[IGSREPORT-19492] Wk 1622 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Feb 24 05:10:45 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1622 (Feb 06, 2011 - Feb 12, 2011)
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 2.1622.
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:
igl1622[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1622 in the SP3 format.
igl16227.sum Combination Report for GPS Week 1622.
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. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics initially.
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 | 349.5 ns
1 | 358.4 ns
2 | 379.9 ns
3 | 347.1 ns
4 | 385.8 ns
5 | 340.5 ns
6 | 365.7 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
----+--------+---------------
1 | GFZ | R07
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 1.1622, 1a.1622).
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 2.1622.0-6)
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 3.1622.0-6).
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 1622 summary. (Feb 06, 2011 - Feb 12, 2011)
Table 1.1622.a GPS week : 1622 MJD: 55598.0-55604.0
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 148| 0 0 2 -11 -11 9 -.14 30 28 | 0 554 3191 3526
| 2 1 4 27 27 230 .04 | 0 1088
cod 238| -1 0 0 22 -45 -14 -.15 17 15 | --- --- --- ---
| 0 0 1 23 44 36 .04 | --- ---
esx 150| 0 0 -4 10 68 8 .39 27 23 | -1435 -2742 4636 9699
| 1 2 1 44 43 65 .05 | 21232 2986
gfz 189| 1 -1 -6 -23 9 11 -.20 43 29 | 212544 -1795 4504 9302
| 2 2 3 68 99 61 .06 | 18311 2420
grg 135| 0 -1 10 -10 20 -29 .19 54 52 | --- --- --- ---
| 4 2 3 31 33 45 .16 | --- ---
iac n/a| 0 0 10 -39 17 2 .05 41 41 | 168805 -310 4621 151479
| 1 1 7 37 31 117 .07 | 515675 1064
mcc n/a| 0 0 40 -26 30 402 -.14 143 143 | --- --- --- ---
| 4 2 16 74 60 303 .25 | --- ---
Table 1.1622.b GPS week : 1622 MJD: 55598.0-55604.0
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 14 11 13 11 15 16 |
R02 | 15 10 12 12 10 9 10 |
R05 | 8 11 13 11 12 17 13 |
R06 | 8 11 18 14 12 14 10 |
R07 | 12 13 11 17 10 11 23 |
R08 | 9 10 11 11 9 11 12 |
R09 | 11 9 10 9 9 13 10 |
R10 | 11 9 14 10 9 12 11 |
R11 | 15 24 23 20 17 16 16 |
R12 | 9 7 10 8 8 10 8 |
R13 | 11 12 11 12 10 9 10 |
R15 | 10 10 10 11 11 11 9 |
R16 | 8 7 8 10 13 12 8 |
R17 | 23 16 27 19 20 19 22 |
R18 | 11 11 14 13 18 21 18 |
R19 | 23 14 16 16 14 12 15 |
R20 | 21 29 18 17 18 19 18 |
R21 | 13 15 14 15 14 18 14 |
R22 | 16 16 16 16 13 15 19 |
R23 | 13 15 17 15 18 18 17 |
R24 | 19 17 15 17 15 27 16 |
Table 1.1622.c GPS week : 1622 MJD: 55598.0-55604.0
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 1622 0 | -35 -1 146 682 -1760 556 86.6 1748 1748 | 349500 0
