[IGSREPORT-16239] Wk 1477 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Fri May 16 05:03:35 PDT 2008
******************************************************************************
IGS Electronic Report 16 May 05:03:42 PDT 2008 Message Number 16239
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1477 (Apr 27, 2008 - May 03, 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 2.1477.
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:
igl1477[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1477 in the SP3 format.
igl14777.sum Combination Report for GPS Week 1477.
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 | 1030.3 ns
1 | 965.5 ns
2 | 1039.8 ns
3 | 1012.6 ns
4 | 1015.2 ns
5 | 1003.4 ns
6 | 1012.9 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 | R01
2 | ESX | R06 R13 R19
3 | ESX | R08 R09 R19
4 | BKG | R13
4 | ESX | R08
5 | BKG | R13
6 | ESX | R08
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 1.1477, 1a.1477).
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 2.1477.0-6)
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 3.1477.0-6).
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 1477 summary. (Apr 27, 2008 - May 03, 2008)
Table 1.1477.a GPS week : 1477 MJD: 54583.0-54589.0
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 68| 0 0 -7 35 -2 41 -.15 57 33 | 0 187 3503 3644
| 1 3 9 52 66 108 .06 | 0 137
cod 196| -1 0 -5 -5 -13 -8 -.13 34 24 | --- --- --- ---
| 2 2 3 30 43 45 .06 | --- ---
esx 118| -1 0 2 -13 -57 -64 .40 1528 54 | -4538 6767 13234 31766
| 2 3 7 53 27 51 .12 | 24730 13167
iac n/a| 2 -1 11 5 26 21 -.01 38 38 | 1009969 3134 14051 29662
| 3 1 4 27 42 60 .05 | 21835 8479
mcc n/a| 5 -7 35 67 -87 -1534 .44 268 268 | --- --- --- ---
| 14 8 14 215 198 1587 .21 | --- ---
Table 1.1477.b GPS week : 1477 MJD: 54583.0-54589.0
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 | 19 18 14 15 19 16 11 |
R04 | 15 13 25 14 13 19 14 |
R06 | 26 21 33 23 29 21 25 |
R07 | 19 24 23 25 20 30 21 |
R08 | 29 20 23 32 28 22 20 |
R09 | 81 63 27 15 11 22 22 |
R10 | 16 16 15 14 15 20 23 |
R11 | 50 47 27 26 17 25 20 |
R13 | 114 71 18 23 30 23 23 |
R14 | 13 10 13 15 13 18 15 |
R15 | 21 16 20 25 19 16 23 |
R17 | 21 33 21 26 16 18 19 |
R19 | 17 19 22 22 13 17 25 |
R20 | 18 15 16 15 17 16 17 |
R23 | 22 26 23 21 21 19 23 |
R24 | 26 18 19 13 19 19 25 |
Table 1.1477.c GPS week : 1477 MJD: 54583.0-54589.0
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 1477 0 | -11 -191 502 226 -4181 -7683 99.1 6565 6565 | 1030266 0
brd 1477 1 | -814 -370 131 1260 -15590 -5579 213.2 >>>>> >>>>> | 965456 0
brd 1477 2 | -224 185 485 1916 -6338 -3568 96.1 8572 8572 | 1039845 0
brd 1477 3 | 107 -375 612 5781 5888 10500 101.6 8610 8610 | 1012573 0
brd 1477 4 | -17 202 230 -2896 1351 -2661 95.5 5965 5965 | 1015157 0
brd 1477 5 | -147 527 984 -9826 2404 -25200 92.6 6883 6883 | 1003392 0
