[IGSREPORT-23977] Wk 1865 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Oct 23 19:20:08 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1865 (Oct 04, 2015 - Oct 10, 2015)
Contact: igs.acc at noaa.gov
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 2.1865.
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:
igl1865[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1865 in the SP3 format.
igl18657.sum Combination Report for GPS Week 1865.
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 | -1.7 ns
1 | 4.1 ns
2 | 9.5 ns
3 | 2.7 ns
4 | 6.8 ns
5 | 8.4 ns
6 | 6.2 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESX | R13
1 | ESX | R13
1 | GRG | R19
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 1.1865, 1a.1865).
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 2.1865.0-6)
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 3.1865.0-6).
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 1865 summary. (Oct 04, 2015 - Oct 10, 2015)
Table 1.1865.a GPS week : 1865 MJD: 57299.0-57305.0
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| -1 0 2 31 4 -49 .28 49 49 | --- --- --- ---
| 2 1 3 31 25 41 .04 | --- ---
cof n/a| -1 0 5 39 3 -40 .34 51 50 | --- --- --- ---
| 2 1 3 37 24 55 .06 | --- ---
emx n/a| -1 -1 -2 -34 -60 -51 .28 27 28 | 1812 -1439 4210 7760
| 1 1 1 23 16 31 .01 | 8005 1612
esx n/a| 0 -1 2 -67 27 -70 -.06 19 18 | 0 -518 4477 8618
| 1 0 3 17 15 38 .04 | 0 1429
gfz n/a| -1 0 -6 29 60 79 -.04 20 15 | -283508 -3003 83670 290708
| 1 1 1 18 23 43 .05 | 489466 3661
grg n/a| 0 0 -3 9 -37 -80 -.38 43 37 | -686599 -2125 289630 774443
| 1 3 4 38 32 70 .02 | 214102 2514
iac n/a| 3 0 3 42 -36 70 -.09 19 19 | -279640 -1294 288732 291190
| 1 1 1 20 28 64 .05 | 492102 1758
mcc n/a| 0 0 85 156 -132 -97 -.57 249 249 | --- --- --- ---
| 10 10 24 216 108 219 .45 | --- ---
Table 1.1865.b GPS week : 1865 MJD: 57299.0-57305.0
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 | 12 15 15 13 13 13 15 |
R02 | 8 7 11 10 8 9 8 |
R03 | 8 9 8 8 9 11 8 |
R04 | 8 13 8 9 10 11 8 |
R05 | 12 14 12 13 13 11 13 |
R06 | 11 9 8 9 10 8 9 |
R07 | 9 8 16 11 9 10 9 |
R08 | 10 10 10 11 9 9 11 |
R09 | 15 13 14 11 11 14 11 |
R10 | 9 8 8 10 8 9 9 |
R11 | 22 22 21 21 22 21 19 |
R12 | 25 21 21 22 18 18 20 |
R13 | 17 18 15 14 14 12 11 |
R14 | 12 13 14 14 16 16 15 |
R15 | 10 8 13 12 10 11 12 |
R16 | 11 11 8 10 10 9 11 |
R17 | 11 9 13 11 15 17 16 |
R18 | 9 6 6 9 8 7 8 |
R19 | 8 7 6 7 8 7 8 |
R20 | 12 10 11 11 12 14 12 |
R21 | 9 9 8 8 8 8 9 |
R22 | 10 11 9 9 10 7 7 |
R23 | 7 9 8 10 10 9 7 |
R24 | 14 12 13 14 11 12 12 |
R26 | 0 0 0 0 0 0 0 |
Table 1.1865.c GPS week : 1865 MJD: 57299.0-57305.0
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 1865 0 | -63 70 -102 -671 89 3165 86.1 1511 1511 | -1684 0
brd 1865 1 | -45 -17 -93 150 -153 4188 87.3 1556 1556 | 4072 0