brd 1622 1 | 14 -19 150 -423 -2594 -3689 83.9 1982 1982 | 358434 0
brd 1622 2 | 11 21 131 -2190 -1243 -4760 85.8 3832 3832 | 379928 0
brd 1622 3 | 66 27 205 -921 1760 -8552 84.3 5469 5469 | 347078 0
brd 1622 4 | -17 116 272 -2412 2211 -10960 89.1 4898 4898 | 385811 0
brd 1622 5 | 103 33 279 958 481 -10100 86.6 3768 3768 | 340506 0
brd 1622 6 | 6 70 272 2052 -754 -9922 89.5 1996 1996 | 365674 0
-------------+------------------------------------------------------------+----------------
brd 1622 mean| 21 35 208 -321 -271 -6775 86.5 3384 3384 | 360990 0
brd 1622 sdev| 48 45 66 1658 1809 4261 2.1 1503 1503 | 17070 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 2.1622.0 GPS week: 1622 Day: 0 MJD: 55598
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 148| -2 1 4 37 39 247 -.12 26 24 | 0 306 3603 3928
cod 238| -2 0 0 -8 -65 -50 -.11 15 13 | --- --- --- ---
esx 150| 0 -3 -3 -49 -18 -100 .46 28 24 | -13281 -200 4253 9501
gfz 189| 6 -2 -6 34 92 -71 -.15 36 23 | 201568 957 4041 8449
grg 135| 3 -1 9 9 -47 1 -.03 59 54 | --- --- --- ---
iac n/a| 0 0 0 -13 76 60 -.05 34 34 | 348634 -487 4268 9859
mcc n/a| 1 0 21 -10 143 346 -.36 138 138 | --- --- --- ---
Table 2.1622.1 GPS week: 1622 Day: 1 MJD: 55599
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 148| 2 0 3 -6 -23 -99 -.11 25 21 | 0 2269 3141 3456
cod 238| -1 2 0 -6 -27 -1 -.10 17 15 | --- --- --- ---
esx 150| -2 0 -2 -25 70 12 .41 34 24 | -2301 -2135 5453 8196
gfz 189| -1 -1 -7 87 24 48 -.14 54 33 | 212430 -1514 4651 7417
grg 135| -7 0 8 19 17 2 .05 56 53 | --- --- --- ---
iac n/a| 2 1 3 -12 7 128 .10 38 38 | 359057 -388 5446 8199
mcc n/a| 0 -3 13 70 75 554 -.22 197 197 | --- --- --- ---
Table 2.1622.2 GPS week: 1622 Day: 2 MJD: 55600
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 148| 1 -1 -2 -8 -41 -309 -.20 34 34 | 0 1941 3073 3365
cod 238| -1 0 1 21 17 59 -.12 19 16 | --- --- --- ---
esx 150| 1 0 -5 61 108 70 .37 26 23 | 29834 -8538 4929 12508
gfz 189| -1 3 -9 -21 -135 57 -.24 36 29 | 235830 -5254 4943 12174
grg 135| 2 -3 16 -73 42 -6 .27 54 57 | --- --- --- ---
iac n/a| 0 -1 17 -92 -25 9 .09 38 38 | 382440 -1924 4922 12728
mcc n/a| 8 0 44 -78 -7 -48 .18 107 107 | --- --- --- ---
Table 2.1622.3 GPS week: 1622 Day: 3 MJD: 55601
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 148| 1 -3 -1 -36 -28 223 -.19 31 29 | 0 -380 4157 4813
cod 238| 0 0 -1 33 -10 -23 -.17 17 15 | --- --- --- ---
esx 150| 0 2 -2 41 109 -1 .41 24 20 | -13707 -1954 4913 9201
gfz 189| 1 0 -4 -115 -108 6 -.23 35 34 | 199302 -3380 4971 9201
grg 135| 0 -2 12 9 44 -68 .34 51 50 | --- --- --- ---
iac n/a| 1 0 14 -90 27 -218 .10 41 41 | -999999 -342 4811 999999
mcc n/a| 0 0 49 -155 10 64 .10 147 147 | --- --- --- ---
