[IGSREPORT-26550] Wk 2049 IGLOS Final Orbits
acc
acc at igs.org
Sun May 5 18:05:47 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2049 (Apr 14, 2019 - Apr 20, 2019)
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 2.2049.
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:
igl2049[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2049 in the SP3 format.
igl20497.sum Combination Report for GPS Week 2049.
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 | 3.7 ns
1 | 4.6 ns
2 | 1.1 ns
3 | 1.4 ns
4 | -1.3 ns
5 | 0.8 ns
6 | -0.8 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 1.2049, 1a.2049).
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 2.2049.0-6)
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 3.2049.0-6).
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 2049 summary. (Apr 14, 2019 - Apr 20, 2019)
Table 1.2049.a GPS week : 2049 MJD: 58587.0-58593.0
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 8 33 12 1 .09 27 22 | 8536 1194 3495 9675
| 0 1 2 15 20 23 .03 | 3393 2128
cof n/a| 1 0 9 28 16 -4 .10 29 24 | 8530 1202 3503 9688
| 1 1 2 16 24 23 .05 | 3393 2109
emx n/a| 0 0 -4 31 -22 20 .04 24 24 | -3871 991 3263 9088
| 1 1 2 24 16 37 .04 | 9781 1497
esx n/a| -1 0 -3 18 -4 -3 .12 22 19 | -1335 1761 3272 11223
| 1 0 1 21 16 34 .02 | 8738 2813
gfz n/a| -1 0 5 0 19 -9 .07 27 22 | 0 924 3275 8937
| 1 0 1 21 23 27 .06 | 0 2537
grg n/a| 2 0 0 -100 -2 -29 -.36 27 25 | 825 857 3280 8453
| 1 1 3 14 12 121 .03 | 1359 2440
iac n/a| 1 -1 -5 29 24 2 -.10 32 32 | 2332 -159 4019 10589
| 1 0 2 48 68 104 .04 | 2297 1240
mcc n/a| -4 0 -7 94 59 -146 -.49 140 140 | --- --- --- ---
| 10 6 18 91 152 424 .49 | --- ---
Table 1.2049.b GPS week : 2049 MJD: 58587.0-58593.0
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 | 22 23 23 19 22 23 21 |
R02 | 7 7 7 7 9 7 7 |
R03 | 13 8 9 10 10 12 10 |
R04 | 9 8 7 9 8 10 11 |
R05 | 11 10 11 13 10 11 10 |
R07 | 12 15 12 10 8 9 10 |
R08 | 9 11 10 8 9 9 10 |
R09 | 6 6 7 5 7 8 8 |
R10 | 7 7 8 9 9 10 6 |
R11 | 7 8 8 5 7 9 8 |
R13 | 11 10 10 12 11 7 8 |
R14 | 8 9 7 9 9 8 8 |
R15 | 8 10 11 9 9 9 9 |
R16 | 16 17 22 18 16 17 17 |
R17 | 10 8 9 9 10 11 8 |
R18 | 9 6 7 7 9 8 7 |
R19 | 20 19 21 20 19 18 17 |
R20 | 12 12 15 14 14 17 15 |
R21 | 9 10 12 10 11 11 8 |
R22 | 9 10 12 10 10 11 10 |
R23 | 10 11 11 11 11 11 13 |
R24 | 15 11 20 15 15 15 14 |
R26 | 30 56 0 18 19 16 21 |
Table 1.2049.c GPS week : 2049 MJD: 58587.0-58593.0
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 2049 0 | 9 84 201 -611 -241 5179 82.4 1511 1511 | 3672 0
brd 2049 1 | 29 74 203 2135 2357 3902 82.1 1394 1394 | 4603 0
