[IGSREPORT-25464] Wk 1961 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 25 05:04:29 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1961 (Aug 06, 2017 - Aug 12, 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 2.1961.
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:
igl1961[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1961 in the SP3 format.
igl19617.sum Combination Report for GPS Week 1961.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 1.2 ns
1 | 0.5 ns
2 | 0.4 ns
3 | 0.7 ns
4 | -0.3 ns
5 | 0.4 ns
6 | -1.2 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 1.1961, 1a.1961).
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 2.1961.0-6)
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 3.1961.0-6).
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 1961 summary. (Aug 06, 2017 - Aug 12, 2017)
Table 1.1961.a GPS week : 1961 MJD: 57971.0-57977.0
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 8 -36 8 5 .03 36 35 | 7492 -41 3152 10905
| 0 1 3 17 21 20 .02 | 1270 1035
cof n/a| 0 0 11 -23 11 21 .08 39 37 | 7499 -67 3152 10905
| 1 1 3 22 16 23 .04 | 1269 1022
emx n/a| -1 0 2 -3 -30 52 .05 23 22 | -1615 -260 3166 10178
| 0 1 3 12 19 16 .04 | 8009 813
esx n/a| 0 0 -2 4 18 -30 .15 16 14 | 1757 126 3189 12655
| 0 1 0 4 10 21 .03 | 10248 1342
gfz n/a| 0 0 -6 -33 60 8 .11 27 22 | 0 197 3174 10760
| 1 1 2 20 20 36 .05 | 0 1401
grg n/a| 0 0 2 -10 -11 -40 -.38 31 29 | 35 277 3155 10149
| 0 1 5 22 20 75 .05 | 359 1223
iac n/a| 1 0 -3 41 -37 8 -.15 23 23 | 1195 -127 3173 10009
| 1 1 2 17 39 66 .07 | 889 1104
mcc n/a| 0 -3 33 91 -79 -108 -.59 156 156 | --- --- --- ---
| 6 2 11 55 42 535 .38 | --- ---
Table 1.1961.b GPS week : 1961 MJD: 57971.0-57977.0
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 | 16 13 17 16 16 16 16 |
R02 | 14 11 9 14 12 11 11 |
R03 | 9 10 13 10 11 12 10 |
R04 | 9 10 11 10 10 9 10 |
R05 | 15 16 11 15 14 14 14 |
R06 | 11 11 11 12 11 9 10 |
R07 | 11 11 10 10 11 12 11 |
R08 | 8 9 8 9 9 10 11 |
R09 | 8 8 8 9 9 8 10 |
R10 | 9 7 8 7 7 9 6 |
R11 | 7 8 7 7 8 8 7 |
R13 | 7 7 7 7 8 8 8 |
R15 | 8 8 11 11 13 12 11 |
R16 | 15 12 13 12 12 13 11 |
R17 | 10 12 11 11 9 9 8 |
R18 | 8 8 9 8 8 11 9 |
R19 | 15 14 14 14 12 13 13 |
R20 | 15 13 15 13 13 14 12 |
R21 | 11 11 9 9 10 11 10 |
R22 | 11 10 9 9 11 11 8 |
R23 | 10 8 9 9 9 8 7 |
R24 | 15 19 15 16 18 20 16 |
R26 | 22 18 19 18 12 27 14 |
Table 1.1961.c GPS week : 1961 MJD: 57971.0-57977.0
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 1961 0 | 51 -4 154 -638 534 2986 82.8 1309 1309 | 1214 0
