[IGSREPORT-16103] Wk 1471 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 3 06:57:45 PDT 2008
******************************************************************************
IGS Electronic Report 03 Apr 06:57:52 PDT 2008 Message Number 16103
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1471 (Mar 16, 2008 - Mar 22, 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 2.1471.
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:
igl1471[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1471 in the SP3 format.
igl14717.sum Combination Report for GPS Week 1471.
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 | 1158.0 ns
1 | 1200.2 ns
2 | 1164.0 ns
3 | 1156.1 ns
4 | 1199.3 ns
5 | 1193.2 ns
6 | 1120.3 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 | R08 R09 R11 R13
1 | ESX | R08
2 | ESX | R09 R13
3 | ESX | R08 R09 R13
4 | ESX | R09 R13 R17
5 | ESX | R09 R11 R13
6 | ESX | R04 R13
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 1.1471, 1a.1471).
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 2.1471.0-6)
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 3.1471.0-6).
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 1471 summary. (Mar 16, 2008 - Mar 22, 2008)
Table 1.1471.a GPS week : 1471 MJD: 54541.0-54547.0
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 66| 0 -1 0 -19 -19 -81 -.20 39 38 | 0 223 2683 2774
| 1 3 2 56 21 97 .09 | 0 244
cod 177| 0 2 0 9 31 95 -.18 36 25 | --- --- --- ---
| 1 1 7 32 26 63 .08 | --- ---
esx 109| -1 -1 -3 50 -28 29 .27 673 79 | -36473 -278 7218 18354
| 7 4 5 48 67 83 .12 | 30205 3835
iac n/a| -2 0 2 -35 -37 -21 .26 55 55 | 1170786 -2156 6637 15008
| 2 3 5 18 34 24 .08 | 29112 2460
mcc n/a| -5 7 52 87 -101 1855 .08 261 261 | --- --- --- ---
| 19 21 44 326 84 444 .63 | --- ---
Table 1.1471.b GPS week : 1471 MJD: 54541.0-54547.0
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 | 24 16 17 28 20 20 40 |
R04 | 18 16 26 15 22 16 18 |
R06 | 30 20 26 31 19 27 21 |
R07 | 54 40 30 22 14 21 10 |
R08 | 17 17 19 20 28 43 32 |
R09 | 25 26 16 20 19 22 18 |
R10 | 29 16 18 16 15 18 17 |
R11 | 29 41 35 34 30 31 32 |
R13 | 32 32 22 19 24 14 21 |
R14 | 15 15 19 15 14 13 14 |
R15 | 27 28 24 20 41 16 24 |
R17E | 61 24 34 38 39 43 50 |
R19E | 42 42 53 39 24 23 41 |
R20E | 30 38 48 41 32 27 32 |
R23E | 46 28 37 41 37 35 41 |
R24E | 20 18 26 22 21 25 27 |
Table 1.1471.c GPS week : 1471 MJD: 54541.0-54547.0
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 1471 0 | -196 50 158 -3031 -737 -22850 101.3 6071 6071 | 1158013 0
brd 1471 1 | -11 -156 -30 894 -321 -15890 101.3 6676 6676 | 1200194 0
brd 1471 2 | -55 4 338 740 1436 -25410 95.0 6033 6033 | 1164043 0
brd 1471 3 | -297 29 580 -487 -4669 -25200 97.9 6207 6207 | 1156130 0
brd 1471 4 | 397 -129 399 993 4043 -14200 97.9 6391 6391 | 1199335 0
brd 1471 5 | 27 -205 777 189 789 -13350 93.7 7923 7923 | 1193188 0
