[IGSREPORT-16637] Wk 1495 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Sep 18 07:05:38 PDT 2008
******************************************************************************
IGS Electronic Report 18 Sep 07:05:41 PDT 2008 Message Number 16637
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1495 (Aug 31, 2008 - Sep 06, 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 2.1495.
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:
igl1495[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1495 in the SP3 format.
igl14957.sum Combination Report for GPS Week 1495.
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 | 597.6 ns
1 | 633.8 ns
2 | 627.1 ns
3 | 534.9 ns
4 | 636.7 ns
5 | 637.5 ns
6 | 603.4 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
----+--------+---------------
0 | IAC | R23
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 1.1495, 1a.1495).
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 2.1495.0-6)
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 3.1495.0-6).
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 1495 summary. (Aug 31, 2008 - Sep 06, 2008)
Table 1.1495.a GPS week : 1495 MJD: 54709.0-54715.0
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 64| 1 0 0 -19 16 -27 -.05 42 32 | 0 -154 2470 2605
| 3 3 5 50 35 128 .08 | 0 210
cod 217| -5 -2 -2 12 22 17 -.09 28 18 | --- --- --- ---
| 2 2 4 20 51 38 .07 | --- ---
esx 115| 4 0 1 -38 -59 -28 .37 66 59 | 4174 -103 9320 20047
| 6 8 5 80 70 115 .10 | 40083 9712
iac n/a| 4 2 2 0 -3 -3 -.07 49 49 | 613748 -2249 7582 14990
| 2 3 9 36 45 94 .08 | 38959 6147
mcc n/a| 0 12 77 71 -4 301 .28 430 430 | --- --- --- ---
| 29 26 41 234 468 1220 .74 | --- ---
Table 1.1495.b GPS week : 1495 MJD: 54709.0-54715.0
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 | 16 19 26 24 22 20 21 |
R06 | 32 19 20 22 27 29 28 |
R07 | 19 13 21 17 17 11 22 |
R09 | 0 0 0 0 0 0 0 |
R10 | 16 20 19 15 19 15 19 |
R11 | 23 19 22 18 17 21 28 |
R13 | 26 15 14 18 21 14 23 |
R14 | 15 14 15 10 8 13 15 |
R15 | 16 22 20 15 13 13 27 |
R17 | 32 33 16 24 16 18 25 |
R19 | 23 36 16 36 24 29 34 |
R20 | 21 29 17 19 19 28 22 |
R23 | 43 46 48 685 29 73 49 |
R24 | 21 29 27 21 17 21 23 |
Table 1.1495.c GPS week : 1495 MJD: 54709.0-54715.0
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 1495 0 | -74 216 175 -418 743 -10700 91.8 6718 6718 | 597650 0
brd 1495 1 | 544 28 750 11850 -934 20150 <<<< >>>>> >>>>> | 633774 0
brd 1495 2 | -34 -63 149 3640 -4218 -13150 94.9 5826 5826 | 627144 0
brd 1495 3 | -96 3 167 3137 -2708 -12390 97.1 2768 2768 | 534912 0
brd 1495 4 | -121 0 306 -4751 -887 -13310 100.7 8842 8842 | 636712 0
brd 1495 5 | -19 -245 216 5016 2750 -18880 98.9 6955 6955 | 637483 0
brd 1495 6 | -18 -111 -7 -296 -575 -14070 95.9 5379 5379 | 603389 0
