[IGSREPORT-26314] Wk 2030 IGLOS Final Orbits
acc
acc at igs.org
Sun Dec 30 15:38:33 PST 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2030 (Dec 02, 2018 - Dec 08, 2018)
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 2.2030.
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:
igl2030[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2030 in the SP3 format.
igl20307.sum Combination Report for GPS Week 2030.
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 | 4.9 ns
1 | 4.7 ns
2 | 3.7 ns
3 | 5.1 ns
4 | 5.8 ns
5 | 5.5 ns
6 | 5.1 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 1.2030, 1a.2030).
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 2.2030.0-6)
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 3.2030.0-6).
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 2030 summary. (Dec 02, 2018 - Dec 08, 2018)
Table 1.2030.a GPS week : 2030 MJD: 58454.0-58460.0
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 17 0 19 .21 22 18 | 1591 -222 3128 9582
| 1 1 1 12 13 22 .04 | 508 1332
cof n/a| 0 0 -1 21 8 17 .13 25 20 | 1575 -224 3125 9589
| 1 1 2 18 29 25 .12 | 514 1338
emx n/a| 0 0 -3 -16 -8 37 .03 25 25 | -100 -386 3047 8841
| 1 0 4 15 19 45 .07 | 7576 865
esx n/a| 0 0 0 14 -21 42 .11 22 18 | 7765 146 3050 10802
| 1 0 2 12 21 26 .04 | 13023 1102
gfz n/a| -2 0 -3 14 31 54 .01 28 21 | 0 -597 3053 9147
| 1 1 2 18 17 32 .07 | 0 1050
grg n/a| 2 1 3 -50 -8 -112 -.33 22 20 | 5151 -390 3134 8610
| 0 1 5 17 21 31 .07 | 571 1180
iac n/a| 1 0 5 28 16 -40 -.08 22 20 | 6995 -167 4133 13666
| 1 1 2 18 63 29 .04 | 2146 1145
mcc n/a| -3 2 24 17 16 961 .14 286 286 | --- --- --- ---
| 16 6 16 172 143 591 1.05 | --- ---
Table 1.2030.b GPS week : 2030 MJD: 58454.0-58460.0
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 | 21 16 15 14 18 22 21 |
R02 | 6 6 8 6 6 9 9 |
R03 | 9 7 7 7 7 7 8 |
R04 | 5 4 6 7 6 6 8 |
R05 | 10 8 9 10 12 16 14 |
R07 | 6 7 8 7 7 7 11 |
R08 | 8 8 10 11 8 12 13 |
R09 | 7 7 8 7 7 8 9 |
R10 | 6 8 6 7 6 7 7 |
R11 | 8 7 6 6 6 9 9 |
R13 | 7 7 8 8 9 10 11 |
R14 | 8 8 9 7 7 10 10 |
R15 | 10 12 10 9 10 10 11 |
R16 | 12 13 14 16 12 15 23 |
R17 | 11 9 8 9 9 9 9 |
R18 | 7 8 8 7 8 8 12 |
R19 | 23 19 23 22 21 24 26 |
R20 | 12 11 17 12 13 13 14 |
R21 | 8 9 10 10 8 8 10 |
R22 | 8 8 9 10 10 9 9 |
R23 | 10 11 10 10 8 10 11 |
R24 | 15 17 16 12 13 12 13 |
R26 | 31 26 19 14 19 0 0 |
Table 1.2030.c GPS week : 2030 MJD: 58454.0-58460.0
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 2030 0 | 12 37 -11 -16 1941 -2827 83.7 1695 1695 | 4906 0
brd 2030 1 | -9 -100 38 242 276 -4059 82.3 1605 1605 | 4747 0