Table 2.1622.4 GPS week: 1622 Day: 4 MJD: 55602
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 148| -3 0 6 -24 4 238 -.14 29 28 | 0 -47 2599 2878
cod 238| 0 0 -2 57 -79 -42 -.15 15 15 | --- --- --- ---
esx 150| 0 -2 -3 20 57 -21 .30 26 22 | 23753 -3679 4364 8248
gfz 189| 1 -4 -11 -86 108 -76 -.12 33 30 | 237849 -3908 4343 8376
grg 135| 7 0 12 1 18 -109 .08 50 51 | --- --- --- ---
iac n/a| 1 0 17 -37 29 -30 .05 40 40 | 386330 -293 4362 8820
mcc n/a| -5 1 56 -44 -38 786 .03 135 135 | --- --- --- ---
Table 2.1622.5 GPS week: 1622 Day: 5 MJD: 55603
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 148| 1 1 8 4 -3 -215 -.13 34 29 | 0 105 3455 3779
cod 238| -3 0 0 31 -114 -9 -.18 20 18 | --- --- --- ---
esx 150| 0 1 -6 -30 87 104 .36 30 26 | -29536 614 4292 10570
gfz 189| 2 -2 -6 -19 92 61 -.27 29 22 | 189479 459 4249 10364
grg 135| 1 -4 5 -25 15 16 .38 56 52 | --- --- --- ---
iac n/a| 1 0 14 -22 0 112 .09 50 50 | 338788 1723 4291 11047
mcc n/a| -5 1 47 32 4 471 -.26 111 111 | --- --- --- ---
Table 2.1622.6 GPS week: 1622 Day: 6 MJD: 55604
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 148| 0 1 -3 -44 -27 -18 -.08 29 28 | 0 -313 2313 2466
cod 238| -1 0 2 28 -40 -30 -.19 19 17 | --- --- --- ---
esx 150| 0 -1 -5 53 61 -1 .39 22 20 | -4813 -3303 4250 9674
gfz 189| 2 -2 0 -43 -7 52 -.25 80 31 | 211353 72 4334 9138
grg 135| 0 3 7 -12 54 -39 .21 52 46 | --- --- --- ---
iac n/a| 0 0 7 -4 9 -45 -.03 45 45 | 366386 -460 4252 9705
mcc n/a| 3 3 48 -2 27 642 -.46 165 165 | --- --- --- ---
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 3.1622.0 GPS week: 1622 Day: 0 MJD: 55598
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1610 24 17 20 24 56 36 --- 11 | 51 60 53 57 39 37 --- 51
R02 | 1499 27 17 23 60 55 17 --- 14 | 39 33 46 83 31 31 --- 37
R05 | 2678 17 7 16 13 44 23 35 7 | 44 43 46 45 31 32 48 39
R06 | 2175 16 11 18 27 38 9 --- 8 | 33 42 38 31 36 37 --- 38
R07 | 1605 11 17 26 45 66 15 --- 11 | 45 49 49 81 48 51 --- 48
R08 | 1407 18 11 19 21 52 22 78 8 | 29 40 41 45 33 27 52 33
R09 | 1054 19 16 30 29 63 22 --- 11 | 27 27 53 49 46 23 --- 29
R10 | 1370 18 11 31 18 40 27 --- 10 | 21 21 32 33 32 26 --- 20
R11 | 730 41 16 20 46 71 29 120 14 | 28 33 46 66 53 30 27 32
R12 | 1649 18 12 20 18 36 22 --- 8 | 38 22 30 33 25 28 --- 25
R13 | 2160 27 15 27 25 46 16 --- 11 | 34 23 42 38 34 30 --- 28
R15 | 2870 20 14 18 29 58 18 61 9 | 27 21 30 23 47 23 23 21
R16 | 947 16 10 18 18 45 15 --- 7 | 26 23 37 32 35 26 --- 24
XR17E | 6806 57 16 50 --- 55 40 --- 23 | 35 43 70 --- 52 65 --- 46
R18E | 1689 27 12 25 26 37 28 --- 11 | 36 26 36 37 25 35 --- 24
R19E | 1231 56 19 50 62 61 48 --- 22 | 57 46 63 65 59 48 --- 41
R20E | 1905 38 25 42 43 127 66 --- 20 | 133 162 149 161 179 152 --- 150
