[IGSREPORT-25536] Wk 1966 IGLOS Final Orbits
acc
acc at igs.org
Mon Oct 2 04:14:13 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1966 (Sep 10, 2017 - Sep 16, 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 2.1966.
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:
igl1966[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1966 in the SP3 format.
igl19667.sum Combination Report for GPS Week 1966.
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 | 0.2 ns
1 | -1.3 ns
2 | -0.2 ns
3 | -0.3 ns
4 | -1.1 ns
5 | 1.2 ns
6 | 0.1 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
----+--------+---------------
6 | IAC | R01
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 1.1966, 1a.1966).
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 2.1966.0-6)
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 3.1966.0-6).
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 1966 summary. (Sep 10, 2017 - Sep 16, 2017)
Table 1.1966.a GPS week : 1966 MJD: 58006.0-58012.0
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 0 3 -14 16 -4 .03 28 28 | 11157 1670 3413 10864
| 1 0 1 12 13 43 .03 | 2387 6292
cof n/a| 0 0 4 -4 14 -6 .12 30 30 | 11152 1676 3415 10863
| 1 1 1 23 25 41 .06 | 2386 6283
emx n/a| 0 1 -8 3 -26 24 .13 26 26 | -1904 -1311 3362 10019
| 1 1 1 33 20 30 .03 | 5302 688
esx n/a| 0 0 0 -12 25 -24 .19 15 14 | 3708 -820 3348 12278
| 1 0 2 10 15 25 .03 | 5740 2377
gfz n/a| 0 1 0 -9 22 62 .02 22 21 | 0 -1474 3356 10492
| 1 0 2 29 12 42 .05 | 0 1204
grg n/a| -2 0 0 -42 16 -137 -.36 30 27 | -38923 74756 3356 9420
| 1 1 4 16 31 100 .05 | 99587 191234
iac n/a| 1 0 2 52 -43 41 -.13 64 19 | 934 -664 3736 10206
| 1 0 2 28 36 40 .05 | 1050 979
mcc n/a| 14 8 82 562 315 1763 -2.73 1333 1333 | --- --- --- ---
| 182 25 127 1299 1048 2690 8.30 | --- ---
Table 1.1966.b GPS week : 1966 MJD: 58006.0-58012.0
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 10 10 10 14 12 12 |
R02 | 7 9 8 8 7 7 7 |
R03 | 8 7 8 8 8 8 8 |
R04 | 8 7 7 8 8 8 10 |
R05 | 12 11 14 11 11 11 12 |
R06 | 8 9 9 10 12 9 9 |
R07 | 8 8 8 10 9 7 7 |
R08 | 8 8 9 9 9 7 6 |
R09 | 12 14 7 8 8 14 8 |
R10 | 6 7 8 6 7 9 9 |
R11 | 9 9 7 7 7 8 9 |
R13 | 8 6 7 9 6 6 7 |
R15 | 15 17 15 14 15 11 10 |
R16 | 17 16 15 18 12 11 10 |
R17 | 8 9 8 8 11 10 11 |
R18 | 7 8 10 8 7 8 8 |
R19 | 11 10 10 11 9 11 10 |
R20 | 12 10 18 10 11 15 14 |
R21 | 9 11 10 10 10 8 8 |
R22 | 7 8 9 11 9 10 9 |
R23 | 9 7 7 7 8 8 8 |
R24 | 13 18 20 17 10 11 12 |
R26 | 32 22 13 14 17 18 26 |
Table 1.1966.c GPS week : 1966 MJD: 58006.0-58012.0
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 1966 0 | -110 -72 -11 -193 128 1808 111.0 >>>>> >>>>> | 178 0