brd 1471 6 | -3 -245 531 1775 -4974 -14180 87.1 6677 6677 | 1120312 0
-------------+------------------------------------------------------------+----------------
brd 1471 mean| -19 -93 393 153 -633 -18725 96.3 6568 6568 | 1170173 0
brd 1471 sdev| 218 120 270 1569 3251 5502 5.0 652 652 | 29297 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 2.1471.0 GPS week: 1471 Day: 0 MJD: 54541
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 66| 0 -1 0 35 -17 -125 -.31 45 40 | 0 117 2614 2688
cod 177| 0 2 10 22 41 219 -.20 64 28 | --- --- --- ---
esx 109| 0 2 -6 15 -46 -18 .21 2487 80 | -55252 -2419 7561 23007
iac n/a| -3 -1 -2 -19 -18 2 .17 53 53 | 1156952 -1674 6054 16265
mcc n/a| 5 26 34 122 -173 1737 .13 312 312 | --- --- --- ---
Table 2.1471.1 GPS week: 1471 Day: 1 MJD: 54542
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 66| 0 -3 -3 -42 -8 42 -.29 41 42 | 0 285 3143 3267
cod 177| 1 4 0 16 58 63 -.11 37 26 | --- --- --- ---
esx 109| -2 3 3 30 -37 -94 .18 97 49 | -9110 4182 8211 17773
iac n/a| -4 -3 4 -43 -108 -42 .26 40 40 | 1200545 -1218 8027 15051
mcc n/a| -6 4 69 477 -66 2158 -.92 241 241 | --- --- --- ---
Table 2.1471.2 GPS week: 1471 Day: 2 MJD: 54543
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 66| 1 1 2 81 -47 -63 -.10 39 35 | 0 243 2946 3067
cod 177| 1 0 7 -35 56 64 -.25 31 25 | --- --- --- ---
esx 109| -13 -1 -6 81 -37 -6 .15 683 77 | -44741 -6061 7362 16644
iac n/a| 2 -2 -3 -24 -38 -22 .42 60 60 | 1167326 -7284 7132 14853
mcc n/a| -2 44 124 61 -65 2231 -.40 220 220 | --- --- --- ---
Table 2.1471.3 GPS week: 1471 Day: 3 MJD: 54544
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 66| 1 4 -1 -63 14 -238 -.12 37 36 | 0 24 2326 2406
cod 177| 0 2 0 -17 -1 90 -.19 27 23 | --- --- --- ---
esx 109| -5 -3 -5 52 115 76 .45 341 103 | -56660 4265 7151 16589
iac n/a| -3 6 4 -63 -45 -4 .21 54 54 | 1154576 -948 6489 14366
mcc n/a| -47 -17 79 403 -222 2376 1.00 343 343 | --- --- --- ---
Table 2.1471.4 GPS week: 1471 Day: 4 MJD: 54545
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 66| 2 -2 2 -33 -39 -136 -.23 35 35 | 0 -27 2602 2678
cod 177| 0 3 3 -11 9 120 -.12 26 22 | --- --- --- ---
esx 109| 2 -7 -8 91 -96 173 .31 592 63 | 535 -580 6092 17205
iac n/a| -1 -2 -2 -30 -31 -59 .20 56 56 | 1201389 -3128 5960 13797
mcc n/a| 0 -7 55 -1 -59 1852 -.13 158 158 | --- --- --- ---
Table 2.1471.5 GPS week: 1471 Day: 5 MJD: 54546
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 66| -2 -2 1 -50 -7 29 -.20 35 36 | 0 209 2743 2823
cod 177| 0 3 -3 52 49 18 -.09 25 18 | --- --- --- ---
esx 109| -1 -5 -6 -27 -66 44 .40 262 60 | -10545 1489 7615 17408
iac n/a| -7 -3 3 -14 0 -33 .26 69 69 | 1192261 -916 6527 13220
mcc n/a| 7 1 7 75 -148 1104 .36 230 230 | --- --- --- ---
Table 2.1471.6 GPS week: 1471 Day: 6 MJD: 54547
