[IGSREPORT-27932] Wk 2155 IGLOS Final Orbits
acc
acc at igs.org
Mon May 17 00:45:18 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2155 (Apr 25, 2021 - May 01, 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 2.2155.
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:
igl2155[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2155 in the SP3 format.
igl21557.sum Combination Report for GPS Week 2155.
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 | 1.0 ns
1 | -0.5 ns
2 | -0.9 ns
3 | 0.8 ns
4 | 0.9 ns
5 | 0.0 ns
6 | 0.2 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 1.2155, 1a.2155).
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 2.2155.0-6)
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 3.2155.0-6).
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 2155 summary. (Apr 25, 2021 - May 01, 2021)
Table 1.2155.a GPS week : 2155 MJD: 59329.0-59335.0
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 0 -1 20 -20 24 .14 23 18 | -92 330 3372 8177
| 0 1 1 11 12 27 .02 | 1454 959
emx n/a| 0 1 5 -21 -11 -43 -.10 32 27 | -2912 735 3378 8574
| 0 1 2 17 20 29 .04 | 4563 718
esx n/a| 1 0 0 10 31 -43 -.06 28 20 | 3108 855 3365 8173
| 1 0 2 10 17 23 .05 | 5458 943
gfz n/a| 0 1 0 -14 1 -48 -.08 33 17 | 0 214 3338 7950
| 1 1 1 19 19 39 .04 | 0 1126
grg n/a| 1 -1 -6 -2 22 -40 .32 33 22 | 21 253 3387 7653
| 0 1 3 25 11 46 .05 | 601 672
iac n/a| -1 -3 3 7 -23 188 -.27 34 31 | 2208 -214 3370 8621
| 3 2 3 41 24 71 .06 | 861 1276
mcc n/a| -1 1 -44 30 -67 9 -.63 260 260 | --- --- --- ---
| 11 8 7 158 91 705 .52 | --- ---
Table 1.2155.b GPS week : 2155 MJD: 59329.0-59335.0
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 | 15 15 12 13 14 15 16 |
R02 | 6 6 8 6 9 8 8 |
R03 | 6 9 8 6 7 7 7 |
R04 | 12 10 13 12 13 11 10 |
R05 | 8 9 10 9 9 7 9 |
R07 | 8 6 6 9 8 7 7 |
R08 | 8 7 8 8 9 6 9 |
R09 | 13 20 20 15 18 17 16 |
R11 | 12 9 9 10 9 8 9 |
R12 | 12 11 11 10 10 10 11 |
R13 | 18 22 21 21 20 19 19 |
R14 | 8 8 7 7 9 10 7 |
R15 | 9 9 9 9 8 8 10 |
R16 | 12 14 12 14 17 14 13 |
R17 | 8 7 9 8 8 8 10 |
R18 | 7 7 11 7 8 7 8 |
R19 | 19 17 17 20 21 19 19 |
R20 | 22 25 22 20 21 21 24 |
R21 | 9 9 8 9 9 9 10 |
R22 | 29 24 25 27 23 22 27 |
R24 | 8 9 8 9 9 10 8 |
Table 1.2155.c GPS week : 2155 MJD: 59329.0-59335.0
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 2155 0 | -55 -56 164 468 756 6757 83.1 1584 1584 | 1017 0
brd 2155 1 | -64 40 102 -690 -108 758 81.0 1445 1445 | -477 0
brd 2155 2 | 62 60 -16 527 -59 -2566 83.6 1558 1558 | -858 0
brd 2155 3 | -29 110 95 -2037 -1519 -6025 83.6 1865 1865 | 816 0
brd 2155 4 | -8 60 126 -1618 -2798 -4725 79.7 2221 2221 | 863 0
