[IGSREPORT-16659] Wk 1496 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Sep 25 06:24:22 PDT 2008
******************************************************************************
IGS Electronic Report 25 Sep 06:24:25 PDT 2008 Message Number 16659
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1496 (Sep 07, 2008 - Sep 13, 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 2.1496.
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:
igl1496[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1496 in the SP3 format.
igl14967.sum Combination Report for GPS Week 1496.
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 | 635.0 ns
1 | 634.4 ns
2 | 634.9 ns
3 | 639.1 ns
4 | 593.3 ns
5 | 568.7 ns
6 | 650.5 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
----+--------+---------------
4 | ESX | R19
5 | ESX | R19
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 1.1496, 1a.1496).
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 2.1496.0-6)
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 3.1496.0-6).
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 1496 summary. (Sep 07, 2008 - Sep 13, 2008)
Table 1.1496.a GPS week : 1496 MJD: 54716.0-54722.0
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 63| 1 0 -6 6 6 30 -.05 38 31 | 0 -56 2571 2670
| 2 0 4 67 36 83 .05 | 0 142
cod 215| -5 0 3 -4 13 82 -.12 30 22 | --- --- --- ---
| 1 1 5 54 36 67 .07 | --- ---
esx 126| 1 -5 10 -28 -62 -128 .42 7472 >>>> | 74650 1783 9284 17641
| 3 7 8 61 78 141 .07 | 29060 10090
iac n/a| 5 1 -2 21 15 -78 -.07 43 43 | 624074 -1335 6746 14270
| 4 2 10 65 58 74 .09 | 28388 4923
mcc n/a| -4 -5 60 11 43 -952 -.56 191 191 | --- --- --- ---
| 14 12 25 152 137 931 .62 | --- ---
Table 1.1496.b GPS week : 1496 MJD: 54716.0-54722.0
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 | 20 34 27 19 20 16 25 |
R06 | 32 23 19 26 23 19 28 |
R07 | 15 11 11 15 14 16 15 |
R09 | 0 0 0 0 0 0 0 |
R10 | 22 15 13 19 12 21 15 |
R11 | 13 20 23 21 19 13 15 |
R13 | 32 19 17 13 23 25 21 |
R14 | 15 9 10 19 16 17 12 |
R15 | 25 19 13 22 13 15 16 |
R17 | 27 27 25 30 28 26 32 |
R19 | 32 20 24 23 28 30 35 |
R20 | 25 28 29 27 25 25 24 |
R23 | 40 52 29 46 47 45 41 |
R24 | 29 21 17 18 17 14 18 |
Table 1.1496.c GPS week : 1496 MJD: 54716.0-54722.0
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 1496 0 | -103 244 229 -2333 -33 -10770 92.3 3641 3641 | 634966 0
brd 1496 1 | 2281 639 1737 -3636 14570 -33200 <<<< >>>>> >>>>> | 634380 0
brd 1496 2 | -71 -230 149 2068 -54 1668 98.4 3815 3815 | 634886 0
brd 1496 3 | 18 138 47 -3158 408 151 97.8 3753 3753 | 639108 0
brd 1496 4 | -203 235 224 -1876 -949 -6392 92.0 3313 3313 | 593339 0
brd 1496 5 | -77 24 116 -2397 2476 -489 95.9 2366 2366 | 568722 0
brd 1496 6 | -35 -196 76 -3168 886 -3809 94.1 3741 3741 | 650526 0
-------------+------------------------------------------------------------+----------------
brd 1496 mean| 258 122 368 -2071 2471 -7548 <<<< >>>>> >>>>> | 622275 0
brd 1496 sdev| 894 297 607 1922 5439 12095 822.1 >>>>> >>>>> | 29589 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 2.1496.0 GPS week: 1496 Day: 0 MJD: 54716
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 63| 1 0 -13 -68 77 109 -.02 45 35 | 0 -48 2061 2134
cod 215| -6 0 6 70 15 8 -.10 30 22 | --- --- --- ---
esx 126| 1 -11 6 -35 -198 -243 .37 67 55 | 80394 13961 9767 17097
iac n/a| 5 5 2 -62 76 31 -.21 52 52 | 634612 5031 6091 14130