brd 2049 2 | 56 -18 192 190 -239 2093 81.5 1964 1964 | 1066 0
brd 2049 3 | -42 -31 181 -170 -1032 2823 82.4 1276 1276 | 1445 0
brd 2049 4 | 8 53 201 -552 -953 3685 82.9 1127 1127 | -1347 0
brd 2049 5 | 23 -41 199 814 326 3904 81.2 1307 1307 | 789 0
brd 2049 6 | -35 -15 184 0 386 3344 82.2 1312 1312 | -800 0
-------------+------------------------------------------------------------+----------------
brd 2049 mean| 6 15 195 258 86 3561 82.1 1412 1412 | 1346 0
brd 2049 sdev| 35 53 8 957 1143 967 .6 269 269 | 2170 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 2.2049.0 GPS week: 2049 Day: 0 MJD: 58587
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 8 27 52 3 .11 29 23 | 3179 1076 3265 9728
cof n/a| 1 -2 8 39 28 -4 .07 29 25 | 3185 1062 3263 9729
emx n/a| 0 0 -1 6 -32 11 .01 22 22 | -12409 1080 3267 9748
esx n/a| 0 0 -5 21 -1 -16 .11 23 19 | 2963 1531 3265 12105
gfz n/a| 0 -1 5 -5 -4 3 .04 23 19 | 0 704 3277 9506
grg n/a| 1 0 -2 -84 5 44 -.32 29 27 | 3248 940 3270 9000
iac n/a| 2 -1 -1 34 8 -109 -.05 30 30 | 5256 -1006 4137 10008
mcc n/a| -8 -6 -3 -19 163 -528 -.32 135 135 | --- --- --- ---
Table 2.2049.1 GPS week: 2049 Day: 1 MJD: 58588
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 10 51 9 -24 .04 30 23 | 5704 5211 3005 9278
cof n/a| 0 1 13 27 28 -45 .03 33 25 | 5704 5212 3008 9282
emx n/a| 1 0 -4 45 -14 -49 .05 24 24 | 9093 3599 2996 9373
esx n/a| -2 0 -2 18 -30 -26 .15 21 16 | 1670 6490 2993 11967
gfz n/a| 0 -1 6 -11 55 -46 .04 22 23 | 0 5194 3006 9205
grg n/a| 1 0 -5 -108 -20 122 -.36 26 26 | 1994 4897 3001 8513
iac n/a| 3 -1 -1 95 47 49 -.09 34 34 | 3350 1276 3895 12912
mcc n/a| -16 -3 18 151 235 339 .07 146 146 | --- --- --- ---
Table 2.2049.2 GPS week: 2049 Day: 2 MJD: 58589
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 8 36 6 -4 .09 28 21 | 7684 250 3551 8755
cof n/a| 1 0 12 50 44 -20 .14 32 22 | 7676 275 3545 8750
emx n/a| -1 1 -5 24 -43 26 .03 24 24 | -10179 1332 3542 8713
esx n/a| 0 0 -4 1 -2 -43 .09 24 20 | 1835 331 3539 10911
gfz n/a| -2 0 8 4 13 -30 .13 33 25 | 0 -37 3564 8642
grg n/a| 4 1 1 -87 19 110 -.40 29 27 | 933 101 3564 8342
iac n/a| 2 0 -5 -50 46 -47 -.16 36 35 | 2971 -1874 3661 8738
mcc n/a| -7 -7 14 -52 103 306 -.24 130 130 | --- --- --- ---
Table 2.2049.3 GPS week: 2049 Day: 3 MJD: 58590
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 9 50 21 -22 .09 30 23 | 11663 2213 3115 8816
cof n/a| 0 2 10 23 40 -2 .14 28 23 | 11674 2189 3115 8819
emx n/a| 2 -3 -8 69 -19 64 .11 24 24 | 9390 865 2998 8727
esx n/a| -2 0 -3 22 17 -11 .13 22 18 | 2480 4156 3012 10889
gfz n/a| -1 1 5 -40 11 -2 .04 27 21 | 0 2587 3029 8730
grg n/a| 1 1 2 -86 -2 -50 -.30 21 17 | 250 2409 3022 8258