brd 1865 2 | 24 65 26 -909 695 4774 86.3 1632 1632 | 9465 0
brd 1865 3 | 35 26 31 380 -290 2536 85.8 1636 1636 | 2698 0
brd 1865 4 | 10 62 110 -322 -353 2577 84.4 1340 1340 | 6817 0
brd 1865 5 | 15 75 27 -2093 -54 4566 86.4 1510 1510 | 8434 0
brd 1865 6 | -33 -9 58 594 1036 656 85.7 1620 1620 | 6212 0
-------------+------------------------------------------------------------+----------------
brd 1865 mean| -8 39 8 -409 138 3208 86.0 1543 1543 | 5144 0
brd 1865 sdev| 38 39 78 922 527 1450 .9 104 104 | 3812 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 2.1865.0 GPS week: 1865 Day: 0 MJD: 57299
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 4 91 -19 -29 .25 45 36 | --- --- --- ---
cof n/a| 1 1 8 83 -9 -27 .33 49 37 | --- --- --- ---
emx n/a| -3 -1 -3 -11 -61 -21 .28 27 28 | -3100 -1234 3759 6609
esx n/a| 0 -1 2 -54 26 -76 -.08 23 18 | 0 -1847 4678 8022
gfz n/a| -2 1 -6 6 22 102 .03 20 16 | -999999 -7977 306361 999999
grg n/a| 1 3 -5 43 -9 -45 -.42 40 38 | -999999 -3973 999999 999999
iac n/a| 2 -1 5 34 -18 37 -.16 21 21 | -999999 -2654 999999 999999
mcc n/a| -18 1 55 125 -19 -23 -.58 163 163 | --- --- --- ---
Table 2.1865.1 GPS week: 1865 Day: 1 MJD: 57300
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| -4 0 2 22 21 -10 .22 47 59 | --- --- --- ---
cof n/a| 0 0 8 9 20 -6 .30 49 61 | --- --- --- ---
emx n/a| 0 -1 -4 -33 -37 -48 .29 26 29 | 8318 -849 4577 9170
esx n/a| 0 -1 8 -82 35 -17 -.06 20 17 | 0 -2466 5550 9550
gfz n/a| -2 1 -6 24 52 114 -.03 18 15 | -999999 -6537 261004 999999
grg n/a| 0 -7 -13 -13 -52 -59 -.39 70 41 | -999999 -4445 999999 999999
iac n/a| 4 0 4 79 -41 -42 -.09 19 19 | -999999 -3178 999999 999999
mcc n/a| -2 16 119 145 -143 185 .32 353 353 | --- --- --- ---
Table 2.1865.2 GPS week: 1865 Day: 2 MJD: 57301
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 0 3 13 42 -22 .30 51 60 | --- --- --- ---
cof n/a| -3 0 8 27 14 24 .28 53 60 | --- --- --- ---
emx n/a| -2 -1 -2 -13 -37 -107 .30 27 27 | 5982 -698 4814 9081
esx n/a| 0 0 1 -64 8 -20 .01 19 17 | 0 82 4830 10522
gfz n/a| -3 2 -7 14 53 149 -.13 23 18 | 3741 882 3345 8067
grg n/a| -4 0 -1 61 -2 -92 -.35 39 33 | -561913 -1078 11139 685471
iac n/a| 5 0 2 29 -44 26 -.07 18 18 | 11439 -841 4816 9221
mcc n/a| 11 -10 107 564 -24 -51 -.53 258 258 | --- --- --- ---
Table 2.1865.3 GPS week: 1865 Day: 3 MJD: 57302
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 4 26 -28 -43 .28 49 50 | --- --- --- ---
cof n/a| 1 1 6 55 -28 -22 .44 52 51 | --- --- --- ---
emx n/a| -3 -1 -2 -56 -63 -36 .26 29 30 | -14153 -4442 4520 7802
esx n/a| 2 0 1 -49 4 -88 -.04 19 20 | 0 716 4513 8317
gfz n/a| -1 1 -6 28 86 68 -.02 21 15 | -3719 -503 4146 7031
grg n/a| 1 0 -1 -39 -94 -153 -.40 37 38 | -562227 123 4511 683382
iac n/a| 1 -1 3 56 -2 117 -.10 19 19 | 4980 -103 4529 7911