mcc n/a| -29 -20 115 -297 30 1045 .57 350 350 | --- --- --- ---
Table 2.1496.1 GPS week: 1496 Day: 1 MJD: 54717
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 63| 3 1 -9 -27 -4 141 -.10 40 26 | 0 -106 2123 2225
cod 215| -6 0 8 14 2 23 -.15 29 24 | --- --- --- ---
esx 126| 2 -4 20 81 36 -265 .47 66 46 | 87461 -2660 8435 15718
iac n/a| 9 0 -13 -44 0 -110 -.01 43 43 | 636527 -7632 5897 12704
mcc n/a| 5 -21 44 87 195 -1332 -.55 173 173 | --- --- --- ---
Table 2.1496.2 GPS week: 1496 Day: 2 MJD: 54718
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 63| 1 0 -6 -8 -15 -79 .00 31 27 | 0 71 2150 2243
cod 215| -2 1 7 21 47 157 -.24 25 21 | --- --- --- ---
esx 126| 3 0 2 -45 6 -51 .40 47 36 | 90399 8849 10681 16199
iac n/a| 4 -1 -12 -4 -96 -118 -.09 48 48 | 635030 4887 8139 13306
mcc n/a| 14 -1 56 73 2 -1175 -.88 109 109 | --- --- --- ---
Table 2.1496.3 GPS week: 1496 Day: 3 MJD: 54719
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 63| 0 0 -5 -18 -42 -49 -.02 38 31 | 0 -329 3403 3536
cod 215| -7 2 8 -15 70 142 -.13 32 26 | --- --- --- ---
esx 126| 6 0 10 -44 -70 12 .41 60 52 | 100012 -11833 7490 19880
iac n/a| 7 1 -12 46 -7 -79 .00 44 44 | 645538 -5621 7325 21128
mcc n/a| 6 9 48 -84 263 -1653 -1.37 186 186 | --- --- --- ---
Table 2.1496.4 GPS week: 1496 Day: 4 MJD: 54720
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 63| -4 0 -2 -15 17 29 -.00 31 26 | 0 -96 2802 2955
cod 215| -5 -2 0 25 -37 160 -.06 40 23 | --- --- --- ---
esx 126| 5 -19 23 -52 -115 -301 .28 >>>> >>>> | 42781 12385 13655 19692
iac n/a| 3 2 -5 20 66 -52 .00 31 31 | 592398 -857 8276 14469
mcc n/a| -3 6 40 89 -59 -1658 -.14 305 305 | --- --- --- ---
Table 2.1496.5 GPS week: 1496 Day: 5 MJD: 54721
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 63| 5 -1 -9 142 1 -14 -.08 39 35 | 0 76 2367 2409
cod 215| -6 -2 -1 -80 12 45 -.11 23 18 | --- --- --- ---
esx 126| 0 -3 0 -116 -66 -100 .49 121 53 | 24859 -527 8004 16222
iac n/a| 11 1 10 74 31 -21 -.01 39 39 | 575441 -4139 5362 10016
mcc n/a| -11 -2 69 134 -121 -815 -.75 97 97 | --- --- --- ---
Table 2.1496.6 GPS week: 1496 Day: 6 MJD: 54722
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 63| 2 -1 0 38 10 79 -.11 41 35 | 0 38 3092 3189
cod 215| -5 -1 -6 -68 -13 40 -.05 30 24 | --- --- --- ---
esx 126| -5 3 7 12 -29 51 .48 54 40 | 96649 -7694 6958 18680
iac n/a| 0 -2 10 121 38 -200 -.15 46 46 | 648975 -1016 6132 14142
mcc n/a| -11 -5 46 74 -7 -1081 -.79 120 120 | --- --- --- ---
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 3.1496.0 GPS week: 1496 Day: 0 MJD: 54716
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 845 --- --- --- 845
R04 | 5951 36 22 55 28 --- 19 | 52 26 64 27 --- 31
R06 | 6049 74 53 38 43 --- 32 | 71 111 125 77 --- 89
R07 | 991 34 13 40 17 --- 14 | 40 20 32 13 --- 13
XR09 |30764 --- --- 20 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2462 26 9 78 40 --- 22 | 16 28 50 31 --- 24
R11 | 3089 23 10 36 26 291 13 | 34 23 43 32 177 22
R13 | 1883 27 31 112 55 --- 32 | 30 27 124 61 --- 37
R14 | 2041 23 14 47 25 --- 15 | 32 32 32 30 --- 25
R15 | 1603 26 33 61 59 173 25 | 48 43 76 67 60 48
R17E | 3187 36 19 65 71 --- 26 | 56 55 74 80 --- 56
R19E | 722 65 39 79 48 --- 32 | 65 57 9999 54 --- 45
R20E | 1276 50 27 61 46 --- 25 | 54 23 54 66 --- 34
R23E | 7386 66 40 92 95 --- 40 | 236 228 252 241 --- 230
R24E | 2564 49 36 61 61 503 28 | 66 40 73 86 343 51
------+------------------------------------+--------------------------------