brd 2155 5 | -71 -66 125 -355 -1521 5622 82.5 2254 2254 | 0 0
brd 2155 6 | -60 -9 223 -596 -998 6262 83.1 1662 1662 | 187 0
-------------+------------------------------------------------------------+----------------
brd 2155 mean| -32 19 117 -614 -892 869 82.4 1798 1798 | 221 0
brd 2155 sdev| 47 65 73 964 1187 5431 1.5 326 326 | 718 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 2.2155.0 GPS week: 2155 Day: 0 MJD: 59329
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 0 29 -19 62 .12 20 18 | -536 1136 3493 8686
emx n/a| 0 1 2 -22 -3 -58 -.13 29 25 | -3865 1434 3499 9118
esx n/a| 3 0 -1 6 48 -51 -.12 30 22 | 4601 920 3482 7066
gfz n/a| 1 0 1 -49 -22 -91 -.09 39 24 | 0 1544 3516 8540
grg n/a| 1 0 -4 -2 9 -2 .28 29 18 | 1135 -199 3487 8074
iac n/a| 4 0 5 55 -47 93 -.15 32 32 | 1219 2110 3476 9053
mcc n/a| 5 13 -51 -45 -156 -371 -1.17 208 208 | --- --- --- ---
Table 2.2155.1 GPS week: 2155 Day: 1 MJD: 59330
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 -2 8 -5 38 .17 25 21 | -598 -411 3452 7620
emx n/a| 0 0 1 7 -13 2 -.12 31 27 | 817 -151 3468 8010
esx n/a| 1 -1 -1 3 6 -39 -.06 30 21 | 9799 265 3452 9047
gfz n/a| -1 0 3 -24 -16 -103 -.09 30 13 | 0 -594 3437 7523
grg n/a| 1 0 0 -5 18 2 .31 32 21 | -397 -143 3524 7141
iac n/a| 0 -2 1 44 21 122 -.29 33 33 | 2357 -384 3454 8028
mcc n/a| 9 -3 -42 139 -45 -815 .10 264 264 | --- --- --- ---
Table 2.2155.2 GPS week: 2155 Day: 2 MJD: 59331
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 40 -20 30 .11 24 17 | -1831 -1446 3543 8810
emx n/a| 0 1 8 -22 28 -74 -.02 32 28 | -9436 -206 3545 9257
esx n/a| 0 0 1 8 7 -35 -.02 28 20 | 8934 -764 3526 10570
gfz n/a| 1 1 0 -10 0 -48 -.08 33 17 | 0 -1583 3510 8661
grg n/a| 1 0 -8 -40 12 -64 .25 30 19 | -466 -691 3438 7588
iac n/a| -6 -7 2 19 -40 311 -.31 34 34 | 1267 -1038 3548 9270
mcc n/a| 1 9 -40 15 -197 -511 .08 312 312 | --- --- --- ---
Table 2.2155.3 GPS week: 2155 Day: 3 MJD: 59332
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 12 -19 -23 .15 22 17 | -1293 1327 3246 10125
emx n/a| 0 2 8 -10 -22 -26 -.13 31 27 | -6033 1234 3240 10654
esx n/a| 1 0 0 2 41 -1 -.06 25 18 | 3385 2133 3238 9653
gfz n/a| 1 0 -2 5 5 -18 -.11 36 16 | 0 1078 3209 9463
grg n/a| 3 0 -10 -7 38 -24 .30 31 18 | 92 1272 3194 9621
iac n/a| -5 -5 8 2 -41 198 -.33 37 30 | 2106 837 3244 10655
mcc n/a| 4 4 -29 69 -46 1033 -1.00 192 192 | --- --- --- ---
Table 2.2155.4 GPS week: 2155 Day: 4 MJD: 59333
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 -3 24 -38 19 .12 22 19 | 721 517 3632 7844
emx n/a| -2 1 6 -40 -9 -63 -.15 33 26 | -4645 1502 3626 7952
esx n/a| 2 1 0 21 34 -37 -.11 26 19 | -4608 580 3635 6419
gfz n/a| 2 1 0 -20 -7 11 .02 29 16 | 0 1191 3622 7551
