 2 2 -33 49 -83 -.47 31 28 | 813 2474 129 1827
iac n/a| 0 1 1 61 -91 73 -.04 20 20 | 2749 77 47 817
mcc n/a| 5 0 32 80 -131 188 .07 129 129 | --- --- --- ---
Table 2.1967.3 GPS week: 1967 Day: 3 MJD: 58016
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 0 -3 11 -15 .02 27 29 | 10272 -2951 68 494
cof n/a| 0 -1 -1 10 7 -31 .06 31 32 | 10254 -2934 29 483
emx n/a| 0 1 -4 46 -21 93 .03 27 27 | -13662 -2815 71 841
esx n/a| 0 1 -1 -45 20 4 .27 16 16 | 3719 -3338 129 2441
gfz n/a| 0 1 -3 -16 19 50 -.09 22 18 | 0 -3028 41 247
grg n/a| 0 -1 0 -60 29 -100 -.51 33 26 | 38 -2663 135 2199
iac n/a| 0 0 5 41 -43 -64 -.10 20 19 | 771 -2597 61 867
mcc n/a| -2 2 19 34 -19 -199 -.74 180 180 | --- --- --- ---
Table 2.1967.4 GPS week: 1967 Day: 4 MJD: 58017
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 -2 43 57 .05 26 28 | 9942 1212 69 442
cof n/a| 0 0 -3 -14 22 37 .12 29 29 | 9931 1202 30 429
emx n/a| 0 1 -3 -24 -18 26 .01 24 24 | 12576 387 64 700
esx n/a| 0 0 -1 -31 12 -5 .30 19 17 | -8092 729 57 2168
gfz n/a| 0 1 0 -12 12 40 .04 21 20 | 0 2077 49 317
grg n/a| 0 0 14 -74 -45 -107 -.50 26 26 | -462 1848 110 1855
iac n/a| 2 0 0 135 -2 -28 .01 21 21 | 1217 -228 58 916
mcc n/a| 7 -10 36 183 -55 -644 -.23 112 112 | --- --- --- ---
Table 2.1967.5 GPS week: 1967 Day: 5 MJD: 58018
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 -2 31 1 10 .07 27 29 | 11548 -4010 69 590
cof n/a| 0 -1 -4 55 27 33 .18 32 33 | 11518 -3979 33 580
emx n/a| 0 2 -5 -22 37 -11 .09 26 26 | 3974 -2901 62 567
esx n/a| 1 -1 0 3 29 21 .22 17 14 | -2377 -2858 235 2115
gfz n/a| 0 2 0 3 29 68 -.03 24 27 | 0 -4303 56 402
grg n/a| -2 0 12 -69 37 -147 -.42 28 31 | -757 -4062 101 2205
iac n/a| 0 0 -2 29 -119 -51 -.03 22 22 | 1095 -3370 47 900
mcc n/a| -3 -2 39 115 -77 -881 -.08 129 129 | --- --- --- ---
Table 2.1967.6 GPS week: 1967 Day: 6 MJD: 58019
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 -4 12 54 -25 .02 27 29 | 8269 -2778 74 632
cof n/a| -1 0 -6 12 -8 0 .05 37 30 | 8259 -2779 52 624
emx n/a| -1 1 -3 -9 -11 24 -.00 22 22 | -2803 -2205 57 557
esx n/a| 0 0 0 -1 11 -4 .22 15 14 | -10148 -157 169 2729
gfz n/a| 0 0 0 -5 3 36 -.02 22 15 | 0 -3249 67 545
grg n/a| 0 -1 11 -63 -15 -200 -.45 26 27 | -822 -2771 92 2065
iac n/a| 2 1 -1 30 7 125 -.01 22 22 | -599 -2368 56 795
mcc n/a| 12 -1 40 98 14 -868 .11 161 161 | --- --- --- ---
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 3.1967.0 GPS week: 1967 Day: 0 MJD: 58013
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1495 30 28 21 12 23 23 218 --- 10 | 81 78 81 85 86 82 220 --- 82
R02E | 926 13 14 20 13 17 24 15 113 7 | 85 89 79 81 81 83 80 114 80
R03E | 4080 21 17 17 15 22 23 10 83 8 | 68 69 73 63 71 73 71 77 67
R04E | 1529 20 19 19 11 17 20 14 --- 7 | 49 49 52 44 45 55 51 --- 46
