[IGSREPORT-14889] Wk 1416 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Mar 15 07:40:19 PDT 2007
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IGS Electronic Report 15 Mar 07:40:43 PDT 2007 Message Number 14889
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1416 (Feb 25, 2007 - Mar 03, 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 2.1416.
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:
igl1416[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1416 in the SP3 format.
igl14167.sum Combination Report for GPS Week 1416.
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 | 693.2 ns
1 | 726.2 ns
2 | 713.9 ns
3 | 655.4 ns
4 | 747.7 ns
5 | 747.8 ns
6 | 743.4 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
----+--------+---------------
4 | IAC | R03
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 1.1416, 1a.1416).
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 2.1416.0-6)
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 3.1416.0-6).
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 1416 summary. (Feb 25, 2007 - Mar 03, 2007)
Table 1.1416.a GPS week : 1416 MJD: 54156.0-54162.0
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 55| -3 -1 8 83 -36 -12 -.15 48 37 | 0 867 3993 4298
| 2 4 4 45 52 202 .08 | 0 451
cod 165| 0 1 -8 128 -33 44 -.08 44 38 | --- --- --- ---
| 3 3 7 69 52 121 .09 | --- ---
esx 42| 1 0 22 241 57 -65 -.33 195 68 | -172392 -144253 358699 592906
| 5 4 12 152 81 218 .14 | 584460 379245
iac n/a| -1 0 -13 -251 61 -20 .34 43 43 | 401697 -136884 385756 561196
| 3 4 4 31 24 55 .08 | 724282 381819
mcc n/a| 1 -6 -15 -180 22 501 .24 305 305 | --- --- --- ---
| 17 24 26 460 117 458 1.12 | --- ---
Table 1.1416.b GPS week : 1416 MJD: 54156.0-54162.0
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 | 31 28 23 32 22 17 19 |
R02 | 17 18 20 15 20 18 20 |
R03 | 0 0 0 0 0 0 488 |
R04 | 26 15 16 17 23 24 15 |
R06 | 33 31 24 22 18 27 24 |
R07 | 23 30 24 20 22 18 20 |
R08 | 22 38 23 23 37 37 17 |
R10 | 30 33 29 23 24 40 19 |
R14 | ---- ---- ---- ---- 131 26 34 |
R15 | 0 0 0 0 0 0 0 |
R18 | 23 56 27 40 36 49 39 |
R19 | 20 20 27 25 23 13 16 |
R21 | 26 31 81 0 0 112 93 |
R22 | 25 28 31 28 39 27 23 |
R23 | 71 79 76 71 66 76 75 |
R24 | 77 78 85 68 84 73 83 |
Table 1.1416.c GPS week : 1416 MJD: 54156.0-54162.0
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 1416 0 | 243 362 -1181 934 -25350 -381900 87.0 6604 6604 | 693197 0
brd 1416 1 | 180 266 -1031 3422 -18890 -374500 97.1 5245 5245 | 726155 0
brd 1416 2 | -244 23 -1207 1941 -14630 -375900 90.1 5919 5919 | 713907 0
brd 1416 3 | -434 -270 -1290 682 -14270 -360600 92.6 8786 8786 | 655386 0
brd 1416 4 | -146 -270 -1047 6026 -11900 -358500 94.6 6445 6445 | 747735 0
brd 1416 5 | -68 338 -780 -3928 -10960 -363000 86.5 7863 7863 | 747821 0
