[IGSREPORT-15035] Wk 1422 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Apr 26 01:31:56 PDT 2007
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IGS Electronic Report 26 Apr 01:32:02 PDT 2007 Message Number 15035
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1422 (Apr 08, 2007 - Apr 14, 2007)
Contact: Gerd Gendt (gendt at gfz-potsdam.de)
Thomas Nischan ( nisn at gfz-potsdam.de)
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 2.1422.
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:
igl1422[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1422 in the SP3 format.
igl14227.sum Combination Report for GPS Week 1422.
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 | 872.5 ns
1 | 867.0 ns
2 | 894.6 ns
3 | 897.1 ns
4 | 877.5 ns
5 | 821.3 ns
6 | 804.0 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESX | R24
1 | ESX | R24
2 | ESX | R24
3 | ESX | R24
4 | ESX | R24
5 | ESX | R24
6 | COD | R22
6 | ESX | R18 R21 R22 R23 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 1.1422, 1a.1422).
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 2.1422.0-6)
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 3.1422.0-6).
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 1422 summary. (Apr 08, 2007 - Apr 14, 2007)
Table 1.1422.a GPS week : 1422 MJD: 54198.0-54204.0
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 57| -1 0 2 135 -37 -68 -.01 37 30 | 0 1311 5346 5742
| 3 4 4 49 53 144 .16 | 0 1623
cod 165| -1 0 8 148 -51 182 -.14 44 34 | --- --- --- ---
| 5 2 6 79 49 159 .11 | --- ---
esx 46| 2 0 -8 14 -44 -203 -.18 159 52 | 22397 5147 15467 25651
| 5 7 12 141 117 175 .16 | 22541 19673
iac n/a| -1 0 -4 -223 92 1 .19 30 30 | 861572 -185 14446 24693
| 1 2 8 44 55 166 .09 | 37658 11305
mcc n/a| 0 0 -2 -132 33 48 -.02 798 798 | --- --- --- ---
| 3 5 13 174 119 118 .20 | --- ---
Table 1.1422.b GPS week : 1422 MJD: 54198.0-54204.0
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 | 19 20 17 19 14 19 17 |
R02 | 14 18 20 14 19 19 16 |
R03 | 23 27 42 33 25 20 16 |
R04 | 16 17 15 19 18 18 20 |
R06 | 20 21 14 21 23 25 12 |
R07 | 16 26 22 27 24 24 19 |
R08 | 19 19 17 16 28 35 70 |
R10 | 25 15 16 15 27 26 18 |
R14 | 25 17 15 27 20 19 16 |
R19E | 20 23 19 25 27 23 21 |
R23E | 0 226 0 0 0 81 58 |
R24E | 27 32 25 38 30 32 25 |
Table 1.1422.c GPS week : 1422 MJD: 54198.0-54204.0
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 1422 0 | -359 334 -295 -803 5923 -381800 93.2 5242 5242 | 872474 0
brd 1422 1 | -609 -42 -622 -4907 -7646 -388300 105.5 5201 5201 | 867031 0
brd 1422 2 | 458 -125 55 -6423 96 -400300 90.5 7693 7693 | 894552 0
brd 1422 3 | 912 -589 430 213 9536 -378700 100.6 9060 9060 | 897119 0
brd 1422 4 | 883 -379 627 260 -485 -372600 96.3 15300 15300 | 877488 0
brd 1422 5 | 96 -17 746 2549 7200 -371000 91.8 13900 13900 | 821339 0
brd 1422 6 | -809 157 677 -4854 4439 -387100 110.5 16100 16100 | 804033 0
-------------+------------------------------------------------------------+----------------
brd 1422 mean| 81 -94 231 -1994 2723 -382828 98.3 10356 10356 | 862005 0
brd 1422 sdev| 700 311 532 3373 5836 10133 7.5 4681 4681 | 35780 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 2.1422.0 GPS week: 1422 Day: 0 MJD: 54198