brd 1961 1 | -13 -41 239 383 -1357 3871 83.3 1282 1282 | 530 0
brd 1961 2 | -30 -65 216 1602 -1900 1965 82.4 1430 1430 | 357 0
brd 1961 3 | 62 -15 215 -248 -2313 3472 82.8 1425 1425 | 728 0
brd 1961 4 | -49 36 220 -318 -984 1691 84.2 41190 41190 | -347 0
brd 1961 5 | -26 10 182 698 -425 -574 83.8 1280 1280 | 395 0
brd 1961 6 | -8 -13 90 1503 -569 1068 82.9 1199 1199 | -1239 0
-------------+------------------------------------------------------------+----------------
brd 1961 mean| -2 -13 188 426 -1002 2068 83.2 7016 7016 | 234 0
brd 1961 sdev| 42 33 51 890 960 1538 .6 15069 15069 | 800 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 2.1961.0 GPS week: 1961 Day: 0 MJD: 57971
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 10 -22 31 12 .01 34 33 | 5385 1680 3547 10942
cof n/a| 1 0 16 -3 16 33 .14 40 37 | 5407 1615 3540 10941
emx n/a| -2 2 -1 -20 -40 63 .09 25 24 | 11002 571 3557 10225
esx n/a| 1 1 -2 6 21 -25 .17 17 16 | -11149 1111 3551 12454
gfz n/a| -1 0 -4 -55 47 -25 .12 27 21 | 0 1972 3568 10718
grg n/a| 0 0 3 32 -33 -83 -.41 30 28 | -119 2409 3525 9881
iac n/a| 2 -1 -2 36 -18 57 -.07 22 22 | 1128 1501 3562 10117
mcc n/a| 9 -4 13 40 -42 375 -.09 186 186 | --- --- --- ---
Table 2.1961.1 GPS week: 1961 Day: 1 MJD: 57972
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 14 -25 -16 43 .08 34 35 | 7976 641 3028 10725
cof n/a| 0 2 16 -1 -21 55 .11 35 35 | 7986 613 3028 10728
emx n/a| -2 0 3 -16 -34 55 .08 22 22 | -9151 302 3044 9861
esx n/a| 0 0 -2 3 14 -12 .12 17 16 | 4732 360 3033 12081
gfz n/a| -2 0 -6 -57 49 36 .08 26 23 | 0 501 3033 10454
grg n/a| 0 1 -8 -8 -8 -10 -.43 34 31 | -3 792 3032 9881
iac n/a| 1 0 0 67 -20 -64 -.15 21 21 | 2457 -581 3038 9844
mcc n/a| 0 -4 29 95 -76 -774 -.45 120 120 | --- --- --- ---
Table 2.1961.2 GPS week: 1961 Day: 2 MJD: 57973
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 7 -52 0 14 .03 37 35 | 7894 -433 3034 9514
cof n/a| -1 3 9 -54 15 6 .13 40 37 | 7897 -448 3032 9513
emx n/a| -1 0 -2 -14 -37 71 -.01 23 23 | -723 536 3052 8725
esx n/a| 0 0 -2 5 26 -57 .19 16 14 | -12332 445 3061 11479
gfz n/a| 0 -1 -11 -26 58 1 .18 26 20 | 0 655 3065 9428
grg n/a| 0 0 8 -8 -9 35 -.30 30 28 | 347 -38 3064 8791
iac n/a| 2 -1 -1 48 -44 -92 -.17 22 22 | 1480 -491 3061 8686
mcc n/a| -9 -3 29 82 -112 -711 -.29 140 140 | --- --- --- ---
Table 2.1961.3 GPS week: 1961 Day: 3 MJD: 57974
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 6 -32 44 -13 .01 35 32 | 8669 389 2978 11608
cof n/a| -1 0 9 -43 30 -21 .06 39 34 | 8665 380 2980 11608
