[IGSREPORT-27871] Wk 2151 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 16 06:48:21 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2151 (Mar 28, 2021 - Apr 03, 2021)
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 2.2151.
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:
igl2151[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2151 in the SP3 format.
igl21517.sum Combination Report for GPS Week 2151.
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 | 1.4 ns
1 | -1.7 ns
2 | -0.4 ns
3 | 0.8 ns
4 | -1.9 ns
5 | 0.3 ns
6 | -1.5 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 1.2151, 1a.2151).
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 2.2151.0-6)
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 3.2151.0-6).
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 2151 summary. (Mar 28, 2021 - Apr 03, 2021)
Table 1.2151.a GPS week : 2151 MJD: 59301.0-59307.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 7 4 1 16 -.50 26 20 | 11822 -614 3353 7851
| 1 1 2 15 22 35 .03 | 2017 2761
emx n/a| 0 0 -4 -14 -1 -75 .10 31 27 | 956 7 3375 8424
| 1 1 2 16 36 27 .03 | 3349 1813
esx n/a| 0 0 -2 4 -13 -40 .11 31 23 | 4125 -562 3352 7265
| 1 1 1 10 29 28 .02 | 6831 2856
gfz n/a| 0 0 6 -4 -9 -73 .09 30 17 | 0 -896 3377 7607
| 1 1 3 28 18 16 .03 | 0 2609
grg n/a| 3 -1 -5 13 14 43 .50 31 23 | 6 -1074 3385 7514
| 0 1 5 16 20 20 .05 | 239 2705
iac n/a| -3 -1 -3 -15 -3 121 -.11 31 27 | 1664 -520 3351 8333
| 2 2 5 29 52 70 .06 | 2139 1804
mcc n/a| -2 0 -10 64 -83 102 -.42 119 119 | --- --- --- ---
| 5 5 11 52 70 430 .11 | --- ---
Table 1.2151.b GPS week : 2151 MJD: 59301.0-59307.0
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 | 17 16 16 17 17 18 18 |
R02 | 7 6 8 9 7 7 8 |
R03 | 10 11 9 9 9 8 9 |
R04 | 11 13 13 11 11 12 8 |
R05 | 10 10 8 11 8 21 11 |
R07 | 10 8 11 8 9 8 10 |
R08 | 9 8 8 7 9 9 8 |
R09 | 11 11 13 14 10 13 14 |
R11 | 15 12 8 9 11 9 14 |
R12 | 10 11 9 9 9 8 10 |
R13 | 17 18 14 16 15 21 23 |
R14 | 8 8 6 9 8 7 8 |
R15 | 10 8 7 9 9 10 9 |
R16 | 15 17 15 12 14 13 12 |
R17 | 10 9 9 9 9 9 9 |
R18 | 9 9 7 8 13 10 6 |
R19 | 17 17 20 20 18 22 24 |
R20 | 26 31 24 22 25 28 22 |
R21 | 10 10 10 8 10 8 10 |
R22 | 20 22 22 22 28 27 24 |
R24 | 10 11 9 9 11 9 8 |
Table 1.2151.c GPS week : 2151 MJD: 59301.0-59307.0
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 2151 0 | 21 -79 110 2903 559 -1006 84.3 1423 1423 | 1382 0
brd 2151 1 | 26 -96 142 1635 -981 7004 84.6 1521 1521 | -1694 0
brd 2151 2 | 14 86 188 684 -194 7460 82.4 1702 1702 | -362 0
brd 2151 3 | -43 -57 178 622 64 8275 83.0 1557 1557 | 834 0
brd 2151 4 | 39 -55 122 1351 312 9000 82.7 1443 1443 | -1886 0