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 57| -3 -3 -3 116 -107 72 .14 26 24 | 0 1360 5725 6095
cod 165| -2 0 13 89 25 127 -.14 32 32 | --- --- --- ---
esx 46| 4 6 8 13 -70 -197 -.03 136 38 | 36150 -29501 16563 18805
iac n/a| -1 0 -15 -219 127 -136 .27 29 29 | 879541 -23871 16581 20999
mcc n/a| 0 -10 19 -237 -146 -36 -.18 516 516 | --- --- --- ---
Table 2.1422.1 GPS week: 1422 Day: 1 MJD: 54199
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 57| 4 6 5 95 -23 -257 -.00 41 37 | 0 3562 6056 6304
cod 165| -10 1 16 274 -109 273 -.34 44 35 | --- --- --- ---
esx 46| 5 1 0 12 24 -139 .08 118 46 | 20128 7805 20511 26894
iac n/a| 0 2 -15 -174 73 114 .16 23 23 | 858400 9410 19564 26948
mcc n/a| 7 -2 -11 -268 183 63 -.31 424 424 | --- --- --- ---
Table 2.1422.2 GPS week: 1422 Day: 2 MJD: 54200
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 57| -3 -3 0 133 -40 -210 -.05 23 23 | 0 904 3546 3813
cod 165| 0 0 6 77 -18 119 -.14 36 33 | --- --- --- ---
esx 46| -3 3 0 128 -210 -134 -.27 125 41 | 35135 -9234 16044 34876
iac n/a| 0 -4 -3 -292 142 249 .01 27 27 | 902396 -3673 14141 32992
mcc n/a| -4 8 -24 -419 196 309 .32 355 355 | --- --- --- ---
Table 2.1422.3 GPS week: 1422 Day: 3 MJD: 54201
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 57| 0 6 6 99 -48 -164 -.06 36 34 | 0 -522 5844 6761
cod 165| -6 -3 6 94 -73 20 -.12 41 30 | --- --- --- ---
esx 46| -7 -7 -7 225 -42 -160 -.31 156 48 | 24783 13192 10030 21462
iac n/a| -2 2 -8 -250 111 80 .18 33 33 | 890652 7414 9339 19712
mcc n/a| 0 0 0 0 0 0 .0 1266 1266 | --- --- --- ---
Table 2.1422.4 GPS week: 1422 Day: 4 MJD: 54202
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 57| -7 -4 9 104 67 42 .24 32 28 | 0 1575 4827 5177
cod 165| 1 4 -1 87 -61 -13 -.01 31 25 | --- --- --- ---
esx 46| 5 4 -20 -201 -155 -79 -.32 142 59 | 41651 28841 14546 20835
iac n/a| -3 1 6 -233 151 3 .30 43 43 | 878598 3065 13189 19294
mcc n/a| 0 0 0 0 0 0 .0 1073 1073 | --- --- --- ---
Table 2.1422.5 GPS week: 1422 Day: 5 MJD: 54203
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 57| 0 -3 -2 168 -64 98 -.08 39 29 | 0 -734 5556 5854
cod 165| 3 0 12 190 -103 359 -.21 38 36 | --- --- --- ---
esx 46| 4 3 -9 -107 -3 -592 -.11 127 62 | 24612 21812 14892 29760
iac n/a| 0 0 -1 -232 32 -249 .21 32 32 | 820718 5494 13190 27138
mcc n/a| 0 0 0 0 0 0 .0 1082 1082 | --- --- --- ---
Table 2.1422.6 GPS week: 1422 Day: 6 MJD: 54204
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 57| 0 -1 1 232 -43 -57 -.27 63 38 | 0 3032 5869 6195
cod 165| 5 2 5 223 -17 387 -.04 88 49 | --- --- --- ---
esx 46| 8 -15 -28 27 143 -121 -.31 306 66 | -25674 3114 15688 26927
iac n/a| -2 1 5 -160 8 -50 .17 23 23 | 800703 866 15120 25771
mcc n/a| 0 0 0 0 0 0 .0 875 875 | --- --- --- ---
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 3.1422.0 GPS week: 1422 Day: 0 MJD: 54198
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2471 32 31 46 17 --- 18 | 30 41 38 32 --- 26
R02 | 3536 18 22 32 27 --- 14 | 39 32 39 26 --- 23
XR03 |52844 29 22 --- 40 --- 22 | 46 42 --- 37 --- 29
R04 | 7342 17 35 38 20 --- 15 | 25 41 43 22 --- 22
R06 | 4396 31 30 51 29 --- 20 | 28 21 46 36 --- 25
R07 | 4360 14 25 32 34 83 15 | 28 29 40 32 5 23