R21E | 1962 22 18 21 34 57 40 --- 13 | 31 39 50 55 60 52 --- 38
R22E | 948 28 15 32 24 53 55 --- 15 | 26 36 53 42 34 48 --- 33
R23E | 2427 24 14 23 31 63 44 265 13 | 95 111 105 114 120 96 108 103
R24E | 1049 18 18 48 59 35 47 --- 18 | 41 36 54 39 50 49 --- 33
------+----------------------------------------------+------------------------------------------
RMS | 1747 26 15 28 36 59 33 138 |T 42 44 53 56 50 45 51 42
WRMS | 1747 24 13 24 23 54 33 138 |NE 34 33 41 47 37 30 37 32
MEDI | 1610 22 15 23 27 55 27 78 |MD 35 36 46 45 39 35 48 33
Table 3.1622.1 GPS week: 1622 Day: 1 MJD: 55599
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1469 20 11 23 36 68 50 --- 13 | 28 38 51 68 22 19 --- 36
R02 | 838 10 17 25 21 89 22 --- 9 | 22 29 49 35 65 35 --- 29
R05 | 1453 20 18 22 30 59 22 44 11 | 23 27 37 42 59 22 46 24
R06 | 1618 24 10 20 27 58 29 --- 10 | 21 21 29 39 81 29 --- 23
R07 | 2066 21 11 21 200 63 39 --- 12 | 18 36 39 194 42 51 --- 31
R08 | 574 14 14 14 35 46 23 124 10 | 40 38 40 49 36 37 66 37
R09 | 1162 19 11 27 16 48 16 --- 9 | 23 14 37 21 41 21 --- 16
R10 | 2596 16 19 14 18 37 23 --- 9 | 16 32 27 35 30 25 --- 21
R11 | 706 47 33 68 42 47 44 126 23 | 23 43 65 57 35 22 28 31
R12 | 779 8 12 14 14 62 24 --- 7 | 18 18 25 23 39 23 --- 18
R13 | 2318 15 19 24 35 63 25 --- 11 | 14 21 43 51 54 36 --- 24
R15 | 2912 12 16 19 26 36 28 61 10 | 23 28 28 47 34 16 38 24
R16 | 646 10 10 13 19 34 18 --- 6 | 18 19 20 29 30 14 --- 15
XR17E | 4003 26 13 27 --- 79 46 --- 15 | 29 33 45 --- 58 49 --- 33
R18E | 3746 18 9 17 23 54 41 --- 10 | 35 38 39 41 60 35 --- 33
R19E | 2012 29 20 30 27 69 34 --- 13 | 54 64 81 76 109 43 --- 61
R20E | 3375 63 25 88 41 59 66 --- 28 | 102 120 168 130 120 106 --- 116
R21E | 586 21 18 24 46 50 44 --- 14 | 33 35 36 41 45 44 --- 25
R22E | 1141 22 17 33 39 51 50 --- 15 | 35 37 51 52 46 53 --- 34
R23E | 3197 20 17 36 27 51 53 396 14 | 110 117 121 124 126 109 184 114
R24E | 1252 15 18 40 47 57 57 --- 17 | 23 29 46 37 56 55 --- 28
------+----------------------------------------------+------------------------------------------
RMS | 1982 25 17 34 54 56 38 197 |T 33 39 51 59 56 40 72 36
WRMS | 1982 21 15 24 33 53 38 197 |NE 22 28 37 53 43 26 44 25
MEDI | 1469 20 17 24 27 57 34 124 |MD 23 33 40 42 46 35 46 29
Table 3.1622.2 GPS week: 1622 Day: 2 MJD: 55600
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1083 15 13 13 36 65 36 --- 11 | 48 39 35 42 51 19 --- 34
R02 | 559 23 12 21 31 51 41 --- 12 | 45 22 45 44 30 26 --- 26
R05 | 1054 46 8 22 32 55 16 117 12 | 33 35 59 61 33 32 71 38
XR06 |>>>>> 35 18 --- --- 85 26 --- 17 | 27 29 --- --- 69 19 --- 19
R07 | 2434 18 18 25 30 69 15 --- 10 | 33 40 32 52 46 39 --- 34