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 66| -1 -4 1 -65 -29 -75 -.13 40 41 | 0 714 2413 2495
cod 177| 2 1 -12 40 4 90 -.31 40 34 | --- --- --- ---
esx 109| 10 4 5 109 -29 30 .18 247 122 | -79543 -2825 6540 19854
iac n/a| -2 0 11 -54 -19 6 .27 54 54 | 1122456 74 6275 17506
mcc n/a| 4 -3 -5 -526 26 1534 .54 327 327 | --- --- --- ---
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 3.1471.0 GPS week: 1471 Day: 0 MJD: 54541
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4053 41 22 70 21 --- 24 | 48 56 93 53 --- 55
R04 | 5927 30 21 43 25 --- 17 | 28 34 54 45 --- 32
R06 | 4431 66 30 31 58 --- 29 | 61 74 79 91 --- 64
R07 | 2770 65 155 81 42 269 53 | 25 131 71 20 98 40
R08 | 7368 21 24 262 26 --- 16 | 23 20 132 39 --- 23
R09 |12874 25 48 7803 31 --- 25 | 25 39 9999 37 --- 29
R10 | 3154 22 59 76 35 --- 28 | 18 36 54 35 --- 20
R11 | 3806 36 33 1976 49 --- 28 | 29 47 9999 82 --- 49
R13 | 9248 23 61 5276 45 --- 31 | 14 54 9999 39 --- 21
R14 | 1419 22 16 35 24 --- 14 | 30 25 20 34 --- 24
R15 | 6213 38 33 75 31 105 26 | 28 34 80 39 119 31
R17E | 5998 89 101 100 129 --- 61 | 47 68 94 134 --- 56
XR19E | 2582 52 43 --- 75 --- 41 | 57 53 --- 81 --- 57
R20E | 992 39 47 54 63 --- 29 | 41 37 38 85 --- 29
R23E | 7897 65 97 81 74 --- 45 | 30 80 72 95 --- 43
R24E | 1993 25 27 53 27 456 19 | 52 48 68 63 149 53
------+------------------------------------+--------------------------------
RMS | 6070 45 64 2486 53 312 |T 34 52 71 60 122 39
WRMS | 6070 40 28 80 53 312 |NE 29 50 72 46 108 35
MEDI | 4053 36 33 76 35 269 |MD 29 47 71 45 119 32
Table 3.1471.1 GPS week: 1471 Day: 1 MJD: 54542
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3936 26 16 54 21 --- 16 | 59 51 65 47 --- 49
R04 | 6135 28 15 35 31 --- 15 | 34 50 64 45 --- 43
R06 | 1598 36 30 47 29 --- 19 | 83 98 116 107 --- 96
R07 | 2199 51 92 57 55 222 40 | 21 107 53 25 87 43
R08 | 4682 24 17 246 27 --- 16 | 30 22 177 37 --- 22
R09 |14815 33 25 94 33 --- 26 | 29 43 867 58 --- 37
R10 | 3668 18 30 43 20 --- 15 | 15 26 33 14 --- 12
R11 |11719 65 31 158 31 --- 41 | 30 61 387 67 --- 66
R13 | 9799 37 36 120 36 --- 32 | 21 31 980 41 --- 32
R14 | 1806 29 14 38 25 --- 14 | 12 18 64 34 --- 23
R15 | 4577 58 25 77 40 164 27 | 21 32 111 55 51 35
R17E | 8988 51 27 46 40 --- 23 | 42 36 52 67 --- 29
XR19E | 2934 62 35 --- 75 --- 41 | 49 67 --- 96 --- 63
R20E | 2042 46 56 64 86 --- 38 | 48 38 48 80 --- 39
R23E | 2836 47 37 73 46 --- 28 | 36 44 95 64 --- 39
R24E | 1604 28 24 42 30 313 17 | 46 35 64 46 74 40
------+------------------------------------+--------------------------------
RMS | 6676 41 37 97 40 241 |T 36 47 211 55 70 41
WRMS | 6676 42 26 49 40 241 |NE 32 49 265 48 69 41
MEDI | 3668 36 27 57 31 222 |MD 30 38 65 47 74 39
Table 3.1471.2 GPS week: 1471 Day: 2 MJD: 54543
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4011 33 21 42 29 --- 17 | 35 49 55 33 --- 36
R04 | 5814 27 25 88 47 --- 26 | 19 29 96 41 --- 29
