[IGSREPORT-19015] Wk 1601 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 30 06:06:02 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1601 (Sep 12, 2010 - Sep 18, 2010)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths 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 centers
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 2.1601.
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:
igl1601[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1601 in the SP3 format.
igl16017.sum Combination Report for GPS Week 1601.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
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.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
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.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 456.1 ns
1 | 407.6 ns
2 | 460.9 ns
3 | 460.3 ns
4 | 456.7 ns
5 | 404.1 ns
6 | 408.5 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1601, 1a.1601).
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 2.1601.0-6)
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 3.1601.0-6).
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 1601 summary. (Sep 12, 2010 - Sep 18, 2010)
Table 1.1601.a GPS week : 1601 MJD: 55451.0-55457.0
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]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 1 -4 -2 -10 46 -.20 20 20 | 0 -125 1907 2045
| 1 0 3 39 24 103 .03 | 0 525
cod 230| 0 -1 0 30 -8 37 -.11 18 17 | --- --- --- ---
| 1 1 4 39 22 71 .03 | --- ---
esx 131| 0 -1 0 -3 32 38 .44 21 19 | 93465 -474 4039 7898
| 1 1 2 27 23 78 .02 | 27567 2100
gfz 198| 0 1 -1 -34 -47 40 -.13 28 26 | 266734 -2007 4042 7357
| 2 2 2 52 60 66 .04 | 30031 2058
iac n/a| 1 2 8 -53 -16 -238 -.27 30 30 | 436832 -816 4040 7670
| 1 2 20 25 20 367 .04 | 27532 1323
mcc n/a| 1 3 14 -72 8 351 -.01 116 116 | --- --- --- ---
| 6 8 32 121 90 457 .36 | --- ---
Table 1.1601.b GPS week : 1601 MJD: 55451.0-55457.0
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 | 16 18 19 18 13 17 15 |
R02 | 14 16 13 13 10 9 14 |
R04 | 10 10 11 17 13 10 16 |
R05 | 11 11 14 14 16 13 10 |
R07 | 13 11 10 16 11 13 13 |
R08 | 12 11 12 11 14 12 15 |
R10 | 12 11 12 13 15 13 10 |
R11 | 19 22 19 12 17 17 21 |
R13 | 12 10 11 11 15 11 15 |
R14 | 8 12 14 12 16 19 18 |
R15 | 10 10 8 9 12 15 16 |
R17 | 12 10 12 12 11 14 13 |
R18 | 8 9 9 8 10 9 12 |
R19 | 9 10 9 7 9 9 12 |
R20 | 13 11 10 14 13 12 12 |
R21 | 9 14 9 11 10 17 10 |
R22 | 8 9 11 11 10 12 20 |
R23 | 9 12 9 14 11 11 11 |
R24 | 14 8 11 12 8 11 11 |
Table 1.1601.c GPS week : 1601 MJD: 55451.0-55457.0
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 1601 0 | -21 -39 316 988 -2777 -15360 84.3 2752 2752 | 456111 0
brd 1601 1 | 47 -203 357 -190 -187 -17610 88.1 2007 2007 | 407604 0