grg n/a| 1 -1 -5 -23 21 -66 .31 38 25 | 462 510 3682 7420
iac n/a| -3 -3 3 2 -31 194 -.31 37 35 | 3583 -800 3638 8413
mcc n/a| 6 -2 -47 -227 66 725 -1.00 206 206 | --- --- --- ---
Table 2.2155.5 GPS week: 2155 Day: 5 MJD: 59334
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 16 -7 7 .15 22 16 | 354 634 3040 6734
emx n/a| 0 1 5 -43 -25 -67 -.08 33 28 | -1600 881 3070 7171
esx n/a| 0 0 4 27 46 -71 .01 26 20 | -3062 1355 3047 5300
gfz n/a| -1 2 -1 10 17 -45 -.10 33 21 | 0 -291 3059 6664
grg n/a| 1 -2 -8 33 35 -6 .36 33 23 | -169 182 3117 6736
iac n/a| 0 -2 3 -72 -20 167 -.26 27 24 | 1944 -562 3037 7105
mcc n/a| -22 -7 -52 -18 -100 407 -.57 275 275 | --- --- --- ---
Table 2.2155.6 GPS week: 2155 Day: 6 MJD: 59335
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 9 -33 35 .15 25 18 | 2536 553 3204 7426
emx n/a| -1 3 7 -21 -34 -18 -.07 35 25 | 4377 454 3198 7856
esx n/a| 0 0 2 1 39 -65 -.08 27 19 | 2710 1497 3179 9162
gfz n/a| -1 2 -1 -10 32 -43 -.07 31 15 | 0 154 3017 7250
grg n/a| 1 -3 -7 26 18 -123 .41 35 28 | -507 843 3267 6996
iac n/a| 0 -4 -1 1 -8 230 -.25 34 29 | 2983 -1664 3195 7823
mcc n/a| -12 -7 -49 279 5 -402 -.83 362 362 | --- --- --- ---
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 3.2155.0 GPS week: 2155 Day: 0 MJD: 59329
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 | 530 31 27 55 21 23 25 --- 15 | 82 76 64 72 62 82 --- 70
R02 | 721 9 8 10 14 12 20 220 5 | 52 47 54 52 48 59 161 50
R03 | 752 6 10 17 9 13 20 --- 5 | 57 60 56 64 65 66 --- 59
XR04 | 984 23 23 24 --- 22 20 --- 11 | 57 55 38 --- 40 36 --- 45
R05 | 1221 14 12 24 25 16 17 72 8 | 36 46 50 46 34 40 60 38
R07 | 723 8 13 10 19 12 33 111 7 | 59 59 56 61 55 61 160 57
R08 | 689 11 14 13 19 20 32 --- 8 | 57 59 55 63 59 81 --- 60
R09 | 3411 13 17 20 21 56 34 --- 13 | 99 93 109 108 78 114 --- 95
XR11 | 2805 14 28 15 15 --- 38 --- 11 | 29 31 29 38 --- 49 --- 30
R12 | 1137 27 38 23 11 16 35 --- 12 | 87 51 54 70 65 75 --- 66
R13 | 3875 33 45 56 41 38 25 --- 18 | 116 75 70 117 98 107 --- 93
R14 | 804 14 26 12 12 15 29 --- 8 | 94 81 88 92 91 103 --- 90
R15 | 649 21 21 10 16 12 28 --- 8 | 72 47 50 62 58 50 --- 57
R16 | 980 15 23 24 42 30 27 --- 12 | 58 48 74 63 74 75 --- 63
R17E | 1663 9 26 15 18 10 29 --- 8 | 94 91 92 100 93 96 --- 93
R18E | 1063 10 17 14 10 13 25 --- 6 | 35 31 37 37 43 46 --- 35
R19E | 1193 20 49 45 62 36 43 --- 19 | 36 35 49 74 53 47 --- 37
R20E | 916 35 59 43 68 30 66 --- 22 | 76 82 84 101 83 86 --- 78
R21E | 921 13 29 14 19 12 23 328 8 | 69 69 72 82 73 63 88 70
R22E | 1998 39 34 62 115 77 40 --- 29 | 32 49 73 80 57 58 --- 37
R24E | 1685 13 27 14 16 12 28 --- 8 | 53 50 48 56 55 71 --- 52
