[IGSREPORT-24427] Wk 1893 IGLOS Final Orbits
IGS ACC
acc at igs.org
Fri May 6 15:17:11 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1893 (Apr 17, 2016 - Apr 23, 2016)
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 2.1893.
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:
igl1893[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1893 in the SP3 format.
igl18937.sum Combination Report for GPS Week 1893.
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
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 | -8.8 ns
1 | -7.2 ns
2 | -8.2 ns
3 | -6.0 ns
4 | -9.5 ns
5 | -4.4 ns
6 | -8.1 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 1.1893, 1a.1893).
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 2.1893.0-6)
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 3.1893.0-6).
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 1893 summary. (Apr 17, 2016 - Apr 23, 2016)
Table 1.1893.a GPS week : 1893 MJD: 57495.0-57501.0
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 1 19 32 -18 0 .24 35 35 | --- --- --- ---
| 1 1 5 31 13 36 .05 | --- ---
cof n/a| 0 0 19 27 -3 -6 .21 38 36 | --- --- --- ---
| 1 0 6 31 22 37 .04 | --- ---
emx n/a| -1 0 2 -30 -77 -34 .22 28 28 | -12484 604 3906 7939
| 1 1 2 17 25 43 .06 | 3695 1797
esx n/a| 0 0 0 25 1 -6 -.14 17 15 | -10742 -561 3962 9015
| 0 1 1 25 11 25 .02 | 4341 3528
gfz n/a| 0 1 -9 14 63 40 .11 23 20 | 0 -256 3850 7704
| 1 1 1 23 47 29 .07 | 0 3112
grg n/a| 0 -1 -7 -22 28 -6 -.39 37 36 | -438507 -242 4894 618339
| 1 2 5 27 36 37 .08 | 7217 3736
iac n/a| 1 0 -1 -16 -1 -1 .04 17 17 | -6720 -102 3957 7781
| 0 0 2 41 32 29 .03 | 1370 2729
mcc n/a| 4 0 -4 -22 7 -373 -.02 190 190 | --- --- --- ---
| 11 17 22 304 152 1111 .46 | --- ---
Table 1.1893.b GPS week : 1893 MJD: 57495.0-57501.0
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 | 13 13 13 14 12 11 11 |
R02 | 10 10 9 14 11 7 7 |
R03 | 9 8 9 12 11 8 9 |
R04 | 9 8 7 11 9 8 7 |
R05 | 14 13 12 13 14 13 13 |
R06 | 9 9 9 10 7 8 8 |
R07 | 9 9 9 10 9 7 8 |
R08 | 11 10 9 11 9 9 10 |
R09 | 8 8 8 8 6 7 8 |
R10 | 9 10 10 13 11 9 8 |
R13 | 10 9 9 9 9 8 11 |
R14 | 16 16 15 12 11 13 20 |
R15 | 12 11 12 10 11 14 12 |
R16 | 12 16 13 13 13 11 13 |
R17 | 8 11 11 9 10 9 10 |
R18 | 8 8 8 8 6 9 8 |
R19 | 9 8 10 10 9 8 9 |
R20 | 13 14 15 11 14 13 13 |
R21 | 8 9 9 10 11 10 11 |
R22 | 10 10 10 10 12 10 11 |
R23 | 8 9 7 8 10 9 10 |
R24 | 13 18 17 13 14 15 14 |
R26 | 0 0 112 51 55 47 56 |
Table 1.1893.c GPS week : 1893 MJD: 57495.0-57501.0
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 1893 0 | 69 52 87 -1077 461 1176 83.7 1250 1250 | -8782 0
