[IGSREPORT-23749] Wk 1852 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Jul 23 07:50:38 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1852 (Jul 05, 2015 - Jul 11, 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 2.1852.
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:
igl1852[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1852 in the SP3 format.
igl18527.sum Combination Report for GPS Week 1852.
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 | 16.8 ns
1 | -0.3 ns
2 | 0.8 ns
3 | 0.5 ns
4 | 0.6 ns
5 | 0.9 ns
6 | -0.7 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 | GFZ | R17
0 | GRG | R02
1 | COD | R11 R12
3 | GFZ | R17
6 | GFZ | R17
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 1.1852, 1a.1852).
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 2.1852.0-6)
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 3.1852.0-6).
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 1852 summary. (Jul 05, 2015 - Jul 11, 2015)
Table 1.1852.a GPS week : 1852 MJD: 57208.0-57214.0
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 -4 36 -66 15 .29 46 37 | --- --- --- ---
| 1 1 2 24 17 27 .05 | --- ---
cof n/a| -1 0 -5 31 -60 2 .19 49 40 | --- --- --- ---
| 1 1 2 31 25 29 .08 | --- ---
emx n/a| 0 0 2 33 -26 -78 .20 27 25 | 2935 -60 4487 7824
| 1 1 2 38 19 35 .06 | 12038 1203
esx n/a| 0 0 0 -46 35 39 -.11 23 21 | -1983 473 4490 8540
| 1 1 1 15 22 23 .07 | 10807 1158
gfz n/a| 0 0 1 34 61 87 .05 71 19 | 0 773 4223 7402
| 1 2 1 27 16 31 .07 | 0 1297
grg n/a| 0 1 6 -21 -1 97 -.36 43 34 | -774506 409 6215 689991
| 2 1 4 25 17 64 .11 | 19797 1657
iac n/a| 0 0 -2 -21 -20 -69 -.12 22 22 | 4612 -539 4492 7751
| 1 0 2 21 17 70 .07 | 6974 1118
mcc n/a| 0 5 -13 35 -91 -794 -.05 181 181 | --- --- --- ---
| 8 6 24 104 150 546 .34 | --- ---
Table 1.1852.b GPS week : 1852 MJD: 57208.0-57214.0
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 | 15 8 9 12 11 12 10 |
R02 | 10 7 7 8 9 11 7 |
R03 | 10 9 8 11 11 11 7 |
R04 | 10 8 7 6 7 8 5 |
R05 | 14 14 13 12 14 13 21 |
R06 | 8 9 9 11 12 9 10 |
R07 | 8 7 7 6 7 9 8 |
R08 | 8 8 7 8 8 6 6 |
R09 | 15 15 13 13 14 17 15 |
R10 | 8 10 7 8 19 9 16 |
R11 | 25 16 25 23 24 25 23 |
R12 | 28 19 28 24 22 26 25 |
R13 | 8 10 9 9 10 10 10 |
R14 | 14 15 16 15 14 20 18 |
R15 | 9 9 8 9 8 9 10 |
R16 | 10 9 10 10 13 12 9 |
R17 | 17 15 24 17 36 28 25 |
R18 | 9 10 8 9 8 6 8 |
R19 | 9 11 12 9 10 10 8 |
R20 | 16 16 16 16 15 14 15 |
R21 | 9 10 12 10 13 11 10 |
R22 | 10 9 9 10 10 11 11 |
R23 | 10 7 11 10 10 11 7 |
R24 | 10 12 13 13 15 13 13 |
Table 1.1852.c GPS week : 1852 MJD: 57208.0-57214.0
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 1852 0 | -71 -49 168 -436 -709 3135 84.1 2546 2546 | 16836 0
