[IGSREPORT-15261] Wk 1432 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Jul 5 01:10:03 PDT 2007
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IGS Electronic Report 05 Jul 01:10:08 PDT 2007 Message Number 15261
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1432 (Jun 17, 2007 - Jun 23, 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 2.1432.
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:
igl1432[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1432 in the SP3 format.
igl14327.sum Combination Report for GPS Week 1432.
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 | 1103.8 ns
1 | 1075.0 ns
2 | 1069.3 ns
3 | 1095.2 ns
4 | 1062.4 ns
5 | 1086.5 ns
6 | 1060.5 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 | COD | R15
0 | ESX | R23 R24
1 | COD | R15 R23
1 | ESX | R24
2 | COD | R15
2 | ESX | R24
2 | IAC | R23
3 | COD | R15
3 | ESX | R23 R24
4 | COD | R15
4 | ESX | R23 R24
5 | COD | R15
5 | ESX | R23
6 | COD | R15
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 1.1432, 1a.1432).
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 2.1432.0-6)
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 3.1432.0-6).
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 1432 summary. (Jun 17, 2007 - Jun 23, 2007)
Table 1.1432.a GPS week : 1432 MJD: 54268.0-54274.0
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| 0 0 -7 -8 29 7 -.07 39 34 | 0 -86 4715 4798
| 3 2 6 32 47 178 .09 | 0 345
cod 168| -1 -3 -3 19 -26 68 -.03 44 42 | --- --- --- ---
| 4 1 9 69 82 103 .07 | --- ---
esx 43| -2 0 9 91 -10 -94 -.13 209 78 | 2286396 2329 17151 28832
| 5 4 9 165 51 285 .09 | 4310561 40380
iac n/a| 2 -1 4 -12 -23 3 .13 42 42 | 1076106 2911 17349 28164
| 2 5 8 53 41 119 .09 | 15330 13414
mcc n/a| 11 -5 2 -55 -86 24 .53 192 192 | --- --- --- ---
| 16 14 17 150 194 638 .68 | --- ---
Table 1.1432.b GPS week : 1432 MJD: 54268.0-54274.0
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 15 23 23 20 28 31 |
R03 | 35 26 20 25 18 23 33 |
R04 | 34 16 25 17 20 20 21 |
R06 | 26 24 21 23 29 18 23 |
R07 | 23 17 20 15 21 17 21 |
R08 | 34 28 26 26 40 27 32 |
R10E | 27 21 23 32 26 34 24 |
R14E | 50 19 21 20 24 15 19 |
R19 | 38 30 27 30 28 74 178 |
R21 | 49 53 31 24 36 31 39 |
R22 | 0 0 0 0 0 0 0 |
R23 | 31 215 354 44 47 47 25 |
R24 | 23 19 28 15 21 15 19 |
Table 1.1432.c GPS week : 1432 MJD: 54268.0-54274.0
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 1432 0 | 288 -155 -709 2865 6982 -362000 97.9 10060 10060 | 1103833 0
brd 1432 1 | -114 88 -302 -1097 -516 -351300 100.1 5499 5499 | 1075004 0
brd 1432 2 | -128 -720 438 1071 -5580 -365100 85.3 5756 5756 | 1069264 0
brd 1432 3 | 0 -158 794 -2954 3837 -364900 101.0 7479 7479 | 1095220 0
brd 1432 4 | -500 -5 204 6929 -2188 -363600 99.0 10580 10580 | 1062425 0
brd 1432 5 | -294 -150 -165 -5398 -6734 -360400 77.7 7660 7660 | 1086514 0
brd 1432 6 | 421 -412 151 5971 1846 -357400 83.9 5415 5415 | 1060480 0
-------------+------------------------------------------------------------+----------------
brd 1432 mean| -46 -216 58 1055 -336 -360671 92.1 7492 7492 | 1078962 0
brd 1432 sdev| 319 271 497 4551 4960 4940 9.5 2139 2139 | 16656 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 2.1432.0 GPS week: 1432 Day: 0 MJD: 54268
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| -2 -1 1 -16 9 222 -.21 45 43 | 0 -327 5190 4386
