[IGSREPORT-27989] Wk 2159 IGLOS Final Orbits
acc
acc at igs.org
Tue Jun 15 02:52:24 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2159 (May 23, 2021 - May 29, 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 2.2159.
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:
igl2159[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2159 in the SP3 format.
igl21597.sum Combination Report for GPS Week 2159.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | -10.7 ns
1 | -7.0 ns
2 | -9.7 ns
3 | -11.3 ns
4 | -6.4 ns
5 | -9.5 ns
6 | -8.5 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 1.2159, 1a.2159).
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 2.2159.0-6)
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 3.2159.0-6).
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 2159 summary. (May 23, 2021 - May 29, 2021)
Table 1.2159.a GPS week : 2159 MJD: 59357.0-59363.0
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 -1 10 -5 -4 .11 25 19 | -1816 -2087 3327 8182
| 0 1 1 18 13 22 .04 | 1864 3257
emx n/a| -2 2 3 26 -7 2 -.15 45 32 | -7332 -1049 3320 8696
| 2 2 3 16 27 32 .05 | 9589 2124
esx n/a| 1 1 2 52 17 -34 -.12 37 25 | -7076 -1371 3314 9131
| 1 1 1 15 19 38 .03 | 10899 3461
gfz n/a| 0 0 0 -2 17 -40 -.07 33 18 | 0 -2198 3338 7870
| 1 0 3 20 26 26 .05 | 0 3632
grg n/a| 2 0 2 -47 6 -46 .26 34 23 | -8055 -2175 3344 7777
| 1 1 5 15 9 35 .03 | 1081 3216
iac n/a| -1 -4 -9 -38 -21 162 -.11 32 28 | -7068 -484 3322 8681
| 1 3 4 41 40 59 .05 | 1850 1901
mcc n/a| -1 5 -31 5 -88 -20 -.36 196 196 | --- --- --- ---
| 12 10 9 149 124 449 .32 | --- ---
Table 1.2159.b GPS week : 2159 MJD: 59357.0-59363.0
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 16 17 17 15 16 |
R02 | 8 9 6 10 8 8 10 |
R03 | 8 7 8 7 6 6 7 |
R04 | 9 10 11 15 12 10 10 |
R05 | 9 7 8 9 9 7 7 |
R07 | 8 6 7 6 6 9 7 |
R08 | 8 9 9 10 8 7 9 |
R09 | 10 12 16 14 15 17 13 |
R11 | 8 8 12 11 13 10 12 |
R12 | 8 7 8 9 8 8 8 |
R13 | 20 15 15 23 14 16 15 |
R14 | 8 7 7 8 9 10 8 |
R15 | 7 8 8 9 10 8 8 |
R16 | 12 13 14 18 17 15 13 |
R17 | 8 9 8 8 8 8 8 |
R18 | 9 8 9 10 10 10 9 |
R19 | 22 26 25 25 26 27 28 |
R20 | 31 27 30 33 38 34 27 |
R21 | 11 11 12 10 9 10 10 |
R22 | 33 33 31 32 32 34 30 |
R24 | 11 11 11 13 12 11 12 |
Table 1.2159.c GPS week : 2159 MJD: 59357.0-59363.0
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 2159 0 | -30 11 201 -1195 2553 9529 84.0 1609 1609 | -10730 0
brd 2159 1 | 1 -91 79 435 108 10090 83.3 1636 1636 | -6976 0
brd 2159 2 | -1 24 82 998 12 8096 83.9 1318 1318 | -9736 0
brd 2159 3 | -55 22 68 723 -1087 6795 83.9 1857 1857 | -11284 0
brd 2159 4 | -96 -4 118 -350 -1805 7718 85.1 2277 2277 | -6432 0