brd 1852 1 | 81 -46 192 -838 -2108 2658 86.0 3649 3649 | -277 0
brd 1852 2 | 31 50 107 -1907 316 4688 85.2 2445 2445 | 751 0
brd 1852 3 | 70 -4 68 -860 287 3618 84.4 2185 2185 | 535 0
brd 1852 4 | -27 6 136 228 -1474 2664 86.5 1806 1806 | 564 0
brd 1852 5 | -719 659 313 855 18320 639 88.0 >>>>> >>>>> | 880 0
brd 1852 6 |-8163 5437 602 58830 18730 -28380 12.7 >>>>> >>>>> | -682 0
-------------+------------------------------------------------------------+----------------
brd 1852 mean|-1256 864 226 7981 4766 -1568 75.3 >>>>> >>>>> | 2658 0
brd 1852 sdev| 3058 2031 182 22439 9440 11886 27.6 >>>>> >>>>> | 6277 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 2.1852.0 GPS week: 1852 Day: 0 MJD: 57208
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 3 -6 81 -92 4 .24 49 36 | --- --- --- ---
cof n/a| 0 2 -7 83 -70 -35 .31 50 37 | --- --- --- ---
emx n/a| 0 -1 4 3 -23 -74 .12 24 20 | 23674 1904 4943 8679
esx n/a| 0 -1 2 -35 49 10 -.10 22 23 | 21497 2890 4984 8395
gfz n/a| 0 2 0 -9 84 104 .09 49 21 | 0 3063 4888 7761
grg n/a| -1 0 1 -16 2 158 -.44 60 33 | -748150 3236 16647 688749
iac n/a| 0 0 1 -2 -36 -44 -.05 22 22 | 20376 7 4963 8307
mcc n/a| -5 14 -39 64 -266 -1509 -.17 168 168 | --- --- --- ---
Table 2.1852.1 GPS week: 1852 Day: 1 MJD: 57209
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 -6 6 -67 -1 .21 54 38 | --- --- --- ---
cof n/a| -4 0 -8 0 -58 15 .17 58 42 | --- --- --- ---
emx n/a| 0 0 2 23 -14 -46 .14 29 28 | 9658 -458 4653 9537
esx n/a| -1 -1 0 -63 29 59 -.02 22 20 | -9907 -323 4643 9945
gfz n/a| 0 0 1 5 44 82 .14 22 22 | 0 -417 4549 9356
grg n/a| 4 1 2 -1 21 75 -.45 29 28 | -769799 -624 4874 696463
iac n/a| 1 0 -2 4 -35 -145 -.10 20 20 | 2385 -2431 4652 9452
mcc n/a| -10 12 3 245 -197 -1123 -.26 132 132 | --- --- --- ---
Table 2.1852.2 GPS week: 1852 Day: 2 MJD: 57210
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 -1 41 -33 8 .29 46 32 | --- --- --- ---
cof n/a| 0 -1 -3 33 -27 -4 .14 46 34 | --- --- --- ---
emx n/a| 0 -1 2 -15 -33 -99 .19 26 23 | 7640 -46 3959 7551
esx n/a| 0 0 -1 -34 12 63 -.03 23 20 | -9244 926 3955 7728
gfz n/a| 0 2 1 63 52 72 .02 29 13 | 0 1784 3763 6695
grg n/a| 0 0 7 -20 3 50 -.41 32 30 | -767603 1027 3953 694728
iac n/a| 2 0 -2 -9 -8 -54 -.04 25 25 | 2801 21 3951 7450
mcc n/a| 12 -6 17 -32 -30 -547 -.13 143 143 | --- --- --- ---
Table 2.1852.3 GPS week: 1852 Day: 3 MJD: 57211
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -2 -2 35 -67 -26 .34 42 31 | --- --- --- ---
cof n/a| 0 0 -2 33 -69 -24 .20 44 33 | --- --- --- ---
emx n/a| -1 1 4 104 2 -61 .24 28 27 | -2784 -955 4724 6850
esx n/a| 0 -1 0 -69 67 14 -.14 21 19 | -2159 254 4705 8012
