[IGSREPORT-27667] Wk 2135 IGLOS Final Orbits
acc
acc at igs.org
Sun Dec 27 05:47:34 UTC 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2135 (Dec 06, 2020 - Dec 12, 2020)
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 2.2135.
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:
igl2135[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2135 in the SP3 format.
igl21357.sum Combination Report for GPS Week 2135.
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 | -0.3 ns
1 | -0.5 ns
2 | 0.2 ns
3 | -0.2 ns
4 | 0.8 ns
5 | 0.4 ns
6 | 1.7 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 1.2135, 1a.2135).
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 2.2135.0-6)
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 3.2135.0-6).
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 2135 summary. (Dec 06, 2020 - Dec 12, 2020)
Table 1.2135.a GPS week : 2135 MJD: 59189.0-59195.0
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 1 -4 -16 12 .06 24 19 | 15995 -1313 2981 7791
| 1 0 1 14 21 15 .03 | 2262 1391
emx n/a| 0 0 -3 -24 23 -43 .12 41 39 | -2007 -591 3044 8029
| 1 1 1 30 21 14 .03 | 8012 978
esx n/a| 0 0 2 11 -22 -54 .11 36 25 | 9682 -991 3045 10295
| 1 1 2 10 13 27 .03 | 9686 2597
gfz n/a| 0 0 0 -10 0 -56 .13 27 15 | 0 -306 3071 7565
| 1 1 1 18 19 30 .03 | 0 1509
grg n/a| 0 0 -2 15 0 0 -.42 31 24 | 432 -465 3050 7268
| 1 1 2 15 11 20 .05 | 286 1753
iac n/a| 3 0 2 15 14 133 .04 29 24 | 1959 -115 3023 8154
| 2 3 2 21 40 68 .06 | 875 815
mcc n/a| 0 -4 -4 65 32 435 -.88 176 176 | --- --- --- ---
| 4 6 11 65 166 667 .50 | --- ---
Table 1.2135.b GPS week : 2135 MJD: 59189.0-59195.0
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 15 15 17 15 17 14 |
R02 | 8 10 8 8 6 6 8 |
R03 | 6 5 8 8 8 8 8 |
R04 | 9 7 9 10 7 8 12 |
R05 | 9 9 10 9 9 7 9 |
R07 | 8 8 7 6 7 7 7 |
R08 | 8 7 8 8 7 8 10 |
R09 | 8 7 6 7 9 8 10 |
R11 | 9 13 11 10 9 13 21 |
R12 | 7 7 8 7 8 10 10 |
R13 | 16 14 15 17 23 17 22 |
R14 | 6 8 10 8 7 7 9 |
R15 | 7 8 10 9 8 8 11 |
R16 | 11 11 10 11 12 12 15 |
R17 | 9 10 11 9 9 11 13 |
R18 | 9 8 7 7 7 6 9 |
R19 | 31 29 33 37 28 31 44 |
R20 | 24 24 25 29 30 29 27 |
R21 | 11 11 10 8 8 12 12 |
R22 | 16 12 16 14 15 23 30 |
R24 | 10 10 8 10 8 10 11 |
Table 1.2135.c GPS week : 2135 MJD: 59189.0-59195.0
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 2135 0 | -13 -94 27 643 1124 -5034 84.4 1475 1475 | -288 0
brd 2135 1 | -54 57 198 198 744 -2679 82.7 1587 1587 | -529 0
brd 2135 2 | 87 12 148 2041 2307 -1407 84.1 1742 1742 | 219 0
brd 2135 3 | 61 1 117 -891 904 -863 82.9 1529 1529 | -231 0
brd 2135 4 | -55 56 156 898 -767 -2147 83.2 1696 1696 | 826 0