brd 2151 5 | -20 80 307 -506 900 6095 81.4 1618 1618 | 324 0
brd 2151 6 | 36 27 283 570 1647 4140 82.4 1930 1930 | -1481 0
-------------+------------------------------------------------------------+----------------
brd 2151 mean| 10 -13 190 1037 329 5852 83.0 1599 1599 | -411 0
brd 2151 sdev| 31 76 77 1067 834 3408 1.1 174 174 | 1308 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 2.2151.0 GPS week: 2151 Day: 0 MJD: 59301
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 4 10 3 -37 -38 -.54 27 20 | 14027 2607 3165 8457
emx n/a| 0 3 -5 -32 21 -35 .08 30 27 | 4611 2349 3210 9023
esx n/a| 0 3 -4 0 29 -10 .13 31 24 | 7374 1946 3127 8394
gfz n/a| -2 0 10 21 -28 -56 .09 30 18 | 0 2226 3167 8125
grg n/a| 3 -3 -14 -3 11 50 .53 29 22 | -94 2661 3230 8103
iac n/a| -1 -1 5 -16 14 64 -.23 31 31 | 3644 -331 3162 8891
mcc n/a| 5 0 4 44 -81 141 -.55 117 117 | --- --- --- ---
Table 2.2151.1 GPS week: 2151 Day: 1 MJD: 59302
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 10 0 26 -1 -.49 28 24 | 13721 -3668 3233 7115
emx n/a| -1 0 -7 13 46 -111 .10 31 26 | 2746 -1992 3283 7775
esx n/a| 0 0 0 17 -3 -66 .09 30 22 | 13710 -3466 3216 9432
gfz n/a| 2 -1 6 20 2 -88 .09 33 19 | 0 -3654 3265 6887
grg n/a| 2 -1 -10 0 -19 80 .47 34 24 | 258 -4144 3276 6969
iac n/a| 0 0 -3 -79 -73 181 -.11 30 30 | 1022 -2159 3223 7602
mcc n/a| 3 -1 -20 136 -108 484 -.27 133 133 | --- --- --- ---
Table 2.2151.2 GPS week: 2151 Day: 2 MJD: 59303
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 6 -2 12 6 -.49 26 18 | 10807 -410 3438 7682
emx n/a| -1 0 -5 -29 39 -84 .11 30 27 | 3610 -548 3457 8329
esx n/a| 0 0 -1 -6 -23 0 .10 27 18 | 10381 -275 3438 7287
gfz n/a| -1 0 5 22 -4 -50 .06 27 17 | 0 -473 3507 7223
grg n/a| 2 -3 -4 9 13 26 .50 30 17 | 323 -1419 3454 7642
iac n/a| -6 3 -3 3 -59 86 -.05 32 27 | -169 2572 3458 8269
mcc n/a| -5 0 -18 70 -55 558 -.34 154 154 | --- --- --- ---
Table 2.2151.3 GPS week: 2151 Day: 3 MJD: 59304
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 6 36 -6 52 -.51 26 20 | 13503 1864 3358 9198
emx n/a| -1 1 -5 -21 -20 -82 .16 28 25 | 1615 1290 3403 9766
esx n/a| -3 1 -2 6 -19 -62 .11 29 20 | -6464 2331 3342 6502
gfz n/a| 0 3 7 -27 18 -73 .08 30 17 | 0 1549 3363 9015
grg n/a| 3 -2 0 0 10 46 .53 30 19 | -144 1427 3403 9168
iac n/a| -3 -5 -7 -16 -8 173 -.10 30 28 | 5507 -2429 3355 9772
mcc n/a| -9 12 -18 37 10 397 -.35 112 112 | --- --- --- ---
Table 2.2151.4 GPS week: 2151 Day: 4 MJD: 59305
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 5 7 13 70 -.45 23 17 | 11962 -4175 3499 7016
emx n/a| 0 1 -6 -21 -23 -87 .12 28 25 | 1475 -2401 3480 7490
esx n/a| 0 0 -3 20 8 -58 .14 31 25 | 1290 -3915 3541 6340