gfz n/a| 0 -3 2 36 44 114 -.01 217 24 | 0 -632 4373 6524
grg n/a| 1 0 5 -64 7 115 -.44 38 36 | -767126 -793 4737 692788
iac n/a| 1 1 -4 -27 -37 -98 -.10 20 20 | 2004 -1425 4708 6834
mcc n/a| -3 4 5 66 30 95 -.55 187 187 | --- --- --- ---
Table 2.1852.4 GPS week: 1852 Day: 4 MJD: 57212
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 50 -63 37 .30 44 35 | --- --- --- ---
cof n/a| 0 0 -4 40 -28 54 .15 47 35 | --- --- --- ---
emx n/a| -1 -1 3 43 -57 -29 .27 28 26 | -2128 -459 4293 6984
esx n/a| 3 0 1 -45 44 48 -.18 26 24 | -4432 -496 4307 7842
gfz n/a| 2 0 3 36 83 130 .01 41 17 | 0 166 4310 6804
grg n/a| -2 2 5 -37 -28 203 -.28 53 44 | -766124 -965 4403 694563
iac n/a| -1 0 -3 -42 -23 -161 -.20 20 20 | 2199 -140 4292 6749
mcc n/a| 7 2 -9 -47 137 -609 .53 185 185 | --- --- --- ---
Table 2.1852.5 GPS week: 1852 Day: 5 MJD: 57213
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 -6 18 -65 56 .36 44 44 | --- --- --- ---
cof n/a| -2 -1 -6 -14 -75 0 .10 48 48 | --- --- --- ---
emx n/a| -1 -2 4 48 -20 -128 .28 28 27 | -1229 -1560 4687 7984
esx n/a| 0 0 3 -27 42 64 -.19 24 21 | -7262 13 4706 9840
gfz n/a| 0 0 1 60 56 36 -.05 34 15 | 0 542 4030 8026
grg n/a| 0 0 7 14 -22 47 -.16 45 35 | -804438 -865 4734 723906
iac n/a| 0 0 -4 -55 -10 -12 -.11 22 22 | 1325 -788 4714 8291
mcc n/a| -4 2 -24 -50 -245 -583 .16 197 197 | --- --- --- ---
Table 2.1852.6 GPS week: 1852 Day: 6 MJD: 57214
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 -7 23 -76 29 .32 45 47 | --- --- --- ---
cof n/a| -1 0 -6 42 -96 12 .29 47 48 | --- --- --- ---
emx n/a| 0 0 -2 24 -38 -110 .20 24 22 | -14283 1148 4153 7185
esx n/a| 0 -1 0 -49 3 20 -.15 24 20 | -2377 53 4131 8018
gfz n/a| -1 2 2 45 63 72 .12 103 17 | 0 907 3653 6651
grg n/a| 1 3 14 -28 6 32 -.32 41 31 | -798308 1851 4162 638742
iac n/a| 0 0 -5 -19 9 32 -.24 25 25 | 1197 981 4165 7179
mcc n/a| 2 6 -47 5 -70 -1286 .06 257 257 | --- --- --- ---
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 3.1852.0 GPS week: 1852 Day: 0 MJD: 57208
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 | 800 21 21 26 38 40 26 34 --- 14 | 58 63 71 63 65 73 80 --- 62
R02 | 980 17 16 16 17 19 233 24 217 9 | 63 61 62 59 57 107 57 99 57
R03 | 750 12 11 15 9 24 52 16 --- 10 | 53 56 59 64 58 69 57 --- 58
R04 | 607 19 24 15 13 22 52 17 --- 10 | 57 60 59 53 52 49 51 --- 51
R05 | 625 40 28 20 25 28 63 17 --- 13 | 54 59 73 85 62 68 73 --- 69
R06 | 1138 24 26 13 19 20 13 16 --- 7 | 30 29 46 60 43 46 41 --- 44
R07 | 1807 14 18 17 17 12 24 17 223 7 | 66 69 61 76 66 73 71 80 68
R08 | 1286 17 20 12 19 14 23 20 --- 8 | 59 61 66 67 66 54 57 --- 60
R09 | 908 23 31 22 33 43 49 33 --- 15 | 62 69 62 76 72 64 83 --- 69