brd 2135 5 | 38 8 26 318 -319 -846 82.2 1825 1825 | 369 0
brd 2135 6 | -9 15 34 -61 -221 -2798 79.8 1768 1768 | 1665 0
-------------+------------------------------------------------------------+----------------
brd 2135 mean| 7 8 101 449 538 -2253 82.8 1660 1660 | 290 0
brd 2135 sdev| 56 50 71 904 1054 1463 1.5 131 131 | 759 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 2.2135.0 GPS week: 2135 Day: 0 MJD: 59189
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 1 -40 -10 .10 27 21 | 19443 -2791 2637 7455
emx n/a| 0 0 -4 -57 9 -46 .11 37 37 | -15097 -1698 2663 7760
esx n/a| 0 0 3 10 -37 -58 .12 31 26 | 16732 -2601 2651 9932
gfz n/a| 1 0 -1 27 37 -81 .11 27 15 | 0 -1445 2659 7176
grg n/a| 1 2 1 0 -9 21 -.40 26 21 | 696 -2200 2678 6780
iac n/a| 0 -5 1 -16 26 189 .03 30 26 | 1783 -753 2631 7832
mcc n/a| -3 -1 3 144 144 642 -.58 188 188 | --- --- --- ---
Table 2.2135.1 GPS week: 2135 Day: 1 MJD: 59190
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 20 6 3 .08 26 21 | 16874 -1257 2754 6935
emx n/a| -2 1 -6 -63 51 -38 .10 36 36 | 3828 -730 2756 7202
esx n/a| 0 1 3 -5 -33 -80 .12 33 26 | 15122 -3398 2775 9976
gfz n/a| 0 0 1 -16 -8 -67 .15 24 13 | 0 -1645 2801 6510
grg n/a| -2 0 -3 13 22 8 -.40 24 18 | 163 -1425 2780 6432
iac n/a| 4 0 3 44 0 194 .09 28 23 | 1451 -534 2758 7295
mcc n/a| -4 -3 11 101 268 853 -.32 164 164 | --- --- --- ---
Table 2.2135.2 GPS week: 2135 Day: 2 MJD: 59191
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 0 -21 2 36 .03 18 15 | 17164 -1326 2976 8046
emx n/a| 0 0 -4 -2 39 -33 .12 43 35 | -8407 -285 2989 8106
esx n/a| 1 0 3 19 -14 -59 .13 40 26 | 19285 -1039 2988 10228
gfz n/a| 1 0 2 -17 -6 -44 .15 27 17 | 0 -1122 3007 7671
grg n/a| 0 4 -3 2 7 9 -.39 32 26 | 507 -685 2989 7396
iac n/a| 1 -2 3 -9 -50 71 -.04 29 24 | 2101 -447 2976 8246
mcc n/a| -6 -6 -16 12 31 1182 -1.83 198 198 | --- --- --- ---
Table 2.2135.3 GPS week: 2135 Day: 3 MJD: 59192
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 0 -2 -4 15 .02 24 20 | 14989 -2908 3167 8079
emx n/a| 0 0 -3 -48 26 -66 .18 46 37 | -3246 -1887 3183 8037
esx n/a| 0 -2 1 7 -17 -85 .12 41 24 | 6655 -3988 3175 10512
gfz n/a| 0 0 0 -10 -23 -67 .12 28 17 | 0 -1354 3237 7528
grg n/a| 0 -1 -3 0 -6 -26 -.38 31 23 | 922 -2443 3154 7371
iac n/a| 1 0 5 28 51 176 .08 26 23 | 324 763 3173 8236
mcc n/a| 0 0 -9 -11 -10 879 -.84 135 135 | --- --- --- ---
Table 2.2135.4 GPS week: 2135 Day: 4 MJD: 59193
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 2 -7 -41 20 .07 23 17 | 13258 628 3226 7958
emx n/a| 0 2 -3 -8 -10 -60 .07 46 46 | 8050 73 3265 8045
esx n/a| -1 -1 -2 26 -35 -48 .12 42 25 | 16201 509 3264 10480