brd 1893 1 | 0 -15 117 51 -1753 -171 83.0 1301 1301 | -7223 0
brd 1893 2 | 40 -38 176 -126 -1182 -1458 82.6 1451 1451 | -8161 0
brd 1893 3 | 0 -48 153 15 1366 -3510 82.2 1530 1530 | -5971 0
brd 1893 4 | -50 -38 139 1719 -1302 -1626 83.5 1291 1291 | -9472 0
brd 1893 5 | 26 19 145 -672 -197 -806 83.4 1367 1367 | -4358 0
brd 1893 6 | 36 -5 160 -820 -548 -583 83.6 1492 1492 | -8139 0
-------------+------------------------------------------------------------+----------------
brd 1893 mean| 17 -10 139 -129 -450 -997 83.1 1383 1383 | -7443 0
brd 1893 sdev| 38 36 29 925 1092 1445 .6 108 108 | 1762 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 2.1893.0 GPS week: 1893 Day: 0 MJD: 57495
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 22 20 -14 -52 .24 33 31 | --- --- --- ---
cof n/a| 0 0 19 22 -17 -25 .14 35 33 | --- --- --- ---
emx n/a| -3 0 1 -47 -67 -18 .21 28 28 | -12014 398 3547 7825
esx n/a| 0 0 0 47 -9 16 -.10 16 13 | -13949 -789 3545 8595
gfz n/a| 0 1 -8 -27 24 59 .03 24 22 | 0 -560 3509 7688
grg n/a| -1 -2 -12 -23 37 -9 -.26 36 35 | -436589 -115 3534 616356
iac n/a| 2 1 0 -15 26 -43 .08 17 17 | -8189 -926 3529 7665
mcc n/a| 25 1 -35 156 -291 -1075 -.90 106 106 | --- --- --- ---
Table 2.1893.1 GPS week: 1893 Day: 1 MJD: 57496
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 20 34 2 27 .30 34 34 | --- --- --- ---
cof n/a| -1 0 22 58 37 -7 .15 36 34 | --- --- --- ---
emx n/a| -1 -2 6 -17 -41 -48 .15 28 29 | -19773 702 3595 7601
esx n/a| 0 0 2 26 8 -23 -.16 16 16 | -11760 1822 3676 9321
gfz n/a| -2 3 -11 14 52 66 .11 25 23 | 0 617 3528 7210
grg n/a| 2 2 -12 7 52 -18 -.34 35 33 | -435327 348 3628 615897
iac n/a| 0 0 -1 -71 -26 1 .06 18 18 | -6458 -803 3640 7485
mcc n/a| -4 13 -9 -131 82 -2193 .27 266 266 | --- --- --- ---
Table 2.1893.2 GPS week: 1893 Day: 2 MJD: 57497
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 20 46 -11 -12 .26 34 34 | --- --- --- ---
cof n/a| 1 0 16 19 -6 -50 .23 37 38 | --- --- --- ---
emx n/a| -1 1 0 -15 -107 -55 .29 29 29 | -13103 -172 3616 7377
esx n/a| 0 -1 0 61 2 -9 -.17 18 17 | -8346 -830 3651 8701
gfz n/a| -1 2 -8 -1 -10 6 .12 21 15 | 0 -1402 3506 7101
grg n/a| 0 -3 -11 24 48 -50 -.39 39 39 | -434066 -1434 3615 618208
iac n/a| 1 0 1 -43 39 42 .03 16 16 | -6630 -1676 3632 7209
mcc n/a| 6 16 12 160 32 -849 .39 166 166 | --- --- --- ---
Table 2.1893.3 GPS week: 1893 Day: 3 MJD: 57498
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 -2 6 1 -18 -37 .27 33 34 | --- --- --- ---
cof n/a| 0 -1 8 -15 -17 12 .22 38 37 | --- --- --- ---
emx n/a| 0 0 0 -44 -74 -33 .27 24 25 | -9470 -91 3787 7863
esx n/a| 0 0 -1 9 19 -19 -.16 17 16 | -4738 -1551 3794 8826