R10 | 1144 18 19 16 22 17 18 16 --- 8 | 43 43 38 52 42 40 45 --- 41
R11 | 1081 138 137 35 23 45 53 35 --- 24 | 113 116 39 48 67 56 52 --- 40
R12 | 1156 151 166 52 34 58 46 30 60 28 | 133 141 47 50 69 60 52 68 39
R13 | 5270 24 21 17 17 14 26 11 --- 7 | 51 48 38 40 34 40 37 --- 36
R14 | 1455 30 18 33 25 37 40 26 --- 14 | 23 34 33 44 48 27 34 --- 28
R15 | 9459 23 22 16 21 26 15 16 --- 8 | 44 40 32 40 33 27 33 --- 32
R16 | 947 31 38 19 18 20 29 17 --- 9 | 83 86 76 71 70 61 71 --- 71
R17E | 729 37 35 27 36 197 43 27 --- 16 | 44 53 42 72 189 65 47 --- 48
R18E | 2708 29 29 17 11 21 36 13 145 9 | 41 39 30 34 33 39 33 46 30
R19E | 1729 34 25 16 14 20 29 15 --- 9 | 42 35 23 30 31 31 23 --- 23
R20E | 637 39 39 39 23 43 46 30 --- 16 | 44 52 41 39 42 40 32 --- 30
R21E | 2041 23 21 17 16 23 26 17 138 8 | 46 42 32 39 43 47 35 16 35
R22E | 1053 25 27 24 19 19 37 18 --- 10 | 39 39 25 35 30 34 26 --- 26
R23E | 1507 27 27 15 17 18 41 17 --- 9 | 42 42 40 50 44 37 40 --- 39
R24E | 1641 20 29 25 19 22 25 21 --- 10 | 36 54 35 49 33 34 39 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 2546 49 50 24 22 49 60 22 167 |T 55 57 47 54 56 51 48 61 45
WRMS | 2546 36 37 20 23 21 33 22 167 |NE 62 64 53 59 56 57 55 82 51
MEDI | 1138 24 25 17 19 22 36 17 145 |MD 46 53 41 50 48 47 45 68 40
Table 3.1852.1 GPS week: 1852 Day: 1 MJD: 57209
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 | 1402 23 30 21 14 12 14 21 --- 8 | 39 69 47 55 62 51 57 --- 49
R02 | 1235 13 18 16 16 18 9 16 137 7 | 35 33 44 32 29 71 37 74 33
R03 | 3442 13 20 27 12 14 31 15 --- 8 | 35 33 35 28 33 50 31 --- 29
R04 | 1389 17 14 15 12 12 31 22 --- 8 | 33 30 33 26 36 31 42 --- 31
R05 | 615 27 30 45 29 25 34 18 --- 13 | 31 34 76 44 49 46 44 --- 44
R06 | 972 16 24 17 26 15 21 22 --- 9 | 18 16 33 39 29 25 18 --- 22
R07 | 1584 12 17 13 17 9 23 15 125 6 | 43 47 38 55 47 40 48 37 44
R08 | 1435 16 20 16 23 14 16 15 --- 7 | 35 40 42 55 41 32 48 --- 41
R09 | 2988 25 39 22 35 44 42 31 --- 15 | 83 95 89 89 87 93 95 --- 87
R10 | 1287 13 12 25 33 11 25 13 --- 9 | 45 53 57 62 56 58 44 --- 49
R11 | 1629 150 159 40 26 28 47 19 --- 16 | 100 105 49 46 66 47 48 --- 50
R12 | 1110 179 187 62 19 39 37 16 118 18 | 118 123 63 62 73 55 57 41 60
R13 | 5970 24 29 24 16 17 23 22 --- 9 | 42 50 46 34 43 41 35 --- 36
R14 | 1638 26 36 44 41 28 37 25 --- 15 | 22 38 37 49 46 38 33 --- 25
R15 |12206 15 25 13 21 31 17 12 --- 9 | 32 38 35 32 50 21 29 --- 30
R16 | 1217 27 31 18 17 19 16 18 --- 8 | 92 92 92 83 85 89 82 --- 86
XR17E | 1169 33 31 17 37 --- 30 28 --- 15 | 43 55 46 68 --- 48 34 --- 42
R18E | 5509 31 31 19 15 23 23 12 120 9 | 42 42 32 32 35 25 35 32 29