brd 2159 5 | 60 -4 255 -68 194 8498 83.2 2072 2072 | -9544 0
brd 2159 6 | -23 128 168 541 1418 8106 81.8 1895 1895 | -8452 0
-------------+------------------------------------------------------------+----------------
brd 2159 mean| -20 12 139 154 199 8404 83.6 1809 1809 | -9022 0
brd 2159 sdev| 49 64 71 751 1457 1107 1.0 318 318 | 1827 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 2.2159.0 GPS week: 2159 Day: 0 MJD: 59357
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 32 11 -9 .08 22 16 | -442 -2824 3381 7949
emx n/a| 1 2 0 11 3 -36 -.13 44 33 | -10799 -1561 3384 8362
esx n/a| 0 1 1 47 37 -77 -.11 37 22 | -13699 -2495 3367 6138
gfz n/a| -1 0 3 10 -27 -57 -.06 37 18 | 0 -3494 3375 7543
grg n/a| 3 0 3 -45 -2 -99 .24 36 26 | -9113 -3380 3413 7246
iac n/a| -3 -4 -3 -53 -6 221 -.08 29 26 | -9620 -16 3392 8505
mcc n/a| 19 15 -35 131 42 -182 -.84 224 224 | --- --- --- ---
Table 2.2159.1 GPS week: 2159 Day: 1 MJD: 59358
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 0 31 -5 -21 .06 23 18 | -546 2726 2988 9195
emx n/a| 0 3 3 13 -34 0 -.14 42 31 | -21131 1670 2990 9670
esx n/a| 0 0 5 24 41 -62 -.08 37 27 | -7077 4464 2975 8461
gfz n/a| -1 1 3 -3 43 -47 -.05 33 17 | 0 3155 3000 8988
grg n/a| 2 -1 -6 -55 2 -3 .22 35 25 | -8395 2491 3000 8494
iac n/a| -1 -3 -5 -43 -29 206 -.12 27 25 | -6686 2621 2972 9695
mcc n/a| -6 19 -20 -103 -186 -139 -.58 251 251 | --- --- --- ---
Table 2.2159.2 GPS week: 2159 Day: 2 MJD: 59359
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 0 1 2 -25 .13 26 20 | -75 -1723 3380 8474
emx n/a| -2 0 5 51 30 56 -.19 46 35 | 1628 -1848 3304 8799
esx n/a| 2 0 2 45 27 -43 -.12 39 26 | -1762 -1247 3356 10268
gfz n/a| 0 0 2 25 46 -61 -.08 32 16 | 0 -2054 3406 8425
grg n/a| 3 -1 1 -59 12 -47 .27 32 22 | -9292 -1517 3350 8190
iac n/a| 0 -1 -6 -8 -57 214 -.09 30 25 | -6195 -2469 3386 8916
mcc n/a| -16 0 -32 67 -259 816 -.62 205 205 | --- --- --- ---
Table 2.2159.3 GPS week: 2159 Day: 3 MJD: 59360
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 0 0 -21 -17 .14 27 22 | -2306 -5692 3396 7686
emx n/a| -5 0 10 12 -6 18 -.07 43 30 | -16862 -3322 3387 8209
esx n/a| 2 -1 2 57 26 -39 -.14 40 28 | 3990 -5030 3387 9443
gfz n/a| 0 1 0 0 22 -42 .00 35 21 | 0 -6627 3377 7361
grg n/a| 2 -1 -1 -69 15 -19 .23 40 22 | -8352 -6020 3433 7192
iac n/a| 0 0 -16 -47 -64 109 -.07 35 35 | -9063 -1484 3410 8222
mcc n/a| -16 10 -22 -220 -89 -407 -.27 189 189 | --- --- --- ---
Table 2.2159.4 GPS week: 2159 Day: 4 MJD: 59361
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 -1 22 -5 34 .13 28 22 | -1972 1842 3450 8305
emx n/a| -1 1 0 39 -41 22 -.21 53 29 | 5550 2224 3450 8929