brd 1966 1 | -12 -123 -23 -984 70 -920 104.5 >>>>> >>>>> | -1303 0
brd 1966 2 | -26 -50 29 1139 -799 3404 83.8 1169 1169 | -181 0
brd 1966 3 | 20 26 11 685 988 2765 83.8 1239 1239 | -283 0
brd 1966 4 | 1 18 80 -469 1231 2145 84.3 1607 1607 | -1117 0
brd 1966 5 | 0 -59 61 -1686 312 4815 84.9 1607 1607 | 1174 0
brd 1966 6 | 104 20 158 -1801 -390 4189 85.2 1726 1726 | 60 0
-------------+------------------------------------------------------------+----------------
brd 1966 mean| -3 -34 43 -472 220 2600 91.1 >>>>> >>>>> | -210 0
brd 1966 sdev| 63 57 62 1119 714 1885 11.6 >>>>> >>>>> | 832 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 2.1966.0 GPS week: 1966 Day: 0 MJD: 58006
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 3 -5 -3 -78 .02 32 31 | 12595 1033 3581 10727
cof n/a| 0 -2 6 -28 -16 -57 .14 33 32 | 12586 1051 3593 10729
emx n/a| -1 0 -9 42 -24 -15 .09 27 27 | -9591 -843 3504 9462
esx n/a| -1 0 -2 -27 28 12 .19 16 15 | 4533 -129 3518 10830
gfz n/a| 0 0 1 8 12 108 .04 21 20 | 0 72 3532 9954
grg n/a| -2 0 0 -32 22 -226 -.27 32 24 | -389 1257 3513 8983
iac n/a| 2 0 3 22 -27 60 -.15 14 14 | 360 173 3842 10343
mcc n/a| -23 3 23 349 -59 525 -.67 132 132 | --- --- --- ---
Table 2.1966.1 GPS week: 1966 Day: 1 MJD: 58007
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 -27 32 -29 .03 31 31 | 6231 15640 4080 12422
cof n/a| 2 0 5 -21 -1 -43 .05 35 34 | 6234 15622 4078 12421
emx n/a| 0 0 -10 22 -41 2 .11 28 29 | -8854 -2477 4048 11390
esx n/a| 0 -2 1 -10 30 -55 .21 15 14 | 12574 -1810 4035 13687
gfz n/a| 0 0 0 0 18 55 .09 21 18 | 0 -2976 4030 12048
grg n/a| -5 2 0 -60 43 -172 -.39 38 34 | -588 -1180 4054 10583
iac n/a| 0 0 1 40 -46 82 -.17 16 16 | -854 -788 4291 11489
mcc n/a| 2 3 26 -63 -161 -552 -.42 202 202 | --- --- --- ---
Table 2.1966.2 GPS week: 1966 Day: 2 MJD: 58008
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -1 1 5 22 22 .03 29 29 | 11408 -1250 3415 11432
cof n/a| -1 0 3 24 32 37 .12 32 31 | 11390 -1215 3415 11433
emx n/a| 1 3 -6 40 -47 79 .16 34 33 | -267 -1095 3385 10439
esx n/a| 0 0 -2 3 54 -22 .15 15 14 | 8935 1240 3362 12384
gfz n/a| 0 1 -3 -39 40 122 -.07 22 20 | 0 -1290 3370 10727
grg n/a| -3 0 2 -62 56 -230 -.31 31 30 | 793 -1755 3355 9898
iac n/a| 1 1 4 27 -109 3 -.15 20 20 | 227 -80 4453 10647
mcc n/a| 355 53 20 3451 2619 4908-21.05 4308 4308 | --- --- --- ---
Table 2.1966.3 GPS week: 1966 Day: 3 MJD: 58009
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 3 -14 11 47 .07 29 29 | 11975 -846 3268 10017
cof n/a| -1 0 4 25 -4 21 .10 29 30 | 11966 -833 3269 10014
emx n/a| 0 1 -9 -19 -41 34 .08 25 23 | 2042 -1130 2995 9300
