[IGSREPORT-27956] Wk 2157 IGLOS Final Orbits
acc
acc at igs.org
Fri May 28 01:41:02 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2157 (May 09, 2021 - May 15, 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 2.2157.
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:
igl2157[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2157 in the SP3 format.
igl21577.sum Combination Report for GPS Week 2157.
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 | -3.5 ns
1 | -5.0 ns
2 | -3.8 ns
3 | -4.2 ns
4 | -4.0 ns
5 | 4.6 ns
6 | 1.4 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 1.2157, 1a.2157).
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 2.2157.0-6)
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 3.2157.0-6).
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 2157 summary. (May 09, 2021 - May 15, 2021)
Table 1.2157.a GPS week : 2157 MJD: 59343.0-59349.0
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 14 -23 -15 .24 29 22 | 888 3590 3298 8317
| 1 0 1 12 19 27 .09 | 12226 3781
emx n/a| -1 2 13 11 -13 -16 -.04 35 26 | -1713 2417 3292 8716
| 1 0 2 22 22 31 .09 | 6424 2259
esx n/a| 0 0 3 18 0 -51 -.07 32 22 | 3504 4108 3284 9763
| 1 2 1 10 20 25 .05 | 5877 4149
gfz n/a| 1 0 -1 -10 -11 -57 -.12 37 19 | 0 3480 3321 8048
| 1 1 1 24 20 34 .15 | 0 3652
grg n/a| 0 0 -8 -25 45 -12 .29 31 22 | -4016 3531 3322 7831
| 1 2 4 20 11 54 .04 | 2877 3553
iac n/a| -2 -4 -4 -5 -12 162 -.28 29 27 | 522 -597 3293 8763
| 2 1 2 40 58 72 .15 | 4138 1565
mcc n/a| 2 3 -6 80 -118 635 -.21 222 222 | --- --- --- ---
| 13 17 17 120 149 971 .41 | --- ---
Table 1.2157.b GPS week : 2157 MJD: 59343.0-59349.0
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 20 12 13 16 15 |
R02 | 7 6 7 8 7 6 7 |
R03 | 6 8 8 7 7 7 6 |
R04 | 7 8 12 12 11 10 8 |
R05 | 8 9 12 10 12 10 8 |
R07 | 5 6 7 7 8 9 7 |
R08 | 8 8 8 8 8 9 11 |
R09 | 16 12 16 18 16 14 10 |
R11 | 11 13 10 11 10 9 7 |
R12 | 9 10 13 13 9 11 8 |
R13 | 14 16 19 18 16 16 21 |
R14 | 7 9 11 9 8 8 7 |
R15 | 9 10 10 14 9 11 8 |
R16 | 13 14 12 12 12 13 14 |
R17 | 8 10 8 9 10 9 9 |
R18 | 10 8 7 7 8 8 8 |
R19 | 29 28 21 22 26 27 26 |
R20 | 23 25 28 28 26 24 31 |
R21 | 12 11 9 10 10 10 8 |
R22 | 25 28 29 31 32 25 15 |
R24 | 11 10 11 11 10 10 12 |
Table 1.2157.c GPS week : 2157 MJD: 59343.0-59349.0
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 2157 0 | 28 27 150 -1277 -105 -237 82.7 1580 1580 | -3490 0
brd 2157 1 | -24 108 194 668 707 3698 83.1 1544 1544 | -5012 0
brd 2157 2 | -4 17 113 -843 -1115 4099 81.2 1685 1685 | -3815 0
brd 2157 3 | 22 -4 39 312 -287 5417 84.1 1839 1839 | -4196 0
brd 2157 4 | -22 56 115 2427 -535 4377 84.8 1699 1699 | -4013 0