gfz n/a| 0 1 -11 28 58 42 .10 24 26 | 0 110 3720 7593
grg n/a| -1 1 -8 -40 44 -25 -.48 35 32 | -432460 -89 3772 616945
iac n/a| 0 0 3 16 -28 15 .01 20 20 | -5515 1227 3783 7727
mcc n/a| 8 -26 34 389 81 243 -.18 127 127 | --- --- --- ---
Table 2.1893.4 GPS week: 1893 Day: 4 MJD: 57499
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 17 -8 -22 41 .26 36 35 | --- --- --- ---
cof n/a| 0 0 20 0 -27 66 .22 39 36 | --- --- --- ---
emx n/a| 1 0 0 -29 -53 19 .25 25 26 | -13840 34 4170 8875
esx n/a| -1 2 1 -4 0 16 -.14 17 15 | -18073 -1092 4193 9206
gfz n/a| 1 0 -6 27 117 11 .05 23 16 | 0 -1382 4056 8587
grg n/a| -1 -5 2 -43 -47 -24 -.48 35 32 | -437402 -1826 4189 618611
iac n/a| 0 -1 -3 27 -24 -24 .00 18 18 | -8993 -1569 4231 8550
mcc n/a| 3 -20 -19 15 0 674 .41 197 197 | --- --- --- ---
Table 2.1893.5 GPS week: 1893 Day: 5 MJD: 57500
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 23 45 -21 35 .19 37 36 | --- --- --- ---
cof n/a| -2 0 26 32 -11 -33 .26 38 37 | --- --- --- ---
emx n/a| 0 0 2 -50 -106 6 .14 27 28 | -9049 4473 5234 8866
esx n/a| -1 0 2 -3 -15 -47 -.12 15 13 | -8364 5067 5444 9666
gfz n/a| 1 2 -9 15 80 14 .24 22 22 | 0 5589 5258 8787
grg n/a| -1 -3 -3 -45 52 67 -.44 40 39 | -453992 6941 5401 627113
iac n/a| 2 0 -5 27 31 18 .07 14 14 | -5504 5509 5447 9014
mcc n/a| -7 13 -10 -194 -48 1006 -.22 208 208 | --- --- --- ---
Table 2.1893.6 GPS week: 1893 Day: 6 MJD: 57501
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 22 85 -41 -5 .16 40 38 | --- --- --- ---
cof n/a| 0 0 26 77 15 -8 .23 42 39 | --- --- --- ---
emx n/a| -3 0 5 -6 -93 -111 .23 32 28 | -10145 -1116 3393 7166
esx n/a| 0 1 0 38 4 20 -.13 18 16 | -9964 -6559 3432 8795
gfz n/a| 0 -1 -10 45 120 80 .15 20 19 | 0 -4770 3373 6968
grg n/a| -2 0 -6 -36 14 13 -.37 36 41 | -439716 -5519 10125 615248
iac n/a| 1 0 -2 -59 -30 -15 .06 16 16 | -5751 -2477 3440 6819
mcc n/a| -4 7 -3 -550 195 -420 .06 261 261 | --- --- --- ---
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 3.1893.0 GPS week: 1893 Day: 0 MJD: 57495
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 947 49 49 30 15 24 40 29 --- 13 | 121 102 111 109 115 114 103 --- 108
R02E | 768 25 36 25 18 23 35 10 --- 9 | 156 153 148 169 174 144 156 --- 159
R03E | 827 30 28 24 12 24 26 12 --- 8 | 57 54 48 53 57 56 53 --- 51
R04E | 1609 25 23 21 18 22 30 16 --- 9 | 51 48 49 42 50 60 46 --- 45
R05E | 1619 27 31 43 24 39 33 28 --- 14 | 40 40 47 38 51 60 46 --- 38
R06E | 616 26 26 22 12 20 27 15 --- 8 | 100 105 100 104 101 95 101 --- 100
R07E | 1559 29 27 23 11 23 31 12 --- 8 | 46 47 44 47 57 54 44 --- 45
R08E | 1855 30 20 30 18 22 32 23 --- 11 | 73 73 76 65 83 80 85 --- 74
