[IGSREPORT-28067] Wk 2165 IGLOS Final Orbits
acc
acc at igs.org
Fri Jul 23 03:37:27 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2165 (Jul 04, 2021 - Jul 10, 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 2.2165.
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:
igl2165[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2165 in the SP3 format.
igl21657.sum Combination Report for GPS Week 2165.
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 | -3.7 ns
1 | -2.6 ns
2 | -6.6 ns
3 | -4.1 ns
4 | -7.9 ns
5 | -6.1 ns
6 | -6.8 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 1.2165, 1a.2165).
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 2.2165.0-6)
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 3.2165.0-6).
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 2165 summary. (Jul 04, 2021 - Jul 10, 2021)
Table 1.2165.a GPS week : 2165 MJD: 59399.0-59405.0
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 5 9 -20 -25 .14 25 19 | -10241 830 3584 8408
| 1 1 1 14 15 31 .02 | 840 1402
emx n/a| -3 0 -14 24 9 -24 -.13 49 38 | -7343 543 3608 8888
| 1 1 3 31 26 56 .05 | 12446 1074
esx n/a| 0 0 3 30 14 -6 -.11 34 25 | -1243 1260 3582 8733
| 1 1 2 11 23 26 .04 | 6468 1426
gfz n/a| 0 0 6 -15 -2 -13 -.12 24 18 | 0 737 3628 8131
| 2 0 2 14 24 38 .04 | 0 1879
grg n/a| 5 1 -15 -21 17 -92 .40 36 28 | -5796 471 3586 7998
| 1 1 6 12 17 37 .06 | 1645 1742
iac n/a| -1 -1 0 -15 -21 181 -.20 27 26 | -3695 -346 3575 8925
| 1 2 4 28 61 80 .03 | 1610 1785
mcc n/a| 0 -2 3 56 3 -56 -.75 184 184 | --- --- --- ---
| 12 10 16 145 123 631 .55 | --- ---
Table 1.2165.b GPS week : 2165 MJD: 59399.0-59405.0
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 | 18 19 21 18 22 21 23 |
R02 | 7 8 9 9 10 10 9 |
R03 | 7 7 8 8 9 9 8 |
R04 | 15 11 9 11 11 13 11 |
R05 | 9 8 9 8 10 11 13 |
R07 | 8 10 9 8 9 9 13 |
R08 | 8 10 12 8 9 10 9 |
R09 | 12 13 14 11 11 12 12 |
R11 | 8 13 9 11 14 10 11 |
R12 | 7 7 10 12 10 9 9 |
R13 | 17 17 16 16 19 17 17 |
R14 | 8 8 7 8 9 13 11 |
R15 | 8 7 6 8 6 8 8 |
R16 | 13 13 13 13 12 13 14 |
R17 | 8 7 8 8 7 8 9 |
R18 | 10 10 8 8 7 8 11 |
R19 | 23 24 22 27 29 26 25 |
R20 | 26 28 22 23 26 22 22 |
R21 | 8 9 9 8 10 9 7 |
R22 | 24 22 25 25 23 23 28 |
R24 | 11 11 11 10 12 11 11 |
Table 1.2165.c GPS week : 2165 MJD: 59399.0-59405.0
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 2165 0 | -19 30 310 -123 -2273 6336 80.8 1599 1599 | -3707 0
brd 2165 1 | 71 23 182 752 -358 5982 81.9 1715 1715 | -2554 0
brd 2165 2 | 9 71 233 -480 -213 7582 83.9 1971 1971 | -6593 0
brd 2165 3 | 21 -1 248 -1373 -1303 4694 83.2 1640 1640 | -4132 0
brd 2165 4 | 70 -32 236 -380 -487 182 82.6 1382 1382 | -7933 0