esx n/a| 0 0 0 -9 15 3 .25 16 15 | -2852 -43 2974 11294
gfz n/a| -1 2 0 -31 28 57 .03 21 21 | 0 -734 2989 9801
grg n/a| -1 0 -2 -47 25 -196 -.39 27 26 | -9809 18181 2971 8465
iac n/a| 2 0 6 83 -42 25 -.16 20 20 | 1933 -2204 3992 9612
mcc n/a| 6 -18 46 272 60 520 -.42 283 283 | --- --- --- ---
Table 2.1966.4 GPS week: 1966 Day: 4 MJD: 58010
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 2 -14 4 -17 -.01 26 26 | 12993 -1900 3635 10398
cof n/a| 1 0 4 -10 13 33 .24 30 29 | 13001 -1914 3629 10394
emx n/a| -2 2 -6 -47 -10 18 .17 23 21 | -1360 -1508 3647 9783
esx n/a| 0 0 3 -4 4 -25 .18 16 14 | -3140 -1443 3639 12382
gfz n/a| -1 2 1 -35 1 63 .04 23 28 | 0 -2595 3635 10317
grg n/a| 0 0 -2 -47 -29 -139 -.37 23 22 | -264591 508136 3647 9230
iac n/a| 3 0 3 100 9 86 -.11 19 18 | 1635 -1754 3654 9739
mcc n/a| 24 -4 49 269 374 128 -1.07 200 200 | --- --- --- ---
Table 2.1966.5 GPS week: 1966 Day: 5 MJD: 58011
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 6 -13 30 33 .05 26 28 | 12789 -2078 2981 10813
cof n/a| -1 0 6 4 55 14 .13 27 30 | 12790 -2081 2989 10816
emx n/a| -1 1 -8 -4 10 40 .15 25 25 | 534 -1782 3004 10195
esx n/a| 3 0 2 -15 17 -39 .17 14 13 | 3070 -5342 2987 13066
gfz n/a| 0 0 -2 -11 22 28 -.02 22 21 | 0 -2449 2989 10433
grg n/a| 0 0 -3 -19 18 24 -.38 31 29 | 2323 -2093 3012 9566
iac n/a| 1 0 1 51 -60 -19 -.14 17 17 | 1905 -360 2974 10025
mcc n/a| -273 31 371 -405 -493 6324 4.58 4100 4100 | --- --- --- ---
Table 2.1966.6 GPS week: 1966 Day: 6 MJD: 58012
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 0 2 -30 13 -13 .05 23 24 | 10109 1093 2934 10239
cof n/a| 0 2 2 -28 25 -48 .10 26 25 | 10098 1107 2934 10239
emx n/a| -1 1 -7 -9 -28 13 .12 22 22 | 4163 -348 2954 9568
esx n/a| 2 0 0 -21 27 -45 .17 15 14 | 2838 1782 2924 12308
gfz n/a| 1 0 1 42 30 0 .02 20 20 | 0 -348 2948 10167
grg n/a| -1 0 10 -25 -22 -22 -.41 27 27 | -206 746 2940 9218
iac n/a| 0 0 -2 43 -29 49 -.04 343 29 | 1332 362 2950 9589
mcc n/a| 7 -11 41 61 -129 491 -.09 109 109 | --- --- --- ---
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 3.1966.0 GPS week: 1966 Day: 0 MJD: 58006
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 |>>>>> 52 53 19 10 21 30 16 --- 10 | 69 69 71 71 72 70 173 --- 68
R02E |>>>>> 26 23 18 7 18 23 11 177 7 | 124 122 135 128 127 125 131 622 128
R03E |>>>>> 31 31 21 10 22 23 9 172 8 | 79 75 74 73 81 81 74 915 75
R04E |>>>>> 29 28 20 11 20 16 8 --- 7 | 29 29 30 28 33 27 26 --- 26
R05E |>>>>> 32 32 29 25 27 30 25 --- 12 | 37 36 43 55 53 50 40 --- 42
R06E |>>>>> 30 38 20 16 14 16 15 --- 8 | 96 98 95 95 93 100 99 --- 96