emx n/a| -1 0 3 8 -6 23 .02 22 22 | 4065 103 3002 10971
esx n/a| 0 -1 -1 0 7 -28 .18 17 14 | 9629 -1017 2996 13284
gfz n/a| 0 0 -5 -23 57 21 .13 28 21 | 0 1213 3007 11474
grg n/a| 0 0 0 -11 -42 47 -.42 30 27 | 299 843 2986 10944
iac n/a| 2 0 -2 47 10 32 -.04 23 23 | 1445 1270 3007 10709
mcc n/a| -2 -5 39 184 -82 -196 -1.10 172 172 | --- --- --- ---
Table 2.1961.4 GPS week: 1961 Day: 4 MJD: 57975
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 9 -60 -2 -4 .03 38 39 | 6580 -240 3107 11401
cof n/a| 2 0 9 -15 8 20 .02 39 39 | 6575 -250 3115 11403
emx n/a| -2 0 0 3 0 51 .09 21 21 | 1606 -1130 3122 10688
esx n/a| 1 -1 -2 -3 26 -25 .15 17 14 | 11853 478 3268 13223
gfz n/a| -2 3 -3 -2 48 -41 .11 26 21 | 0 -1461 3127 11300
grg n/a| 0 0 5 -19 -11 -37 -.34 32 31 | -232 -335 3088 10772
iac n/a| 3 1 -5 44 -83 52 -.17 24 24 | 165 -708 3138 10481
mcc n/a| 1 -2 41 113 -138 343 -.85 176 176 | --- --- --- ---
Table 2.1961.5 GPS week: 1961 Day: 5 MJD: 57976
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -2 8 -13 4 -17 .06 35 33 | 9013 -938 3014 11261
cof n/a| 0 -1 8 -40 21 28 .06 37 34 | 9037 -980 3014 11260
emx n/a| -1 2 5 6 -51 38 .05 25 25 | -11779 -1194 3022 10498
esx n/a| 1 -2 -3 11 29 -60 .12 16 14 | 10867 1750 3056 13193
gfz n/a| 0 1 -8 -48 106 65 .03 28 25 | 0 427 3055 11119
grg n/a| 0 3 3 -43 13 -65 -.40 32 30 | 480 -249 3035 10613
iac n/a| -1 0 -8 37 -95 84 -.18 27 25 | 1769 -343 3042 10220
Table 2.1961.6 GPS week: 1961 Day: 6 MJD: 57977
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 4 -46 0 6 .02 41 38 | 6927 -1391 3358 10886
cof n/a| -3 0 14 -2 13 24 .06 41 40 | 6930 -1399 3357 10888
emx n/a| -1 0 5 5 -40 65 .02 21 21 | -6328 -1012 3363 10284
esx n/a| 0 0 -3 3 2 -1 .11 13 12 | -1301 -2244 3361 12871
gfz n/a| 1 2 -7 -20 56 -1 .15 27 25 | 0 -1922 3365 10829
grg n/a| -1 0 2 -16 9 -170 -.35 32 28 | -524 -1483 3361 10163
iac n/a| 1 0 -4 9 -11 -10 -.25 23 23 | -75 -1541 3363 10008
mcc n/a| 0 0 44 30 -24 314 -.77 141 141 | --- --- --- ---
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 3.1961.0 GPS week: 1961 Day: 0 MJD: 57971
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 | 624 65 63 34 19 40 25 30 --- 15 | 95 93 59 50 48 58 39 --- 48
R02 | 523 43 46 27 12 41 36 35 173 14 | 87 87 61 57 39 75 38 61 54
R03 | 1881 32 30 22 14 23 16 14 67 8 | 86 85 71 56 57 62 51 52 60
R04 | 1240 25 30 20 10 22 18 20 --- 8 | 81 83 72 64 54 60 53 --- 62
R05 | 544 42 65 29 28 26 52 26 --- 15 | 78 97 66 53 50 65 49 --- 55
R06 | 1852 20 21 25 27 13 35 20 --- 11 | 50 59 48 79 62 44 60 --- 58