R09 | 978 21 25 22 9 20 30 14 --- 8 | 22 27 30 30 38 31 25 --- 25
R10 | 794 19 23 22 20 25 23 11 --- 8 | 37 37 28 29 22 22 22 --- 22
R13 | 1132 26 31 24 17 20 45 11 --- 10 | 34 36 29 31 23 35 19 --- 22
R14 | 737 57 65 41 29 25 56 20 --- 15 | 38 44 31 45 25 12 27 --- 24
R15 | 2038 30 29 23 8 49 39 12 --- 12 | 40 42 32 30 24 19 27 --- 24
R16 | 817 31 29 27 17 15 59 11 --- 11 | 31 34 31 35 34 19 24 --- 25
R17 | 754 27 21 27 6 20 23 14 --- 8 | 62 58 53 38 36 24 26 --- 35
R18 | 589 22 23 26 10 18 27 11 --- 8 | 54 54 49 39 28 24 28 --- 34
R19 | 2577 37 38 19 10 12 23 17 --- 8 | 68 70 47 37 32 29 27 --- 35
R20 | 969 38 34 33 18 19 58 24 --- 13 | 69 63 59 49 36 26 30 --- 40
R21 | 831 36 41 23 10 17 17 13 106 8 | 66 70 49 32 28 33 31 103 34
R22 | 1249 37 48 29 9 16 33 14 --- 9 | 69 78 49 40 33 25 29 --- 36
R23 | 891 29 20 19 17 17 14 7 --- 7 | 28 34 43 54 33 46 43 --- 42
R24 | 983 43 52 43 15 24 37 23 --- 13 | 80 90 57 62 39 37 48 --- 51
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 53 --- 56
------+---------------------------------------------------+-----------------------------------------------
RMS | 1250 33 35 28 16 24 36 17 106 |T 61 61 55 53 50 47 47 103 48
WRMS | 1250 31 33 28 13 22 35 17 106 |NE 49 52 41 39 30 27 30 103 33
MEDI | 947 29 29 24 15 20 31 14 106 |MD 54 54 48 40 36 33 31 103 38
Table 3.1893.1 GPS week: 1893 Day: 1 MJD: 57496
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1082 44 55 29 18 34 30 24 --- 12 | 107 112 108 106 113 101 95 --- 101
R02E | 1387 29 20 21 14 21 25 23 --- 9 | 136 139 135 135 142 141 128 --- 134
R03E | 1125 26 31 20 11 23 23 10 308 7 | 42 48 44 41 45 47 38 119 39
R04E | 786 22 21 20 15 19 23 15 --- 8 | 44 47 43 43 42 44 35 --- 39
R05E | 1124 21 31 42 26 28 28 29 --- 13 | 44 52 37 47 65 54 53 --- 44
R06E | 1239 26 20 30 13 14 30 15 --- 9 | 52 43 64 39 47 40 44 --- 43
R07E | 2364 31 27 26 11 22 24 17 314 9 | 36 36 35 37 45 45 27 123 32
R08E | 1462 31 31 29 9 28 37 13 --- 10 | 41 38 41 36 49 46 35 --- 35
R09 | 1173 28 26 24 13 16 17 9 --- 7 | 30 31 23 27 37 30 21 --- 24
R10 | 816 33 22 17 17 13 45 13 --- 9 | 31 25 23 33 31 26 22 --- 23
R13 | 624 35 36 28 9 26 28 7 --- 9 | 29 28 27 20 25 18 17 --- 18
R14 | 648 55 40 47 24 39 41 20 --- 15 | 36 51 41 58 58 22 28 --- 39
R15 | 2239 26 30 23 11 40 38 12 --- 10 | 32 33 36 28 41 27 24 --- 25
XR16 | 1201 32 54 39 14 --- 71 14 --- 16 | 34 48 35 30 --- 25 21 --- 24
R17 | 665 42 42 26 15 21 36 16 --- 10 | 46 48 36 39 33 32 17 --- 26
R18 | 707 27 25 21 10 25 16 11 --- 7 | 42 39 37 33 25 20 22 --- 26
R19 | 2748 30 39 17 14 16 20 19 --- 8 | 53 61 49 47 43 32 32 --- 40
R20 | 765 17 37 40 22 10 63 31 --- 14 | 40 60 61 55 48 18 24 --- 38
