[IGSREPORT-16591] Wk 1493 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Sep 4 06:06:51 PDT 2008
******************************************************************************
IGS Electronic Report 04 Sep 06:06:54 PDT 2008 Message Number 16591
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1493 (Aug 17, 2008 - Aug 23, 2008)
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 2.1493.
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:
igl1493[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1493 in the SP3 format.
igl14937.sum Combination Report for GPS Week 1493.
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 | 705.1 ns
1 | 701.2 ns
2 | 633.2 ns
3 | 604.6 ns
4 | 691.7 ns
5 | 624.3 ns
6 | 609.3 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 | ESX | R07
2 | ESX | R04 R07 R13
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 1.1493, 1a.1493).
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 2.1493.0-6)
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 3.1493.0-6).
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 1493 summary. (Aug 17, 2008 - Aug 23, 2008)
Table 1.1493.a GPS week : 1493 MJD: 54695.0-54701.0
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 61| 0 0 -10 -25 13 24 -.12 52 34 | 0 81 2493 2583
| 2 2 7 53 30 136 .05 | 0 188
cod 214| -4 0 -10 37 13 56 -.08 35 27 | --- --- --- ---
| 2 2 2 48 36 72 .06 | --- ---
esx 116| 0 0 9 18 -79 -24 .44 91 59 | -16085 6378 13385 27142
| 4 6 6 94 54 69 .09 | 37063 7604
iac n/a| 4 0 15 -33 3 -73 -.07 33 33 | 655815 -954 7091 15628
| 2 2 6 44 29 76 .09 | 44051 4794
mcc n/a| -10 5 78 38 19 -484 -.05 236 236 | --- --- --- ---
| 18 9 10 99 137 865 .51 | --- ---
Table 1.1493.b GPS week : 1493 MJD: 54695.0-54701.0
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 | 0 0 0 0 0 0 0 |
R04 | 12 22 18 20 23 17 20 |
R06 | 22 31 30 35 21 20 17 |
R07 | 25 24 26 23 25 21 26 |
R09 | 0 0 0 0 0 0 0 |
R10 | 25 21 20 18 12 11 16 |
R11 | 26 19 36 21 24 17 14 |
R13 | 20 25 17 34 18 23 25 |
R14 | 15 11 15 15 14 15 15 |
R15 | 25 16 23 22 21 31 20 |
R17 | 23 23 20 26 25 27 23 |
R19 | 13 15 38 98 93 19 18 |
R20 | 17 19 27 17 21 24 26 |
R23 | 29 36 26 27 21 29 38 |
R24 | 11 10 16 17 15 21 46 |
Table 1.1493.c GPS week : 1493 MJD: 54695.0-54701.0
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 1493 0 | 2 -145 295 -1531 220 -31480 94.0 5222 5222 | 705078 0
brd 1493 1 | -88 51 466 3782 -2883 -27150 96.9 >>>>> >>>>> | 701149 0
brd 1493 2 | -127 157 653 -2183 -3825 -34260 104.4 3427 3427 | 633243 0
brd 1493 3 | -70 -254 436 -584 3153 -25520 98.2 4197 4197 | 604555 0
brd 1493 4 | -113 165 455 1449 -3423 -17800 96.9 4758 4758 | 691698 0
brd 1493 5 | -37 -439 122 1509 -3537 -13210 101.2 4145 4145 | 624278 0
brd 1493 6 | 141 294 -36 -1377 2332 -17260 98.7 4465 4465 | 609281 0
