[IGSREPORT-16190] Wk 1475 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu May 1 06:36:45 PDT 2008
******************************************************************************
IGS Electronic Report 01 May 06:36:48 PDT 2008 Message Number 16190
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1475 (Apr 13, 2008 - Apr 19, 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 2.1475.
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:
igl1475[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1475 in the SP3 format.
igl14757.sum Combination Report for GPS Week 1475.
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 | 1058.1 ns
1 | 1057.3 ns
2 | 1050.6 ns
3 | 1038.3 ns
4 | 1074.5 ns
5 | 1045.9 ns
6 | 1017.1 ns
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 1.1475, 1a.1475).
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 2.1475.0-6)
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 3.1475.0-6).
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 1475 summary. (Apr 13, 2008 - Apr 19, 2008)
Table 1.1475.a GPS week : 1475 MJD: 54569.0-54575.0
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| 2 0 -8 270 219 58 -.11 34 31 | 0 244 3262 3414
| 2 1 4 264 232 137 .06 | 0 209
cod 178| -3 0 0 -88 -71 -12 -.10 27 25 | --- --- --- ---
| 2 1 6 78 97 39 .04 | --- ---
esx 116| -4 0 1 -110 -102 -105 .47 69 53 | -26316 791 12358 36885
| 3 4 11 93 69 143 .13 | 20161 7368
iac n/a| 3 1 8 -94 -77 11 .02 41 41 | 1046827 -4193 11899 33474
| 1 1 9 99 66 54 .04 | 22001 4780
mcc n/a| 13 4 23 -16 -133 -690 .60 318 318 | --- --- --- ---
| 23 12 15 173 208 497 .67 | --- ---
Table 1.1475.b GPS week : 1475 MJD: 54569.0-54575.0
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 | 20 22 17 48 16 18 40 |
R04 | 17 21 17 22 14 14 20 |
R06 | 16 15 13 15 18 17 20 |
R07 | 16 16 22 26 25 39 24 |
R08 | 22 23 20 30 28 36 28 |
R09 | 36 29 28 22 18 19 17 |
R10 | 16 42 19 17 17 13 17 |
R11 | 24 29 45 21 22 37 26 |
R13 | 24 28 30 32 19 23 21 |
R14 | 13 17 18 14 13 14 12 |
R15 | 24 31 35 17 23 17 20 |
R17 | 27 23 20 22 17 18 17 |
R19 | 22 25 35 16 26 18 15 |
R20 | 14 15 21 24 17 18 18 |
R23 | 20 24 27 45 31 27 27 |
R24 | 17 23 27 26 18 14 17 |
Table 1.1475.c GPS week : 1475 MJD: 54569.0-54575.0
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 1475 0 | -247 159 682 1062 -96 -21110 103.6 10390 10390 | 1058070 0
brd 1475 1 | 250 653 1450 -8212 7566 -40370 <<<< >>>>> >>>>> | 1057311 0
brd 1475 2 | 53 -58 175 2119 1667 -28320 92.8 5296 5296 | 1050563 0
brd 1475 3 | -78 179 236 -1187 562 -30830 95.6 6870 6870 | 1038332 0
brd 1475 4 | 111 152 287 -5021 117 -31310 96.4 5268 5268 | 1074523 0
brd 1475 5 | 79 -159 140 -3290 -5999 -38610 90.7 5212 5212 | 1045857 0
brd 1475 6 | -47 88 56 -4686 -386 -38890 87.1 5913 5913 | 1017130 0