R07 | 940 28 27 19 8 31 33 27 200 10 | 94 96 76 70 50 92 50 161 69
R08 | 490 22 29 17 9 21 15 27 --- 8 | 84 87 67 63 61 70 44 --- 62
R09 | 3144 17 23 22 12 14 22 16 --- 7 | 51 51 49 38 49 44 47 --- 43
R10 | 836 16 17 28 18 17 19 15 --- 8 | 63 65 53 72 56 60 61 --- 60
R11 | 618 21 30 10 12 17 21 17 305 7 | 77 84 60 73 57 59 62 109 64
R13 | 875 20 14 18 9 12 21 9 --- 6 | 76 73 60 69 60 65 64 --- 64
R15 | 1191 21 16 19 15 18 18 15 --- 7 | 97 98 81 95 84 95 84 --- 88
R16 | 2905 24 40 44 17 40 40 25 --- 14 | 86 97 55 79 57 79 71 --- 67
R17 | 678 42 49 21 9 33 10 21 --- 10 | 77 81 61 61 48 61 41 --- 56
R18 | 697 29 39 14 13 20 18 16 --- 8 | 59 66 48 55 47 52 42 --- 49
R19 | 831 54 59 32 27 18 31 33 --- 14 | 92 95 68 62 54 65 43 --- 58
R20 | 755 40 61 27 11 39 56 24 --- 14 | 86 84 63 59 41 62 47 --- 55
R21 | 964 40 41 22 9 37 15 22 74 10 | 76 77 65 57 42 59 45 86 55
R22 | 701 46 49 15 13 31 14 21 --- 10 | 80 82 63 55 48 75 53 --- 59
R23 | 1156 12 23 18 24 9 40 15 --- 10 | 45 48 39 56 46 45 45 --- 44
R24 | 736 22 31 42 30 23 41 25 --- 14 | 49 43 61 58 48 52 39 --- 50
XR26 | ---- 29 189 --- --- --- --- 15 --- 22 | 47 147 --- --- --- --- 36 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1309 34 40 25 17 27 30 22 186 |T 74 81 61 62 52 63 50 93 57
WRMS | 1309 33 37 24 16 21 28 22 186 |NE 74 81 61 62 52 63 50 93 57
MEDI | 831 28 31 22 13 22 21 21 173 |MD 78 84 61 59 50 61 47 86 58
Table 3.1961.1 GPS week: 1961 Day: 1 MJD: 57972
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 | 690 57 58 20 22 24 28 20 --- 12 | 60 62 37 32 30 44 33 --- 32
R02 | 1266 41 45 17 13 36 29 21 74 11 | 60 63 38 37 35 45 29 69 35
R03 | 1043 33 35 18 9 30 19 25 63 9 | 55 56 45 40 32 39 28 49 37
R04 | 1120 30 26 28 12 23 14 20 --- 9 | 57 55 51 34 37 41 29 --- 38
R05 | 678 42 28 26 23 25 74 24 --- 16 | 64 57 45 45 47 53 45 --- 44
R06 | 1792 17 15 20 29 14 41 14 --- 11 | 34 35 33 53 42 26 31 --- 35
R07 | 871 39 37 28 8 24 14 32 133 11 | 65 65 53 42 32 39 25 104 39
R08 | 629 24 25 17 10 28 29 22 --- 9 | 60 61 49 46 36 60 37 --- 45
R09 | 2982 14 15 17 18 16 19 17 --- 7 | 30 35 29 30 35 29 31 --- 27
R10 | 976 13 22 17 16 17 18 13 --- 7 | 38 45 33 42 39 30 34 --- 34
R11 | 1526 17 17 19 19 20 19 14 194 8 | 40 39 30 43 31 37 35 115 34
R13 | 1806 15 19 17 17 13 22 11 --- 7 | 47 51 35 42 38 36 42 --- 38
R15 | 1569 22 25 16 18 16 19 12 --- 7 | 58 60 52 63 49 62 55 --- 56
R16 | 1712 32 32 25 21 24 37 28 --- 12 | 75 68 42 55 57 58 50 --- 50
R17 | 560 41 45 24 6 34 29 28 --- 11 | 40 42 35 31 23 36 22 --- 27
R18 | 692 30 30 13 13 20 22 15 --- 8 | 32 32 24 29 20 23 25 --- 23