R19E | 2737 38 38 16 17 21 30 20 --- 11 | 43 43 26 28 30 33 22 --- 24
R20E | 960 36 48 48 26 19 49 34 --- 16 | 52 69 48 47 47 50 32 --- 37
R21E | 2581 31 37 18 14 17 30 15 156 9 | 56 65 43 51 48 45 51 16 46
R22E | 5360 24 23 21 14 15 28 19 --- 9 | 38 34 26 30 29 42 27 --- 28
R23E | 1512 15 21 12 16 12 22 16 --- 7 | 57 58 49 58 55 62 55 --- 54
R24E | 1835 25 25 31 26 26 25 26 --- 12 | 41 56 35 49 45 52 36 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 3649 54 58 28 22 22 29 20 132 |T 48 54 46 48 48 47 43 40 42
WRMS | 3649 38 42 28 20 22 28 20 132 |NE 50 56 51 49 52 49 46 50 44
MEDI | 1512 24 29 19 17 18 25 18 125 |MD 42 47 43 47 47 46 37 37 37
Table 3.1852.2 GPS week: 1852 Day: 2 MJD: 57210
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1437 28 31 20 15 15 33 13 --- 9 | 49 59 70 62 67 75 62 --- 62
R02 | 2381 10 16 12 14 8 23 19 215 6 | 44 53 41 46 47 63 45 93 43
R03 | 586 22 17 16 18 11 17 21 --- 8 | 43 48 37 39 38 38 47 --- 37
R04 | 964 10 15 16 13 12 14 20 --- 6 | 41 48 49 45 37 45 37 --- 40
R05 | 578 22 25 21 29 28 44 24 --- 12 | 34 37 41 52 46 56 51 --- 42
R06 | 893 18 18 25 20 15 24 15 --- 9 | 27 33 26 42 43 54 31 --- 33
R07 | 1140 10 14 13 12 10 25 15 119 6 | 51 43 54 55 57 39 50 73 50
R08 | 765 11 12 13 16 17 22 13 --- 7 | 49 43 53 58 41 44 57 --- 49
R09 | 745 28 33 21 29 31 40 30 --- 13 | 76 102 75 96 92 77 64 --- 78
R10 | 1666 12 25 15 16 14 22 14 --- 7 | 40 41 47 46 40 54 40 --- 41
R11 | 2019 127 108 48 24 31 52 30 --- 24 | 102 89 44 45 52 68 50 --- 40
R12 | 1144 142 148 49 20 50 49 35 118 27 | 112 116 42 44 64 57 52 47 39
R13 | 4973 17 20 18 20 14 23 22 --- 8 | 58 56 59 58 55 49 55 --- 54
R14 | 1490 28 25 40 39 27 29 37 --- 15 | 22 38 30 63 41 49 39 --- 32
R15 | 8710 11 26 14 22 18 25 15 --- 8 | 29 33 33 36 33 24 34 --- 28
R16 | 1372 18 15 19 24 22 19 22 --- 9 | 72 78 78 86 69 75 55 --- 70
R17E | 1949 38 35 28 39 96 43 41 --- 23 | 37 41 48 60 323 47 46 --- 40
R18E | 1090 27 34 15 13 17 23 17 123 8 | 39 42 31 32 31 27 33 43 28
R19E | 1221 45 42 23 24 23 27 21 --- 12 | 51 48 39 49 47 50 24 --- 37
R20E | 1732 40 32 41 25 26 54 27 --- 16 | 53 61 39 56 57 47 32 --- 39
R21E | 2252 37 36 29 19 19 38 21 112 12 | 61 66 42 52 45 50 37 16 42
R22E | 1285 29 28 19 14 16 32 15 --- 9 | 45 41 33 36 37 38 35 --- 32
R23E | 732 23 30 14 23 14 21 38 --- 10 | 64 70 60 69 68 55 39 --- 56
R24E | 1123 25 52 33 22 22 32 34 --- 12 | 35 60 62 53 53 50 42 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 2444 46 46 26 23 29 32 25 143 |T 51 56 47 53 61 51 44 54 44
WRMS | 2444 32 34 23 20 13 30 25 143 |NE 53 57 48 54 51 54 48 71 46
MEDI | 1221 23 26 19 20 17 25 21 119 |MD 45 48 42 52 47 50 42 47 40
Table 3.1852.3 GPS week: 1852 Day: 3 MJD: 57211