brd 2157 5 | -31 25 121 995 -1250 5543 84.8 1661 1661 | 4598 0
brd 2157 6 | 9 26 101 -425 -2323 4441 85.2 8530 8530 | 1445 0
-------------+------------------------------------------------------------+----------------
brd 2157 mean| -3 36 119 265 -701 3905 83.7 2648 2648 | -2069 0
brd 2157 sdev| 23 36 47 1255 969 1946 1.4 2595 2595 | 3624 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 2.2157.0 GPS week: 2157 Day: 0 MJD: 59343
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 7 -16 0 .28 34 25 | -8176 1886 3443 9146
emx n/a| -2 2 17 -3 -14 -15 -.01 34 24 | -9334 823 3398 9450
esx n/a| 0 -1 3 4 -16 -16 -.05 29 18 | 1079 2194 3379 10907
gfz n/a| 0 0 -1 -10 18 -49 -.14 35 16 | 0 1642 3420 8857
grg n/a| 1 0 -11 -27 55 -68 .33 35 23 | -4601 1826 3415 8470
iac n/a| 0 -3 -2 -1 -56 101 -.07 22 20 | -1488 986 3380 9468
mcc n/a| 13 -12 -18 108 -110 -483 -.05 245 245 | --- --- --- ---
Table 2.2157.1 GPS week: 2157 Day: 1 MJD: 59344
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 0 -12 0 .34 30 22 | -7937 -1083 3072 8535
emx n/a| -2 2 17 -5 35 -30 -.04 32 25 | -2278 -302 3078 8850
esx n/a| 0 -1 3 22 32 -61 -.12 32 22 | 8562 -1440 3068 10185
gfz n/a| 1 0 0 -3 11 -75 -.13 38 18 | 0 -1558 3093 8184
grg n/a| 2 3 -14 -33 48 87 .27 34 26 | -4879 -956 3122 7729
iac n/a| -3 -3 -7 14 -92 64 -.19 26 21 | -2089 -1893 3072 8980
mcc n/a| -11 13 6 25 -150 623 -.37 150 150 | --- --- --- ---
Table 2.2157.2 GPS week: 2157 Day: 2 MJD: 59345
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 0 27 -19 -8 .37 32 25 | -6590 1540 3438 8194
emx n/a| -2 1 11 18 -27 0 .07 35 27 | -11013 1636 3425 8529
esx n/a| 1 0 5 21 -1 -83 -.01 34 23 | 8221 2369 3412 10322
gfz n/a| 4 0 1 7 -8 -113 -.31 41 18 | 0 2246 3466 7937
grg n/a| 0 1 -12 -1 41 -1 .26 27 20 | -4563 1469 3409 7407
iac n/a| -3 -5 0 -69 -13 218 -.53 33 31 | -1660 -191 3430 8636
mcc n/a| -2 -3 3 29 -14 1245 .12 229 229 | --- --- --- ---
Table 2.2157.3 GPS week: 2157 Day: 3 MJD: 59346
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 32 3 -6 .21 26 19 | -5607 3596 3327 8762
emx n/a| 0 3 12 32 -30 -36 .01 38 28 | 1297 2956 3351 9220
esx n/a| -1 0 4 8 -27 -52 -.09 37 27 | -7108 4223 3348 10540
gfz n/a| 1 0 -3 -63 -19 -59 -.25 39 19 | 0 3009 3341 8607
grg n/a| -1 0 -4 0 37 -31 .24 28 21 | -5975 3314 3380 8322
iac n/a| -3 -3 -3 -15 18 178 -.32 32 32 | -2217 -166 3346 9237
mcc n/a| 23 4 -19 -68 9 1761 .09 223 223 | --- --- --- ---
Table 2.2157.4 GPS week: 2157 Day: 4 MJD: 59347
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 0 23 -43 -41 .19 28 23 | -1998 7949 3674 8723
emx n/a| 0 2 13 -23 -14 36 -.15 37 26 | 5873 5150 3669 9167
esx n/a| 0 2 2 10 7 -47 -.14 36 22 | 2904 8974 3659 8109