brd 2030 2 | 5 7 78 -269 214 -3057 84.0 1724 1724 | 3749 0
brd 2030 3 | 37 20 29 -153 1058 -2593 83.5 1535 1535 | 5076 0
brd 2030 4 | 43 69 33 -177 2510 -1601 82.0 1286 1286 | 5784 0
brd 2030 5 | -9 -38 -42 -336 827 -2245 81.9 1350 1350 | 5508 0
brd 2030 6 | 0 -31 19 -1381 -1960 -2186 83.5 1631 1631 | 5116 0
-------------+------------------------------------------------------------+----------------
brd 2030 mean| 11 -5 20 -299 695 -2652 83.0 1546 1546 | 4983 0
brd 2030 sdev| 21 56 38 513 1440 781 .9 168 168 | 649 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 2.2030.0 GPS week: 2030 Day: 0 MJD: 58454
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 -2 -2 0 -14 33 .16 21 16 | 2233 1100 3184 9869
cof n/a| 0 -2 -1 -2 -31 22 .10 26 20 | 2222 1087 3183 9873
emx n/a| 0 -1 1 -28 -19 24 .06 29 29 | -6371 591 3143 8889
esx n/a| -1 0 1 21 -29 14 .14 22 17 | 1049 1004 3126 10981
gfz n/a| 0 0 -3 38 13 26 .12 33 20 | 0 91 3128 9473
grg n/a| 1 0 0 -53 1 -66 -.34 21 17 | 4232 1130 3237 8815
iac n/a| 2 0 4 14 53 -17 -.09 21 19 | 9978 1839 5377 24057
mcc n/a| 0 2 21 -124 141 651 -.26 229 229 | --- --- --- ---
Table 2.2030.1 GPS week: 2030 Day: 1 MJD: 58455
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 28 3 53 .18 22 17 | 2189 1186 2768 10433
cof n/a| 0 1 0 26 1 36 .15 24 19 | 2181 1210 2739 10376
emx n/a| 0 0 1 -32 -43 29 -.02 23 23 | -9892 321 2700 9506
esx n/a| -1 0 -2 26 -21 11 .17 21 16 | 7198 1645 2700 12276
gfz n/a| -2 0 -7 19 15 55 .06 26 23 | 0 452 2710 9923
grg n/a| 2 0 -1 -57 -39 -139 -.30 22 19 | 4597 403 3005 9828
iac n/a| 0 -1 7 26 91 -13 -.04 21 19 | 6732 -350 4119 10076
mcc n/a| -12 2 43 -297 181 524 .48 311 311 | --- --- --- ---
Table 2.2030.2 GPS week: 2030 Day: 2 MJD: 58456
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 31 -11 25 .19 21 18 | 1570 -2278 3216 9394
cof n/a| -2 0 -5 47 38 51 .07 27 21 | 1562 -2300 3223 9416
emx n/a| 0 0 0 -20 5 88 -.04 23 23 | 13294 -1905 3180 8704
esx n/a| 0 -1 -2 -2 22 74 .08 23 18 | -3991 -1300 3203 11548
gfz n/a| -1 0 -2 -12 44 74 .00 31 20 | 0 -2443 3178 9029
grg n/a| 0 0 7 -61 2 -146 -.23 22 21 | 4976 -2302 3181 8578
iac n/a| 1 0 1 59 -59 -86 -.10 23 19 | 4161 -540 3576 11804
mcc n/a| 2 3 30 51 -79 1277 1.58 323 323 | --- --- --- ---
Table 2.2030.3 GPS week: 2030 Day: 3 MJD: 58457
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 7 9 27 .19 19 15 | 1145 -1626 3282 9769
cof n/a| -1 0 -1 41 3 -29 .01 22 18 | 1109 -1615 3278 9777
emx n/a| 0 0 -4 -3 -1 80 .01 24 24 | -1905 -898 3117 8953
esx n/a| 0 0 0 13 -13 47 .07 21 16 | 34262 -1115 3112 9154