esx n/a| 3 1 0 70 -4 -57 -.11 39 21 | -1144 2122 3443 10082
gfz n/a| 1 1 0 4 30 -63 -.03 35 19 | 0 2286 3474 7988
grg n/a| 0 0 5 -31 2 -13 .27 32 23 | -7306 1678 3491 7858
iac n/a| -5 -9 -11 -108 21 116 -.12 35 30 | -4196 509 3446 8849
mcc n/a| 3 -5 -34 -115 -114 -456 -.16 136 136 | --- --- --- ---
Table 2.2159.5 GPS week: 2159 Day: 5 MJD: 59362
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 -1 6 4 -8 .15 24 17 | -1810 -4597 3434 8368
emx n/a| -4 0 -1 37 -24 -13 -.18 43 34 | -4796 -2227 3475 9073
esx n/a| 0 2 1 67 -5 22 -.11 31 20 | -1508 -3540 3418 10225
gfz n/a| 0 0 0 -37 1 2 -.17 31 18 | 0 -4435 3455 8124
grg n/a| 2 1 8 -45 -2 -76 .27 37 26 | -7752 -3863 3414 8332
iac n/a| -1 -7 -7 -31 38 75 -.07 31 28 | -6222 -2799 3404 8800
mcc n/a| -1 7 -25 163 100 -108 -.08 161 161 | --- --- --- ---
Table 2.2159.6 GPS week: 2159 Day: 6 MJD: 59363
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 -1 -18 -25 17 .06 24 19 | -5565 -4344 3265 7298
emx n/a| -2 6 2 22 17 -29 -.15 47 29 | -4915 -2285 3250 7830
esx n/a| -1 2 2 56 2 14 -.17 39 28 | -28338 -3875 3258 9302
gfz n/a| -1 0 -5 -16 9 -11 -.08 28 17 | 0 -4217 3283 6661
grg n/a| 2 -1 6 -26 20 -64 .32 28 18 | -6180 -4614 3309 7132
iac n/a| 0 -6 -11 26 -48 193 -.21 36 26 | -7497 249 3249 7780
mcc n/a| 5 -7 -49 115 -115 333 .03 204 204 | --- --- --- ---
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 3.2159.0 GPS week: 2159 Day: 0 MJD: 59357
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 | 672 36 34 29 19 49 42 --- 16 | 83 73 57 76 48 93 --- 70
R02 | 1914 11 12 19 26 19 23 115 8 | 48 47 56 62 47 50 173 49
R03 | 737 15 10 9 15 16 28 214 7 | 56 60 59 65 63 72 135 61
XR04 | 797 14 19 11 --- 14 25 --- 8 | 54 58 40 --- 42 46 --- 46
R05 | 967 14 15 17 17 19 29 417 8 | 126 130 117 122 125 144 231 126
R07 | 571 7 9 7 17 18 31 149 7 | 60 59 62 68 55 68 79 60
R08 | 1006 9 10 18 21 16 25 --- 7 | 53 53 55 65 46 54 --- 52
R09E | 3968 22 20 15 25 18 26 --- 9 | 141 136 130 136 136 142 --- 135
XR11E | 3368 12 18 10 21 --- 17 --- 7 | 59 69 62 68 --- 57 --- 60
R12E | 1594 10 27 9 14 18 21 --- 7 | 48 48 47 47 48 56 --- 48
R13E | 2493 18 36 24 80 41 53 --- 19 | 31 36 38 68 51 44 --- 31
R14E | 1234 9 14 22 13 18 21 --- 7 | 53 50 51 50 55 54 --- 51
R15E | 800 7 23 13 17 14 15 75 6 | 65 66 69 65 67 67 97 65
R16E | 1258 22 27 27 33 30 18 --- 11 | 51 56 69 71 69 65 --- 59
R17 | 1675 13 25 11 12 25 12 --- 7 | 69 37 56 67 62 55 --- 58
R18 | 798 12 26 19 24 12 21 --- 8 | 80 64 83 77 84 68 --- 75
R19 | 943 30 83 36 53 63 36 --- 22 | 82 45 49 101 82 73 --- 65
R20 | 787 45 109 89 64 70 25 --- 30 | 126 51 51 135 134 108 --- 96
R21 | 2059 11 37 21 12 12 42 201 11 | 92 64 72 83 86 99 147 83