R05E | 1507 19 21 28 23 29 32 22 --- 11 | 47 49 36 57 59 51 48 --- 47
R06E | 1965 26 33 19 16 21 24 16 --- 9 | 58 71 53 56 54 62 53 --- 53
R07E | 3608 24 26 16 11 20 18 12 78 7 | 64 65 59 61 62 63 60 59 59
R08E | 2037 13 14 16 11 15 15 11 --- 6 | 81 83 83 82 83 85 83 --- 82
R09E | 1548 12 10 16 13 24 25 17 --- 8 | 28 30 37 22 35 38 35 --- 25
R10 | 895 12 10 16 14 24 15 17 --- 7 | 40 43 35 48 41 39 33 --- 37
R11 | 1075 29 21 24 7 19 15 20 72 8 | 74 72 69 68 65 67 64 94 66
R13 | 848 12 8 17 13 18 25 19 --- 7 | 66 70 69 73 68 68 65 --- 67
R15 | 2640 43 34 35 17 31 16 24 --- 12 | 85 85 73 57 49 60 51 --- 60
R16 | 727 32 45 52 21 19 76 18 --- 16 | 47 47 31 48 34 43 40 --- 36
R17 | 951 29 29 27 10 24 18 24 --- 10 | 38 38 38 40 35 33 27 --- 32
R18 | 784 19 21 21 20 14 22 21 --- 9 | 27 30 30 36 25 21 21 --- 25
R19 | 2297 29 23 28 14 36 33 27 --- 12 | 48 53 45 43 44 41 25 --- 36
R20 | 1661 36 61 36 21 18 55 30 --- 14 | 44 67 50 42 33 30 23 --- 31
R21 | 686 13 15 16 13 14 38 19 90 8 | 45 47 46 45 46 37 32 39 40
R22 | 618 22 25 20 12 26 26 16 --- 9 | 60 65 58 66 58 57 45 --- 56
R23 | 1204 20 22 21 20 15 25 23 --- 9 | 19 21 24 36 27 30 32 --- 25
R24 | 845 30 44 19 20 15 46 28 --- 11 | 50 73 38 47 40 37 31 --- 37
XR26 | ---- 34 78 --- --- --- --- 21 --- 27 | 72 98 --- --- --- --- 79 --- 83
------+---------------------------------------------------+-----------------------------------------------
RMS | 1790 24 28 24 15 22 31 50 88 |T 55 60 52 54 51 52 55 76 50
WRMS | 1790 24 23 24 15 19 31 31 88 |NE 51 57 46 49 43 43 40 66 45
MEDI | 1204 22 22 20 13 19 24 19 83 |MD 50 65 50 48 46 51 48 77 47
Table 3.1967.1 GPS week: 1967 Day: 1 MJD: 58014
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 724 31 24 28 13 29 28 13 --- 10 | 71 77 75 68 73 77 85 --- 71
R02E | 1043 16 13 17 11 23 22 10 81 7 | 52 52 52 53 57 58 49 81 51
R03E | 3773 20 17 17 14 20 19 10 35 7 | 64 67 67 62 69 73 65 73 63
R04E | 2050 19 24 21 14 20 17 15 --- 7 | 45 48 52 50 50 52 52 --- 48
R05E | 1488 21 29 36 19 28 27 19 --- 11 | 38 47 43 41 42 44 33 --- 34
R06E | 954 27 34 27 16 23 13 18 --- 9 | 57 62 55 60 68 52 56 --- 56
R07E | 3078 20 20 17 8 21 18 12 48 7 | 55 60 74 59 72 67 58 63 62
R08E | 1758 15 24 17 11 22 18 15 --- 7 | 74 75 84 75 79 80 74 --- 75
R09E | 1182 14 20 30 43 16 63 17 --- 14 | 30 32 42 27 42 66 26 --- 28
R10 | 1092 11 17 12 12 13 16 16 --- 6 | 23 26 19 24 26 23 19 --- 19
R11 | 1076 23 23 16 8 30 14 14 109 8 | 63 63 62 61 58 61 58 58 59
R13 | 942 16 24 11 23 23 20 15 --- 8 | 51 55 52 59 52 54 52 --- 51
R15 | 1415 49 53 34 20 55 19 31 --- 19 | 44 50 46 39 43 38 38 --- 40
R16 | 897 37 37 64 24 11 84 20 --- 18 | 26 28 31 24 23 22 28 --- 19
R17 | 972 25 29 29 11 24 25 13 --- 9 | 19 21 25 24 21 16 16 --- 18
R18 | 783 12 12 23 16 16 14 17 --- 7 | 19 21 19 28 20 17 15 --- 16