-------------+------------------------------------------------------------+----------------
brd 1493 mean| -41 -24 341 152 -1137 -23811 98.6 >>>>> >>>>> | 652754 0
brd 1493 sdev| 92 263 233 2155 2987 7889 3.4 >>>>> >>>>> | 44723 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 2.1493.0 GPS week: 1493 Day: 0 MJD: 54695
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 61| 1 4 -7 -88 -36 -46 -.07 40 42 | 0 -41 2382 2516
cod 214| -2 1 -11 68 50 110 -.11 29 23 | --- --- --- ---
esx 116| 0 -10 3 102 -68 -86 .32 55 46 | 17674 7344 8118 20628
iac n/a| 5 3 15 -55 -50 -56 -.06 29 29 | 705556 2756 6827 16189
mcc n/a| 3 9 96 155 68 241 .58 229 229 | --- --- --- ---
Table 2.1493.1 GPS week: 1493 Day: 1 MJD: 54696
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 61| -2 0 -9 -24 15 41 -.09 28 28 | 0 192 2678 2777
cod 214| -2 0 -5 81 10 -48 -.07 37 28 | --- --- --- ---
esx 116| 6 -4 0 -14 -65 -18 .31 108 58 | 25348 -2288 10299 27932
iac n/a| 2 2 13 -13 10 44 -.05 30 30 | 710723 -6887 7400 16409
mcc n/a| -9 16 81 -140 189 559 .14 306 306 | --- --- --- ---
Table 2.1493.2 GPS week: 1493 Day: 2 MJD: 54697
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 61| 4 -2 -22 65 46 -138 -.22 47 35 | 0 -19 2583 2662
cod 214| -7 4 -11 -39 35 120 -.15 29 26 | --- --- --- ---
esx 116| -1 11 14 -57 -181 -95 .52 144 71 | -40840 7607 13398 26649
iac n/a| 7 -2 27 13 -20 -111 .12 34 34 | 637322 -795 7254 16930
mcc n/a| 5 1 85 15 38 -1264 -.04 316 316 | --- --- --- ---
Table 2.1493.3 GPS week: 1493 Day: 3 MJD: 54698
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 61| 0 3 -5 21 55 268 -.15 82 35 | 0 27 2787 2835
cod 214| -4 -2 -9 -11 -28 81 .01 42 20 | --- --- --- ---
esx 116| -7 -1 16 -146 -29 -86 .47 105 66 | -62611 -3149 9884 25648
iac n/a| 6 0 17 17 32 -205 -.11 48 48 | 611128 -8019 6679 14685
mcc n/a| -7 12 77 135 -246 -1766 -.60 236 236 | --- --- --- ---
Table 2.1493.4 GPS week: 1493 Day: 4 MJD: 54699
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 61| 2 0 0 -60 4 30 -.10 84 33 | 0 -85 2567 2650
cod 214| -4 -2 -12 60 -42 52 -.02 40 26 | --- --- --- ---
esx 116| 2 -3 10 63 -102 66 .47 100 70 | 23072 8257 10369 19274
iac n/a| 1 0 7 -17 33 -59 -.13 29 29 | 687800 3445 9224 15742
mcc n/a| -37 10 67 70 104 -884 .55 229 229 | --- --- --- ---
Table 2.1493.5 GPS week: 1493 Day: 5 MJD: 54700
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 61| 1 0 -14 -68 -3 106 -.09 37 28 | 0 37 2048 2129
cod 214| -1 2 -14 83 29 -38 -.13 27 25 | --- --- --- ---
esx 116| 2 3 17 87 -97 61 .47 61 51 | -29033 19579 35147 49293
iac n/a| 4 -1 11 -81 13 -90 -.15 32 32 | 625972 -651 5821 12847
mcc n/a| -31 -11 75 48 -48 -477 -.69 276 276 | --- --- --- ---
Table 2.1493.6 GPS week: 1493 Day: 6 MJD: 54701
