[IGSREPORT-18280] Wk 1568 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Feb 11 06:01:07 PST 2010
******************************************************************************
IGS Electronic Report 11 Feb 06:01:30 PST 2010 Message Number 18280
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1568 (Jan 24, 2010 - Jan 30, 2010)
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 2.1568.
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:
igl1568[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1568 in the SP3 format.
igl15687.sum Combination Report for GPS Week 1568.
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 | 476.4 ns
1 | 472.9 ns
2 | 481.0 ns
3 | 479.0 ns
4 | 403.9 ns
5 | 387.8 ns
6 | 395.4 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
----+--------+---------------
3 | BKG | R05
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 1.1568, 1a.1568).
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 2.1568.0-6)
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 3.1568.0-6).
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 1568 summary. (Jan 24, 2010 - Jan 30, 2010)
Table 1.1568.a GPS week : 1568 MJD: 55220.0-55226.0
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 128| 0 1 1 14 3 -28 -.12 20 20 | 0 428 2251 2511
| 1 0 2 15 49 119 .04 | 0 485
cod 242| 0 0 -2 32 -30 22 -.13 13 13 | --- --- --- ---
| 1 0 2 14 25 36 .04 | --- ---
esx 125| 0 0 -2 -45 43 35 .44 27 25 | 95242 -166 4370 9207
| 2 2 4 40 44 37 .05 | 47565 4299
iac n/a| 1 2 5 -40 5 -68 -.10 27 27 | 2775854 7999 516318 575266
| 0 1 7 24 31 109 .07 | 4979039 10737
mcc n/a| 9 2 54 -118 -134 745 -.11 163 163 | --- --- --- ---
| 8 9 22 105 108 1298 .27 | --- ---
Table 1.1568.b GPS week : 1568 MJD: 55220.0-55226.0
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 | 67 47 43 43 22 33 25 |
R02 | 12 12 8 10 10 6 13 |
R03 | 9 13 13 11 8 11 8 |
R04 | 12 10 14 12 9 10 11 |
R05 | 7 16 1636 42 39 26 17 |
R07 | 9 10 8 9 34 32 29 |
R08 | 9 9 11 9 9 12 12 |
R10 | 13 10 10 11 13 12 12 |
R11 | 11 16 14 14 11 11 10 |
R13 | 11 12 8 13 14 10 16 |
R14 | 18 12 11 10 12 12 10 |
R15 | 12 7 9 10 11 10 10 |
R17 | 16 16 12 10 9 11 15 |
R18 | 12 10 9 8 10 9 18 |
R19 | 12 10 17 12 10 8 15 |
R20 | 18 14 15 16 13 9 18 |
R21 | 10 12 12 13 10 11 18 |
R23 | 15 16 16 22 16 16 17 |
Table 1.1568.c GPS week : 1568 MJD: 55220.0-55226.0
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 1568 0 | 16 95 17 181 -2442 -20900 91.9 1784 1784 | 476389 0
brd 1568 1 | -13 86 -65 -2411 598 -18050 87.3 2028 2028 | 472914 0
brd 1568 2 | -42 142 -86 -3409 3011 -19700 87.6 2826 2826 | 480995 0
brd 1568 3 | 43 23 23 -385 -2280 -15780 89.5 2361 2361 | 478973 0
brd 1568 4 | -64 -26 -115 -1578 -2373 -11270 91.7 2288 2288 | 403888 0
brd 1568 5 | -27 -55 -49 -1748 -3155 -12970 90.4 2593 2593 | 387815 0
brd 1568 6 | 33 43 11 -1517 -621 -13450 87.9 2510 2510 | 395431 0
-------------+------------------------------------------------------------+----------------
brd 1568 mean| -7 44 -37 -1552 -1037 -16017 89.5 2341 2341 | 442343 0
brd 1568 sdev| 40 70 55 1196 2199 3651 1.9 350 350 | 43936 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 2.1568.0 GPS week: 1568 Day: 0 MJD: 55220
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 128| 1 0 5 22 21 -123 -.17 22 23 | 0 382 1900 2010
cod 242| -1 -2 -6 19 -30 19 -.10 15 14 | --- --- --- ---
esx 125| 2 1 -4 -32 38 99 .37 25 25 | 131407 1575 3734 8461
iac n/a| 0 1 6 -31 22 -1 -.06 25 25 | 476171 -234 3632 7597
mcc n/a| 12 6 43 -259 37 105 -.15 102 102 | --- --- --- ---
Table 2.1568.1 GPS week: 1568 Day: 1 MJD: 55221
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 128| 0 1 5 -9 -2 -121 -.12 22 22 | 0 -10 1539 1670
cod 242| 1 0 1 48 -23 23 -.14 12 11 | --- --- --- ---
esx 125| -2 -2 -9 -23 51 33 .44 24 23 | 124541 2784 3783 9323