gfz n/a| -2 2 0 34 32 84 -.03 27 21 | 0 -1603 3164 8995
grg n/a| 2 1 2 -37 23 -142 -.28 21 18 | 5491 -1367 3134 8579
iac n/a| 0 -1 8 18 -38 -38 -.04 24 22 | 7897 -931 3664 10860
mcc n/a| -19 2 37 174 129 2141 1.23 264 264 | --- --- --- ---
Table 2.2030.4 GPS week: 2030 Day: 4 MJD: 58458
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 -1 20 5 7 .21 22 17 | 855 608 3473 9651
cof n/a| -1 0 0 3 26 19 .27 28 22 | 843 602 3481 9676
emx n/a| -1 0 -3 -21 7 37 .13 23 23 | 4412 261 3438 9093
esx n/a| 1 0 1 -2 -31 68 .08 20 18 | 12780 606 3444 10975
gfz n/a| -2 0 -1 -2 11 85 -.02 26 27 | 0 114 3434 9188
grg n/a| 3 1 -1 -34 -22 -114 -.32 23 21 | 5517 480 3439 8332
iac n/a| 0 -1 6 24 36 -47 -.12 22 21 | 6210 -853 3929 11537
mcc n/a| 28 -5 2 60 43 920 -.48 379 379 | --- --- --- ---
Table 2.2030.5 GPS week: 2030 Day: 5 MJD: 58459
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 4 24 4 .25 22 22 | 1432 -142 3197 8857
cof n/a| 1 -2 0 18 45 3 .01 23 20 | 1398 -142 3198 8876
emx n/a| 2 -1 -9 -21 -20 49 .11 25 25 | 1645 -600 3053 8307
esx n/a| 0 -1 0 30 -35 22 .12 22 18 | 5336 -364 3062 10145
gfz n/a| -4 0 -4 10 49 -4 -.01 28 21 | 0 -542 3064 8771
grg n/a| 2 3 12 -28 -2 -92 -.40 20 17 | 5827 -631 3215 7938
mcc n/a| -1 15 2 187 -186 797 -1.46 221 221 | --- --- --- ---
Table 2.2030.6 GPS week: 2030 Day: 6 MJD: 58460
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 27 -11 -15 .29 25 24 | 1715 -402 2781 9107
cof n/a| 1 -2 2 12 -26 22 .30 24 23 | 1713 -410 2776 9135
emx n/a| 1 -1 -8 11 11 -49 -.04 25 25 | -1883 -473 2702 8441
esx n/a| -2 0 3 16 -44 61 .10 23 20 | -2276 549 2705 10537
gfz n/a| -2 -1 -4 12 50 56 -.08 27 17 | 0 -250 2699 8650
grg n/a| 2 3 7 -76 -25 -84 -.42 29 26 | 5422 -444 2727 8203
mcc n/a| -17 -4 32 72 -115 417 -.12 274 274 | --- --- --- ---
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 3.2030.0 GPS week: 2030 Day: 0 MJD: 58454
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 991 51 46 55 41 72 29 28 --- 20 | 88 96 82 69 93 52 35 --- 66
R02 | 832 10 16 15 18 7 12 15 313 6 | 51 55 49 56 51 41 30 361 47
R03M | 2710 16 22 22 16 15 28 10 155 8 | 49 52 58 57 59 50 31 112 51
R04M | 1517 9 13 12 11 19 8 8 --- 5 | 64 67 69 65 66 61 30 --- 64
R05M | 792 18 30 19 16 45 16 16 --- 9 | 61 64 61 54 66 54 26 --- 53
R07M | 875 6 15 11 13 14 14 14 --- 5 | 66 68 65 57 65 67 36 --- 61
R08M | 911 15 20 15 19 25 11 15 --- 7 | 57 59 57 66 72 62 34 --- 59
R09M | 4271 12 15 13 15 19 17 19 --- 7 | 48 51 50 57 51 51 34 --- 50
R10M | 1471 5 9 23 14 17 15 9 --- 6 | 53 53 48 61 58 44 37 --- 51
R11 | 1161 20 22 14 10 19 13 26 232 8 | 58 60 42 52 58 47 37 117 48