------+----------------------------------------------+------------------------------------------
RMS | 1584 20 29 30 39 29 32 208 |T 64 58 62 71 64 69 117 60
WRMS | 1584 18 25 22 24 18 32 208 |NE 68 59 60 69 63 71 127 62
MEDI | 984 14 26 17 19 16 28 111 |MD 58 55 56 64 59 66 88 59
Table 3.2155.1 GPS week: 2155 Day: 1 MJD: 59330
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 | 711 29 20 55 27 32 20 --- 14 | 60 56 44 54 64 59 --- 51
R02 | 1356 14 8 19 11 11 19 364 6 | 47 44 48 43 45 48 151 44
R03 | 1223 9 14 13 13 27 40 --- 9 | 50 51 57 57 67 49 --- 53
XR04 | 577 16 20 15 --- 18 31 --- 10 | 47 49 43 --- 42 45 --- 44
R05 | 577 17 22 16 29 16 15 63 9 | 38 42 46 49 37 37 36 39
R07 | 926 13 12 13 9 10 23 117 6 | 54 53 62 59 65 63 120 58
R08 | 830 10 10 18 16 16 17 --- 6 | 50 54 57 60 59 54 --- 54
R09 | 2785 32 26 29 34 80 40 --- 19 | 129 128 129 134 66 101 --- 112
XR11 | 2428 15 23 17 16 --- 21 --- 9 | 45 39 38 48 --- 54 --- 43
R12 | 1261 29 29 20 17 18 21 --- 10 | 77 55 62 63 63 64 --- 62
R13 | 3175 37 57 58 47 46 42 --- 21 | 91 82 83 103 75 105 --- 84
R14 | 948 18 22 16 15 18 22 --- 8 | 110 107 115 109 99 121 --- 109
R15 | 639 22 21 10 16 14 32 --- 9 | 66 56 54 60 61 50 --- 57
R16 | 1199 31 22 40 29 25 28 --- 13 | 56 60 72 67 63 66 --- 60
R17E | 814 12 20 13 9 13 20 --- 6 | 43 39 43 42 47 49 --- 42
R18E | 2428 9 24 12 8 19 21 --- 7 | 30 28 28 20 31 39 --- 26
R19E | 957 24 43 45 41 31 40 --- 17 | 49 56 71 79 52 47 --- 51
R20E | 1141 44 62 44 60 43 73 --- 24 | 70 95 91 95 71 76 --- 76
R21E | 717 13 28 15 17 11 33 358 9 | 55 54 51 49 56 50 49 50
R22E | 1467 49 51 43 64 59 38 --- 23 | 27 45 52 60 65 45 --- 36
R24E | 583 15 19 18 12 21 30 --- 8 | 36 27 29 34 39 50 --- 31
------+----------------------------------------------+------------------------------------------
RMS | 1445 25 31 30 30 32 33 264 |T 58 58 60 64 58 60 89 56
WRMS | 1445 21 27 21 13 21 33 264 |NE 65 62 65 69 62 65 102 62
MEDI | 957 17 22 18 16 18 28 117 |MD 50 54 54 59 61 50 49 51
Table 3.2155.2 GPS week: 2155 Day: 2 MJD: 59331
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 | 668 24 23 36 20 30 21 --- 12 | 66 66 59 62 65 64 --- 60
R02 | 2822 12 10 22 10 15 34 520 8 | 40 40 35 34 29 61 365 36
R03 | 1014 9 11 8 7 16 42 --- 8 | 46 54 51 49 50 39 --- 46
XR04 | 1061 20 23 21 --- 14 45 --- 12 | 43 48 31 --- 34 42 --- 34
R05 | 681 18 22 14 36 10 20 63 9 | 24 43 37 60 31 40 75 33
R07 | 1406 6 8 12 14 12 29 159 6 | 52 47 47 46 47 67 79 49
R08 | 909 7 14 13 27 16 19 --- 7 | 46 43 43 56 47 41 --- 44
R09 | 3375 36 32 32 27 76 32 --- 19 | 119 121 126 116 107 118 --- 111
XR11 | 2954 13 16 13 23 --- 24 --- 9 | 37 45 37 31 --- 57 --- 37