mcc n/a| 4 1 84 213 -227 -154 -.98 251 251 | --- --- --- ---
Table 2.1865.4 GPS week: 1865 Day: 4 MJD: 57303
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 5 -2 18 -23 .27 49 42 | --- --- --- ---
cof n/a| 0 2 4 0 0 -48 .40 50 42 | --- --- --- ---
emx n/a| -1 0 -2 -67 -76 -17 .28 27 28 | 3722 -2759 4280 7842
esx n/a| -1 -2 -3 -54 27 -126 -.07 17 16 | 0 -1671 4277 7948
gfz n/a| -2 0 -7 64 59 38 -.03 20 15 | 4819 -5937 3785 6950
grg n/a| -1 0 0 -6 -11 -192 -.36 42 41 | -556903 -5685 4274 683430
iac n/a| 3 -1 4 43 -27 124 -.15 18 18 | 10401 -3028 4280 7649
mcc n/a| 4 -16 102 104 -58 105 -.45 329 329 | --- --- --- ---
Table 2.1865.5 GPS week: 1865 Day: 5 MJD: 57304
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 16 9 -93 .34 50 53 | --- --- --- ---
cof n/a| -4 0 4 10 44 -47 .37 53 56 | --- --- --- ---
emx n/a| 0 0 -3 -10 -76 -56 .27 25 26 | 3990 63 3612 7361
esx n/a| -1 -2 2 -97 41 -79 -.08 20 20 | 0 1028 3598 8380
gfz n/a| -2 0 -2 37 93 53 -.05 18 14 | 6509 19 3375 6765
grg n/a| 0 3 0 -22 -48 3 -.38 36 37 | -562363 592 3594 684497
iac n/a| 4 2 2 35 -92 104 -.06 20 20 | 7582 1592 3608 7175
mcc n/a| 12 3 62 -166 -311 -435 -.99 185 185 | --- --- --- ---
Table 2.1865.6 GPS week: 1865 Day: 6 MJD: 57305
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 54 -9 -121 .32 50 41 | --- --- --- ---
cof n/a| -1 0 -2 91 -13 -151 .27 53 40 | --- --- --- ---
emx n/a| 0 -4 0 -48 -66 -76 .28 29 30 | 7930 -158 3913 6458
esx n/a| -2 -1 1 -67 45 -84 -.11 18 16 | 0 530 3899 7588
gfz n/a| 0 0 -5 30 56 33 -.03 20 12 | 4086 -971 3678 6150
grg n/a| 0 0 -1 41 -45 -26 -.36 36 29 | -562791 -413 3895 684326
iac n/a| 1 0 3 15 -31 124 -.02 18 18 | 8110 -849 3897 6382
mcc n/a| -4 4 65 106 -145 -307 -.81 204 204 | --- --- --- ---
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 3.1865.0 GPS week: 1865 Day: 0 MJD: 57299
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 | 1225 50 62 26 18 23 27 24 --- 12 | 98 98 92 81 92 89 88 --- 86
R02E | 1980 31 39 17 17 17 26 13 196 8 | 192 192 200 194 200 208 198 277 197
R03E | 1845 32 31 17 13 12 24 12 --- 7 | 79 78 79 78 77 77 80 --- 77
R04E | 778 25 39 15 12 18 23 11 --- 7 | 177 180 184 180 186 196 181 --- 182
R05E | 1058 22 31 33 20 20 45 27 --- 12 | 30 39 37 40 44 44 33 --- 33
R06E | 930 30 34 25 22 21 35 26 --- 11 | 56 63 65 70 64 52 57 --- 59
R07E | 865 31 40 23 15 17 28 12 139 8 | 234 231 244 243 249 253 241 217 243
R08E | 740 38 53 24 18 18 29 9 --- 9 | 202 205 206 216 214 213 211 --- 210
R09 | 1792 36 29 39 22 20 64 28 --- 14 | 43 51 37 50 43 29 48 --- 38
R10 | 2155 19 23 15 24 11 35 11 --- 8 | 42 44 31 44 25 22 30 --- 29
R11 | 1508 114 109 48 31 28 61 33 --- 22 | 91 90 22 42 45 61 48 --- 28
R12 | 859 117 114 28 58 35 64 39 122 24 | 91 91 34 84 47 63 48 59 39
XR13 | 525 57 56 --- 1019 14 43 13 --- 16 | 50 52 --- 206 34 49 29 --- 27