R19 | 1950 36 42 32 13 34 32 29 --- 13 | 25 32 30 31 24 24 22 --- 21
R20 | 1666 31 28 22 25 23 54 23 --- 13 | 26 29 32 33 27 12 15 --- 20
R21 | 563 25 30 30 6 20 22 18 94 9 | 21 24 28 24 22 17 27 30 21
R22 | 761 27 27 21 10 13 22 21 --- 8 | 39 39 40 43 43 51 31 --- 39
R23 | 1313 18 16 20 25 16 29 14 --- 9 | 15 18 16 27 20 17 23 --- 17
R24 | 1588 26 53 24 17 31 65 21 --- 13 | 33 59 31 37 40 31 28 --- 29
XR26 | ---- 33 124 --- --- --- --- 21 --- 26 | 80 128 --- --- --- --- 72 --- 70
------+---------------------------------------------------+-----------------------------------------------
RMS | 1602 25 29 27 18 25 35 18 78 |T 42 48 44 43 44 43 40 61 40
WRMS | 1602 27 30 27 17 20 35 18 78 |NE 34 42 33 34 32 29 31 44 31
MEDI | 1092 23 24 22 14 22 22 17 81 |MD 39 48 42 39 42 44 33 63 39
Table 3.1967.2 GPS week: 1967 Day: 2 MJD: 58015
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 567 35 24 26 13 30 33 15 --- 11 | 87 91 99 97 103 84 101 --- 94
R02E | 995 15 18 14 11 14 9 14 160 6 | 51 47 42 44 42 43 39 217 42
XR03E | 3682 20 19 18 11 18 --- 12 58 7 | 45 43 45 51 51 --- 50 63 47
R04E | 2712 16 14 21 11 19 17 15 --- 7 | 30 32 38 39 40 44 38 --- 36
R05E | 2065 21 23 25 16 25 28 22 --- 10 | 40 35 37 31 47 39 36 --- 32
R06E | 1902 24 23 30 22 14 21 14 --- 9 | 35 41 38 37 30 35 37 --- 32
R07E | 1548 22 22 19 10 18 17 12 58 7 | 42 40 37 46 45 46 40 67 41
R08E | 2239 16 20 20 15 20 19 22 --- 8 | 54 49 52 59 62 48 47 --- 51
R09E | 825 22 18 27 47 17 30 35 --- 15 | 20 20 23 37 30 42 38 --- 21
R10 | 1220 13 11 19 23 13 28 18 --- 9 | 27 30 23 40 30 39 24 --- 28
R11 | 924 23 21 23 13 16 30 14 172 8 | 69 69 72 68 67 64 64 84 65
R13 | 851 14 16 17 11 12 27 20 --- 7 | 63 65 64 61 67 58 57 --- 60
R15 | 1262 58 59 37 17 41 26 27 --- 15 | 78 81 70 58 58 70 55 --- 60
R16 | 1327 41 43 45 19 26 68 14 --- 16 | 37 39 28 29 29 40 30 --- 24
R17 | 777 26 28 26 11 31 17 19 --- 9 | 28 29 29 26 25 23 21 --- 20
R18 | 932 17 16 22 13 13 26 12 --- 7 | 18 21 24 25 23 14 16 --- 18
R19 | 1372 51 54 29 24 35 40 22 --- 14 | 35 42 23 25 24 51 23 --- 22
R20 | 1382 26 37 41 16 20 43 21 --- 12 | 43 54 33 35 33 32 17 --- 22
R21 | 589 36 30 36 10 32 17 23 87 11 | 39 39 41 44 45 37 31 38 37
R22 | 604 30 29 28 10 13 12 26 --- 9 | 52 54 55 55 48 59 40 --- 49
R23 | 799 14 18 16 14 10 21 13 --- 6 | 18 26 17 25 27 17 17 --- 18
R24 | 1144 48 68 37 19 29 54 19 --- 15 | 68 80 35 48 29 35 28 --- 35
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 124 --- 124
------+---------------------------------------------------+-----------------------------------------------
RMS | 1362 30 32 28 18 23 31 20 129 |T 44 46 42 44 43 43 42 93 42
WRMS | 1362 31 33 28 15 19 28 20 129 |NE 44 48 39 41 38 41 39 61 41
MEDI | 1144 22 22 25 13 18 26 18 87 |MD 40 41 37 40 40 42 38 67 36
