[IGSREPORT-22897] Wk 1800 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Jul 24 15:55:49 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1800 (Jul 06, 2014 - Jul 12, 2014)
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 2.1800.
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:
igl1800[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1800 in the SP3 format.
igl18007.sum Combination Report for GPS Week 1800.
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 | 190.4 ns
1 | 189.5 ns
2 | 190.1 ns
3 | 188.5 ns
4 | 187.3 ns
5 | 188.4 ns
6 | 189.2 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 | GRG | R24
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 1.1800, 1a.1800).
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 2.1800.0-6)
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 3.1800.0-6).
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 1800 summary. (Jul 06, 2014 - Jul 12, 2014)
Table 1.1800.a GPS week : 1800 MJD: 56844.0-56850.0
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 34 -63 64 .30 25 24 | --- --- --- ---
| 1 1 3 22 15 40 .04 | --- ---
cof n/a| -2 1 0 19 -47 42 .28 28 26 | --- --- --- ---
| 2 1 4 26 23 34 .06 | --- ---
emx n/a| 0 0 0 -17 9 -3 -.46 31 29 | 188080 375 3954 7001
| 1 2 2 36 6 45 .05 | 925 593
esx n/a| 0 -1 -2 -42 14 17 -.00 23 21 | 188426 -1006 3950 7605
| 0 1 3 19 23 25 .05 | 4416 2438
gfz n/a| -1 0 -1 4 28 26 .15 22 16 | 0 210 3960 6869
| 1 1 1 13 13 26 .04 | 0 1207
grg n/a| 0 2 6 39 -49 56 -.30 112 111 | -172088 -570 3976 98650
| 1 1 5 29 30 45 .07 | 12779 1539
iac n/a| 2 0 -1 4 29 -147 -.03 24 24 | 189989 79 3947 6904
| 1 0 7 18 29 58 .06 | 1061 646
mcc n/a| 0 3 34 9 10 976 -.26 161 161 | --- --- --- ---
| 7 5 20 141 83 460 .45 | --- ---
Table 1.1800.b GPS week : 1800 MJD: 56844.0-56850.0
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 | 10 16 10 11 14 14 10 |
R02 | 7 9 12 9 8 9 9 |
R03 | 10 9 11 11 9 8 10 |
R04 | 7 6 8 6 6 8 6 |
R05 | 8 10 9 8 8 11 10 |
R06 | 6 7 7 8 7 8 10 |
R07 | 8 7 7 8 10 7 7 |
R08 | 7 9 10 9 8 12 7 |
R09 | 17 17 18 16 15 18 13 |
R10 | 10 10 8 11 10 9 9 |
R11 | 19 14 16 19 14 16 13 |
R12 | 18 17 14 16 19 19 18 |
R13 | 11 10 13 12 10 10 11 |
R14 | 19 19 18 18 17 15 17 |
R15 | 8 12 9 10 10 10 9 |
R16 | 16 12 11 10 10 10 8 |
R17 | 18 11 10 10 11 11 11 |
R18 | 9 10 8 7 8 8 8 |
R19 | 9 10 11 9 9 9 11 |
R20 | 12 12 12 14 17 15 16 |
R21 | 16 16 15 16 14 15 15 |
R22 | 11 12 10 9 8 11 10 |
R23 | 10 11 9 8 7 8 9 |
R24 | 11 12 11 11 9 9 9 |
Table 1.1800.c GPS week : 1800 MJD: 56844.0-56850.0
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 1800 0 | -42 45 168 266 755 5219 84.7 1642 1642 | 190355 0
