[IGSREPORT-24560] Wk 1901 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Jun 30 16:50:22 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1901 (Jun 12, 2016 - Jun 18, 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 2.1901.
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:
igl1901[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1901 in the SP3 format.
igl19017.sum Combination Report for GPS Week 1901.
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 | -6.0 ns
1 | -5.1 ns
2 | -4.1 ns
3 | -4.3 ns
4 | -3.5 ns
5 | -5.4 ns
6 | -6.2 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 1.1901, 1a.1901).
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 2.1901.0-6)
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 3.1901.0-6).
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 1901 summary. (Jun 12, 2016 - Jun 18, 2016)
Table 1.1901.a GPS week : 1901 MJD: 57551.0-57557.0
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 2 54 -51 22 .17 32 25 | --- --- --- ---
| 1 1 1 23 22 48 .05 | --- ---
cof n/a| -1 0 1 38 -39 28 .16 36 28 | --- --- --- ---
| 1 1 2 30 28 65 .04 | --- ---
emx n/a| 0 0 5 -53 -25 -56 .10 27 26 | -5037 30 4076 8502
| 1 2 1 33 21 31 .05 | 8169 904
esx n/a| 0 0 0 -22 0 13 -.09 19 16 | -10006 -146 4035 9744
| 0 1 1 36 26 22 .02 | 2372 1898
gfz n/a| 0 0 0 54 47 54 .00 24 17 | 0 -544 3596 7637
| 1 1 1 29 38 43 .04 | 0 1696
grg n/a| 0 0 -3 -27 64 -31 -.27 35 31 | -4922 -96 4042 8398
| 1 1 6 36 20 46 .04 | 1567 1666
iac n/a| 1 0 -1 -11 -35 -18 .07 20 20 | -3687 -521 4072 8256
| 1 0 2 56 53 70 .05 | 1109 1034
mcc n/a| -4 1 16 -30 -49 596 .04 157 157 | --- --- --- ---
| 8 9 12 104 103 495 .52 | --- ---
Table 1.1901.b GPS week : 1901 MJD: 57551.0-57557.0
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 10 9 9 9 10 9 |
R02 | 6 8 9 8 6 8 10 |
R03 | 7 7 7 7 8 6 7 |
R04 | 7 9 7 7 6 7 8 |
R05 | 11 16 16 15 15 12 14 |
R06 | 9 10 12 9 9 9 9 |
R07 | 9 12 9 7 8 7 6 |
R08 | 9 9 8 8 9 8 7 |
R09 | 8 8 8 8 5 7 8 |
R10 | 7 10 10 9 8 8 9 |
R12 | 25 29 24 38 23 21 21 |
R13 | 11 10 12 10 10 10 12 |
R14 | 17 17 17 19 14 15 19 |
R15 | 8 9 9 27 9 10 10 |
R16 | 11 16 12 17 17 12 12 |
R17 | 9 9 9 9 7 8 8 |
R18 | 9 8 9 8 7 9 7 |
R19 | 9 10 9 9 8 9 8 |
R20 | 14 14 14 12 11 11 12 |
R21 | 7 8 10 9 8 8 9 |
R22 | 9 8 10 14 8 7 9 |
R23 | 9 10 8 11 9 10 8 |
R24 | 11 11 11 11 13 14 12 |
Table 1.1901.c GPS week : 1901 MJD: 57551.0-57557.0
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 1901 0 | -124 4 185 -846 -751 -1131 83.8 1517 1517 | -5984 0
brd 1901 1 | 13 15 280 1181 -1055 -2931 85.1 3002 3002 | -5144 0