R13 | 759 10 12 23 10 23 15 15 --- 7 | 55 58 46 61 64 50 38 --- 54
R14 | 1434 14 24 22 12 34 13 17 --- 8 | 73 76 62 61 71 59 41 --- 64
R15 | 1553 24 33 20 18 19 19 23 --- 9 | 133 136 114 112 111 127 53 --- 117
R16E | 579 14 27 27 23 44 32 24 --- 12 | 51 51 50 60 45 41 44 --- 47
R17E | 1669 13 21 26 22 38 22 22 --- 10 | 116 117 121 128 136 110 56 --- 118
R18E | 868 14 15 25 9 23 10 12 --- 7 | 35 33 37 36 40 33 26 --- 34
R19E | 1816 43 58 75 50 68 36 41 --- 23 | 86 90 95 81 96 65 71 --- 78
R20E | 860 18 22 35 19 39 25 27 --- 12 | 47 50 45 44 45 38 31 --- 37
R21E | 721 15 18 28 14 20 16 18 185 8 | 39 42 34 35 45 30 24 131 32
R22E | 883 15 17 30 11 21 17 19 --- 8 | 110 111 120 115 111 122 60 --- 114
R23E | 614 16 26 11 26 28 21 21 --- 9 | 55 63 51 56 51 61 42 --- 53
R24E | 3635 29 36 32 41 36 33 26 --- 15 | 48 65 49 68 71 49 30 --- 47
XR26E | 3738 29 83 --- --- --- --- 33 --- 31 | 57 90 --- --- --- --- 38 --- 50
------+---------------------------------------------------+-----------------------------------------------
RMS | 1694 21 26 29 22 33 21 21 229 |T 65 69 63 65 69 59 38 180 60
WRMS | 1694 16 20 29 17 20 17 19 229 |NE 76 80 65 68 74 62 39 239 66
MEDI | 991 15 22 22 16 23 16 19 185 |MD 57 63 51 60 64 51 36 117 53
Table 3.2030.1 GPS week: 2030 Day: 1 MJD: 58455
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 949 46 60 32 42 37 26 16 --- 15 | 52 78 40 54 59 42 26 --- 41
R02 | 601 8 11 13 13 17 19 12 494 6 | 36 39 38 38 40 36 18 476 33
R03M | 2147 20 22 10 14 16 12 19 238 7 | 33 32 39 41 48 34 29 179 36
R04M | 1918 11 15 7 8 11 9 8 --- 4 | 43 44 42 45 49 40 21 --- 42
R05M | 880 10 24 19 21 15 25 11 --- 8 | 39 42 38 48 34 41 22 --- 36
R07M | 861 16 13 9 9 19 16 17 --- 6 | 42 39 35 37 30 38 16 --- 33
R08M | 1147 16 17 12 16 23 12 19 --- 7 | 36 40 35 41 48 40 22 --- 35
R09M | 3666 12 13 15 10 18 19 19 --- 7 | 39 39 35 41 44 43 29 --- 40
R10M | 2521 9 12 14 23 10 20 16 --- 7 | 39 40 37 55 41 31 29 --- 39
R11 | 1467 13 16 17 14 21 14 15 189 7 | 39 39 32 37 40 27 22 116 32
R13 | 1121 16 19 16 17 13 10 13 --- 6 | 38 35 39 49 41 44 23 --- 39
R14 | 1026 24 17 18 12 20 12 18 --- 8 | 54 50 36 44 58 37 28 --- 43
R15 | 998 24 27 26 12 31 19 38 --- 11 | 106 111 97 93 112 102 44 --- 97
R16E | 668 36 29 31 15 30 32 22 --- 12 | 50 41 35 49 47 52 30 --- 41
R17E | 1631 16 16 25 14 22 16 22 --- 8 | 139 139 145 139 132 131 41 --- 135
R18E | 674 14 22 21 15 18 20 16 --- 7 | 31 33 33 35 36 29 19 --- 29
R19E | 2282 43 41 46 37 55 29 44 --- 19 | 81 82 70 84 114 88 55 --- 81
R20E | 1056 18 21 25 20 31 19 27 --- 10 | 42 46 32 41 50 41 32 --- 35