iac n/a| 0 0 -9 42 40 27 -.07 35 35 | 2802 249 3813 9059
mcc n/a| 5 0 -9 169 -101 19 -.10 114 114 | --- --- --- ---
Table 2.2049.4 GPS week: 2049 Day: 4 MJD: 58591
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 10 36 15 4 .09 26 23 | 8465 -1126 4951 10477
cof n/a| 0 0 9 12 -2 26 .03 31 26 | 8422 -1047 5009 10560
emx n/a| 1 0 -3 22 1 59 .04 23 23 | -925 -1245 3983 9216
esx n/a| -2 0 -2 -2 5 27 .16 22 19 | 5777 -2254 3961 11287
gfz n/a| -1 0 5 23 32 39 -.01 28 22 | 0 -2801 3968 9021
grg n/a| 2 -1 -4 -117 -8 -127 -.39 26 22 | -534 -2885 3979 8581
iac n/a| 1 -2 -7 67 -117 -73 -.11 32 33 | -1912 -348 5619 11490
mcc n/a| 0 -4 -31 163 -186 52 -.49 116 116 | --- --- --- ---
Table 2.2049.5 GPS week: 2049 Day: 5 MJD: 58592
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 5 7 -8 43 .14 24 20 | 12931 1458 3818 12247
cof n/a| 3 1 7 6 -6 18 .10 25 21 | 12935 1438 3817 12246
emx n/a| 0 0 -2 46 -8 17 -.00 23 23 | -12782 1456 3304 9358
esx n/a| -1 1 -4 61 1 56 .10 24 20 | -19989 1275 3306 10992
gfz n/a| 0 0 5 7 -9 -10 .09 29 26 | 0 1471 3288 9151
grg n/a| 4 2 -1 -111 0 -142 -.36 29 28 | 174 1197 3321 8775
iac n/a| 0 0 -6 -7 44 -32 -.10 31 31 | 3183 1498 3910 13558
mcc n/a| 11 6 -14 106 155 -611 -1.10 139 139 | --- --- --- ---
Table 2.2049.6 GPS week: 2049 Day: 6 MJD: 58593
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 26 -9 12 .05 25 22 | 10131 -719 2763 8424
cof n/a| 2 1 6 41 -17 -1 .14 27 24 | 10120 -709 2768 8430
emx n/a| 0 1 -4 2 -38 13 .04 24 24 | -9290 -148 2755 8485
esx n/a| -2 0 -4 4 -20 -8 .12 22 20 | -4082 798 2828 10413
gfz n/a| -3 0 2 21 35 -21 .14 25 17 | 0 -650 2795 8308
grg n/a| 2 1 3 -108 -11 -164 -.37 26 26 | -287 -660 2805 7707
iac n/a| 2 -1 -4 23 103 202 -.15 29 28 | 679 -913 3104 8361
mcc n/a| -12 9 -25 142 44 -603 -1.23 197 197 | --- --- --- ---
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 3.2049.0 GPS week: 2049 Day: 0 MJD: 58587
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 | 1437 70 61 38 55 29 37 60 --- 22 | 114 113 52 61 88 56 32 --- 60
R02 | 1262 18 9 18 11 18 12 18 122 7 | 74 70 57 63 63 57 46 164 59
R03 | 759 20 24 22 29 26 40 37 92 13 | 89 92 67 63 94 98 52 99 75
R04 | 566 22 18 15 19 20 19 29 --- 9 | 80 78 53 53 75 71 40 --- 61
R05 | 847 27 26 15 21 20 22 35 --- 10 | 74 75 56 48 66 70 45 --- 57
R07 | 561 25 24 17 25 19 33 34 157 11 | 93 93 69 65 90 97 54 111 76
R08 | 1628 20 22 18 21 11 23 30 --- 9 | 80 83 68 62 77 76 50 --- 68
R09 | 925 11 13 11 9 16 11 13 --- 5 | 25 27 27 26 36 27 39 --- 28
R10 | 1688 8 15 14 10 21 11 28 --- 7 | 44 42 44 51 61 52 33 --- 48
R11 | 660 14 15 13 19 6 19 21 194 7 | 54 55 52 53 55 59 42 57 51