brd 1901 2 | 37 -36 320 -215 -439 -5068 83.5 1449 1449 | -4146 0
brd 1901 3 | -55 17 266 227 -530 -3102 84.7 1850 1850 | -4290 0
brd 1901 4 | -1 -51 206 123 -870 2809 84.1 1324 1324 | -3486 0
brd 1901 5 | 19 -101 147 941 -1916 4316 85.8 1332 1332 | -5364 0
brd 1901 6 | 42 6 159 1044 -507 4575 83.7 1335 1335 | -6189 0
-------------+------------------------------------------------------------+----------------
brd 1901 mean| -9 -20 223 350 -867 -75 84.4 1687 1687 | -4943 0
brd 1901 sdev| 60 44 65 746 512 3928 .8 608 608 | 1003 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 2.1901.0 GPS week: 1901 Day: 0 MJD: 57551
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 3 25 -75 18 .14 33 24 | --- --- --- ---
cof n/a| -5 0 4 22 -69 13 .22 34 23 | --- --- --- ---
emx n/a| 0 0 5 -96 -31 -113 .10 26 26 | -490 -181 4273 9606
esx n/a| 1 0 0 0 -25 -13 -.09 17 13 | -11193 -998 4264 10191
gfz n/a| 1 1 -1 5 -17 31 .05 23 18 | 0 -2520 3349 8269
grg n/a| 0 1 3 3 95 21 -.26 33 30 | -5318 -748 4278 9531
iac n/a| 2 -1 -3 34 54 60 .09 20 20 | -3334 -1330 4270 9558
mcc n/a| -10 4 16 115 -105 755 .44 186 186 | --- --- --- ---
Table 2.1901.1 GPS week: 1901 Day: 1 MJD: 57552
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 3 24 -22 71 .13 35 27 | --- --- --- ---
cof n/a| -1 2 1 13 -3 111 .18 36 28 | --- --- --- ---
emx n/a| -3 -2 6 -90 -50 -29 .14 32 31 | -15768 -571 4322 9891
esx n/a| 0 -1 -1 -92 10 32 -.08 20 18 | -8834 -617 4345 10978
gfz n/a| 0 0 0 46 56 140 -.02 24 18 | 0 -932 4013 8519
grg n/a| 1 -1 -1 -27 55 -12 -.27 33 32 | -4303 -1592 4341 9880
iac n/a| 0 1 1 92 -72 -164 .07 22 22 | -3408 -1113 4342 9913
mcc n/a| 4 -8 0 17 -156 103 .06 186 186 | --- --- --- ---
Table 2.1901.2 GPS week: 1901 Day: 2 MJD: 57553
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 0 54 -27 11 .23 33 27 | --- --- --- ---
cof n/a| 0 1 0 32 -14 34 .13 39 31 | --- --- --- ---
emx n/a| -1 -3 5 -63 -17 -29 .10 25 25 | -166 29 3491 6462
esx n/a| -1 0 -2 -10 -12 -13 -.07 19 17 | -11475 769 3480 7999
gfz n/a| 0 0 0 54 49 61 .05 24 18 | 0 -64 3365 6163
grg n/a| -2 -2 0 15 65 1 -.27 36 30 | -4063 -30 3499 6229
iac n/a| 0 0 0 -24 -62 -11 .00 20 20 | -2913 -66 3484 6108
mcc n/a| 7 -10 0 68 -108 161 -.66 151 151 | --- --- --- ---
Table 2.1901.3 GPS week: 1901 Day: 3 MJD: 57554
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 3 84 -43 -44 .13 36 28 | --- --- --- ---
cof n/a| 0 -2 -2 84 -33 -65 .15 41 33 | --- --- --- ---
emx n/a| 0 0 2 -2 -1 -74 .19 30 29 | -6907 -1260 3973 7207
esx n/a| 0 1 -1 17 -27 5 -.10 29 20 | -5059 -3846 3757 8549