R19 | 737 53 54 28 20 42 29 22 --- 13 | 44 47 35 32 21 50 25 --- 28
R20 | 959 53 50 23 12 30 40 26 --- 13 | 62 59 49 45 33 37 29 --- 40
R21 | 766 36 33 18 14 33 29 23 84 10 | 38 37 35 29 23 50 24 61 29
R22 | 877 46 45 7 12 32 19 23 --- 10 | 41 42 27 34 25 30 22 --- 26
R23 | 1148 16 16 18 17 17 17 14 --- 7 | 23 28 26 32 29 25 22 --- 24
R24 | 1051 23 34 47 18 37 85 21 --- 18 | 32 43 48 44 42 35 22 --- 32
XR26 | ---- 25 113 --- --- --- --- 11 --- 17 | 16 106 --- --- --- --- 42 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1281 34 35 22 17 26 34 21 120 |T 46 51 38 40 34 40 32 79 34
WRMS | 1281 35 35 22 16 23 31 21 120 |NE 46 51 38 40 34 40 32 79 34
MEDI | 976 30 32 18 16 24 22 21 84 |MD 44 51 35 40 33 37 29 69 34
Table 3.1961.2 GPS week: 1961 Day: 2 MJD: 57973
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 | 666 69 65 18 32 41 57 18 --- 17 | 84 83 53 57 58 83 47 --- 53
R02 | 1392 32 34 20 11 22 16 27 74 9 | 69 71 60 59 45 59 46 36 54
R03 | 1565 36 34 30 10 38 16 37 101 12 | 70 69 66 62 52 68 52 28 58
R04 | 1324 33 37 28 7 27 17 32 --- 10 | 65 67 62 50 43 57 41 --- 50
R05 | 755 41 50 16 16 26 29 24 --- 10 | 68 81 56 61 63 59 52 --- 55
R06 | 1610 26 31 12 28 15 44 12 --- 11 | 37 44 55 67 47 51 48 --- 52
R07 | 693 37 41 25 11 17 14 25 91 9 | 76 77 67 61 56 68 48 58 60
R08 | 674 33 34 19 9 21 17 16 --- 8 | 72 73 56 44 41 57 42 --- 49
R09 | 3197 15 17 12 11 19 25 18 --- 7 | 29 29 29 30 37 42 30 --- 29
R10 | 1374 15 18 17 15 15 27 11 --- 7 | 53 48 48 58 45 61 49 --- 52
R11 | 2361 17 23 16 10 17 20 7 259 6 | 59 61 51 54 49 62 50 43 53
R13 | 1507 14 18 10 12 12 29 11 --- 7 | 64 62 57 58 54 71 54 --- 58
R15 | 840 17 18 15 20 25 44 16 --- 10 | 66 65 53 63 59 55 58 --- 56
R16 | 1669 28 63 25 20 22 41 36 --- 12 | 75 108 48 65 62 50 64 --- 57
R17 | 774 46 47 22 13 33 21 22 --- 11 | 64 65 55 55 47 48 37 --- 49
R18 | 566 33 35 19 14 22 25 13 --- 9 | 48 49 37 44 31 40 31 --- 36
R19 | 847 50 50 40 15 41 17 23 --- 13 | 60 61 56 41 31 43 31 --- 41
R20 | 686 68 76 36 18 33 30 23 --- 14 | 78 87 48 51 41 49 36 --- 44
R21 | 680 33 34 14 10 16 21 26 87 8 | 56 57 47 49 47 47 40 36 45
R22 | 1953 43 41 12 8 29 18 16 --- 9 | 62 61 55 46 45 60 42 --- 49
R23 | 842 10 12 24 22 16 22 12 --- 8 | 38 38 33 45 42 39 32 --- 37
R24 | 1928 36 37 43 15 23 54 21 --- 14 | 42 46 61 50 41 47 35 --- 43
XR26 | ---- 26 113 --- --- --- --- 13 --- 18 | 37 112 --- --- --- --- 32 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1429 37 40 23 16 26 30 22 140 |T 59 65 52 53 47 55 43 40 48
WRMS | 1429 35 37 23 14 20 28 22 140 |NE 59 65 52 53 47 55 43 40 48