-------------+------------------------------------------------------------+----------------
brd 1495 mean| 25 -24 251 2596 -832 -8907 -89.7 >>>>> >>>>> | 610152 0
brd 1495 sdev| 232 141 239 5233 2250 13058 492.7 >>>>> >>>>> | 36883 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 2.1495.0 GPS week: 1495 Day: 0 MJD: 54709
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 64| 1 0 -8 -84 23 119 -.08 40 34 | 0 -279 2336 2433
cod 217| -6 3 -6 30 6 -19 -.15 24 20 | --- --- --- ---
esx 115| 4 9 5 -117 -39 129 .49 61 50 | -15527 8715 9391 16293
iac n/a| 7 -5 20 17 -53 -184 -.05 109 109 | 599235 574 9188 15393
mcc n/a| -10 -12 12 -180 -645 158 1.10 558 558 | --- --- --- ---
Table 2.1495.1 GPS week: 1495 Day: 1 MJD: 54710
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 64| 8 -4 0 56 36 -37 -.12 46 33 | 0 -90 2029 2318
cod 217| -7 -4 -7 -19 31 64 -.02 34 22 | --- --- --- ---
esx 115| -6 3 0 -138 -96 -105 .51 71 61 | 35240 5323 11380 20373
iac n/a| 8 3 5 -13 15 -15 -.16 38 38 | 639516 -3857 8015 18181
mcc n/a| 29 -13 40 210 -203 -300 .35 425 425 | --- --- --- ---
Table 2.1495.2 GPS week: 1495 Day: 2 MJD: 54711
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 64| -2 4 7 -15 41 -167 -.10 41 31 | 0 -43 2515 2617
cod 217| -6 -3 -6 -2 92 -1 -.01 31 18 | --- --- --- ---
esx 115| 6 -7 -8 71 -169 136 .36 61 55 | 28393 -8587 6911 18082
iac n/a| 1 3 2 -55 -76 102 .04 33 33 | 631172 -3705 7686 12618
mcc n/a| 13 34 96 366 611 -971 -.75 499 499 | --- --- --- ---
Table 2.1495.3 GPS week: 1495 Day: 3 MJD: 54712
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 64| 0 2 2 -15 -40 109 -.02 31 29 | 0 -281 2422 2580
cod 217| -2 -1 0 16 89 -2 -.06 21 19 | --- --- --- ---
esx 115| 2 8 6 -23 -96 -156 .31 68 80 | -75608 -16 8090 21590
iac n/a| 2 3 -9 -31 -5 -45 -.04 34 34 | 534593 2633 6338 9311
mcc n/a| 15 -12 60 -154 586 -1096 -.02 773 773 | --- --- --- ---
Table 2.1495.4 GPS week: 1495 Day: 4 MJD: 54713
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 64| 5 0 -2 -15 -22 77 .06 34 26 | 0 -415 2866 2978
cod 217| -6 -2 -2 18 -12 -26 -.15 21 13 | --- --- --- ---
esx 115| 8 -2 3 1 -48 -95 .28 59 49 | 33115 -12281 10750 29625
iac n/a| 6 3 4 12 44 9 -.02 35 35 | 642931 -10062 7252 19051
mcc n/a| 32 18 109 -81 -134 1930 .44 287 287 | --- --- --- ---
Table 2.1495.5 GPS week: 1495 Day: 5 MJD: 54714
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 64| 0 -3 -1 17 17 -146 .02 55 32 | 0 229 2570 2676
cod 217| -1 -4 0 2 -4 53 -.06 29 14 | --- --- --- ---
esx 115| 3 -1 -2 -98 -17 -45 .27 73 56 | 25605 13514 9097 19215
iac n/a| 3 5 -1 58 10 63 -.18 52 52 | 641497 7215 7800 17846
mcc n/a| -42 54 98 352 -335 1802 -.41 211 211 | --- --- --- ---
Table 2.1495.6 GPS week: 1495 Day: 6 MJD: 54715