cod 168| -2 -5 3 71 -134 82 .08 44 45 | --- --- --- ---
esx 43| 5 5 4 86 53 -537 -.13 241 89 | 25614 16505 15390 19501
iac n/a| 3 -12 -6 -37 49 -104 .22 58 58 | 1091983 12539 14251 18971
mcc n/a| 41 -34 -6 -237 -469 -34 1.96 299 299 | --- --- --- ---
Table 2.1432.1 GPS week: 1432 Day: 1 MJD: 54269
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 -3 -9 -55 36 -83 -.00 34 27 | 0 -247 4533 4966
cod 168| 1 -2 -4 -62 -10 115 -.12 49 52 | --- --- --- ---
esx 43| -5 -5 11 259 7 104 -.01 166 55 | -17960 9523 14989 39135
iac n/a| 2 3 10 -36 -39 -33 .12 50 50 | 1079964 4357 14577 36228
mcc n/a| 7 -8 -20 54 41 596 .46 224 224 | --- --- --- ---
Table 2.1432.2 GPS week: 1432 Day: 2 MJD: 54270
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 -11 21 65 68 .02 39 38 | 0 -463 7265 7473
cod 168| 6 0 -6 68 -85 -100 .00 45 50 | --- --- --- ---
esx 43| -6 -1 3 0 -86 144 -.29 170 58 | 4286 -29018 22819 29386
iac n/a| 4 5 6 -59 -55 75 .24 30 30 | 1071564 -16022 21579 28071
mcc n/a| 14 -5 -12 -241 -154 455 .23 170 170 | --- --- --- ---
Table 2.1432.3 GPS week: 1432 Day: 3 MJD: 54271
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 0 -20 -4 -101 .03 31 23 | 0 -60 4619 4841
cod 168| -6 -3 -11 46 94 215 -.03 49 42 | --- --- --- ---
esx 43| -7 1 24 -76 -28 117 -.07 214 79 | -999999 -44557 13505 23588
iac n/a| -2 0 1 27 -15 -70 -.02 36 36 | 1091117 -852 12765 23060
mcc n/a| 18 0 18 -160 -104 622 .27 225 225 | --- --- --- ---
Table 2.1432.4 GPS week: 1432 Day: 4 MJD: 54272
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| -5 2 -3 44 -9 238 -.13 50 42 | 0 436 3807 3920
cod 168| 0 -3 -16 -61 40 -13 -.10 44 33 | --- --- --- ---
esx 43| -3 9 15 -90 -44 -118 -.10 228 70 | 6860051 78488 21766 30714
iac n/a| 4 -2 9 87 -2 -124 .15 35 35 | 1061571 16631 20102 30130
mcc n/a| 10 9 25 38 -57 36 .06 281 281 | --- --- --- ---
Table 2.1432.5 GPS week: 1432 Day: 5 MJD: 54273
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 -18 -15 -8 -246 -.09 49 43 | 0 -283 3771 3996
cod 168| -2 -3 -4 105 9 47 -.07 36 34 | --- --- --- ---
esx 43| 4 -1 -5 115 51 69 -.18 183 64 | 132787 -20800 24167 37605
iac n/a| 0 0 15 -7 -22 83 .13 40 40 | 1085052 -12661 20860 33902
mcc n/a| -12 -3 14 84 138 -1179 .74 50 50 | --- --- --- ---
Table 2.1432.6 GPS week: 1432 Day: 6 MJD: 54274
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 2 -8 -18 116 -48 -.08 27 24 | 0 338 3824 4005
cod 168| -7 -4 11 -27 -98 135 -.01 37 36 | --- --- --- ---
esx 43| -5 -1 9 346 -25 -444 -.10 259 129 | 9999999 6162 7425 21899
iac n/a| 3 -3 -3 -62 -80 200 .09 42 42 | 1051491 16385 17312 26790
mcc n/a| 0 5 0 71 -1 -323 -.02 94 94 | --- --- --- ---
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 3.1432.0 GPS week: 1432 Day: 0 MJD: 54268
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7638 50 41 103 31 --- 31 | 47 50 78 58 --- 46
R03 |27250 66 35 57 75 --- 35 | 67 80 83 81 --- 65
R04 | 2204 62 23 98 53 --- 33 | 41 44 59 43 --- 35
R06 | 1815 11 41 103 20 --- 25 | 30 43 60 34 --- 26
R07 | 7757 17 37 84 23 182 22 | 34 36 73 34 112 34
R08 | 7974 57 52 53 69 --- 34 | 60 58 60 75 --- 53
XR10E | 7585 36 29 --- 47 --- 27 | 32 33 --- 34 --- 20
XR14E | 8545 75 46 --- 83 --- 49 | 31 34 --- 56 --- 29
R19 | 2801 38 47 137 54 --- 37 | 53 134 69 134 --- 126