gfz n/a| 0 0 3 30 26 58 .04 38 16 | 0 -2172 3651 6929
grg n/a| 1 0 -7 -53 88 -14 -.33 41 31 | -3181 -2413 3743 7006
iac n/a| 0 0 0 -53 -17 19 .01 19 19 | -2243 -2140 3938 6983
mcc n/a| -11 0 19 -32 -126 280 -.32 141 141 | --- --- --- ---
Table 2.1901.4 GPS week: 1901 Day: 4 MJD: 57555
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 2 79 -64 -24 .17 29 22 | --- --- --- ---
cof n/a| -1 -1 4 54 -74 -38 .10 38 26 | --- --- --- ---
emx n/a| 1 2 5 -53 -17 -50 .05 26 25 | 8364 -158 3545 9299
esx n/a| 0 -3 0 -6 -15 36 -.11 18 14 | -10670 666 3469 10742
gfz n/a| -1 -1 0 72 49 35 -.05 18 13 | 0 -573 3388 7977
grg n/a| 0 0 2 -85 44 -116 -.28 37 31 | -3653 286 3487 9347
iac n/a| 1 0 -2 -60 -4 12 .11 20 20 | -3569 201 3493 8822
mcc n/a| -4 3 30 -81 62 552 -.04 140 140 | --- --- --- ---
Table 2.1901.5 GPS week: 1901 Day: 5 MJD: 57556
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 55 -50 31 .23 29 23 | --- --- --- ---
cof n/a| 0 -1 1 -2 -21 40 .20 36 27 | --- --- --- ---
emx n/a| 1 0 6 -23 0 -29 .04 26 25 | -11819 895 5041 9396
esx n/a| 0 0 0 -20 23 38 -.08 16 13 | -11472 1333 5037 10818
gfz n/a| -1 -2 0 80 113 1 -.02 21 16 | 0 -202 3918 8467
grg n/a| -1 2 -5 -48 48 -35 -.28 32 29 | -6513 1452 5034 9203
iac n/a| 0 0 -2 -13 -112 -29 .13 19 19 | -5359 -29 5039 8916
mcc n/a| 1 0 30 -144 -30 785 -.11 126 126 | --- --- --- ---
Table 2.1901.6 GPS week: 1901 Day: 6 MJD: 57557
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 1 0 60 -80 89 .19 30 25 | --- --- --- ---
cof n/a| -2 0 2 62 -58 100 .15 31 26 | --- --- --- ---
emx n/a| -1 2 7 -42 -55 -71 .09 25 22 | -8477 1462 3891 7659
esx n/a| 0 -2 3 -48 42 10 -.07 17 15 | -11339 1670 3894 8931
gfz n/a| 0 0 3 90 54 56 -.03 23 18 | 0 2651 3492 7140
grg n/a| -1 -1 -13 3 54 -65 -.20 32 34 | -7429 2372 3916 7596
iac n/a| 2 0 -1 -52 -32 -18 .07 19 19 | -4987 829 3940 7496
mcc n/a| -15 18 21 -158 117 1534 .93 169 169 | --- --- --- ---
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 3.1901.0 GPS week: 1901 Day: 0 MJD: 57551
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 | 1498 26 22 37 32 21 40 18 --- 13 | 49 48 45 46 46 61 40 --- 39
R02 | 1777 11 15 15 8 20 15 13 --- 6 | 49 51 41 38 38 40 39 --- 38
R03 | 1287 13 14 12 10 11 33 15 66 7 | 64 65 54 52 52 58 47 165 52
R04 | 635 16 21 14 12 11 28 17 --- 7 | 48 54 49 45 47 40 37 --- 42
R05 | 618 31 25 27 12 12 46 19 --- 11 | 37 39 52 48 39 26 42 --- 39
R06 | 577 19 19 23 13 13 37 19 --- 9 | 43 39 43 33 39 34 31 --- 34
R07 | 853 18 18 23 9 19 22 27 287 9 | 57 56 62 51 53 34 31 192 46
R08 | 771 29 30 20 8 17 14 25 --- 8 | 56 59 58 42 46 41 38 --- 44