R21E | 519 20 15 22 19 21 13 15 227 8 | 31 31 30 31 36 26 20 140 28
R22E | 983 15 11 28 11 19 17 13 --- 8 | 109 111 105 116 109 112 52 --- 109
R23E | 523 18 21 28 26 37 18 15 --- 11 | 59 66 63 66 69 63 34 --- 59
R24E | 2759 29 20 29 39 44 52 27 --- 17 | 60 69 62 78 68 52 38 --- 60
XR26E | 4112 26 110 --- --- --- --- 24 --- 25 | 39 116 --- --- --- --- 30 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1604 22 24 23 21 26 22 21 311 |T 53 59 50 57 59 52 29 227 50
WRMS | 1604 17 19 23 16 23 19 19 311 |NE 54 58 47 52 58 48 26 296 47
MEDI | 1056 16 19 19 15 20 18 17 227 |MD 42 42 38 45 48 41 29 140 39
Table 3.2030.2 GPS week: 2030 Day: 2 MJD: 58456
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1086 42 42 20 49 30 23 25 --- 15 | 65 70 63 74 58 55 37 --- 54
R02 | 1296 14 21 21 21 22 17 9 --- 7 | 47 52 50 45 56 41 35 --- 45
R03M | 1547 14 14 12 23 19 15 9 172 7 | 50 56 59 64 52 46 46 185 54
R04M | 1023 14 15 9 13 17 12 15 --- 6 | 60 69 69 69 74 58 39 --- 64
R05M | 1009 14 21 18 21 25 27 11 --- 9 | 50 57 58 68 66 45 39 --- 54
R07M | 705 11 14 11 18 24 22 14 457 7 | 55 57 51 56 51 48 39 342 50
R08M | 922 17 12 14 27 22 20 28 --- 10 | 47 50 44 62 55 40 29 --- 45
R09M | 4170 17 19 16 15 24 17 18 --- 8 | 42 45 44 44 49 38 23 --- 40
R10M | 3367 8 14 15 19 10 14 12 --- 6 | 46 45 51 59 49 44 37 --- 48
R11 | 1841 13 13 14 14 14 17 12 232 6 | 47 42 43 48 52 36 29 147 42
R13 | 1178 19 20 16 21 17 15 15 --- 8 | 39 43 37 58 57 41 34 --- 44
R14 | 1062 20 28 18 21 17 28 14 --- 9 | 54 62 50 58 56 49 32 --- 49
R15 | 902 29 30 19 10 16 23 28 --- 10 | 99 97 82 82 81 92 39 --- 85
R16E | 867 33 68 34 27 30 34 28 --- 14 | 60 101 34 60 67 61 40 --- 49
R17E | 1310 13 10 20 13 18 21 13 --- 7 | 87 88 85 81 92 76 35 --- 83
R18E | 971 14 16 22 19 14 17 12 --- 7 | 38 36 38 48 45 34 28 --- 38
R19E | 3518 33 45 54 35 70 35 67 --- 22 | 52 62 52 44 84 58 66 --- 42
R20E | 690 18 21 33 21 81 22 28 --- 17 | 25 31 25 33 93 31 31 --- 28
R21E | 576 19 19 25 25 17 18 18 354 9 | 36 39 34 51 43 36 27 190 37
R22E | 558 18 20 27 13 18 24 19 --- 9 | 125 127 125 121 122 129 75 --- 122
R23E | 1166 24 25 25 23 27 21 17 --- 10 | 30 33 34 48 39 41 38 --- 37
XR24E | 2232 20 32 33 43 --- 30 31 --- 16 | 62 63 56 86 --- 61 40 --- 59
XR26E | 5001 19 67 --- --- --- --- 19 --- 19 | 23 68 --- --- --- --- 33 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1723 21 27 23 23 31 22 23 323 |T 53 60 53 61 63 52 37 216 51
WRMS | 1723 18 21 23 18 20 21 19 323 |NE 58 61 54 60 60 52 34 147 53
MEDI | 1086 18 20 19 21 19 21 17 232 |MD 50 57 50 58 56 45 37 185 48
Table 3.2030.3 GPS week: 2030 Day: 3 MJD: 58457