R07E |>>>>> 34 34 18 7 21 19 13 131 8 | 93 94 91 91 90 85 88 417 89
R08E |>>>>> 31 36 23 11 18 21 10 --- 8 | 69 75 70 68 65 67 67 --- 66
R09 |>>>>> 11 16 23 18 20 62 11 --- 11 | 28 32 30 30 36 91 36 --- 34
R10 |>>>>> 18 20 14 8 12 15 9 --- 5 | 40 42 32 48 33 44 35 --- 38
R11 |>>>>> 31 33 25 10 28 13 13 63 8 | 59 58 46 52 44 53 44 633 47
R13 |>>>>> 12 12 25 25 11 16 8 --- 8 | 48 51 41 59 43 39 43 --- 45
R15 |>>>>> 62 63 36 26 28 23 24 --- 14 | 72 74 48 37 29 41 22 --- 33
R16 |>>>>> 40 41 58 23 18 66 18 --- 16 | 58 59 45 63 46 63 52 --- 52
R17 |>>>>> 26 27 21 12 19 23 16 --- 8 | 25 26 23 24 17 25 18 --- 19
R18 |>>>>> 22 24 17 14 23 14 6 --- 7 | 16 20 20 22 17 12 12 --- 13
R19 |>>>>> 40 35 34 16 28 25 12 --- 11 | 27 31 28 22 22 18 15 --- 17
R20 |>>>>> 22 21 35 19 32 48 11 --- 12 | 24 29 36 40 43 27 23 --- 30
R21 |>>>>> 31 38 20 8 18 28 17 75 8 | 30 32 33 26 24 28 21 842 24
R22 |>>>>> 20 24 13 13 12 15 17 --- 6 | 29 34 28 33 35 26 22 --- 27
R23 |>>>>> 16 18 29 25 9 26 10 --- 9 | 23 26 27 35 31 20 22 --- 24
R24 |>>>>> 29 42 31 15 24 64 16 --- 13 | 39 48 44 35 36 33 30 --- 30
XR26 | 2872 52 51 --- --- --- --- 19 --- 31 | 29 34 --- --- --- --- 41 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 32 33 27 16 21 32 14 132 |T 49 51 49 51 48 51 49 685 46
WRMS |>>>>> 31 32 27 15 20 24 14 132 |NE 36 39 34 37 32 37 29 737 31
MEDI |>>>>> 30 32 21 13 20 23 13 131 |MD 39 42 41 40 36 41 36 633 36
Table 3.1966.1 GPS week: 1966 Day: 1 MJD: 58007
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 |>>>>> 44 36 25 11 23 27 12 --- 10 | 62 62 59 63 69 73 169 --- 63
R02E |>>>>> 30 36 17 14 22 30 16 386 9 | 84 86 89 89 90 73 81 9999 84
R03E |>>>>> 28 31 14 7 17 16 10 144 6 | 79 81 77 79 79 82 78 9999 78
R04E |>>>>> 21 20 17 11 18 18 7 --- 6 | 26 26 29 29 35 34 29 --- 28
R05E |>>>>> 30 28 20 19 23 35 22 --- 10 | 38 42 35 46 51 60 40 --- 42
R06E |>>>>> 22 20 22 20 14 38 10 --- 9 | 97 95 86 99 100 111 93 --- 96
R07E |>>>>> 28 37 20 11 21 19 17 157 8 | 78 81 80 82 85 87 86 423 82
R08E |>>>>> 25 25 19 10 18 22 16 --- 7 | 71 72 72 71 79 70 69 --- 70
R09 |>>>>> 14 13 25 22 16 88 10 --- 14 | 23 25 39 25 35 85 32 --- 29
R10 |>>>>> 16 23 20 15 8 18 12 --- 6 | 34 41 21 37 37 35 26 --- 29
R11 |>>>>> 33 33 18 11 21 22 16 79 8 | 44 45 34 39 35 35 28 827 33
R13 |>>>>> 11 11 24 9 11 19 10 --- 6 | 32 34 28 35 35 29 25 --- 28
R15 |>>>>> 67 69 40 16 45 31 27 --- 16 | 40 43 29 27 38 21 18 --- 19
R16 |>>>>> 31 36 65 22 15 60 16 --- 15 | 51 57 40 38 31 32 34 --- 31
R17 |>>>>> 26 27 25 12 20 19 22 --- 9 | 18 22 22 23 20 23 13 --- 17
R18 |>>>>> 21 22 22 15 17 23 18 --- 8 | 13 14 14 26 23 21 14 --- 14
R19 |>>>>> 38 48 21 18 24 27 15 --- 10 | 17 25 18 18 14 28 18 --- 12