gfz n/a| 0 3 -2 -9 -18 -70 -.09 35 19 | 0 7332 3733 8412
grg n/a| 0 -3 -3 -31 57 -13 .31 30 20 | -7812 7053 3698 8687
iac n/a| -2 -5 -7 61 -8 157 -.24 31 27 | -1918 708 3666 9199
mcc n/a| -15 35 20 200 -337 1590 .23 263 263 | --- --- --- ---
Table 2.2157.5 GPS week: 2157 Day: 5 MJD: 59348
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 2 -20 -66 .13 29 20 | 14609 9469 3078 7636
emx n/a| 0 3 11 37 -19 -6 -.16 37 26 | -765 5639 3068 8082
esx n/a| 0 3 3 29 18 -20 -.04 29 20 | 9506 10297 3074 9150
gfz n/a| 0 2 -2 11 -19 -9 .14 31 21 | 0 9274 3087 7430
grg n/a| 1 -2 -5 -22 54 16 .33 33 23 | -284 9454 3157 7270
iac n/a| 0 -4 -5 -34 -28 134 -.20 29 28 | 7489 -154 3093 8168
mcc n/a| 0 2 -13 -4 -282 -714 -.68 264 264 | --- --- --- ---
Table 2.2157.6 GPS week: 2157 Day: 6 MJD: 59349
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 -3 10 -54 13 .14 25 19 | 21917 1779 3060 7228
emx n/a| -2 3 10 21 -23 -63 .03 34 23 | 4227 1021 3057 7715
esx n/a| 1 1 2 30 -7 -75 -.02 27 21 | 1369 2145 3054 9131
gfz n/a| 0 0 0 -9 -42 -25 -.04 40 22 | 0 2420 3112 6909
grg n/a| 2 0 -6 -59 25 -72 .28 30 19 | -3 2559 3075 6933
iac n/a| -7 -6 -3 3 93 280 -.38 31 31 | 5537 -3473 3069 7659
mcc n/a| 9 -14 -27 272 56 429 -.81 181 181 | --- --- --- ---
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 3.2157.0 GPS week: 2157 Day: 0 MJD: 59343
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 | 1288 44 40 38 27 43 30 --- 16 | 38 48 56 49 41 47 --- 41
R02 | 1022 14 17 16 15 11 17 345 7 | 25 27 31 31 27 40 289 26
R03 | 553 6 9 11 9 22 13 91 5 | 24 26 28 30 27 24 88 24
XR04 | 709 11 9 21 --- 13 11 --- 7 | 22 21 23 --- 26 24 --- 20
R05M | 1310 20 23 21 13 18 14 125 8 | 115 117 128 125 125 124 149 122
R07M | 779 9 11 10 11 12 10 433 4 | 20 19 22 18 22 26 368 18
R08 | 945 16 15 9 15 21 25 --- 8 | 27 26 33 35 30 31 --- 28
R09E | 4416 27 21 21 19 78 25 --- 16 | 110 99 109 109 47 114 --- 96
XR11E | 1990 --- 22 12 17 --- 24 --- 11 | --- 73 70 65 --- 66 --- 68
R12E | 1406 21 22 14 15 21 21 --- 8 | 97 93 95 98 95 92 --- 94
R13E | 1709 47 32 23 31 26 25 --- 14 | 135 127 130 135 132 121 --- 127
R14E | 1337 12 23 12 14 19 16 --- 7 | 86 77 91 90 84 89 --- 86
R15E | 1311 26 21 14 10 25 20 104 8 | 227 231 217 221 211 216 224 220
R16E | 688 26 27 25 20 52 15 --- 12 | 69 61 73 71 84 64 --- 66
R17M | 1725 27 23 12 18 18 12 --- 8 | 61 37 36 55 45 44 --- 44
R18M | 1024 20 16 23 12 24 25 --- 9 | 57 34 48 38 53 38 --- 41
R19M | 1080 38 74 49 112 63 28 --- 29 | 57 58 79 118 77 67 --- 64
R20M | 1245 76 52 69 39 24 27 --- 22 | 89 49 53 74 74 62 --- 55
R21M | 695 37 27 16 22 19 29 139 11 | 87 67 61 79 84 67 105 71
R22M | 945 59 66 53 68 55 32 --- 24 | 40 91 115 70 88 85 --- 76