gfz n/a| 0 0 11 -12 -2 -90 .08 26 18 | 0 -4364 3523 6809
grg n/a| 2 -2 0 16 15 30 .39 28 22 | 157 -4289 3504 6308
iac n/a| -1 -2 -11 0 -14 84 -.09 30 26 | -208 -1655 3492 7394
mcc n/a| 2 -1 -15 -16 -114 64 -.45 98 98 | --- --- --- ---
Table 2.2151.5 GPS week: 2151 Day: 5 MJD: 59306
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 2 8 2 17 7 -.53 27 22 | 9528 1602 3737 7403
emx n/a| 0 0 -1 -10 -44 -87 .07 32 29 | -3627 1569 3704 7915
esx n/a| 3 -1 -2 0 -64 -63 .12 36 26 | 232 2403 3791 7168
gfz n/a| 0 1 4 -51 -23 -91 .14 37 14 | 0 845 3764 7306
grg n/a| 4 0 -9 40 51 45 .52 37 25 | -134 491 3715 6825
iac n/a| -5 -2 0 0 43 222 -.06 29 24 | 1375 996 3741 7885
mcc n/a| -6 -4 -8 57 -206 -583 -.54 103 103 | --- --- --- ---
Table 2.2151.6 GPS week: 2151 Day: 6 MJD: 59307
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 4 -15 -14 19 -.51 28 20 | 9211 -2121 3044 8088
emx n/a| -1 0 -2 0 -26 -39 .09 37 33 | -3735 -215 3093 8676
esx n/a| -1 0 -5 -6 -20 -22 .06 33 27 | 2357 -2960 3011 5735
gfz n/a| 0 1 3 -7 -31 -64 .05 30 15 | 0 -2405 3052 7889
grg n/a| 3 -1 -1 31 22 20 .52 28 28 | -319 -2248 3114 7589
iac n/a| -5 -1 -5 1 73 35 -.11 31 25 | 477 -638 3029 8520
mcc n/a| -5 -3 6 125 -28 -341 -.44 118 118 | --- --- --- ---
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 3.2151.0 GPS week: 2151 Day: 0 MJD: 59301
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 | 1180 52 29 60 16 16 26 --- 16 | 108 67 54 73 69 71 --- 70
R02 | 2037 10 17 14 11 8 29 108 7 | 62 55 61 65 65 67 122 61
R03 | 792 16 18 29 18 20 28 98 9 | 89 69 68 87 86 93 68 80
XR04 | 508 16 19 29 --- 15 28 --- 11 | 101 90 80 --- 90 98 --- 90
R05 | 801 16 22 28 14 17 36 56 10 | 80 67 80 80 76 86 65 75
R07 | 1639 11 20 36 28 13 16 136 10 | 84 63 62 92 75 84 87 76
R08 | 744 21 16 21 21 16 16 --- 8 | 75 64 62 73 64 70 --- 67
R09 | 3234 19 16 17 24 39 23 --- 11 | 69 77 86 87 55 82 --- 72
XR11 | 1435 17 --- 19 14 --- 47 --- 15 | 38 --- 47 43 --- 68 --- 46
R12 | 649 17 20 20 19 17 37 --- 9 | 98 84 97 101 84 99 --- 92
R13 | 1956 23 47 42 22 54 27 --- 17 | 112 99 74 94 117 111 --- 99
R14 | 1300 21 14 13 10 14 30 --- 8 | 75 71 65 69 64 49 --- 65
R15 | 822 13 17 22 12 17 45 75 10 | 83 72 71 77 75 99 121 78
R16 | 1206 24 27 19 36 52 27 --- 15 | 54 59 57 50 78 71 --- 59
R17E | 2081 16 34 17 19 14 28 --- 10 | 120 127 126 125 126 118 --- 123
R18E | 500 11 26 13 19 14 29 --- 8 | 52 52 51 64 63 66 --- 56
R19E | 835 32 43 25 46 30 51 --- 17 | 36 41 63 73 57 45 --- 47
R20E | 580 54 50 49 82 66 28 --- 26 | 38 45 50 81 67 43 --- 42
R21E | 1670 14 31 25 20 17 24 183 10 | 65 65 66 74 66 64 44 65
R22E | 782 49 42 52 40 35 46 --- 19 | 32 33 66 52 51 52 --- 36