Table 3.1967.3 GPS week: 1967 Day: 3 MJD: 58016
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 911 33 30 33 11 22 30 29 --- 11 | 83 88 85 82 85 97 87 --- 83
R02E | 1483 24 23 28 13 20 18 17 339 9 | 66 74 60 67 69 64 63 215 63
R03E | 2398 18 16 22 16 20 27 20 85 8 | 323 329 323 328 322 339 310 316 322
R04E | 2979 15 13 15 10 16 28 14 --- 7 | 34 33 33 34 36 46 42 --- 34
XR05E | 876 32 36 33 27 --- 36 51 --- 18 | 279 285 284 278 --- 302 314 --- 289
R06E | 1640 24 40 28 22 13 20 20 --- 9 | 37 50 39 44 40 41 36 --- 36
R07E | 832 23 21 24 7 16 29 12 148 8 | 40 44 37 41 42 39 39 73 37
R08E | 1256 16 14 18 9 13 23 15 --- 6 | 38 43 46 44 48 46 40 --- 42
R09E | 779 14 15 12 12 18 35 19 --- 8 | 47 50 46 66 55 59 48 --- 51
R10 | 1108 11 11 11 26 12 20 18 --- 8 | 33 37 36 42 30 35 30 --- 33
R11 | 1181 20 19 16 10 17 15 14 122 6 | 303 304 293 306 295 300 303 325 301
R13 | 632 16 18 12 19 24 19 14 --- 8 | 228 226 217 220 217 216 220 --- 220
R15 | 1091 52 59 36 12 31 16 25 --- 13 | 109 111 109 93 80 91 81 --- 91
R16 | 2005 28 31 48 15 26 54 16 --- 13 | 290 292 276 294 290 289 276 --- 285
R17 | 973 28 24 19 11 20 17 19 --- 8 | 33 33 26 32 26 21 23 --- 24
R18 | 742 8 14 21 25 18 26 15 --- 9 | 172 166 159 170 158 155 161 --- 163
R19 | 988 51 53 21 15 33 22 16 --- 12 | 54 57 46 44 37 38 34 --- 39
R20 | 1326 26 57 54 17 19 49 22 --- 14 | 43 71 44 35 28 29 24 --- 25
R21 | 581 29 36 24 12 33 27 26 57 11 | 79 80 71 62 68 66 80 87 69
R22 | 476 34 30 32 9 31 17 23 --- 11 | 41 43 40 36 30 35 30 --- 32
R23 | 791 12 19 13 22 15 37 19 --- 9 | 22 25 24 34 32 34 20 --- 23
R24 | 938 23 36 37 21 24 79 31 --- 16 | 52 61 49 54 35 53 27 --- 40
XR26 | ---- 44 43 --- --- --- --- 30 --- 36 | 63 66 --- --- --- --- 82 --- 75
------+---------------------------------------------------+-----------------------------------------------
RMS | 1341 27 31 27 16 22 33 20 180 |T 107 111 106 109 96 108 103 203 103
WRMS | 1341 29 32 27 16 18 26 19 180 |NE 108 112 106 109 102 104 99 206 101
MEDI | 973 24 24 22 13 20 26 19 122 |MD 54 66 46 54 48 53 48 215 51
Table 3.1967.4 GPS week: 1967 Day: 4 MJD: 58017
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1299 35 28 32 9 26 11 12 --- 10 | 114 115 118 118 133 116 115 --- 118
R02E | 770 18 38 24 11 13 27 19 112 8 | 58 72 54 54 54 63 44 88 52
R03E | 1180 19 17 19 8 23 23 12 77 8 | 9999 9999 9999 9999 9999 9999 9999 9999 9999
R04E | 2293 16 11 16 15 16 23 10 --- 7 | 37 38 36 43 41 42 36 --- 37
R05E | 1721 24 32 26 15 23 44 31 --- 12 | 958 953 954 952 979 976 953 --- 960
R06E | 1047 27 34 20 27 25 28 20 --- 11 | 39 46 32 54 50 38 33 --- 37
R07E | 984 24 24 22 12 16 25 16 144 8 | 43 46 40 42 41 43 31 58 37
R08E | 710 15 15 17 14 16 14 15 --- 6 | 33 33 38 35 40 40 36 --- 34
