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[IGSREPORT-16529] Wk 1490 IGLOS Final Orbits
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IGS Electronic Report 14 Aug 06:45:33 PDT 2008 Message Number 16529
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1490 (Jul 27, 2008 - Aug 02, 2008)
Contact: J. Ray (jim.ray @ noaa.gov),
J. Griffiths (jake.griffiths @ 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 2.1490.
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:
igl1490[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1490 in the SP3 format.
igl14907.sum Combination Report for GPS Week 1490.
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 | 768.5 ns
1 | 692.6 ns
2 | 765.3 ns
3 | 761.8 ns
4 | 755.8 ns
5 | 747.3 ns
6 | 752.3 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
----+--------+---------------
0 | ESX | R13 R19
3 | ESX | R13 R19
4 | ESX | R13
5 | IAC | R11
6 | ESX | R11 R15 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 1.1490, 1a.1490).
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 2.1490.0-6)
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 3.1490.0-6).
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 1490 summary. (Jul 27, 2008 - Aug 02, 2008)
Table 1.1490.a GPS week : 1490 MJD: 54674.0-54680.0
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 62| 1 0 -10 -27 6 54 -.11 47 35 | 0 -53 2750 2737
| 3 3 3 32 52 113 .07 | 0 190
cod 216| -4 0 -3 -5 9 -9 -.12 35 29 | --- --- --- ---
| 4 1 3 36 45 82 .06 | --- ---
esx 117| 4 -2 7 40 -50 17 .39 81 50 | 24630 1317 6261 14981
| 3 4 6 123 67 116 .10 | 25415 4893
iac n/a| 4 3 11 -36 18 -40 -.03 52 52 | 960858 -134051 181833 295817
| 2 1 4 47 48 57 .06 | 381558 354402
mcc n/a| 3 11 80 -45 123 -1549 .38 321 321 | --- --- --- ---
| 28 54 29 619 425 1230 1.09 | --- ---
Table 1.1490.b GPS week : 1490 MJD: 54674.0-54680.0
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 | 21 20 16 12 17 19 23 |
R06 | 32 27 25 27 90 76 23 |
R07 | 22 26 31 27 40 31 21 |
R10 | 21 21 14 18 19 36 17 |
R11 | 17 15 21 15 56 25 21 |
R13 | 16 23 23 27 26 17 26 |
R14 | 12 11 14 18 18 20 17 |
R15 | 20 24 22 24 23 28 22 |
R17 | 26 24 20 16 61 88 27 |
R19 | 23 18 12 19 16 23 15 |
R20 | 28 16 18 15 15 15 20 |
R23 | 16 27 22 28 30 27 24 |
R24 | 18 18 18 17 15 18 20 |
Table 1.1490.c GPS week : 1490 MJD: 54674.0-54680.0
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 1490 0 | 334 52 411 3021 6194 -7563 94.6 5561 5561 | 768494 0
brd 1490 1 | 123 -186 586 348 2412 -25750 89.4 >>>>> >>>>> | 692636 0
brd 1490 2 | -218 -211 350 2556 -2028 -11180 98.3 3211 3211 | 765299 0
brd 1490 3 | -211 -294 385 -802 -2593 -19330 94.4 4620 4620 | 761778 0
brd 1490 4 | 333 -277 218 4011 1156 -14560 95.6 4310 4310 | 755787 0
brd 1490 5 | 98 122 433 -2808 3002 -21360 97.1 3754 3754 | 747345 0
brd 1490 6 | -108 162 594 -2009 -682 -26680 93.4 3488 3488 | 752304 0
-------------+------------------------------------------------------------+----------------
brd 1490 mean| 50 -90 425 616 1065 -18060 94.7 >>>>> >>>>> | 749091 0
brd 1490 sdev| 236 195 132 2638 3105 7253 2.9 >>>>> >>>>> | 25966 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 2.1490.0 GPS week: 1490 Day: 0 MJD: 54674
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 62| 0 0 -8 -47 -66 118 -.02 35 30 | 0 -212 2548 2631