R24E | 925 21 31 18 21 12 18 --- 9 | 63 64 64 69 67 63 --- 63
------+----------------------------------------------+------------------------------------------
RMS | 1422 27 30 31 30 29 31 117 |T 73 68 69 76 74 76 84 69
WRMS | 1422 20 27 24 18 22 31 117 |NE 80 72 68 76 76 82 92 73
MEDI | 925 17 22 22 19 17 28 98 |MD 75 65 65 73 67 71 68 67
Table 3.2151.1 GPS week: 2151 Day: 1 MJD: 59302
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 | 1003 58 24 50 14 30 17 --- 16 | 69 42 42 34 31 36 --- 35
R02 | 2520 12 14 7 14 11 19 64 6 | 44 40 41 43 44 39 65 40
R03 | 836 14 20 34 13 13 35 93 10 | 56 41 39 55 57 62 47 49
XR04 | 681 26 16 37 --- 19 26 --- 13 | 66 55 55 --- 50 63 --- 55
R05 | 803 22 15 31 21 22 18 98 10 | 54 42 55 44 53 52 49 46
R07 | 1762 15 18 26 18 11 17 141 8 | 59 43 50 64 52 50 45 52
R08 | 951 18 17 18 18 14 15 --- 7 | 45 38 44 43 36 33 --- 38
R09 | 2996 16 13 13 11 46 26 --- 10 | 61 60 62 61 38 69 --- 56
XR11 | 1570 12 --- 18 16 --- 30 --- 11 | 21 --- 32 38 --- 44 --- 33
R12 | 627 31 20 15 17 26 29 --- 10 | 85 61 73 64 55 91 --- 69
R13 | 1735 26 52 38 29 59 34 --- 18 | 75 88 62 71 74 83 --- 72
R14 | 687 20 10 12 16 19 27 --- 8 | 54 48 50 62 37 36 --- 47
R15 | 1852 11 14 24 23 13 13 124 7 | 57 58 53 65 54 59 94 56
R16 | 974 33 40 29 25 61 35 --- 17 | 30 39 33 45 76 68 --- 44
R17E | 2342 19 27 16 17 16 18 --- 8 | 60 65 66 61 66 60 --- 61
R18E | 608 14 27 8 12 15 31 --- 8 | 22 23 24 28 34 41 --- 25
R19E | 1371 38 34 28 36 40 49 --- 17 | 25 28 44 49 48 26 --- 28
R20E | 746 46 65 60 103 75 46 --- 31 | 26 37 52 111 65 35 --- 36
R21E | 1887 19 31 24 18 15 26 220 10 | 37 43 41 44 44 36 36 38
R22E | 1334 39 48 51 57 41 50 --- 21 | 37 42 60 60 52 44 --- 33
R24E | 612 26 31 17 19 18 31 --- 11 | 32 30 28 31 43 35 --- 29
------+----------------------------------------------+------------------------------------------
RMS | 1521 28 31 30 33 34 30 133 |T 48 46 47 53 50 50 56 44
WRMS | 1521 24 26 22 19 24 30 133 |NE 55 50 49 53 50 56 60 49
MEDI | 1003 20 20 24 18 19 27 98 |MD 54 42 50 49 50 44 47 44
Table 3.2151.2 GPS week: 2151 Day: 2 MJD: 59303
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 | 1050 44 25 48 19 24 38 --- 15 | 71 52 43 53 43 70 --- 49
R02 | 2827 13 13 9 12 16 34 67 7 | 44 42 44 44 46 43 53 42
R03 | 1586 12 20 24 15 25 17 87 8 | 70 51 52 72 86 65 25 65
XR04 | 631 21 15 37 --- 11 35 --- 13 | 72 63 47 --- 63 85 --- 62
R05 | 606 12 16 26 8 16 18 179 7 | 47 43 35 53 55 57 75 46
R07 | 1104 9 25 34 31 10 23 154 10 | 68 49 48 83 69 77 42 64
R08 | 1131 14 21 16 15 16 27 --- 8 | 57 45 58 64 56 70 --- 56
R09 | 1447 17 15 22 18 57 25 --- 13 | 53 60 67 62 43 49 --- 51