brd 1800 1 | -27 -45 147 901 1079 6005 86.5 1828 1828 | 189524 0
brd 1800 2 | -14 -15 87 555 740 3947 84.3 1827 1827 | 190095 0
brd 1800 3 | 20 -84 116 749 -279 2612 85.3 3880 3880 | 188475 0
brd 1800 4 | 14 0 115 27 1057 5673 87.9 1953 1953 | 187273 0
brd 1800 5 | -58 69 137 8 -862 6370 86.3 2461 2461 | 188386 0
brd 1800 6 | -8 50 199 738 -716 8164 85.2 1862 1862 | 189205 0
-------------+------------------------------------------------------------+----------------
brd 1800 mean| -16 2 138 463 253 5427 85.8 2207 2207 | 189044 0
brd 1800 sdev| 28 56 37 363 845 1776 1.2 780 780 | 1078 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 2.1800.0 GPS week: 1800 Day: 0 MJD: 56844
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 0 25 -61 60 .34 25 24 | --- --- --- ---
cof n/a| -3 3 -7 6 -7 44 .31 28 27 | --- --- --- ---
emx n/a| -2 1 -4 -4 16 -26 -.37 31 27 | 188966 712 4047 7296
esx n/a| 0 -5 -7 -33 46 -3 .03 25 21 | 183620 -372 4040 7954
gfz n/a| -1 0 0 10 40 38 .15 25 18 | 0 635 4055 7342
grg n/a| -1 1 -1 63 -38 129 -.44 558 558 | -191348 -2001 3799 87552
iac n/a| 3 -1 8 11 -12 -104 -.07 22 22 | 190052 1472 4051 7462
mcc n/a| 0 7 38 17 123 732 -.74 112 112 | --- --- --- ---
Table 2.1800.1 GPS week: 1800 Day: 1 MJD: 56845
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 7 16 -68 99 .32 24 22 | --- --- --- ---
cof n/a| -6 0 8 13 -45 86 .37 27 24 | --- --- --- ---
emx n/a| 0 0 -2 22 5 -13 -.44 33 28 | 188978 88 4204 6609
esx n/a| -1 -1 -5 -67 14 64 -.06 23 24 | 187856 -2143 4192 7276
gfz n/a| -1 2 -3 18 41 -9 .14 25 22 | 0 -1309 4202 6505
grg n/a| 1 0 1 -9 -85 36 -.35 44 37 | -170656 -2259 4320 93445
iac n/a| 2 -1 6 6 50 -141 -.12 22 22 | 190488 -185 4186 6816
mcc n/a| 5 1 64 -66 55 791 -.51 115 115 | --- --- --- ---
Table 2.1800.2 GPS week: 1800 Day: 2 MJD: 56846
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 7 13 -37 48 .26 27 27 | --- --- --- ---
cof n/a| 0 0 2 -32 -70 68 .21 30 30 | --- --- --- ---
emx n/a| 0 1 -1 17 0 41 -.52 35 32 | 188623 1236 3969 6959
esx n/a| 0 -1 -2 -51 25 14 -.06 22 22 | 185121 1047 3970 7943
gfz n/a| -3 1 0 -14 11 23 .22 19 17 | 0 1442 4000 6675
grg n/a| 0 0 2 47 -87 47 -.28 35 37 | -149718 1498 4010 132103
iac n/a| 0 -1 -3 36 22 -143 -.03 25 25 | 190935 -388 3969 6471
mcc n/a| 4 2 55 27 -92 554 -.15 143 143 | --- --- --- ---
Table 2.1800.3 GPS week: 1800 Day: 3 MJD: 56847
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 3 72 -87 69 .24 26 25 | --- --- --- ---
cof n/a| -2 1 2 43 -37 40 .24 30 28 | --- --- --- ---
emx n/a| -1 -2 2 -37 6 67 -.48 31 31 | 187414 246 3650 7589
esx n/a| 0 1 -5 -41 -24 24 .03 24 23 | 196741 -4109 3655 7909
gfz n/a| 0 0 0 -12 41 12 .10 22 17 | 0 -145 3643 7405