MEDI | 847 33 35 19 13 22 22 18 91 |MD 64 65 55 54 45 55 42 36 50
Table 3.1961.3 GPS week: 1961 Day: 3 MJD: 57974
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 | 524 67 79 14 14 38 47 33 --- 15 | 76 88 30 34 31 63 26 --- 32
R02 | 1473 49 40 34 11 32 38 23 73 13 | 66 63 54 41 33 47 26 35 37
R03 | 1645 26 32 21 9 27 32 19 145 9 | 68 73 58 48 36 61 41 33 49
R04 | 2158 31 31 25 9 28 12 23 --- 9 | 62 61 51 46 42 47 37 --- 43
R05 | 1515 45 54 22 21 40 46 33 --- 14 | 65 73 59 47 43 57 41 --- 46
R06 | 1264 35 36 20 26 20 39 21 --- 12 | 29 31 45 65 46 34 54 --- 46
R07 | 746 34 32 22 12 27 18 29 84 10 | 74 72 58 53 48 61 36 68 51
R08 | 790 33 36 16 11 22 15 28 --- 9 | 68 71 46 51 36 55 32 --- 45
R09 | 3508 14 13 14 20 20 29 19 --- 9 | 25 25 22 33 40 28 36 --- 27
R10 | 1918 14 24 19 13 17 15 13 --- 6 | 57 63 45 60 44 55 54 --- 51
R11 | 1436 20 22 17 9 19 22 13 327 7 | 52 56 41 42 33 40 41 62 39
R13 | 740 21 26 15 14 20 12 11 --- 6 | 64 66 60 75 61 68 62 --- 65
R15 | 869 23 24 18 28 15 34 19 --- 11 | 66 67 59 75 59 66 62 --- 63
R16 | 768 24 23 26 24 21 38 27 --- 12 | 80 73 54 74 68 60 67 --- 62
R17 | 730 37 43 19 14 33 24 23 --- 10 | 64 68 46 53 33 59 43 --- 48
R18 | 703 31 33 18 10 20 15 17 --- 8 | 51 50 50 45 34 44 38 --- 42
R19 | 1004 46 45 39 17 31 25 28 --- 13 | 64 63 52 49 37 45 34 --- 44
R20 | 662 65 73 21 17 30 28 24 --- 13 | 81 84 47 54 39 42 32 --- 42
R21 | 527 31 38 15 10 35 14 19 83 9 | 59 62 48 47 34 40 40 28 42
R22 | 2254 28 32 14 10 20 27 18 --- 8 | 64 66 45 51 53 65 49 --- 51
R23 | 906 12 15 23 23 11 18 10 --- 8 | 32 31 31 47 34 41 38 --- 36
R24 | 1084 25 27 36 20 47 50 31 --- 15 | 43 43 64 52 41 51 34 --- 40
XR26 | ---- 23 96 --- --- --- --- 13 --- 17 | 28 82 --- --- --- --- 40 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1425 35 39 22 17 28 30 23 172 |T 58 62 48 51 42 51 41 45 44
WRMS | 1425 32 34 22 14 21 27 23 172 |NE 58 62 48 51 42 51 41 45 44
MEDI | 906 31 32 19 14 22 25 21 84 |MD 64 66 48 49 39 51 40 35 44
Table 3.1961.4 GPS week: 1961 Day: 4 MJD: 57975
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 | 507 80 68 13 16 28 46 40 --- 16 | 81 72 31 39 38 62 39 --- 37
R02 | 1174 45 51 29 11 35 17 24 86 11 | 57 61 40 31 27 29 23 67 28
R03 | 1492 38 40 23 15 42 21 17 143 11 | 61 62 45 34 29 47 36 39 36
R04 | 1837 29 30 15 12 24 35 17 --- 9 | 59 59 43 42 42 62 44 --- 44
R05 | 2104 54 49 21 15 30 49 28 --- 14 | 65 58 52 47 52 54 50 --- 48
R06 | 1720 33 38 23 32 16 23 10 --- 11 | 22 31 28 58 42 39 38 --- 36
R07 | 947 37 34 21 14 26 29 28 112 11 | 67 66 58 46 38 64 37 128 47