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 64| 0 5 -4 -79 57 -143 -.13 48 37 | 0 -201 2555 2635
cod 217| -10 -1 3 40 -42 52 -.19 34 22 | --- --- --- ---
esx 115| 14 -13 6 36 52 -60 .35 72 60 | -1998 -7389 9624 15156
iac n/a| 4 3 -4 8 41 48 -.05 43 43 | 607297 -8547 6799 12535
mcc n/a| -33 16 126 -12 91 586 1.26 260 260 | --- --- --- ---
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 3.1495.0 GPS week: 1495 Day: 0 MJD: 54709
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 868 --- --- --- 869
R04 | 1228 23 24 29 34 --- 15 | 63 41 38 29 --- 39
R06 |11579 62 20 47 89 --- 31 | 159 174 197 192 --- 173
R07 | 1572 25 23 62 19 --- 18 | 27 27 64 31 --- 27
XR09 |15513 --- --- 14 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1535 16 17 44 33 --- 15 | 24 27 40 42 --- 25
R11M | 9818 43 18 41 60 414 23 | 31 47 83 91 143 52
R13 |11653 56 10 68 47 --- 25 | 21 22 68 43 --- 26
R14 | 1331 16 14 44 33 --- 15 | 21 32 40 30 --- 24
R15 | 3127 15 17 43 38 93 16 | 37 39 39 37 34 29
R17 |12272 49 39 102 36 --- 32 | 50 73 127 49 --- 54
R19 | 598 41 25 69 23 --- 22 | 133 125 140 125 --- 127
R20 | 1743 49 28 28 35 --- 20 | 86 87 93 90 --- 84
R23 | 1682 55 24 111 362 --- 43 | 9999 9999 9999 9999 --- 9999
R24 | 6758 31 31 36 43 869 20 | 107 130 118 124 453 117
------+------------------------------------+--------------------------------
RMS | 6718 40 23 61 109 558 |T 63 130 87 73 210 126
WRMS | 6718 34 20 50 109 558 |NE 50 153 69 57 34 151
MEDI | 1743 41 20 44 36 414 |MD 37 47 68 43 143 52
Table 3.1495.1 GPS week: 1495 Day: 1 MJD: 54710
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 8 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 |>>>>> 26 18 47 41 --- 18 | 36 25 39 31 --- 23
R06 |>>>>> 38 33 36 26 --- 19 | 197 174 168 163 --- 174
R07 |>>>>> 20 19 30 24 --- 13 | 28 28 49 25 --- 20
XR09 |>>>>> --- --- 14 --- --- 0 | --- --- 9999 --- --- 9999
R10 |>>>>> 25 18 60 39 --- 20 | 37 24 46 47 --- 29
R11 |>>>>> 25 16 68 27 276 19 | 53 29 65 38 66 28
R13 |>>>>> 22 16 49 22 --- 15 | 28 26 59 23 --- 22
R14 |>>>>> 16 14 51 20 --- 14 | 20 22 65 19 --- 19
R15 |>>>>> 27 33 73 26 64 22 | 36 21 92 31 36 27
R17E |>>>>> 55 29 123 28 --- 33 | 28 53 139 48 --- 43
R19E |>>>>> 79 34 107 40 --- 36 | 63 111 174 86 --- 93
R20E |>>>>> 37 47 55 61 --- 29 | 60 93 107 82 --- 72
R23 |>>>>> 100 77 74 63 --- 46 | 9999 9999 9999 9999 --- 9999
R24E |>>>>> 46 34 81 48 680 28 | 82 107 149 104 597 97
------+------------------------------------+--------------------------------
RMS |>>>>> 46 34 71 38 425 |T 55 59 96 58 233 53
WRMS |>>>>> 33 22 61 38 425 |NE 54 45 74 48 36 44
MEDI |>>>>> 27 19 55 28 276 |MD 36 28 65 38 66 28
Table 3.1495.2 GPS week: 1495 Day: 2 MJD: 54711
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 8 --- --- --- 0 | --- 950 --- --- --- 949