gfz n/a| 0 -1 0 -11 8 -92 .16 27 14 | 0 868 3262 7635
grg n/a| -1 1 2 24 0 -25 -.47 27 21 | 291 849 3276 7200
iac n/a| 4 0 1 18 61 170 -.01 25 20 | 2546 221 3217 8232
mcc n/a| 0 3 2 151 127 357 -.53 133 133 | --- --- --- ---
Table 2.2135.5 GPS week: 2135 Day: 5 MJD: 59194
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 1 -15 -23 7 .08 25 22 | 14242 -225 3128 8275
emx n/a| 0 -1 -3 -1 7 -29 .13 43 43 | -3090 -531 3167 8553
esx n/a| 0 -2 0 17 -10 -41 .10 37 25 | -599 146 3178 10736
gfz n/a| -1 -1 2 -16 1 -31 .09 26 11 | 0 177 3214 8061
grg n/a| -2 0 -4 40 -6 -12 -.52 36 29 | 237 224 3174 7648
iac n/a| 5 0 6 11 33 121 .01 28 25 | 2824 -1124 3138 8585
mcc n/a| 2 -6 -5 29 -105 -131 -1.11 180 180 | --- --- --- ---
Table 2.2135.6 GPS week: 2135 Day: 6 MJD: 59195
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]
--------+----------------------------------------------------+------------------------------
emx n/a| 2 0 0 9 37 -30 .14 40 40 | 3910 920 3286 8503
esx n/a| -2 0 5 3 -5 -4 .04 28 24 | -5618 3431 3287 10204
gfz n/a| -1 -1 -1 -31 -7 -6 .09 33 14 | 0 2379 3317 8379
grg n/a| -1 -1 -3 23 -6 21 -.37 41 33 | 213 2425 3303 8055
iac n/a| 3 6 -1 28 -20 14 .13 34 30 | 2685 1065 3269 8658
mcc n/a| 8 -18 -20 35 -229 -737 -.93 238 238 | --- --- --- ---
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 3.2135.0 GPS week: 2135 Day: 0 MJD: 59189
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 604 53 25 44 22 27 22 --- 15 | 77 73 51 62 47 58 --- 59
R02 | 576 10 13 15 11 25 24 179 7 | 38 51 48 48 41 54 138 46
R03 | 2602 9 9 8 11 12 27 93 6 | 53 59 56 56 62 72 95 59
XR04 | 1725 16 25 20 --- 10 18 --- 9 | 60 71 50 --- 58 57 --- 59
R05 | 734 19 24 11 14 17 30 --- 8 | 46 51 47 45 43 42 --- 44
R07 | 1526 21 15 12 9 19 28 313 8 | 56 65 59 56 60 57 87 60
R08 | 920 14 13 23 13 12 25 --- 7 | 53 61 74 65 62 70 --- 64
R09E | 3079 15 16 9 17 17 29 --- 8 | 30 37 45 48 36 60 --- 41
XR11E | 6652 14 --- --- 11 --- 9 --- 8 | 41 --- --- 50 --- 51 --- 47
R12E | 894 12 24 10 16 11 21 --- 7 | 67 76 82 87 79 79 --- 80
R13E | 2194 30 37 28 55 26 29 --- 16 | 67 125 126 141 129 132 --- 126
R14E | 1038 10 17 11 10 13 17 --- 5 | 43 56 65 64 55 64 --- 59
R15E | 1367 15 23 12 13 13 22 --- 7 | 77 103 103 104 100 105 --- 102
R16E | 861 11 34 14 24 21 42 --- 11 | 31 31 38 47 35 45 --- 34
R17 | 587 16 26 22 16 12 20 --- 8 | 62 57 57 75 68 85 --- 69
R18 | 1909 9 28 12 14 16 38 --- 9 | 54 47 65 54 51 85 --- 58
R19 | 1965 56 109 71 69 59 48 --- 31 | 107 61 39 136 90 103 --- 87
R20 | 959 55 67 78 26 30 43 --- 23 | 97 50 45 104 95 116 --- 84
R21 | 1022 21 24 34 26 18 18 54 11 | 62 52 55 81 73 74 78 68