brd 2165 5 | -36 -29 319 1363 212 4054 83.7 1189 1189 | -6134 0
brd 2165 6 | 27 -54 289 2199 724 9779 84.2 1439 1439 | -6786 0
-------------+------------------------------------------------------------+----------------
brd 2165 mean| 20 1 259 279 -528 5515 82.9 1562 1562 | -5405 0
brd 2165 sdev| 40 43 48 1223 991 3016 1.2 253 253 | 1952 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 2.2165.0 GPS week: 2165 Day: 0 MJD: 59399
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 3 -17 -30 -78 .15 23 17 | -11071 251 3848 8174
emx n/a| -4 0 -20 21 55 -86 -.12 49 37 | -4202 576 3880 8549
esx n/a| 0 2 1 14 27 -2 -.10 34 26 | 473 106 3849 7658
gfz n/a| 0 0 6 -17 40 -91 -.09 22 19 | 0 -878 3917 8242
grg n/a| 7 0 -15 -25 19 -111 .44 40 28 | -3367 -858 3865 7848
iac n/a| 0 -4 0 25 -18 255 -.18 24 19 | -1892 -262 3858 8619
mcc n/a| -7 2 22 19 -171 1234 -.56 143 143 | --- --- --- ---
Table 2.2165.1 GPS week: 2165 Day: 1 MJD: 59400
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 21 -40 -49 .14 22 18 | -10339 1901 3830 8764
emx n/a| -3 1 -15 26 -22 39 -.11 55 42 | 9211 1259 3841 9208
esx n/a| 0 -1 5 28 -19 -50 -.15 38 25 | -3122 2709 3829 8733
gfz n/a| 0 1 8 -10 0 32 -.13 22 18 | 0 1611 3909 8574
grg n/a| 6 1 -19 -15 19 -86 .40 38 33 | -3897 2495 3802 8226
iac n/a| -1 1 -4 -51 99 131 -.19 23 21 | -977 -324 3816 9313
mcc n/a| -14 -11 -14 -1 153 144 -1.19 188 188 | --- --- --- ---
Table 2.2165.2 GPS week: 2165 Day: 2 MJD: 59401
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 4 5 -10 -25 .11 26 20 | -10888 -165 3732 7714
emx n/a| 0 2 -11 85 -15 50 -.10 54 44 | -632 -193 3741 8174
esx n/a| 0 1 4 25 -6 11 -.14 32 25 | 7995 362 3727 9588
gfz n/a| -4 0 5 -45 0 5 -.17 26 22 | 0 -544 3767 7378
grg n/a| 4 3 -8 -19 18 -77 .34 32 24 | -6091 -1296 3702 7728
iac n/a| -4 0 -3 -14 -32 90 -.18 23 20 | -3926 -1508 3718 8252
mcc n/a| -3 -20 -17 -116 36 -754 -.36 182 182 | --- --- --- ---
Table 2.2165.3 GPS week: 2165 Day: 3 MJD: 59402
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 6 13 3 -22 .14 23 19 | -10081 3170 3144 7624
emx n/a| -5 0 -10 41 2 -26 -.06 52 39 | -21255 2166 3149 8148
esx n/a| -2 1 5 21 -3 23 -.15 34 23 | 4450 2780 3148 7008
gfz n/a| 0 -1 2 -5 13 -16 -.15 22 15 | 0 4137 3128 7129
grg n/a| 6 0 -11 -41 -12 -110 .48 37 26 | -5562 2518 3132 7276
iac n/a| 0 -1 -3 -3 -95 183 -.22 28 28 | -4446 3106 3152 8143
mcc n/a| 8 -3 -6 -89 -153 -399 .11 181 181 | --- --- --- ---
Table 2.2165.4 GPS week: 2165 Day: 4 MJD: 59403
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 7 25 -7 -22 .13 23 21 | -10973 -1123 3499 7428
emx n/a| -4 0 -15 -1 10 -54 -.19 46 33 | -26375 -1244 3590 8063