R08 | 564 22 17 14 35 58 27 67 11 | 31 42 39 59 32 44 25 39
R09 | 889 26 12 22 26 30 19 --- 10 | 31 24 42 44 34 22 --- 26
R10 | 3372 30 27 31 29 37 14 --- 13 | 17 37 41 29 38 23 --- 21
R11 | 937 72 31 46 42 66 32 87 22 | 26 38 62 74 65 31 39 37
R12 | 1750 29 18 15 14 54 22 --- 10 | 35 26 26 34 52 18 --- 20
R13 | 2761 26 15 23 25 56 19 --- 10 | 27 31 43 39 46 31 --- 29
R15 | 5629 27 11 13 32 61 17 74 9 | 23 21 24 33 49 22 29 18
R16 | 1532 13 14 15 22 59 18 --- 8 | 31 17 27 31 48 27 --- 20
R17E |12928 53 30 35 92 67 60 --- 26 | 39 42 57 105 69 65 --- 43
R18E | 5043 25 16 27 33 50 45 65 14 | 41 23 42 28 43 37 44 20
R19E | 2128 40 15 30 29 57 47 --- 15 | 53 72 90 80 100 41 --- 65
R20E | 3924 41 25 30 42 34 52 --- 18 | 66 63 88 90 77 84 --- 70
R21E | 962 31 20 24 22 37 46 --- 14 | 50 39 68 69 71 75 --- 53
R22E | 748 30 20 27 34 37 54 --- 16 | 35 35 57 47 41 62 --- 36
R23E | 2750 27 19 29 32 55 61 184 16 | 61 62 48 63 48 65 154 53
R24E | 2340 31 15 25 26 62 57 --- 15 | 36 28 46 36 60 52 --- 30
------+----------------------------------------------+------------------------------------------
RMS | 3831 34 19 26 36 54 38 107 |T 37 36 48 53 52 39 60 34
WRMS | 3831 34 16 23 29 57 38 107 |NE 31 30 39 45 45 27 41 27
MEDI | 2128 29 17 24 31 56 32 74 |MD 35 35 43 44 48 32 39 34
Table 3.1622.3 GPS week: 1622 Day: 3 MJD: 55601
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1570 38 16 20 29 73 36 --- 13 | 45 58 46 68 51 38 --- 49
R02 | 1414 23 12 21 38 53 24 --- 11 | 32 30 26 47 37 34 --- 25
R05 | 963 25 14 24 24 42 25 111 11 | 49 49 33 55 38 43 32 42
XR06 | 1837 23 16 --- --- --- 24 --- 14 | 25 46 --- --- --- 32 --- 36
R07 | 3303 32 18 21 67 67 27 --- 16 | 38 42 38 90 43 31 --- 38
R08 | 1576 18 14 10 42 54 18 42 10 | 42 36 33 45 54 33 24 32
R09 | 1854 13 14 19 28 36 19 --- 9 | 28 21 32 32 40 26 --- 18
R10 | 4908 21 17 9 26 46 28 --- 9 | 23 32 29 28 32 30 --- 21
R11 | 988 51 26 49 25 48 46 110 19 | 29 43 67 38 30 30 32 38
R12 | 2336 15 13 13 23 54 22 --- 8 | 27 20 28 34 48 23 --- 20
R13 | 2070 23 16 25 23 24 33 --- 11 | 23 26 39 46 43 44 --- 27
R15 | 5902 24 9 25 26 50 30 81 10 | 29 37 40 57 36 35 29 33
R16 | 2184 31 17 16 9 36 23 --- 10 | 36 24 30 17 48 25 --- 21
R17E |21308 33 20 20 70 67 47 --- 18 | 43 43 48 83 57 61 --- 45
R18E | 4511 18 18 19 27 52 54 51 13 | 42 31 55 62 67 54 14 41
R19E | 2465 43 19 17 32 50 55 --- 15 | 95 104 91 95 115 72 --- 91
R20E | 2619 38 22 35 31 42 56 --- 17 | 90 77 95 84 96 77 --- 79
R21E | 672 38 18 24 29 34 49 --- 15 | 58 69 85 64 88 85 --- 67
R22E | 1347 31 16 35 29 82 59 --- 16 | 53 55 54 57 89 66 --- 49
R23E | 1027 32 17 20 29 35 59 308 15 | 118 130 128 135 130 127 66 126
R24E | 3293 32 16 27 43 41 61 --- 17 | 36 25 45 38 56 52 --- 25