R09 | 2413 12 16 26 13 16 24 18 --- 8 | 22 24 26 28 26 25 29 --- 22
R10 | 949 15 20 17 9 23 21 12 --- 7 | 46 44 40 47 37 37 43 --- 40
R12 | 746 100 99 55 26 51 66 36 --- 24 | 92 92 44 38 44 43 33 --- 31
R13 | 1531 42 31 20 13 23 27 19 --- 10 | 70 65 48 43 30 50 33 --- 40
R14 | 996 38 40 38 36 34 58 27 --- 17 | 38 43 40 64 54 39 37 --- 38
XR15 | 7728 12 19 19 20 --- 16 11 --- 8 | 33 43 39 46 --- 36 36 --- 37
R16 | 780 16 20 35 22 18 37 21 --- 11 | 45 52 39 50 39 41 44 --- 40
R17E | 719 31 25 24 11 18 20 12 --- 8 | 48 44 29 35 36 35 31 --- 32
R18E | 844 31 26 24 11 19 20 19 --- 9 | 41 41 33 31 29 24 35 --- 28
R19E | 3697 33 29 19 9 23 18 13 --- 8 | 52 51 31 33 33 33 33 --- 31
R20E | 1971 35 41 33 22 26 46 27 --- 13 | 51 56 31 44 43 46 40 --- 36
R21E | 868 19 18 19 10 18 21 12 128 7 | 37 34 30 30 31 32 38 139 29
R22E | 2185 24 23 17 10 29 23 12 --- 8 | 34 33 19 30 43 31 27 --- 25
R23E | 1284 21 31 20 14 22 20 22 --- 8 | 36 49 38 38 42 26 36 --- 34
R24E | 1973 32 48 18 21 33 28 20 --- 11 | 48 67 33 39 39 39 38 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1516 33 34 26 17 23 33 20 186 |T 47 49 40 41 40 37 36 165 36
WRMS | 1516 24 23 26 13 18 30 20 186 |NE 49 51 45 44 42 40 37 178 38
MEDI | 996 24 23 20 12 19 24 19 128 |MD 48 49 40 42 39 37 37 165 37
Table 3.1901.1 GPS week: 1901 Day: 1 MJD: 57552
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 | 1360 20 30 24 19 21 28 20 --- 9 | 34 47 30 38 39 41 23 --- 28
R02 | 975 19 13 20 24 10 16 12 --- 8 | 40 32 34 29 32 32 28 --- 27
R03 | 941 9 7 18 15 8 25 10 243 6 | 44 41 42 47 43 45 35 110 40
R04 | 2757 13 17 20 12 13 38 12 --- 8 | 38 37 35 37 32 33 34 --- 31
R05 | 2720 37 35 20 29 27 61 31 --- 15 | 42 42 35 57 51 32 23 --- 34
R06 | 800 27 22 24 17 15 28 23 --- 10 | 34 36 46 36 31 27 16 --- 26
R07 | 1456 22 19 37 15 15 35 33 137 12 | 34 30 50 29 21 28 12 109 20
R08 | 1019 16 28 26 16 18 23 20 --- 9 | 43 57 52 39 41 51 23 --- 37
R09 | 3933 15 18 27 23 12 14 14 --- 8 | 31 41 28 48 42 38 28 --- 34
R10 | 4153 14 18 19 25 16 19 27 --- 9 | 36 44 38 50 44 34 35 --- 37
R12 | 1473 107 101 93 35 56 55 33 --- 29 | 84 86 95 40 59 38 38 --- 37
R13 | 2165 31 43 17 14 24 21 22 --- 9 | 47 56 41 43 33 44 30 --- 35
R14 | 6472 40 30 45 33 39 48 27 --- 17 | 39 44 49 58 52 39 32 --- 35
XR15 |10248 12 20 16 19 --- 19 14 --- 8 | 31 32 37 39 --- 37 32 --- 32
R16 | 4344 20 22 33 31 31 64 29 --- 16 | 34 42 42 52 42 54 38 --- 36
R17E | 1218 31 34 19 10 26 22 10 --- 9 | 51 52 42 42 45 45 33 --- 38
R18E | 1093 33 33 19 9 18 21 12 --- 8 | 45 46 37 40 42 40 34 --- 35
R19E | 3882 31 29 28 11 20 21 21 --- 9 | 52 55 33 39 43 30 28 --- 34