R21 | 617 36 33 22 13 17 26 14 139 8 | 56 54 46 41 32 25 31 71 35
R22 | 1061 47 40 28 10 26 16 12 --- 10 | 58 51 42 31 37 31 25 --- 31
R23 | 1041 21 29 26 20 15 29 9 --- 8 | 29 28 29 37 28 25 21 --- 26
R24 | 700 59 74 28 24 38 79 30 --- 18 | 92 105 67 63 61 49 47 --- 55
XR26 | ---- --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 49 --- 56
------+---------------------------------------------------+-----------------------------------------------
RMS | 1301 34 36 28 16 25 35 18 266 |T 50 53 48 46 49 40 37 104 41
WRMS | 1301 34 34 29 16 23 33 18 266 |NE 43 47 39 38 38 27 26 71 32
MEDI | 1061 30 31 26 14 22 28 14 308 |MD 42 48 41 39 43 31 28 119 35
Table 3.1893.2 GPS week: 1893 Day: 2 MJD: 57497
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1297 54 50 32 14 33 41 12 --- 12 | 116 113 112 111 123 110 103 --- 109
R02E | 1003 26 20 24 23 14 36 9 --- 9 | 116 114 107 116 118 109 114 --- 112
R03E | 1347 26 24 22 16 13 33 15 205 8 | 66 66 65 64 68 57 60 28 61
R04E | 1262 18 14 18 13 19 24 10 --- 7 | 55 58 55 51 58 59 56 --- 52
R05E | 1124 21 33 35 19 20 45 26 --- 12 | 60 69 75 72 76 81 69 --- 68
R06E | 792 22 20 21 20 21 26 17 --- 9 | 67 70 67 66 71 71 72 --- 66
R07E | 2586 33 32 20 15 22 24 13 175 8 | 59 65 58 59 66 68 54 29 57
R08E | 2632 30 27 19 18 21 27 10 --- 8 | 56 59 57 58 63 73 60 --- 58
R09 | 1327 25 31 27 14 22 20 9 --- 8 | 31 36 37 29 30 19 22 --- 23
R10 | 900 31 37 12 20 10 43 18 --- 9 | 44 52 34 42 38 41 21 --- 31
R13 | 894 35 36 19 14 18 43 10 --- 9 | 30 34 25 23 23 20 15 --- 17
R14 | 914 38 44 58 26 19 50 18 --- 14 | 33 31 40 47 36 27 33 --- 31
R15 | 3237 38 39 19 15 39 41 12 --- 11 | 41 44 27 31 37 24 15 --- 20
R16 | 1132 41 33 32 17 25 61 23 --- 13 | 46 43 36 37 31 27 25 --- 27
R17 | 884 39 47 19 23 20 28 21 --- 10 | 52 58 24 46 35 24 16 --- 27
R18 | 540 33 38 20 14 20 17 11 --- 8 | 45 47 29 28 20 21 19 --- 21
R19 | 2157 43 38 24 11 18 28 16 --- 9 | 55 47 40 31 28 26 20 --- 27
R20 | 912 21 54 51 20 15 79 18 --- 14 | 38 49 62 53 47 20 29 --- 38
R21 | 492 32 39 24 17 11 24 15 99 8 | 64 70 58 48 41 28 38 47 43
R22 | 1057 38 48 37 10 19 21 12 --- 9 | 59 68 52 36 30 34 30 --- 34
R23 | 530 22 18 20 16 11 25 9 --- 7 | 27 31 33 39 32 26 27 --- 30
R24 | 709 52 61 38 30 30 56 33 --- 16 | 88 92 80 63 39 32 33 --- 48
XR26 | ---- 205 509 --- --- --- --- 60 --- 112 | 118 353 --- --- --- --- 32 --- 70
------+---------------------------------------------------+-----------------------------------------------
RMS | 1450 34 37 29 18 21 39 16 166 |T 59 72 53 52 50 45 41 34 46
WRMS | 1450 34 38 29 17 15 39 16 166 |NE 51 70 41 39 33 26 25 47 32