------+----------------------------------------------+------------------------------------------
RMS | 5468 31 17 24 35 51 41 147 |T 45 47 52 58 59 48 32 43
WRMS | 5468 29 15 20 34 50 41 147 |NE 32 35 36 46 41 32 29 30
MEDI | 2070 31 16 20 29 48 33 81 |MD 38 42 40 55 48 38 29 38
Table 3.1622.4 GPS week: 1622 Day: 4 MJD: 55602
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1073 23 19 22 24 51 28 --- 11 | 47 67 44 70 58 50 --- 55
R02 | 1819 22 7 18 29 36 25 --- 9 | 34 36 31 52 31 27 --- 31
R05 | 839 43 5 17 29 45 30 105 12 | 27 42 44 68 24 29 26 40
R06 | 1842 25 12 12 46 50 21 --- 11 | 46 52 63 94 35 57 --- 56
R07 | 3600 22 8 20 32 62 22 --- 10 | 23 30 42 43 48 31 --- 29
R08 | 1281 15 12 15 29 36 16 36 8 | 19 34 38 34 34 23 16 28
R09 | 1445 18 17 13 20 43 28 --- 9 | 26 19 26 38 45 21 --- 19
R10 | 3792 21 9 18 14 44 31 --- 8 | 21 21 40 29 33 35 --- 22
R11 | 1078 40 22 33 34 58 54 72 17 | 27 31 55 40 45 27 21 30
R12 | 2822 19 8 20 19 35 16 --- 8 | 19 24 28 25 26 27 --- 19
R13 | 600 23 8 18 29 57 29 --- 10 | 20 36 40 46 43 35 --- 31
R15 | 5692 22 9 16 36 35 36 115 11 | 17 29 38 50 37 25 22 27
R16 | 1381 21 23 27 37 39 20 --- 13 | 24 17 43 47 42 16 --- 20
R17E |19173 24 17 60 47 73 52 --- 19 | 33 40 74 64 68 61 --- 41
R18E | 2497 45 17 31 43 32 53 74 17 | 37 32 46 49 29 50 14 30
R19E | 2684 35 11 23 35 71 51 --- 14 | 36 42 53 62 92 55 --- 41
R20E | 4240 34 24 41 32 65 58 --- 18 | 53 58 66 66 56 58 --- 50
R21E | 1151 36 11 16 35 41 48 --- 13 | 59 74 71 80 76 86 --- 70
R22E | 1111 22 15 30 27 37 47 --- 13 | 35 42 54 53 84 55 --- 42
R23E | 2353 45 20 31 37 53 55 272 17 | 56 82 94 93 116 79 66 77
R24E | 3640 23 13 25 41 60 61 --- 15 | 39 47 66 48 36 78 --- 47
------+----------------------------------------------+------------------------------------------
RMS | 4898 29 15 26 33 50 40 135 |T 33 40 50 54 50 44 27 38
WRMS | 4898 28 14 22 30 51 40 135 |NE 26 33 40 48 38 31 21 31
MEDI | 1842 23 12 20 32 45 31 74 |MD 33 36 44 50 43 35 21 31
Table 3.1622.5 GPS week: 1622 Day: 5 MJD: 55603
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1172 31 23 35 17 86 44 --- 14 | 44 51 68 54 60 26 --- 49
R02 | 1028 15 15 15 13 35 32 --- 8 | 27 19 25 35 24 15 --- 17
R05 | 1022 35 37 21 24 67 56 124 17 | 37 61 31 37 41 27 54 36
R06 | 1280 38 9 40 16 70 23 --- 13 | 20 45 79 52 51 40 --- 45
XR07 | 3623 19 12 16 --- 63 31 --- 10 | 34 35 44 --- 58 52 --- 38
R08 | 1197 24 13 22 23 52 24 69 10 | 25 34 38 41 36 24 22 27
R09 | 637 20 24 27 30 49 20 --- 12 | 27 22 42 46 35 20 --- 23
R10 | 1924 25 20 30 13 57 34 --- 12 | 21 18 40 32 28 33 --- 17
R11 | 1771 27 25 33 31 52 49 59 16 | 37 31 38 28 42 19 33 23
R12 | 1204 19 13 23 16 43 25 --- 9 | 21 26 41 32 29 19 --- 23