RMS | 3640 44 30 67 52 350 |T 61 111 83 66 193 110
WRMS | 3640 35 22 55 52 350 |NE 40 128 68 42 118 126
MEDI | 2462 36 22 61 46 291 |MD 52 32 64 61 177 37
Table 3.1496.1 GPS week: 1496 Day: 1 MJD: 54717
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 9999 --- --- --- 9999
XR04 |>>>>> --- 40 66 45 --- 33 | --- 62 56 21 --- 31
R06 |>>>>> 20 23 92 20 --- 22 | 68 58 128 73 --- 71
R07 |>>>>> 14 18 30 16 --- 11 | 19 21 32 23 --- 14
XR09 |>>>>> --- --- 20 --- --- 0 | --- --- 9999 --- --- 9999
R10 |>>>>> 20 23 38 24 --- 14 | 34 26 47 27 --- 22
R11 |>>>>> 19 11 72 38 122 19 | 19 26 63 51 135 28
R13 |>>>>> 19 11 51 49 --- 18 | 15 27 44 59 --- 23
R14 |>>>>> 9 8 29 17 --- 8 | 25 25 37 22 --- 21
R15 |>>>>> 24 30 42 36 51 18 | 46 32 45 22 53 24
R17E |>>>>> 38 19 87 52 --- 26 | 52 37 120 64 --- 48
R19E |>>>>> 38 25 44 33 --- 19 | 63 36 9999 52 --- 42
R20E |>>>>> 58 39 59 38 --- 27 | 49 41 53 53 --- 37
R23E |>>>>> 98 66 124 90 --- 52 | 154 177 221 157 --- 158
R24E |>>>>> 26 20 49 53 269 20 | 40 48 86 73 302 52
------+------------------------------------+--------------------------------
RMS |>>>>> 40 29 66 43 173 |T 48 47 77 53 163 43
WRMS |>>>>> 26 24 46 43 173 |NE 32 34 56 37 94 29
MEDI |>>>>> 20 20 49 38 122 |MD 40 36 53 52 135 31
Table 3.1496.2 GPS week: 1496 Day: 2 MJD: 54718
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 11 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 3720 42 27 79 44 --- 27 | 31 29 87 24 --- 16
R06 | 1785 40 27 33 28 --- 18 | 84 75 83 85 --- 75
R07 | 2586 13 18 25 20 --- 10 | 13 24 28 27 --- 14
XR09 |21559 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1399 17 20 37 14 --- 13 | 20 25 33 18 --- 14
R11 | 5100 21 10 52 75 95 22 | 25 20 36 54 80 12
R13 | 4953 16 18 41 44 --- 16 | 18 21 39 60 --- 19
R14 | 1085 8 9 27 26 --- 9 | 22 23 39 39 --- 23
R15 | 2360 28 16 23 24 82 13 | 29 41 48 30 28 30
R17E | 4315 33 29 66 54 --- 25 | 62 43 104 77 --- 54
R19E | 1102 38 30 53 50 --- 23 | 30 23 9999 43 --- 20
R20E | 1183 49 44 62 48 --- 28 | 53 23 66 62 --- 36
R23E | 6701 40 31 41 90 --- 28 | 120 112 110 136 --- 108
R24E | 6331 28 15 32 46 140 16 | 20 30 46 50 144 26
------+------------------------------------+--------------------------------
RMS | 3815 31 24 47 48 109 |T 40 37 59 54 84 34
WRMS | 3815 27 21 36 48 109 |NE 30 32 49 42 54 25
MEDI | 2586 28 18 37 44 95 |MD 29 25 46 50 80 23
Table 3.1496.3 GPS week: 1496 Day: 3 MJD: 54719
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 11 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 2408 38 23 49 24 --- 19 | 30 31 49 34 --- 16
R06 | 2007 54 31 47 48 --- 26 | 101 126 144 95 --- 112
R07 | 2675 21 14 41 29 --- 14 | 13 24 40 32 --- 14
XR09 | 7453 --- --- 11 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1400 30 21 59 20 --- 18 | 22 35 87 50 --- 40
R11 | 4873 20 37 33 48 98 20 | 20 17 66 51 53 26
R13 | 2392 20 17 40 15 --- 13 | 29 38 72 37 --- 35
R14 | 1108 28 27 51 32 --- 19 | 45 31 35 50 --- 30
R15 | 8880 39 22 59 36 124 22 | 36 30 63 49 46 26
R17E | 2575 29 36 98 49 --- 30 | 43 40 97 49 --- 35
R19E | 1208 37 24 64 38 --- 22 | 54 42 9999 59 --- 41
R20E | 1416 38 41 45 61 --- 27 | 28 24 43 57 --- 24
R23E | 4342 70 65 107 87 --- 46 | 105 112 166 132 --- 110
R24E | 5065 32 20 42 32 280 17 | 36 46 52 51 97 37
------+------------------------------------+--------------------------------
RMS | 3753 38 32 60 44 186 |T 43 45 76 57 65 42