brd 1477 6 | -341 201 175 -5881 175 -24550 98.8 6229 6229 | 1012872 0
-------------+------------------------------------------------------------+----------------
brd 1477 mean| -207 25 446 -1345 -2327 -8391 113.8 >>>>> >>>>> | 1011365 0
brd 1477 sdev| 306 342 300 5253 7130 12682 43.9 >>>>> >>>>> | 23656 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 2.1477.0 GPS week: 1477 Day: 0 MJD: 54583
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 68| 4 0 -17 86 104 21 -.16 105 42 | 0 99 3259 3374
cod 196| -5 -2 -11 13 -71 55 -.06 59 24 | --- --- --- ---
esx 118| 1 2 17 -95 -113 -20 .34 75 46 | 13832 13409 16807 24989
iac n/a| 6 0 10 -27 86 -73 -.03 65 65 | 1027817 7858 17228 20333
mcc n/a| 7 -5 34 378 146 -253 .58 214 214 | --- --- --- ---
Table 2.1477.1 GPS week: 1477 Day: 1 MJD: 54584
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 68| 0 -4 -14 122 -103 106 -.10 87 31 | 0 149 4142 4293
cod 196| -3 3 -9 10 61 -83 -.23 44 26 | --- --- --- ---
esx 118| -3 -5 3 39 -58 -30 .19 83 54 | -41964 -2469 9627 28778
iac n/a| 3 -2 10 -32 -8 31 .04 36 36 | 969039 2101 10624 26932
mcc n/a| 1 -21 10 -101 -84 -1311 .49 261 261 | --- --- --- ---
Table 2.1477.2 GPS week: 1477 Day: 2 MJD: 54585
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 68| 0 -4 -9 -19 52 12 -.14 36 31 | 0 464 3794 3906
cod 196| 0 0 -4 -37 -34 -10 -.12 29 24 | --- --- --- ---
esx 118| -1 0 -2 51 -47 -25 .48 9807 84 | 9863 -12311 6680 19353
iac n/a| 2 -1 17 7 60 10 -.09 36 36 | 1035779 -4054 7783 15951
mcc n/a| -8 -16 26 -14 -181 -1773 .46 152 152 | --- --- --- ---
Table 2.1477.3 GPS week: 1477 Day: 3 MJD: 54586
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 68| 0 1 -15 40 -22 205 -.23 42 33 | 0 37 3967 4259
cod 196| -1 -2 -2 -53 -48 5 -.07 24 23 | --- --- --- ---
esx 118| -2 4 -1 -42 -43 -146 .55 551 60 | -37597 18165 9193 33113
iac n/a| 0 0 17 31 62 -38 -.02 35 35 | 997191 8959 9879 29716
mcc n/a| 9 -4 45 188 -344 -2807 .24 180 180 | --- --- --- ---
Table 2.1477.4 GPS week: 1477 Day: 4 MJD: 54587
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 68| 0 -1 4 25 -34 -94 -.12 50 32 | 0 130 2436 2540
cod 196| 1 4 -4 18 0 -5 -.16 21 19 | --- --- --- ---
esx 118| -3 -4 -2 -43 -67 -35 .44 67 37 | -822 25893 20474 50958
iac n/a| 1 -2 14 -1 10 84 -.04 31 31 | 1012490 16954 22591 53847
mcc n/a| 10 -1 48 219 190 -3271 .51 251 251 | --- --- --- ---
Table 2.1477.5 GPS week: 1477 Day: 5 MJD: 54588
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 68| 1 4 5 -8 -8 -80 -.23 46 33 | 0 213 3993 4089
cod 196| -3 -1 -4 -15 -3 26 -.15 30 27 | --- --- --- ---
esx 118| -5 0 -5 -29 -30 -69 .36 51 47 | 8016 4801 12417 32743
iac n/a| -1 -1 4 27 -17 87 .07 29 29 | 1012557 -5691 12740 32052
mcc n/a| 30 -7 53 66 -261 -2566 .70 478 478 | --- --- --- ---
Table 2.1477.6 GPS week: 1477 Day: 6 MJD: 54589
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 68| -1 4 -8 0 -2 116 -.10 33 26 | 0 222 2930 3049