R12 | 1769 21 34 14 24 19 26 --- 10 | 63 26 41 64 59 50 --- 48
R13 | 1006 37 56 65 44 29 38 --- 20 | 124 98 88 104 122 116 --- 102
R14 | 833 18 18 14 8 14 21 --- 7 | 103 96 94 99 105 103 --- 99
R15 | 831 16 25 16 13 11 29 --- 8 | 53 36 35 45 53 74 --- 47
R16 | 2185 21 28 22 25 22 37 --- 11 | 50 34 43 47 50 65 --- 42
R17E | 580 12 26 15 18 10 34 --- 8 | 49 52 53 55 58 60 --- 53
R18E | 1320 16 33 16 27 24 26 --- 10 | 29 41 27 26 36 41 --- 26
R19E | 941 24 52 35 52 22 46 --- 17 | 31 54 46 60 39 41 --- 32
R20E | 1075 38 52 46 63 30 69 --- 22 | 64 82 88 100 72 62 --- 71
R21E | 1365 15 24 10 15 17 16 300 7 | 50 47 49 45 52 44 93 46
R22E | 1879 48 45 50 76 66 46 --- 25 | 43 29 52 50 63 60 --- 37
R24E | 1471 16 25 14 15 14 14 --- 7 | 35 35 30 35 47 36 --- 33
------+----------------------------------------------+------------------------------------------
RMS | 1557 24 32 28 33 30 34 312 |T 55 54 52 59 58 61 153 51
WRMS | 1557 17 28 20 17 19 34 312 |NE 61 56 54 62 61 66 173 56
MEDI | 1075 18 25 16 23 16 29 159 |MD 49 47 46 50 50 60 79 46
Table 3.2155.3 GPS week: 2155 Day: 3 MJD: 59332
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 | 1182 30 30 30 24 25 29 --- 12 | 71 67 50 54 44 59 --- 55
R02 | 2618 6 14 13 9 10 30 246 6 | 43 41 47 44 40 59 324 43
R03 | 1308 8 12 19 8 11 23 --- 6 | 53 54 44 49 52 69 --- 51
XR04 | 1002 18 24 25 --- 17 40 --- 12 | 51 53 35 --- 38 36 --- 40
R05 | 732 15 20 25 15 14 25 91 8 | 35 39 46 37 34 28 65 33
R07 | 1502 10 17 16 18 19 38 238 8 | 53 52 58 55 46 78 39 54
R08 | 1027 9 15 13 17 10 36 --- 7 | 54 51 53 56 55 64 --- 53
R09 | 4137 29 24 20 24 48 52 --- 14 | 56 49 58 62 24 52 --- 44
XR11 | 2631 14 19 10 19 --- 41 --- 10 | 39 42 33 33 --- 73 --- 39
R12 | 2651 19 32 18 21 20 20 --- 9 | 62 48 45 61 54 52 --- 51
R13 | 647 40 57 53 58 28 40 --- 21 | 102 63 55 109 97 67 --- 76
R14 | 1414 16 17 12 12 14 27 --- 7 | 84 78 80 80 86 79 --- 80
R15 | 1086 12 30 11 16 17 31 228 8 | 58 34 49 61 50 75 88 52
R16 | 2551 17 25 23 41 40 37 --- 13 | 50 50 67 57 69 76 --- 57
R17E | 845 14 25 10 16 14 32 --- 8 | 37 38 35 37 42 46 --- 36
R18E | 759 11 16 9 20 16 18 --- 6 | 33 28 30 27 37 39 --- 30
R19E | 1353 26 49 27 72 45 54 --- 20 | 51 44 36 88 47 35 --- 39
R20E | 2322 27 54 47 54 35 51 --- 19 | 72 76 70 84 80 84 --- 71
R21E | 885 18 27 13 23 12 28 85 9 | 60 52 54 67 56 50 58 54
R22E | 2257 42 34 46 84 81 64 --- 26 | 38 45 59 55 71 56 --- 39
R24E | 1903 12 29 12 21 17 31 --- 9 | 39 29 37 44 44 39 --- 35
------+----------------------------------------------+------------------------------------------
RMS | 1865 22 31 25 36 31 37 192 |T 54 49 49 58 53 57 114 49