R13 | 4405 7 13 23 19 33 33 26 --- 11 | 49 55 41 58 74 72 39 --- 54
R14 | 1846 12 11 17 15 25 15 24 --- 8 | 50 51 41 53 64 57 33 --- 49
R15 | 1888 15 14 16 8 14 24 23 --- 7 | 73 74 72 65 71 66 52 --- 66
R16 | 1181 42 51 33 21 25 56 23 --- 15 | 74 71 49 67 70 74 51 --- 62
R17 | 786 28 27 19 20 23 17 23 --- 9 | 90 92 79 80 95 66 66 --- 79
R18 | 911 10 13 26 10 23 24 16 --- 8 | 93 92 87 90 102 97 89 --- 91
R19 | 1378 74 62 33 35 33 32 42 --- 19 | 79 79 46 34 37 41 42 --- 33
R20 | 735 15 26 31 19 31 27 26 --- 11 | 64 69 39 51 84 64 55 --- 56
R21 | 1759 20 17 18 14 17 17 27 78 8 | 52 52 32 29 52 47 39 63 38
R22 | 671 24 26 20 17 21 16 22 --- 9 | 66 68 44 37 63 50 37 --- 47
R23 | 1328 23 29 24 29 16 14 25 --- 10 | 77 77 75 95 79 80 95 --- 82
R24 | 930 21 32 17 18 37 61 35 --- 15 | 59 63 57 76 93 83 74 --- 68
XR26 | 5386 27 177 --- --- --- --- 32 --- 29 | 80 172 --- --- --- --- 97 --- 87
------+---------------------------------------------------+-----------------------------------------------
RMS | 1510 29 29 22 23 23 29 30 135 |T 71 75 54 58 72 66 52 98 60
WRMS | 1510 23 25 22 19 19 27 30 135 |NE 71 75 54 58 72 66 52 98 60
MEDI | 1181 20 24 18 19 21 22 26 122 |MD 74 74 52 58 71 66 46 99 60
Table 3.2049.1 GPS week: 2049 Day: 1 MJD: 58588
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 | 810 80 89 32 58 27 25 65 --- 22 | 80 95 39 52 65 40 26 --- 42
R02 | 1468 12 20 15 9 16 18 23 146 6 | 52 59 51 52 57 41 37 121 48
R03 | 1156 25 22 15 18 15 11 23 172 8 | 64 63 47 51 65 50 41 83 52
R04 | 1090 26 30 13 15 15 14 19 --- 7 | 53 57 38 38 33 39 37 --- 36
R05 | 896 30 25 15 23 10 23 27 --- 9 | 58 56 41 41 42 45 30 --- 39
R07 | 882 20 22 24 31 32 43 48 153 15 | 63 66 44 43 78 85 34 114 55
R08 | 1938 16 12 15 14 27 24 47 --- 10 | 53 55 47 46 64 51 27 --- 47
R09 | 1029 11 14 13 7 16 19 19 --- 6 | 19 19 23 21 29 20 34 --- 21
R10 | 3431 15 15 20 7 20 11 14 --- 6 | 27 28 28 37 41 35 41 --- 34
R11 | 694 11 14 19 10 15 27 19 98 7 | 30 29 33 39 38 47 38 65 36
R13 | 2535 15 27 25 7 27 27 26 --- 9 | 31 28 31 35 45 40 21 --- 32
R14 | 1973 10 10 19 15 26 21 33 --- 9 | 29 27 25 30 44 43 20 --- 30
R15 | 1424 16 19 19 15 24 20 37 --- 9 | 47 47 50 40 55 37 30 --- 42
R16 | 534 42 61 42 19 29 57 42 --- 17 | 57 73 56 44 53 42 28 --- 42
R17 | 633 26 25 20 13 14 14 23 --- 8 | 95 96 98 91 96 82 85 --- 91
R18 | 864 12 13 18 8 8 13 19 --- 6 | 100 103 100 100 101 99 98 --- 99
R19 | 1073 68 62 40 31 29 31 62 --- 19 | 67 67 49 51 55 61 47 --- 46
R20 | 846 20 21 30 25 23 33 30 --- 12 | 44 42 38 41 50 55 46 --- 42
R21 | 745 20 17 26 18 24 20 30 152 10 | 44 43 36 35 47 46 29 80 37