R14 | 1866 47 39 24 23 22 40 17 --- 11 | 57 52 30 48 43 33 37 --- 35
R15 | 2888 28 22 21 19 26 27 14 --- 9 | 35 35 24 28 34 27 22 --- 22
R16 | 1040 33 47 23 25 24 24 21 --- 11 | 53 63 45 40 34 20 26 --- 30
XR17 | 1094 37 43 21 13 --- 33 14 --- 10 | 30 44 34 52 --- 56 39 --- 39
R18 | 959 15 18 13 21 18 33 19 233 8 | 49 46 50 57 57 41 38 59 48
R19 | 910 22 23 19 9 16 31 10 --- 7 | 64 63 61 54 45 79 43 --- 49
R20 | 980 25 36 26 12 21 59 22 --- 11 | 51 53 58 51 54 40 37 --- 46
R21 | 2455 23 22 26 10 14 28 17 80 8 | 59 57 65 48 54 41 43 63 50
R22 | 1770 22 19 34 15 11 32 22 --- 10 | 61 57 77 63 55 34 39 --- 53
R23 | 958 12 16 12 22 13 30 8 --- 7 | 25 25 32 44 36 20 30 --- 31
R24 | 949 37 67 41 22 22 55 19 --- 13 | 55 74 54 41 37 31 28 --- 35
XR26 | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 59 --- 61
------+---------------------------------------------------+-----------------------------------------------
RMS | 1510 45 49 27 23 20 40 21 163 |T 80 82 76 85 76 74 69 135 69
WRMS | 1510 36 37 28 18 16 38 21 163 |NE 53 56 43 59 42 40 37 60 38
MEDI | 1040 31 36 24 19 18 32 17 139 |MD 56 57 54 52 47 44 43 63 46
Table 3.1865.1 GPS week: 1865 Day: 1 MJD: 57300
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 | 1702 57 56 28 30 30 43 28 --- 15 | 150 153 136 142 140 156 126 --- 136
R02E | 2739 31 32 15 9 16 21 12 666 7 | 172 172 175 178 181 180 185 202 179
R03E | 1474 31 45 18 15 19 28 13 --- 8 | 52 53 57 56 58 56 55 --- 54
R04E | 825 33 34 18 13 16 89 11 --- 13 | 129 127 134 134 132 139 130 --- 130
R05E | 603 24 25 44 24 24 53 22 --- 13 | 39 37 34 33 40 41 34 --- 29
R06E | 917 19 23 21 21 14 23 18 --- 8 | 52 52 55 65 50 54 51 --- 53
R07E | 848 29 29 23 15 14 23 14 355 8 | 168 173 174 172 178 166 182 293 174
R08E | 1196 34 37 21 23 15 29 14 --- 9 | 163 169 166 182 178 167 174 --- 173
R09 | 1448 15 26 37 27 22 41 31 --- 13 | 42 42 41 59 40 31 37 --- 38
R10 | 2257 31 32 10 16 18 28 10 --- 8 | 38 40 22 31 27 24 21 --- 21
R11 | 1324 127 131 45 22 32 36 29 --- 21 | 68 74 43 56 59 48 39 --- 39
R12 | 1020 121 124 33 33 25 51 34 120 21 | 68 75 40 72 55 47 37 41 39
XR13 | 969 72 65 --- 904 15 35 10 --- 18 | 55 56 --- 434 22 32 19 --- 21
R14 | 1246 42 49 27 25 18 54 25 --- 13 | 54 68 49 53 48 30 27 --- 38
R15 | 3685 28 40 20 15 12 33 14 --- 8 | 31 43 36 34 39 41 21 --- 28
R16 | 853 40 29 27 15 18 39 16 --- 10 | 40 36 44 29 35 21 18 --- 26
XR17 | 1466 24 19 20 18 --- 17 12 --- 8 | 22 44 30 36 --- 24 23 --- 24
R18 | 1038 11 18 14 11 14 20 14 108 6 | 35 42 27 24 38 43 19 119 26
R19 | 1462 21 22 12 14 16 260 11 --- 7 | 40 39 34 31 20 171 28 --- 28
R20 | 931 21 34 16 10 13 61 16 --- 9 | 36 69 38 36 36 38 44 --- 35
R21 | 1835 20 27 21 20 11 30 18 168 8 | 45 52 49 34 41 34 27 74 36
R22 | 1434 21 26 27 17 17 52 16 --- 10 | 37 40 48 33 44 20 26 --- 32