R06 | 9723 38 37 43 61 --- 25 | 46 65 82 108 --- 62
R07 | 5192 28 39 105 27 198 29 | 46 48 142 63 85 59
R08 | 3193 29 24 43 39 --- 18 | 52 25 50 38 --- 30
R09 | 8760 25 14 2003 30 --- 16 | 22 32 9999 50 --- 28
R10 | 2126 18 17 62 30 --- 17 | 22 26 69 34 --- 23
R11 | 5666 32 34 127 53 --- 35 | 22 49 254 66 --- 50
R13 |10539 21 28 1707 42 --- 21 | 25 42 9999 55 --- 31
R14 | 1912 38 18 45 34 --- 19 | 18 37 49 39 --- 21
R15 | 4738 34 30 54 54 230 24 | 20 57 47 54 107 29
R17E | 9913 68 39 83 54 --- 34 | 57 46 89 67 --- 35
XR19E | 3496 72 39 --- 115 --- 52 | 37 80 --- 100 --- 56
R20E | 3032 49 50 49 155 --- 47 | 49 41 68 65 --- 35
R23E | 1783 55 32 91 89 --- 36 | 29 44 98 77 --- 32
R24E | 1776 54 33 61 28 229 25 | 47 36 65 41 87 34
------+------------------------------------+--------------------------------
RMS | 6033 39 31 683 60 219 |T 34 44 89 58 93 36
WRMS | 6033 35 25 77 60 219 |NE 29 41 93 52 96 36
MEDI | 4011 33 30 62 42 229 |MD 29 42 69 54 87 32
Table 3.1471.3 GPS week: 1471 Day: 3 MJD: 54544
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3020 39 31 88 53 --- 28 | 59 74 131 59 --- 62
R04 | 6254 22 18 35 35 --- 15 | 30 51 67 57 --- 45
R06 |10445 35 38 116 30 --- 30 | 129 119 179 137 --- 126
R07 | 2876 33 20 44 59 360 22 | 59 66 58 49 230 45
R08 | 4006 22 23 202 39 --- 19 | 28 46 105 67 --- 45
R09 |10792 29 17 1073 41 --- 20 | 46 24 987 62 --- 32
R10 | 1508 15 15 53 31 --- 15 | 23 24 58 36 --- 21
R11 | 5085 53 20 138 32 --- 34 | 42 53 188 57 --- 45
R13 |10425 29 25 681 26 --- 19 | 41 43 369 54 --- 40
R14 | 3476 23 17 49 23 --- 15 | 26 23 55 19 --- 21
R15 | 2433 26 21 75 25 379 20 | 24 42 96 54 240 36
R17E |10339 49 22 146 62 --- 37 | 54 53 84 75 --- 43
XR19E | 1957 45 40 --- 82 --- 38 | 69 76 --- 86 --- 64
R20E | 2460 43 43 36 129 --- 40 | 64 63 66 82 --- 52
R23E | 1814 58 44 131 71 --- 40 | 39 40 118 101 --- 46
R24E | 2926 45 24 33 51 282 22 | 49 47 60 42 176 42
------+------------------------------------+--------------------------------
RMS | 6206 37 27 341 54 343 |T 48 52 174 64 215 47
WRMS | 6206 36 23 103 54 343 |NE 46 51 208 59 235 47
MEDI | 3020 33 22 88 39 360 |MD 42 47 96 57 230 45
Table 3.1471.4 GPS week: 1471 Day: 4 MJD: 54545
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6918 34 26 48 42 --- 20 | 29 40 60 50 --- 33
R04 | 6358 41 21 71 26 --- 21 | 47 28 81 36 --- 34
R06 | 3264 20 28 53 34 --- 18 | 64 84 94 73 --- 73
R07 | 5246 22 11 46 25 54 13 | 43 52 67 62 133 51
R08 | 5104 38 18 107 43 --- 28 | 35 58 146 48 --- 50
R09 | 9546 29 14 363 41 --- 19 | 40 35 985 31 --- 27
R10 | 1234 26 15 48 21 --- 14 | 32 31 39 38 --- 25
R11 | 6401 53 20 74 75 --- 30 | 20 53 110 99 --- 47
R13 |10667 40 31 2233 29 --- 23 | 36 46 9999 41 --- 29
R14 | 3570 26 16 42 18 --- 14 | 23 21 32 22 --- 18
R15 | 6626 30 30 182 33 210 40 | 22 31 179 40 149 32