R22 | 1076 22 23 21 36 56 37 --- 16 | 51 49 57 61 61 89 --- 59
R24 | 627 25 31 26 10 14 19 --- 9 | 71 68 71 76 69 82 --- 74
------+----------------------------------------------+------------------------------------------
RMS | 1475 27 37 31 27 26 30 188 |T 59 62 61 73 65 75 99 65
WRMS | 1475 21 37 26 15 21 26 188 |NE 63 58 55 70 62 74 99 63
MEDI | 1038 16 24 15 14 17 25 93 |MD 56 57 56 62 61 72 87 59
Table 3.2135.1 GPS week: 2135 Day: 1 MJD: 59190
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 732 51 31 44 18 29 18 --- 15 | 55 59 39 49 35 35 --- 43
R02 | 1013 17 16 22 11 24 34 114 9 | 28 41 42 40 39 56 66 39
R03 | 1829 10 14 12 9 8 17 160 5 | 36 44 42 42 44 49 85 42
XR04 | 2339 7 13 15 --- 19 13 --- 7 | 42 55 51 --- 46 47 --- 48
R05 | 787 24 25 24 21 11 19 --- 9 | 37 39 44 41 38 37 --- 36
R07 | 648 13 14 22 16 9 30 255 8 | 36 43 54 38 45 37 57 41
R08 | 1156 12 14 21 15 17 14 --- 7 | 35 43 55 49 34 45 --- 43
R09E | 4619 17 17 13 10 12 21 --- 6 | 25 25 30 31 24 33 --- 25
XR11E | 8455 16 --- --- 18 --- 20 --- 13 | 23 --- --- 37 --- 37 --- 30
R12E | 1533 14 24 11 13 13 15 --- 6 | 59 67 72 72 63 67 --- 68
R13E | 1283 34 39 29 36 25 24 --- 14 | 75 128 132 136 128 127 --- 127
R14E | 882 16 26 20 15 15 14 --- 8 | 46 60 62 63 52 65 --- 58
R15E | 1446 15 25 17 16 12 15 --- 7 | 68 88 97 89 90 95 --- 90
R16E | 1685 10 24 18 28 34 25 --- 11 | 28 33 39 52 26 36 --- 31
R17 | 620 12 33 27 17 16 19 --- 9 | 36 40 35 47 48 44 --- 43
R18 | 1320 11 23 17 11 19 22 --- 7 | 44 39 46 43 40 43 --- 41
R19 | 1693 50 97 78 70 52 34 --- 29 | 63 63 66 95 38 59 --- 59
R20 | 759 49 61 70 25 37 75 --- 23 | 44 33 26 32 43 76 --- 30
R21 | 1039 16 29 38 10 17 26 59 10 | 38 38 37 45 46 58 46 44
R22 | 1559 19 35 15 27 30 33 --- 12 | 39 38 32 41 43 45 --- 37
R24 | 659 31 23 20 16 25 11 --- 10 | 40 47 52 47 41 52 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 1587 26 36 33 24 24 28 163 |T 42 51 52 54 48 54 63 48
WRMS | 1587 21 36 26 13 18 23 163 |NE 40 44 44 46 41 48 63 42
MEDI | 1283 16 24 20 16 17 20 114 |MD 39 43 44 45 43 47 57 43
Table 3.2135.2 GPS week: 2135 Day: 2 MJD: 59191
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 799 39 38 42 24 39 14 --- 15 | 75 78 39 52 36 54 --- 58
R02 | 849 7 15 15 12 21 27 206 7 | 33 41 35 36 25 50 170 36
R03 | 1279 11 17 20 10 18 28 243 8 | 39 48 33 36 30 46 153 37
XR04 | 1622 10 22 25 --- 20 14 --- 8 | 41 53 33 --- 36 43 --- 41
R05 | 1504 16 23 26 28 15 18 --- 9 | 41 50 35 33 45 45 --- 37
R07 | 927 13 12 19 18 13 21 217 7 | 48 51 46 60 59 45 46 52
R08 | 958 10 9 26 15 27 21 --- 8 | 47 48 56 54 58 40 --- 48
R09E | 5371 11 15 12 14 15 18 --- 6 | 29 35 34 35 30 32 --- 30