XR04 | 2349 50 30 --- 29 --- 25 | 39 29 --- 32 --- 23
R06 |13624 30 19 63 29 --- 19 | 88 97 156 89 --- 97
R07 | 2172 41 20 68 23 --- 21 | 31 36 73 27 --- 26
XR09 |12960 --- --- 16 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1317 28 21 57 32 --- 19 | 24 25 81 41 --- 26
R11 | 4429 42 19 62 34 209 21 | 43 22 81 23 81 23
R13 | 9339 17 20 41 19 --- 13 | 29 25 66 34 --- 31
R14 | 2079 22 16 47 25 --- 15 | 28 22 52 28 --- 21
R15 | 5673 32 15 49 39 103 19 | 46 28 56 33 23 29
R17E | 6879 26 26 43 22 --- 16 | 36 35 62 36 --- 32
R19E | 745 32 27 28 22 --- 16 | 62 59 119 81 --- 69
R20E | 1459 22 22 57 22 --- 17 | 58 71 106 74 --- 70
R23E | 873 82 72 122 69 --- 47 | 9999 9999 9999 9999 --- 9999
R24E | 4595 67 43 47 27 832 27 | 58 96 100 103 424 83
------+------------------------------------+--------------------------------
RMS | 5826 41 31 61 33 498 |T 45 115 86 50 176 113
WRMS | 5826 31 18 55 33 498 |NE 40 151 80 40 23 150
MEDI | 2349 32 20 49 27 209 |MD 39 35 81 34 81 31
Table 3.1495.3 GPS week: 1495 Day: 3 MJD: 54712
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 5 --- --- --- 0 | --- 431 --- --- --- 434
R04 | 3583 37 22 82 36 --- 23 | 34 31 74 46 --- 27
R06 | 2665 40 31 38 44 --- 21 | 254 252 256 235 --- 246
R07 | 2179 23 17 38 40 --- 16 | 17 35 55 39 --- 26
XR09 |17468 --- --- 13 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1220 31 12 43 23 --- 14 | 27 40 37 44 --- 34
R11 | 2017 27 19 66 24 80 18 | 16 37 78 37 183 28
R13 | 2513 25 24 60 19 --- 17 | 18 44 48 40 --- 24
R14 | 4331 17 13 31 12 --- 10 | 38 19 33 33 --- 25
R15 | 3474 24 11 47 28 111 14 | 36 26 60 42 48 30
R17E | 1395 39 20 79 41 --- 23 | 40 25 84 45 --- 26
R19E | 1176 44 31 147 36 --- 35 | 91 92 147 108 --- 89
R20E | 2264 29 15 65 29 --- 18 | 74 62 90 74 --- 65
XR23E |11511 --- 311 --- 1037 --- 684 | --- 9999 --- 9999 --- 9999
R24E | 4013 29 25 24 56 1332 20 | 71 79 80 109 933 78
------+------------------------------------+--------------------------------
RMS | 2768 31 21 68 34 773 |T 59 90 86 71 388 87
WRMS | 2768 29 19 80 34 773 |NE 60 109 80 68 48 105
MEDI | 2513 29 19 47 36 111 |MD 36 40 74 44 183 30
Table 3.1495.4 GPS week: 1495 Day: 4 MJD: 54713
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 5 --- --- --- 0 | --- 484 --- --- --- 487
R04 |19397 59 21 49 17 --- 21 | 66 45 50 25 --- 31
R06 | 2778 47 35 86 34 --- 27 | 82 105 172 81 --- 99
R07 | 1145 24 13 60 30 --- 17 | 15 32 44 32 --- 23
XR09 |39574 --- --- 9 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2033 22 17 73 27 --- 19 | 23 23 55 28 --- 18
R11 | 2173 21 18 60 24 194 16 | 31 28 71 35 101 28
R13 | 2146 23 16 73 44 --- 21 | 31 48 104 35 --- 41
R14 | 3074 6 8 30 16 --- 8 | 21 20 32 22 --- 18
R15 | 3321 23 8 27 32 185 12 | 33 19 37 34 27 18
R17E | 2291 29 16 43 32 --- 16 | 40 20 57 39 --- 26