R21 | 7367 52 71 110 108 --- 48 | 93 106 101 154 --- 101
XR22 | ---- --- 10 --- --- --- 0 | --- 301 --- --- --- 305
R23 | 3652 32 48 530 50 --- 31 | 764 737 723 819 --- 788
R24 | 2140 29 23 475 41 382 22 | 43 73 441 69 329 57
------+------------------------------------+--------------------------------
RMS |10064 45 44 241 58 299 |T 107 133 174 132 220 129
WRMS |10064 43 45 89 58 299 |NE 123 151 174 150 220 148
MEDI | 7367 38 41 103 50 182 |MD 43 58 73 58 112 53
Table 3.1432.1 GPS week: 1432 Day: 1 MJD: 54269
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3519 22 25 21 31 --- 14 | 38 47 52 41 --- 35
R03 |12321 46 37 45 46 --- 25 | 62 115 130 133 --- 100
R04 | 5719 24 22 41 21 --- 15 | 40 39 70 34 --- 30
R06 | 1776 35 38 55 38 --- 23 | 30 36 63 41 --- 24
R07 | 6426 17 31 49 21 95 17 | 24 35 55 30 83 26
R08 | 1927 49 42 66 35 --- 28 | 102 69 59 81 --- 78
XR10E | 6220 22 28 --- 36 --- 20 | 21 26 --- 35 --- 16
XR14E | 7010 22 27 --- 32 --- 19 | 30 35 --- 55 --- 31
R19 | 3858 26 59 87 34 --- 29 | 43 59 37 53 --- 51
R21 | 3086 48 101 94 118 --- 52 | 52 57 100 173 --- 82
XR22 | ---- --- 8 --- --- --- 0 | --- 297 --- --- --- 300
XR23 |12731 191 634 --- 241 --- 215 | 804 706 --- 884 --- 889
R24 | 1630 19 38 465 20 302 18 | 14 35 256 22 301 17
------+------------------------------------+--------------------------------
RMS | 5499 34 49 165 50 224 |T 105 119 91 131 192 129
WRMS | 5499 27 52 55 50 224 |NE 120 135 91 149 192 148
MEDI | 3858 24 37 55 34 95 |MD 38 47 63 41 83 35
Table 3.1432.2 GPS week: 1432 Day: 2 MJD: 54270
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3288 47 40 20 38 --- 22 | 43 42 45 48 --- 38
R03 | 6898 43 38 38 22 --- 20 | 67 133 122 94 --- 94
R04 | 3265 22 38 78 32 --- 24 | 32 44 60 44 --- 27
R06 |12112 34 47 47 22 --- 21 | 38 48 59 30 --- 26
R07 | 5268 44 26 54 17 99 20 | 35 39 72 40 72 36
R08 | 2018 35 55 62 28 --- 25 | 63 67 56 67 --- 58
XR10E | 3456 32 36 --- 29 --- 23 | 19 47 --- 46 --- 27
XR14E | 8499 31 32 --- 24 --- 20 | 24 42 --- 39 --- 27
R19 | 4894 30 62 54 39 --- 26 | 54 107 60 100 --- 100
R21 | 3039 49 34 98 35 --- 31 | 55 63 92 81 --- 66
XR22 | ---- --- 9 --- --- --- 0 | --- 105 --- --- --- 103
XR23 | ---- 337 370 --- 1119 --- 353 | 232 418 --- 650 --- 209
R24 | 4164 39 54 480 28 220 28 | 30 61 333 29 150 31
------+------------------------------------+--------------------------------
RMS | 5755 39 45 170 30 170 |T 57 93 99 105 111 64
WRMS | 5755 38 50 58 30 170 |NE 64 102 99 118 111 71
MEDI | 4164 35 38 54 28 99 |MD 38 61 60 46 72 38
Table 3.1432.3 GPS week: 1432 Day: 3 MJD: 54271
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3032 27 36 47 49 --- 22 | 38 57 49 41 --- 36
R03 |13122 33 49 70 26 --- 24 | 70 97 134 112 --- 92
R04 | 3102 12 43 40 25 --- 16 | 24 45 52 45 --- 29
R06 |14749 26 51 54 33 --- 22 | 44 46 72 33 --- 31
R07 | 2925 17 32 31 26 83 14 | 30 28 43 42 66 27
R08 | 3436 40 54 65 26 --- 25 | 128 132 123 146 --- 136
XR10E | 1460 31 57 --- 48 --- 31 | 19 65 --- 40 --- 25
XR14E | 7041 20 27 --- 34 --- 19 | 25 35 --- 45 --- 27
R19 | 4075 35 58 98 31 --- 30 | 57 124 76 106 --- 117
R21 | 3949 24 38 72 40 --- 23 | 77 86 81 100 --- 82
XR22 | ---- --- 16 --- --- --- 0 | --- 111 --- --- --- 110
R23 | 8555 55 74 469 62 --- 44 | 389 196 315 378 --- 317
R24 | 4994 9 34 455 18 307 14 | 43 51 367 35 53 40