WRMS | 1865 17 27 18 16 18 30 192 |NE 57 51 51 58 53 61 129 52
MEDI | 1353 16 25 18 20 17 32 228 |MD 53 49 49 55 47 59 65 51
Table 3.2155.4 GPS week: 2155 Day: 4 MJD: 59333
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 | 946 29 33 27 20 39 32 --- 13 | 60 62 55 59 38 57 --- 52
R02 | 2438 17 12 16 12 20 41 173 9 | 45 46 46 48 58 58 155 47
R03 | 2640 13 13 10 18 19 27 166 7 | 52 55 57 62 56 55 21 55
XR04 | 589 20 --- 19 --- 21 29 --- 12 | 45 --- 40 --- 32 42 --- 38
R05 | 682 19 23 22 21 12 14 107 8 | 34 35 36 36 35 30 39 30
R07 | 3246 14 10 10 16 19 31 310 7 | 49 50 44 45 45 50 77 45
R08 | 2973 16 15 18 12 15 36 --- 8 | 44 48 41 47 53 64 --- 46
R09 | 4858 21 20 20 24 85 56 --- 17 | 105 106 111 107 98 119 --- 101
XR11 | 1990 13 18 10 21 --- 32 --- 9 | 39 37 42 47 --- 46 --- 40
R12 | 1884 18 27 15 10 12 41 --- 9 | 66 50 49 48 63 88 --- 57
R13 | 1583 45 48 51 37 44 40 --- 20 | 111 90 89 90 116 105 --- 95
R14 | 1550 20 17 12 8 20 36 --- 8 | 100 88 94 93 92 103 --- 94
R15 | 864 15 24 17 10 15 21 283 7 | 57 36 41 50 57 63 28 49
R16 | 2729 27 27 23 47 49 48 --- 16 | 43 42 62 54 65 78 --- 51
R17E | 696 14 24 13 18 12 17 --- 7 | 41 44 43 50 45 52 --- 43
R18E | 780 11 23 11 16 22 32 --- 8 | 29 26 30 26 38 38 --- 27
R19E | 1157 19 84 25 43 46 51 --- 20 | 40 61 45 55 46 43 --- 38
R20E | 1409 34 49 56 53 42 51 --- 21 | 68 67 104 102 66 65 --- 74
R21E | 1222 13 24 19 19 27 26 98 9 | 43 35 39 42 43 43 37 37
R22E | 3480 29 38 49 60 83 42 --- 22 | 41 54 77 67 64 51 --- 47
R24E | 1330 12 28 14 23 15 27 --- 9 | 36 30 29 45 40 43 --- 33
------+----------------------------------------------+------------------------------------------
RMS | 2220 22 33 26 29 38 37 206 |T 54 53 55 58 57 61 59 52
WRMS | 2220 19 26 19 16 25 35 206 |NE 60 57 57 60 62 68 64 57
MEDI | 1550 18 24 18 19 20 32 166 |MD 45 48 45 50 53 55 37 47
Table 3.2155.5 GPS week: 2155 Day: 5 MJD: 59334
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 | 731 23 42 35 23 50 30 --- 15 | 45 59 60 62 29 49 --- 45
R02 | 806 11 13 11 13 22 29 220 7 | 37 41 49 45 32 62 55 42
R03 | 2768 12 8 16 11 19 20 183 6 | 43 48 58 54 46 53 11 49
XR04 | 748 15 24 16 --- 23 28 --- 10 | 43 51 41 --- 30 36 --- 37
R05 | 709 16 15 14 16 16 12 164 6 | 32 31 34 34 32 34 20 30
R07 | 2853 8 13 12 13 14 30 353 7 | 41 42 45 35 38 31 112 36
R08 | 3260 9 10 12 17 19 14 --- 6 | 39 38 46 40 49 53 --- 42
R09 | 4828 17 18 22 26 83 40 --- 17 | 109 112 121 123 84 118 --- 106
XR11 | 1808 11 18 10 17 --- 21 --- 7 | 28 31 34 36 --- 36 --- 31
R12 | 1527 19 28 18 28 17 27 --- 10 | 59 39 43 62 55 53 --- 49
R13 | 1888 39 44 51 44 30 34 --- 18 | 68 53 53 74 67 47 --- 53
R14 | 1072 14 22 15 28 14 36 --- 9 | 54 47 55 70 48 35 --- 49