R20E | 3754 44 40 31 17 33 33 32 --- 14 | 48 50 39 35 44 34 34 --- 30
R21E | 3955 21 27 22 12 17 22 16 162 8 | 43 47 31 33 33 42 33 95 32
R22E | 2938 21 27 16 9 21 21 12 --- 7 | 40 43 37 43 45 53 37 --- 39
R23E | 2975 24 26 26 18 19 24 17 --- 9 | 39 42 41 43 41 41 29 --- 34
R24E | 3232 40 53 22 18 22 27 20 --- 11 | 54 78 55 48 53 55 47 --- 47
------+---------------------------------------------------+-----------------------------------------------
RMS | 3002 35 36 32 20 24 33 22 186 |T 42 46 42 41 41 39 30 104 33
WRMS | 3002 27 28 31 18 18 32 22 186 |NE 40 44 43 42 40 38 28 109 32
MEDI | 2757 22 27 22 17 19 24 20 162 |MD 40 44 39 40 42 39 32 109 34
Table 3.1901.2 GPS week: 1901 Day: 2 MJD: 57553
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 | 1028 20 27 12 19 17 44 13 --- 9 | 39 50 47 48 53 69 52 --- 47
R02 | 632 21 33 24 14 11 25 19 --- 8 | 47 61 55 37 44 38 24 --- 38
R03 | 1386 22 30 16 18 13 21 9 176 7 | 48 54 36 32 36 38 31 65 33
R04 | 552 13 17 14 10 13 34 14 --- 7 | 37 42 39 32 37 29 34 --- 32
R05 | 1448 21 22 38 26 21 71 33 --- 15 | 26 34 50 45 40 36 33 --- 32
R06 | 922 33 30 21 24 21 41 17 --- 11 | 36 39 41 39 45 29 32 --- 31
R07 | 775 16 21 17 12 10 45 18 163 9 | 41 46 46 41 41 27 27 83 34
R08 | 1136 11 10 21 15 20 30 13 --- 8 | 43 42 55 41 36 64 46 --- 44
R09 | 2390 13 14 19 9 17 31 14 --- 7 | 23 20 28 25 24 25 27 --- 21
R10 | 1777 21 28 23 21 26 26 19 --- 10 | 47 46 40 51 33 35 41 --- 38
R12 | 1478 100 118 44 22 57 58 37 --- 24 | 83 101 50 61 51 82 27 --- 36
R13 | 665 45 47 20 18 31 20 18 --- 11 | 60 64 38 36 28 40 36 --- 32
R14 | 1336 31 39 44 38 37 48 25 --- 16 | 32 35 29 65 45 32 41 --- 34
XR15 |10273 19 21 20 18 --- 20 15 --- 9 | 30 33 34 36 --- 27 29 --- 28
R16 | 1147 23 23 20 25 30 38 20 --- 11 | 31 41 46 46 40 51 43 --- 36
R17E | 883 23 48 17 11 21 30 17 --- 8 | 47 65 34 35 36 52 35 --- 34
R18E | 1192 31 32 19 14 16 18 16 --- 8 | 42 45 31 32 30 34 35 --- 29
R19E | 2487 32 36 26 10 18 18 14 --- 9 | 44 47 32 31 32 29 28 --- 28
R20E | 3297 37 49 40 18 26 31 30 --- 13 | 46 55 37 35 40 41 35 --- 30
R21E | 965 26 25 23 16 19 23 22 103 9 | 43 40 27 36 39 40 35 59 31
R22E | 1118 29 20 20 15 23 29 20 --- 10 | 43 43 22 30 31 42 34 --- 27
R23E | 779 23 23 15 18 11 21 14 --- 7 | 27 30 30 39 31 39 31 --- 29
R24E | 993 28 32 27 19 24 33 22 --- 11 | 47 52 47 44 51 54 37 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1448 33 39 25 19 24 36 20 151 |T 41 47 38 39 38 41 34 69 33
WRMS | 1448 27 31 25 17 18 30 20 151 |NE 41 47 42 42 39 41 34 74 34
MEDI | 1136 23 28 20 18 20 30 18 163 |MD 43 45 38 37 37 38 34 65 32