brd 1416 6 | 307 72 -1068 -2099 -2454 -386600 105.2 7952 7952 | 743409 0
-------------+------------------------------------------------------------+----------------
brd 1416 mean| -23 74 -1086 996 -14064 -371571 93.3 6973 6973 | 718230 0
brd 1416 sdev| 276 267 164 3316 7072 10989 6.5 1261 1261 | 34248 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 2.1416.0 GPS week: 1416 Day: 0 MJD: 54156
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 55| -2 -1 10 137 -26 -12 -.17 42 34 | 0 1591 4207 4548
cod 165| 0 1 -23 47 -34 101 -.06 42 35 | --- --- --- ---
esx 42| -1 -1 42 110 92 -5 -.42 191 57 | 348507 -999999 999999 999999
iac n/a| 5 2 -12 -224 64 -87 .25 45 45 | 960007 -999999 999999 999999
Table 2.1416.1 GPS week: 1416 Day: 1 MJD: 54157
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 55| 0 4 11 81 -83 240 -.04 60 49 | 0 1237 3729 4143
cod 165| -6 -6 -6 61 -36 -70 -.01 43 29 | --- --- --- ---
esx 42| -3 -7 21 214 137 -396 -.25 187 71 | -999999 -20380 297956 999999
iac n/a| 2 4 -15 -304 43 -76 .49 54 54 | -178454 -4485 505277 999999
mcc n/a| 19 -31 -3 617 13 1299 1.64 489 489 | --- --- --- ---
Table 2.1416.2 GPS week: 1416 Day: 2 MJD: 54158
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 55| -5 0 7 38 -107 21 -.24 47 31 | 0 746 4113 4249
cod 165| 1 1 -12 223 57 -11 .04 54 44 | --- --- --- ---
esx 42| 12 2 30 245 39 -131 -.60 184 77 | -35959 -31191 31473 201290
iac n/a| -1 1 -6 -256 65 49 .35 45 45 | 675062 -13595 37541 171784
mcc n/a| -30 0 -5 -84 28 521 -.46 340 340 | --- --- --- ---
Table 2.1416.3 GPS week: 1416 Day: 3 MJD: 54159
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 55| 0 -3 14 136 -50 -415 -.21 54 41 | 0 993 4025 4256
cod 165| 0 2 -10 97 -17 252 -.13 38 36 | --- --- --- ---
esx 42| 2 0 5 481 69 179 -.19 183 78 | -35018 64201 86787 167529
iac n/a| -3 1 -6 -258 82 31 .38 38 38 | 674067 12157 37343 61543
mcc n/a| -1 27 16 -766 -126 22 -.51 234 234 | --- --- --- ---
Table 2.1416.4 GPS week: 1416 Day: 4 MJD: 54160
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 55| -7 -10 7 14 43 84 -.05 51 36 | 0 790 3833 4206
cod 165| 4 4 -8 218 -114 -108 -.19 46 40 | --- --- --- ---
esx 42| 2 7 10 42 122 191 -.24 200 60 | 239896 27528 58483 405271
iac n/a| -5 4 -17 -255 89 -16 .33 43 43 | 828622 29551 73361 357945
mcc n/a| 10 9 -6 -337 135 311 1.53 203 203 | --- --- --- ---
Table 2.1416.5 GPS week: 1416 Day: 5 MJD: 54161
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 55| -4 -3 1 84 -41 -67 -.23 46 34 | 0 312 3085 3371
cod 165| 2 6 2 117 -17 97 -.05 45 42 | --- --- --- ---
esx 42| 0 0 28 395 49 -26 -.37 198 72 | -999999 -1370 999999 999999
iac n/a| -3 -6 -17 -258 16 16 .33 45 45 | -999999 56467 999999 999999
mcc n/a| 7 -7 -47 -389 -85 687 .25 353 353 | --- --- --- ---
Table 2.1416.6 GPS week: 1416 Day: 6 MJD: 54162