R09E | 807 18 17 14 12 14 30 17 --- 8 | 138 139 131 128 130 123 132 --- 129
R10 | 676 8 11 13 22 14 10 12 --- 6 | 58 60 49 58 46 54 52 --- 51
R11 | 1348 17 20 8 12 26 12 23 149 8 | 876 875 887 891 899 899 870 916 887
R13 | 455 7 8 16 23 12 17 18 --- 7 | 787 781 785 801 794 800 787 --- 793
XR14 | 2271 4 11 --- --- --- --- --- --- 0 | 9999 9999 --- --- --- --- --- --- 9999
R15 | 1747 49 40 26 15 36 20 25 --- 13 | 109 104 99 92 89 106 85 --- 94
R16 | 1834 22 43 48 38 14 54 38 --- 17 | 714 697 701 686 687 695 716 --- 699
R17 | 1569 28 32 16 9 20 17 19 --- 8 | 35 38 30 34 42 29 24 --- 29
R18 | 632 27 27 24 29 20 30 14 --- 11 | 411 408 409 424 417 413 418 --- 415
R19 | 718 54 55 24 13 32 20 24 --- 13 | 79 79 69 77 82 74 88 --- 77
R20 | 594 23 32 27 20 16 22 20 --- 9 | 63 59 59 54 48 76 72 --- 58
R21 | 720 23 21 16 10 22 12 15 42 7 | 139 143 143 138 132 142 129 144 136
R22 | 531 32 35 19 17 27 23 33 --- 11 | 47 48 40 55 41 60 39 --- 45
R23 | 755 10 14 25 28 6 26 23 --- 10 | 27 34 42 39 28 40 25 --- 29
R24 | 1240 25 28 41 27 25 31 24 --- 13 | 35 42 41 53 33 25 26 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1180 26 29 24 19 21 26 21 112 |T 228 229 226 229 228 231 217 301 226
WRMS | 1180 28 29 24 17 20 26 21 112 |NE 260 259 258 261 256 262 242 530 257
MEDI | 984 23 27 20 15 20 23 19 112 |MD 63 72 59 58 54 74 65 88 58
Table 3.1967.5 GPS week: 1967 Day: 5 MJD: 58018
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 441 26 28 21 13 18 20 16 --- 8 | 68 75 75 68 80 81 74 --- 71
R02E | 676 24 16 16 11 16 24 10 129 7 | 59 56 45 51 50 58 49 111 50
R03E | 829 22 13 16 9 17 15 17 90 7 | 9999 9999 9999 9999 9999 9999 9999 9999 9999
R04E | 2255 15 23 14 8 21 21 12 --- 6 | 57 60 57 58 63 60 59 --- 57
R05E | 1546 25 52 23 22 20 32 28 --- 11 | 9999 9999 9999 9999 9999 9999 9999 --- 9999
R06E | 1390 35 46 23 32 16 23 24 --- 12 | 42 47 32 58 44 43 39 --- 39
R07E | 989 19 14 15 9 15 25 15 146 7 | 46 43 49 44 53 69 48 58 48
R08E | 998 17 9 15 12 15 21 12 --- 6 | 62 66 72 68 70 72 70 --- 67
R09E | 1096 19 28 19 37 13 26 23 --- 11 | 222 219 228 249 232 221 232 --- 233
R10 | 1658 10 15 14 11 20 16 10 --- 6 | 58 57 58 52 59 55 54 --- 54
R11 | 1184 20 25 10 11 27 35 21 189 9 | 9999 9999 9999 9999 9999 9999 9999 9999 9999
R13 | 799 9 21 16 19 24 29 27 --- 9 | 9999 9999 9999 9999 9999 9999 9999 --- 9999
XR14 | 1675 23 24 --- --- --- 24 33 --- 19 | 9999 9999 --- --- --- 9999 9999 --- 9999
R15 | 3632 50 62 33 18 47 22 21 --- 14 | 116 119 116 112 111 101 112 --- 110
R16 | 1629 29 37 59 11 26 59 26 --- 16 | 9999 9999 9999 9999 9999 9999 9999 --- 9999
R17 | 1068 34 33 26 10 28 13 18 --- 9 | 35 34 34 28 26 24 41 --- 29
R18 | 683 18 12 14 15 18 10 20 --- 7 | 677 683 680 670 672 684 668 --- 674
R19 | 662 45 43 30 7 31 24 41 --- 13 | 93 94 95 93 93 99 91 --- 92