R20 |>>>>> 12 37 29 11 17 46 17 --- 9 | 44 62 39 34 26 25 17 --- 26
R21 |>>>>> 36 36 29 13 29 35 10 63 10 | 21 19 21 32 33 23 20 940 21
R22 |>>>>> 25 30 22 17 16 19 13 --- 8 | 21 22 23 31 30 26 16 --- 21
R23 |>>>>> 10 13 25 15 13 22 9 --- 7 | 22 29 20 29 32 22 19 --- 21
R24 |>>>>> 51 70 50 11 25 81 27 --- 17 | 55 69 40 28 29 22 18 --- 26
XR26 | 2301 30 46 --- --- --- --- 15 --- 21 | 28 58 --- --- --- --- 43 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 31 35 28 15 21 38 16 202 |T 43 48 41 44 45 46 42 730 39
WRMS |>>>>> 31 34 29 14 18 34 16 202 |NE 30 37 27 30 29 30 22 883 24
MEDI |>>>>> 28 31 22 13 18 23 15 144 |MD 38 43 34 34 35 32 28 827 29
Table 3.1966.2 GPS week: 1966 Day: 2 MJD: 58008
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 | 794 41 49 25 10 24 19 20 --- 10 | 97 104 85 95 99 97 128 --- 94
R02E | 2052 25 24 16 11 15 18 17 4566 7 | 68 67 72 71 74 68 63 9999 68
R03E | 854 30 28 23 9 20 14 11 4876 7 | 45 44 33 40 39 45 40 9999 38
R04E | 1283 22 19 17 7 16 22 8 --- 6 | 34 33 33 34 33 35 30 --- 30
R05E | 1286 30 32 30 18 29 45 35 --- 13 | 31 43 31 32 38 38 29 --- 25
R06E | 1853 20 21 21 21 13 24 17 --- 8 | 74 75 75 63 63 70 71 --- 66
R07E | 779 30 31 22 7 23 19 8 --- 8 | 101 103 98 103 107 98 103 --- 101
R08E | 787 21 22 31 16 23 15 13 --- 8 | 95 97 98 103 86 96 96 --- 95
R09 | 1708 10 15 17 13 18 19 11 --- 6 | 28 28 32 30 40 28 39 --- 31
R10 | 1267 10 16 18 23 18 15 18 --- 8 | 31 34 40 47 27 30 29 --- 33
R11 | 1426 23 21 14 11 18 15 18 3790 7 | 39 37 35 37 30 31 33 9999 33
R13 | 905 13 15 15 16 17 18 15 --- 7 | 31 34 35 43 32 41 32 --- 34
R15 | 1907 62 59 35 8 34 28 35 --- 15 | 55 51 42 29 24 37 19 --- 25
R16 | 700 30 46 62 13 23 47 24 --- 14 | 43 47 36 44 39 32 46 --- 37
R17 | 865 20 19 19 9 14 15 23 --- 7 | 19 21 22 27 25 26 17 --- 20
R18 | 838 26 29 34 20 23 19 11 --- 9 | 16 19 25 32 22 20 22 --- 20
R19 | 609 37 35 25 15 21 28 16 --- 10 | 25 27 25 28 26 17 20 --- 19
R20 | 913 33 40 77 17 17 68 18 --- 17 | 46 51 59 31 32 30 19 --- 20
R21 | 679 37 39 32 6 25 26 12 3904 10 | 22 25 25 22 18 33 19 9999 18
R22 | 574 27 22 24 8 23 16 19 --- 8 | 22 23 21 22 25 27 21 --- 20
R23 | 680 11 16 13 16 13 18 15 --- 6 | 18 22 19 22 21 20 23 --- 17
R24 | 1038 32 43 66 25 38 68 40 --- 19 | 42 48 43 43 30 39 19 --- 29
XR26 | 3122 15 35 --- --- --- --- 12 --- 13 | 18 45 --- --- --- --- 28 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1168 29 31 33 15 22 31 20 4308 |T 43 46 44 45 42 43 41 --- 38
WRMS | 1168 29 31 33 14 20 30 20 4308 |NE 30 34 32 32 27 29 25 --- 25
MEDI | 905 26 28 23 13 20 19 17 3904 |MD 34 43 35 34 32 33 29 --- 30