R22 | 620 24 24 24 18 22 15 25 --- 9 | 47 52 38 34 53 48 33 --- 41
R23 | 837 30 24 23 24 11 26 28 --- 10 | 83 86 87 106 94 97 82 --- 92
R24 | 1204 24 26 30 12 20 34 26 --- 11 | 38 44 35 49 45 71 38 --- 43
XR26 | 5519 46 124 --- --- --- --- 66 --- 55 | 130 178 --- --- --- --- 93 --- 97
------+---------------------------------------------------+-----------------------------------------------
RMS | 1393 30 33 24 21 22 26 34 146 |T 57 61 47 48 56 53 43 92 49
WRMS | 1393 23 25 24 16 23 26 34 146 |NE 57 61 47 48 56 53 43 92 49
MEDI | 1029 20 22 20 15 20 21 27 152 |MD 53 56 39 41 53 46 37 83 42
Table 3.2049.2 GPS week: 2049 Day: 2 MJD: 58589
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 | 1211 75 67 30 55 28 39 65 --- 23 | 94 89 42 46 74 61 34 --- 46
R02 | 1283 15 13 11 10 12 27 22 130 7 | 53 53 42 51 54 31 33 97 43
R03 | 998 17 14 17 19 22 22 22 166 8 | 70 67 55 49 71 60 47 77 57
R04 | 880 17 15 13 10 14 16 19 --- 6 | 62 62 47 49 60 54 37 --- 50
R05 | 614 24 22 18 29 21 24 24 --- 10 | 60 67 42 53 52 61 44 --- 48
R07 | 896 18 18 14 20 23 31 53 143 11 | 76 76 63 54 78 84 45 80 65
R08 | 1190 15 20 17 16 22 29 35 --- 10 | 63 67 47 50 67 78 43 --- 56
R09 | 863 9 9 20 8 14 18 17 --- 6 | 19 20 30 21 24 20 25 --- 19
R10 | 4505 11 10 17 15 20 24 24 --- 8 | 36 37 35 51 47 41 28 --- 38
R11 | 766 8 12 17 11 25 23 14 90 7 | 45 46 36 43 62 47 43 52 44
R13 | 1647 18 19 12 9 25 34 34 --- 10 | 28 33 36 36 45 52 25 --- 35
R14 | 2062 16 25 14 18 14 12 23 --- 7 | 38 45 28 43 34 41 30 --- 33
R15 | 1094 16 20 13 20 32 22 46 --- 11 | 55 60 49 51 69 51 48 --- 52
R16 | 665 29 34 45 36 73 58 43 --- 21 | 55 60 41 46 97 50 37 --- 45
R17 | 651 24 22 20 14 16 12 28 --- 8 | 67 67 61 57 59 58 42 --- 57
R18 | 522 7 12 20 12 11 21 21 --- 7 | 75 73 64 77 70 82 68 --- 72
R19 | 6366 66 88 32 39 40 43 66 --- 21 | 78 97 51 47 55 56 49 --- 46
R20 | 878 18 44 35 22 55 23 35 --- 14 | 48 74 41 39 80 52 47 --- 44
R21 | 551 24 25 23 21 42 15 30 109 11 | 39 44 22 29 55 26 28 47 27
R22 | 673 31 27 21 24 37 15 32 --- 12 | 65 66 51 43 72 56 55 --- 53
R23 | 942 20 27 19 33 26 18 26 --- 11 | 122 125 125 132 121 125 135 --- 125
R24 | 1873 26 29 52 27 59 55 40 --- 19 | 63 71 54 82 123 114 67 --- 77
XR26 | 8089 --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 67 --- 71
------+---------------------------------------------------+-----------------------------------------------
RMS | 1964 28 32 24 24 33 29 36 130 |T 59 63 48 52 66 59 46 70 52
WRMS | 1964 21 22 24 20 25 27 35 130 |NE 59 63 48 52 66 59 46 70 52
MEDI | 942 18 20 18 19 23 23 28 130 |MD 60 66 42 49 62 54 43 77 48
Table 3.2049.3 GPS week: 2049 Day: 3 MJD: 58590