-------------+------------------------------------------------------------+----------------
brd 1475 mean| 17 144 432 -2745 490 -32777 5.2 >>>>> >>>>> | 1048826 0
brd 1475 sdev| 159 257 491 3644 3975 6963 236.1 >>>>> >>>>> | 18001 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 2.1475.0 GPS week: 1475 Day: 0 MJD: 54569
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| 3 0 -4 18 14 -168 -.21 35 32 | 0 250 2827 2953
cod 178| -3 2 -11 -7 1 28 -.10 22 18 | --- --- --- ---
esx 116| -6 4 12 32 13 -48 .46 61 45 | -22482 -4023 17186 45867
iac n/a| 3 -1 17 -12 -42 117 .03 39 39 | 1064741 -4984 12978 44445
mcc n/a| -5 -7 35 244 20 -873 .67 155 155 | --- --- --- ---
Table 2.1475.1 GPS week: 1475 Day: 1 MJD: 54570
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| 4 -2 -5 198 154 223 -.15 35 33 | 0 552 4059 4234
cod 178| -8 0 -5 -137 -49 0 -.18 32 30 | --- --- --- ---
esx 116| -7 -1 -1 -23 -89 -353 .48 54 45 | -25125 -1231 18329 29535
iac n/a| 3 2 13 -58 -100 -13 .06 43 43 | 1058886 -4249 18450 26426
mcc n/a| 40 0 28 -20 66 -1224 .92 214 214 | --- --- --- ---
Table 2.1475.2 GPS week: 1475 Day: 2 MJD: 54571
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| 4 1 -8 393 369 -14 -.14 36 34 | 0 -48 4198 4389
cod 178| -7 0 1 -107 -226 -6 -.04 35 31 | --- --- --- ---
esx 116| 1 -7 -5 -106 -149 86 .43 76 56 | -39044 -12948 15098 64976
iac n/a| 5 1 12 -222 -128 -56 -.02 41 41 | 1039184 -13586 16005 64667
mcc n/a| 38 15 -8 -122 -549 -481 1.40 316 316 | --- --- --- ---
Table 2.1475.3 GPS week: 1475 Day: 3 MJD: 54572
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 -9 654 538 75 -.05 43 35 | 0 41 3459 3571
cod 178| -1 0 3 -207 -167 -13 -.08 27 23 | --- --- --- ---
esx 116| -8 3 -4 -164 -213 -137 .35 70 54 | -52143 6661 9096 35555
iac n/a| 3 1 5 -209 -184 -2 -.01 55 55 | 1027420 14 9017 32012
mcc n/a| 19 13 33 -269 -162 -1284 -.20 515 515 | --- --- --- ---
Table 2.1475.4 GPS week: 1475 Day: 4 MJD: 54573
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| 7 -2 -9 551 457 190 -.07 36 32 | 0 263 2695 2819
cod 178| -2 0 9 -134 -96 -69 -.08 20 19 | --- --- --- ---
esx 116| -6 0 4 -253 -119 -44 .67 63 53 | 12673 4273 9380 26897
iac n/a| 4 2 -12 -157 -80 -11 .01 38 38 | 1080580 -5504 9542 23978
mcc n/a| -18 23 29 82 10 -33 .90 344 344 | --- --- --- ---
Table 2.1475.5 GPS week: 1475 Day: 5 MJD: 54574
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 -17 75 22 -27 -.06 25 24 | 0 210 2836 2991
cod 178| -3 -2 4 -14 1 31 -.10 30 27 | --- --- --- ---
esx 116| -4 5 19 -121 -80 -33 .30 86 64 | -23628 6105 7602 33252
iac n/a| 3 2 7 -1 -7 20 .10 35 35 | 1038268 -1495 7821 27220
mcc n/a| -5 -8 25 -135 -151 -123 .94 258 258 | --- --- --- ---
Table 2.1475.6 GPS week: 1475 Day: 6 MJD: 54575
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 0 -6 4 -21 130 -.13 29 29 | 0 445 2762 2945