XR11E | 7866 13 --- --- 17 --- 14 --- 10 | 35 --- --- 45 --- 42 --- 39
R12E | 1811 8 28 20 15 17 17 --- 7 | 43 39 41 54 40 50 --- 44
R13E | 1913 22 47 33 41 30 27 --- 14 | 69 89 91 99 103 90 --- 91
R14E | 757 15 26 29 24 9 23 --- 9 | 35 33 53 46 32 41 --- 37
R15E | 995 11 39 17 24 26 19 --- 10 | 36 45 41 52 53 53 --- 45
R16E | 1263 8 21 22 28 35 16 --- 10 | 33 30 47 47 37 31 --- 30
R17 | 510 10 41 33 16 23 27 --- 10 | 45 35 36 58 52 65 --- 50
R18 | 492 8 22 13 11 19 17 --- 6 | 42 30 46 45 40 54 --- 43
R19 | 733 37 115 104 69 87 33 --- 32 | 79 41 49 112 80 76 --- 73
R20 | 654 29 85 93 27 34 68 --- 25 | 79 51 49 79 80 118 --- 74
R21 | 1159 11 33 35 15 19 28 90 10 | 51 44 36 48 61 72 69 52
R22 | 2844 16 41 30 33 51 49 --- 16 | 42 44 46 62 43 55 --- 43
R24 | 862 16 34 15 14 15 15 --- 8 | 48 48 50 52 51 64 --- 54
------+----------------------------------------------+------------------------------------------
RMS | 1741 18 43 40 27 32 29 198 |T 47 46 44 55 49 55 109 48
WRMS | 1741 15 35 26 17 26 24 198 |NE 50 47 42 55 49 59 109 49
MEDI | 995 11 26 25 17 20 21 206 |MD 42 44 41 52 43 50 69 44
Table 3.2135.3 GPS week: 2135 Day: 3 MJD: 59192
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 505 44 41 39 40 40 20 --- 17 | 67 78 45 46 35 65 --- 55
R02 | 1099 14 14 19 13 21 21 118 7 | 32 37 44 37 20 24 145 30
R03 | 700 8 17 13 20 8 31 168 8 | 42 54 48 62 50 48 118 49
XR04 | 643 17 23 23 --- 17 18 --- 9 | 43 47 30 --- 34 41 --- 39
R05 | 1272 19 33 16 18 19 13 --- 8 | 36 48 33 31 23 27 --- 30
R07 | 838 11 10 11 23 9 14 151 6 | 43 57 50 49 58 58 92 53
R08 | 1004 16 12 15 8 14 30 --- 8 | 44 48 51 47 58 42 --- 47
R09E | 4815 16 11 13 13 18 18 --- 7 | 23 26 29 32 19 29 --- 23
XR11E | 7065 15 --- --- 14 --- 11 --- 10 | 26 --- --- 36 --- 36 --- 30
R12E | 1807 10 29 14 16 6 17 --- 7 | 43 30 32 46 35 47 --- 38
R13E | 1287 26 55 42 55 18 25 --- 17 | 94 150 159 158 145 144 --- 148
R14E | 1515 13 27 19 12 13 19 --- 7 | 36 38 46 46 33 47 --- 39
R15E | 566 14 35 14 17 17 23 --- 9 | 38 33 39 47 41 44 --- 38
R16E | 841 20 28 28 33 24 14 --- 11 | 20 26 43 59 29 30 --- 28
R17 | 726 14 37 25 12 16 13 --- 8 | 49 38 40 56 57 59 --- 52
R18 | 587 12 22 15 11 17 20 --- 7 | 48 52 56 48 45 55 --- 50
R19 | 903 52 126 109 53 86 69 --- 36 | 67 60 64 102 83 121 --- 76
R20 | 832 40 97 111 53 49 29 --- 29 | 86 70 45 131 122 100 --- 93
R21 | 1059 20 24 20 14 15 17 89 8 | 48 40 48 55 44 43 46 48
R22 | 1892 24 33 21 27 47 33 --- 14 | 38 30 46 39 37 49 --- 37
R24 | 771 19 34 23 23 24 17 --- 10 | 48 38 42 69 44 60 --- 52
------+----------------------------------------------+------------------------------------------