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 61| -2 2 -15 -25 14 -93 -.11 50 39 | 0 461 2410 2514
cod 214| -7 3 -8 16 41 117 -.12 40 38 | --- --- --- ---
esx 116| 0 2 6 96 -16 -13 .54 64 53 | -46208 7302 6484 20571
iac n/a| 1 0 13 -95 3 -33 -.10 27 27 | 612205 3469 6436 16595
mcc n/a| 7 -1 63 -16 29 199 -.31 60 60 | --- --- --- ---
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 3.1493.0 GPS week: 1493 Day: 0 MJD: 54695
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 10 --- --- --- 0 | --- 246 --- --- --- 249
R04 | 2758 15 14 41 16 --- 12 | 30 32 50 32 --- 31
R06 | 5464 52 41 30 21 --- 21 | 100 124 123 115 --- 113
R07 | 2688 40 30 88 26 --- 25 | 34 62 87 56 --- 47
XR09 |20127 --- --- 11 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2109 42 22 79 39 --- 25 | 29 28 77 23 --- 21
R11 |14605 32 44 75 31 159 25 | 34 50 79 51 48 35
R13 | 3202 55 14 47 24 --- 19 | 25 43 63 39 --- 34
R14 | 3721 37 12 37 24 --- 15 | 24 24 46 37 --- 24
R15 | 4863 63 33 57 26 84 24 | 30 28 63 40 41 26
R17 | 3230 38 32 67 30 --- 22 | 175 181 173 169 --- 172
R19 | 1618 23 12 45 16 --- 13 | 894 926 960 902 --- 916
R20 | 1717 34 23 44 23 --- 17 | 157 158 151 148 --- 153
R23 | 1798 40 48 46 55 --- 28 | 47 69 103 95 --- 69
R24 | 5003 22 19 22 17 353 11 | 75 73 76 70 159 71
------+------------------------------------+--------------------------------
RMS | 5221 40 29 55 29 229 |T 127 146 157 136 82 140
WRMS | 5221 42 23 46 29 229 |NE 127 146 157 136 82 140
MEDI | 3202 38 22 45 24 159 |MD 34 62 79 56 48 47
Table 3.1493.1 GPS week: 1493 Day: 1 MJD: 54696
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 271 --- --- --- 272
R04 |>>>>> 16 33 95 14 --- 22 | 31 47 113 46 --- 38
R06 |>>>>> 35 56 57 60 --- 30 | 79 144 159 80 --- 103
R07 | 1830 20 47 311 31 --- 24 | 25 54 224 29 --- 23
XR09 |>>>>> --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10 |>>>>> 26 23 71 34 --- 21 | 16 37 62 32 --- 25
R11 |>>>>> 31 25 60 23 157 18 | 47 45 78 56 80 44
R13 |>>>>> 36 54 72 22 --- 25 | 41 90 57 51 --- 51
R14 |>>>>> 12 17 34 16 --- 10 | 24 32 44 16 --- 21
R15 |>>>>> 21 24 62 12 114 16 | 29 35 83 35 75 32
R17 |>>>>> 31 38 60 36 --- 22 | 189 196 207 186 --- 188
R19 |>>>>> 23 21 56 13 --- 15 | 990 998 9999 989 --- 997
R20 |>>>>> 30 27 51 30 --- 19 | 134 148 201 132 --- 138
R23 |>>>>> 45 65 112 44 --- 35 | 33 83 106 87 --- 59
R24 |>>>>> 14 13 37 12 493 10 | 94 101 93 82 268 90
------+------------------------------------+--------------------------------
RMS |>>>>> 28 37 108 30 306 |T 133 162 118 140 141 148
WRMS |>>>>> 28 28 58 30 306 |NE 133 162 118 140 141 148
MEDI |>>>>> 26 25 60 23 157 |MD 41 83 93 56 80 51
Table 3.1493.2 GPS week: 1493 Day: 2 MJD: 54697
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 11 --- --- --- 0 | --- 159 --- --- --- 158