esx n/a| 0 0 2 37 37 3 -.06 29 23 | -581 -910 3505 9508
gfz n/a| 1 0 7 -6 -23 2 -.07 26 16 | 0 -1354 3539 6975
grg n/a| 7 0 -17 -26 5 -144 .38 40 28 | -7386 -1558 3541 6913
iac n/a| -3 0 -1 -48 -60 220 -.24 29 29 | -4634 -2742 3483 8028
mcc n/a| 16 2 5 119 13 -111 -.64 181 181 | --- --- --- ---
Table 2.2165.5 GPS week: 2165 Day: 5 MJD: 59404
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 8 16 -26 6 .16 29 21 | -9525 766 3784 9907
emx n/a| -2 2 -14 2 15 -4 -.19 46 33 | -650 740 3778 10378
esx n/a| 0 2 3 39 31 0 -.06 35 27 | -10862 1601 3753 11674
gfz n/a| 1 0 7 -13 -32 -2 -.09 20 14 | 0 1128 3843 9523
grg n/a| 4 3 -26 -15 45 -22 .32 32 28 | -6649 570 3833 9148
iac n/a| -1 -4 8 9 1 92 -.21 33 33 | -4852 -115 3752 10407
mcc n/a| 13 1 9 185 29 -275 -1.14 199 199 | --- --- --- ---
Table 2.2165.6 GPS week: 2165 Day: 6 MJD: 59405
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 5 0 -33 13 .12 26 19 | -8811 1011 3256 9250
emx n/a| -4 -1 -13 -6 23 -91 -.17 43 35 | -7504 498 3278 9697
esx n/a| -3 0 0 48 32 -33 -.10 37 26 | -7060 2176 3265 6967
gfz n/a| 2 0 4 -7 -19 -26 -.14 29 18 | 0 1065 3299 9097
grg n/a| 3 2 -10 -2 28 -96 .46 33 30 | -7623 1432 3228 8850
iac n/a| 1 -1 0 -27 -41 295 -.16 32 32 | -5141 -583 3249 9713
mcc n/a| -14 11 23 279 114 -231 -1.47 213 213 | --- --- --- ---
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 3.2165.0 GPS week: 2165 Day: 0 MJD: 59399
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 619 50 54 44 28 52 19 --- 18 | 127 71 83 117 84 96 --- 98
R02M | 1576 8 37 8 10 22 18 150 7 | 80 42 72 81 80 71 161 73
R03M | 664 11 33 9 12 19 14 133 7 | 84 60 77 90 87 72 88 79
XR04 | 864 28 20 21 --- 12 43 --- 14 | 80 67 74 --- 67 59 --- 68
R05 | 780 9 25 22 20 21 20 98 8 | 69 60 87 85 64 57 147 70
R07M | 1043 9 37 20 10 13 22 175 8 | 93 55 69 92 83 97 99 84
R08M | 972 13 35 12 11 27 17 --- 8 | 85 55 77 94 92 94 --- 84
R09M | 2963 23 20 13 22 50 25 --- 11 | 67 77 72 76 45 69 --- 64
XR11M | 2762 17 25 16 11 --- 16 --- 8 | 45 52 49 40 --- 40 --- 40
R12 | 1118 13 26 16 13 17 10 --- 6 | 69 41 73 60 58 65 --- 62
R13M | 2340 37 57 36 32 34 33 --- 16 | 89 47 61 79 56 87 --- 70
R14M | 1220 20 25 10 18 20 18 --- 8 | 64 43 67 64 58 65 --- 60
R15M | 901 6 33 9 20 23 13 109 7 | 69 48 66 75 54 65 77 64
R16M | 1172 30 39 28 23 34 18 --- 12 | 57 59 95 88 84 81 --- 75
R17 | 1620 8 31 10 16 13 22 --- 7 | 31 25 32 30 36 30 --- 27
R18 | 1221 11 28 27 19 34 23 --- 10 | 31 37 26 36 32 27 --- 27
R19 | 1618 41 99 42 29 94 18 --- 23 | 42 53 42 43 53 51 --- 40
R20 | 2866 20 119 71 55 68 30 --- 26 | 58 82 48 59 51 42 --- 49
R21 | 2104 9 41 9 8 18 19 172 7 | 36 34 39 33 37 49 99 36