RMS | 1528 24 46 41 28 31 26 135 |T 46 50 49 59 50 55 100 50
WRMS | 1528 20 37 24 17 23 23 135 |NE 49 49 45 59 50 56 100 50
MEDI | 903 16 28 19 17 17 19 118 |MD 43 40 45 47 41 47 92 47
Table 3.2135.4 GPS week: 2135 Day: 4 MJD: 59193
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1361 40 40 43 29 28 13 --- 14 | 46 63 24 42 28 41 --- 42
R02 | 1263 10 7 19 8 12 20 70 6 | 33 39 57 43 43 37 67 42
R03 | 602 13 15 18 17 18 17 107 7 | 35 47 65 63 40 51 71 51
XR04 | 978 13 15 24 --- 7 13 --- 7 | 46 51 49 --- 48 48 --- 50
R05 | 626 20 24 27 17 12 14 --- 8 | 28 40 33 30 27 30 --- 28
R07 | 1060 6 11 18 12 27 12 213 7 | 36 48 52 49 58 57 61 51
R08 | 1003 11 17 21 11 14 23 --- 7 | 33 40 59 43 45 45 --- 44
R09E | 5477 18 21 11 17 31 18 --- 9 | 23 29 29 37 32 29 --- 26
XR11E | 6796 14 --- --- 10 --- 11 --- 8 | 31 --- --- 40 --- 35 --- 34
R12E | 1097 13 28 16 11 15 19 --- 7 | 50 37 45 45 41 47 --- 43
R13E | 2322 37 64 64 75 32 29 --- 23 | 107 120 90 131 122 98 --- 105
R14E | 1290 14 22 16 14 12 14 --- 6 | 36 34 44 48 37 43 --- 40
R15E | 650 12 27 19 16 14 20 --- 8 | 52 45 48 56 44 55 --- 48
R16E | 1212 19 32 22 29 19 35 --- 12 | 22 27 31 37 28 43 --- 24
R17 | 1567 8 35 25 23 14 17 --- 9 | 39 33 43 69 50 61 --- 54
R18 | 767 7 15 26 13 18 16 --- 7 | 25 31 49 27 45 34 --- 33
R19 | 747 41 116 80 34 50 53 --- 27 | 53 43 45 76 63 83 --- 59
R20 | 925 39 111 120 37 50 49 --- 30 | 59 46 45 100 98 110 --- 79
R21 | 588 16 27 24 14 15 13 95 8 | 34 39 45 55 44 44 32 47
R22 | 677 25 29 28 31 50 30 --- 15 | 31 40 61 50 52 62 --- 45
R24 | 1707 22 38 14 9 12 8 --- 8 | 47 47 48 49 51 58 --- 52
------+----------------------------------------------+------------------------------------------
RMS | 1696 23 46 42 27 27 25 133 |T 41 44 48 54 49 52 57 47
WRMS | 1696 17 46 25 14 21 20 133 |NE 38 43 48 53 49 54 57 48
MEDI | 1060 14 27 22 16 15 17 95 |MD 36 40 45 48 44 47 61 45
Table 3.2135.5 GPS week: 2135 Day: 5 MJD: 59194
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2023 52 23 53 26 41 12 --- 17 | 76 45 43 45 26 34 --- 36
R02 | 1006 12 10 20 10 19 12 148 6 | 42 40 54 48 33 39 78 41
R03 | 913 11 12 10 11 19 29 86 7 | 51 34 37 34 31 46 58 36
XR04 | 612 11 11 19 --- 17 17 --- 7 | 58 45 44 --- 50 61 --- 51
R05 | 499 7 16 17 17 12 18 --- 6 | 44 36 45 38 43 41 --- 38
R07 | 678 14 20 11 9 26 13 295 7 | 50 54 52 53 54 53 68 50
R08 | 933 16 14 17 14 22 20 --- 7 | 47 41 48 45 38 46 --- 40
R09E | 5337 13 19 12 12 16 30 --- 8 | 22 24 29 33 28 40 --- 26
XR11E | 6361 15 --- --- 14 --- 25 --- 13 | 35 --- --- 35 --- 45 --- 33
R12E | 1422 14 26 13 14 26 31 --- 9 | 72 57 60 61 63 50 --- 58