R04 | 2089 33 23 210 22 --- 18 | 64 55 154 40 --- 43
R06 | 2428 48 26 109 48 --- 30 | 220 218 186 186 --- 199
R07 | 2130 49 30 314 31 --- 25 | 24 53 240 62 --- 41
XR09 |29030 --- --- 18 --- --- 0 | --- --- 9999 --- --- 9999
XR10 | 3125 21 26 --- 33 --- 19 | 31 34 --- 26 --- 24
R11 | 5391 34 36 159 32 148 36 | 28 58 139 36 103 37
R13 | 4146 35 19 147 20 --- 17 | 18 35 156 23 --- 23
R14 | 2430 26 12 55 21 --- 15 | 14 27 55 31 --- 22
R15 | 5863 32 24 88 30 99 23 | 30 40 118 21 57 32
R17 | 1419 53 22 46 24 --- 20 | 158 173 200 176 --- 170
R19 | 2445 99 48 62 56 --- 37 | 653 751 765 729 --- 723
XR20 | 1024 37 35 --- 41 --- 26 | 130 150 --- 122 --- 135
R23 | 1228 24 34 87 45 --- 26 | 51 88 125 87 --- 74
R24 | 4284 29 22 42 25 519 16 | 96 92 120 84 362 88
------+------------------------------------+--------------------------------
RMS | 3427 47 29 144 34 316 |T 116 138 205 124 174 126
WRMS | 3427 35 26 71 34 316 |NE 116 138 205 124 174 126
MEDI | 2430 34 24 87 31 148 |MD 51 58 154 62 103 43
Table 3.1493.3 GPS week: 1493 Day: 3 MJD: 54698
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 235 --- --- --- 234
R04 | 2140 40 18 71 30 --- 20 | 37 41 96 43 --- 34
R06 | 4796 99 33 72 55 --- 35 | 146 137 176 106 --- 128
R07 | 1942 34 33 77 30 --- 22 | 47 58 93 53 --- 50
XR09 |34654 --- --- 15 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2747 25 12 71 30 --- 17 | 33 27 81 25 --- 24
R11 | 9471 36 25 65 35 206 20 | 40 58 78 72 64 56
R13 | 3459 23 12 168 43 --- 34 | 53 47 99 61 --- 40
R14 | 4108 23 17 42 31 --- 15 | 46 38 43 32 --- 32
R15 | 5477 41 20 90 23 100 22 | 35 43 99 20 54 31
R17 | 1638 65 30 81 24 --- 25 | 195 207 243 212 --- 206
R19 | 1387 250 130 237 121 --- 97 | 9999 9999 9999 9999 --- 9999
R20 | 1156 31 18 61 24 --- 16 | 66 73 93 74 --- 66
R23 | 3113 42 25 100 44 --- 27 | 32 62 91 66 --- 46
R24 | 5086 24 18 46 37 338 17 | 111 103 105 67 205 90
------+------------------------------------+--------------------------------
RMS | 4197 82 42 105 48 236 |T 70 86 108 69 107 79
WRMS | 4197 35 20 66 48 236 |NE 70 86 108 69 107 79
MEDI | 3113 36 18 71 31 206 |MD 46 58 93 61 64 50
Table 3.1493.4 GPS week: 1493 Day: 4 MJD: 54699
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 9 --- --- --- 0 | --- 420 --- --- --- 418
R04 | 3992 42 23 90 27 --- 23 | 38 38 69 31 --- 26
R06 | 8635 34 41 41 33 --- 21 | 191 223 184 188 --- 197
R07 | 1987 27 26 100 31 --- 24 | 30 44 111 23 --- 28
XR09 |12465 --- --- 12 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1177 26 17 36 15 --- 12 | 17 31 36 27 --- 22
R11 | 7297 51 15 99 21 164 24 | 23 28 104 37 34 31
R13 | 1934 22 27 73 14 --- 18 | 35 30 83 27 --- 21
R14 | 4040 15 15 56 21 --- 14 | 26 30 61 20 --- 22
R15 | 4931 27 38 33 39 102 21 | 26 41 62 14 39 20
R17 | 7832 46 21 94 32 --- 24 | 175 212 264 199 --- 202