grg n/a| 0 4 4 12 -64 -18 -.22 38 38 | -177569 -995 3693 92022
iac n/a| 2 0 -3 9 45 -144 .01 22 22 | 190168 12 3646 7317
mcc n/a| -2 3 14 -88 22 439 .14 142 142 | --- --- --- ---
Table 2.1800.4 GPS week: 1800 Day: 4 MJD: 56848
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 1 53 -68 -4 .34 25 23 | --- --- --- ---
cof n/a| 1 0 0 41 -80 -24 .34 25 23 | --- --- --- ---
emx n/a| 0 -1 1 -83 11 -13 -.44 29 29 | 187092 -384 3798 6501
esx n/a| 0 -1 1 -11 4 -12 -.02 19 17 | 186361 -3800 3786 6944
gfz n/a| -1 0 0 6 12 29 .14 21 14 | 0 -1320 3807 6415
grg n/a| -1 2 11 74 -31 54 -.25 33 31 | -165435 -1607 3832 81098
iac n/a| 1 0 -11 -22 73 -130 .03 29 29 | 187733 135 3786 6551
mcc n/a| -13 12 10 -173 -22 1643 -.63 204 204 | --- --- --- ---
Table 2.1800.5 GPS week: 1800 Day: 5 MJD: 56849
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 45 -68 52 .28 25 24 | --- --- --- ---
cof n/a| 0 1 1 35 -37 32 .24 27 25 | --- --- --- ---
emx n/a| 1 0 1 -10 18 -7 -.46 27 27 | 186848 906 3915 6676
esx n/a| 0 -2 2 -62 0 3 -.02 25 20 | 187867 2368 3914 7112
gfz n/a| -1 0 0 1 30 17 .16 21 13 | 0 1697 3914 6437
grg n/a| 0 2 11 54 -5 88 -.28 42 46 | -172132 1246 3976 90033
iac n/a| 1 0 -10 1 11 -93 .06 24 24 | 189865 -70 3915 6503
mcc n/a| 0 -1 37 79 79 1402 .49 212 212 | --- --- --- ---
Table 2.1800.6 GPS week: 1800 Day: 6 MJD: 56850
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 2 -3 17 -51 122 .30 23 20 | --- --- --- ---
cof n/a| -3 2 -1 31 -52 50 .28 27 23 | --- --- --- ---
emx n/a| 0 -3 -3 -28 9 -70 -.52 28 26 | 188641 -177 4099 7382
esx n/a| -1 0 -2 -31 34 31 .09 24 21 | 191421 -37 4095 8103
gfz n/a| 0 1 -1 19 19 75 .16 19 14 | 0 474 4104 7304
grg n/a| 2 4 11 30 -31 60 -.29 33 33 | -177761 126 4206 114302
iac n/a| 1 0 1 -12 11 -271 -.05 25 25 | 190683 -417 4080 7214
mcc n/a| 8 -2 21 267 -91 1274 -.43 200 200 | --- --- --- ---
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 3.1800.0 GPS week: 1800 Day: 0 MJD: 56844
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 | 1012 27 31 17 29 17 25 14 --- 10 | 79 79 66 46 55 59 57 --- 57
R02 | 807 18 30 14 11 15 14 21 --- 7 | 63 63 67 62 69 52 54 --- 60
R03 | 788 27 29 20 33 20 14 13 --- 10 | 63 68 65 92 84 61 69 --- 72
R04 | 714 15 16 19 10 15 16 15 --- 6 | 76 73 63 62 66 64 65 --- 65
R05 | 759 14 15 18 12 21 23 22 100 8 | 73 71 63 63 55 63 54 56 59
R06 | 1228 10 15 17 11 10 22 14 --- 6 | 59 56 72 59 63 64 55 --- 60
R07 | 713 9 20 12 13 8 59 16 123 8 | 83 87 82 82 82 73 85 30 81
XR08 | 836 10 14 16 17 10 --- 16 --- 7 | 67 65 72 62 61 --- 65 --- 64
R09 | 815 46 42 50 37 23 50 30 --- 17 | 41 43 32 56 38 35 52 --- 30