R22 | 1128 34 27 93 16 50 58 --- 23 | 47 59 44 51 46 62 --- 41
R24 | 1670 17 48 16 10 37 21 --- 10 | 39 41 40 39 41 34 --- 36
------+----------------------------------------------+------------------------------------------
RMS | 1599 23 49 34 22 40 24 143 |T 64 52 61 66 60 62 111 59
WRMS | 1599 17 37 26 19 28 19 143 |NE 50 49 50 48 48 47 123 45
MEDI | 1220 17 33 16 16 23 19 133 |MD 67 53 67 64 56 65 99 64
Table 3.2165.1 GPS week: 2165 Day: 1 MJD: 59400
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 878 43 61 57 32 42 18 --- 18 | 76 44 54 70 59 66 --- 60
R02M | 1183 17 35 13 12 18 15 189 7 | 52 27 44 45 51 40 136 42
R03M | 1841 10 26 10 13 17 21 177 7 | 56 39 54 59 57 47 45 52
XR04 | 592 21 23 13 --- 16 25 --- 10 | 51 39 45 --- 51 36 --- 43
R05 | 627 22 24 22 10 13 17 211 8 | 51 47 69 56 54 64 95 55
R07M | 701 7 33 26 22 22 28 194 10 | 59 40 46 75 57 72 98 61
R08M | 905 11 31 13 13 18 35 --- 9 | 59 38 55 59 61 82 --- 61
R09M | 3901 24 15 25 20 50 31 --- 12 | 60 57 58 60 33 64 --- 52
XR11M | 1681 30 23 17 18 --- 30 --- 12 | 20 24 25 31 --- 41 --- 22
R12 | 1092 22 23 9 14 15 11 --- 7 | 57 44 55 46 49 45 --- 48
R13M | 2289 27 63 42 27 46 31 --- 16 | 53 27 47 70 61 71 --- 55
R14M | 1094 12 31 11 13 21 17 --- 7 | 49 29 47 62 58 44 --- 48
R15M | 1386 13 26 9 14 17 13 87 6 | 49 37 49 44 43 50 65 45
R16M | 1471 24 31 37 24 33 22 --- 12 | 49 48 73 68 48 60 --- 57
R17 | 1477 14 37 8 12 15 16 --- 7 | 26 21 19 22 25 25 --- 20
R18 | 701 14 38 34 11 22 22 --- 10 | 21 27 33 21 21 20 --- 18
R19 | 1004 35 113 53 52 53 32 --- 23 | 26 39 22 24 39 33 --- 20
R20 | 2674 33 137 85 31 75 34 --- 27 | 34 69 45 28 28 28 --- 19
R21 | 2196 10 39 23 13 28 15 237 8 | 22 21 23 24 29 20 137 20
R22 | 1049 29 54 84 24 78 17 --- 21 | 25 39 32 34 45 28 --- 21
R24 | 2220 9 64 19 10 30 20 --- 10 | 27 37 24 24 30 34 --- 25
------+----------------------------------------------+------------------------------------------
RMS | 1715 22 55 38 22 38 23 188 |T 43 37 43 46 44 46 96 40
WRMS | 1715 18 42 25 18 33 21 188 |NE 34 38 36 31 37 33 116 28
MEDI | 1183 21 33 22 14 22 21 189 |MD 49 39 46 45 48 44 95 45
Table 3.2165.2 GPS week: 2165 Day: 2 MJD: 59401
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 703 52 56 55 49 35 30 --- 20 | 95 54 60 99 65 56 --- 68
R02M | 2249 14 36 12 17 25 14 151 8 | 65 53 63 64 82 56 70 62
R03M | 2426 15 27 16 16 17 15 209 7 | 71 61 72 74 67 62 45 67
XR04 | 733 14 27 13 --- 22 13 --- 8 | 68 61 70 --- 80 75 --- 69
R05 | 639 12 35 22 16 15 17 194 8 | 56 51 66 61 63 47 69 55
R07M | 782 15 32 15 22 30 15 174 9 | 82 65 75 94 70 84 73 79
R08M | 2030 20 38 19 15 25 37 --- 11 | 75 60 71 94 84 95 --- 81
R09M | 3441 16 17 42 22 48 26 --- 14 | 67 70 77 77 68 72 --- 67