R23 | 697 20 18 25 19 11 37 9 --- 8 | 21 23 34 30 25 17 21 --- 22
R24 | 878 29 21 29 22 13 53 22 --- 11 | 45 35 50 34 28 29 11 --- 25
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 76 --- 77
------+---------------------------------------------------+-----------------------------------------------
RMS | 1555 47 49 26 20 18 70 19 353 |T 66 71 65 82 65 67 57 145 59
WRMS | 1555 59 61 29 17 15 41 19 353 |NE 42 48 39 64 37 40 29 78 32
MEDI | 1196 29 29 21 18 16 36 14 168 |MD 45 52 44 36 41 41 34 119 36
Table 3.1865.2 GPS week: 1865 Day: 2 MJD: 57301
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 | 2739 47 56 29 37 32 34 30 --- 15 | 92 102 88 116 122 97 86 --- 98
R02E | 1811 34 36 16 18 19 32 27 350 10 | 137 142 147 149 151 143 121 90 139
R03E | 770 28 28 17 13 18 26 10 --- 7 | 48 50 44 47 50 53 47 --- 46
R04E | 771 29 30 21 15 19 20 13 --- 8 | 153 151 157 152 154 151 157 --- 154
R05E | 701 35 36 32 19 24 33 20 --- 11 | 46 53 36 45 54 44 43 --- 40
R06E | 2186 19 19 24 17 13 19 17 --- 8 | 54 53 52 51 45 47 48 --- 47
R07E | 1099 31 35 19 20 16 103 15 398 16 | 197 198 207 204 210 273 206 364 211
R08E | 1006 31 32 30 21 14 23 18 --- 10 | 166 171 182 167 179 184 170 --- 173
XR09 |14031 31 56 34 --- 31 33 18 --- 14 | 55 88 48 --- 47 28 40 --- 36
R10 | 1653 31 39 18 19 19 16 13 --- 8 | 44 53 27 39 32 29 22 --- 26
R11 | 713 136 131 31 19 47 38 20 --- 20 | 80 77 35 44 74 49 41 --- 37
R12 | 579 131 130 37 30 39 43 20 104 21 | 73 76 37 60 69 49 43 19 41
R13 | 1398 75 88 39 13 26 40 21 --- 14 | 64 77 41 269 25 38 23 --- 23
R14 | 1279 49 50 37 31 17 34 28 --- 14 | 57 64 48 52 44 34 32 --- 34
R15 | 4053 42 31 23 19 42 28 21 --- 12 | 30 29 39 27 38 19 19 --- 20
R16 | 988 27 36 21 15 13 25 9 --- 7 | 43 49 32 30 23 22 23 --- 24
XR17 | 2092 29 47 24 26 --- 41 13 --- 12 | 32 45 43 39 --- 32 21 --- 27
R18 | 1997 15 17 13 15 13 17 11 150 6 | 39 37 42 39 37 32 34 37 35
R19 | 1431 18 18 14 10 15 20 12 --- 6 | 45 46 33 39 39 79 31 --- 34
R20 | 915 16 30 41 11 16 36 22 --- 11 | 62 56 72 53 49 51 44 --- 50
R21 | 2179 21 22 11 16 13 31 13 134 7 | 51 49 40 36 34 33 47 41 38
R22 | 1307 14 15 14 14 12 53 11 --- 9 | 47 49 39 48 50 25 52 --- 43
R23 | 759 26 28 20 14 12 27 14 --- 8 | 21 21 31 37 32 17 36 --- 28
R24 | 801 17 30 45 14 17 52 22 --- 13 | 29 40 52 38 34 49 16 --- 29
XR26 | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 48 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1632 51 53 27 19 23 39 18 258 |T 69 74 65 77 69 65 58 110 59
WRMS | 1632 60 60 27 17 18 33 18 258 |NE 48 53 41 56 41 36 33 32 33
MEDI | 1279 29 32 23 17 17 32 17 150 |MD 51 53 42 47 47 44 43 41 38
Table 3.1865.3 GPS week: 1865 Day: 3 MJD: 57302
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 | 1636 44 34 27 31 21 37 23 --- 13 | 106 105 106 106 97 111 101 --- 100