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 | 1358 70 60 24 46 17 19 66 --- 19 | 92 85 41 22 46 47 28 --- 36
R02 | 1057 13 18 12 11 11 13 31 85 6 | 59 63 43 47 56 48 23 72 46
R03 | 711 16 19 18 17 25 10 44 159 9 | 70 75 53 52 76 61 27 74 57
R04 | 802 16 17 16 18 26 16 35 --- 9 | 58 53 46 42 72 66 34 --- 52
R05 | 639 24 17 24 28 29 27 38 --- 12 | 55 58 36 52 76 72 31 --- 51
R07 | 1014 19 21 15 29 20 20 33 112 10 | 75 76 59 41 76 78 39 42 61
R08 | 590 14 15 17 10 18 18 30 --- 7 | 69 70 61 57 76 80 45 --- 65
R09 | 881 9 12 13 8 13 8 19 --- 5 | 13 18 17 20 24 13 24 --- 15
R10 | 4158 13 13 19 18 26 14 27 --- 8 | 43 43 37 50 53 46 36 --- 42
R11 | 814 6 17 13 9 11 12 17 116 5 | 42 48 33 46 42 44 43 43 40
R13 | 1704 24 29 23 9 20 38 43 --- 12 | 35 36 33 43 56 64 25 --- 43
R14 | 1799 18 13 12 20 16 20 36 --- 9 | 47 48 42 46 49 49 29 --- 42
R15 | 1080 24 33 19 14 18 17 32 --- 9 | 52 59 48 35 50 42 32 --- 41
R16 | 622 44 31 35 34 54 40 27 --- 18 | 57 58 58 44 87 57 42 --- 51
R17 | 642 20 22 23 16 22 15 27 --- 9 | 113 115 105 104 107 103 102 --- 105
R18 | 621 9 7 18 14 10 12 21 --- 6 | 122 123 126 132 132 115 133 --- 126
R19 | 633 75 67 45 30 33 25 48 --- 19 | 88 85 65 61 73 73 70 --- 61
R20 | 664 26 35 32 20 51 22 38 --- 14 | 72 79 57 62 92 54 54 --- 60
R21 | 589 21 22 25 17 28 15 30 77 10 | 55 53 36 38 57 54 33 50 43
R22 | 541 36 29 19 13 17 15 25 --- 9 | 59 54 35 35 48 30 30 --- 36
R23 | 787 15 11 20 31 27 20 36 --- 11 | 72 79 70 85 69 62 88 --- 71
R24 | 747 18 29 44 28 39 23 34 --- 14 | 73 80 52 87 97 74 76 --- 74
XR26 | 5240 13 144 --- --- --- --- 24 --- 18 | 48 126 --- --- --- --- 40 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1275 30 28 24 22 27 21 35 114 |T 63 68 52 54 68 60 47 56 54
WRMS | 1275 23 23 24 18 21 17 35 114 |NE 63 68 52 54 68 60 47 56 54
MEDI | 787 18 21 19 17 20 17 32 112 |MD 59 63 46 46 69 57 36 50 51
Table 3.2049.4 GPS week: 2049 Day: 4 MJD: 58591
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 | 1021 60 74 38 59 38 11 66 --- 21 | 84 98 57 34 76 46 23 --- 44
R02 | 783 14 18 16 18 14 26 32 51 9 | 58 57 53 44 52 72 31 98 51
R03 | 677 23 24 18 25 16 21 35 128 10 | 71 70 55 43 60 60 32 78 52
R04 | 2203 11 16 15 10 14 22 34 --- 8 | 52 56 39 44 49 56 21 --- 43
R05 | 696 19 21 22 21 14 24 33 --- 10 | 40 40 44 51 50 55 26 --- 43
R07 | 722 17 22 14 16 13 14 28 132 7 | 66 70 54 48 60 58 51 101 54
R08 | 1036 18 16 14 15 19 22 28 --- 8 | 65 62 54 51 69 70 48 --- 58
R09 | 1010 12 20 12 13 25 11 13 --- 6 | 20 24 19 18 34 35 31 --- 21
R10 | 2138 12 14 18 12 19 34 27 --- 9 | 35 33 25 34 48 55 29 --- 35
R11 | 1173 11 11 13 12 12 22 18 168 6 | 45 43 41 42 42 43 37 51 40