R10 | 2942 16 24 27 22 13 33 22 --- 9 | 25 32 40 26 22 32 17 --- 19
R11 | 966 34 42 62 28 48 40 31 98 18 | 24 31 36 50 75 59 48 35 41
R12 | 1610 37 32 37 25 54 71 28 --- 18 | 25 31 27 40 74 41 53 --- 38
R13 | 1035 27 25 17 16 23 56 21 --- 11 | 23 26 23 33 46 44 33 --- 28
R14 | 1782 31 41 68 45 25 54 28 --- 18 | 23 32 46 40 32 34 30 --- 21
R15 | 1025 9 20 15 27 12 34 15 161 8 | 22 31 19 24 21 35 14 49 14
R16 | 1045 23 33 16 34 23 117 12 --- 16 | 34 47 19 27 29 72 29 --- 24
R17E | 1066 18 17 18 19 27 135 28 61 18 | 63 70 66 73 81 94 64 44 68
XR18E | 925 15 34 23 19 17 --- 14 --- 8 | 32 44 36 39 38 --- 37 --- 34
R19E | 4029 13 15 21 25 19 42 14 --- 9 | 36 45 43 48 48 50 37 --- 41
R20E | 1852 19 22 29 23 24 52 28 --- 12 | 67 72 76 77 88 91 80 --- 76
R21E | 1475 36 33 37 25 31 74 29 106 16 | 42 57 39 63 73 90 44 69 51
XR22E | 845 16 14 34 18 19 --- 21 --- 11 | 96 93 90 94 100 --- 92 --- 94
XR23E | 3544 18 23 26 18 14 --- 25 --- 10 | 57 50 60 50 52 --- 59 --- 54
R24E | 2512 18 22 26 22 17 2485 21 --- 10 | 29 36 28 41 41 9999 32 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1642 25 28 31 25 25 558 22 112 |T 50 54 51 54 58 58 51 47 49
WRMS | 1642 24 27 27 21 18 558 22 112 |NE 48 52 49 51 54 52 48 42 45
MEDI | 1025 18 23 20 22 19 42 21 100 |MD 42 50 46 50 55 59 53 44 51
Table 3.1800.1 GPS week: 1800 Day: 1 MJD: 56845
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 | 1440 34 29 18 21 15 98 17 --- 15 | 51 46 37 44 23 62 31 --- 30
R02 | 756 15 19 13 11 17 39 24 --- 9 | 46 42 45 45 53 30 61 --- 46
R03 | 1423 23 26 20 27 15 22 13 --- 9 | 41 41 40 52 46 52 52 --- 44
R04 | 4157 8 9 17 14 10 16 17 --- 6 | 46 43 40 38 46 54 47 --- 42
R05 | 1226 23 30 17 24 25 13 18 97 9 | 44 52 36 24 25 39 43 41 29
R06 | 1270 14 14 18 15 18 12 11 --- 6 | 34 42 41 42 36 40 32 --- 34
R07 | 1383 15 17 16 15 11 23 16 89 7 | 50 53 48 45 39 36 40 19 41
XR08 | 1059 12 20 16 17 17 --- 20 --- 8 | 44 51 45 45 43 --- 31 --- 39
R09 | 1566 44 51 48 44 21 38 27 --- 16 | 31 44 39 67 48 34 43 --- 36
R10 | 1960 14 17 28 25 15 21 22 --- 9 | 24 26 21 25 25 26 21 --- 17
R11 | 841 33 31 44 18 29 54 19 128 14 | 23 26 34 24 41 54 28 10 23
R12 | 1319 34 25 39 22 56 29 31 --- 16 | 24 35 35 33 71 35 38 --- 32
R13 | 1739 15 25 26 16 18 37 23 --- 9 | 27 35 31 30 30 31 20 --- 22
R14 | 1241 28 26 75 30 44 60 23 --- 19 | 22 28 35 35 44 42 25 --- 18
R15 | 2168 9 19 27 29 23 61 15 142 12 | 20 27 22 23 23 29 15 18 15
R16 | 1231 17 21 34 35 16 46 19 --- 12 | 24 26 22 38 26 36 25 --- 21
R17E | 1256 15 29 25 15 16 44 28 54 10 | 74 85 79 88 92 92 78 38 82
XR18E | 1485 17 28 22 17 18 --- 23 --- 9 | 28 31 29 31 33 --- 36 --- 27
R19E | 2318 20 38 23 13 19 35 23 --- 9 | 48 52 50 59 57 66 56 --- 53