R24M | 2165 26 37 18 15 25 23 --- 11 | 59 31 38 51 45 59 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 1579 34 34 29 35 35 22 245 |T 72 67 73 78 70 71 203 68
WRMS | 1579 25 24 18 16 23 20 245 |NE 27 29 34 36 30 33 188 27
MEDI | 1245 26 23 18 15 22 23 125 |MD 59 58 61 70 53 64 149 64
Table 3.2157.1 GPS week: 2157 Day: 1 MJD: 59344
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 | 829 48 30 36 29 31 30 --- 15 | 27 21 48 37 36 37 --- 28
R02 | 1469 9 8 15 10 13 21 --- 6 | 27 22 26 26 21 31 --- 23
R03 | 911 11 11 9 11 21 27 109 7 | 24 20 19 18 19 30 84 18
XR04 | 813 16 13 18 --- 12 20 --- 8 | 24 21 25 --- 23 23 --- 20
R05M | 1394 23 20 27 23 10 18 81 9 | 90 93 109 102 87 100 115 95
R07M | 1104 7 10 15 12 13 17 219 5 | 24 22 20 21 22 16 277 17
R08 | 684 20 15 15 14 15 21 --- 7 | 25 20 37 35 30 29 --- 27
R09E | 4146 20 22 14 26 46 25 --- 12 | 118 122 113 121 94 127 --- 113
XR11E | 2076 29 24 12 17 --- 33 --- 12 | 44 83 89 89 --- 82 --- 83
R12E | 1511 19 28 16 18 27 18 --- 9 | 97 95 88 94 99 105 --- 95
R13E | 2132 41 38 36 33 37 27 --- 16 | 141 128 139 141 145 136 --- 135
R14E | 1156 10 28 13 20 26 19 --- 9 | 90 84 93 91 93 92 --- 88
R15E | 1166 21 25 16 17 32 16 172 9 | 215 215 207 208 199 210 184 209
R16E | 661 20 27 18 39 50 20 --- 13 | 81 74 81 83 93 77 --- 78
R17M | 1444 21 21 16 30 19 23 --- 9 | 45 38 39 55 46 42 --- 41
R18M | 665 12 22 17 13 23 13 --- 7 | 35 36 35 31 36 40 --- 32
R19M | 977 36 76 55 97 64 37 --- 28 | 49 54 89 92 74 54 --- 58
R20M | 792 58 56 79 51 29 41 --- 24 | 65 53 65 71 61 60 --- 55
R21M | 698 27 29 20 14 20 28 126 10 | 77 79 72 76 87 65 34 74
R22M | 1930 58 38 58 88 76 48 --- 27 | 54 89 102 86 75 83 --- 74
R24M | 1576 19 34 18 22 13 18 --- 9 | 46 39 36 45 47 48 --- 41
------+----------------------------------------------+------------------------------------------
RMS | 1543 30 32 32 38 34 26 150 |T 66 67 72 76 69 70 138 66
WRMS | 1543 22 25 22 18 26 21 150 |NE 25 20 31 29 25 30 84 23
MEDI | 1156 20 25 17 20 23 21 126 |MD 49 54 72 76 61 60 115 58
Table 3.2157.2 GPS week: 2157 Day: 2 MJD: 59345
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 | 1035 49 29 52 47 37 50 --- 20 | 25 22 52 47 26 44 --- 24
R02 | 2321 8 9 15 19 8 22 461 6 | 22 19 24 22 21 28 301 18
R03 | 1728 6 9 14 19 13 32 136 7 | 22 25 28 34 16 38 101 22
XR04 | 798 23 24 13 --- 19 34 --- 11 | 19 15 25 --- 21 39 --- 15
R05M | 1361 27 22 27 34 8 33 69 11 | 113 115 110 126 114 128 138 114
R07M | 1317 13 12 18 15 11 20 102 6 | 21 19 25 24 21 28 201 17
R08 | 963 16 12 19 22 13 25 --- 8 | 24 17 35 34 22 38 --- 23
R09E | 3237 29 36 27 37 35 44 --- 15 | 109 98 109 118 105 115 --- 105
XR11E | 2152 26 15 15 20 --- 23 --- 10 | 80 101 100 110 --- 98 --- 100