R22 | 2042 44 87 106 87 86 28 --- 33 | 43 72 108 54 40 48 --- 42
R24 | 775 13 54 18 18 26 18 --- 11 | 75 36 68 78 79 77 --- 69
------+----------------------------------------------+------------------------------------------
RMS | 1608 22 44 37 37 36 29 224 |T 71 62 66 77 70 73 143 66
WRMS | 1608 16 33 22 18 26 26 224 |NE 74 60 66 81 70 75 153 68
MEDI | 1006 13 25 18 19 18 25 149 |MD 60 58 59 68 62 67 135 60
Table 3.2159.1 GPS week: 2159 Day: 1 MJD: 59358
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 | 859 25 20 40 23 32 32 --- 13 | 52 48 41 55 31 66 --- 46
R02 | 2267 11 16 13 16 16 35 133 8 | 33 31 31 28 22 52 119 30
R03 | 654 15 13 16 15 9 14 242 6 | 38 40 52 49 40 40 104 41
XR04 | 692 12 10 25 --- 22 26 --- 10 | 38 40 30 --- 32 60 --- 38
R05 | 649 18 16 17 13 11 18 314 7 | 99 96 87 89 95 101 158 93
R07 | 1118 10 11 11 13 16 13 118 5 | 37 37 41 44 44 40 47 38
R08 | 1352 13 10 7 23 22 32 --- 9 | 30 29 30 42 30 35 --- 29
R09E | 4613 17 22 18 37 28 31 --- 11 | 125 117 111 121 115 127 --- 118
XR11E | 3401 10 16 13 16 --- 21 --- 7 | 55 59 57 59 --- 46 --- 54
R12E | 722 9 26 16 11 11 19 --- 7 | 27 32 26 26 31 35 --- 26
R13E | 1211 24 28 29 38 43 35 --- 14 | 29 36 50 69 54 47 --- 38
R14E | 887 9 15 19 13 19 19 --- 7 | 33 38 39 36 43 43 --- 36
R15E | 1295 9 24 14 17 9 27 43 8 | 61 56 64 63 55 72 70 61
R16E | 1075 24 24 28 39 24 35 --- 13 | 21 26 39 55 33 37 --- 25
R17 | 2235 15 29 12 17 24 25 --- 9 | 40 26 35 39 51 28 --- 34
R18 | 1155 10 27 18 19 22 13 --- 8 | 64 57 59 58 74 61 --- 60
R19 | 1015 37 89 48 62 82 30 --- 26 | 42 44 67 68 57 43 --- 43
R20 | 972 49 96 86 41 42 27 --- 26 | 67 38 41 60 60 55 --- 48
R21 | 1387 13 40 21 10 20 32 432 10 | 57 43 45 46 67 75 287 54
R22 | 1786 51 74 99 90 83 23 --- 32 | 54 79 63 50 40 49 --- 42
R24 | 856 20 50 14 15 13 22 --- 10 | 45 31 42 40 46 43 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1636 23 42 37 33 35 27 251 |T 49 47 50 54 51 55 130 47
WRMS | 1636 18 31 27 17 25 25 251 |NE 49 45 47 51 49 53 143 45
MEDI | 1118 15 24 18 17 22 26 133 |MD 42 40 42 50 44 47 104 41
Table 3.2159.2 GPS week: 2159 Day: 2 MJD: 59359
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 | 905 34 38 34 30 38 34 --- 15 | 63 80 51 57 46 50 --- 52
R02 | 1898 10 12 13 12 9 20 199 5 | 37 37 35 35 40 40 148 35
R03 | 666 14 28 16 13 9 28 286 8 | 44 60 51 47 47 55 230 47
XR04 | 590 21 22 14 --- 28 24 --- 11 | 50 45 39 --- 33 47 --- 40
R05 | 589 21 19 19 15 14 21 192 8 | 130 139 134 137 130 150 193 134
R07 | 1334 7 12 13 10 17 24 126 6 | 48 50 45 48 51 40 143 44
R08 | 1859 12 9 15 21 11 37 --- 9 | 44 40 53 52 44 36 --- 41