R13 | 1214 24 12 17 11 41 22 --- 8 | 21 31 32 25 37 20 --- 23
R15 | 3840 26 14 18 30 60 22 111 11 | 24 35 21 37 29 23 32 24
R16 | 848 25 19 27 18 42 27 --- 11 | 38 15 53 45 62 26 --- 31
R17E |15271 17 19 27 56 55 66 --- 18 | 42 43 50 65 60 78 --- 36
R18E | 1172 53 22 27 38 49 79 88 20 | 41 47 41 39 66 67 14 36
R19E | 2074 21 16 19 19 47 50 --- 12 | 47 42 36 44 43 46 --- 36
R20E | 1365 49 20 29 30 60 70 --- 18 | 89 72 71 68 74 73 --- 68
R21E | 1560 32 20 31 33 78 77 --- 18 | 71 83 102 81 81 108 --- 82
R22E | 811 24 17 17 27 --- 67 --- 14 | 38 33 40 35 --- 64 --- 34
R23E | 2407 50 19 30 34 37 58 175 18 | 111 100 92 109 112 119 104 101
R24E | 1431 65 22 64 53 46 71 --- 26 | 60 42 76 67 77 73 --- 47
------+----------------------------------------------+------------------------------------------
RMS | 3767 34 20 29 29 56 50 111 |T 41 42 50 48 52 46 43 38
WRMS | 3767 29 18 26 22 51 50 111 |NE 28 32 42 38 40 26 35 28
MEDI | 1280 25 19 27 24 52 44 88 |MD 37 35 41 41 43 33 32 36
Table 3.1622.6 GPS week: 1622 Day: 6 MJD: 55604
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2465 24 33 14 52 50 30 --- 15 | 45 68 59 62 43 52 --- 57
R02 | 1387 16 19 20 28 43 21 --- 10 | 30 33 43 46 37 31 --- 33
R05 | 1041 19 26 29 15 42 30 94 12 | 58 63 38 41 61 38 63 45
R06 | 768 16 17 16 27 45 22 --- 9 | 42 48 46 42 38 35 --- 41
R07 | 1884 34 17 32 97 71 20 --- 22 | 37 44 61 81 56 50 --- 45
R08 | 2331 27 12 22 36 68 15 139 11 | 24 41 53 55 38 32 47 37
R09 | 590 26 22 12 14 26 23 --- 10 | 31 22 35 37 41 29 --- 26
R10 | 1223 25 15 19 31 36 25 --- 11 | 22 18 33 40 33 28 --- 21
R11 | 2207 27 25 23 42 58 51 68 16 | 39 35 46 41 47 38 30 34
R12 | 1247 18 11 10 20 29 26 --- 8 | 28 25 28 30 25 27 --- 24
R13 | 3095 21 16 19 14 43 25 --- 9 | 35 34 44 35 38 31 --- 34
R15 | 3497 22 7 13 25 46 17 67 8 | 20 21 25 37 28 32 42 22
R16 | 1249 21 12 13 18 52 22 --- 8 | 23 27 27 28 47 24 --- 22
R17E | 1710 39 14 20 329 78 78 --- 21 | 45 50 48 195 65 79 --- 49
R18E | 997 34 22 26 24 45 74 --- 18 | 28 32 43 30 56 62 --- 29
R19E | 2123 26 16 24 28 65 56 --- 14 | 41 35 35 40 34 49 --- 33
R20E | 3619 30 28 27 31 48 72 --- 18 | 76 67 70 74 76 88 --- 68
R21E | 1971 17 13 29 22 46 59 --- 14 | 60 83 73 80 87 96 --- 75
R22E | 972 40 21 30 39 72 62 --- 18 | 27 35 64 56 67 55 --- 40
R23E | 2458 52 19 22 31 43 49 313 17 | 62 67 66 70 77 70 150 63
R24E | 966 36 15 21 35 45 60 --- 16 | 42 26 40 31 51 59 --- 30
------+----------------------------------------------+------------------------------------------
RMS | 1995 29 19 22 80 52 45 165 |T 38 41 46 54 49 47 66 39
WRMS | 1995 28 17 20 31 46 45 165 |NE 33 36 41 44 40 34 45 33
MEDI | 1710 26 17 21 28 46 30 94 |MD 37 35 44 41 47 38 47 34
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