R12E | 1605 14 33 24 25 32 38 --- 13 | 112 105 103 115 126 101 --- 108
R13E | 1732 46 56 29 54 32 40 --- 19 | 162 161 152 165 170 144 --- 156
R14E | 905 16 29 16 14 27 36 --- 11 | 71 67 64 66 86 67 --- 68
R15E | 1301 21 25 12 16 21 34 197 10 | 191 188 196 198 199 202 107 195
R16E | 1055 18 23 31 32 26 28 --- 12 | 45 42 44 41 52 47 --- 41
R17M | 1276 24 21 18 12 14 18 --- 8 | 49 39 34 38 44 41 --- 39
R18M | 571 12 18 14 12 14 16 --- 6 | 38 33 35 33 38 38 --- 34
R19M | 1652 40 67 44 52 39 29 --- 21 | 54 80 57 56 53 59 --- 48
R20M | 588 63 78 76 70 36 41 --- 27 | 81 77 72 83 72 67 --- 63
R21M | 946 26 24 20 16 13 19 172 9 | 66 53 48 54 65 59 70 56
R22M | 3430 59 38 68 111 58 38 --- 29 | 40 74 95 67 74 77 --- 61
R24M | 1609 32 29 18 10 14 30 --- 10 | 58 37 35 46 57 51 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 1685 32 35 34 41 27 33 229 |T 66 66 68 73 69 71 153 64
WRMS | 1685 25 27 23 18 20 31 229 |NE 22 19 32 34 21 37 201 20
MEDI | 1317 24 24 19 20 19 32 136 |MD 54 53 52 54 53 59 107 48
Table 3.2157.3 GPS week: 2157 Day: 3 MJD: 59346
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 | 2398 26 19 33 23 31 16 --- 11 | 40 39 51 48 40 44 --- 38
R02 | 2851 7 11 22 11 15 34 388 8 | 36 41 34 43 40 54 251 39
R03 | 1317 9 11 11 18 14 21 140 6 | 39 42 44 37 35 47 92 38
XR04 | 690 21 26 16 --- 26 24 --- 11 | 38 39 40 --- 41 46 --- 37
R05M | 1036 22 22 20 32 13 20 92 10 | 56 56 45 51 54 47 101 47
R07M | 1242 14 12 11 17 13 18 147 6 | 37 33 32 31 32 36 159 31
R08 | 1210 9 9 18 18 19 24 --- 7 | 36 33 40 37 29 45 --- 32
R09E | 3395 33 40 28 31 42 59 --- 18 | 105 121 98 92 103 104 --- 97
XR11E | 1932 19 21 21 18 --- 25 --- 10 | 49 57 65 64 --- 67 --- 58
R12E | 1615 21 29 23 22 26 44 --- 12 | 124 115 113 120 106 144 --- 118
R13E | 942 33 48 41 45 31 46 --- 18 | 122 113 129 123 117 117 --- 116
R14E | 682 11 24 21 15 19 21 --- 8 | 79 75 82 78 79 78 --- 77
R15E | 1401 16 48 15 22 15 52 273 13 | 216 222 220 211 209 214 96 214
R16E | 1189 19 27 22 36 23 29 --- 11 | 42 48 44 55 56 49 --- 42
R17M | 1421 17 30 23 18 13 17 --- 9 | 109 100 95 111 111 111 --- 105
R18M | 804 13 14 17 11 20 15 --- 7 | 53 48 50 52 56 45 --- 50
R19M | 1587 32 77 56 58 40 27 --- 22 | 56 57 70 75 78 58 --- 55
R20M | 824 63 75 90 66 33 32 --- 28 | 85 97 92 100 68 59 --- 70
R21M | 1262 25 25 19 12 22 19 151 9 | 67 56 48 58 68 44 76 55
R22M | 4195 41 54 78 109 67 47 --- 30 | 61 95 114 71 83 82 --- 72
R24M | 764 22 35 23 25 20 23 --- 11 | 104 92 99 100 91 93 --- 95
------+----------------------------------------------+------------------------------------------
RMS | 1838 26 38 37 39 28 32 223 |T 74 75 76 77 74 75 129 70
WRMS | 1838 19 28 27 19 21 32 223 |NE 37 38 41 41 37 47 171 36