Table 3.1966.3 GPS week: 1966 Day: 3 MJD: 58009
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 | 874 43 48 24 9 26 22 13 --- 10 | 81 77 72 67 73 73 173 --- 67
R02E | 3301 25 27 25 9 14 19 16 74 8 | 68 68 80 69 68 58 64 9999 67
R03E | 785 26 25 22 15 15 14 9 202 7 | 92 90 86 79 86 89 88 9999 84
R04E | 900 20 24 16 12 20 19 14 --- 7 | 43 44 46 45 43 43 37 --- 41
R05E | 802 25 23 21 17 25 28 31 --- 11 | 36 36 31 39 47 37 39 --- 34
R06E | 1405 17 17 26 27 18 23 16 --- 10 | 115 118 106 126 120 127 124 --- 119
R07E | 785 37 35 19 14 21 15 25 576 9 | 80 85 72 76 73 74 59 484 69
R08E | 764 23 24 20 12 18 19 28 --- 9 | 102 105 109 114 103 99 93 --- 103
R09 | 1503 16 15 16 15 16 25 12 --- 7 | 26 26 29 29 40 28 29 --- 26
R10 | 1518 11 16 15 15 17 12 11 --- 6 | 29 28 25 35 26 25 30 --- 27
R11 | 645 18 17 12 6 18 19 17 131 6 | 38 35 24 29 17 32 24 9999 25
R13 | 865 15 18 18 24 9 31 19 --- 9 | 35 36 32 44 33 30 32 --- 30
R15 | 1809 57 49 35 16 30 21 26 --- 13 | 55 51 37 24 29 30 15 --- 24
R16 | 996 28 35 55 26 15 58 40 --- 17 | 55 56 45 65 45 34 43 --- 45
R17 | 711 24 31 18 12 15 18 17 --- 7 | 21 23 16 22 27 22 16 --- 16
R18 | 795 25 26 18 18 24 15 10 --- 8 | 18 19 19 28 20 20 17 --- 19
R19 | 659 43 44 19 12 32 21 13 --- 10 | 29 30 26 23 24 25 21 --- 20
R20 | 628 19 23 33 11 15 30 14 --- 9 | 27 37 39 32 33 28 19 --- 24
R21 | 536 35 35 27 9 19 16 25 64 9 | 30 30 31 26 27 24 23 9999 23
R22 | 490 29 34 17 18 28 33 20 --- 10 | 28 32 24 30 26 33 16 --- 23
R23 | 718 10 12 18 17 10 20 11 --- 6 | 15 15 26 29 19 22 19 --- 18
R24 | 1961 37 28 41 20 38 61 26 --- 16 | 32 32 34 38 35 34 29 --- 28
XR26 | 2853 17 129 --- --- --- --- 11 --- 13 | 32 145 --- --- --- --- 22 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1238 29 29 25 16 21 27 20 283 |T 47 52 45 48 46 44 44 484 41
WRMS | 1238 29 30 23 15 21 26 20 283 |NE 31 39 29 32 28 27 23 --- 24
MEDI | 802 25 26 19 15 18 20 16 131 |MD 35 36 32 35 33 32 29 484 27
Table 3.1966.4 GPS week: 1966 Day: 4 MJD: 58010
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 | 970 44 43 26 24 32 23 33 --- 13 | 190 198 196 203 197 200 119 --- 194
R02E | 4441 23 27 17 12 18 22 7 86 7 | 40 41 39 40 41 40 41 9999 37
R03E | 1262 24 33 17 11 19 14 16 356 7 | 81 83 76 72 73 71 81 453 75
R04E | 700 22 19 19 10 18 15 16 --- 7 | 53 53 50 52 56 59 56 --- 52
R05E | 1236 24 19 20 21 25 33 25 --- 11 | 34 34 29 44 46 39 34 --- 33
R06E | 528 20 15 28 32 14 17 30 --- 11 | 76 87 80 108 93 80 69 --- 83
R07E | 982 26 27 24 10 23 22 9 183 8 | 103 106 96 103 109 113 109 9999 104
R08E | 960 23 22 20 15 21 27 15 --- 9 | 95 95 96 93 100 110 96 --- 96