Table 3.1901.3 GPS week: 1901 Day: 3 MJD: 57554
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 | 1185 20 22 17 22 13 34 12 --- 8 | 46 38 37 43 48 40 50 --- 41
R02 | 630 18 24 18 8 21 26 10 --- 7 | 49 53 49 40 50 41 37 --- 42
R03 | 1535 13 19 12 12 13 32 10 132 6 | 62 59 49 58 59 63 48 40 54
R04 | 764 16 20 11 14 8 33 10 --- 7 | 50 51 36 50 43 38 37 --- 40
R05 | 1213 19 23 40 27 17 67 25 --- 14 | 47 49 65 52 50 58 38 --- 44
R06 | 900 30 31 24 15 10 33 11 --- 9 | 47 43 51 49 48 55 40 --- 45
R07 | 1692 19 26 14 16 15 20 15 198 7 | 55 56 51 52 61 54 42 59 50
R08 | 1029 8 14 16 18 9 43 8 --- 8 | 47 48 53 50 55 37 53 --- 47
R09 | 1841 13 22 17 11 12 29 18 --- 7 | 33 42 27 36 41 41 32 --- 31
R10 | 909 15 35 20 18 22 28 19 --- 9 | 49 70 44 59 43 48 38 --- 43
R12 | 1082 111 112 48 105 73 113 50 --- 37 | 101 103 59 101 41 138 33 --- 43
R13 | 743 44 57 20 12 21 21 10 --- 10 | 67 78 45 47 43 59 43 --- 46
R14 | 1307 44 49 69 42 33 43 22 --- 19 | 46 69 53 68 48 46 46 --- 42
R15 | 6132 30 32 28 29 138 41 24 --- 27 | 31 31 34 39 25 41 33 --- 36
R16 | 1049 24 31 58 33 29 56 19 --- 16 | 43 48 50 61 45 60 50 --- 43
R17E | 1673 24 20 19 17 23 25 14 --- 8 | 55 50 38 43 40 37 35 --- 37
R18E | 1062 24 38 28 11 16 21 13 --- 8 | 39 52 33 33 29 37 32 --- 30
R19E | 3067 34 31 23 13 21 17 15 --- 9 | 53 50 33 34 34 35 30 --- 32
R20E | 1490 37 30 27 18 30 32 23 --- 12 | 50 48 25 34 40 46 36 --- 30
R21E | 1133 25 20 23 11 22 21 15 55 8 | 46 50 35 41 43 43 40 40 38
R22E | 1028 55 69 32 17 24 37 17 --- 13 | 59 70 28 35 37 44 32 --- 28
R23E | 1419 35 43 22 24 14 28 21 --- 10 | 43 47 34 59 47 38 39 --- 40
R24E | 1209 25 35 29 19 20 30 20 --- 10 | 46 56 49 52 57 36 38 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1849 36 41 30 29 38 41 19 141 |T 50 54 42 49 44 49 39 46 40
WRMS | 1849 28 33 29 20 16 31 19 141 |NE 51 55 46 53 46 54 41 49 43
MEDI | 1185 24 31 23 17 21 32 15 132 |MD 47 50 44 49 43 43 38 40 41
Table 3.1901.4 GPS week: 1901 Day: 4 MJD: 57555
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 | 1245 24 38 16 17 13 44 15 --- 9 | 39 62 31 49 40 47 45 --- 37
R02 | 795 13 8 12 8 7 24 18 --- 6 | 41 38 33 40 47 44 35 --- 38
R03 | 1577 15 17 19 15 15 35 13 122 8 | 53 59 61 58 48 45 52 29 51
R04 | 1016 11 14 9 9 10 19 16 --- 5 | 48 47 45 40 51 60 39 --- 44
R05 | 855 18 22 39 20 14 73 36 --- 14 | 38 39 67 46 37 41 26 --- 36
R06 | 807 24 23 15 8 11 37 22 --- 8 | 43 47 45 31 36 45 38 --- 35
R07 | 1457 11 12 11 10 9 42 16 203 7 | 51 51 48 52 54 91 49 48 53
R08 | 970 12 12 25 16 21 31 14 --- 8 | 49 44 47 49 53 50 40 --- 44