R02E | 1065 31 51 25 13 17 36 20 442 9 | 153 156 157 157 158 165 147 147 154
R03E | 921 28 27 17 17 15 23 15 --- 8 | 60 62 57 57 61 57 62 --- 57
R04E | 825 35 34 17 11 17 23 18 --- 8 | 137 139 137 141 135 143 128 --- 135
R05E | 1532 40 45 38 21 23 49 17 --- 13 | 39 52 33 33 46 42 32 --- 29
R06E | 3004 39 38 24 18 15 20 17 --- 9 | 42 52 41 49 41 47 43 --- 41
R07E | 1079 27 29 25 13 16 35 33 --- 11 | 160 166 167 158 161 185 145 --- 158
R08E | 859 31 24 39 16 16 29 16 --- 10 | 147 157 147 155 160 162 154 --- 153
R09 | 873 25 36 20 29 17 46 13 --- 11 | 50 61 49 58 54 35 41 --- 46
R10 | 1067 27 25 34 21 14 24 14 --- 9 | 38 37 28 39 30 22 28 --- 26
R11 | 822 127 141 41 11 32 38 30 --- 20 | 92 105 40 37 53 51 44 --- 33
R12 | 506 129 127 33 11 49 37 28 94 21 | 77 74 40 43 82 45 50 23 41
R13 | 860 73 72 22 20 23 42 16 --- 13 | 62 62 23 130 28 35 25 --- 23
R14 | 928 42 45 47 21 22 49 23 --- 14 | 46 47 38 41 35 43 31 --- 27
R15 | 4559 32 28 32 22 34 21 18 --- 12 | 33 38 32 30 30 26 18 --- 18
R16 | 674 17 20 30 16 13 39 19 --- 9 | 40 44 52 41 32 31 26 --- 32
XR17 | 922 26 37 15 18 --- 37 17 --- 10 | 37 40 37 34 --- 36 24 --- 25
R18 | 2395 11 13 16 18 18 37 14 178 8 | 45 50 59 61 43 41 51 90 49
R19 | 1096 13 16 17 13 13 35 11 --- 7 | 49 53 57 47 52 49 42 --- 45
R20 | 759 20 28 31 21 12 49 21 --- 11 | 44 51 73 66 58 60 35 --- 54
R21 | 2476 13 19 8 23 8 35 13 125 8 | 52 59 48 62 45 34 44 79 47
R22 | 1088 14 17 20 18 14 43 7 --- 8 | 51 55 60 56 48 21 44 --- 47
R23 | 656 31 35 20 21 17 42 15 --- 10 | 20 22 26 50 50 17 32 --- 35
R24 | 1403 35 39 47 16 24 44 21 --- 13 | 45 51 42 47 43 50 26 --- 35
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 36 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1635 49 52 29 19 21 37 19 251 |T 67 72 64 70 67 62 56 84 57
WRMS | 1635 50 51 30 20 15 38 19 251 |NE 48 53 44 52 45 37 35 64 36
MEDI | 928 31 34 25 18 17 37 17 125 |MD 49 53 48 50 50 43 42 79 41
Table 3.1865.4 GPS week: 1865 Day: 4 MJD: 57303
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 | 1588 46 34 33 27 18 37 24 --- 13 | 74 75 76 68 57 64 52 --- 58
R02E | 2190 27 29 22 16 17 21 9 612 7 | 109 110 117 116 116 104 112 151 112
R03E | 759 24 61 23 13 11 42 14 --- 8 | 55 74 55 61 60 60 58 --- 56
R04E | 928 37 39 25 11 13 33 21 --- 9 | 161 162 165 153 151 157 143 --- 152
R05E | 1400 35 44 36 15 27 50 19 --- 12 | 46 47 42 47 43 61 38 --- 37
R06E | 2576 35 39 24 15 17 29 19 --- 9 | 49 62 57 52 46 55 44 --- 47
R07E | 777 40 44 20 12 21 28 16 --- 9 | 186 184 194 191 192 205 190 --- 191
R08E | 840 37 36 18 18 15 34 9 --- 9 | 156 160 165 153 153 150 149 --- 153
R09 | 722 25 27 20 24 16 47 19 --- 10 | 45 36 35 49 44 26 38 --- 36
R10 | 982 14 15 18 16 14 32 13 --- 7 | 32 30 26 28 23 20 25 --- 22
R11 | 690 139 125 38 16 33 57 22 --- 21 | 90 79 25 45 55 44 33 --- 29
R12 | 614 112 114 32 11 33 40 27 82 18 | 75 75 30 36 41 37 37 23 27