R20E | 2403 16 28 28 25 27 41 29 --- 12 | 58 65 68 64 68 72 62 --- 61
R21E | 2049 39 32 40 20 35 55 29 148 16 | 31 48 42 64 80 78 46 70 52
XR22E | 814 17 24 38 16 16 --- 25 --- 11 | 95 103 104 96 103 --- 103 --- 98
XR23E | 3175 15 21 29 16 20 --- 26 --- 10 | 34 41 40 41 38 --- 36 --- 34
XR24E | 2327 14 19 33 29 19 --- 20 --- 11 | 31 44 33 53 29 --- 39 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1827 24 27 33 23 25 44 22 114 |T 39 45 42 46 46 47 42 32 38
WRMS | 1827 22 24 28 24 22 37 22 114 |NE 34 38 35 38 38 40 34 22 30
MEDI | 1423 16 25 26 18 18 38 22 97 |MD 34 42 39 42 41 40 38 19 34
Table 3.1800.2 GPS week: 1800 Day: 2 MJD: 56846
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 | 783 33 41 28 19 15 23 19 --- 10 | 61 71 61 50 48 45 35 --- 45
R02 | 627 24 34 25 7 13 63 24 --- 12 | 48 58 53 36 36 39 52 --- 36
R03 | 658 26 30 18 26 15 31 30 --- 11 | 56 54 49 74 71 50 54 --- 60
R04 | 883 18 19 16 11 18 12 22 --- 7 | 62 67 53 52 68 55 40 --- 54
R05 | 1532 23 23 27 17 12 24 17 106 8 | 65 65 56 42 59 48 36 68 48
R06 | 1153 15 16 25 18 9 17 12 --- 7 | 46 50 51 39 44 48 39 --- 41
R07 | 1510 19 13 19 10 12 17 15 109 6 | 61 50 60 59 51 47 46 21 52
XR08 | 1024 15 17 19 10 15 --- 37 --- 10 | 53 54 62 56 54 --- 29 --- 48
R09 | 2085 54 56 62 45 19 26 28 --- 18 | 32 35 34 58 33 34 42 --- 27
R10 | 2109 13 13 19 23 10 20 11 --- 7 | 23 23 25 24 24 20 25 --- 18
R11 | 1104 44 50 36 23 27 56 27 166 15 | 34 41 36 56 63 58 38 16 42
R12 | 1126 40 51 32 20 31 41 30 --- 14 | 23 30 30 37 59 58 42 --- 36
R13 | 1337 20 22 32 32 24 29 31 --- 12 | 20 31 16 34 42 34 37 --- 25
R14 | 2000 37 32 88 22 24 34 33 --- 18 | 32 35 45 37 49 42 24 --- 30
R15 | 4961 12 16 21 15 16 41 18 119 9 | 21 26 14 17 24 42 19 37 13
R16 | 1231 16 17 35 23 13 40 28 --- 11 | 21 25 41 22 23 33 23 --- 17
R17E | 1429 22 30 25 19 15 31 27 72 10 | 91 94 87 98 95 97 82 62 91
XR18E | 1975 14 15 16 13 14 --- 19 --- 7 | 28 34 27 44 38 --- 34 --- 33
R19E | 2637 15 19 26 21 17 41 27 --- 10 | 55 57 54 53 59 67 46 --- 52
R20E | 1107 23 40 29 16 29 32 33 --- 12 | 85 97 86 92 101 94 80 --- 88
R21E | 1620 33 26 36 23 25 57 29 229 14 | 46 56 54 63 70 89 55 59 58
R22E | 957 18 22 29 13 20 31 25 --- 10 | 88 92 85 95 107 70 83 --- 94
R23E | 2169 20 17 30 17 12 28 16 --- 8 | 41 43 42 31 37 40 38 --- 34
R24E | 1888 12 22 24 24 16 32 37 --- 11 | 29 45 25 47 45 574 36 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1827 27 30 35 22 19 35 25 143 |T 46 51 47 50 54 76 43 43 44
WRMS | 1827 27 30 32 22 17 37 25 143 |NE 41 44 42 43 46 43 36 35 37
MEDI | 1337 20 22 26 19 15 31 27 109 |MD 46 50 49 47 49 48 38 37 41
Table 3.1800.3 GPS week: 1800 Day: 3 MJD: 56847