R09 | 1833 8 16 17 13 17 29 13 --- 7 | 27 28 28 25 39 31 28 --- 26
R10 | 1719 7 12 18 14 18 13 12 --- 6 | 22 30 20 32 22 26 34 --- 24
R11 | 720 18 18 15 9 23 11 15 176 6 | 39 36 39 38 35 34 43 9999 37
R13 | 1643 13 16 12 16 14 12 14 --- 6 | 30 36 28 40 28 33 42 --- 33
R15 | 1571 49 54 28 20 47 27 27 --- 14 | 39 43 27 18 24 29 21 --- 18
R16 | 1218 24 34 44 15 17 37 19 --- 12 | 60 67 49 47 47 41 54 --- 45
R17 | 793 33 33 26 15 24 16 25 --- 10 | 17 27 27 30 26 14 19 --- 18
R18 | 559 22 23 20 14 17 13 11 --- 7 | 21 26 17 18 24 13 16 --- 15
R19 | 1107 34 35 14 14 19 12 23 --- 9 | 30 33 24 29 21 34 21 --- 23
R20 | 751 26 60 16 18 37 31 17 --- 11 | 43 75 56 39 27 22 32 --- 30
R21 | 643 27 33 26 15 24 28 18 46 10 | 23 28 28 25 23 30 19 9999 21
R22 | 511 30 27 17 10 21 23 14 --- 8 | 27 31 24 25 21 19 24 --- 22
R23 | 1501 11 14 23 20 15 18 12 --- 7 | 23 26 33 23 27 24 21 --- 22
R24 | 3344 26 18 27 16 20 34 12 --- 10 | 32 38 41 37 28 32 29 --- 25
XR26 | ---- 21 84 --- --- --- --- 12 --- 16 | 35 94 --- --- --- --- 34 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1606 26 30 23 16 23 23 19 200 |T 49 57 50 51 50 49 45 453 46
WRMS | 1606 26 29 21 14 28 22 18 200 |NE 31 41 31 30 28 27 29 --- 25
MEDI | 982 24 27 20 15 19 22 15 176 |MD 35 38 33 38 28 33 34 453 30
Table 3.1966.5 GPS week: 1966 Day: 5 MJD: 58011
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 | 1928 37 30 30 19 29 22 26 --- 12 | 155 158 154 168 169 152 291 --- 156
R02E | 2828 19 17 16 12 17 24 12 4553 7 | 105 107 112 110 105 92 111 9999 107
R03E | 1289 23 21 24 12 17 20 15 --- 8 | 140 137 136 130 127 135 134 --- 132
R04E | 662 18 22 24 8 16 16 20 --- 7 | 68 68 75 62 64 64 56 --- 62
R05E | 1195 18 20 27 23 20 26 31 --- 11 | 66 67 61 77 69 66 57 --- 64
R06E | 893 21 22 25 20 12 27 15 --- 9 | 89 88 83 85 85 97 91 --- 87
R07E | 2353 23 24 15 10 19 22 12 4115 7 | 58 60 58 58 62 74 61 9999 59
R08E | 2367 19 17 18 8 18 21 12 --- 6 | 87 87 96 91 93 107 90 --- 93
R09 | 1692 17 22 17 8 26 78 18 --- 13 | 27 28 28 39 29 74 36 --- 34
R10 | 1093 24 24 23 22 15 10 15 --- 8 | 31 33 30 34 26 17 34 --- 26
R11 | 742 28 31 16 9 25 23 14 3936 8 | 35 37 30 39 39 37 31 9999 33
R13 | 2281 10 14 15 9 12 24 14 --- 6 | 33 36 35 40 37 35 33 --- 34
R15 | 1468 47 42 27 12 29 14 20 --- 11 | 37 37 39 32 26 30 31 --- 30
R16 | 728 23 17 27 17 23 41 20 --- 11 | 62 53 50 56 49 39 53 --- 50
R17 | 910 31 34 28 7 32 26 18 --- 10 | 24 28 20 31 33 36 23 --- 24
R18 | 685 21 23 21 15 19 11 15 --- 7 | 20 23 20 30 25 21 26 --- 21
R19 | 1373 40 39 25 16 22 25 15 --- 10 | 22 25 23 30 34 24 22 --- 23
R20 | 1104 39 39 52 17 29 54 15 --- 14 | 50 54 51 32 33 21 27 --- 30