R20 | 737 38 42 37 15 38 52 17 --- 14 | 114 119 109 116 130 100 116 --- 113
R21 | 852 29 34 22 13 31 12 23 29 9 | 261 259 266 259 256 259 247 262 257
R22 | 700 37 40 21 13 21 19 29 --- 10 | 79 83 80 78 83 66 69 --- 75
R23 | 798 11 17 17 11 16 21 20 --- 7 | 21 24 23 25 25 28 23 --- 21
R24 | 1415 17 33 48 28 26 44 20 --- 14 | 35 48 47 34 37 33 22 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1365 27 32 26 17 24 28 22 129 |T 120 122 121 121 122 120 118 143 118
WRMS | 1365 29 33 26 14 27 31 22 129 |NE 148 152 150 146 149 144 144 262 144
MEDI | 998 23 28 19 12 20 23 20 129 |MD 62 66 72 68 70 69 69 111 67
Table 3.1967.6 GPS week: 1967 Day: 6 MJD: 58019
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 493 24 55 15 18 31 35 19 --- 10 | 100 116 106 99 108 102 110 --- 99
R02E | 2355 16 17 15 13 11 27 16 177 7 | 130 129 118 123 124 130 127 117 124
R03E | 830 19 27 15 8 20 14 21 128 7 | 9999 9999 9999 9999 9999 9999 9999 9999 9999
R04E | 1719 15 19 15 7 19 20 15 --- 6 | 78 79 74 75 72 83 77 --- 75
R05E | 1462 30 30 24 18 26 33 42 --- 13 | 9999 9999 9999 9999 9999 9999 9999 --- 9999
R06E | 736 25 98 26 23 15 22 21 --- 10 | 64 104 66 76 67 71 62 --- 67
R07E | 1036 17 11 13 11 14 28 14 141 7 | 74 77 73 73 76 83 66 47 72
R08E | 1500 15 15 14 12 19 26 16 --- 7 | 91 91 97 91 97 102 85 --- 92
R09E | 1287 13 17 18 10 11 16 14 --- 6 | 343 344 340 322 338 347 338 --- 335
R10 | 1871 27 22 24 28 18 32 14 --- 11 | 74 75 77 87 77 75 80 --- 78
R11 | 1471 22 21 12 8 33 25 19 245 9 | 9999 9999 9999 9999 9999 9999 9999 9999 9999
R13 | 1089 10 13 12 12 13 17 14 --- 6 | 9999 9999 9999 9999 9999 9999 9999 --- 9999
XR14 | 1040 30 40 --- --- --- 54 33 --- 28 | 9999 9999 --- --- --- 9999 9999 --- 9999
R15 | 3629 57 50 26 16 29 25 21 --- 13 | 163 162 160 162 159 164 159 --- 160
R16 | 737 39 34 21 9 34 33 25 --- 12 | 9999 9999 9999 9999 9999 9999 9999 --- 9999
R17 | 1026 25 20 25 8 24 18 18 --- 8 | 64 64 67 68 65 62 55 --- 63
R18 | 624 17 27 20 15 18 20 11 --- 7 | 957 953 952 955 952 950 959 --- 954
R19 | 746 35 32 33 13 16 22 38 --- 12 | 138 140 140 132 136 136 130 --- 134
R20 | 650 37 56 44 16 24 47 19 --- 14 | 185 193 195 186 175 181 174 --- 182
R21 | 732 27 30 21 9 24 16 21 47 8 | 437 440 437 425 421 427 427 425 428
R22 | 849 31 35 21 11 22 17 30 --- 9 | 94 98 88 96 94 89 78 --- 89
R23 | 1407 18 24 25 22 9 26 20 --- 9 | 30 32 28 45 33 40 32 --- 33
XR24 | 1269 14 21 46 18 --- 27 22 --- 13 | 41 46 47 47 --- 42 42 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1436 27 37 22 15 22 26 22 161 |T 180 184 180 180 187 181 176 196 177
WRMS | 1436 29 30 22 14 15 27 22 161 |NE 218 220 219 220 234 216 213 425 216
MEDI | 1040 24 27 21 12 19 25 19 141 |MD 94 104 97 96 97 102 85 117 92
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