brd 1601 2 | -30 -138 153 -1380 253 -10050 87.3 1922 1922 | 460926 0
brd 1601 3 | 8 -53 324 -482 -572 -5699 88.1 1989 1989 | 460270 0
brd 1601 4 | 76 26 270 1978 -190 -7543 88.5 1851 1851 | 456735 0
brd 1601 5 | -58 86 179 -3010 -395 -11940 88.7 2351 2351 | 404086 0
brd 1601 6 | -45 -30 142 -595 -1432 -13270 84.6 2375 2375 | 408477 0
-------------+------------------------------------------------------------+----------------
brd 1601 mean| -3 -50 249 -384 -757 -11638 87.1 2178 2178 | 436315 0
brd 1601 sdev| 49 96 89 1604 1030 4219 1.9 325 325 | 27768 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 2.1601.0 GPS week: 1601 Day: 0 MJD: 55451
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]
--------+----------------------------------------------------+------------------------------
bkg 131| 2 1 -2 -19 -51 45 -.22 19 19 | 0 -1296 2882 3429
cod 230| -1 0 2 39 -11 21 -.09 19 18 | --- --- --- ---
esx 131| -1 -2 0 23 48 68 .45 20 19 | 119834 2884 4097 7549
gfz 198| -3 2 0 11 -128 65 -.18 27 23 | 295170 -2350 4108 6986
iac n/a| 0 0 -2 -72 -32 -155 -.19 22 22 | 458004 -1253 4097 7299
mcc n/a| 2 -4 32 15 -71 335 -.19 93 93 | --- --- --- ---
Table 2.1601.1 GPS week: 1601 Day: 1 MJD: 55452
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]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 0 -4 -72 -16 109 -.19 19 19 | 0 47 1617 1679
cod 230| 0 -2 2 94 32 -16 -.08 19 19 | --- --- --- ---
esx 131| -1 0 4 21 24 27 .44 21 20 | 74126 -797 4305 9671
gfz 198| 0 1 -1 -105 -27 52 -.09 26 31 | 240265 -1618 4294 8813
iac n/a| 1 2 -3 -74 -31 -155 -.23 25 25 | 408202 -402 4290 9157
mcc n/a| 15 2 27 -157 -30 702 .12 111 111 | --- --- --- ---
Table 2.1601.2 GPS week: 1601 Day: 2 MJD: 55453
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]
--------+----------------------------------------------------+------------------------------
bkg 131| 1 1 -2 13 18 133 -.16 18 18 | 0 158 1669 1716
cod 230| -1 -1 0 40 -36 -29 -.09 17 15 | --- --- --- ---
esx 131| -2 -1 2 -21 14 -63 .47 21 19 | 118395 -2133 3978 8838
gfz 198| -2 0 -1 -73 25 -62 -.10 30 26 | 295837 -5388 3978 7835
iac n/a| 0 2 -1 -49 -5 -55 -.31 28 28 | 461826 -1417 3988 7996
mcc n/a| -2 0 40 -2 38 -363 .02 87 87 | --- --- --- ---
Table 2.1601.3 GPS week: 1601 Day: 3 MJD: 55454
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]
--------+----------------------------------------------------+------------------------------
bkg 131| -1 1 0 50 -9 -19 -.16 19 19 | 0 -83 1956 2034
cod 230| 0 -1 1 -39 0 -9 -.15 19 20 | --- --- --- ---
esx 131| 0 0 1 -39 1 -12 .43 20 18 | 112805 -1506 3654 6784
gfz 198| 0 1 -1 44 -9 -41 -.16 26 23 | 288658 -2823 3653 6330
iac n/a| 2 -1 -6 -5 5 59 -.26 31 31 | 459576 -1414 3644 6637
mcc n/a| -3 0 48 21 83 23 .34 96 96 | --- --- --- ---
Table 2.1601.4 GPS week: 1601 Day: 4 MJD: 55455