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 55| -3 1 5 90 12 61 -.11 39 30 | 0 401 4962 5313
cod 165| 0 1 -3 132 -70 50 -.18 43 39 | --- --- --- ---
esx 42| 0 -3 19 202 -108 -266 -.26 224 61 | 275824 -48564 36200 376260
iac n/a| 0 -6 -15 -205 65 -59 .24 34 34 | 852576 -38288 46772 337103
mcc n/a| 4 -35 -49 -123 171 165 -1.03 213 213 | --- --- --- ---
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 3.1416.0 GPS week: 1416 Day: 0 MJD: 54156
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 6330 48 35 75 65 30 | 97 122 109 107 107
R02 | 6030 26 29 47 26 17 | 41 48 47 52 41
XR03 | ---- --- 14 --- --- 0 | --- 242 --- --- 466
R04 | 5317 52 23 49 50 25 | 50 45 46 60 44
R06 |13591 35 47 150 39 33 | 37 61 70 40 34
R07 | 4742 22 40 84 36 23 | 43 46 75 24 28
R08 | 7143 36 38 52 31 21 | 30 60 67 60 43
XR10 | 5208 42 43 --- 43 30 | 64 46 --- 32 42
XR15 | ---- --- 14 --- --- 0 | --- 329 --- --- 329
XR18 | 3726 --- 26 54 31 23 | --- 194 199 190 198
R19 | 8053 28 39 25 39 20 | 45 54 48 58 46
R21 | 2968 35 34 99 39 25 | 23 103 133 55 90
R22 | 5307 37 52 56 31 24 | 60 70 82 80 61
R23 | 2287 48 47 396 71 71 | 54 76 136 92 51
R24 | 3112 67 62 432 41 76 | 742 732 769 720 731
------+-------------------------------+---------------------------
RMS | 6603 42 42 191 45 |T 107 148 148 120 154
WRMS | 6603 34 35 57 45 |NE 107 148 148 120 154
MEDI | 5307 36 38 56 39 |MD 45 70 75 60 51
Table 3.1416.1 GPS week: 1416 Day: 1 MJD: 54157
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3732 61 34 62 39 --- 27 | 45 79 67 73 --- 53
R02 | 6430 25 18 87 13 --- 18 | 75 56 81 60 --- 60
XR03 | ---- --- 8 --- --- --- 0 | --- 337 --- --- --- 303
R04 | 6577 20 22 43 24 --- 14 | 54 68 46 73 --- 60
R06 | 5836 37 23 128 57 --- 31 | 52 53 58 64 --- 48
R07 | 6053 27 47 89 57 300 29 | 53 42 73 47 31 35
R08 | 4395 38 36 196 26 --- 38 | 47 43 160 54 --- 50
XR10 | 3249 29 46 --- 60 --- 33 | 55 61 --- 38 --- 45
XR15 | ---- --- 8 --- --- --- 0 | --- 9999 --- --- --- 9999
R18 | 3704 134 71 52 87 --- 56 | 171 133 124 129 --- 147
R19 | 8066 35 29 24 40 --- 19 | 37 61 57 56 --- 45
R21 | 5509 65 31 82 47 --- 30 | 20 112 130 57 --- 112
R22 | 2076 33 57 75 38 624 27 | 66 77 76 57 23 54
R23 | 2958 36 48 432 75 --- 79 | 41 53 147 60 --- 30
R24 | 4400 95 60 374 87 --- 77 | 512 479 537 486 --- 489
------+------------------------------------+--------------------------------
RMS | 5245 60 43 187 54 489 |T 94 118 129 96 27 109
WRMS | 5245 49 29 71 54 489 |NE 94 118 129 96 27 109
MEDI | 4400 36 34 82 47 300 |MD 53 61 76 60 23 53
Table 3.1416.2 GPS week: 1416 Day: 2 MJD: 54158
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2367 26 47 69 33 --- 23 | 57 63 80 61 --- 51
R02 | 5012 22 42 54 30 --- 19 | 65 63 84 79 --- 66
XR03 | ---- --- 15 --- --- --- 0 | --- 212 --- --- --- 397
R04 | 8908 20 28 47 25 --- 15 | 33 43 53 44 --- 30