R15 | 815 16 21 16 17 20 18 446 8 | 49 37 36 46 54 40 27 41
R16 | 2177 25 23 24 40 40 31 --- 13 | 47 43 58 61 83 66 --- 55
R17E | 1255 11 21 12 22 19 22 --- 8 | 67 68 70 73 81 75 --- 70
R18E | 1038 10 16 15 13 14 23 --- 7 | 27 20 31 24 37 32 --- 25
R19E | 1081 26 64 28 64 23 42 --- 19 | 53 34 44 76 34 32 --- 37
R20E | 575 43 51 52 61 43 31 --- 21 | 97 115 130 131 94 93 --- 105
R21E | 1016 20 27 16 18 14 15 144 8 | 42 34 34 44 49 34 42 37
R22E | 5151 37 68 45 61 59 23 --- 22 | 34 72 52 40 64 36 --- 31
R24E | 967 12 29 15 34 19 20 --- 9 | 41 37 36 54 44 38 --- 38
------+----------------------------------------------+------------------------------------------
RMS | 2254 22 33 26 33 33 27 275 |T 50 50 53 59 52 50 44 48
WRMS | 2254 16 28 20 21 23 24 275 |NE 49 48 52 57 49 50 45 47
MEDI | 1081 16 22 16 22 19 27 183 |MD 43 42 46 54 48 40 27 42
Table 3.2155.6 GPS week: 2155 Day: 6 MJD: 59335
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 | 710 39 39 36 34 37 29 --- 16 | 71 76 65 67 49 61 --- 61
R02 | 795 18 14 17 8 20 26 295 7 | 50 48 54 54 47 62 95 50
R03 | 2415 10 13 14 11 23 24 223 7 | 61 62 73 72 72 62 22 66
XR04 | 1193 15 17 11 --- 19 31 --- 9 | 62 57 53 --- 50 45 --- 53
R05 | 1039 17 25 14 20 21 30 219 9 | 40 43 60 61 42 66 58 48
R07 | 995 12 14 18 15 13 20 339 7 | 54 60 50 49 57 59 139 52
R08 | 1699 11 14 18 18 17 33 --- 8 | 52 58 59 59 63 56 --- 56
R09 | 3807 17 30 16 15 67 53 --- 15 | 124 137 130 127 88 140 --- 120
XR11 | 2217 15 17 12 23 --- 24 --- 9 | 41 47 51 54 --- 41 --- 45
R12 | 1298 21 29 26 20 19 27 --- 10 | 70 37 47 65 54 69 --- 54
R13 | 1377 46 40 51 34 27 39 --- 18 | 111 74 73 105 94 64 --- 83
R14 | 983 12 22 10 13 12 21 --- 6 | 82 66 68 75 80 71 --- 73
R15 | 600 16 22 14 13 23 37 662 9 | 67 52 49 64 75 47 27 57
R16 | 3196 20 29 31 22 43 28 --- 13 | 74 72 83 75 100 92 --- 78
R17E | 1090 17 22 17 18 22 37 --- 10 | 108 109 106 111 106 120 --- 108
R18E | 1175 12 21 12 14 18 24 --- 7 | 38 37 36 34 39 38 --- 35
R19E | 1569 30 49 31 46 56 40 --- 18 | 39 32 48 60 53 37 --- 37
R20E | 788 51 50 57 61 42 55 --- 24 | 107 102 104 126 131 136 --- 109
R21E | 1022 18 27 21 21 16 33 224 10 | 56 51 50 57 56 62 75 53
R22E | 1414 32 88 35 81 72 47 --- 27 | 46 104 57 53 54 76 --- 50
R24E | 1491 16 29 14 13 20 17 --- 8 | 55 49 58 58 58 60 --- 54
------+----------------------------------------------+------------------------------------------
RMS | 1662 25 35 27 31 35 34 362 |T 67 65 65 71 68 69 69 63
WRMS | 1662 18 25 19 15 28 29 362 |NE 68 63 65 71 67 66 68 64
MEDI | 1193 17 25 17 18 21 30 224 |MD 61 58 58 61 57 62 58 54
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