[IGSREPORT-15753] Wk 1455 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Dec 13 01:48:14 PST 2007
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IGS Electronic Report 13 Dec 01:48:17 PST 2007 Message Number 15753
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1455 (Nov 25, 2007 - Dec 01, 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 2.1455.
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:
igl1455[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1455 in the SP3 format.
igl14557.sum Combination Report for GPS Week 1455.
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 | 1526.2 ns
1 | 1548.7 ns
2 | 1498.5 ns
3 | 1533.3 ns
4 | 1531.9 ns
5 | 1500.0 ns
6 | 1519.0 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 | BKG | R14
0 | COD | R07
0 | ESX | R23 R24
1 | COD | R07
1 | ESX | R23 R24
2 | ESX | R23 R24
2 | IAC | R08
3 | ESX | R23 R24
3 | IAC | R08
4 | BKG | R14
4 | ESX | R23 R24
5 | ESX | R23 R24
6 | BKG | R21
6 | ESX | 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 1.1455, 1a.1455).
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 2.1455.0-6)
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 3.1455.0-6).
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 1455 summary. (Nov 25, 2007 - Dec 01, 2007)
Table 1.1455.a GPS week : 1455 MJD: 54429.0-54435.0
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 58| -1 0 3 -9 -7 -283 -.03 75 40 | 0 71 4800 5163
| 2 4 6 49 79 253 .09 | 0 753
cod 179| 0 -5 10 7 -23 -51 -.11 76 83 | --- --- --- ---
| 6 6 7 66 78 148 .18 | --- ---
esx 51| 0 3 -20 18 45 408 -.37 226 69 | 117526 1830 8476 14994
| 5 7 10 54 151 117 .15 | 345712 7417
iac n/a| 3 1 0 -10 5 99 .27 61 61 | 78954 198187 576306 579132
| 3 3 7 54 37 160 .15 | 1345708 446195
mcc n/a| 0 0 0 0 0 0 .0 424 424 | --- --- --- ---
| 0 0 0 0 0 0 .0 | --- ---
Table 1.1455.b GPS week : 1455 MJD: 54429.0-54435.0
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 | 15 24 15 20 18 14 12 |
R04 | 18 21 19 16 17 17 12 |
R06 | 47 23 18 22 24 23 30 |
R07 | --- --- 0 0 0 0 0 |
R08 | 30 306 0 0 128 48 66 |
R10E | 176 126 123 61 90 130 80 |
R14E | 0 0 0 0 277 244 266 |
R15E | 0 0 166 776 130 300 140 |
R17 | --- --- --- 0 0 0 0 |
R19 | 83 67 71 101 104 99 63 |
R20 | 143 86 104 105 92 124 46 |
R21 | 0 0 0 0 88 58 289 |
R23 | 47 48 17 32 31 23 25 |
R24 | 26 48 38 29 41 35 28 |
Table 1.1455.c GPS week : 1455 MJD: 54429.0-54435.0
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 1455 0 | 313 -316 -188 839 9259 -29790 99.2 4683 4683 | 1526231 0
brd 1455 1 | 140 320 208 -2001 5601 -24970 81.3 4435 4435 | 1548684 0
brd 1455 2 | -95 258 -229 1677 -1111 -23910 88.5 4785 4785 | 1498523 0
brd 1455 3 | -565 130 -212 -495 -669 -20530 87.8 5326 5326 | 1533302 0
brd 1455 4 | 432 -359 319 2314 13830 -30710 92.1 6497 6497 | 1531933 0
brd 1455 5 | -16 109 2153 -9115 995 -48540 70.8 6493 6493 | 1500040 0
brd 1455 6 | 29 -242 2041 6544 -4317 -61380 74.6 6166 6166 | 1519038 0
-------------+------------------------------------------------------------+----------------
brd 1455 mean| 33 -14 584 -34 3369 -34261 84.9 5483 5483 | 1522535 0
brd 1455 sdev| 323 284 1055 4813 6457 15021 10.0 891 891 | 18241 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 2.1455.0 GPS week: 1455 Day: 0 MJD: 54429
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 58| -3 -6 0 25 -22 -298 -.03 70 39 | 0 -264 2706 2881
cod 179| 8 4 12 58 -149 -118 -.17 75 91 | --- --- --- ---