R06 | 7919 47 30 79 25 --- 23 | 56 52 59 46 --- 39
R07 | 7167 43 52 42 26 94 23 | 67 30 58 27 20 32
R08 | 7216 34 39 57 39 --- 22 | 37 32 81 75 --- 43
XR10 | 8811 34 56 --- 30 --- 28 | 55 61 --- 34 --- 42
XR15 | ---- --- 15 --- --- --- 0 | --- 583 --- --- --- 579
R18 | 7930 46 52 76 30 --- 27 | 162 158 194 157 --- 157
R19 | 4062 21 72 57 33 --- 26 | 58 109 31 31 --- 49
XR21 | 7306 --- 86 288 33 --- 81 | --- 166 221 61 --- 132
R22 | 2920 27 62 124 35 472 31 | 40 105 149 42 23 56
R23 | 2777 49 69 393 83 --- 75 | 49 74 135 58 --- 39
R24 | 3672 110 73 417 82 --- 85 | 693 716 821 786 --- 736
------+------------------------------------+--------------------------------
RMS | 5918 47 54 184 45 340 |T 114 164 163 115 21 163
WRMS | 5918 31 44 77 45 340 |NE 114 164 163 115 21 163
MEDI | 7167 34 52 69 33 94 |MD 56 74 81 58 20 51
Table 3.1416.3 GPS week: 1416 Day: 3 MJD: 54159
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2322 68 32 134 29 --- 32 | 57 65 113 58 --- 49
R02 | 2752 28 22 47 17 --- 14 | 52 36 73 48 --- 34
XR03 | ---- --- 16 --- --- --- 0 | --- 170 --- --- --- 9999
R04 | 8610 26 32 54 20 --- 17 | 67 100 63 79 --- 76
R06 |18828 33 31 97 20 --- 21 | 44 39 109 49 --- 34
R07 | 9703 36 31 67 23 95 19 | 61 44 89 37 28 36
R08 |10340 28 35 85 33 --- 22 | 52 75 147 115 --- 84
XR10 | 6877 25 37 --- 30 --- 22 | 37 47 --- 45 --- 33
XR15 | ---- --- 16 --- --- --- 0 | --- 480 --- --- --- 484
R18 |12396 105 49 49 54 --- 39 | 201 176 177 147 --- 171
R19 | 1385 44 42 72 32 --- 24 | 63 92 101 42 --- 59
XR21 | ---- --- 16 --- --- --- 0 | --- 384 --- --- --- 382
R22 | 4680 60 33 107 26 317 28 | 77 56 104 43 21 44
R23 | 3115 38 56 403 62 --- 70 | 52 75 155 64 --- 52
R24 | 4383 65 46 381 61 --- 68 | 463 481 464 497 --- 477
------+------------------------------------+--------------------------------
RMS | 8785 54 38 183 38 234 |T 102 154 145 102 24 143
WRMS | 8785 41 36 78 38 234 |NE 102 154 145 102 24 143
MEDI | 4680 36 32 85 29 95 |MD 57 75 109 49 21 52
Table 3.1416.4 GPS week: 1416 Day: 4 MJD: 54160
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4526 39 38 31 36 --- 21 | 68 72 55 46 --- 46
R02 | 2747 30 38 36 34 --- 20 | 62 43 50 40 --- 37
XR03 | ---- --- 17 --- >>>> --- 0 | --- 155 --- 9999 --- 9999
R04 | 4601 39 31 49 43 --- 22 | 38 79 46 55 --- 48
R06 |10935 32 27 45 29 --- 17 | 48 48 42 63 --- 41
R07 | 7866 30 38 76 27 85 21 | 50 33 77 28 28 30
XR08 | ---- --- 39 98 45 --- 36 | --- 84 78 77 --- 70
XR10 | 8030 33 41 --- 23 --- 24 | 57 108 --- 61 --- 75
XR14 | 8774 135 126 --- --- --- 130 | 66 83 --- --- --- 52
XR15 | ---- --- 18 --- --- --- 0 | --- 393 --- --- --- 389
XR18 |12999 --- 47 48 53 --- 35 | --- 244 198 187 --- 207
R19 | 1413 49 32 50 30 --- 22 | 69 47 43 39 --- 41
XR21 |15433 --- 17 --- --- --- 0 | --- 502 --- --- --- 505