XR11 | 2149 10 --- 19 11 --- 17 --- 8 | 22 --- 24 25 --- 35 --- 24
R12 | 929 26 24 14 17 13 26 --- 9 | 69 50 61 75 68 57 --- 62
R13 | 3129 27 28 42 18 26 44 --- 14 | 89 71 64 69 79 105 --- 75
R14 | 836 15 14 9 11 15 19 --- 6 | 65 64 65 64 68 71 --- 64
R15 | 1109 10 21 16 14 12 23 223 7 | 66 54 58 73 67 67 189 63
R16 | 2031 29 39 13 17 56 23 --- 14 | 40 33 36 36 62 52 --- 40
R17E | 3647 17 29 12 14 13 34 --- 9 | 40 39 47 47 55 50 --- 44
R18E | 867 16 15 12 12 14 21 --- 6 | 21 22 21 22 31 24 --- 20
R19E | 1812 47 49 28 39 43 56 --- 19 | 23 49 47 57 43 28 --- 30
R20E | 1001 47 49 49 59 61 48 --- 23 | 31 28 62 60 52 47 --- 36
R21E | 1109 17 26 21 15 12 36 155 9 | 37 39 50 52 51 40 50 43
R22E | 1134 37 54 49 65 34 38 --- 21 | 26 44 60 70 51 34 --- 31
R24E | 928 23 32 12 16 12 19 --- 9 | 22 20 21 30 37 31 --- 23
------+----------------------------------------------+------------------------------------------
RMS | 1701 26 30 27 27 30 32 154 |T 49 45 48 55 56 55 72 47
WRMS | 1701 18 27 18 17 17 27 154 |NE 59 52 50 59 61 64 76 54
MEDI | 1109 17 24 21 15 16 26 154 |MD 47 45 48 57 55 52 50 46
Table 3.2151.3 GPS week: 2151 Day: 3 MJD: 59304
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 | 1294 41 27 53 30 31 42 --- 17 | 79 46 54 70 57 75 --- 58
R02 | 2552 13 12 13 19 19 31 68 8 | 42 33 34 47 34 23 74 32
R03 | 1546 14 17 28 14 24 21 66 9 | 69 55 45 71 80 59 28 62
XR04 | 901 21 15 32 --- 15 17 --- 10 | 72 52 40 --- 72 61 --- 58
R05 | 1660 17 22 35 14 27 32 146 11 | 51 41 41 52 67 64 56 48
R07 | 993 18 13 31 13 13 13 131 8 | 63 47 42 62 60 58 38 54
R08 | 999 14 15 19 14 18 17 --- 7 | 56 45 48 50 55 49 --- 49
R09 | 951 25 18 14 19 63 30 --- 14 | 65 62 61 65 51 62 --- 55
XR11 | 1055 14 --- 16 15 --- 20 --- 9 | 20 --- 28 32 --- 35 --- 25
R12 | 1212 25 17 25 16 17 16 --- 9 | 65 46 40 60 50 55 --- 51
R13 | 1890 41 28 46 38 19 31 --- 15 | 83 70 43 80 72 88 --- 70
R14 | 1006 16 10 17 16 11 41 --- 9 | 50 43 37 42 47 63 --- 44
R15 | 604 12 18 19 12 19 38 120 9 | 60 48 49 55 52 72 113 54
R16 | 786 19 28 8 32 43 15 --- 12 | 45 49 47 53 59 52 --- 47
R17E | 3632 15 29 13 12 18 30 --- 9 | 41 44 45 46 49 53 --- 44
R18E | 1090 18 17 15 17 23 18 --- 8 | 22 23 28 30 38 31 --- 25
R19E | 1428 50 51 33 57 35 35 --- 20 | 24 38 36 65 36 19 --- 25
R20E | 1201 39 50 45 56 48 51 --- 21 | 28 33 59 77 51 47 --- 36
R21E | 1751 15 24 16 16 15 23 115 8 | 42 39 50 49 56 44 82 45
R22E | 1246 39 55 50 62 47 34 --- 22 | 33 39 92 94 78 55 --- 54
R24E | 551 15 29 16 15 17 28 --- 9 | 25 23 26 32 39 39 --- 26
------+----------------------------------------------+------------------------------------------
RMS | 1557 26 28 29 30 30 30 112 |T 49 43 45 56 55 52 65 45