XR11M | 895 14 23 18 14 --- 19 --- 8 | 48 55 52 58 --- 42 --- 49
R12 | 1039 17 46 19 15 13 21 --- 9 | 71 47 64 55 66 61 --- 60
R13M | 3124 32 52 22 44 41 27 --- 16 | 76 55 60 59 69 67 --- 61
R14M | 1034 9 27 16 12 19 16 --- 7 | 61 59 74 63 71 63 --- 64
R15M | 1518 12 26 8 15 15 9 79 6 | 70 56 66 62 74 65 45 65
R16M | 1396 20 37 35 24 40 22 --- 13 | 55 52 77 68 56 59 --- 59
R17 | 1261 15 32 14 14 10 18 --- 7 | 53 52 44 54 51 48 --- 49
R18 | 538 10 26 24 21 11 11 --- 7 | 48 43 49 52 52 42 --- 46
R19 | 3205 49 104 54 32 31 36 --- 21 | 48 63 41 50 32 48 --- 45
R20 | 2815 45 109 52 33 46 31 --- 22 | 54 85 54 51 47 47 --- 48
R21 | 1752 19 28 13 18 15 22 240 8 | 44 42 49 43 46 50 100 44
R22 | 1376 35 91 66 50 76 26 --- 24 | 51 94 51 66 46 59 --- 51
R24 | 2047 16 69 17 8 12 23 --- 10 | 53 51 54 48 58 41 --- 48
------+----------------------------------------------+------------------------------------------
RMS | 1971 26 54 32 26 32 23 182 |T 62 58 61 64 62 59 67 58
WRMS | 1971 20 44 25 22 24 20 182 |NE 54 58 54 53 54 51 84 51
MEDI | 1396 16 35 19 17 22 21 174 |MD 61 55 63 61 65 59 69 60
Table 3.2165.3 GPS week: 2165 Day: 3 MJD: 59402
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 1175 38 54 57 32 27 20 --- 17 | 93 47 42 89 77 73 --- 72
R02M | 2774 19 31 10 6 29 21 109 8 | 65 39 55 50 50 63 71 53
R03M | 2040 10 37 16 17 15 19 223 8 | 64 37 61 71 63 51 35 59
XR04 | 1425 21 23 17 --- 31 21 --- 11 | 50 28 48 --- 33 41 --- 38
R05 | 512 12 24 20 15 21 23 186 8 | 48 38 54 43 57 37 75 44
R07M | 796 9 31 18 16 14 25 173 8 | 74 48 58 77 76 69 62 68
R08M | 897 13 34 8 12 19 25 --- 8 | 68 43 70 68 68 83 --- 68
R09M | 2589 15 12 27 16 49 23 --- 11 | 57 59 61 64 27 74 --- 55
XR11M | 1238 20 26 8 26 --- 20 --- 10 | 30 31 28 33 --- 24 --- 23
R12 | 582 13 53 10 12 25 40 --- 11 | 60 26 51 51 46 89 --- 53
R13M | 2405 40 49 33 36 30 28 --- 16 | 77 35 42 64 53 57 --- 53
R14M | 737 10 20 25 11 25 19 --- 8 | 49 39 68 45 66 38 --- 49
R15M | 1194 12 19 12 8 24 30 81 8 | 61 42 55 54 65 47 37 53
R16M | 1147 36 37 23 24 22 30 --- 13 | 42 51 71 62 68 78 --- 59
R17 | 1514 9 30 13 11 18 23 --- 7 | 20 15 21 22 27 20 --- 18
R18 | 525 18 33 20 11 19 16 --- 8 | 20 22 19 18 24 24 --- 16
R19 | 3318 33 135 54 36 78 41 --- 26 | 27 62 39 42 36 32 --- 32
R20 | 1157 31 87 66 38 61 41 --- 23 | 44 69 50 57 47 32 --- 44
R21 | 1221 21 21 12 11 20 17 253 7 | 33 36 33 41 43 40 60 36
R22 | 1732 36 67 81 41 77 39 --- 25 | 48 56 53 54 51 28 --- 37
R24 | 801 17 55 16 8 20 24 --- 10 | 24 23 24 26 31 34 --- 22
------+----------------------------------------------+------------------------------------------