esx 51| 0 -7 -12 -39 173 274 -.46 189 71 | 875029 -6711 9902 13817
iac n/a| 4 3 7 71 -32 250 .26 58 58 | 1524371 -2929 9389 15174
mcc n/a| 0 0 0 0 0 0 .0 573 573 | --- --- --- ---
Table 2.1455.1 GPS week: 1455 Day: 1 MJD: 54430
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 58| 0 0 -6 -113 -47 -440 .08 74 37 | 0 -479 2142 2381
cod 179| -5 -8 0 71 -10 -23 .26 50 63 | --- --- --- ---
esx 51| -6 6 -1 120 15 560 -.59 216 68 | 10881 -2265 4955 10493
iac n/a| 0 -4 -5 -13 59 45 .24 72 72 | -999999 -42719 999999 999999
mcc n/a| 0 0 0 0 0 0 .0 358 358 | --- --- --- ---
Table 2.1455.2 GPS week: 1455 Day: 2 MJD: 54431
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 58| 1 -4 6 24 70 50 -.12 86 33 | 0 1252 8019 8713
cod 179| -3 -1 7 -14 -59 135 -.15 70 79 | --- --- --- ---
esx 51| 2 15 -33 -41 -133 301 -.45 272 71 | -36134 -7362 14543 17211
iac n/a| 7 0 1 -86 36 -191 .44 70 70 | 1503884 -8122 14208 17946
mcc n/a| 0 0 0 0 0 0 .0 366 366 | --- --- --- ---
Table 2.1455.3 GPS week: 1455 Day: 3 MJD: 54432
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 58| 0 5 -2 25 132 -275 -.04 110 56 | 0 -230 4174 4521
cod 179| -2 -10 20 86 -78 94 -.19 98 93 | --- --- --- ---
esx 51| 0 -2 -19 14 151 300 -.41 233 67 | -8348 11946 10525 20270
iac n/a| 10 0 -6 -28 -2 -8 .38 88 88 | 1524423 7693 10555 20810
mcc n/a| 0 0 0 0 0 0 .0 738 738 | --- --- --- ---
Table 2.1455.4 GPS week: 1455 Day: 4 MJD: 54433
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 58| -1 -1 13 -10 -43 -608 .10 76 42 | 0 -194 5519 5795
cod 179| 1 -15 2 -62 29 14 -.27 95 100 | --- --- --- ---
esx 51| 4 9 -21 20 256 505 -.29 247 79 | 74998 6678 6719 14991
iac n/a| -1 5 5 -41 -41 211 .08 52 52 | -999999 -64568 999999 999999
mcc n/a| 0 0 0 0 0 0 .0 526 526 | --- --- --- ---
Table 2.1455.5 GPS week: 1455 Day: 5 MJD: 54434
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 58| -6 0 7 4 -53 -463 -.13 77 32 | 0 1043 5927 6290
cod 179| 10 0 18 -80 20 -203 -.21 103 110 | --- --- --- ---
esx 51| -6 1 -24 13 -123 410 -.14 182 54 | -182148 3471 6899 14107
iac n/a| 3 2 -11 -25 27 233 .43 58 58 | -999999 335803 999999 999999
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1455.6 GPS week: 1455 Day: 6 MJD: 54435
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 58| -2 5 3 -19 -89 48 -.07 34 37 | 0 -629 5113 5564
cod 179| -7 -4 11 -9 84 -261 -.05 43 44 | --- --- --- ---
esx 51| 6 4 -31 43 -21 506 -.25 248 74 | 88404 7058 5791 14069
iac n/a| 2 5 5 49 -10 153 .10 31 31 | -999999 1162153 999999 999999
mcc n/a| 0 0 0 0 0 0 .0 407 407 | --- --- --- ---
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 3.1455.0 GPS week: 1455 Day: 0 MJD: 54429
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2913 29 23 21 26 --- 14 | 33 45 41 48 --- 36
R04 | 2361 16 44 37 24 --- 17 | 45 61 43 46 --- 44
R06 | 6986 58 100 74 86 --- 46 | 54 89 58 59 --- 39
R08 | 3499 58 50 59 38 --- 29 | 127 182 7 406 --- 171
XR10E | 3051 151 205 --- --- --- 176 | 97 190 --- --- --- 108
XR14E | 2941 5079 15 --- --- --- 0 | 9999 307 --- --- --- 321
XR15E | 7160 --- 15 --- --- 488 0 | --- 381 --- --- 190 385
R19 | 2607 133 140 216 100 --- 82 | 684 683 632 707 --- 698
XR20 | 6746 183 159 --- 237 --- 142 | 231 215 --- 332 --- 251
XR21 |18380 --- 14 --- --- --- 0 | --- 845 --- --- --- 843
R23 | 1910 85 55 259 50 --- 46 | 92 67 223 67 --- 67
R24 | 8242 34 47 356 31 573 26 | 126 133 366 123 354 122
------+------------------------------------+--------------------------------