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 910 30 35 30 36 22 30 27 --- 13 | 76 77 73 52 59 53 23 --- 56
R02 | 1021 10 17 12 13 10 12 17 --- 5 | 48 52 49 47 45 48 16 --- 44
R03M | 2065 12 14 15 11 17 14 22 81 7 | 50 47 49 42 41 42 21 85 42
R04M | 1345 7 11 13 18 23 14 11 --- 6 | 47 45 51 55 49 49 17 --- 47
R05M | 588 18 15 28 16 39 15 17 --- 10 | 43 49 56 48 67 40 21 --- 44
R07M | 860 17 16 14 16 18 12 15 334 7 | 56 54 54 46 37 49 22 125 46
R08M | 938 18 24 17 26 24 19 37 --- 11 | 49 48 46 65 59 43 17 --- 47
R09M | 3793 17 24 15 12 28 11 11 --- 7 | 32 42 29 28 48 30 26 --- 29
R10M | 2282 10 13 18 11 12 21 11 --- 6 | 46 48 39 50 44 58 27 --- 46
R11 | 750 13 14 15 11 19 7 9 190 5 | 47 47 41 40 38 38 25 103 39
R13 | 503 7 10 16 20 21 22 13 --- 7 | 45 47 34 60 56 38 32 --- 45
R14 | 649 16 14 13 14 11 20 14 --- 7 | 45 44 39 49 44 32 32 --- 40
R15 | 2579 27 28 18 10 12 17 27 --- 9 | 76 77 55 53 58 53 50 --- 56
R16E | 1276 30 34 47 31 39 37 31 --- 16 | 75 70 53 63 74 57 40 --- 54
R17E | 824 12 21 22 19 26 18 18 --- 8 | 142 143 147 148 148 131 33 --- 141
R18E | 730 12 11 12 21 15 16 16 --- 7 | 22 26 28 42 43 24 18 --- 28
R19E | 2472 39 39 50 49 66 38 55 --- 22 | 70 71 72 68 97 51 54 --- 64
R20E | 805 24 22 29 24 34 29 26 --- 12 | 28 29 36 39 57 29 35 --- 26
R21E | 709 17 16 29 15 32 16 20 352 9 | 28 29 20 23 40 27 20 113 22
R22E | 510 19 10 29 17 20 17 23 --- 9 | 78 81 79 89 83 85 42 --- 82
R23E | 1300 19 31 22 17 24 20 24 --- 9 | 73 75 74 77 78 81 32 --- 73
XR24E | 2008 17 31 22 29 --- 22 31 --- 12 | 36 43 42 42 --- 33 34 --- 36
XR26E | 3959 13 93 --- --- --- --- 15 --- 14 | 28 82 --- --- --- --- 29 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1534 19 22 24 21 27 21 24 264 |T 53 57 53 55 60 49 28 106 49
WRMS | 1534 15 18 24 16 21 18 22 264 |NE 56 57 48 50 50 43 29 103 46
MEDI | 938 17 17 18 17 22 17 18 190 |MD 47 48 49 49 56 43 27 103 45
Table 3.2030.4 GPS week: 2030 Day: 4 MJD: 58458
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 836 52 60 35 40 32 43 28 --- 17 | 61 69 50 34 45 36 37 --- 39
R02 | 576 11 17 8 14 15 15 17 535 6 | 43 48 40 46 41 43 29 393 39
R03M | 1304 7 13 10 8 21 16 22 174 6 | 42 51 40 44 48 59 35 92 42
R04M | 1227 9 13 12 11 15 9 16 --- 5 | 51 51 56 50 47 56 34 --- 51
R05M | 591 20 20 32 24 41 14 26 --- 12 | 48 51 53 52 63 44 29 --- 43
R07M | 1012 14 24 13 13 24 19 10 584 7 | 48 56 46 35 56 45 34 233 43
R08M | 616 19 23 15 18 13 17 23 --- 8 | 46 56 53 64 56 61 40 --- 54
R09M | 3096 18 20 18 13 19 10 12 --- 7 | 35 37 27 31 36 27 42 --- 28
R10M | 1634 8 9 19 14 10 17 9 --- 6 | 45 48 39 51 49 49 40 --- 45