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]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 1 -6 29 -24 -120 -.25 21 21 | 0 -19 1602 1668
cod 230| 0 0 3 36 2 52 -.14 18 17 | --- --- --- ---
esx 131| 0 -2 2 -29 59 21 .48 19 19 | 108764 159 3961 7172
gfz 198| -2 0 0 -19 -117 83 -.14 25 29 | 282046 1514 3974 6642
iac n/a| 0 2 -4 -39 -39 112 -.32 29 29 | 456027 386 3956 7154
mcc n/a| -4 -1 11 51 56 234 -.56 99 99 | --- --- --- ---
Table 2.1601.5 GPS week: 1601 Day: 5 MJD: 55456
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]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 1 -9 -10 19 180 -.22 23 23 | 0 188 1593 1650
cod 230| -2 0 -8 19 -22 66 -.12 16 15 | --- --- --- ---
esx 131| 0 -3 -1 26 17 38 .42 20 19 | 55515 1316 3854 7406
gfz 198| 3 -1 -5 -73 0 66 -.14 28 24 | 230685 -1215 3848 7071
iac n/a| 1 4 41 -64 11 -571 -.29 36 36 | 406228 -2804 3871 7530
mcc n/a| 0 12 -34 -180 118 489 -.29 138 138 | --- --- --- ---
Table 2.1601.6 GPS week: 1601 Day: 6 MJD: 55457
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]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 0 -9 -8 -12 0 -.19 24 23 | 0 126 2031 2141
cod 230| -1 0 -2 20 -20 178 -.08 16 15 | --- --- --- ---
esx 131| 1 -1 -2 -5 58 188 .41 24 22 | 64818 -3244 4426 7868
gfz 198| 1 4 1 -24 -76 118 -.08 31 24 | 234480 -2175 4440 7824
iac n/a| 3 4 35 -70 -21 -903 -.25 39 39 | 407963 1192 4437 7923
mcc n/a| 6 17 -25 -253 -133 1043 .47 188 188 | --- --- --- ---
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 3.1601.0 GPS week: 1601 Day: 0 MJD: 55451
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1748 11 39 18 28 30 --- 15 | 29 64 30 26 18 --- 31
R02 | 2259 18 26 23 23 26 --- 13 | 28 50 37 33 23 --- 28
R04 | 2706 14 18 18 24 13 --- 9 | 30 52 41 46 35 --- 38
R05 | 734 12 15 23 16 23 --- 10 | 42 59 42 52 51 --- 46
R07 | 3861 12 24 25 23 24 --- 12 | 33 60 36 53 34 --- 38
R08 | 4522 21 25 13 35 24 136 12 | 23 60 42 49 40 36 39
R10 | 1342 19 15 22 29 24 --- 11 | 47 35 37 34 38 --- 36
R11 | 981 38 25 28 46 35 --- 18 | 39 61 61 45 55 --- 50
R13 | 1362 19 8 27 28 23 --- 11 | 26 23 35 30 28 --- 23
R14 | 1860 11 11 16 26 13 --- 7 | 34 33 30 32 35 --- 30
R15 | 3670 20 12 17 25 18 63 10 | 32 34 37 33 39 42 33
R17 | 1398 23 15 18 30 23 --- 11 | 58 62 71 57 80 --- 65
R18 | 1225 12 14 8 23 18 --- 7 | 18 18 27 22 34 --- 19
R19 | 739 19 13 9 21 18 --- 8 | 12 21 22 14 31 --- 17
R20 | 4827 30 13 15 18 23 --- 12 | 43 50 50 46 47 --- 46
R21 | 3202 23 9 13 21 15 --- 9 | 31 23 39 39 31 --- 28
R22 | 2900 15 10 13 24 12 --- 7 | 18 24 33 30 31 --- 24
R23 | 4840 12 15 19 20 14 58 9 | 20 22 36 31 33 35 24
R24 | 1231 19 18 35 36 21 --- 14 | 16 24 45 33 29 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2751 19 19 20 27 22 93 |T 30 40 39 37 37 37 33
WRMS | 2751 19 18 19 23 22 93 |NE 30 40 39 37 37 37 33