XR09E | 4463 26 --- 28 38 26 35 --- 15 | 102 --- 122 114 92 120 --- 107
XR11E | 4472 14 25 15 17 --- 38 --- 11 | 45 38 45 49 --- 50 --- 43
R12E | 1086 11 28 15 15 17 22 --- 8 | 24 27 25 25 30 39 --- 24
R13E | 2061 25 40 27 37 41 25 --- 14 | 36 32 36 61 57 43 --- 36
R14E | 871 10 18 18 14 11 18 --- 6 | 34 35 40 38 45 38 --- 36
R15E | 792 11 26 15 17 16 20 192 7 | 49 46 53 50 48 53 171 48
R16E | 903 28 32 27 43 31 21 --- 13 | 24 28 37 50 40 32 --- 27
R17 | 2154 17 28 15 16 14 15 --- 7 | 53 31 49 49 38 43 --- 44
R18 | 1491 5 31 24 17 27 18 --- 9 | 45 37 53 35 50 44 --- 41
R19 | 1546 48 95 38 47 76 26 --- 25 | 56 49 55 78 56 43 --- 49
R20 | 849 42 101 109 51 45 42 --- 30 | 96 37 36 100 102 103 --- 78
R21 | 1092 15 42 30 10 22 40 --- 12 | 69 41 60 65 61 88 --- 64
R22 | 1120 58 78 86 82 57 59 --- 31 | 33 71 68 53 38 85 --- 37
R24 | 869 18 47 20 25 11 24 --- 11 | 50 33 39 55 47 56 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 1317 26 46 39 32 32 30 205 |T 53 47 53 59 54 59 177 51
WRMS | 1317 20 35 26 16 22 25 205 |NE 58 53 54 62 55 62 178 53
MEDI | 1092 17 28 19 17 17 24 192 |MD 48 38 49 50 47 47 171 44
Table 3.2159.3 GPS week: 2159 Day: 3 MJD: 59360
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 43 28 42 29 20 47 --- 16 | 59 53 49 51 52 65 --- 46
R02 | 1077 12 9 10 16 19 51 160 10 | 39 39 43 48 46 47 146 37
R03 | 901 7 13 12 11 11 27 172 6 | 42 48 46 38 39 55 219 43
XR04 | 629 24 21 21 --- 33 42 --- 14 | 45 49 27 --- 18 47 --- 34
R05 | 687 16 10 11 20 17 32 184 8 | 67 75 86 91 71 81 162 77
R07 | 1862 7 8 7 17 14 18 176 5 | 46 53 54 62 46 50 121 51
R08 | 1274 16 15 18 20 12 41 --- 9 | 48 56 52 49 42 33 --- 44
R09E | 5185 31 20 21 23 42 45 --- 14 | 97 97 112 108 107 132 --- 104
XR11E | 4812 15 12 11 24 --- 40 --- 11 | 32 36 38 41 --- 40 --- 34
R12E | 1349 8 24 16 12 21 30 --- 8 | 24 30 32 28 44 24 --- 27
R13E | 3559 31 37 37 57 88 36 --- 22 | 35 42 51 55 107 48 --- 44
R14E | 994 14 18 18 14 14 22 --- 7 | 26 30 32 28 38 45 --- 29
R15E | 1462 11 29 13 23 16 22 229 8 | 71 70 70 71 70 76 164 70
R16E | 1655 28 40 40 45 50 45 --- 18 | 26 31 50 58 57 41 --- 31
R17 | 1113 11 31 13 19 12 21 --- 8 | 60 39 46 61 55 56 --- 52
R18 | 865 16 28 21 27 15 27 --- 10 | 42 40 57 71 48 48 --- 48
R19 | 1756 56 90 47 35 59 33 --- 25 | 70 48 55 72 57 60 --- 49
R20 | 732 36 112 101 65 69 49 --- 33 | 103 63 74 126 135 109 --- 90
R21 | 891 14 34 23 11 14 30 204 9 | 71 50 54 68 67 84 224 64
R22 | 1282 54 44 98 85 80 32 --- 31 | 29 61 93 47 38 60 --- 40
R24 | 822 15 54 24 26 16 31 --- 13 | 74 37 52 76 70 82 --- 63
------+----------------------------------------------+------------------------------------------
RMS | 1857 27 43 40 35 40 35 189 |T 52 49 55 62 60 61 172 51