R08 | 1249 32 33 14 9 18 14 30 --- 8 | 64 65 45 44 39 48 30 --- 41
R09 | 4010 22 24 10 15 22 31 19 --- 8 | 26 28 28 32 35 35 33 --- 26
R10 | 1273 18 29 20 14 12 19 10 --- 7 | 52 65 36 54 45 45 50 --- 45
R11 | 1336 28 35 15 15 24 15 13 330 8 | 50 53 34 37 33 34 35 75 34
R13 | 821 16 13 18 17 21 20 12 --- 8 | 57 60 48 63 54 53 55 --- 54
R15 | 1219 37 32 14 29 25 38 25 --- 12 | 70 69 59 74 57 59 51 --- 59
R16 | 730 32 39 23 20 22 35 26 --- 11 | 69 70 45 61 51 47 54 --- 49
R17 | 689 34 33 12 14 34 12 21 --- 9 | 54 55 47 51 29 52 38 --- 44
R18 | 599 24 32 17 9 18 19 20 --- 7 | 37 42 31 35 29 43 34 --- 32
R19 | 1077 57 61 22 14 26 13 28 --- 11 | 64 69 47 41 40 44 31 --- 41
R20 | 635 54 43 29 11 30 34 22 --- 12 | 58 52 40 42 31 36 31 --- 35
R21 | 649 38 39 23 9 30 18 17 72 9 | 44 44 38 35 30 36 33 38 33
R22 |>>>>> 33 40 10 16 29 40 18 --- 10 | 50 55 41 37 38 59 41 --- 39
R23 | 1396 20 17 26 25 9 17 13 --- 9 | 35 39 31 52 46 39 42 --- 39
R24 | 1020 18 30 32 21 28 75 44 --- 17 | 33 44 45 51 41 47 30 --- 38
XR26 | ---- 16 41 --- --- --- --- 8 --- 11 | 16 50 --- --- --- --- 31 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS |41193 38 39 21 17 26 32 24 176 |T 51 55 41 45 39 47 38 69 39
WRMS |41193 39 39 21 14 21 31 24 176 |NE 51 55 41 45 39 47 38 69 39
MEDI | 1174 33 35 20 15 25 21 20 112 |MD 57 58 41 42 38 47 37 67 39
Table 3.1961.5 GPS week: 1961 Day: 5 MJD: 57976
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 771 73 79 21 17 28 41 39 15 | 71 75 32 28 39 56 26 30
R02 | 1732 46 47 26 9 29 18 27 11 | 57 59 40 33 24 36 23 32
R03 | 604 42 47 30 9 29 23 38 12 | 57 59 46 43 39 29 39 37
R04 | 823 26 25 18 8 32 16 17 8 | 50 46 36 36 23 36 37 33
R05 | 1735 39 38 27 18 30 49 31 14 | 58 69 56 60 72 48 51 54
R06 | 3142 17 22 14 20 15 24 22 8 | 23 24 22 34 31 24 26 23
R07 | 792 45 42 22 7 37 26 36 12 | 63 62 51 46 47 59 28 44
R08 | 833 33 27 15 13 23 29 24 9 | 60 57 49 41 34 63 34 43
R09 | 2388 13 16 15 20 18 16 20 8 | 22 23 26 32 32 38 25 26
R10 | 753 15 13 20 14 14 34 10 8 | 48 43 34 44 35 39 39 38
R11 | 1534 21 22 14 15 18 21 12 7 | 47 49 41 51 35 32 41 42
R13 | 1046 13 18 19 13 19 22 14 7 | 48 53 47 45 37 45 45 43
R15 | 833 46 50 24 10 34 22 29 11 | 93 93 91 95 98 91 92 90
R16 | 734 35 35 37 26 25 21 23 12 | 50 52 39 52 43 35 45 40
R17 | 557 33 32 14 9 29 15 24 8 | 41 37 35 39 31 31 33 34
R18 | 670 25 23 20 12 31 20 36 10 | 26 25 24 33 22 30 23 24
R19 | 1483 61 63 25 11 39 18 29 13 | 54 54 39 30 19 20 22 27
R20 | 701 22 45 36 17 25 57 22 14 | 28 36 37 32 29 47 24 24