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 | 680 23 17 25 28 19 34 19 --- 10 | 68 62 58 48 61 44 55 --- 54
R02 | 844 21 22 26 17 14 24 13 --- 8 | 56 55 57 37 42 45 39 --- 42
R03 | 4517 14 22 23 29 16 42 18 --- 10 | 52 58 60 75 69 37 50 --- 57
R04 | 2901 14 15 14 12 11 25 11 --- 6 | 64 60 58 46 52 38 51 --- 51
R05 | 1644 21 33 13 18 13 26 16 114 8 | 76 80 58 57 64 72 53 108 61
R06 | 2778 11 20 19 10 23 20 21 --- 8 | 53 52 69 58 75 61 50 --- 59
R07 | 4199 9 34 28 11 12 26 20 106 8 | 72 93 78 70 76 88 61 30 71
XR08 | 914 14 20 22 15 18 --- 18 --- 8 | 60 62 67 56 59 --- 46 --- 55
R09 | 8053 45 62 53 42 24 24 22 --- 16 | 31 44 39 61 42 31 47 --- 33
R10 | 1376 21 26 22 28 14 32 24 --- 10 | 31 41 40 34 33 25 25 --- 25
R11 | 1272 54 41 29 32 43 63 28 164 18 | 37 44 67 71 88 62 55 25 56
R12 | 1754 44 47 27 24 34 56 29 --- 16 | 22 27 38 47 69 53 54 --- 41
R13 | 3096 27 30 33 26 20 44 15 --- 12 | 21 28 31 36 41 55 35 --- 29
R14 | 2882 39 32 59 36 27 43 35 --- 17 | 23 34 50 58 43 55 30 --- 32
R15 | 3280 10 13 21 25 19 37 21 119 9 | 27 29 23 36 23 26 19 75 18
R16 | 7519 16 19 24 24 26 35 15 --- 10 | 30 31 24 25 36 32 24 --- 19
R17E | 786 19 19 26 19 22 30 17 91 9 | 122 125 125 130 135 140 130 111 128
XR18E | 2289 11 24 18 15 10 --- 17 --- 7 | 36 44 35 45 37 --- 37 --- 35
R19E | 2144 11 17 27 15 11 40 17 --- 8 | 36 41 46 54 46 69 45 --- 44
R20E | 4486 29 30 53 19 23 34 31 --- 14 | 84 93 106 93 90 86 77 --- 84
R21E | 8998 28 47 43 26 30 67 30 218 16 | 48 75 43 71 82 87 49 155 58
R22E | 2192 21 24 25 14 16 32 19 --- 9 | 112 117 121 114 111 53 112 --- 113
R23E | 886 12 13 19 18 16 23 22 --- 8 | 46 45 39 50 43 47 34 --- 41
R24E | 2148 16 16 32 21 14 44 19 --- 10 | 33 41 42 46 37 222 33 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 3880 26 30 31 24 22 38 22 142 |T 51 57 57 59 60 64 50 84 51
WRMS | 3880 25 28 31 23 17 38 22 142 |NE 45 50 51 50 54 48 43 59 43
MEDI | 2192 19 22 25 19 18 34 19 114 |MD 46 45 50 54 52 53 47 75 44
Table 3.1800.4 GPS week: 1800 Day: 4 MJD: 56848
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 | 803 20 30 39 17 13 56 39 --- 13 | 53 65 61 59 50 40 80 --- 52
R02 | 813 11 17 11 10 17 24 28 --- 7 | 38 42 37 42 47 45 41 --- 39
R03 | 653 20 21 24 15 24 15 22 --- 9 | 47 45 60 56 49 54 33 --- 47
R04 | 949 8 13 14 10 10 26 15 --- 6 | 47 52 57 56 48 46 45 --- 48
R05 | 1237 15 16 14 15 15 17 26 290 7 | 55 54 53 67 58 61 73 131 59
R06 | 2141 12 12 21 12 10 25 15 --- 7 | 45 48 66 44 44 71 52 --- 49
R07 | 2997 13 14 21 15 17 8 41 151 9 | 63 60 56 69 70 66 34 24 59
XR08 | 1056 14 18 23 11 9 --- 18 --- 7 | 48 54 53 49 55 --- 43 --- 48
R09 | 2536 48 38 49 28 21 18 29 --- 15 | 28 32 49 52 49 35 51 --- 36