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 | 1048 30 26 19 24 26 47 16 --- 11 | 50 49 55 64 55 49 56 --- 51
R02 | 1371 10 12 17 16 18 38 11 303 8 | 52 54 59 53 68 47 58 173 55
R03 | 781 23 26 38 17 12 33 16 --- 10 | 55 56 64 71 66 47 65 --- 61
R04 | 680 10 15 14 17 8 18 10 --- 5 | 53 50 56 47 54 70 57 --- 53
R05 | 778 21 18 35 20 23 39 18 --- 11 | 53 51 51 50 47 71 42 --- 45
R06 | 1399 19 23 25 23 10 52 14 --- 10 | 31 30 39 55 39 86 35 --- 42
R07 | 2067 16 20 12 11 8 24 12 210 6 | 62 67 61 55 58 59 53 152 56
R08 | 721 16 24 19 17 9 36 9 --- 7 | 51 59 61 50 51 36 45 --- 47
R09 | 722 25 28 33 31 31 39 20 --- 13 | 80 74 81 81 70 80 93 --- 77
R10 | 1417 13 11 15 19 17 28 14 --- 8 | 62 68 72 76 65 104 63 --- 69
R11 | 1440 115 124 34 21 33 69 27 --- 23 | 108 113 48 46 65 70 52 --- 48
R12 | 1093 122 114 46 25 33 58 30 100 24 | 110 102 51 66 67 59 56 107 50
R13 | 1750 19 22 20 24 17 24 20 --- 9 | 74 79 73 70 71 81 57 --- 67
R14 | 2519 35 30 34 34 35 50 25 --- 15 | 32 43 34 51 47 39 38 --- 30
R15 | 8268 10 19 19 18 28 18 16 --- 8 | 35 40 40 29 47 27 33 --- 33
R16 | 1595 19 17 27 21 23 27 16 --- 10 | 109 114 116 100 107 112 111 --- 107
R17E | 840 38 36 47 28 1061 28 28 --- 17 | 42 41 60 67 877 43 49 --- 45
R18E | 1616 27 31 16 14 19 29 14 144 8 | 45 49 35 41 44 43 35 70 36
R19E | 599 31 48 20 15 18 30 13 --- 9 | 38 49 38 31 22 48 21 --- 26
R20E | 992 37 45 41 33 28 44 29 --- 15 | 46 55 39 46 44 36 32 --- 30
R21E | 2928 38 40 23 12 17 29 14 91 9 | 54 54 34 46 42 52 37 31 38
R22E | 894 35 28 23 12 21 36 18 --- 10 | 46 43 36 33 34 35 30 --- 29
R23E | 1280 21 32 17 17 24 36 23 --- 10 | 40 46 35 53 49 55 44 --- 42
R24E | 1178 15 41 35 20 27 39 31 --- 12 | 36 56 41 45 50 33 39 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 2185 42 44 28 21 217 38 20 187 |T 56 60 53 55 89 57 50 106 48
WRMS | 2185 31 33 27 19 24 36 20 187 |NE 63 65 60 60 61 64 57 144 55
MEDI | 1178 21 26 23 19 21 36 16 144 |MD 51 54 51 51 51 49 45 107 45
Table 3.1852.4 GPS week: 1852 Day: 4 MJD: 57212
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 | 1239 27 22 15 24 25 46 22 --- 11 | 50 65 47 65 69 41 60 --- 53
R02 | 1233 15 14 18 19 13 39 16 161 8 | 49 47 59 58 60 70 39 203 49
R03 | 889 39 35 18 28 17 42 11 --- 11 | 38 43 61 79 60 41 63 --- 59
R04 | 946 11 15 11 13 18 13 17 --- 6 | 42 43 45 47 53 53 53 --- 47
R05 | 613 37 36 36 35 18 47 23 --- 14 | 48 50 48 42 39 34 49 --- 36
R06 | 2174 17 21 20 29 11 61 17 --- 11 | 30 33 47 59 48 83 37 --- 42
R07 | 1948 10 14 19 11 15 23 12 251 6 | 59 64 67 61 66 59 63 128 61
R08 | 1002 15 13 19 17 12 27 14 --- 7 | 50 46 57 44 36 39 35 --- 40
R09 | 1162 35 38 27 36 28 45 26 --- 14 | 56 72 39 52 50 28 51 --- 42