cod 196| 0 -2 -2 24 4 -46 -.15 29 27 | --- --- --- ---
esx 118| 2 0 7 21 -43 -124 .45 61 51 | 16901 -116 17445 32434
iac n/a| 7 0 7 35 -10 49 -.01 34 34 | 1014915 -4186 17516 28809
mcc n/a| -13 2 31 -261 -80 1237 .09 343 343 | --- --- --- ---
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 3.1477.0 GPS week: 1477 Day: 0 MJD: 54583
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6065 43 23 44 28 --- 18 | 25 30 75 30 --- 26
R04 | 2467 28 20 29 26 --- 14 | 38 38 47 51 --- 41
R06 | 9630 83 23 56 25 --- 25 | 145 137 9999 137 --- 133
R07 | 3434 47 25 30 33 206 18 | 30 48 52 52 67 40
R08 |10674 56 25 93 32 --- 29 | 42 35 79 36 --- 26
R09 |14781 241 109 158 96 --- 81 | 536 810 852 717 --- 746
R10 | 1788 35 18 41 24 --- 16 | 45 48 49 50 --- 43
R11 | 4431 131 45 133 60 --- 50 | 261 397 490 347 --- 374
R13 | 8674 271 184 133 204 --- 114 | 947 9999 9999 9999 --- 9999
R14 | 2527 16 19 32 18 --- 12 | 24 25 39 28 --- 24
R15 | 5148 38 26 51 36 152 21 | 106 119 136 114 39 115
R17 | 6306 44 25 42 37 --- 20 | 40 54 90 62 --- 52
R19 | 1604 43 26 27 27 --- 17 | 39 61 153 58 --- 51
R20 | 3050 37 21 46 26 --- 18 | 46 44 78 45 --- 44
R23 | 4331 40 33 38 42 --- 22 | 38 56 86 66 --- 55
R24 | 2894 65 34 52 41 267 26 | 221 272 278 240 242 254
------+------------------------------------+--------------------------------
RMS | 6565 105 59 75 65 214 |T 161 144 178 135 116 134
WRMS | 6565 42 24 46 65 214 |NE 161 144 178 135 116 134
MEDI | 4331 43 25 44 32 206 |MD 42 54 79 58 67 51
Table 3.1477.1 GPS week: 1477 Day: 1 MJD: 54584
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 28 26 166 24 --- 18 | 14 22 109 37 --- 22
R04 |>>>>> 37 12 35 13 --- 13 | 47 21 38 56 --- 33
R06 |>>>>> 58 23 50 22 --- 20 | 223 230 9999 225 --- 226
R07 |>>>>> 19 35 73 34 244 23 | 34 51 69 39 103 34
R08 |>>>>> 39 36 33 30 --- 19 | 20 65 34 33 --- 30
R09 |>>>>> 221 73 114 43 --- 62 | 539 594 595 583 --- 573
R10 |>>>>> 36 26 24 22 --- 15 | 53 68 49 54 --- 55
R11 |>>>>> 150 48 118 34 --- 47 | 241 330 399 315 --- 311
R13 |>>>>> 186 110 148 85 --- 71 | 705 746 874 655 --- 710
R14 |>>>>> 19 10 26 16 --- 9 | 18 22 31 27 --- 19
R15 |>>>>> 27 25 50 16 116 16 | 93 101 81 112 58 97
R17 |>>>>> 36 55 95 45 --- 33 | 40 60 109 58 --- 46
R19 |>>>>> 28 21 47 34 --- 18 | 30 56 238 61 --- 45
R20 |>>>>> 25 16 50 20 --- 15 | 40 53 67 33 --- 40
R23 |>>>>> 42 38 49 50 --- 26 | 47 75 90 30 --- 48
R24 |>>>>> 35 20 52 26 363 18 | 296 326 325 313 254 315
------+------------------------------------+--------------------------------
RMS |>>>>> 87 44 83 36 261 |T 152 176 207 164 138 162
WRMS |>>>>> 31 26 54 36 261 |NE 152 176 207 164 138 162
MEDI |>>>>> 36 26 50 26 244 |MD 47 65 90 56 103 46
Table 3.1477.2 GPS week: 1477 Day: 2 MJD: 54585
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8110 15 16 30 31 --- 13 | 25 32 69 39 --- 25
R04 |10097 36 44 26 57 --- 25 | 26 70 44 37 --- 35