R13E | 2329 43 45 38 41 34 27 --- 17 | 125 149 152 149 153 133 --- 144
R14E | 988 12 21 10 15 12 15 --- 6 | 57 59 58 65 56 55 --- 57
R15E | 1005 10 27 14 24 12 17 --- 8 | 86 75 82 77 77 79 --- 77
R16E | 1699 15 36 22 19 18 41 --- 11 | 33 20 40 38 29 42 --- 27
R17 | 2201 8 34 31 11 16 38 --- 11 | 62 36 40 47 39 69 --- 46
R18 | 1326 8 23 14 10 15 14 --- 6 | 46 31 34 40 27 35 --- 33
R19 | 1784 35 123 73 51 100 21 --- 31 | 93 33 32 67 77 46 --- 49
R20 | 768 45 91 102 33 51 52 --- 28 | 102 40 41 74 79 85 --- 61
R21 | 872 9 36 39 21 24 20 113 11 | 62 33 33 63 57 58 46 47
R22 | 695 46 33 28 64 69 49 --- 22 | 39 41 55 59 59 74 --- 46
R24 | 1830 22 24 10 16 23 27 --- 9 | 68 45 47 51 47 43 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 1825 25 43 37 26 36 28 180 |T 60 46 51 56 53 55 62 49
WRMS | 1825 22 43 25 11 29 25 180 |NE 60 39 43 51 47 52 62 44
MEDI | 1006 14 23 17 15 19 21 113 |MD 57 40 44 48 47 46 58 46
Table 3.2135.6 GPS week: 2135 Day: 6 MJD: 59195
Weighted Average Orbit Dynamics (7 days)
PRN | brd emx esx gfz grg iac mcc IGL | emx esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1869 31 37 13 20 27 --- 13 | 66 52 62 56 63 --- 57
R02 | 672 15 12 13 17 19 249 7 | 42 48 47 35 45 139 42
R03 | 671 12 11 8 14 27 108 7 | 53 56 56 49 71 60 56
XR04 | 718 16 17 --- 14 31 --- 11 | 55 41 --- 47 64 --- 50
R05 | 666 15 15 11 21 28 --- 9 | 45 43 56 36 69 --- 48
R07 | 817 15 15 8 13 17 366 7 | 67 66 72 69 76 111 69
R08 | 1219 22 15 15 19 24 --- 9 | 52 63 68 56 71 --- 61
R09E | 3912 17 8 14 19 38 --- 10 | 24 29 33 24 47 --- 29
XR11E | 4485 --- --- 18 --- 24 --- 21 | --- --- 37 --- 46 --- 36
R12E | 2574 28 12 21 20 22 --- 10 | 86 84 94 86 85 --- 86
R13E | 1335 46 35 55 43 36 --- 22 | 128 133 146 130 134 --- 132
R14E | 964 19 13 14 22 17 --- 8 | 79 88 86 76 82 --- 82
R15E | 1741 27 11 22 19 29 --- 11 | 115 120 128 118 119 --- 120
R16E | 1794 37 19 37 26 28 --- 15 | 27 49 71 41 44 --- 44
R17 | 2164 22 24 23 17 40 --- 13 | 53 54 81 66 87 --- 68
R18 | 1758 23 9 6 17 27 --- 8 | 40 54 46 42 62 --- 48
R19 | 2801 119 73 97 99 35 --- 44 | 49 44 147 119 106 --- 82
R20 | 1155 53 57 49 72 22 --- 26 | 41 45 107 117 106 --- 78
R21 | 892 30 18 17 24 28 139 11 | 47 50 67 73 72 75 61
R22 | 1075 49 19 37 95 86 --- 30 | 42 66 69 61 116 --- 66
R24 | 1596 26 17 18 20 31 --- 11 | 60 68 84 69 86 --- 73
------+-----------------------------------------+-------------------------------------
RMS | 1767 40 28 33 41 34 238 |T 58 62 77 68 78 96 66
WRMS | 1767 40 24 14 33 30 238 |NE 50 53 74 63 78 96 61
MEDI | 1335 23 15 17 20 28 139 |MD 52 54 69 61 72 75 61
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