R10 | 882 15 18 22 22 9 42 26 --- 10 | 33 32 30 25 27 37 24 --- 22
R11 | 2350 35 48 27 21 31 40 26 156 13 | 34 39 48 61 67 52 50 23 49
R12 | 1242 53 36 38 31 39 52 33 --- 18 | 33 43 39 66 72 48 50 --- 44
R13 | 1015 23 27 18 17 20 28 21 --- 9 | 24 30 33 33 39 43 34 --- 28
R14 | 1624 43 26 40 37 31 24 44 --- 16 | 23 56 38 71 69 42 31 --- 42
R15 | 1208 14 20 30 20 20 29 22 144 10 | 21 28 34 24 31 34 24 30 18
R16 | 2023 22 22 29 24 15 23 24 --- 10 | 32 34 39 36 31 28 18 --- 24
R17E | 1252 23 16 20 14 16 39 32 160 10 | 70 77 80 86 85 106 66 77 79
XR18E | 1180 12 20 17 17 18 --- 18 --- 8 | 31 37 29 32 40 --- 38 --- 30
R19E | 1563 12 21 30 14 15 30 17 --- 8 | 26 36 30 30 34 35 31 --- 27
R20E | 1708 23 22 42 20 40 44 55 --- 16 | 71 78 89 86 104 100 57 --- 81
R21E | 3028 34 20 40 19 23 51 27 267 14 | 45 64 51 66 61 68 60 140 55
R22E | 4552 14 31 27 10 17 21 22 --- 8 | 69 67 68 72 76 42 77 --- 72
R23E | 1003 13 19 17 15 12 25 16 --- 7 | 58 61 57 61 62 49 54 --- 57
R24E | 2195 17 20 21 14 15 33 16 --- 8 | 32 39 35 37 39 171 39 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1952 25 25 29 19 21 33 29 204 |T 42 48 49 53 54 57 46 70 45
WRMS | 1952 23 23 29 17 14 31 29 204 |NE 39 44 47 50 50 46 42 52 41
MEDI | 1242 15 20 23 15 17 26 24 156 |MD 38 45 49 56 49 46 43 30 47
Table 3.1800.5 GPS week: 1800 Day: 5 MJD: 56849
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 | 641 32 33 24 50 9 28 23 --- 13 | 53 49 46 38 42 33 52 --- 40
R02 | 790 10 15 28 14 13 42 19 --- 9 | 32 33 40 33 22 34 25 --- 27
R03 | 733 14 18 17 16 10 34 17 --- 7 | 40 53 42 43 31 21 42 --- 35
R04 | 1068 6 16 23 13 10 37 18 --- 7 | 43 45 48 36 39 31 44 --- 38
R05 | 1058 18 20 16 16 15 60 24 300 10 | 43 49 43 47 32 30 54 63 38
R06 | 3020 21 17 13 20 18 12 18 --- 8 | 34 40 57 67 39 61 56 --- 49
R07 | 2506 12 22 19 13 7 18 18 145 6 | 43 33 61 48 44 47 48 18 46
XR08 | 1174 13 22 16 15 23 --- 38 --- 11 | 48 43 44 49 53 --- 38 --- 44
R09 | 2981 35 33 30 45 33 62 47 --- 18 | 30 31 26 65 55 43 42 --- 32
R10 | 1356 13 15 18 21 17 35 22 --- 9 | 22 25 22 21 30 23 24 --- 17
R11 | 2005 47 34 34 15 39 50 17 160 15 | 37 45 53 57 78 67 54 15 54
R12 | 1404 49 57 39 19 47 76 27 --- 19 | 28 35 39 46 69 38 43 --- 39
R13 | 7599 28 33 13 23 19 28 19 --- 9 | 21 22 26 33 36 21 30 --- 25
R14 | 1307 33 31 37 37 23 33 31 --- 14 | 23 38 31 50 47 39 33 --- 30
R15 | 2537 10 19 22 26 19 37 23 138 10 | 21 23 17 22 23 39 28 29 15
R16 | 1944 23 26 23 26 17 24 21 --- 10 | 24 32 21 27 26 32 19 --- 16
R17E | 965 12 15 18 26 12 43 36 263 11 | 80 78 79 80 91 93 87 69 82
XR18E | 1425 11 13 15 15 17 --- 19 --- 8 | 34 35 37 44 44 --- 42 --- 38
R19E | 1158 14 19 23 14 17 33 22 --- 9 | 24 31 35 33 37 56 37 --- 30