MEDI | 1003 33 37 22 16 19 28 15 175 |MD 55 58 52 47 38 28 32 29 38
Table 3.1893.3 GPS week: 1893 Day: 3 MJD: 57498
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1413 55 59 41 17 31 23 21 --- 13 | 111 114 102 104 108 107 109 --- 103
R02E | 916 27 37 28 22 32 41 37 --- 14 | 113 124 122 118 128 113 117 --- 116
R03E | 2415 25 25 19 14 22 34 36 120 11 | 70 71 66 72 82 91 68 33 70
R04E | 1756 14 17 18 22 22 25 32 --- 10 | 76 80 79 72 81 77 79 --- 74
R05E | 863 24 42 30 24 25 47 25 --- 12 | 37 39 50 49 55 60 57 --- 46
R06E | 882 23 27 25 21 18 23 17 --- 9 | 38 37 39 56 53 50 49 --- 45
R07E | 1782 35 43 17 16 21 26 20 152 9 | 58 72 65 72 79 75 64 47 66
R08E | 2407 38 44 22 15 19 36 19 --- 10 | 68 73 57 54 64 70 65 --- 58
R09 | 1880 22 23 22 10 24 25 12 --- 8 | 29 30 33 33 39 26 29 --- 29
R10 | 1124 45 54 35 9 33 45 12 --- 12 | 60 65 57 26 22 25 23 --- 27
R13 | 1058 28 40 15 10 24 33 10 --- 8 | 34 41 30 27 24 32 22 --- 22
R14 | 1580 29 26 32 22 18 38 19 --- 11 | 30 38 34 40 32 19 22 --- 26
R15 | 3972 31 34 20 16 40 16 9 --- 10 | 36 39 23 25 25 28 14 --- 16
R16 | 513 39 44 24 25 25 55 9 --- 12 | 42 51 32 47 29 29 26 --- 28
R17 | 1112 36 36 12 18 14 29 21 --- 9 | 63 62 42 43 30 45 24 --- 36
R18 | 486 22 26 13 17 17 16 17 --- 7 | 46 51 39 44 24 43 23 --- 33
R19 | 833 43 41 20 14 20 22 15 --- 9 | 57 60 43 38 26 24 22 --- 30
R20 | 935 22 28 29 14 19 41 20 --- 10 | 36 47 47 32 28 26 30 --- 26
R21 | 445 34 34 18 17 25 28 13 104 9 | 67 65 54 51 31 29 38 40 43
R22 | 584 43 39 23 8 21 37 9 --- 10 | 65 64 48 36 30 19 34 --- 35
R23 | 533 26 35 14 17 16 28 13 --- 8 | 27 29 42 53 44 26 47 --- 42
R24 | 962 33 46 31 15 26 56 23 --- 13 | 80 85 88 62 53 51 57 --- 62
XR26 | ---- 82 238 --- --- --- --- 30 --- 51 | 104 331 --- --- --- --- 40 --- 54
------+---------------------------------------------------+-----------------------------------------------
RMS | 1530 33 38 24 17 24 35 20 127 |T 58 72 54 52 49 48 46 40 47
WRMS | 1530 34 37 25 16 26 32 20 127 |NE 51 70 43 39 31 30 30 40 33
MEDI | 962 31 37 22 16 22 29 19 120 |MD 58 62 47 47 32 32 38 40 42
Table 3.1893.4 GPS week: 1893 Day: 4 MJD: 57499
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 | 2256 60 64 27 16 26 32 19 --- 12 | 84 88 71 71 76 79 71 --- 70
R02 | 736 28 24 22 21 22 24 28 --- 10 | 109 119 107 118 118 113 96 --- 107
R03 | 1645 39 42 19 17 23 32 21 74 10 | 88 94 76 89 90 90 62 29 78
R04 | 1459 25 30 15 19 18 41 8 --- 9 | 51 54 49 54 54 54 47 --- 48
R05 | 933 24 28 33 27 27 36 36 --- 14 | 83 90 78 91 80 82 65 --- 73
R06 | 1326 19 21 11 12 19 27 12 --- 7 | 52 51 43 48 42 48 35 --- 41
R07 | 1469 37 39 21 13 26 29 7 321 9 | 56 60 52 52 64 66 48 41 51