R09 | 1860 12 13 10 8 10 16 9 --- 4 | 26 23 21 29 34 35 27 --- 27
R10 | 670 13 21 15 19 18 24 15 --- 7 | 43 39 35 46 36 47 38 --- 38
R12 | 1019 82 101 54 40 34 58 43 --- 22 | 87 106 42 50 45 69 41 --- 42
R13 | 884 43 50 20 12 20 27 13 --- 10 | 58 65 35 34 32 40 31 --- 32
R14 | 1524 32 34 44 26 19 43 21 --- 13 | 46 55 38 47 38 26 38 --- 33
XR15 | 4878 12 23 22 15 --- 21 14 --- 8 | 35 34 36 27 --- 29 39 --- 31
R16 | 703 36 53 50 30 24 67 29 --- 16 | 53 71 33 47 34 38 46 --- 31
R17E | 1200 18 24 17 13 17 15 12 --- 6 | 45 47 36 37 44 35 37 --- 37
R18E | 913 17 22 17 10 16 19 14 --- 6 | 36 40 32 33 35 41 33 --- 32
R19E | 1793 25 44 24 10 18 16 15 --- 8 | 47 62 48 39 42 40 37 --- 38
R20E | 1333 32 55 21 19 27 30 19 --- 11 | 52 69 36 37 41 45 35 --- 34
R21E | 773 24 34 26 9 18 16 17 51 8 | 45 49 33 36 42 40 42 32 36
R22E | 785 27 38 23 11 16 20 13 --- 8 | 42 50 30 38 39 33 34 --- 32
R23E | 3102 27 33 21 20 11 28 16 --- 9 | 36 45 38 42 36 41 36 --- 34
XR24E | 1274 32 27 24 25 --- 34 20 --- 13 | 36 49 36 49 --- 46 33 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1324 29 38 26 18 18 37 20 140 |T 45 51 39 41 41 44 37 36 36
WRMS | 1324 22 26 25 14 13 31 20 140 |NE 47 52 41 43 41 47 38 38 38
MEDI | 1019 24 24 21 15 16 28 16 122 |MD 45 49 36 40 40 41 38 32 36
Table 3.1901.5 GPS week: 1901 Day: 5 MJD: 57556
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 | 762 18 18 31 20 18 24 16 --- 9 | 36 34 22 43 42 36 25 --- 29
R02 | 1181 13 24 18 7 9 44 12 --- 8 | 27 38 29 29 35 30 28 --- 24
R03 | 2256 17 13 15 7 14 21 10 137 6 | 41 29 44 35 36 21 37 21 34
R04 | 1289 10 16 13 7 19 25 16 --- 6 | 35 34 48 48 57 29 33 --- 41
R05 | 2264 28 35 28 15 17 44 28 --- 11 | 41 58 47 39 48 32 31 --- 35
R06 | 863 28 32 29 11 15 25 19 --- 9 | 31 30 23 38 31 48 43 --- 32
R07 | 1252 15 20 17 9 10 24 16 162 6 | 43 46 44 41 37 47 35 47 39
R08 | 1133 21 23 17 14 13 20 16 --- 7 | 33 37 33 32 38 39 28 --- 30
R09 | 1670 15 25 13 11 18 22 16 --- 7 | 21 34 19 28 34 34 19 --- 21
R10 | 819 11 22 15 22 21 22 12 --- 8 | 29 44 37 54 34 38 33 --- 36
R12 | 969 85 104 44 17 42 63 34 --- 21 | 75 97 36 60 53 46 43 --- 38
R13 | 1316 38 28 23 14 16 23 24 --- 10 | 50 45 31 33 35 39 25 --- 31
R14 | 1044 34 46 42 26 34 43 28 --- 15 | 31 53 37 37 58 25 32 --- 29
XR15 | 3662 17 12 21 22 --- 28 13 --- 10 | 23 27 34 38 --- 31 29 --- 28
R16 | 1144 28 52 35 19 22 33 26 --- 12 | 52 68 28 42 48 39 39 --- 35
R17E | 1043 23 23 21 11 18 20 9 --- 7 | 43 45 30 39 42 32 35 --- 34
R18E | 986 14 19 22 12 15 47 12 --- 9 | 24 31 26 25 29 45 27 --- 23
R19E | 1215 19 25 21 15 23 22 16 --- 8 | 43 47 44 35 36 43 34 --- 34