R06 |14287 55 46 >>>> 38 --- 33 | 141 172 9999 150 --- 146
R07 | 4640 29 31 63 32 145 22 | 53 53 55 29 104 33
R08 | 3728 39 35 35 48 --- 23 | 47 20 46 26 --- 25
R09 |11449 26 28 70 58 --- 26 | 283 322 355 317 --- 315
R10 | 6533 25 19 34 24 --- 14 | 77 63 79 74 --- 67
R11 | 9837 70 13 59 38 --- 27 | 252 316 362 303 --- 305
R13 | 7671 23 17 449 35 --- 18 | 569 534 831 513 --- 534
R14 | 4075 25 15 31 17 --- 12 | 26 34 47 35 --- 28
R15 |11278 34 20 52 33 115 20 | 75 81 97 78 61 76
R17 |15341 28 31 56 27 --- 20 | 32 36 74 20 --- 24
R19 | 5308 32 32 332 28 --- 22 | 34 45 548 30 --- 28
R20 | 1881 23 23 25 35 --- 15 | 59 69 54 38 --- 53
R23 | 1588 39 35 54 33 --- 23 | 34 57 96 70 --- 53
R24 | 5041 44 26 39 20 188 19 | 106 164 171 133 192 143
------+------------------------------------+--------------------------------
RMS | 8571 36 29 9807 36 152 |T 114 129 195 118 119 118
WRMS | 8571 31 24 84 36 152 |NE 114 129 195 118 119 118
MEDI | 6533 29 26 52 33 145 |MD 53 63 79 39 104 53
Table 3.1477.3 GPS week: 1477 Day: 3 MJD: 54586
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5664 39 17 30 21 --- 14 | 29 55 61 41 --- 44
R04 | 5331 24 15 41 21 --- 14 | 38 38 62 37 --- 39
R06 |15746 69 22 40 31 --- 23 | 307 309 9999 296 --- 301
R07 | 8163 32 26 67 52 142 25 | 53 49 98 39 59 47
R08 |11421 48 42 185 47 --- 31 | 63 59 155 41 --- 46
R09 |14117 31 15 278 19 --- 14 | 426 443 483 412 --- 434
R10 | 4363 29 17 26 26 --- 13 | 102 112 115 91 --- 102
R11 | 8735 62 28 66 35 --- 26 | 129 189 250 173 --- 182
R13 | 9403 66 15 54 31 --- 23 | 550 583 564 587 --- 587
R14 | 2018 30 23 25 29 --- 15 | 22 38 37 33 --- 25
R15 | 6243 25 29 70 49 69 25 | 78 100 108 124 49 97
R17 |13524 42 37 72 33 --- 26 | 39 71 89 47 --- 47
R19 | 6405 21 25 2171 41 --- 21 | 30 48 9999 27 --- 29
R20 | 2591 26 16 40 28 --- 15 | 26 22 48 22 --- 20
R23 | 3373 43 23 35 49 --- 21 | 43 49 63 83 --- 51
R24 | 3502 35 12 24 19 269 12 | 287 297 304 304 128 297
------+------------------------------------+--------------------------------
RMS | 8609 42 24 551 35 180 |T 138 153 174 147 78 146
WRMS | 8609 33 23 60 35 180 |NE 138 153 174 147 78 146
MEDI | 6243 32 22 41 31 142 |MD 53 59 98 47 59 47
Table 3.1477.4 GPS week: 1477 Day: 4 MJD: 54587
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4225 29 15 56 32 --- 19 | 46 45 66 43 --- 45
R04 | 4048 22 11 27 28 --- 12 | 24 24 25 34 --- 21
XR06 | ---- 32 36 --- 54 --- 29 | 132 164 --- 145 --- 148
R07 | 6660 23 25 44 44 161 20 | 24 35 54 61 52 36
R08 | 8097 50 36 222 32 --- 27 | 58 40 206 43 --- 34
R09 |12370 26 10 16 24 --- 10 | 164 182 195 185 --- 179
R10 | 3195 27 19 16 39 --- 15 | 61 81 62 81 --- 70
R11 | 4113 36 22 36 24 --- 16 | 122 135 166 148 --- 140
R13 | 6303 134 32 56 44 --- 30 | 315 383 437 342 --- 373
R14 | 1691 33 9 26 23 --- 13 | 23 26 39 28 --- 21
R15 | 4964 39 15 41 42 101 19 | 45 60 77 73 54 55