MEDI | 1262 21 26 22 22 20 24 147 |MD 56 57 65 64 68 58 96 55
Table 3.2157.4 GPS week: 2157 Day: 4 MJD: 59347
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 | 1483 32 28 30 27 31 27 --- 13 | 36 34 45 44 30 28 --- 31
R02 | 1865 8 15 16 14 13 21 --- 6 | 23 19 23 28 20 25 --- 20
R03 | 1036 10 12 15 10 12 27 185 7 | 24 23 23 29 24 46 139 25
XR04 | 913 17 23 21 --- 18 25 --- 10 | 23 26 30 --- 25 32 --- 23
R05M | 794 21 27 28 22 24 39 207 12 | 118 121 116 114 122 131 305 118
R07M | 774 11 11 14 19 17 29 277 8 | 19 21 22 21 25 34 251 19
R08 | 1997 9 9 14 18 22 20 --- 7 | 22 19 23 30 20 29 --- 20
R09E | 4042 38 41 22 28 33 41 --- 15 | 85 86 74 83 77 78 --- 74
XR11E | 2561 16 21 12 11 --- 33 --- 10 | 43 47 47 45 --- 44 --- 40
R12E | 1267 23 26 17 25 17 13 --- 9 | 83 77 78 82 84 75 --- 79
R13E | 1197 28 31 38 41 31 37 --- 15 | 70 66 85 79 65 73 --- 67
R14E | 585 15 22 20 18 16 16 --- 8 | 66 68 80 75 71 62 --- 69
R15E | 1764 12 30 15 22 15 22 322 9 | 149 148 152 162 145 172 86 154
R16E | 933 21 29 22 29 25 25 --- 11 | 43 39 47 45 46 47 --- 39
R17M | 1797 16 30 23 19 13 27 --- 9 | 151 142 152 158 155 143 --- 150
R18M | 1735 12 22 13 20 12 27 --- 8 | 81 76 81 77 81 91 --- 80
R19M | 1501 40 93 55 49 52 54 --- 26 | 50 68 56 72 69 72 --- 50
R20M | 739 59 70 73 70 26 44 --- 26 | 79 52 64 97 44 75 --- 57
R21M | 1466 26 28 22 12 16 20 298 9 | 58 36 38 51 52 50 114 46
R22M | 2688 47 43 95 91 86 45 --- 32 | 54 68 122 79 94 67 --- 70
R24M | 869 24 31 19 21 19 17 --- 10 | 142 154 157 154 149 164 --- 152
------+----------------------------------------------+------------------------------------------
RMS | 1699 27 37 36 35 30 31 263 |T 67 66 72 76 69 73 179 65
WRMS | 1699 23 26 22 19 20 27 263 |NE 25 24 28 32 23 32 139 23
MEDI | 1466 21 28 21 21 18 27 277 |MD 58 66 64 75 65 67 139 57
Table 3.2157.5 GPS week: 2157 Day: 5 MJD: 59348
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 | 552 44 34 25 34 40 26 --- 15 | 29 24 46 47 24 35 --- 29
R02 | 2589 10 14 11 8 16 16 276 5 | 16 25 28 25 19 19 268 18
R03 | 714 8 8 11 17 14 25 124 6 | 18 14 23 23 19 40 121 18
XR04 | 722 10 19 25 --- 16 24 --- 10 | 19 20 27 --- 25 31 --- 20
R05M | 1150 21 14 19 12 26 31 278 9 | 105 110 126 129 112 118 158 115
R07M | 1334 14 15 14 26 17 29 419 9 | 14 12 23 28 16 28 257 14
R08 | 2363 11 16 13 23 16 28 --- 8 | 15 17 23 31 16 28 --- 16
R09E | 3701 37 26 18 25 32 39 --- 13 | 120 112 112 119 107 88 --- 107
XR11E | 3000 16 21 11 18 --- 18 --- 8 | 29 32 30 40 --- 31 --- 29
R12E | 1327 18 31 14 27 31 28 --- 11 | 82 78 77 86 90 88 --- 82
R13E | 1991 33 40 39 43 24 35 --- 16 | 82 87 82 75 78 77 --- 75
R14E | 787 15 22 16 20 11 20 --- 8 | 57 47 60 63 57 53 --- 55