R08 | 1617 38 43 20 20 17 28 11 --- 9 | 62 66 63 68 64 67 63 --- 62
R09 | 2495 17 21 20 11 10 19 8 --- 6 | 19 29 20 30 34 24 28 --- 25
R10 | 1391 39 65 20 20 17 45 16 --- 10 | 46 68 33 35 21 20 18 --- 23
R13 | 1156 36 24 23 12 18 32 7 --- 8 | 34 25 28 18 23 17 19 --- 16
R14 | 1261 38 42 26 21 18 31 25 --- 11 | 30 36 36 30 25 15 23 --- 19
R15 | 1840 43 35 23 16 42 18 11 --- 11 | 32 30 23 20 48 21 17 --- 17
R16 | 719 37 46 27 19 20 61 21 --- 12 | 37 35 36 36 22 24 38 --- 28
R17 | 1031 40 48 31 6 23 15 13 --- 9 | 50 55 40 21 19 17 19 --- 21
R18 | 493 19 21 12 8 18 14 10 --- 5 | 42 42 30 33 28 23 28 --- 28
R19 | 563 37 41 15 20 17 24 19 --- 9 | 53 58 34 39 33 22 24 --- 30
R20 | 746 41 44 30 16 21 53 31 --- 13 | 58 60 44 36 37 39 29 --- 29
R21 | 477 48 41 33 11 27 36 10 89 11 | 53 50 41 21 29 37 24 26 23
R22 | 575 35 37 24 18 18 54 17 --- 11 | 53 55 39 43 31 24 26 --- 30
R23 | 655 38 35 23 24 14 30 9 --- 9 | 27 30 35 59 47 34 40 --- 41
R24 | 799 29 30 43 21 33 50 19 --- 14 | 55 55 68 55 37 32 48 --- 46
XR26 | ---- 105 752 --- --- --- --- 28 --- 55 | 98 649 --- --- --- --- 35 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1291 36 39 25 17 23 35 18 197 |T 55 82 47 48 46 43 39 32 40
WRMS | 1291 35 36 26 15 16 32 18 197 |NE 45 85 36 34 31 24 27 26 27
MEDI | 1031 37 39 23 17 19 31 16 89 |MD 53 55 40 39 37 32 35 29 30
Table 3.1893.5 GPS week: 1893 Day: 5 MJD: 57500
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 | 2209 61 62 20 18 25 24 17 --- 11 | 54 54 57 62 66 62 49 --- 54
R02 | 1267 26 25 19 13 14 24 10 --- 7 | 79 80 81 76 79 75 72 --- 75
R03 | 1055 36 36 14 14 18 24 14 101 8 | 56 53 56 51 53 50 47 21 49
R04 | 832 34 36 15 12 20 29 8 --- 7 | 58 59 62 57 66 70 55 --- 58
R05 | 763 31 26 39 22 26 53 24 --- 13 | 48 49 43 47 52 47 51 --- 42
R06 | 965 21 23 24 13 18 23 9 --- 7 | 31 35 34 35 39 33 32 --- 31
R07 | 769 40 34 13 9 17 24 8 325 7 | 61 62 55 54 60 55 51 24 53
R08 | 1544 30 35 21 16 20 33 15 --- 8 | 45 49 45 46 50 62 45 --- 44
R09 | 1987 22 21 16 12 14 29 12 --- 7 | 17 16 23 14 18 15 22 --- 15
XR10 | 1761 21 18 17 14 25 --- 16 --- 9 | 27 27 25 27 17 --- 20 --- 21
R13 | 1126 21 31 11 15 15 43 11 --- 8 | 27 34 19 31 36 15 27 --- 25
R14 | 789 51 46 55 13 15 51 11 --- 13 | 31 32 57 25 21 14 18 --- 20
R15 | 2923 39 44 21 14 45 74 8 --- 13 | 28 37 19 23 24 38 18 --- 15
R16 | 1338 33 43 16 16 28 63 14 --- 11 | 30 45 34 38 21 26 40 --- 30
R17 | 1198 34 30 29 11 23 28 14 --- 9 | 44 38 36 25 23 21 16 --- 20
R18 | 482 28 26 27 8 29 22 12 --- 8 | 37 35 30 25 26 21 22 --- 21
R19 | 758 35 34 14 12 13 12 17 --- 7 | 41 41 18 28 26 27 18 --- 21
R20 | 679 46 58 29 23 28 37 23 --- 12 | 54 66 39 28 32 23 27 --- 25