R19 | 5201 276 116 263 52 --- 93 | 773 927 9999 887 --- 891
R20 | 613 51 23 60 25 --- 20 | 137 153 147 140 --- 146
R23 | 2422 38 21 79 25 --- 20 | 50 56 93 59 --- 55
R24 | 2487 28 20 41 23 345 15 | 86 71 79 75 107 69
------+------------------------------------+--------------------------------
RMS | 4758 84 40 100 29 228 |T 123 164 107 132 60 153
WRMS | 4758 33 26 70 29 228 |NE 123 164 107 132 60 153
MEDI | 3992 34 21 60 25 164 |MD 38 44 83 37 39 31
Table 3.1493.5 GPS week: 1493 Day: 5 MJD: 54700
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 10 --- --- --- 0 | --- 180 --- --- --- 178
R04 | 3392 11 32 38 32 --- 17 | 22 39 80 28 --- 28
R06 | 6925 36 33 50 22 --- 20 | 164 181 175 153 --- 165
R07 | 1472 25 18 78 26 --- 21 | 25 28 116 24 --- 22
XR09 |81394 --- --- 14 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 3632 11 18 25 22 --- 11 | 19 18 35 17 --- 12
R11 | 3473 25 26 30 34 163 16 | 30 44 32 44 63 29
R13 | 1722 34 39 43 40 --- 22 | 30 62 80 63 --- 47
R14 | 6299 30 12 45 15 --- 14 | 30 46 54 19 --- 27
R15 | 4492 31 26 116 42 101 31 | 17 25 92 30 56 21
R17 | 2047 65 27 44 47 --- 27 | 131 165 168 166 --- 153
R19 | 6993 32 26 35 36 --- 18 | 844 876 948 881 --- 877
R20 | 2419 60 24 52 33 --- 24 | 124 149 149 144 --- 142
R23 | 3379 31 36 106 23 --- 28 | 38 66 88 53 --- 48
R24 | 1793 45 24 49 34 439 21 | 80 79 91 76 228 73
------+------------------------------------+--------------------------------
RMS | 4144 37 27 61 32 276 |T 119 139 162 130 115 130
WRMS | 4144 28 25 51 32 276 |NE 119 139 162 130 115 130
MEDI | 3392 31 26 44 33 163 |MD 30 62 91 53 63 47
Table 3.1493.6 GPS week: 1493 Day: 6 MJD: 54701
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 10 --- --- --- 0 | --- 256 --- --- --- 254
R04 | 1817 28 33 36 35 --- 19 | 43 31 43 24 --- 24
R06 | 6459 25 37 31 25 --- 17 | 189 188 192 181 --- 185
R07 | 1599 58 28 75 23 --- 26 | 31 44 69 30 --- 26
XR09 |13610 --- --- 10 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 6491 27 27 33 22 --- 15 | 17 20 24 25 --- 14
R11 | 3712 32 23 27 16 38 14 | 24 50 58 55 66 45
R13 | 6586 41 35 67 37 --- 25 | 37 40 60 46 --- 36
R14 | 5339 35 22 25 23 --- 15 | 45 40 52 51 --- 44
R15 | 3149 33 36 36 32 76 19 | 39 39 62 23 73 26
R17 | 1720 47 28 69 22 --- 23 | 125 134 185 126 --- 134
R19 | 4322 36 30 48 17 --- 18 | 652 695 708 684 --- 684
R20 | 1609 54 48 60 24 --- 26 | 136 153 159 148 --- 149
R23 | 4573 39 81 108 28 --- 37 | 72 80 88 91 --- 77
R24 | 5359 118 50 122 36 --- 46 | 126 133 82 102 --- 99
------+------------------------------------+--------------------------------
RMS | 4465 50 40 64 27 60 |T 118 135 137 122 69 128
WRMS | 4465 39 38 53 27 60 |NE 118 135 137 122 69 128
MEDI | 4322 36 30 36 24 38 |MD 45 50 69 55 66 45
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