R08 | 4363 28 36 32 30 --- 18 | 61 42 76 42 --- 47
XR10 | 5856 37 32 --- 33 --- 24 | 48 34 --- 20 --- 28
XR14 | 2669 37 33 --- 33 --- 24 | 32 54 --- 45 --- 32
R19E | 7829 27 34 48 28 --- 19 | 73 77 65 82 --- 70
XR23E | 5908 --- 11 --- --- --- 0 | --- 387 --- --- --- 372
R24E | 5347 33 40 370 42 725 27 | 99 113 186 126 142 109
------+------------------------------------+--------------------------------
RMS | 5241 26 32 136 29 516 |T 46 76 66 45 73 67
WRMS | 5241 24 32 38 29 516 |NE 37 37 47 32 5 28
MEDI | 4396 29 31 38 30 83 |MD 39 41 43 36 5 28
Table 3.1422.1 GPS week: 1422 Day: 1 MJD: 54199
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3159 39 24 56 19 --- 19 | 29 42 40 26 --- 24
R02 | 3066 32 31 44 22 --- 18 | 47 37 42 28 --- 30
XR03 |55389 20 57 --- 34 --- 27 | 50 39 --- 44 --- 42
R04 | 2268 40 35 28 18 --- 17 | 32 45 35 20 --- 24
R06 | 4589 36 55 27 23 --- 20 | 39 31 32 27 --- 22
R07 | 6533 28 66 69 23 102 26 | 25 69 65 23 6 25
R08 | 6241 22 46 48 17 --- 18 | 51 64 94 23 --- 50
XR10 | 3005 21 24 --- 18 --- 14 | 32 28 --- 24 --- 20
XR14 | 5266 30 22 --- 19 --- 16 | 28 29 --- 27 --- 23
R19E | 5008 55 45 43 22 --- 23 | 57 111 105 85 --- 82
XR23E | 5267 --- 209 243 --- --- 226 | --- 179 149 --- --- 273
R24E | 8007 61 36 312 37 590 31 | 81 102 122 91 152 86
------+------------------------------------+--------------------------------
RMS | 5201 41 44 118 23 423 |T 42 64 76 38 79 58
WRMS | 5201 37 35 46 23 423 |NE 37 42 51 26 6 28
MEDI | 5008 32 36 48 22 102 |MD 39 42 65 27 6 25
Table 3.1422.2 GPS week: 1422 Day: 2 MJD: 54200
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4088 29 27 38 26 --- 17 | 35 41 45 21 --- 24
R02 | 3922 6 36 72 21 --- 19 | 31 40 45 35 --- 26
XR03 |44414 60 45 --- 66 --- 42 | 96 33 --- 39 --- 50
R04 | 2878 26 17 41 23 --- 15 | 36 48 65 27 --- 36
R06 |12000 21 31 18 21 --- 13 | 42 36 34 30 --- 29
R07 | 9658 19 53 59 28 134 22 | 29 35 59 39 8 24
R08 |10827 12 37 43 26 --- 16 | 51 36 72 46 --- 47
XR10 | 3769 15 28 --- 24 --- 16 | 31 24 --- 20 --- 20
XR14 | 6211 12 28 --- 23 --- 14 | 30 47 --- 29 --- 28
R19E | 5595 32 35 30 31 --- 18 | 59 56 79 77 --- 62
XR23E | 6921 --- 9 --- --- --- 0 | --- 398 --- --- --- 404
R24E | 6867 26 41 334 39 484 25 | 91 97 143 86 400 84
------+------------------------------------+--------------------------------
RMS | 7692 23 36 125 27 355 |T 48 74 67 40 204 69
WRMS | 7692 23 33 41 27 355 |NE 42 37 53 31 8 31
MEDI | 6211 21 31 41 26 134 |MD 36 40 59 35 8 29
Table 3.1422.3 GPS week: 1422 Day: 3 MJD: 54201
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6076 37 28 38 30 --- 19 | 40 36 62 28 --- 27
R02 | 4806 27 24 29 17 --- 14 | 41 39 30 37 --- 26
XR03 |33011 29 63 --- 41 --- 32 | 40 40 --- 42 --- 31
R04 | 3467 38 22 43 26 --- 18 | 31 33 68 48 --- 32
R06 |10999 20 53 35 26 --- 20 | 46 53 57 44 --- 35
R07 |11407 36 39 69 40 --- 26 | 40 58 64 32 --- 35
R08 |15748 31 24 33 22 --- 16 | 71 56 98 42 --- 64
XR10 | 4762 26 20 --- 19 --- 15 | 35 35 --- 27 --- 30
XR14 | 7002 25 52 --- 31 --- 26 | 32 73 --- 36 --- 34
R19E | 6177 49 57 34 26 --- 24 | 54 86 104 77 --- 71
XR23E | 6600 --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
R24E | 6877 41 57 426 59 1265 38 | 84 103 229 78 461 79