R22 | 7819 70 48 152 37 274 38 | 77 77 77 55 24 60
R23 | 7081 28 38 384 51 --- 66 | 49 58 130 67 --- 44
R24 | 5469 97 89 419 78 --- 84 | 658 692 798 722 --- 695
------+------------------------------------+--------------------------------
RMS | 6445 51 46 200 43 203 |T 112 169 144 120 26 156
WRMS | 6445 36 40 60 43 203 |NE 112 169 144 120 26 156
MEDI | 7819 39 38 50 37 85 |MD 62 79 77 55 24 52
Table 3.1416.5 GPS week: 1416 Day: 5 MJD: 54161
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7074 30 33 37 22 --- 17 | 71 61 75 52 --- 57
R02 | 5625 29 34 52 22 --- 18 | 41 56 74 32 --- 36
XR03 | ---- --- 9 --- >>>> --- 0 | --- 137 --- 9999 --- 9999
R04 | 2871 39 43 47 38 --- 23 | 62 61 48 50 --- 49
R06 | 4277 33 45 91 42 --- 27 | 29 53 72 44 --- 30
R07 | 8368 15 35 64 25 31 18 | 28 29 75 23 23 22
R08 |16183 77 32 59 74 --- 37 | 55 36 120 87 --- 45
XR10 | 6591 41 73 --- 48 --- 39 | 36 77 --- 46 --- 46
XR14 | 6764 32 39 --- 38 --- 26 | 43 80 --- 26 --- 45
XR15 | ---- --- 10 --- --- --- 0 | --- 732 --- --- --- 730
R18 |10446 77 86 154 65 --- 49 | 165 204 234 213 --- 201
R19 | 1995 23 20 38 20 --- 13 | 54 56 56 41 --- 46
XR21 |15112 --- 84 433 70 --- 111 | --- 123 243 63 --- 101
R22 | 9419 42 25 135 17 477 26 | 35 43 98 30 27 29
R23 | 4365 46 61 447 41 --- 76 | 72 92 112 61 --- 59
R24 | 4370 50 45 409 75 380 72 | 795 773 781 794 9 785
------+------------------------------------+--------------------------------
RMS | 7863 46 45 198 45 353 |T 114 163 165 111 19 152
WRMS | 7863 34 42 72 45 353 |NE 114 163 165 111 19 152
MEDI | 6591 39 35 64 41 380 |MD 54 61 75 46 23 46
Table 3.1416.6 GPS week: 1416 Day: 6 MJD: 54162
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |11980 32 30 41 31 --- 18 | 54 60 68 57 --- 54
R02 | 8735 35 41 56 22 --- 20 | 31 64 57 31 --- 30
XR03 | ---- --- 559 --- 426 --- 488 | --- 132 --- 9999 --- 9999
R04 | 5468 29 24 36 22 --- 15 | 50 40 45 34 --- 35
R06 | 4470 33 48 99 15 --- 23 | 38 68 68 34 --- 32
R07 |11066 17 28 97 25 51 19 | 34 50 78 23 26 27
R08 | 8374 23 32 34 31 --- 17 | 36 32 76 57 --- 36
XR10 | 3703 21 37 --- 20 --- 19 | 34 60 --- 34 --- 38
XR14 | 7676 45 54 --- 43 --- 33 | 47 61 --- 20 --- 41
XR15 | ---- --- 10 --- --- --- 0 | --- 834 --- --- --- 834
R18 |10605 58 76 142 37 --- 38 | 178 252 284 262 --- 257
R19 | 4130 26 29 46 22 --- 16 | 50 59 63 36 --- 43
XR21 |19954 --- 89 373 53 --- 93 | --- 138 253 63 --- 111
R22 | 9005 28 34 77 43 --- 23 | 73 46 86 73 --- 58
R23 | 2577 57 34 480 40 --- 75 | 80 70 196 69 --- 56
R24 | 3990 57 61 517 58 297 83 | 928 937 923 951 9 935
------+------------------------------------+--------------------------------
RMS | 7951 39 42 224 34 213 |T 125 181 183 124 17 172
WRMS | 7951 30 39 61 34 213 |NE 125 181 183 124 17 172
MEDI | 7676 32 34 77 31 51 |MD 50 61 76 36 9 43
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