RMS | 4682 70 75 189 58 573 |T 165 266 195 223 272 257
WRMS | 4682 39 91 71 58 573 |NE 174 257 195 223 354 252
MEDI | 3051 58 47 74 38 488 |MD 97 182 58 67 190 122
Table 3.1455.1 GPS week: 1455 Day: 1 MJD: 54430
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4497 23 44 40 49 --- 23 | 41 43 39 58 --- 37
R04 | 2362 21 37 51 27 --- 20 | 28 34 48 46 --- 31
R06 | 3976 52 15 58 27 --- 23 | 39 46 57 39 --- 34
XR08 | 4573 --- 267 --- 350 --- 305 | --- 244 --- 697 --- 369
XR10E | 2097 143 109 --- --- --- 125 | 53 151 --- --- --- 78
XR14E | 2039 --- 8 --- --- --- 0 | --- 98 --- --- --- 103
XR15E |18948 --- 8 --- --- 365 0 | --- 180 --- --- 179 270
R19 | 1570 119 80 120 145 --- 67 | 513 511 440 538 --- 518
XR20 | 5617 87 80 --- 183 --- 86 | 182 169 --- 260 --- 208
XR21 |24582 --- 8 --- --- --- 0 | --- 275 --- --- --- 280
XR23 | 1992 --- 40 280 55 --- 47 | --- 50 146 83 --- 52
R24 | 7364 98 52 459 37 358 47 | 173 160 353 150 137 145
------+------------------------------------+--------------------------------
RMS | 4434 74 50 215 72 358 |T 147 163 180 233 158 177
WRMS | 4434 37 63 68 72 358 |NE 162 170 180 233 137 186
MEDI | 3976 87 40 58 49 358 |MD 53 151 57 83 137 103
Table 3.1455.2 GPS week: 1455 Day: 2 MJD: 54431
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6786 22 20 50 22 --- 15 | 39 45 64 31 --- 30
R04 | 1942 31 32 23 36 --- 18 | 43 47 34 49 --- 36
R06 | 4750 21 27 54 28 --- 17 | 45 39 53 40 --- 31
XR07 | ---- --- 9 --- --- 521 0 | --- 536 --- --- 29 234
XR08 | 5515 --- 9 --- 2216 --- 0 | --- 402 --- 9999 --- 430
XR10E | 2239 136 110 --- --- --- 123 | 63 174 --- --- --- 92
XR14E | 2965 --- 9 --- --- --- 0 | --- 81 --- --- --- 112
XR15E |12604 282 171 --- 242 290 165 | 125 80 --- 453 152 264
R19 | 2023 125 96 193 113 --- 71 | 622 638 552 616 --- 633
R20 | 4018 167 144 352 129 --- 103 | 109 103 136 159 --- 134
XR21 |33139 --- 9 --- --- --- 0 | --- 113 --- --- --- 104
R23 | 1893 22 21 310 24 --- 16 | 32 45 174 39 --- 34
R24 | 8004 75 45 503 40 366 37 | 178 238 447 218 324 212
------+------------------------------------+--------------------------------
RMS | 4785 86 70 272 70 366 |T 139 195 208 200 168 180
WRMS | 4785 33 79 71 70 366 |NE 152 220 208 164 176 187
MEDI | 4018 75 27 193 40 366 |MD 63 103 136 49 152 112
Table 3.1455.3 GPS week: 1455 Day: 3 MJD: 54432
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8083 16 32 60 18 --- 19 | 44 47 58 53 --- 44
R04 | 1860 24 29 27 25 --- 15 | 34 46 55 35 --- 39
R06 | 5966 54 23 33 38 --- 22 | 65 43 46 45 --- 36
XR07 | ---- --- 16 --- --- 120 0 | --- 219 --- --- 25 125
XR08 |11767 --- 16 --- 2450 --- 0 | --- 132 --- 9999 --- 127
XR10E | 2668 68 55 --- --- --- 61 | 107 112 --- --- --- 74
XR14E | 3383 --- 16 --- --- --- 0 | --- 88 --- --- --- 139
XR15E | 3528 --- 837 --- 718 1280 775 | --- 76 --- 696 443 662
XR17 | ---- --- 16 --- --- --- 0 | --- 300 --- --- --- 298
R19 | 2521 210 161 227 113 --- 100 | 288 363 506 294 --- 303
R20 | 2239 182 187 153 192 --- 105 | 86 80 96 239 --- 138
XR21 | ---- --- 16 --- --- --- 0 | --- 221 --- --- --- 208
R23 | 2731 26 58 326 40 --- 31 | 38 90 268 40 --- 49
R24 | 8681 55 33 439 34 738 28 | 227 229 392 222 601 225
------+------------------------------------+--------------------------------
RMS | 5326 110 98 233 88 738 |T 111 146 203 203 356 176
WRMS | 5326 56 93 67 88 738 |NE 111 160 203 132 313 144
MEDI | 3383 54 29 153 40 738 |MD 65 90 96 53 443 127