cod 178| -1 0 1 -10 35 -58 -.13 26 23 | --- --- --- ---
esx 116| -1 -4 -15 -133 -80 -211 .57 76 56 | -34463 6700 9821 22114
iac n/a| 0 1 14 -1 0 29 .01 37 37 | 1018710 453 9483 15570
mcc n/a| 26 0 19 102 -165 -811 -.43 426 426 | --- --- --- ---
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 3.1475.0 GPS week: 1475 Day: 0 MJD: 54569
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5633 38 18 48 44 --- 20 | 34 48 50 55 --- 40
R04 | 3664 34 9 58 22 --- 17 | 46 46 56 31 --- 41
R06 | 2964 17 8 51 36 --- 15 | 37 53 33 73 --- 48
R07 |31666 26 18 51 21 128 16 | 29 25 71 41 42 28
R08 | 4070 41 20 73 19 --- 21 | 41 38 67 53 --- 40
R09 |14776 32 35 140 41 --- 36 | 32 33 142 47 --- 31
R10 | 1743 30 19 34 30 --- 15 | 63 75 95 80 --- 75
R11 | 6460 60 24 58 31 --- 24 | 48 45 101 56 --- 52
R13 | 8693 30 29 72 42 --- 23 | 34 54 82 45 --- 39
R14 | 3088 23 18 28 26 --- 13 | 27 36 39 20 --- 25
R15 |11020 42 19 62 53 127 24 | 40 44 58 57 78 39
R17 |10693 27 37 53 71 --- 27 | 52 55 79 83 --- 57
R19 | 2906 46 13 50 46 --- 21 | 40 46 55 53 --- 40
R20 | 1854 22 16 39 26 --- 14 | 34 38 50 32 --- 34
R23 | 1122 33 23 46 42 --- 19 | 403 426 421 429 --- 420
R24 | 7542 35 21 25 34 199 16 | 159 158 161 152 216 155
------+------------------------------------+--------------------------------
RMS |10390 35 22 61 39 155 |T 69 76 97 81 112 72
WRMS |10390 32 18 45 39 155 |NE 69 76 97 81 112 72
MEDI | 4070 32 19 51 34 128 |MD 40 46 67 53 78 40
Table 3.1475.1 GPS week: 1475 Day: 1 MJD: 54570
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 20 37 55 42 --- 22 | 29 43 51 40 --- 26
R04 |>>>>> 21 36 58 30 --- 20 | 32 43 73 28 --- 26
R06 |>>>>> 26 20 40 23 --- 15 | 33 49 47 39 --- 32
R07 |19381 21 13 51 23 158 15 | 36 28 53 39 21 23
R08 |>>>>> 45 19 70 18 --- 22 | 38 28 77 43 --- 25
R09 |>>>>> 45 35 44 71 --- 29 | 36 33 54 83 --- 33
XR10 |>>>>> --- 38 107 32 --- 42 | --- 56 85 39 --- 39
R11 |>>>>> 48 18 92 37 --- 28 | 34 38 161 55 --- 48
R13 |>>>>> 20 61 59 45 --- 28 | 45 83 52 31 --- 43
R14 |>>>>> 23 32 29 31 --- 17 | 30 41 32 29 --- 22
R15 |>>>>> 46 37 40 80 99 31 | 29 45 77 91 31 41
R17 |>>>>> 36 20 43 56 --- 23 | 65 35 74 57 --- 45
R19 |>>>>> 33 40 77 22 --- 25 | 58 64 92 28 --- 30
R20 |>>>>> 23 21 37 24 --- 15 | 39 33 33 27 --- 24
R23 |>>>>> 43 19 44 56 --- 24 | 358 330 339 344 --- 341
R24 |>>>>> 51 38 27 30 321 22 | 108 166 147 125 107 134
------+------------------------------------+--------------------------------
RMS |>>>>> 35 32 54 43 214 |T 64 69 90 68 53 58
WRMS |>>>>> 33 30 45 43 214 |NE 64 69 90 68 53 58
MEDI |>>>>> 33 32 44 31 158 |MD 36 43 73 39 31 32
Table 3.1475.2 GPS week: 1475 Day: 2 MJD: 54571
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7137 31 26 33 26 --- 16 | 69 41 74 56 --- 49
R04 | 4928 32 24 45 18 --- 16 | 61 40 54 33 --- 36