RMS | 1640 23 52 34 22 37 28 181 |T 50 40 47 51 50 49 56 45
WRMS | 1640 19 39 23 15 26 28 181 |NE 37 37 39 39 39 37 67 34
MEDI | 1194 18 33 18 15 24 23 173 |MD 49 39 51 51 50 41 60 49
Table 3.2165.4 GPS week: 2165 Day: 4 MJD: 59403
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 1679 56 44 57 49 47 31 --- 22 | 86 48 35 81 55 47 --- 55
R02M | 1909 14 30 13 23 25 26 105 9 | 56 40 47 70 46 72 98 54
R03M | 1721 10 30 18 21 12 22 226 8 | 61 40 44 72 55 62 59 56
XR04 | 1073 25 21 12 --- 22 23 --- 10 | 56 36 48 --- 47 37 --- 44
R05 | 708 16 31 20 18 23 24 178 9 | 51 28 59 54 37 42 51 45
R07M | 1352 11 36 19 19 14 24 195 9 | 71 40 54 76 62 72 90 63
R08M | 518 13 32 12 13 23 24 --- 8 | 72 49 69 66 89 80 --- 69
R09M | 2120 11 17 21 16 57 17 --- 11 | 66 78 67 70 63 72 --- 64
XR11M | 1437 18 19 24 13 --- 54 --- 14 | 27 28 33 26 --- 41 --- 22
R12 | 542 11 27 13 23 22 36 --- 10 | 49 32 52 40 41 69 --- 45
R13M | 1234 33 58 31 30 68 42 --- 18 | 75 46 53 74 37 92 --- 61
R14M | 1129 13 20 22 18 17 27 --- 9 | 46 34 60 38 53 49 --- 46
R15M | 941 13 18 13 13 11 16 98 6 | 55 36 49 47 50 43 60 47
R16M | 988 30 24 20 22 35 24 --- 11 | 47 46 70 72 68 76 --- 61
R17 | 879 8 30 12 12 14 22 --- 7 | 26 21 23 26 28 29 --- 23
R18 | 865 11 20 18 12 14 23 --- 7 | 19 20 21 27 26 17 --- 18
R19 | 2731 39 138 50 28 96 35 --- 28 | 31 36 27 20 49 34 --- 20
XR20 | 1020 36 --- 78 55 43 28 --- 26 | 30 --- 35 51 32 37 --- 33
R21 | 550 10 34 12 19 17 33 236 9 | 25 23 31 28 30 43 51 27
R22 | 1645 32 27 71 58 64 39 --- 23 | 52 68 38 51 50 30 --- 38
R24 | 950 18 53 21 12 31 32 --- 12 | 23 21 27 16 31 29 --- 19
------+----------------------------------------------+------------------------------------------
RMS | 1382 23 46 29 26 40 29 181 |T 48 38 44 50 47 51 68 43
WRMS | 1382 21 33 23 16 28 29 181 |NE 36 31 36 34 37 36 51 31
MEDI | 1073 14 30 20 19 23 26 178 |MD 51 36 47 51 47 43 59 45
Table 3.2165.5 GPS week: 2165 Day: 5 MJD: 59404
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 2100 70 47 58 29 33 24 --- 21 | 91 33 35 60 47 55 --- 49
R02M | 1439 16 31 14 21 17 29 90 9 | 55 31 40 62 41 49 62 47
R03M | 1586 7 32 16 22 16 18 179 8 | 50 31 40 67 48 55 29 49
XR04 | 1302 27 21 12 --- 21 37 --- 12 | 57 41 44 --- 46 63 --- 47
R05 | 1346 18 42 21 18 22 28 143 10 | 49 27 61 57 40 52 68 45
R07M | 1178 11 32 15 13 14 30 280 8 | 61 42 50 57 62 78 59 57
R08M | 468 10 35 22 18 25 26 --- 10 | 64 45 56 76 69 60 --- 62
R09M | 1494 20 20 27 19 40 34 --- 12 | 70 66 64 66 33 77 --- 59
XR11M | 2551 19 23 12 16 --- 30 --- 10 | 26 27 22 22 --- 22 --- 19
R12 | 486 11 32 20 13 16 34 --- 9 | 46 31 51 52 43 40 --- 42
R13M | 857 42 43 35 30 43 36 --- 17 | 74 49 32 59 38 77 --- 52