R13 | 749 77 73 29 12 29 35 16 --- 13 | 58 52 33 80 36 28 25 --- 19
R14 | 773 28 25 32 31 34 83 21 --- 16 | 40 37 27 48 34 47 32 --- 28
R15 | 2243 36 42 14 21 22 24 15 --- 9 | 30 34 31 35 38 31 23 --- 27
R16 | 713 26 30 27 19 12 37 21 --- 10 | 31 35 42 35 31 23 29 --- 28
XR17 | 1212 22 37 28 28 --- 50 23 --- 14 | 34 60 43 46 --- 28 17 --- 26
R18 | 2397 16 21 16 12 11 35 15 191 7 | 40 44 58 56 54 43 38 169 47
R19 | 940 20 15 21 9 11 44 15 --- 8 | 45 44 60 48 49 38 34 --- 42
R20 | 1006 23 22 40 21 16 45 17 --- 11 | 38 60 54 63 47 58 36 --- 45
R21 | 1897 15 13 28 13 18 24 13 126 8 | 48 42 46 52 42 61 39 132 43
R22 | 990 18 19 25 12 16 48 15 --- 9 | 47 47 51 47 40 20 27 --- 37
R23 | 760 32 36 14 20 15 52 13 --- 10 | 16 22 35 52 46 18 34 --- 36
R24 | 877 30 41 32 13 24 33 17 --- 10 | 29 44 32 40 59 31 32 --- 35
XR26 | ---- --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 92 --- 94
------+---------------------------------------------------+-----------------------------------------------
RMS | 1339 49 50 27 17 20 42 18 329 |T 63 67 62 66 63 58 55 118 57
WRMS | 1339 42 42 28 16 15 41 18 329 |NE 43 46 39 47 42 34 34 108 36
MEDI | 928 28 36 25 15 17 37 16 126 |MD 46 47 43 49 46 43 37 132 37
Table 3.1865.5 GPS week: 1865 Day: 5 MJD: 57304
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 | 1784 48 45 34 18 18 38 25 --- 12 | 74 68 58 60 66 76 53 --- 56
R02E | 2863 22 18 15 15 17 29 24 187 8 | 108 110 112 109 110 114 108 244 109
R03E | 710 34 43 27 17 16 28 31 --- 11 | 111 114 110 126 129 128 116 --- 119
R04E | 1927 49 56 26 23 19 25 16 --- 11 | 153 160 162 174 169 169 167 --- 166
R05E | 716 29 33 35 18 17 32 26 --- 11 | 42 53 34 43 43 33 35 --- 35
R06E | 1487 35 33 22 13 11 22 14 --- 8 | 57 56 51 53 54 52 56 --- 52
R07E | 1574 44 49 22 12 17 33 16 147 9 | 156 155 160 164 171 178 156 311 163
R08E | 2297 43 46 14 19 16 19 14 --- 8 | 129 136 138 137 140 135 126 --- 134
R09 | 818 30 37 39 24 26 53 23 --- 14 | 40 67 52 52 49 27 31 --- 36
R10 | 814 16 12 22 21 12 41 14 --- 9 | 28 29 30 35 33 19 21 --- 23
R11 | 871 144 149 25 11 34 37 17 --- 20 | 83 89 33 36 48 48 29 --- 29
R12 | 682 117 111 34 15 28 25 20 99 17 | 74 71 26 36 41 30 25 33 27
R13 | 1085 69 79 25 20 12 24 15 --- 11 | 44 54 35 51 28 31 19 --- 23
R14 | 800 39 47 30 37 23 62 31 --- 15 | 33 43 37 47 35 23 30 --- 29
R15 | 2537 26 24 18 32 22 22 18 --- 10 | 34 35 32 40 45 35 20 --- 28
R16 | 1276 25 25 27 19 12 26 14 --- 8 | 30 38 44 41 36 25 28 --- 31
XR17 | 996 31 42 29 41 --- 46 25 --- 17 | 21 35 26 58 --- 34 16 --- 24
R18 | 2325 9 20 10 13 11 21 19 277 6 | 33 35 35 36 38 45 20 103 31
R19 | 900 18 19 11 11 8 23 22 --- 7 | 37 40 40 40 38 52 21 --- 34
R20 | 1207 24 41 34 25 14 74 18 --- 14 | 36 29 43 42 34 25 16 --- 28
R21 | 1690 20 22 24 8 11 28 13 166 7 | 45 48 44 37 36 27 38 84 35