R17E |11720 31 34 264 97 --- 38 | 36 33 258 82 --- 24
XR19E | 1224 27 19 --- 57 --- 24 | 40 40 --- 70 --- 37
R20E | 1591 26 42 50 95 --- 31 | 43 37 43 76 --- 32
R23E | 2995 57 37 71 98 --- 36 | 29 31 70 99 --- 31
R24E | 2666 32 17 44 55 166 20 | 40 46 45 52 161 40
------+------------------------------------+--------------------------------
RMS | 6390 35 26 592 56 158 |T 36 41 157 57 147 36
WRMS | 6390 35 22 63 56 158 |NE 35 43 179 49 141 38
MEDI | 5104 30 20 71 41 166 |MD 36 37 70 50 149 32
Table 3.1471.5 GPS week: 1471 Day: 5 MJD: 54546
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8155 35 19 55 40 --- 19 | 51 43 67 51 --- 34
R04 | 5441 35 16 32 35 --- 16 | 22 40 50 52 --- 34
R06 | 3156 36 45 44 65 --- 26 | 90 77 93 115 --- 81
R07 | 2320 24 18 69 47 89 20 | 43 64 83 41 51 48
R08 | 6227 37 46 168 52 --- 43 | 43 45 141 62 --- 48
R09 |10486 35 19 736 47 --- 22 | 63 48 861 51 --- 46
R10 | 1198 18 12 54 49 --- 17 | 27 17 77 26 --- 17
R11 | 9964 25 25 300 89 --- 30 | 35 51 284 104 --- 52
R13 |11504 25 14 575 20 --- 13 | 69 63 483 58 --- 60
R14 | 2792 22 12 39 25 --- 13 | 23 21 41 21 --- 16
R15 | 6075 34 14 43 27 178 16 | 37 34 54 29 71 29
R17E |15849 36 26 111 147 --- 42 | 30 40 124 115 --- 34
XR19E | 1815 28 24 --- 54 --- 23 | 36 45 --- 54 --- 35
R20E |12149 29 17 73 83 --- 26 | 67 52 79 50 --- 49
R23E | 1101 56 33 56 115 --- 35 | 44 28 83 124 --- 43
R24E | 1893 55 19 41 61 345 24 | 48 44 60 49 105 41
------+------------------------------------+--------------------------------
RMS | 7923 35 25 262 69 230 |T 45 44 172 62 75 41
WRMS | 7923 36 18 60 69 230 |NE 45 45 203 55 61 42
MEDI | 5441 34 19 56 49 178 |MD 43 44 83 51 71 41
Table 3.1471.6 GPS week: 1471 Day: 6 MJD: 54547
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8514 54 89 82 34 --- 40 | 32 106 68 61 --- 56
R04 | 3082 20 30 233 25 --- 18 | 34 60 158 39 --- 41
R06 | 4547 41 39 28 29 --- 21 | 75 91 93 100 --- 85
R07 | 2756 19 15 19 19 94 10 | 49 78 82 66 56 64
R08 | 6793 38 32 113 34 --- 31 | 39 36 89 53 --- 38
XR09 | 6165 16 25 --- 34 --- 18 | 38 44 --- 48 --- 36
R10 | 2463 18 27 42 31 --- 16 | 34 30 58 34 --- 32
R11 | 7582 45 28 108 42 --- 31 | 23 40 174 66 --- 31
R13 |11875 33 31 878 20 --- 21 | 25 47 9999 30 --- 29
R14 | 1798 18 16 34 27 --- 13 | 29 34 40 19 --- 22
R15 | 5966 30 20 82 29 165 23 | 39 25 76 29 35 23
R17E |15728 46 59 126 116 --- 49 | 69 68 130 128 --- 73
R19E | 1459 28 47 125 85 --- 41 | 49 27 9999 66 --- 25
R20E | 3731 47 33 95 54 --- 32 | 59 69 86 90 --- 56
R23E | 1908 65 49 72 95 --- 40 | 42 51 88 105 --- 48
R24E | 1320 60 25 35 54 534 26 | 50 42 44 57 88 41
------+------------------------------------+--------------------------------
RMS | 6676 40 40 247 54 327 |T 42 53 91 61 59 43
WRMS | 6676 41 34 122 54 327 |NE 37 53 93 49 45 41
MEDI | 3731 33 30 82 34 165 |MD 39 44 86 57 56 38
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