MEDI | 1860 19 15 18 24 23 63 |MD 30 35 37 33 34 36 31
Table 3.1601.1 GPS week: 1601 Day: 1 MJD: 55452
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3743 27 21 35 21 39 --- 17 | 27 43 64 34 17 --- 31
R02 | 1602 16 40 11 19 32 --- 15 | 22 39 16 27 30 --- 13
R04 | 2812 13 18 18 19 17 --- 9 | 25 39 31 26 29 --- 29
R05 | 1104 11 24 21 22 19 --- 11 | 27 38 28 38 21 --- 26
R07 | 1502 16 16 19 36 21 --- 10 | 35 33 50 19 33 --- 34
R08 | 1974 18 14 21 21 18 160 10 | 25 34 52 24 30 43 33
R10 | 1665 10 14 25 27 24 --- 10 | 33 36 30 32 29 --- 28
R11 | 1168 38 26 26 27 58 --- 22 | 31 51 65 65 54 --- 45
R13 | 1559 16 15 20 20 18 --- 10 | 26 28 28 27 26 --- 22
R14 | 1166 19 18 22 20 20 --- 11 | 27 28 30 24 28 --- 22
R15 | 2635 18 10 15 36 22 62 9 | 30 22 30 35 31 41 25
R17 | 1665 18 12 20 28 16 --- 9 | 44 46 46 48 57 --- 46
R18 | 1410 11 14 20 29 19 --- 9 | 13 21 33 29 30 --- 17
R19 | 612 16 15 18 32 21 --- 10 | 12 28 29 30 23 --- 16
R20 | 1298 16 17 19 27 19 --- 10 | 48 38 45 44 31 --- 38
R21 | 2442 21 17 30 26 23 --- 13 | 21 22 47 40 21 --- 23
R22 | 2678 19 15 11 24 16 --- 9 | 20 28 23 31 26 --- 18
R23 | 2953 22 12 26 28 16 87 11 | 31 36 41 31 39 40 31
R24 | 1029 14 14 12 24 14 --- 8 | 13 28 19 26 25 --- 13
------+-----------------------------------------+-------------------------------------
RMS | 2006 19 19 21 26 25 111 |T 26 33 37 33 30 41 26
WRMS | 2006 19 19 20 31 25 111 |NE 26 33 37 33 30 41 26
MEDI | 1602 16 15 20 26 19 87 |MD 27 34 31 31 29 41 26
Table 3.1601.2 GPS week: 1601 Day: 2 MJD: 55453
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3455 18 38 36 37 34 --- 18 | 24 39 38 42 27 --- 17
R02 | 2335 14 13 18 19 41 --- 12 | 19 30 36 32 26 --- 19
R04 | 2386 15 22 18 20 16 --- 10 | 27 46 33 36 29 --- 32
R05 | 1080 20 21 22 38 32 --- 13 | 27 49 49 30 24 --- 34
R07 | 1686 11 14 14 23 26 --- 9 | 46 52 43 47 35 --- 43
R08 | 2179 23 15 22 27 23 133 12 | 22 37 50 39 25 56 30
R10 | 3066 24 13 22 49 22 --- 12 | 25 37 38 54 31 --- 28
R11 | 1349 36 26 28 29 43 --- 19 | 35 54 65 59 56 --- 47
R13 | 1100 20 15 17 34 27 --- 11 | 31 25 28 30 29 --- 21
R14 | 986 12 22 21 24 40 --- 14 | 25 26 42 34 29 --- 24
R15 | 2033 13 12 11 27 19 44 8 | 19 26 24 30 33 32 22
R17 | 1010 17 13 26 39 23 --- 11 | 52 48 62 57 66 --- 52
R18 | 1060 15 9 15 30 19 --- 8 | 9 21 24 28 23 --- 14
R19 | 665 10 8 17 21 22 --- 8 | 16 15 23 24 29 --- 13
R20 | 1657 14 15 15 43 28 --- 10 | 21 29 27 35 31 --- 23
R21 | 1181 13 8 17 25 25 --- 9 | 14 18 31 28 27 --- 18
R22 | 1813 17 13 23 24 25 --- 11 | 24 28 48 39 29 --- 28
R23 | 2965 12 14 16 28 19 53 8 | 32 32 32 37 45 43 31
R24 | 1403 15 12 25 19 20 --- 10 | 12 16 36 24 28 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 1921 18 17 21 30 28 87 |T 25 33 38 37 32 43 27
WRMS | 1921 18 15 19 26 28 87 |NE 25 33 38 37 32 43 27