R17 | 9658 36 24 34 19 --- 16 | 40 61 66 62 --- 54
R19 | 3748 28 22 15 18 --- 12 | 18 36 330 33 --- 25
R20 | 3617 29 19 41 31 --- 17 | 41 39 62 40 --- 35
R23 | 2040 57 25 30 33 --- 20 | 56 34 39 43 --- 29
R24 | 4197 57 14 41 15 391 18 | 101 153 166 143 281 142
------+------------------------------------+--------------------------------
RMS | 5965 50 21 67 31 251 |T 79 93 132 94 129 87
WRMS | 5965 32 19 37 31 251 |NE 79 93 132 94 129 87
MEDI | 4197 32 19 36 31 161 |MD 46 45 66 61 54 45
Table 3.1477.5 GPS week: 1477 Day: 5 MJD: 54588
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5942 23 26 51 15 --- 16 | 31 49 63 39 --- 35
R04 | 3237 29 28 57 21 --- 19 | 25 41 85 25 --- 34
XR06 | ---- 22 36 --- 26 --- 20 | 200 227 --- 201 --- 214
R07 | 9935 37 45 66 56 135 29 | 24 31 75 64 57 38
R08 | 4171 39 36 66 15 --- 22 | 31 31 72 26 --- 23
R09 |12810 42 18 64 30 --- 21 | 441 464 478 454 --- 460
R10 | 3387 31 29 51 30 --- 19 | 93 102 102 79 --- 90
R11 |10860 49 27 75 27 --- 25 | 56 94 135 78 --- 81
R13 | 9258 129 33 33 32 --- 23 | 397 479 479 465 --- 472
R14 | 2835 31 27 36 30 --- 17 | 29 34 43 30 --- 22
R15 | 7445 23 25 29 31 182 16 | 71 83 88 91 89 81
R17 | 5704 26 25 53 24 --- 18 | 50 51 90 58 --- 54
R19 | 2413 23 25 30 37 --- 17 | 57 61 217 26 --- 41
R20 | 4177 30 20 48 15 --- 16 | 57 59 81 68 --- 59
R23 | 4063 38 33 42 18 --- 18 | 74 58 59 50 --- 52
R24 | 5799 34 36 42 17 797 18 | 207 219 257 238 418 227
------+------------------------------------+--------------------------------
RMS | 6882 46 30 51 29 478 |T 115 130 154 124 188 123
WRMS | 6882 33 27 47 29 478 |NE 115 130 154 124 188 123
MEDI | 5704 31 27 51 26 182 |MD 57 59 88 64 89 54
Table 3.1477.6 GPS week: 1477 Day: 6 MJD: 54589
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4526 21 15 24 16 --- 11 | 38 44 36 41 --- 39
R04 | 6060 22 22 32 17 --- 13 | 36 38 31 37 --- 33
XR06 | ---- 34 38 --- 30 --- 25 | 214 286 --- 234 --- 249
R07 | 5377 47 30 43 26 157 21 | 55 52 59 51 92 47
R08 | 5207 22 31 156 30 --- 20 | 46 33 65 40 --- 33
R09 |11539 35 25 60 36 --- 22 | 348 417 444 370 --- 393
R10 | 8677 37 24 64 36 --- 23 | 77 95 67 87 --- 81
R11 | 7855 30 26 57 21 --- 19 | 70 86 118 81 --- 84
R13 | 6989 27 27 73 27 --- 22 | 270 293 291 279 --- 282
R14 | 2596 16 18 39 30 --- 15 | 20 24 34 33 --- 19
R15 | 7200 47 34 40 39 232 23 | 50 65 61 70 96 56
R17 | 5669 22 35 31 41 --- 19 | 46 40 69 76 --- 49
R19 | 3058 20 33 60 57 --- 25 | 66 75 211 65 --- 69
R20 | 1972 27 21 42 27 --- 16 | 70 70 95 59 --- 69
R23 | 5954 23 43 44 46 --- 23 | 44 44 76 75 --- 48
R24 | 3202 60 31 31 39 524 24 | 113 175 173 147 722 150
------+------------------------------------+--------------------------------
RMS | 6228 33 29 61 34 343 |T 97 114 122 109 303 106
WRMS | 6228 26 27 51 34 343 |NE 97 114 122 109 303 106
MEDI | 5669 27 27 43 30 232 |MD 55 65 69 70 96 56
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