R06 | 3306 17 14 35 24 --- 12 | 51 34 61 24 --- 26
R07 | 5016 29 18 71 37 173 22 | 53 27 93 46 37 29
R08 | 6224 19 30 32 49 --- 19 | 66 18 51 65 --- 37
R09 | 8428 28 25 79 63 --- 28 | 62 31 82 54 --- 30
R10 | 1935 31 18 49 35 --- 18 | 68 49 67 63 --- 49
R11 | 4149 41 46 173 52 --- 45 | 56 68 177 56 --- 48
R13 | 6715 36 47 96 35 --- 30 | 58 43 104 57 --- 46
R14 | 3355 20 33 43 33 --- 18 | 52 32 56 35 --- 26
R15 | 3819 65 55 70 54 109 34 | 66 64 114 76 43 57
R17 | 9615 32 16 59 37 --- 20 | 73 71 59 94 --- 69
R19 | 3191 19 47 137 28 --- 34 | 53 54 111 42 --- 25
R20 | 4267 41 30 35 38 --- 21 | 81 43 59 35 --- 44
R23 | 2618 38 49 39 55 --- 27 | 345 386 379 374 --- 368
R24 | 2816 57 42 39 39 507 26 | 226 291 287 276 219 266
------+------------------------------------+--------------------------------
RMS | 5295 36 35 76 41 316 |T 90 80 114 86 99 75
WRMS | 5295 34 31 56 41 316 |NE 90 80 114 86 99 75
MEDI | 4149 31 30 45 37 173 |MD 62 43 74 56 43 44
Table 3.1475.3 GPS week: 1475 Day: 3 MJD: 54572
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |11835 56 43 170 71 --- 48 | 89 74 170 56 --- 53
R04 | 1453 37 13 68 37 --- 21 | 75 59 104 48 --- 53
R06 | 2217 17 11 48 29 --- 14 | 71 39 58 43 --- 39
R07 | 1365 43 28 30 78 207 26 | 70 34 52 67 38 30
R08 | 8005 32 34 50 90 --- 30 | 81 35 59 100 --- 38
R09 |11728 18 28 71 31 --- 21 | 64 33 71 27 --- 28
R10 | 2834 41 17 31 24 --- 16 | 73 33 50 38 --- 35
R11 | 4031 44 28 44 35 --- 21 | 83 50 76 51 --- 49
R13 | 9680 23 36 81 82 --- 31 | 65 50 87 78 --- 36
R14 | 2906 19 19 29 30 --- 13 | 65 37 35 19 --- 29
R15 | 4188 33 17 49 25 68 17 | 85 53 76 54 74 55
R17 | 5221 39 18 48 56 --- 22 | 81 74 79 113 --- 74
R19 | 2533 27 16 35 37 --- 15 | 71 41 89 36 --- 36
R20 | 3975 41 35 48 47 --- 24 | 74 52 58 45 --- 45
R23 |14432 90 34 114 91 --- 45 | 182 241 253 247 --- 218
R24 | 1645 65 21 62 36 864 26 | 121 126 153 123 478 121
------+------------------------------------+--------------------------------
RMS | 6869 43 27 70 55 515 |T 84 64 91 71 196 58
WRMS | 6869 35 23 54 55 515 |NE 84 64 91 71 196 58
MEDI | 3975 37 21 48 37 207 |MD 74 50 76 51 74 39
Table 3.1475.4 GPS week: 1475 Day: 4 MJD: 54573
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6598 21 20 49 27 --- 15 | 58 42 86 45 --- 40
R04 | 1072 28 12 40 24 --- 13 | 60 28 59 51 --- 32
R06 | 2919 18 25 50 37 --- 18 | 49 35 59 39 --- 27
R07 | 4158 47 17 64 55 111 24 | 74 39 78 38 113 38
R08 | 6604 22 13 102 62 --- 28 | 62 53 123 60 --- 41
R09 | 9532 32 17 60 30 --- 18 | 57 35 79 42 --- 27
R10 | 4549 35 16 43 36 --- 17 | 52 31 50 54 --- 34
R11 | 9803 28 16 87 34 --- 22 | 64 37 74 40 --- 31
R13 | 6013 25 13 69 35 --- 19 | 71 41 52 71 --- 42
R14 | 2352 25 10 38 21 --- 12 | 46 40 56 31 --- 30
R15 | 5744 68 29 36 22 179 23 | 74 57 52 29 72 42
R17 | 4961 42 15 22 39 --- 17 | 69 75 74 95 --- 74