WRMS | 1557 20 25 20 17 19 28 112 |NE 58 49 43 56 58 58 61 50
MEDI | 1201 18 18 19 16 19 30 115 |MD 50 44 43 53 52 55 56 48
Table 3.2151.4 GPS week: 2151 Day: 4 MJD: 59305
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 | 809 36 35 64 15 35 23 --- 16 | 76 36 42 63 81 60 --- 56
R02 | 1064 14 12 10 15 14 24 43 7 | 41 29 37 40 38 24 45 33
R03 | 1003 16 17 23 18 13 26 69 8 | 65 53 52 62 65 42 36 55
XR04 | 728 23 17 25 --- 12 25 --- 10 | 74 66 52 --- 72 54 --- 63
R05 | 2176 11 23 23 13 12 23 162 8 | 53 42 52 64 66 69 46 56
R07 | 1233 11 18 36 23 11 18 103 9 | 64 52 42 74 63 63 30 59
R08 | 1251 10 19 22 25 11 27 --- 9 | 52 49 44 67 52 56 --- 52
R09 | 1096 16 13 13 18 39 29 --- 10 | 67 71 73 77 43 70 --- 65
XR11 | 1248 11 --- 17 20 --- 25 --- 10 | 14 --- 30 27 --- 32 --- 18
R12 | 1179 17 17 23 12 19 32 --- 9 | 67 60 54 64 53 81 --- 61
R13 | 1889 30 32 47 19 35 26 --- 14 | 91 101 63 82 95 75 --- 83
R14 | 1401 23 14 13 15 10 24 --- 8 | 64 64 63 58 59 69 --- 61
R15 | 740 17 11 18 19 13 31 76 8 | 65 54 52 50 56 61 84 53
R16 | 1622 13 36 20 19 55 26 --- 13 | 38 39 41 33 50 51 --- 36
R17E | 2478 15 28 17 10 18 23 --- 8 | 60 60 67 63 65 73 --- 63
XR18E | 1283 16 22 --- 35 24 25 --- 12 | 18 35 --- 30 45 35 --- 24
R19E | 1882 44 43 38 41 29 45 --- 18 | 26 40 43 67 32 40 --- 28
R20E | 1135 43 53 59 71 54 56 --- 25 | 25 32 52 78 53 42 --- 33
R21E | 1118 17 28 14 15 27 24 90 9 | 25 27 26 35 37 36 21 26
XR22E | 715 53 --- 57 68 51 42 --- 28 | 31 --- 97 107 58 51 --- 55
R24E | 1105 17 35 20 16 20 30 --- 10 | 24 21 28 38 44 40 --- 28
------+----------------------------------------------+------------------------------------------
RMS | 1442 23 28 31 26 28 30 98 |T 49 49 50 58 56 53 43 48
WRMS | 1442 17 25 25 18 22 26 98 |NE 59 55 49 58 61 57 48 53
MEDI | 1179 17 22 22 18 19 26 76 |MD 53 49 52 63 53 54 36 55
Table 3.2151.5 GPS week: 2151 Day: 5 MJD: 59306
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 49 25 76 15 20 23 --- 18 | 78 59 64 62 59 78 --- 61
R02 | 730 17 10 14 13 11 19 85 6 | 42 31 39 32 39 31 76 33
R03 | 985 11 19 16 15 15 21 78 7 | 56 45 50 51 57 59 36 52
XR04 | 5211 24 19 21 --- 18 30 --- 11 | 69 67 63 --- 56 64 --- 62
R05 | 1846 20 23 23 33 105 30 167 21 | 52 56 56 65 100 58 27 49
R07 | 1242 13 20 27 10 20 19 87 8 | 59 49 51 54 71 67 49 57
R08 | 1279 12 20 26 24 19 20 --- 9 | 49 44 38 48 45 58 --- 45
R09 | 1127 21 24 10 20 49 29 --- 12 | 58 67 56 65 31 52 --- 52
XR11 | 2168 10 --- 14 9 --- 22 --- 8 | 17 --- 23 29 --- 24 --- 20
R12 | 830 21 18 21 11 12 16 --- 7 | 55 44 66 62 55 54 --- 54
R13 | 4211 31 56 55 40 55 37 --- 20 | 67 63 51 81 84 83 --- 67