R14M | 906 18 32 17 13 20 65 --- 13 | 46 34 61 49 43 105 --- 53
R15M | 824 12 21 15 14 22 28 151 8 | 52 35 49 46 42 59 67 45
R16M | 1410 21 21 43 21 34 28 --- 13 | 38 46 68 41 43 51 --- 43
R17 | 831 8 34 17 9 11 28 --- 8 | 21 22 26 21 26 19 --- 19
R18 | 884 15 22 25 9 16 22 --- 8 | 23 21 18 23 25 36 --- 21
R19 | 1418 46 130 48 23 53 41 --- 25 | 30 44 21 30 28 39 --- 20
R20 | 1195 64 60 62 33 41 32 --- 22 | 29 49 46 48 37 37 --- 31
R21 | 690 9 36 14 10 23 22 275 8 | 35 31 30 35 46 33 152 33
R22 | 1090 30 38 82 33 62 50 --- 22 | 43 54 40 43 42 41 --- 36
R24 | 1077 12 41 15 11 41 24 --- 11 | 26 26 34 33 35 37 --- 27
------+----------------------------------------------+------------------------------------------
RMS | 1189 29 46 35 20 32 33 199 |T 46 37 42 47 41 51 72 40
WRMS | 1189 21 33 27 14 28 33 199 |NE 35 34 37 38 36 39 110 32
MEDI | 1178 18 32 20 18 22 29 151 |MD 46 34 40 48 42 51 62 45
Table 3.2165.6 GPS week: 2165 Day: 6 MJD: 59405
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 1929 57 57 71 49 32 28 --- 23 | 101 32 47 86 70 66 --- 64
R02M | 2081 13 31 13 14 16 32 102 9 | 68 39 56 67 57 66 88 60
R03M | 1581 15 24 8 10 20 21 288 7 | 71 46 63 71 63 62 37 63
XR04 | 1154 22 24 11 --- 21 25 --- 10 | 72 48 61 --- 60 67 --- 61
R05 | 1593 18 36 19 29 21 45 137 12 | 61 28 68 77 49 61 76 56
R07M | 1072 13 40 21 23 16 50 340 12 | 76 44 61 82 70 85 91 70
R08M | 557 11 28 15 20 22 22 --- 8 | 72 48 70 79 69 83 --- 71
R09M | 1409 17 22 16 17 46 25 --- 11 | 63 71 62 67 38 66 --- 57
XR11M | 2965 17 23 22 14 --- 31 --- 10 | 122 122 123 123 --- 121 --- 121
R12 | 467 8 33 16 18 25 24 --- 9 | 63 41 69 72 72 49 --- 61
R13M | 729 43 39 27 34 51 22 --- 16 | 98 46 61 85 51 77 --- 70
R14M | 781 14 25 22 14 21 45 --- 11 | 70 56 87 65 62 95 --- 72
R15M | 827 17 21 9 12 13 26 115 7 | 87 73 81 77 77 84 77 80
R16M | 2108 20 25 26 31 21 49 --- 13 | 77 67 97 78 81 108 --- 83
R17 | 1260 19 22 11 12 21 25 --- 8 | 31 30 30 34 50 39 --- 32
R18 | 1270 17 32 22 15 18 39 --- 11 | 30 30 26 28 29 36 --- 27
R19 | 2698 43 107 48 36 64 22 --- 24 | 31 36 36 40 27 32 --- 26
R20 | 865 45 58 74 33 32 39 --- 21 | 33 40 54 50 41 42 --- 37
R21 | 556 8 28 12 10 16 17 178 7 | 39 31 37 42 41 41 176 38
R22 | 1941 22 51 96 72 67 25 --- 27 | 40 64 58 66 46 44 --- 43
R24 | 983 15 44 17 15 24 23 --- 10 | 38 40 46 47 44 44 --- 41
------+----------------------------------------------+------------------------------------------
RMS | 1438 26 43 37 29 33 32 213 |T 63 49 61 66 54 65 90 58
WRMS | 1438 19 35 26 18 30 32 213 |NE 43 38 48 50 45 45 126 42
MEDI | 1260 17 31 19 17 21 25 137 |MD 68 44 61 67 51 66 77 61
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