R19 | 2582 41 20 104 23 --- 25 | 55 28 114 38 --- 36
R20 | 2981 34 23 44 24 --- 17 | 61 53 67 55 --- 49
R23 | 2048 45 37 88 58 --- 30 | 371 393 461 389 --- 392
R24 | 1791 35 25 27 40 557 18 | 214 232 214 210 293 218
------+------------------------------------+--------------------------------
RMS | 5268 36 20 63 38 344 |T 89 76 106 80 159 72
WRMS | 5268 32 19 53 38 344 |NE 89 76 106 80 159 72
MEDI | 4158 32 17 49 34 179 |MD 61 40 74 45 113 38
Table 3.1475.5 GPS week: 1475 Day: 5 MJD: 54574
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3765 25 30 59 22 --- 18 | 25 34 83 37 --- 23
R04 | 3075 25 14 33 26 --- 13 | 36 33 43 34 --- 29
R06 | 3481 22 27 50 29 --- 17 | 33 33 36 52 --- 27
R07 | 5092 28 28 172 65 127 39 | 26 36 169 57 60 30
R08 | 5481 36 28 155 51 --- 35 | 44 45 176 66 --- 48
R09 | 7007 24 26 73 21 --- 18 | 23 38 63 20 --- 20
R10 | 6554 17 21 45 19 --- 13 | 26 33 59 40 --- 31
R11 | 7168 33 49 155 42 --- 36 | 47 45 111 49 --- 38
R13 | 5779 18 24 97 37 --- 23 | 45 41 94 68 --- 42
R14 | 1817 23 26 35 16 --- 14 | 33 49 52 32 --- 34
R15 | 6962 23 27 52 25 120 16 | 39 36 59 31 34 28
R17 | 6819 25 30 34 33 --- 17 | 36 57 40 62 --- 44
R19 | 3630 23 28 62 27 --- 18 | 26 41 70 27 --- 23
R20 | 2416 18 15 58 40 --- 17 | 27 23 51 26 --- 19
R23 | 5649 32 56 54 45 --- 26 | 260 238 240 247 --- 246
R24 | 4093 21 12 32 30 412 13 | 92 118 125 123 249 111
------+------------------------------------+--------------------------------
RMS | 5211 25 30 86 35 258 |T 51 56 91 60 114 49
WRMS | 5211 24 27 64 35 258 |NE 51 56 91 60 114 49
MEDI | 5092 23 27 54 29 127 |MD 33 38 63 40 60 30
Table 3.1475.6 GPS week: 1475 Day: 6 MJD: 54575
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2062 52 12 184 35 --- 40 | 35 43 79 62 --- 43
R04 | 1464 18 29 54 41 --- 19 | 36 46 58 47 --- 36
R06 | 3238 32 23 49 43 --- 20 | 41 35 39 44 --- 32
R07 | 5178 38 26 55 52 164 23 | 40 45 100 79 90 51
R08 | 7283 17 35 93 62 --- 28 | 59 67 93 98 --- 64
R09 |10732 15 20 65 25 --- 16 | 21 38 55 28 --- 27
R10 | 2735 37 22 35 26 --- 17 | 27 34 69 45 --- 35
R11 | 6078 27 27 109 34 --- 26 | 58 45 153 56 --- 56
R13 | 9981 32 25 57 39 --- 20 | 39 38 70 35 --- 29
R14 | 2130 15 16 28 29 --- 12 | 21 42 34 40 --- 30
R15 | 6040 18 22 77 30 75 19 | 30 37 77 45 35 33
R17 | 7674 21 19 60 25 --- 16 | 48 64 85 73 --- 58
R19 | 4085 23 25 40 21 --- 15 | 27 43 48 33 --- 26
R20 | 3401 20 25 58 31 --- 17 | 30 18 66 22 --- 20
R23 | 7940 44 47 63 40 --- 27 | 333 321 335 330 --- 328
R24 | 3492 22 19 56 31 715 16 | 147 170 171 153 210 157
------+------------------------------------+--------------------------------
RMS | 5913 29 26 76 37 426 |T 62 67 95 74 111 64
WRMS | 5913 29 23 56 37 426 |NE 62 67 95 74 111 64
MEDI | 4085 22 23 57 31 164 |MD 36 43 70 45 90 35
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