R14 | 2700 24 11 9 17 13 12 --- 7 | 45 42 45 48 58 53 --- 46
R15 | 1273 13 22 32 16 24 27 78 10 | 49 49 50 57 57 69 39 52
R16 | 2146 34 24 33 12 32 28 --- 12 | 42 33 29 34 37 31 --- 30
R17E | 1074 12 28 15 8 24 29 --- 9 | 72 77 82 82 88 78 --- 78
R18E | 923 13 16 16 25 26 27 --- 9 | 27 28 41 38 40 37 --- 28
R19E | 1710 40 55 47 68 26 38 --- 21 | 47 47 56 91 40 42 --- 44
R20E | 1142 40 57 63 88 50 61 --- 27 | 28 30 66 85 45 47 --- 33
R21E | 707 15 25 14 14 20 18 91 8 | 35 37 38 39 43 31 33 34
R22E | 977 55 54 61 86 38 43 --- 26 | 24 30 97 99 64 54 --- 49
R24E | 602 16 30 15 14 16 19 --- 8 | 40 40 37 39 43 37 --- 36
------+----------------------------------------------+------------------------------------------
RMS | 1617 27 32 36 37 37 29 103 |T 48 46 52 58 55 52 43 46
WRMS | 1617 22 29 26 14 25 24 103 |NE 52 49 48 52 57 55 45 48
MEDI | 1142 20 23 21 15 20 27 85 |MD 49 44 51 54 55 54 36 49
Table 3.2151.6 GPS week: 2151 Day: 6 MJD: 59307
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 | 1425 47 37 67 23 29 17 --- 17 | 105 58 67 92 84 87 --- 79
R02 | 1107 8 17 20 9 13 27 142 7 | 56 41 45 55 56 52 108 50
R03 | 717 7 25 26 11 20 26 88 9 | 76 59 60 81 87 83 38 74
XR04 | 1039 17 11 17 --- 12 14 --- 7 | 88 82 76 --- 79 79 --- 80
R05 | 1140 23 20 23 35 17 20 167 10 | 68 60 82 99 73 75 37 74
R07 | 768 11 22 28 24 14 31 128 10 | 81 63 65 96 86 92 69 80
R08 | 759 12 17 11 21 14 22 --- 7 | 67 53 57 73 63 67 --- 63
R09 | 1442 32 28 16 24 49 27 --- 14 | 66 65 60 63 47 41 --- 50
XR11 | 1292 20 --- 20 14 --- 35 --- 13 | 21 --- 21 27 --- 44 --- 25
R12 | 963 25 34 25 19 14 16 --- 10 | 82 55 74 85 75 72 --- 73
R13 | 6157 33 77 57 29 69 17 --- 22 | 110 66 70 108 131 110 --- 97
R14 | 2267 18 16 18 15 19 14 --- 7 | 72 60 73 70 67 65 --- 66
R15 | 1543 17 24 24 14 14 25 90 9 | 80 66 70 73 79 87 65 74
R16 | 2250 28 32 28 18 36 18 --- 12 | 54 44 60 66 76 62 --- 58
R17E | 586 16 29 16 13 16 26 --- 9 | 96 99 101 98 100 108 --- 99
R18E | 938 12 16 10 12 16 17 --- 6 | 29 26 33 29 40 42 --- 30
R19E | 1250 45 71 54 64 25 49 --- 23 | 38 46 50 84 58 49 --- 42
R20E | 1462 42 55 56 56 38 49 --- 22 | 50 49 51 73 63 62 --- 43
R21E | 742 14 28 11 10 21 34 62 9 | 39 41 44 47 51 40 28 41
R22E | 2038 58 49 36 64 29 69 --- 24 | 31 27 68 64 50 55 --- 41
R24E | 1170 14 26 18 15 16 18 --- 8 | 46 42 43 47 48 41 --- 42
------+----------------------------------------------+------------------------------------------
RMS | 1929 28 37 33 30 28 31 118 |T 64 55 60 71 70 67 57 61
WRMS | 1929 20 33 27 15 28 25 118 |NE 73 59 62 76 77 72 63 67
MEDI | 1170 18 26 23 18 17 25 90 |MD 67 55 60 73 67 65 38 63
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