R22 | 1115 17 12 24 15 6 20 14 --- 7 | 43 38 48 40 36 33 27 --- 35
R23 | 985 30 33 15 26 11 29 14 --- 8 | 23 26 29 47 37 21 30 --- 31
R24 | 1078 29 31 25 16 15 57 23 --- 11 | 41 48 57 48 47 22 48 --- 40
XR26 | ---- --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 76 --- 78
------+---------------------------------------------------+-----------------------------------------------
RMS | 1510 50 53 25 20 18 36 20 185 |T 61 65 59 64 63 57 52 155 55
WRMS | 1510 53 56 26 20 14 37 20 185 |NE 40 45 38 42 38 31 29 73 33
MEDI | 1085 30 33 25 18 16 28 18 166 |MD 42 48 43 47 43 33 30 103 35
Table 3.1865.6 GPS week: 1865 Day: 6 MJD: 57305
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 | 2149 59 66 30 26 30 33 35 --- 15 | 80 95 61 84 87 80 48 --- 67
R02E | 3404 28 39 21 13 17 19 18 161 8 | 135 136 148 142 142 146 139 143 141
R03E | 703 20 19 26 12 19 18 19 --- 8 | 154 158 151 158 157 166 159 --- 157
R04E | 2791 26 29 21 15 18 22 12 --- 7 | 184 181 197 193 193 190 186 --- 190
R05E | 531 38 49 40 17 24 44 23 --- 12 | 52 62 38 32 44 56 31 --- 31
R06E | 1447 36 47 25 16 15 29 12 --- 8 | 59 58 62 76 75 64 71 --- 69
R07E | 2156 42 50 27 10 15 27 13 132 9 | 208 203 214 215 214 226 214 242 214
R08E | 3254 42 44 23 17 20 35 20 --- 10 | 164 162 170 164 168 164 162 --- 164
R09 | 918 17 34 34 20 16 41 20 --- 10 | 42 53 34 49 41 28 35 --- 35
R10 | 860 27 36 27 16 10 42 13 --- 9 | 45 54 41 47 38 18 30 --- 33
R11 | 807 132 136 33 21 24 40 22 --- 19 | 101 103 29 45 56 53 38 --- 33
R12 | 598 132 133 36 22 29 43 17 69 19 | 100 102 26 49 54 60 38 34 33
R13 | 757 65 49 18 14 13 36 9 --- 10 | 63 57 27 108 28 34 18 --- 20
R14 | 911 36 28 50 35 17 46 20 --- 14 | 49 42 31 52 31 34 29 --- 30
R15 | 2190 46 46 25 13 41 23 17 --- 12 | 38 36 29 31 30 26 20 --- 22
R16 | 632 26 24 26 20 31 29 12 --- 10 | 41 40 29 38 31 20 27 --- 26
XR17 | 638 30 37 51 21 --- 46 22 --- 16 | 21 34 57 24 --- 30 17 --- 22
R18 | 1074 13 15 24 13 8 30 14 371 7 | 49 51 60 48 45 38 34 76 43
R19 | 992 21 19 17 10 12 29 17 --- 7 | 64 64 59 49 52 58 37 --- 47
R20 | 897 26 23 46 14 12 55 18 --- 12 | 41 42 74 55 50 38 36 --- 47
R21 | 714 24 21 26 7 11 48 11 148 8 | 65 64 67 54 56 39 47 61 52
R22 | 611 16 16 25 11 9 23 14 --- 7 | 65 62 72 57 55 37 45 --- 54
R23 | 1909 24 26 21 14 15 18 11 --- 7 | 23 29 38 45 38 33 30 --- 33
R24 | 1263 9 38 31 24 18 54 20 --- 11 | 49 70 59 63 60 33 44 --- 50
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 111 --- 112
------+---------------------------------------------------+-----------------------------------------------
RMS | 1620 50 53 29 18 20 36 18 204 |T 78 81 73 78 75 69 65 111 69
WRMS | 1620 41 40 30 16 12 29 18 204 |NE 53 56 45 50 44 36 37 57 40
MEDI | 911 27 36 26 15 17 33 17 148 |MD 59 62 59 52 54 38 38 76 47
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