R19E | 6376 39 22 84 31 --- 23 | 52 53 101 38 --- 46
R20E | 1970 27 18 60 38 --- 19 | 60 39 77 54 --- 47
R23E |22995 48 40 49 67 --- 29 | 9999 9999 9999 9999 --- 9999
R24E | 4301 36 19 23 38 419 16 | 64 58 73 82 700 62
------+------------------------------------+--------------------------------
RMS | 8841 34 21 59 35 287 |T 43 74 72 42 276 72
WRMS | 8841 26 13 49 35 287 |NE 38 97 70 36 27 91
MEDI | 2778 27 17 49 32 194 |MD 33 39 57 35 101 31
Table 3.1495.5 GPS week: 1495 Day: 5 MJD: 54714
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 3 --- --- --- 0 | --- 556 --- --- --- 556
R04 | 6601 43 9 64 31 --- 20 | 25 18 76 32 --- 17
R06 | 2455 67 30 68 44 --- 28 | 235 200 239 190 --- 207
R07 | 1419 22 8 24 22 --- 10 | 23 29 38 22 --- 23
XR09 |14718 --- --- 8 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 3111 30 14 38 27 --- 14 | 17 29 37 37 --- 25
R11 | 2983 36 23 66 29 211 20 | 36 41 76 49 100 38
R13 | 2355 28 16 39 24 --- 14 | 14 27 36 22 --- 16
R14 | 2130 21 11 34 30 --- 13 | 24 23 38 53 --- 28
R15 | 2959 19 18 31 23 218 12 | 31 28 39 28 24 21
R17E | 3205 38 25 45 24 --- 18 | 41 41 41 30 --- 27
R19E | 8333 58 30 82 46 --- 28 | 65 91 89 81 --- 72
R20E | 1825 29 27 102 41 --- 27 | 43 48 84 49 --- 44
R23E |21184 151 76 175 143 --- 73 | 9999 9999 9999 9999 --- 9999
R24E | 2812 29 19 41 59 204 21 | 49 50 71 80 379 53
------+------------------------------------+--------------------------------
RMS | 6954 55 29 73 52 211 |T 50 90 72 56 167 86
WRMS | 6954 32 14 56 52 211 |NE 52 113 71 54 24 111
MEDI | 2959 30 18 41 30 211 |MD 31 41 41 37 100 28
Table 3.1495.6 GPS week: 1495 Day: 6 MJD: 54715
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 8 --- --- --- 0 | --- 431 --- --- --- 429
R04 | 2269 19 17 71 41 --- 21 | 28 37 71 21 --- 27
R06 | 5062 61 43 58 31 --- 27 | 185 178 177 155 --- 171
R07 | 1353 53 37 35 20 --- 22 | 21 54 59 27 --- 31
XR09 |23397 --- --- 14 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2577 21 24 59 32 --- 19 | 33 33 65 38 --- 34
R11 | 7363 46 31 98 27 269 28 | 31 34 102 35 137 29
R13 | 1330 38 26 76 28 --- 23 | 46 28 96 39 --- 35
R14 | 2443 29 14 42 19 --- 14 | 23 27 42 41 --- 26
R15 | 1395 37 15 79 59 159 27 | 30 30 65 56 18 36
R17E | 6949 35 27 68 49 --- 24 | 42 33 65 54 --- 31
R19E | 1401 46 46 94 57 --- 33 | 110 76 92 97 --- 81
R20E | 826 31 27 71 34 --- 22 | 75 59 92 74 --- 66
R23E |14542 101 73 103 66 --- 48 | 9999 9999 9999 9999 --- 9999
R24E | 3253 45 19 36 55 325 23 | 70 70 80 109 335 79
------+------------------------------------+--------------------------------
RMS | 5379 48 34 72 43 260 |T 57 83 83 62 163 82
WRMS | 5379 37 22 60 43 260 |NE 52 102 82 53 18 98
MEDI | 2443 38 26 68 34 269 |MD 33 37 71 41 137 35
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