------+------------------------------------+--------------------------------
RMS | 9059 36 41 156 33 1265 |T 46 55 89 44 461 42
WRMS | 9059 34 30 48 33 1265 |NE 41 47 63 37 --- 34
MEDI | 6600 31 28 35 26 1265 |MD 40 53 64 42 461 34
Table 3.1422.4 GPS week: 1422 Day: 4 MJD: 54202
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7061 22 15 40 26 --- 14 | 31 32 42 30 --- 26
R02 | 5906 30 20 58 33 --- 19 | 43 47 62 33 --- 36
R03 |37285 31 30 66 55 --- 24 | 49 44 52 31 --- 29
R04 | 2555 20 24 38 45 --- 17 | 26 34 47 48 --- 28
R06 |13845 26 42 56 43 --- 23 | 39 97 54 48 --- 52
R07 | 9754 26 32 48 61 --- 23 | 37 49 95 77 --- 48
R08 |15869 43 27 91 45 --- 27 | 59 56 88 25 --- 56
XR10 | 5324 38 27 --- 49 --- 26 | 34 32 --- 57 --- 26
XR14 | 8645 35 23 --- 24 --- 20 | 30 52 --- 42 --- 35
R19E | 8387 41 32 93 30 --- 27 | 61 78 89 79 --- 63
XR23E | 4182 --- 7 --- --- --- 0 | --- 695 --- --- --- 703
R24E | 4135 40 45 387 42 1072 30 | 85 101 213 98 240 92
------+------------------------------------+--------------------------------
RMS |15302 32 31 142 43 1072 |T 44 109 82 51 240 99
WRMS |15302 28 25 59 43 1072 |NE 38 49 62 43 --- 37
MEDI | 7061 31 27 58 43 1072 |MD 39 49 62 48 240 36
Table 3.1422.5 GPS week: 1422 Day: 5 MJD: 54203
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6195 16 27 73 26 --- 19 | 47 37 81 31 --- 35
R02 | 7866 15 26 75 21 --- 18 | 42 40 74 36 --- 39
R03 |35131 22 41 60 23 --- 19 | 25 33 40 36 --- 28
R04 | 2810 23 42 40 24 --- 18 | 30 58 45 37 --- 29
R06 | 5877 48 47 48 34 --- 25 | 23 62 36 45 --- 34
R07 | 4441 18 38 88 34 --- 24 | 37 25 63 63 --- 39
R08 |15410 76 28 108 36 --- 34 | 117 98 151 43 --- 110
XR10 | 3293 44 27 --- 37 --- 26 | 39 50 --- 30 --- 24
XR14 | 6452 24 26 --- 27 --- 18 | 32 32 --- 41 --- 27
R19E | 9247 48 40 52 27 --- 23 | 48 64 49 63 --- 53
XR23E | 2986 134 68 --- 124 --- 81 | 88 258 --- 11 --- 222
R24E | 4454 36 46 323 51 1081 32 | 72 71 182 107 314 80
------+------------------------------------+--------------------------------
RMS |13902 39 38 127 32 1081 |T 50 69 80 45 314 60
WRMS |13902 29 36 62 32 1081 |NE 43 48 70 40 --- 40
MEDI | 5877 24 38 73 27 1081 |MD 39 50 63 37 314 35
Table 3.1422.6 GPS week: 1422 Day: 6 MJD: 54204
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3350 37 38 59 13 --- 16 | 55 32 69 31 --- 28
R02 | 8582 26 33 71 11 --- 15 | 43 53 84 25 --- 32
R03 |38205 29 28 72 12 --- 15 | 35 34 38 24 --- 22
R04 | 4736 31 63 66 14 --- 19 | 23 59 81 43 --- 30
R06 | 9058 14 40 39 9 --- 11 | 38 32 50 28 --- 23
R07 | 5436 19 51 83 14 --- 18 | 31 32 58 42 --- 22
R08 |26335 132 208 256 36 --- 69 | 130 143 277 41 --- 115
XR10 | 3680 26 53 --- 12 --- 17 | 36 33 --- 37 --- 26
XR14 | 6495 26 37 --- 15 --- 15 | 26 35 --- 38 --- 28
R19 |13826 57 43 40 21 --- 20 | 92 95 75 85 --- 85
R23 | 2939 117 124 772 51 --- 58 | 54 246 113 9 --- 223
R24 | 4523 35 76 497 15 875 24 | 135 146 326 153 260 145
------+------------------------------------+--------------------------------
RMS |16101 63 88 306 23 875 |T 58 78 117 46 260 64
WRMS |16101 38 49 66 23 875 |NE 58 78 117 46 260 64
MEDI | 5436 29 43 71 14 875 |MD 38 35 75 37 260 28
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