R21 | 976 15 20 17 11 23 26 14 3752 7 | 27 31 31 37 35 24 28 9999 30
R22 | 589 26 33 26 10 30 26 15 --- 9 | 22 25 26 28 25 30 20 --- 22
R23 | 1414 24 22 26 16 12 14 13 --- 8 | 21 21 23 27 25 31 25 --- 23
R24 | 3065 20 34 32 16 19 47 16 --- 11 | 48 56 33 40 29 26 30 --- 31
XR26 | ---- 23 203 --- --- --- --- 13 --- 17 | 28 180 --- --- --- --- 28 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1606 26 27 25 14 22 31 17 4100 |T 54 62 55 58 55 56 58 --- 52
WRMS | 1606 28 30 25 13 21 29 17 4100 |NE 32 44 31 35 31 31 29 --- 29
MEDI | 1195 23 23 24 12 19 24 15 3936 |MD 37 53 35 39 35 36 33 --- 33
Table 3.1966.6 GPS week: 1966 Day: 6 MJD: 58012
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 | 1872 33 38 25 18 25 19 1610 --- 12 | 178 176 172 170 173 173 270 --- 171
R02E | 1784 17 16 17 13 16 20 15 66 7 | 106 106 108 105 104 101 102 9999 103
R03E | 2476 23 28 18 14 18 23 13 147 8 | 141 140 131 128 138 148 135 561 135
R04E | 1067 20 25 23 14 19 38 17 --- 9 | 103 101 96 114 116 101 110 --- 107
R05E | 887 20 23 24 22 26 43 20 --- 11 | 42 42 31 45 50 44 41 --- 38
R06E | 1458 25 21 15 15 13 36 14 --- 9 | 76 77 79 77 75 83 70 --- 74
R07E | 3512 20 15 15 8 17 14 14 116 6 | 80 80 77 76 77 81 78 9999 77
R08E | 2960 15 13 16 11 15 17 9 --- 6 | 100 99 95 102 100 101 101 --- 99
R09 | 1601 15 19 13 17 13 25 16 --- 7 | 29 33 26 30 35 51 30 --- 29
R10 | 857 19 15 14 15 16 19 27 --- 8 | 42 40 31 50 35 44 36 --- 38
R11 | 842 28 29 19 15 26 11 22 111 9 | 50 52 37 42 33 40 32 9999 36
R13 | 1136 9 12 9 12 22 19 19 --- 7 | 38 43 36 49 46 39 36 --- 39
R15 | 2470 37 37 20 15 26 18 18 --- 10 | 61 61 49 40 36 42 33 --- 37
R16 | 729 25 48 21 16 13 40 23 --- 10 | 70 93 68 71 64 55 57 --- 62
R17 | 849 29 30 27 10 24 30 28 --- 11 | 29 31 28 26 22 40 20 --- 23
R18 | 670 19 19 22 11 22 16 20 --- 8 | 20 22 21 30 27 18 18 --- 20
R19 | 1862 33 40 25 11 16 21 21 --- 9 | 29 33 25 25 21 28 20 --- 21
R20 | 1674 29 19 41 17 11 51 26 --- 13 | 46 37 51 42 43 30 26 --- 34
R21 | 580 16 17 16 12 27 18 10 89 7 | 34 33 39 33 24 27 27 9999 28
R22 | 729 23 21 24 9 24 23 16 --- 8 | 36 39 35 31 28 37 23 --- 30
R23 | 1225 19 24 20 18 14 15 22 --- 8 | 21 26 22 33 23 26 25 --- 23
R24 | 2408 21 20 38 24 20 36 22 --- 12 | 63 62 39 47 43 48 30 --- 39
XR26 | ---- 30 155 --- --- --- --- 22 --- 26 | 37 166 --- --- --- --- 36 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1725 23 26 22 15 20 27 343 109 |T 62 69 58 62 59 61 58 561 56
WRMS | 1725 24 25 22 14 20 27 29 109 |NE 40 51 36 39 34 37 29 --- 32
MEDI | 1225 21 21 20 14 18 20 20 111 |MD 46 52 39 45 43 44 36 561 38
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