R20E | 1231 33 32 46 30 21 36 31 --- 14 | 51 58 64 65 58 63 49 --- 54
R21E | 2032 29 36 41 16 21 76 18 215 14 | 44 67 51 65 62 63 55 38 53
R22E | 2636 11 13 42 16 20 30 18 --- 10 | 86 92 87 88 94 39 93 --- 88
R23E | 1859 12 29 16 24 11 27 14 --- 7 | 39 58 40 46 42 38 38 --- 39
R24E | 3045 16 16 18 15 21 26 25 --- 9 | 32 35 29 35 42 182 37 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 2461 25 27 27 25 21 42 24 212 |T 38 43 43 47 47 49 44 38 40
WRMS | 2461 24 25 27 20 13 46 24 212 |NE 33 37 38 42 41 37 39 31 34
MEDI | 1404 14 20 22 16 17 34 21 160 |MD 34 38 40 46 42 39 42 29 38
Table 3.1800.6 GPS week: 1800 Day: 6 MJD: 56850
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 | 817 19 22 27 32 12 18 25 --- 10 | 78 80 82 60 71 78 59 --- 68
R02 | 917 18 24 22 18 12 28 15 --- 8 | 57 60 58 45 52 53 39 --- 49
R03 | 560 7 11 12 36 7 29 24 --- 9 | 59 60 61 85 64 45 44 --- 60
R04 | 1122 10 18 18 15 11 13 11 --- 5 | 65 70 59 58 66 57 52 --- 59
R05 | 1087 21 18 20 18 14 20 32 327 9 | 69 66 64 51 54 46 45 43 54
R06 | 1867 22 25 31 16 17 33 12 --- 9 | 55 53 73 70 72 58 61 --- 62
R07 | 1845 8 8 14 10 13 27 13 133 6 | 78 78 81 74 77 69 72 21 74
XR08 | 890 9 10 18 13 15 --- 14 --- 7 | 75 74 76 70 79 --- 57 --- 71
R09 | 3534 27 32 37 30 19 24 35 --- 13 | 22 28 28 57 41 32 55 --- 32
R10 | 1078 14 14 20 29 12 27 21 --- 9 | 34 37 34 30 28 33 28 --- 25
R11 | 2338 33 49 34 15 28 44 19 142 13 | 32 37 58 57 79 74 60 14 56
R12 | 1159 56 53 32 17 37 54 23 --- 17 | 19 27 54 52 79 69 56 --- 50
R13 | 726 25 26 18 21 26 33 19 --- 10 | 21 27 30 37 54 38 36 --- 33
R14 | 1349 28 42 64 36 30 43 29 --- 17 | 21 39 27 40 42 25 36 --- 23
R15 | 3911 16 14 22 26 18 17 15 130 8 | 22 23 21 27 22 22 24 42 15
R16 | 1589 15 23 18 23 13 22 20 --- 8 | 29 33 29 32 27 31 24 --- 23
R17E | 1512 18 22 18 42 13 23 23 250 10 | 56 60 67 77 59 68 57 69 61
XR18E | 1497 15 12 17 12 15 --- 23 --- 8 | 40 42 36 43 41 --- 51 --- 40
R19E | 920 13 13 21 23 17 24 44 --- 11 | 30 36 35 36 41 37 48 --- 34
R20E | 2579 29 28 45 24 22 58 42 --- 16 | 65 73 83 78 79 76 80 --- 72
R21E | 1349 33 45 38 17 27 51 27 126 14 | 79 97 67 77 72 95 75 41 72
R22E | 1850 17 15 25 16 14 32 28 --- 9 | 68 70 69 68 74 38 79 --- 70
R23E | 2039 18 11 15 16 16 34 22 --- 9 | 42 45 39 45 44 47 56 --- 44
R24E | 2292 13 18 15 20 13 35 24 --- 9 | 36 46 32 40 42 250 43 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 1861 23 27 28 24 19 33 25 200 |T 48 52 52 54 56 60 51 38 49
WRMS | 1861 20 23 26 21 14 33 25 200 |NE 46 49 52 52 56 48 46 30 47
MEDI | 1349 18 18 20 18 15 28 23 133 |MD 42 46 58 52 54 47 52 41 50
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