WRMS | 1857 22 30 28 21 22 35 189 |NE 56 50 56 66 56 62 174 52
MEDI | 1274 16 28 21 23 17 32 176 |MD 46 48 52 58 52 55 162 46
Table 3.2159.4 GPS week: 2159 Day: 4 MJD: 59361
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 | 1907 43 24 36 31 37 49 --- 17 | 58 51 44 50 42 53 --- 42
R02 | 1356 13 15 12 16 19 30 191 8 | 39 35 44 54 58 49 78 44
R03 | 1766 9 9 7 16 9 21 118 5 | 38 38 42 49 45 44 76 40
XR04 | 672 21 25 17 --- 25 26 --- 11 | 41 44 26 --- 30 30 --- 30
R05 | 1201 17 13 21 15 15 36 87 9 | 140 146 141 149 148 157 178 145
R07 | 786 9 11 9 8 11 27 153 6 | 44 42 49 47 46 67 62 48
R08 | 1073 14 13 10 17 12 37 --- 8 | 42 44 41 46 35 31 --- 37
R09E | 6127 34 32 22 27 42 39 --- 15 | 106 117 109 112 115 100 --- 106
XR11E | 5088 12 17 13 27 --- 47 --- 12 | 42 45 52 52 --- 51 --- 45
R12E | 1519 14 21 11 23 17 18 --- 7 | 33 31 33 37 38 36 --- 32
R13E | 5218 29 41 21 51 20 24 --- 14 | 24 43 38 50 51 40 --- 33
R14E | 803 15 25 21 18 14 31 --- 9 | 25 31 32 28 30 47 --- 26
R15E | 1913 14 32 22 19 17 33 81 10 | 114 123 136 117 125 110 92 120
R16E | 2895 37 44 21 42 46 36 --- 17 | 27 32 54 65 68 46 --- 43
R17 | 911 14 29 11 18 19 22 --- 8 | 57 38 44 49 56 49 --- 48
R18 | 695 8 22 24 13 17 37 --- 9 | 45 45 57 44 49 34 --- 44
R19 | 1638 42 122 42 47 40 50 --- 25 | 73 41 47 73 58 73 --- 49
R20 | 716 55 143 113 66 63 54 --- 37 | 112 100 63 112 107 105 --- 85
R21 | 1096 18 27 18 19 14 31 149 9 | 69 49 61 70 66 46 90 60
R22 | 852 48 64 91 83 77 35 --- 31 | 45 66 75 48 43 45 --- 39
R24 | 692 19 56 20 16 13 32 --- 11 | 69 40 55 63 62 71 --- 59
------+----------------------------------------------+------------------------------------------
RMS | 2277 28 52 39 35 32 35 136 |T 59 57 59 65 63 61 96 55
WRMS | 2277 22 29 21 19 23 30 136 |NE 62 55 56 65 60 61 96 55
MEDI | 1201 17 25 21 19 17 33 118 |MD 45 44 49 50 51 49 78 44
Table 3.2159.5 GPS week: 2159 Day: 5 MJD: 59362
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 | 1995 29 33 32 27 42 36 --- 14 | 54 51 62 62 46 65 --- 53
R02 | 1367 10 14 21 12 17 22 264 7 | 32 29 34 38 35 42 111 32
R03 | 1972 12 12 10 9 17 14 141 5 | 33 34 35 37 48 35 43 34
XR04 | 599 18 25 12 --- 24 19 --- 9 | 34 31 20 --- 20 20 --- 22
R05 | 939 12 16 16 17 11 22 91 7 | 128 125 122 116 129 129 145 124
R07 | 756 15 22 17 21 16 24 179 8 | 40 33 57 63 49 43 44 47
R08 | 1067 14 17 13 16 12 20 --- 7 | 38 31 41 48 43 51 --- 40
R09E | 5689 41 31 24 35 43 54 --- 17 | 115 113 114 112 110 122 --- 109
XR11E | 5155 16 15 11 23 --- 26 --- 9 | 35 40 42 53 --- 39 --- 39
R12E | 1115 11 26 11 14 17 28 --- 8 | 50 51 37 46 45 51 --- 44
R13E | 4037 27 48 25 43 33 38 --- 15 | 39 43 35 53 62 57 --- 39