R20E | 2078 33 50 25 18 21 22 25 --- 10 | 54 69 41 42 40 40 38 --- 36
R21E | 710 24 28 21 11 17 20 12 54 7 | 39 42 29 36 40 35 34 31 32
R22E | 1089 25 27 21 9 15 17 12 --- 7 | 33 34 27 27 34 31 28 --- 24
R23E | 1539 24 27 25 21 17 28 13 --- 9 | 34 48 31 37 34 33 30 --- 29
R24E | 1043 33 31 39 24 36 41 24 --- 14 | 33 42 41 51 50 37 31 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1331 29 36 26 16 21 32 19 126 |T 37 44 33 38 40 36 32 33 31
WRMS | 1331 23 27 25 13 16 29 19 126 |NE 37 44 34 39 41 35 32 34 32
MEDI | 1144 23 25 21 14 17 24 16 137 |MD 35 42 33 38 37 36 32 31 32
Table 3.1901.6 GPS week: 1901 Day: 6 MJD: 57557
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 | 996 21 23 19 16 13 36 16 --- 9 | 43 48 41 46 49 70 46 --- 44
R02 | 883 27 19 18 18 24 18 20 --- 9 | 49 46 37 41 43 31 32 --- 35
R03 | 2805 16 19 10 9 12 21 21 201 7 | 69 70 65 62 64 54 50 42 59
R04 | 952 14 16 16 17 11 31 10 --- 7 | 56 58 63 56 58 51 47 --- 53
R05 | 2077 35 20 18 14 29 65 21 --- 14 | 62 67 83 71 77 42 65 --- 65
R06 | 1175 28 31 16 10 14 23 23 --- 8 | 46 49 40 49 53 35 52 --- 45
R07 | 1649 12 22 19 11 9 15 16 153 6 | 64 67 57 63 62 51 59 57 59
R08 | 704 8 11 16 13 12 23 14 --- 6 | 55 56 58 59 51 58 48 --- 53
R09 | 1458 20 23 14 13 15 31 12 --- 7 | 26 31 20 26 34 46 25 --- 25
R10 | 814 20 23 18 27 16 25 13 --- 9 | 44 45 31 52 38 45 39 --- 39
R12 | 731 86 77 41 24 40 49 37 --- 21 | 81 87 51 30 48 43 41 --- 30
R13 | 1053 39 43 31 13 28 35 13 --- 12 | 65 67 32 37 32 46 33 --- 34
R14 | 1044 41 23 48 33 57 51 27 --- 19 | 41 50 36 49 68 33 43 --- 37
XR15 | 8582 12 18 18 26 --- 26 13 --- 10 | 34 33 37 46 --- 34 37 --- 35
R16 | 914 26 40 39 21 21 30 20 --- 11 | 48 63 27 46 39 40 47 --- 37
R17E | 1537 18 21 15 11 22 22 17 --- 7 | 49 49 32 40 51 31 34 --- 37
R18E | 836 13 27 16 14 13 17 15 --- 6 | 31 42 29 28 31 27 34 --- 27
R19E | 1005 26 25 18 13 16 18 13 --- 7 | 40 37 28 32 33 32 28 --- 29
R20E | 1177 29 26 30 15 27 31 25 --- 11 | 51 52 43 58 62 40 52 --- 47
R21E | 935 22 18 24 13 21 18 15 147 8 | 40 38 28 31 38 29 34 45 30
R22E | 2068 22 23 25 8 26 21 16 --- 8 | 33 35 28 30 35 24 30 --- 26
R23E | 1482 20 29 23 15 11 23 13 --- 8 | 34 44 27 35 31 35 35 --- 29
R24E | 741 26 51 29 29 22 35 24 --- 12 | 33 65 42 50 33 28 36 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1334 30 31 25 17 23 32 19 169 |T 47 52 40 45 46 40 41 48 39
WRMS | 1334 25 26 22 15 18 34 19 169 |NE 52 55 45 48 51 45 44 49 43
MEDI | 1044 22 23 18 14 16 25 16 153 |MD 46 49 37 46 43 40 39 45 37
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