R15E | 2448 10 30 13 20 22 37 197 10 | 117 112 110 119 105 124 93 113
R16E | 969 26 30 23 40 31 27 --- 13 | 46 34 42 70 48 47 --- 42
R17M | 1234 15 25 20 21 20 22 --- 9 | 218 219 217 219 218 231 --- 220
R18M | 1220 9 26 13 15 17 19 --- 7 | 117 120 118 120 115 112 --- 116
R19M | 870 41 102 44 55 61 49 --- 26 | 42 56 41 64 47 50 --- 36
R20M | 602 60 71 66 35 50 26 --- 24 | 70 42 48 54 65 37 --- 44
R21M | 1302 24 26 19 13 9 36 192 10 | 49 33 32 36 42 51 152 37
R22M | 1690 49 20 65 67 77 27 --- 25 | 44 60 84 66 100 64 --- 63
R24M | 715 18 34 17 24 15 17 --- 9 | 224 230 221 226 224 227 --- 225
------+----------------------------------------------+------------------------------------------
RMS | 1660 29 37 29 31 33 29 264 |T 72 70 74 82 76 75 174 70
WRMS | 1660 20 26 20 21 23 28 264 |NE 19 20 29 31 20 30 194 20
MEDI | 1234 18 26 18 23 20 27 197 |MD 49 47 48 64 57 51 152 44
Table 3.2157.6 GPS week: 2157 Day: 6 MJD: 59349
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 | 1059 32 29 20 26 47 45 --- 15 | 42 48 37 44 37 41 --- 36
R02 | 713 13 12 13 19 16 16 115 6 | 28 31 34 34 24 37 175 28
R03 | 1188 7 10 10 20 12 17 136 5 | 33 34 34 43 30 41 117 33
XR04 | 929 6 15 13 --- 16 28 --- 8 | 29 35 34 --- 26 40 --- 29
R05M | 1982 15 8 17 25 18 18 163 7 | 123 128 132 135 132 131 160 129
R07M | 862 11 12 17 20 13 25 323 7 | 26 30 32 36 35 45 138 30
R08 | 1054 11 16 20 19 15 48 --- 10 | 25 26 36 35 30 37 --- 26
R09E | 2908 15 22 14 15 24 41 --- 10 | 129 137 131 129 129 134 --- 130
XR11E | 3432 11 16 7 14 --- 21 --- 7 | 41 40 41 47 --- 45 --- 41
R12E | 1120 16 27 14 21 10 19 --- 8 | 89 91 80 86 79 79 --- 83
R13E | 1347 26 34 33 97 25 46 --- 20 | 92 98 98 135 98 86 --- 94
R14E | 691 13 17 17 13 10 23 --- 7 | 67 67 61 68 70 74 --- 66
R15E | 2218 9 23 11 18 17 23 135 7 | 138 144 140 136 148 140 122 140
R16E | 842 21 27 18 57 34 24 --- 13 | 42 45 49 60 56 51 --- 43
R17M | 1079 20 20 22 15 16 23 --- 9 | 340 335 328 338 345 336 --- 337
R18M | 614 14 19 12 14 16 25 --- 7 | 148 142 145 145 150 148 --- 146
R19M | 693 41 81 39 62 72 40 --- 25 | 57 60 35 81 50 54 --- 39
R20M | 668 64 82 77 68 67 45 --- 30 | 90 47 50 85 82 49 --- 44
R21M | 980 21 23 16 14 8 13 124 7 | 71 41 42 59 55 55 109 53
R22M |36767 28 29 31 54 20 38 --- 15 | 76 97 128 93 113 96 --- 96
R24M | 909 22 40 22 32 15 26 --- 11 | 331 329 337 335 334 337 --- 333
------+----------------------------------------------+------------------------------------------
RMS | 8530 25 34 27 40 30 31 181 |T 96 95 95 106 101 97 136 93
WRMS | 8530 19 23 21 22 19 31 181 |NE 31 34 35 39 29 39 146 30
MEDI | 1054 15 22 17 20 16 25 135 |MD 71 60 50 81 70 55 122 53
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