R11 | 661 13 19 16 9 20 15 7 124 6 | 46 50 37 45 50 31 37 73 40
R13 | 1296 14 21 17 23 12 28 12 --- 8 | 47 50 40 52 42 27 38 --- 40
R14 | 440 17 22 15 13 13 16 15 --- 6 | 55 57 44 52 46 39 37 --- 48
R15 | 2747 21 29 20 13 32 21 24 --- 10 | 98 103 83 88 92 93 53 --- 88
R16E | 1297 21 49 32 26 21 36 24 --- 12 | 68 95 50 65 64 66 37 --- 58
R17E | 1049 17 16 19 16 21 18 29 --- 9 | 82 84 86 91 82 82 54 --- 79
R18E | 797 11 11 17 18 20 17 17 --- 7 | 20 23 18 28 32 21 31 --- 20
R19E | 1086 48 52 52 40 51 39 46 --- 20 | 71 74 65 78 81 70 61 --- 68
R20E | 1066 27 29 23 30 34 23 28 --- 12 | 35 43 29 48 61 27 34 --- 33
R21E | 662 11 12 20 9 23 15 21 210 7 | 26 26 22 22 31 24 24 69 21
R22E | 607 17 17 26 16 27 17 22 --- 9 | 83 83 83 91 89 85 64 --- 84
R23E | 578 23 42 13 16 20 15 18 --- 8 | 31 35 20 30 27 27 39 --- 23
R24E | 1182 22 34 23 22 35 40 23 --- 12 | 35 47 37 35 37 40 46 --- 29
XR26E | 3611 18 51 --- --- --- --- 19 --- 18 | 28 65 --- --- --- --- 30 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1286 22 28 23 20 26 23 22 379 |T 49 56 46 51 53 47 39 172 45
WRMS | 1286 17 22 23 18 27 21 21 379 |NE 58 62 49 52 52 44 38 233 49
MEDI | 1049 17 21 18 16 21 17 21 210 |MD 46 51 40 48 48 43 37 92 42
Table 3.2030.5 GPS week: 2030 Day: 5 MJD: 58459
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg mcc IGL | cod cof emx esx gfz grg mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 770 50 45 32 33 60 42 --- 22 | 55 60 48 44 80 36 --- 43
R02 | 597 11 26 10 17 18 25 370 8 | 39 47 39 44 45 28 209 35
R03M | 818 9 11 13 15 16 12 185 6 | 40 36 36 47 55 41 115 41
R04M | 733 10 11 9 11 17 10 --- 5 | 78 80 76 80 94 79 --- 80
R05M | 954 38 20 29 30 38 25 --- 16 | 73 75 72 76 93 82 --- 73
R07M | 1243 13 13 11 8 22 14 --- 7 | 42 37 44 45 50 34 --- 40
R08M | 1000 14 7 23 32 20 22 --- 11 | 36 44 46 62 51 36 --- 42
R09M | 3383 18 20 15 13 19 11 --- 7 | 51 53 46 49 54 44 --- 46
R10M | 1809 9 9 15 11 18 12 --- 6 | 43 43 42 43 38 49 --- 42
R11 | 628 18 20 22 9 14 19 68 8 | 50 48 38 41 47 40 83 41
R13 | 696 13 14 21 24 24 18 --- 10 | 41 40 29 42 22 38 --- 32
R14 | 494 16 15 20 23 18 17 --- 9 | 42 42 36 39 39 32 --- 34
R15 | 2179 13 15 26 15 26 15 --- 9 | 91 92 81 81 98 88 --- 87
R16E | 685 23 25 45 27 24 30 --- 15 | 40 52 54 55 46 62 --- 45
R17E | 1286 18 16 20 19 17 10 --- 8 | 137 138 141 139 136 139 --- 137
R18E | 725 12 10 16 15 19 17 --- 8 | 41 35 35 43 45 33 --- 35
R19E | 2729 44 56 60 49 58 29 --- 24 | 109 116 123 123 131 101 --- 113
R20E | 823 20 19 30 23 37 20 --- 13 | 41 38 30 43 58 27 --- 34