R10 | 1560 23 24 16 20 18 139 19 --- 18 | 49 46 50 42 41 106 39 --- 43
R11 | 1356 121 112 37 15 37 71 34 --- 24 | 110 107 68 70 80 93 69 --- 67
R12 | 1012 117 121 31 24 28 53 30 158 22 | 110 112 67 63 64 73 71 45 62
R13 | 2596 24 47 26 13 27 43 11 --- 10 | 93 96 96 89 76 75 87 --- 86
R14 | 1963 30 32 32 30 24 58 24 --- 14 | 41 50 38 47 42 41 35 --- 32
R15 | 4316 8 15 12 19 22 30 16 --- 8 | 46 50 47 55 51 35 42 --- 45
R16 | 1857 24 30 27 35 21 62 14 --- 13 | 54 58 64 47 51 45 42 --- 46
R17E | 799 57 72 63 50 167 67 24 --- 36 | 41 56 37 59 228 56 42 --- 48
R18E | 1935 17 18 14 13 14 39 13 221 7 | 39 39 37 39 40 52 28 62 34
R19E | 647 24 20 25 13 28 29 12 --- 9 | 40 41 33 29 38 30 25 --- 27
R20E | 1135 42 63 33 36 34 37 26 --- 15 | 51 69 50 62 55 39 33 --- 40
R21E | 3717 40 37 40 26 20 34 15 88 13 | 49 49 35 43 38 40 27 18 29
R22E | 1353 37 32 26 14 22 29 15 --- 10 | 44 43 33 36 38 32 27 --- 29
R23E | 975 26 34 19 17 29 31 15 --- 9 | 35 34 31 35 38 30 33 --- 30
R24E | 1248 22 41 37 33 38 57 24 --- 15 | 27 57 33 48 42 27 33 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1805 44 47 28 26 41 53 20 185 |T 52 57 49 52 58 50 45 91 44
WRMS | 1805 35 35 26 24 17 44 20 185 |NE 57 61 56 57 55 57 52 125 50
MEDI | 1239 24 32 25 20 22 42 16 161 |MD 48 50 47 48 50 41 39 62 42
Table 3.1852.5 GPS week: 1852 Day: 5 MJD: 57213
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 |>>>>> 30 34 21 24 37 33 18 --- 12 | 36 60 46 49 56 61 38 --- 40
R02 |>>>>> 13 20 14 13 11 65 18 111 10 | 46 57 46 47 47 97 30 91 44
R03 |>>>>> 39 45 23 30 13 18 15 --- 10 | 34 34 60 81 52 64 43 --- 55
R04 |>>>>> 12 11 9 11 9 40 17 --- 7 | 35 43 42 45 39 21 49 --- 39
R05 |>>>>> 22 31 30 22 21 53 28 --- 13 | 57 69 43 56 51 38 56 --- 47
R06 | ---- 16 20 9 23 12 32 23 --- 9 | 31 33 33 44 34 26 45 --- 34
R07 |>>>>> 10 9 13 11 21 45 13 315 8 | 45 43 53 51 43 32 47 65 44
R08 |>>>>> 12 12 8 13 15 18 13 --- 6 | 36 37 45 47 49 63 39 --- 44
R09 |>>>>> 28 34 39 42 23 64 32 --- 17 | 54 52 52 67 62 66 69 --- 56
R10 | ---- 21 25 20 27 11 24 11 --- 8 | 57 59 48 59 50 30 54 --- 48
R11 | ---- 118 126 41 31 38 58 39 --- 24 | 100 104 57 63 70 80 74 --- 60
R12 |>>>>> 130 132 45 21 48 47 31 130 25 | 109 106 74 54 68 74 68 49 59
R13 | ---- 27 24 21 18 17 35 14 --- 9 | 102 103 107 100 94 89 89 --- 95
R14 |>>>>> 21 27 41 34 24 111 28 --- 19 | 29 36 32 39 48 64 27 --- 28
R15 |>>>>> 15 23 9 24 24 34 12 --- 9 | 38 37 41 42 45 37 33 --- 36
R16 |>>>>> 30 34 21 23 20 46 23 --- 11 | 83 88 79 90 83 74 75 --- 80
R17E |>>>>> 38 65 53 49 120 38 37 --- 28 | 39 69 55 71 213 36 37 --- 43
R18E |>>>>> 18 20 10 13 13 24 10 220 6 | 36 36 27 34 37 46 29 31 31
R19E | ---- 25 26 27 12 22 29 15 --- 9 | 30 34 32 34 42 28 19 --- 25