cod 216| 1 -1 2 21 38 -57 -.03 35 28 | --- --- --- ---
esx 117| 0 -2 2 100 12 199 .44 83 52 | 37673 -413 5689 12262
iac n/a| 6 3 3 -2 -19 -136 -.02 27 27 | 770691 -4304 5396 10993
mcc n/a| -14 -24 47 -313 -151 -2387 1.14 282 282 | --- --- --- ---
Table 2.1490.1 GPS week: 1490 Day: 1 MJD: 54675
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 62| 7 -2 -10 0 -35 113 -.14 37 35 | 0 177 2027 2132
cod 216| -8 -1 -6 -21 -38 -12 -.13 27 23 | --- --- --- ---
esx 117| 3 1 2 104 -50 -27 .44 52 46 | -32389 2206 5964 15077
iac n/a| 5 4 14 -9 64 0 .04 31 31 | 692594 -504 5941 13600
mcc n/a| -19 1 59 -410 -571 607 .86 277 277 | --- --- --- ---
Table 2.1490.2 GPS week: 1490 Day: 2 MJD: 54676
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 62| 0 2 -17 20 41 115 -.15 31 27 | 0 -75 2525 2586
cod 216| 0 -3 -2 -5 -44 -86 -.14 29 26 | --- --- --- ---
esx 117| 8 -7 12 -227 44 74 .47 51 45 | 40340 -1901 5199 15046
iac n/a| 0 4 12 16 42 -93 -.06 25 25 | 1357238 -2446 241340 999999
mcc n/a| 31 100 52 1181 776 -631 2.12 322 322 | --- --- --- ---
Table 2.1490.3 GPS week: 1490 Day: 3 MJD: 54677
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 62| -1 -3 -10 -4 51 102 -.23 34 30 | 0 -284 3475 2771
cod 216| -9 0 -1 11 -27 -16 -.11 30 25 | --- --- --- ---
esx 117| 2 2 11 11 -76 -50 .48 72 29 | 33150 1087 6739 13148
iac n/a| 5 4 8 -27 47 25 -.04 29 29 | 1651261 -937736 999999 999999
mcc n/a| 3 -55 81 -262 169 -1542 .23 448 448 | --- --- --- ---
Table 2.1490.4 GPS week: 1490 Day: 4 MJD: 54678
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 62| 1 2 -5 -59 71 149 -.09 85 44 | 0 95 2794 2939
cod 216| -5 -1 -8 14 52 -9 -.19 43 34 | --- --- --- ---
esx 117| 4 -4 14 76 -161 -171 .38 91 61 | 29607 11808 7127 20038
iac n/a| 8 4 16 -63 68 3 -.01 81 81 | 753137 4758 7155 18840
mcc n/a| 29 10 123 405 393 -2041 -.50 186 186 | --- --- --- ---
Table 2.1490.5 GPS week: 1490 Day: 5 MJD: 54679
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 62| 1 2 -13 -42 17 -106 -.05 65 39 | 0 141 2650 2697
cod 216| -4 0 -1 20 20 -47 -.05 46 34 | --- --- --- ---
esx 117| 9 -9 10 103 -87 65 .22 76 60 | 32774 -1454 5794 16555
iac n/a| 4 1 12 -125 -24 -46 -.15 143 143 | 748996 652 5832 16181
mcc n/a| 31 -19 110 -445 241 -1681 -1.14 281 281 | --- --- --- ---
Table 2.1490.6 GPS week: 1490 Day: 6 MJD: 54680
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 62| 3 -4 -10 -61 -38 -114 -.06 41 37 | 0 -217 3234 3406
cod 216| -3 1 -3 -81 64 165 -.19 35 31 | --- --- --- ---
esx 117| 1 -1 -2 114 -36 35 .32 143 54 | 31260 -2110 7317 12747
iac n/a| 3 4 11 -41 -48 -35 .04 30 30 | 752089 1217 7172 11109
mcc n/a| -38 64 91 -475 6 -3170 -.04 454 454 | --- --- --- ---
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 3.1490.0 GPS week: 1490 Day: 0 MJD: 54674
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 4 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 4164 33 28 59 25 --- 20 | 36 37 73 28 --- 24
R06 | 6214 71 71 27 28 --- 31 | 142 167 163 157 --- 150
R07 | 3525 17 48 62 23 --- 22 | 53 67 44 46 --- 52
R10 | 1885 31 26 59 28 --- 20 | 30 19 44 28 --- 18
R11 | 5284 25 16 50 26 395 17 | 21 22 46 72 151 25
R13 | 1954 20 24 188 21 --- 15 | 30 41 149 50 --- 36
R14 | 2825 22 15 31 14 --- 11 | 26 27 37 27 --- 23
R15 | 3186 37 30 47 30 120 20 | 27 35 53 35 20 31