R21E | 744 9 12 23 16 19 14 138 8 | 35 39 33 33 42 37 131 34
R22E | 647 15 15 23 19 22 11 --- 9 | 76 80 81 75 79 82 --- 77
R23E | 1271 23 22 17 20 21 15 --- 9 | 41 41 47 43 52 43 --- 42
R24E | 711 19 30 17 18 36 26 --- 11 | 47 45 41 39 52 32 --- 37
XR26E | 3038 4 39 --- --- --- --- --- 0 | 34 40 --- --- --- --- --- 34
------+----------------------------------------------+------------------------------------------
RMS | 1349 22 23 25 22 28 20 221 |T 55 57 55 58 63 53 134 53
WRMS | 1349 22 20 25 18 21 17 221 |NE 53 54 45 48 55 43 146 45
MEDI | 818 15 16 20 18 20 17 138 |MD 42 45 44 44 52 40 115 42
Table 3.2030.6 GPS week: 2030 Day: 6 MJD: 58460
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg mcc IGL | cod cof emx esx gfz grg mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 968 47 48 43 36 46 30 --- 20 | 87 91 85 68 81 66 --- 71
R02 | 887 13 15 13 17 11 31 412 9 | 54 57 56 58 52 42 325 50
R03M | 699 12 17 7 10 29 17 323 8 | 60 64 65 60 67 58 223 59
R04M | 1069 11 8 14 11 16 22 --- 7 | 98 100 102 97 105 99 --- 98
R05M | 542 31 36 27 34 19 12 --- 13 | 81 88 84 75 77 74 --- 73
R07M | 1244 14 12 14 13 34 25 --- 10 | 60 61 59 52 63 52 --- 54
R08M | 1475 29 15 22 37 20 10 --- 13 | 56 69 61 88 72 58 --- 64
R09M | 4863 14 12 15 10 25 25 --- 9 | 72 73 74 67 70 72 --- 68
R10M | 919 10 10 11 14 14 15 --- 6 | 55 53 48 61 53 49 --- 53
R11 | 789 12 17 22 13 15 27 109 9 | 60 64 48 51 57 68 78 54
R13 | 929 12 13 27 16 15 32 --- 10 | 60 65 57 72 65 82 --- 64
R14 | 580 13 13 21 16 12 33 --- 10 | 56 53 45 53 55 60 --- 50
R15 | 1662 15 18 22 15 17 33 --- 10 | 121 122 111 114 114 127 --- 115
R16E | 504 41 47 28 38 38 73 --- 22 | 105 124 111 136 117 125 --- 115
R17E | 2151 20 17 22 14 10 17 --- 8 | 103 103 106 100 100 97 --- 99
R18E | 925 30 15 18 16 28 25 --- 12 | 61 52 51 51 55 49 --- 48
R19E | 2720 51 48 58 52 59 24 --- 25 | 143 146 150 136 151 141 --- 140
R20E | 758 24 23 33 17 36 26 --- 13 | 45 46 39 45 64 42 --- 42
R21E | 755 23 20 21 10 17 25 125 9 | 46 46 42 45 48 42 69 42
R22E | 924 22 15 21 11 17 18 --- 9 | 76 75 73 79 79 76 --- 75
R23E | 2131 16 22 18 28 15 26 --- 10 | 77 81 81 83 75 84 --- 78
R24E | 1540 23 28 19 19 39 28 --- 13 | 71 71 77 79 76 83 --- 75
XR26E | 3153 5 56 --- --- --- --- --- 0 | 37 68 --- --- --- --- --- 38
------+----------------------------------------------+------------------------------------------
RMS | 1630 25 24 25 23 27 29 274 |T 73 77 73 75 77 74 173 70
WRMS | 1630 24 23 25 20 17 26 274 |NE 73 75 67 69 70 74 201 67
MEDI | 929 16 17 21 16 17 25 125 |MD 61 69 65 68 70 68 78 64
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