R21 | 521 31 29 18 10 37 25 28 10 | 38 36 34 37 23 38 22 30
R22 | 563 30 26 15 11 42 22 30 10 | 39 37 35 36 37 39 42 34
R23 | 1074 15 16 13 21 18 25 12 8 | 28 32 31 41 28 31 27 31
R24 | 1019 24 27 62 28 24 76 30 20 | 51 56 42 62 52 41 33 44
XR26 | ---- 33 44 --- --- --- --- 21 26 | 14 69 --- --- --- --- 51 33
------+----------------------------------------------+------------------------------------------
RMS | 1279 35 37 25 16 28 32 27 |T 46 49 40 43 37 41 36 37
WRMS | 1279 33 34 25 14 25 30 25 |NE 46 49 40 43 37 41 36 37
MEDI | 823 31 29 20 13 28 22 24 |MD 48 52 37 39 34 38 33 34
Table 3.1961.6 GPS week: 1961 Day: 6 MJD: 57977
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 | 799 87 76 24 19 33 41 30 --- 15 | 94 87 45 36 44 65 37 --- 39
R02 | 1354 50 46 23 11 21 20 27 72 10 | 87 84 61 48 41 56 37 52 49
R03 | 681 43 44 20 6 25 25 30 85 10 | 83 87 61 55 50 66 53 82 56
R04 | 922 37 33 24 7 31 23 22 --- 9 | 71 70 59 54 54 49 44 --- 51
R05 | 2229 51 48 23 17 44 45 22 --- 13 | 74 84 64 64 69 66 55 --- 60
R06 | 2147 14 18 24 20 18 32 10 --- 9 | 41 48 37 58 46 35 44 --- 43
R07 | 864 49 52 17 7 31 25 31 200 10 | 90 97 66 59 49 77 40 154 59
R08 | 711 37 39 18 13 33 33 27 --- 10 | 84 87 59 60 44 79 45 --- 58
R09 | 2354 18 27 10 8 19 50 19 --- 9 | 33 35 31 30 33 35 40 --- 31
R10 | 1159 10 26 12 12 14 13 14 --- 5 | 61 70 47 64 50 60 57 --- 57
R11 | 1287 21 22 12 13 15 20 12 195 6 | 65 70 57 68 55 58 54 131 60
R13 | 1127 13 16 22 17 12 18 13 --- 7 | 84 87 63 84 72 87 76 --- 77
R15 | 1309 59 59 23 12 25 18 20 --- 10 | 114 115 85 93 85 93 91 --- 90
R16 | 1099 29 48 23 16 23 36 33 --- 11 | 83 89 58 79 60 72 73 --- 70
R17 | 572 35 36 12 6 20 17 23 --- 7 | 83 84 62 66 58 62 51 --- 62
R18 | 611 23 26 21 12 23 22 21 --- 8 | 56 57 46 52 43 59 45 --- 48
R19 | 703 62 66 24 18 37 26 28 --- 13 | 88 92 67 63 47 55 44 --- 58
R20 | 793 35 17 29 10 21 50 16 --- 11 | 74 80 41 47 35 58 38 --- 43
R21 | 675 37 36 18 12 23 16 30 92 9 | 69 68 52 51 38 53 42 49 48
R22 | 523 30 33 15 8 30 17 23 --- 8 | 72 72 56 52 43 63 52 --- 53
R23 | 824 9 14 15 12 19 20 14 --- 6 | 39 40 39 53 43 40 45 --- 43
R24 | 1002 43 42 33 15 39 70 21 --- 16 | 76 81 64 67 52 57 52 --- 57
XR26 | ---- 19 60 --- --- --- --- 11 --- 14 | 30 74 --- --- --- --- 43 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1198 41 41 21 13 27 32 23 141 |T 71 76 55 59 50 61 50 93 54
WRMS | 1198 38 40 21 12 25 28 23 141 |NE 71 76 55 59 50 61 50 93 54
MEDI | 864 35 36 21 12 23 23 22 92 |MD 74 81 58 58 47 59 45 82 56
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