MEDI | 1657 15 14 18 27 25 53 |MD 24 30 36 35 29 43 24
Table 3.1601.3 GPS week: 1601 Day: 3 MJD: 55454
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3385 23 21 29 16 52 --- 17 | 19 41 49 26 46 --- 24
R02 | 2365 17 23 19 23 30 --- 12 | 32 39 30 28 19 --- 25
R04 | 1305 25 30 24 20 40 --- 16 | 24 43 50 46 44 --- 33
R05 | 637 10 28 30 24 18 --- 13 | 39 46 31 29 30 --- 31
R07 | 1637 21 29 22 37 40 --- 16 | 29 58 56 62 38 --- 39
R08 | 1774 11 20 11 17 34 133 11 | 37 51 43 46 37 32 36
R10 | 4200 24 15 27 30 21 --- 13 | 39 37 50 37 41 --- 36
R11 | 1378 24 15 17 26 26 --- 12 | 41 57 54 47 49 --- 46
R13 | 1263 21 18 14 34 20 --- 10 | 22 31 38 30 30 --- 25
R14 | 1083 18 23 15 25 31 --- 12 | 20 22 27 32 41 --- 20
R15 | 2132 9 12 13 29 26 40 8 | 26 31 41 51 37 26 30
R17 | 561 22 20 18 17 22 --- 12 | 54 66 60 50 82 --- 60
R18 | 2599 15 9 9 18 18 --- 7 | 17 18 26 27 29 --- 16
R19 | 612 9 10 13 23 16 --- 7 | 16 20 19 23 25 --- 15
R20 | 3232 22 14 17 20 42 --- 13 | 36 32 37 33 33 --- 28
R21 | 1197 16 16 15 17 29 --- 10 | 23 23 31 25 34 --- 20
R22 | 831 21 10 18 41 22 --- 10 | 20 19 31 39 30 --- 19
R23 | 1254 18 13 31 22 33 90 13 | 21 25 56 37 40 38 32
R24 | 1303 16 11 20 31 35 --- 11 | 16 19 36 29 44 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 1988 19 19 20 26 31 96 |T 27 35 40 36 38 32 29
WRMS | 1988 19 20 18 23 31 96 |NE 27 35 40 36 38 32 29
MEDI | 1305 18 16 18 23 29 90 |MD 24 32 38 33 37 32 28
Table 3.1601.4 GPS week: 1601 Day: 4 MJD: 55455
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2627 16 27 23 21 12 --- 12 | 19 27 39 29 29 --- 19
R02 | 1521 18 12 13 28 23 --- 9 | 20 30 37 33 44 --- 24
R04 | 1002 13 20 17 18 36 --- 12 | 21 31 35 29 32 --- 21
R05 | 945 29 27 27 21 25 --- 16 | 22 47 53 32 26 --- 34
R07 | 2353 10 22 21 30 18 --- 11 | 31 47 30 50 36 --- 30
R08 | 759 23 25 22 23 28 110 14 | 26 46 38 45 40 14 30
R10 | 3047 15 13 30 27 40 --- 14 | 24 25 39 31 40 --- 22
R11 | 950 22 32 20 23 44 --- 17 | 42 49 51 47 50 --- 42
R13 | 1446 34 20 23 27 27 --- 15 | 35 21 47 40 44 --- 26
R14 | 2179 36 16 19 25 40 --- 16 | 18 18 26 25 43 --- 17
R15 | 4003 19 14 17 23 35 63 12 | 22 20 31 28 46 20 21
R17 | 666 26 13 13 20 24 --- 11 | 53 61 68 55 81 --- 62
R18 | 2564 11 17 18 21 22 --- 10 | 13 20 20 19 38 --- 14
R19 | 984 10 13 16 43 19 --- 8 | 27 15 28 39 33 --- 16
R20 | 1346 23 15 18 32 37 --- 13 | 35 40 42 23 33 --- 32
R21 | 1189 15 9 17 18 27 --- 9 | 18 18 26 26 40 --- 17
R22 | 889 17 11 19 24 19 --- 9 | 26 24 44 31 30 --- 27
R23 | 1236 15 11 14 16 36 117 11 | 22 18 25 20 37 30 20
R24 | 1124 20 11 12 18 12 --- 8 | 22 15 25 25 34 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 1851 21 18 19 25 29 99 |T 26 30 37 33 39 21 25
WRMS | 1851 21 17 19 29 29 99 |NE 26 30 37 33 39 21 25
MEDI | 1236 18 15 18 23 27 110 |MD 22 25 37 31 38 20 22