------+------------------------------------+--------------------------------
RMS | 7478 31 49 214 36 225 |T 78 82 131 93 59 82
WRMS | 7478 23 42 79 36 225 |NE 90 88 131 103 59 92
MEDI | 3949 26 43 65 31 83 |MD 43 65 76 45 53 40
Table 3.1432.4 GPS week: 1432 Day: 4 MJD: 54272
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2617 41 26 54 30 --- 20 | 46 67 85 54 --- 56
R03 |21593 39 20 51 22 --- 17 | 118 80 98 84 --- 87
R04 | 4638 42 19 67 22 --- 19 | 34 38 70 49 --- 34
R06 |22644 35 62 71 34 --- 28 | 35 57 60 40 --- 34
R07 | 2035 22 47 41 30 130 20 | 25 47 53 33 86 23
R08 | 6774 109 34 90 50 --- 39 | 69 91 108 82 --- 74
XR10E | 4718 44 34 --- 31 --- 25 | 21 28 --- 38 --- 19
XR14E | 6458 21 35 --- 37 --- 23 | 37 22 --- 55 --- 31
R19 | 4730 38 35 106 31 --- 27 | 67 79 70 82 --- 98
R21 | 5206 44 48 143 31 --- 35 | 74 72 63 83 --- 79
XR22 | ---- --- 11 --- --- --- 0 | --- 89 --- --- --- 86
R23 | 3206 50 79 438 62 --- 46 | 329 271 297 341 --- 311
R24 | 1387 35 35 519 19 375 21 | 32 49 393 38 142 33
------+------------------------------------+--------------------------------
RMS |10579 50 44 227 35 281 |T 73 76 129 81 114 74
WRMS |10579 42 33 70 35 281 |NE 82 85 129 88 114 83
MEDI | 4718 39 35 71 31 130 |MD 37 67 70 54 86 56
Table 3.1432.5 GPS week: 1432 Day: 5 MJD: 54273
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4566 61 38 70 34 --- 27 | 37 86 134 62 --- 68
R03 |17111 50 32 57 31 --- 23 | 39 46 86 39 --- 36
R04 | 4683 38 25 61 24 --- 20 | 32 34 71 46 --- 34
R06 | 8838 33 32 29 29 --- 17 | 27 43 46 34 --- 26
R07 | 2154 15 27 52 24 50 17 | 20 30 54 28 58 20
R08 | 4740 75 29 62 24 --- 26 | 98 103 94 68 --- 80
XR10E | 8366 57 56 --- 29 --- 34 | 22 38 --- 34 --- 23
XR14E | 6407 21 23 --- 20 --- 15 | 22 23 --- 40 --- 24
XR19 |12698 --- 74 --- 73 --- 73 | --- 111 --- 140 --- 94
R21 | 4713 45 39 96 45 --- 30 | 44 61 107 71 --- 46
XR22 | ---- --- 7 --- --- --- 0 | --- 89 --- --- --- 87
R23 | 2516 54 59 491 79 --- 47 | 163 137 274 222 --- 184
XR24 | 2368 27 18 --- 20 --- 15 | 64 59 --- 55 --- 57
------+------------------------------------+--------------------------------
RMS | 7659 49 36 183 40 50 |T 51 66 108 69 58 59
WRMS | 7659 43 34 64 40 50 |NE 58 72 108 76 58 66
MEDI | 4713 45 32 61 29 50 |MD 37 59 86 46 58 46
Table 3.1432.6 GPS week: 1432 Day: 6 MJD: 54274
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6305 25 50 99 62 --- 30 | 69 111 100 93 --- 88
R03 | 6079 37 23 135 58 --- 32 | 66 64 157 76 --- 65
R04 | 2619 32 28 69 29 --- 20 | 38 36 48 40 --- 31
R06 | 9101 20 48 62 39 --- 22 | 37 43 35 38 --- 30
R07 | 4525 12 34 87 27 94 20 | 30 37 75 25 57 29
XR08 | 2520 39 60 --- 32 --- 32 | 79 61 --- 45 --- 47
XR10E | 3127 26 42 --- 32 --- 23 | 24 50 --- 28 --- 22
XR14E | 6814 20 29 --- 30 --- 18 | 34 33 --- 63 --- 37
XR19 |21225 --- 100 --- 241 --- 178 | --- 192 --- 281 --- 200
XR21 | 3703 46 42 --- 79 --- 39 | 130 129 --- 130 --- 128
XR22 | ---- --- 12 --- --- --- 0 | --- 139 --- --- --- 140
R23 | 2694 32 36 440 40 --- 25 | 282 220 365 321 --- 279
R24 | 3330 23 35 482 21 --- 19 | 50 75 470 48 --- 55
------+------------------------------------+--------------------------------
RMS | 5414 27 37 259 42 94 |T 76 91 178 99 57 88
WRMS | 5414 24 36 129 42 94 |NE 86 100 178 109 57 99
MEDI | 3703 26 36 99 32 94 |MD 50 64 100 48 57 55
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