Table 3.1455.4 GPS week: 1455 Day: 4 MJD: 54433
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9624 27 28 59 23 --- 18 | 24 25 64 35 --- 28
R04 | 3931 34 34 43 14 --- 16 | 33 34 42 41 --- 31
R06 | 5905 36 51 79 19 --- 23 | 53 41 60 43 --- 36
XR07 | ---- --- 10 --- --- 145 0 | --- 298 --- --- 46 138
XR08 |15912 177 207 --- 170 --- 127 | 173 75 --- 692 --- 211
XR10E | 4038 188 90 --- 86 --- 89 | 74 41 --- 62 --- 60
XR14E | 3994 868 441 --- 173 --- 277 | 9999 74 --- 410 --- 354
XR15E | 3940 182 265 --- 137 502 129 | 129 86 --- 900 334 184
XR17 | ---- --- 11 --- --- --- 0 | --- 250 --- --- --- 250
XR19 | 2102 144 158 --- 142 --- 103 | 735 780 --- 792 --- 765
R20 | 1861 155 197 226 118 --- 91 | 109 91 93 215 --- 164
XR21 | ---- --- 132 --- 61 --- 87 | --- 157 --- 80 --- 212
R23 | 6624 48 67 338 26 --- 31 | 61 66 257 50 --- 49
R24 | 7936 72 83 435 28 526 41 | 135 203 378 161 621 157
------+------------------------------------+--------------------------------
RMS | 6497 76 95 247 52 526 |T 152 158 149 290 333 188
WRMS | 6497 42 100 79 52 526 |NE 165 183 149 234 333 185
MEDI | 4038 144 83 79 61 502 |MD 74 75 64 80 334 157
Table 3.1455.5 GPS week: 1455 Day: 5 MJD: 54434
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |10987 24 15 41 15 --- 13 | 29 25 27 44 --- 25
R04 | 5247 35 29 47 10 --- 17 | 31 29 45 32 --- 29
R06 | 4957 33 59 29 38 --- 23 | 38 41 48 41 --- 34
XR07 | ---- --- 17 --- --- 64 0 | --- 222 --- --- 22 64
XR08 |18514 62 80 --- 66 --- 48 | 55 62 --- 418 --- 64
XR10E | 3541 256 72 --- 155 --- 129 | 90 74 --- 58 --- 55
XR14E | 5646 437 300 --- 285 --- 243 | 841 140 --- 344 --- 339
XR15E |10891 --- 441 --- 203 961 300 | --- 90 --- 388 129 412
XR17 | ---- --- 17 --- --- --- 0 | --- 140 --- --- --- 144
R19 | 3189 161 215 230 122 --- 99 | 467 475 732 521 --- 497
XR20 | 2966 151 185 --- 186 --- 124 | 123 92 --- 253 --- 149
XR21 | ---- --- 85 --- 40 --- 58 | --- 270 --- 115 --- 153
R23 | 5269 35 47 328 19 --- 23 | 54 48 182 61 --- 49
XR24 | 5690 31 77 --- 41 334 34 | 187 195 --- 155 231 168
------+------------------------------------+--------------------------------
RMS | 6492 77 103 182 58 0 |T 191 135 206 202 127 155
WRMS | 6492 32 110 54 58 0 |NE 123 145 206 182 126 125
MEDI | 5269 35 72 47 41 334 |MD 55 90 48 115 129 64
Table 3.1455.6 GPS week: 1455 Day: 6 MJD: 54435
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9552 22 16 22 22 --- 12 | 50 43 51 57 --- 49
R04 | 6142 22 13 41 17 --- 11 | 42 32 46 42 --- 36
R06 | 5026 52 64 63 39 --- 30 | 43 68 45 53 --- 37
XR07 | ---- --- 17 --- --- 286 0 | --- 261 --- --- 34 114
XR08 | 9325 48 108 --- 107 --- 65 | 65 90 --- 342 --- 71
XR10E | 4832 122 84 --- 122 --- 79 | 73 89 --- 49 --- 78
XR14E | 8011 --- 307 --- 230 --- 266 | --- 80 --- 293 --- 160
XR15E | 8225 228 182 --- 179 578 139 | 147 78 --- 244 102 199
XR17 | ---- --- 18 --- --- --- 0 | --- 93 --- --- --- 91
R19 | 2316 38 44 398 39 --- 63 | 587 591 643 587 --- 589
XR20 | 2871 60 60 --- 72 --- 46 | 151 130 --- 216 --- 163
XR21 | ---- >>>> 333 --- 249 --- 288 | 6 272 --- 123 --- 225
R23 | 5335 27 40 354 37 --- 25 | 57 70 311 52 --- 55
R24 | 6326 36 55 280 25 407 28 | 139 140 351 132 267 130
------+------------------------------------+--------------------------------
RMS | 6165 34 43 248 31 407 |T 123 145 241 182 134 142
WRMS | 6165 37 44 74 31 407 |NE 126 162 241 178 150 141
MEDI | 6142 48 55 63 39 407 |MD 65 89 51 123 102 91
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