WRMS | 3753 31 26 52 44 186 |NE 37 41 69 49 49 37
MEDI | 2408 32 23 47 36 124 |MD 36 35 63 50 53 35
Table 3.1496.4 GPS week: 1496 Day: 4 MJD: 54720
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 1425 33 23 79 13 --- 20 | 20 35 71 26 --- 23
R06 | 3136 22 40 73 33 --- 22 | 50 77 125 74 --- 67
R07 | 1500 25 16 43 17 --- 13 | 15 25 43 38 --- 23
XR09 |13597 --- --- 27 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1471 15 17 43 13 --- 11 | 28 29 46 30 --- 26
R11 | 2147 11 22 78 24 102 18 | 14 24 48 36 38 11
R13 | 1191 14 30 103 18 --- 23 | 23 39 106 34 --- 28
R14 | 1356 24 25 58 16 --- 16 | 34 38 68 32 --- 31
R15 | 6292 14 18 44 22 143 13 | 35 30 45 49 68 32
R17E | 2568 33 47 80 45 --- 27 | 43 37 79 59 --- 38
R19E | 2346 34 44 >>>> 38 --- 27 | 56 42 9999 58 --- 41
R20E | 1563 32 41 66 42 --- 24 | 32 29 94 65 --- 38
R23E | 6328 71 97 122 55 --- 47 | 87 108 155 92 --- 82
R24E | 4936 25 34 31 27 499 17 | 38 38 63 48 137 37
------+------------------------------------+--------------------------------
RMS | 3313 31 40 >>>> 31 305 |T 36 42 78 49 81 36
WRMS | 3313 26 23 >>>> 31 305 |NE 27 37 69 39 53 30
MEDI | 2147 25 25 66 24 143 |MD 34 37 68 48 68 32
Table 3.1496.5 GPS week: 1496 Day: 5 MJD: 54721
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 684 --- --- --- 683
R04 | 1363 39 13 43 22 --- 15 | 36 41 56 30 --- 32
R06 | 3364 15 27 70 22 --- 18 | 88 81 106 60 --- 75
R07 | 2043 35 13 49 23 --- 15 | 28 33 64 43 --- 29
XR09 |20381 --- --- 12 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1770 35 19 81 24 --- 20 | 48 42 57 34 --- 33
R11 | 1142 23 14 30 28 109 12 | 29 31 62 23 47 20
R13 | 1040 40 18 96 37 --- 24 | 21 51 123 29 --- 41
R14 | 1988 28 26 28 36 --- 17 | 38 56 25 33 --- 36
R15 | 4226 24 12 58 22 85 15 | 35 23 40 33 53 23
R17E | 2628 56 32 61 47 --- 26 | 64 55 61 56 --- 45
R19E | 1952 40 36 349 53 --- 29 | 28 44 9999 54 --- 36
R20E | 1718 41 18 80 50 --- 24 | 42 27 85 51 --- 30
R23E | 3303 68 34 167 77 --- 44 | 106 104 229 70 --- 97
R24E | 1864 30 12 36 30 --- 14 | 41 36 61 45 --- 40
------+------------------------------------+--------------------------------
RMS | 2365 39 23 121 39 97 |T 46 93 80 43 50 87
WRMS | 2365 35 18 53 39 97 |NE 40 115 66 35 50 108
MEDI | 1952 35 18 58 30 85 |MD 38 42 61 43 47 36
Table 3.1496.6 GPS week: 1496 Day: 6 MJD: 54722
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 441 --- --- --- 441
R04 | 1896 62 29 42 31 --- 24 | 41 30 56 25 --- 22
R06 | 6941 68 24 41 57 --- 28 | 70 92 101 86 --- 81
R07 | 3294 15 23 37 27 --- 15 | 48 26 52 41 --- 35
XR09 |11959 --- --- 9 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 7744 14 23 33 32 --- 15 | 29 32 37 43 --- 29
R11 | 1835 19 17 40 26 119 14 | 16 28 43 37 66 24
R13 | 1141 30 33 51 29 --- 20 | 31 42 58 29 --- 28
R14 | 2538 20 11 29 27 --- 12 | 25 22 24 36 --- 20
R15 | 2058 17 25 44 20 120 15 | 31 34 31 47 51 29
R17E | 3038 65 43 56 61 --- 32 | 59 63 45 56 --- 48
R19E | 1084 50 28 88 76 --- 34 | 56 23 9999 58 --- 32
R20E | 1124 28 26 37 69 --- 23 | 49 31 49 43 --- 32
R23E | 2537 52 61 108 58 --- 40 | 106 128 181 130 --- 119
R24E | 5083 32 17 35 40 --- 17 | 32 34 50 56 --- 35
------+------------------------------------+--------------------------------
RMS | 3740 41 30 54 46 120 |T 45 73 60 52 58 69
WRMS | 3740 35 24 40 46 120 |NE 36 83 50 43 58 78
MEDI | 2537 30 24 40 32 119 |MD 41 32 49 43 51 32
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