R17 |14239 36 42 64 43 --- 26 | 56 81 101 75 --- 62
R19 | 1328 34 29 149 32 --- 22 | 27 33 100 59 --- 37
R20 | 6699 36 27 95 30 --- 27 | 31 27 95 26 --- 26
R23 | 1384 23 22 36 28 --- 15 | 22 38 50 33 --- 26
R24 | 5370 33 38 32 17 259 17 | 99 73 92 90 180 86
------+------------------------------------+--------------------------------
RMS | 5560 35 35 83 27 282 |T 46 51 80 55 117 45
WRMS | 5560 30 28 52 27 282 |NE 46 51 80 55 117 45
MEDI | 3525 33 27 59 28 259 |MD 30 37 73 46 151 31
Table 3.1490.1 GPS week: 1490 Day: 1 MJD: 54675
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
R04 |>>>>> 43 15 55 28 --- 20 | 36 28 66 31 --- 32
R06 |>>>>> 57 41 53 39 --- 27 | 183 199 203 186 --- 188
XR07 |15117 42 35 --- 32 --- 25 | 79 70 --- 35 --- 56
R10 |>>>>> 44 16 53 33 --- 20 | 36 32 53 20 --- 19
R11 |>>>>> 25 26 37 15 380 14 | 30 28 68 43 139 25
R13 |>>>>> 21 22 77 33 --- 22 | 14 30 65 19 --- 22
R14 |>>>>> 22 15 23 16 --- 11 | 23 35 39 40 --- 31
R15 |>>>>> 29 26 82 23 218 23 | 35 29 110 46 23 43
R17 |>>>>> 29 31 60 47 --- 24 | 27 63 58 62 --- 47
R19 |>>>>> 22 35 26 32 --- 17 | 27 30 70 51 --- 29
R20 |>>>>> 34 17 28 31 --- 16 | 33 33 56 27 --- 25
R23 |>>>>> 60 39 54 30 --- 26 | 40 48 60 29 --- 21
R24 |>>>>> 31 25 36 35 197 18 | 65 84 102 84 172 76
------+------------------------------------+--------------------------------
RMS |>>>>> 37 27 52 31 277 |T 48 54 79 51 111 47
WRMS |>>>>> 35 23 46 31 277 |NE 48 54 79 51 111 47
MEDI |>>>>> 31 25 53 32 218 |MD 35 33 65 40 139 31
Table 3.1490.2 GPS week: 1490 Day: 2 MJD: 54676
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 6173 36 17 28 26 --- 16 | 32 25 41 29 --- 20
R06 | 1775 55 31 53 31 --- 24 | 140 165 189 151 --- 155
XR07 | 7536 40 54 --- 36 --- 31 | 56 80 --- 32 --- 44
R10 | 1618 17 14 41 24 --- 13 | 31 30 43 33 --- 29
XR11 | 2887 35 34 --- 17 471 21 | 20 57 --- 54 196 31
R13 | 2259 37 33 73 21 --- 22 | 29 43 95 33 --- 29
R14 | 2805 18 14 42 25 --- 14 | 26 35 50 31 --- 26
R15 | 2129 21 32 72 28 213 21 | 27 51 76 36 38 32
R17 | 3030 27 35 65 15 --- 20 | 26 28 81 67 --- 36
R19 | 1012 22 18 24 20 --- 12 | 27 43 43 32 --- 31
R20 | 2369 26 20 60 23 --- 18 | 21 27 50 24 --- 16
R23 | 3565 30 48 45 28 --- 22 | 17 52 59 30 --- 24
R24 | 4847 35 33 23 27 403 17 | 109 103 113 110 406 104
------+------------------------------------+--------------------------------
RMS | 3211 31 29 51 25 322 |T 43 56 76 50 213 44
WRMS | 3211 27 26 45 25 322 |NE 43 56 76 50 213 44
MEDI | 2805 30 31 45 25 403 |MD 27 43 59 33 196 31
Table 3.1490.3 GPS week: 1490 Day: 3 MJD: 54677
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 4555 20 16 26 22 --- 12 | 31 38 31 25 --- 25
R06 | 3158 57 51 43 33 --- 27 | 204 167 188 175 --- 176
XR07 | 6249 22 39 --- 47 --- 27 | 52 90 --- 50 --- 61
R10 | 1992 23 21 58 22 --- 18 | 32 30 53 25 --- 21
R11 | 4092 29 24 26 21 603 14 | 48 45 59 51 350 40
R13 |12820 45 36 142 32 --- 27 | 40 50 115 62 --- 47
R14 | 3432 28 13 56 25 --- 18 | 31 41 82 43 --- 39
R15 | 1520 26 13 65 49 57 23 | 51 51 85 54 57 50
R17 | 1790 23 28 41 21 --- 16 | 28 41 58 78 --- 40
R19 | 1487 34 22 142 20 --- 18 | 28 32 131 34 --- 28
R20 | 1971 25 29 30 18 --- 14 | 27 41 28 26 --- 20
R23 | 3561 47 46 63 39 --- 27 | 24 26 78 46 --- 22
R24 | 2075 29 29 29 29 486 16 | 51 60 54 71 348 54
------+------------------------------------+--------------------------------