R13 | 1383 18 19 24 8 38 27 24 --- 10 | 34 34 40 46 61 53 35 --- 43
R14 | 1131 10 18 19 12 23 20 36 --- 9 | 43 48 38 37 56 53 26 --- 40
R15 | 872 18 16 15 17 16 17 35 --- 8 | 58 54 57 50 68 57 41 --- 54
R16 | 784 33 59 13 23 31 64 21 --- 15 | 44 69 53 60 61 57 58 --- 52
R17 | 1264 20 19 22 20 31 12 21 --- 9 | 63 63 56 51 64 52 47 --- 53
R18 | 1186 14 15 21 22 16 23 15 --- 8 | 66 66 64 65 74 73 67 --- 66
R19 | 851 61 55 48 22 38 34 39 --- 18 | 60 53 48 44 53 46 52 --- 38
R20 | 1008 22 25 25 19 48 40 36 --- 14 | 61 53 43 46 63 28 44 --- 43
R21 | 859 21 20 22 19 35 12 33 55 10 | 51 54 42 35 62 42 38 47 42
R22 | 552 30 36 20 15 29 12 24 --- 9 | 56 64 42 42 54 38 45 --- 43
R23 | 765 16 24 18 28 26 21 32 --- 10 | 110 110 119 125 112 118 131 --- 118
R24 | 996 26 36 41 22 50 24 36 --- 15 | 50 56 35 57 86 62 58 --- 52
XR26 | 4855 15 66 --- --- --- --- 22 --- 18 | 62 106 --- --- --- --- 65 --- 68
------+---------------------------------------------------+-----------------------------------------------
RMS | 1127 26 31 23 22 28 26 32 116 |T 56 60 49 48 61 55 45 75 50
WRMS | 1127 23 26 23 19 22 22 32 116 |NE 56 60 49 48 61 55 45 75 50
MEDI | 1008 18 20 18 18 23 22 32 128 |MD 58 56 44 44 60 55 41 78 44
Table 3.2049.5 GPS week: 2049 Day: 5 MJD: 58592
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 | 608 62 47 41 60 29 38 56 --- 22 | 76 67 67 53 67 50 28 --- 52
R02 | 1157 11 12 12 12 11 19 23 158 6 | 55 58 56 47 60 65 45 51 54
R03 | 1207 21 24 20 28 26 31 33 113 11 | 64 68 48 52 76 75 38 83 57
R04 | 1794 21 22 17 22 22 18 33 --- 9 | 59 57 45 42 64 58 37 --- 49
R05 | 534 18 24 14 32 15 18 41 --- 10 | 54 59 49 52 53 52 44 --- 49
R07 | 702 18 11 15 17 15 17 34 135 8 | 64 56 56 55 57 56 43 46 55
R08 | 1305 18 23 14 17 14 23 27 --- 8 | 62 69 47 50 62 65 44 --- 54
R09 | 1419 14 21 11 11 18 32 16 --- 8 | 20 23 26 25 27 36 33 --- 22
R10 | 2668 7 13 16 23 43 18 20 --- 10 | 28 35 25 29 56 39 24 --- 29
R11 | 1524 9 19 13 15 19 26 28 189 8 | 35 39 34 38 39 45 26 53 34
R13 | 1429 8 13 15 12 15 18 28 --- 7 | 33 39 32 41 35 36 22 --- 31
R14 | 554 13 16 15 16 16 17 32 --- 8 | 37 37 30 32 37 33 19 --- 30
R15 | 482 15 22 14 17 20 15 35 --- 8 | 53 56 41 43 54 47 34 --- 45
R16 | 738 19 34 27 24 26 78 25 --- 16 | 49 53 39 39 53 74 39 --- 42
R17 | 1663 20 17 20 16 43 19 23 --- 10 | 82 80 77 66 76 83 74 --- 75
R18 | 1086 12 15 21 7 27 18 12 --- 7 | 119 121 113 114 107 125 125 --- 115
R19 | 993 46 57 43 27 34 37 42 --- 17 | 48 52 57 59 56 63 63 --- 52
R20 | 2068 20 16 37 24 61 42 33 --- 16 | 57 54 48 53 84 45 47 --- 51
R21 | 1348 17 16 25 17 29 20 31 71 10 | 58 54 53 53 59 53 44 46 52