R20E | ---- 35 40 39 18 41 29 24 --- 14 | 45 58 51 36 50 43 37 --- 35
R21E | ---- 38 43 22 16 23 30 16 129 10 | 47 50 27 35 37 38 28 18 28
R22E | ---- 44 46 29 12 23 29 10 --- 11 | 46 48 35 34 43 34 27 --- 29
R23E |>>>>> 30 28 24 16 23 28 24 --- 10 | 39 46 42 46 48 50 38 --- 39
R24E |>>>>> 22 35 38 20 27 33 24 --- 12 | 33 51 42 35 46 35 31 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 44 48 28 24 34 45 22 197 |T 50 56 48 52 58 51 45 50 44
WRMS |>>>>> 44 48 27 21 15 35 22 197 |NE 55 60 53 58 55 57 52 68 50
MEDI |>>>>> 25 28 22 20 22 33 18 130 |MD 39 50 45 47 48 43 38 49 40
Table 3.1852.6 GPS week: 1852 Day: 6 MJD: 57214
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 |>>>>> 32 42 22 23 14 24 17 --- 9 | 55 59 67 56 61 66 74 --- 61
R02 |>>>>> 19 20 16 18 15 21 8 258 7 | 64 61 68 49 55 64 54 109 56
R03 |>>>>> 26 27 7 22 15 17 11 --- 7 | 52 56 65 71 67 64 64 --- 63
R04 |>>>>> 13 19 9 9 12 19 11 --- 5 | 55 51 58 50 53 54 55 --- 53
R05 |>>>>> 34 29 33 27 91 61 19 --- 21 | 64 73 77 82 110 70 79 --- 71
R06 |>>>>> 23 20 15 19 20 29 22 --- 9 | 38 43 47 64 55 58 53 --- 50
R07 |>>>>> 21 21 15 13 12 31 16 372 8 | 73 73 68 67 62 51 66 87 63
R08 |>>>>> 16 12 8 18 8 21 10 --- 6 | 61 64 69 62 63 70 63 --- 63
R09 | ---- 33 26 25 33 28 54 29 --- 14 | 37 44 36 56 48 52 52 --- 41
R10 |>>>>> 22 26 23 15 20 96 18 --- 16 | 49 49 38 61 52 100 48 --- 51
R11 | ---- 114 118 37 27 36 57 41 --- 22 | 113 118 65 83 81 74 76 --- 66
R12 | ---- 136 141 32 33 43 50 41 82 24 | 125 137 85 113 112 95 92 55 89
R13 |>>>>> 24 31 21 18 19 40 16 --- 10 | 99 89 105 94 93 69 84 --- 91
R14 |>>>>> 45 21 28 39 48 35 44 --- 17 | 33 47 47 63 67 29 30 --- 39
R15 |>>>>> 20 19 18 22 29 25 24 --- 10 | 57 64 59 71 62 53 46 --- 56
R16 | ---- 27 32 16 19 24 23 17 --- 9 | 73 75 69 74 66 59 71 --- 68
R17E |>>>>> 39 49 51 47 484 61 49 --- 25 | 43 64 57 74 341 70 55 --- 52
R18E |>>>>> 24 29 16 18 13 29 15 256 8 | 44 46 30 33 33 32 33 32 31
R19E |>>>>> 26 22 13 10 18 30 19 --- 8 | 43 40 33 34 31 41 23 --- 29
R20E | ---- 36 40 28 18 38 38 37 --- 14 | 50 56 45 42 61 36 35 --- 35
R21E | ---- 34 36 20 16 23 38 12 230 10 | 45 51 29 39 40 44 28 18 30
R22E |>>>>> 40 49 17 17 28 29 21 --- 10 | 45 48 32 32 40 38 23 --- 27
R23E | ---- 24 26 13 17 8 22 13 --- 7 | 38 36 36 39 33 37 36 --- 34
R24E |>>>>> 30 32 28 30 24 36 24 --- 12 | 40 51 47 47 35 28 36 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 45 47 24 24 103 41 25 257 |T 58 62 55 60 71 56 53 60 52
WRMS |>>>>> 47 48 22 20 17 31 25 257 |NE 65 68 63 69 69 64 62 83 61
MEDI |>>>>> 26 27 18 18 20 30 18 256 |MD 50 56 57 61 61 54 53 55 52
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