RMS | 4620 34 30 72 29 448 |T 49 54 80 56 251 47
WRMS | 4620 30 25 29 29 448 |NE 49 54 80 56 251 47
MEDI | 3158 28 24 43 25 486 |MD 32 41 59 50 348 40
Table 3.1490.4 GPS week: 1490 Day: 4 MJD: 54678
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
R04 | 3816 32 23 26 39 --- 17 | 30 33 37 40 --- 25
R06 | 2099 270 80 136 82 --- 89 | 217 392 427 371 --- 338
R07 | 3679 63 74 62 73 --- 39 | 36 124 79 53 --- 72
R10 | 3485 22 28 52 23 --- 19 | 29 21 122 41 --- 41
R11 | 7842 47 56 65 184 --- 55 | 34 30 60 227 --- 55
R13 | 8870 42 36 226 31 --- 26 | 20 31 196 35 --- 23
R14 | 3874 39 15 36 32 --- 17 | 31 23 47 30 --- 16
R15 | 2024 18 17 61 54 109 23 | 25 30 72 28 26 24
R17 | 3223 69 54 129 165 --- 61 | 32 41 140 222 --- 74
R19 | 1604 31 11 43 16 --- 15 | 22 21 87 26 --- 24
R20 | 2337 25 23 23 30 --- 14 | 42 54 36 25 --- 37
R23 | 2279 57 48 47 54 --- 29 | 20 51 69 57 --- 32
R24 | 3723 19 21 32 28 239 14 | 77 67 76 75 193 69
------+------------------------------------+--------------------------------
RMS | 4309 85 43 91 81 186 |T 47 70 111 94 109 63
WRMS | 4309 44 34 61 81 186 |NE 47 70 111 94 109 63
MEDI | 3485 39 23 52 39 109 |MD 31 33 76 41 26 37
Table 3.1490.5 GPS week: 1490 Day: 5 MJD: 54679
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 4 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 1846 22 26 48 32 --- 18 | 41 46 50 49 --- 38
R06 | 3965 191 100 120 88 --- 75 | 187 360 396 332 --- 302
R07 | 4162 33 53 75 47 --- 30 | 38 64 60 36 --- 28
R10 | 6404 50 34 116 27 --- 35 | 28 42 108 49 --- 40
R11 | 2158 36 17 53 411 --- 25 | 21 18 58 355 --- 17
R13 | 3971 23 26 39 32 --- 17 | 30 37 37 43 --- 34
R14 | 4302 36 18 41 44 --- 20 | 22 28 62 51 --- 30
R15 | 5913 31 42 48 69 163 28 | 39 23 80 69 25 36
R17 | 3000 64 77 160 264 --- 88 | 76 99 87 262 --- 97
R19 | 2263 48 22 36 48 --- 22 | 27 47 78 85 --- 45
R20 | 2610 28 17 27 31 --- 14 | 32 26 39 35 --- 23
R23 | 1440 28 50 50 55 --- 27 | 20 57 70 44 --- 30
R24 | 2969 45 29 22 17 362 18 | 72 92 95 73 73 79
------+------------------------------------+--------------------------------
RMS | 3754 65 46 76 142 281 |T 48 72 93 114 49 61
WRMS | 3754 39 34 60 142 281 |NE 48 72 93 114 49 61
MEDI | 3000 36 26 48 47 163 |MD 32 46 70 51 25 36
Table 3.1490.6 GPS week: 1490 Day: 6 MJD: 54680
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 12 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 1719 36 45 44 34 --- 23 | 46 24 49 31 --- 27
R06 | 3288 64 38 32 24 --- 23 | 321 410 434 410 --- 391
R07 | 4856 41 42 33 28 --- 21 | 28 51 29 33 --- 24
R10 | 6835 21 26 33 32 --- 16 | 20 32 34 22 --- 20
R11 | 1381 37 27 283 26 620 21 | 42 43 151 85 329 42
R13 | 4042 41 36 67 33 --- 26 | 27 40 64 42 --- 28
R14 | 3171 40 22 25 27 --- 16 | 24 43 47 34 --- 31
R15 | 2430 35 33 152 26 248 22 | 32 42 105 31 22 29
R17 | 2302 42 46 56 43 --- 27 | 178 190 217 175 --- 180
R19 | 2846 20 26 384 17 --- 15 | 54 58 290 67 --- 59
R20 | 2954 37 31 40 29 --- 19 | 48 42 46 20 --- 26
R23 | 2103 45 46 32 38 --- 23 | 24 68 55 56 --- 39
R24 | 3648 55 29 35 15 416 20 | 86 93 108 87 162 88
------+------------------------------------+--------------------------------
RMS | 3488 41 35 143 30 454 |T 71 87 125 84 171 75
WRMS | 3488 37 31 54 30 454 |NE 71 87 125 84 171 75
MEDI | 2954 40 31 40 28 416 |MD 42 43 64 42 162 31