R22 | 780 30 27 24 22 22 19 28 --- 11 | 48 46 38 30 45 42 42 --- 38
R23 | 1248 27 29 19 34 17 20 25 --- 11 | 89 91 92 107 108 96 106 --- 98
R24 | 953 21 22 38 20 51 30 29 --- 14 | 45 56 33 55 73 53 53 --- 46
XR26 | 4286 11 50 --- --- --- --- 20 --- 15 | 68 99 --- --- --- --- 61 --- 68
------+---------------------------------------------------+-----------------------------------------------
RMS | 1306 24 25 23 24 29 29 31 139 |T 56 59 50 51 61 58 47 55 52
WRMS | 1306 20 21 23 20 26 28 31 139 |NE 56 59 50 51 61 58 47 55 52
MEDI | 1207 18 22 17 17 22 19 28 135 |MD 55 56 47 50 57 53 43 51 51
Table 3.2049.6 GPS week: 2049 Day: 6 MJD: 58593
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 | 621 56 53 43 53 36 28 49 --- 20 | 97 107 70 72 96 61 44 --- 66
R02 | 595 15 11 21 9 9 17 17 236 6 | 72 70 69 63 67 60 55 116 64
R03 | 1026 18 15 16 26 24 20 28 127 10 | 94 90 76 67 101 93 59 98 81
R04 | 1161 14 17 18 23 28 28 31 --- 10 | 81 82 62 60 90 91 50 --- 71
R05 | 480 26 23 19 23 14 21 33 --- 10 | 68 63 55 58 64 72 45 --- 58
R07 | 817 16 21 26 15 20 23 27 160 9 | 85 87 64 63 85 89 56 89 72
R08 | 936 26 28 27 19 20 17 20 --- 10 | 81 80 63 70 84 88 54 --- 73
R09 | 2733 13 18 11 14 13 28 23 --- 7 | 28 27 29 26 41 34 45 --- 30
R10 | 1937 9 9 10 10 16 18 20 --- 6 | 45 47 41 50 60 47 38 --- 46
R11 | 1165 7 7 11 19 9 25 25 251 7 | 53 52 52 51 52 58 43 76 50
R13 | 2119 13 13 20 10 19 24 22 --- 8 | 53 56 50 54 67 65 38 --- 54
R14 | 798 15 16 15 8 22 16 25 --- 7 | 58 61 51 50 62 53 32 --- 51
R15 | 493 14 20 17 19 13 21 33 --- 8 | 77 81 71 62 77 77 48 --- 68
R16 | 1146 37 38 41 15 20 66 30 --- 16 | 66 76 49 65 74 93 54 --- 63
R17 | 1058 20 21 23 10 17 16 23 --- 8 | 75 74 69 66 77 76 64 --- 69
R18 | 734 7 9 16 11 14 21 22 --- 7 | 111 109 108 112 108 115 113 --- 110
R19 | 692 50 53 33 33 36 31 36 --- 16 | 68 67 53 58 65 65 64 --- 51
R20 | 2497 16 25 35 24 49 32 41 --- 15 | 76 78 57 57 105 73 57 --- 68
R21 | 1024 15 13 21 9 18 16 22 180 7 | 69 69 52 52 78 61 47 60 58
R22 | 1175 28 24 22 17 19 14 30 --- 9 | 60 60 35 35 56 49 39 --- 43
R23 | 1422 28 35 24 35 24 21 27 --- 12 | 115 120 121 134 126 120 133 --- 123
R24 | 931 30 44 28 16 47 29 31 --- 14 | 51 70 50 67 108 71 61 --- 65
XR26 | 3119 14 43 --- --- --- --- 27 --- 21 | 78 103 --- --- --- --- 87 --- 87
------+---------------------------------------------------+-----------------------------------------------
RMS | 1312 25 27 24 22 25 26 29 197 |T 72 75 61 63 79 73 57 87 66
WRMS | 1312 22 24 24 20 17 26 28 197 |NE 72 75 61 63 79 73 57 87 66
MEDI | 1026 16 21 21 16 19 21 27 180 |MD 72 74 55 60 77 71 54 89 65
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