R21 | 488 48 48 29 13 18 31 14 120 10 | 41 41 30 21 22 32 20 24 17
R22 | 511 42 38 32 11 25 42 9 --- 10 | 42 39 34 23 32 23 18 --- 21
R23 | 2422 37 36 19 15 18 27 15 --- 8 | 20 23 30 34 25 21 35 --- 28
R24 | 1088 23 21 52 18 18 75 21 --- 14 | 47 60 86 57 50 24 39 --- 49
XR26 | ---- 100 203 --- --- --- --- 21 --- 46 | 115 240 --- --- --- --- 43 --- 54
------+---------------------------------------------------+-----------------------------------------------
RMS | 1366 37 38 27 15 22 40 14 208 |T 44 52 41 37 38 35 34 23 34
WRMS | 1366 36 37 28 13 22 39 14 208 |NE 40 51 34 28 26 23 25 24 25
MEDI | 1055 34 35 20 13 18 29 14 120 |MD 42 41 34 31 32 27 32 24 28
Table 3.1893.6 GPS week: 1893 Day: 6 MJD: 57501
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 | 2283 57 58 21 17 22 28 20 --- 11 | 73 74 65 69 73 72 59 --- 64
R02 | 1969 25 28 22 13 15 23 8 --- 7 | 80 85 79 80 81 81 71 --- 77
R03 | 1009 42 42 18 13 19 26 12 246 8 | 64 65 49 54 58 54 47 33 50
R04 | 869 39 37 14 12 15 19 7 --- 7 | 57 59 51 49 53 52 49 --- 49
R05 | 831 42 46 37 21 29 38 27 --- 13 | 59 65 60 53 62 45 58 --- 51
R06 | 1075 22 20 24 14 15 21 16 --- 8 | 41 40 38 40 38 36 38 --- 36
R07 | 759 36 41 14 17 11 29 9 332 7 | 51 53 43 39 43 45 41 34 39
R08 | 524 36 27 25 25 16 21 12 --- 9 | 50 50 41 39 45 45 47 --- 40
R09 | 2080 23 31 20 11 13 33 11 --- 7 | 25 27 22 20 25 26 25 --- 21
R10 | 1907 23 26 19 15 16 30 9 --- 7 | 38 43 28 35 24 27 18 --- 24
R13 | 1043 44 44 25 17 24 44 11 --- 10 | 47 42 36 36 26 26 21 --- 25
R14 | 1534 61 64 83 31 20 65 30 --- 20 | 43 57 39 45 38 14 17 --- 24
R15 | 2754 40 37 21 15 35 55 11 --- 12 | 41 39 33 38 46 15 23 --- 28
R16 | 1514 16 35 48 26 19 43 19 --- 12 | 41 49 39 41 27 20 34 --- 30
R17 | 1174 38 39 28 15 13 33 17 --- 9 | 63 63 51 41 32 29 23 --- 32
R18 | 562 34 34 26 11 19 15 12 --- 8 | 58 56 43 39 27 25 25 --- 31
R19 | 854 52 51 15 10 21 17 8 --- 8 | 71 72 36 41 37 29 28 --- 34
R20 | 619 44 54 30 28 16 39 25 --- 12 | 73 81 58 50 35 34 40 --- 41
R21 | 573 45 51 30 16 29 19 18 182 11 | 68 72 52 42 33 28 29 49 35
R22 | 1003 51 51 38 10 26 17 12 --- 10 | 68 69 52 37 35 31 29 --- 34
R23 | 2839 37 42 26 20 13 36 11 --- 9 | 28 32 35 49 40 37 43 --- 39
R24 | 1384 31 35 41 20 18 69 20 --- 13 | 76 85 80 69 57 25 53 --- 57
XR26 | ---- 117 101 --- --- --- --- 25 --- 55 | 111 92 --- --- --- --- 27 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1492 40 42 32 18 20 36 16 261 |T 57 59 46 45 42 36 36 38 38
WRMS | 1492 38 39 28 16 19 41 16 261 |NE 56 58 43 41 34 26 29 49 32
MEDI | 1043 39 41 25 15 18 29 12 246 |MD 58 59 43 41 38 29 34 34 35
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