R14E | 881 17 26 20 11 25 27 --- 9 | 30 33 36 28 33 44 --- 28
R15E | 2514 11 23 15 14 18 27 91 8 | 94 96 90 89 95 87 76 91
R16E | 1242 34 31 13 43 32 38 --- 14 | 25 19 31 60 43 59 --- 32
R17 | 1138 14 32 11 21 16 20 --- 8 | 44 31 42 49 37 36 --- 39
R18 | 905 12 31 18 15 24 30 --- 9 | 37 35 38 35 47 33 --- 34
R19 | 1051 37 118 47 45 76 42 --- 27 | 72 46 44 83 93 65 --- 63
XR20 | 942 39 --- 113 64 33 40 --- 34 | 89 --- 68 114 87 78 --- 82
R21 | 1330 13 38 17 21 21 22 130 9 | 50 32 39 50 62 39 56 44
R22 | 791 50 68 98 81 97 44 --- 34 | 35 77 81 53 51 36 --- 41
R24 | 896 15 54 17 15 19 22 --- 10 | 52 37 43 47 52 49 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 2072 24 43 31 31 37 31 161 |T 53 49 52 61 59 56 79 51
WRMS | 2072 17 34 20 18 26 28 161 |NE 52 45 51 61 57 51 79 50
MEDI | 1115 15 26 17 21 21 27 130 |MD 40 35 42 53 48 49 56 41
Table 3.2159.6 GPS week: 2159 Day: 6 MJD: 59363
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 | 1260 27 25 36 34 37 54 --- 16 | 80 68 54 69 59 101 --- 68
R02 | 2556 17 13 16 18 11 52 372 10 | 50 48 65 60 56 86 195 57
R03 | 719 8 15 12 11 11 29 141 6 | 51 54 59 52 57 58 51 54
XR04 | 819 19 22 18 --- 21 18 --- 9 | 53 48 27 --- 34 38 --- 38
R05 | 689 9 18 22 8 18 23 149 7 | 150 153 140 147 151 150 184 147
R07 | 1548 8 11 10 19 17 18 172 6 | 59 55 63 71 63 55 79 61
R08 | 956 20 17 30 15 10 18 --- 8 | 52 56 82 71 66 61 --- 63
R09E | 4756 30 27 23 32 26 34 --- 13 | 119 115 115 111 108 109 --- 111
XR11E | 4035 16 16 16 31 --- 31 --- 11 | 55 58 55 66 --- 61 --- 56
R12E | 1007 13 28 12 14 11 25 --- 7 | 59 62 59 58 65 65 --- 60
R13E | 3140 32 39 25 38 15 48 --- 14 | 31 38 33 64 38 56 --- 33
R14E | 974 9 19 18 16 15 24 --- 7 | 37 42 42 43 41 49 --- 39
R15E | 1771 11 28 17 16 11 22 162 7 | 93 93 99 95 94 91 107 93
R16E | 1829 28 28 19 32 30 35 --- 13 | 34 30 44 51 48 38 --- 36
R17 | 1630 9 37 14 14 13 22 --- 8 | 72 45 63 74 67 66 --- 65
R18 | 1058 17 37 17 13 19 20 --- 9 | 66 57 71 64 70 63 --- 64
R19 | 983 35 128 51 54 64 40 --- 28 | 92 53 54 120 104 98 --- 84
R20 | 1299 41 100 92 47 36 33 --- 26 | 139 58 55 155 144 128 --- 114
R21 | 1245 12 44 19 18 13 21 119 9 | 89 57 70 88 86 93 86 81
R22 | 2318 52 44 106 46 64 72 --- 29 | 33 66 120 45 78 58 --- 48
R24 | 1227 15 44 25 21 17 46 --- 12 | 74 48 67 83 79 74 --- 70
------+----------------------------------------------+------------------------------------------
RMS | 1895 24 47 39 28 28 36 204 |T 70 62 68 79 75 76 117 68
WRMS | 1895 19 29 28 17 18 26 204 |NE 75 61 70 84 79 80 119 72
MEDI | 1260 17 28 19 18 17 29 149 |MD 59 56 63 69 66 65 86 63
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