Table 3.1601.5 GPS week: 1601 Day: 5 MJD: 55456
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1245 17 32 28 27 40 --- 17 | 11 36 42 38 24 --- 21
R02 | 2038 13 12 17 27 22 --- 9 | 18 28 27 23 40 --- 23
R04 | 1898 20 10 10 22 32 --- 9 | 31 28 35 32 38 --- 30
R05 | 1993 23 24 11 15 32 --- 12 | 19 42 34 39 25 --- 30
R07 | 1758 24 16 20 22 31 --- 12 | 31 39 33 31 57 --- 32
R08 | 1503 25 14 14 20 31 119 11 | 32 54 47 37 63 16 46
R10 | 2276 25 11 19 40 39 --- 12 | 42 33 36 47 32 --- 31
R11 | 1437 35 14 16 50 53 --- 16 | 40 49 46 68 55 --- 43
R13 | 1304 22 8 21 25 30 --- 11 | 28 28 32 34 31 --- 21
R14 | 2740 49 12 28 20 40 --- 18 | 19 18 26 25 33 --- 16
R15 | 6008 17 12 23 31 54 131 14 | 21 20 29 32 39 16 19
R17 | 1391 21 21 24 30 31 --- 13 | 36 51 58 53 66 --- 47
R18 | 3557 17 6 14 20 26 --- 8 | 14 24 26 20 22 --- 15
R19 | 1164 17 11 13 20 26 --- 9 | 16 19 18 16 28 --- 10
R20 | 2044 22 9 16 32 38 --- 11 | 26 24 33 38 46 --- 25
R21 | 2320 24 19 39 35 32 --- 16 | 19 15 49 33 28 --- 18
R22 | 830 16 16 16 18 36 --- 11 | 16 23 29 23 38 --- 17
R23 | 1996 14 15 13 23 38 161 11 | 12 21 37 37 46 32 23
R24 | 1906 12 16 18 21 29 --- 10 | 20 19 30 24 33 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 2351 23 16 20 28 36 138 |T 23 30 35 34 39 21 25
WRMS | 2351 23 15 19 24 36 138 |NE 23 30 35 34 39 21 25
MEDI | 1906 21 14 17 23 32 131 |MD 20 28 33 33 38 16 23
Table 3.1601.6 GPS week: 1601 Day: 6 MJD: 55457
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1041 23 21 18 27 49 --- 15 | 41 59 52 62 30 --- 43
R02 | 3588 17 19 23 15 41 --- 13 | 26 42 48 39 30 --- 32
R04 | 1769 31 13 33 16 31 --- 15 | 20 37 66 48 37 --- 38
R05 | 2890 13 13 16 21 32 --- 10 | 34 47 41 45 33 --- 38
R07 | 3197 24 19 14 37 36 --- 13 | 33 49 42 55 33 --- 37
R08 | 2236 27 21 25 28 39 137 15 | 33 62 63 48 39 33 47
R10 | 2173 7 8 13 36 38 --- 9 | 37 33 33 46 44 --- 32
R11 | 1046 42 18 38 65 55 --- 21 | 54 58 72 69 62 --- 59
R13 | 1021 20 15 32 23 41 --- 15 | 22 28 51 35 33 --- 25
R14 | 1587 41 20 15 28 46 --- 17 | 19 20 24 27 36 --- 17
R15 | 5554 37 17 15 31 47 184 16 | 27 21 29 29 41 29 23
R17 | 2801 22 13 11 41 42 --- 12 | 55 65 74 58 100 --- 68
R18 | 1778 14 17 20 22 38 --- 12 | 11 24 21 19 40 --- 18
R19 | 839 19 17 18 19 31 --- 11 | 11 22 20 15 35 --- 14
R20 | 2071 16 12 18 29 40 --- 11 | 33 33 41 42 52 --- 33
R21 | 1185 13 11 15 18 31 --- 9 | 17 14 29 21 33 --- 17
R22 | 964 22 21 54 34 32 --- 20 | 17 19 57 23 40 --- 21
R23 | 2054 20 10 21 38 24 231 10 | 19 26 42 36 37 40 27
R24 | 1923 19 11 23 28 28 --- 11 | 24 20 40 26 43 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2375 24 16 24 31 39 188 |T 28 35 44 39 42 34 32
WRMS | 2375 23 15 22 24 39 188 |NE 28 35 44 39 42 34 32
MEDI | 1923 20 17 18 28 38 184 |MD 26 33 42 39 37 33 32
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