iac n/a| 1 0 0 -48 -17 39 -.15 29 29 | 472630 2411 3787 8612
mcc n/a| 9 -13 48 -116 -104 -1158 .01 142 142 | --- --- --- ---
Table 2.1568.2 GPS week: 1568 Day: 2 MJD: 55222
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 128| 0 1 0 28 70 -8 -.14 17 16 | 0 1042 2227 2397
cod 242| 0 0 -1 21 -76 -14 -.08 14 14 | --- --- --- ---
esx 125| 2 2 -2 -73 71 30 .48 27 26 | 133424 -3348 5140 11897
iac n/a| 1 1 9 -13 14 8 -.21 26 26 | 482177 -1657 5009 10657
mcc n/a| 14 10 16 -113 -87 -146 .14 134 134 | --- --- --- ---
Table 2.1568.3 GPS week: 1568 Day: 3 MJD: 55223
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 128| 2 0 -2 17 55 192 -.05 17 17 | 0 -49 2415 2621
cod 242| -2 0 -5 19 -45 -17 -.08 11 10 | --- --- --- ---
esx 125| -2 0 0 -98 -41 15 .51 37 31 | 140783 -3113 5911 9088
iac n/a| 2 4 16 -20 38 -258 -.10 27 27 | -999999 5843 601802 999999
mcc n/a| 18 -5 59 -37 -304 631 -.55 139 139 | --- --- --- ---
Table 2.1568.4 GPS week: 1568 Day: 4 MJD: 55224
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 128| 0 0 1 29 -21 53 -.14 17 16 | 0 1160 2363 2537
cod 242| 0 -1 0 23 -11 4 -.16 12 12 | --- --- --- ---
esx 125| 0 0 -5 -5 62 41 .48 23 22 | 59196 -5671 4141 9140
iac n/a| 1 2 11 -68 10 -176 -.09 28 28 | -999999 4022 999999 999999
mcc n/a| 9 13 78 44 -116 1144 -.02 158 158 | --- --- --- ---
Table 2.1568.5 GPS week: 1568 Day: 5 MJD: 55225
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 128| -2 2 0 12 -71 -134 -.10 21 20 | 0 188 3095 3914
cod 242| 0 -1 -1 47 3 63 -.13 11 10 | --- --- --- ---
esx 125| 1 1 -1 -87 97 49 .37 22 22 | 29267 6908 3905 7444
iac n/a| 0 2 2 -23 -55 -32 -.04 24 24 | 9999999 27315 999999 999999
mcc n/a| 9 9 81 -108 -133 2049 .17 191 191 | --- --- --- ---
Table 2.1568.6 GPS week: 1568 Day: 6 MJD: 55226
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 128| 0 1 1 -2 -25 -55 -.12 28 24 | 0 288 2221 2433
cod 242| -2 -1 -2 49 -28 76 -.19 19 17 | --- --- --- ---
esx 125| 2 -2 6 0 26 -23 .42 29 24 | 48078 -299 3979 9100
iac n/a| 0 2 -5 -76 22 -58 -.02 29 29 | 9999999 18293 999999 999999
mcc n/a| -7 -3 53 -237 -231 2594 -.36 275 275 | --- --- --- ---
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 3.1568.0 GPS week: 1568 Day: 0 MJD: 55220
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 52 --- 87 --- 67 | --- 59 --- 123 --- 79
R02 | 2408 25 17 21 23 --- 12 | 22 32 31 28 --- 25
XR03 | 564 12 8 --- 18 --- 9 | 24 27 --- 31 --- 26
R04 | 2111 18 16 25 22 --- 11 | 23 19 38 34 --- 22
R05 | 1862 11 10 12 16 --- 7 | 325 496 38 31 --- 328
R07 | 1626 13 15 17 18 --- 9 | 33 29 34 24 --- 26
R08 | 1494 16 11 17 16 144 8 | 45 47 41 36 139 41
R10 | 2749 33 12 30 12 --- 13 | 27 19 39 21 --- 17
R11 | 1821 24 15 16 23 76 11 | 13 15 39 23 103 13
R13 | 928 20 13 22 19 --- 10 | 25 26 40 21 --- 25
R14 | 2072 28 23 44 26 --- 17 | 21 10 54 29 --- 19
R15 | 2200 27 18 16 15 70 11 | 28 20 25 27 37 21
R17 | 855 31 15 15 42 --- 15 | 30 37 40 52 --- 36
R18 | 2115 12 11 35 20 --- 11 | 25 26 39 36 --- 25
R19 | 1638 24 12 25 22 --- 12 | 23 32 42 33 --- 27
R20 | 1024 20 21 33 46 --- 17 | 15 18 45 25 --- 19
R21 | 832 15 12 17 24 --- 10 | 26 32 37 40 --- 31
R23 | 1350 24 17 34 30 --- 15 | 61 73 98 83 --- 75
------+------------------------------------+--------------------------------
RMS | 1784 22 15 25 25 102 |T 45 56 42 38 93 47
WRMS | 1784 23 14 25 25 102 |NE 45 56 42 38 93 47
MEDI | 1638 20 15 21 22 76 |MD 25 27 39 31 103 25
Table 3.1568.1 GPS week: 1568 Day: 1 MJD: 55221
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 30 --- 73 --- 47 | --- 51 --- 62 --- 47
R02 | 2499 28 13 19 26 --- 12 | 22 24 25 25 --- 19
XR03 | 688 19 12 --- 26 --- 12 | 24 24 --- 28 --- 20
R04 | 1815 23 10 17 19 --- 9 | 30 19 33 19 --- 19
XR05 | 1734 --- 8 28 35 --- 16 | --- 623 34 29 --- 337
R07 | 2903 14 12 24 18 --- 9 | 21 18 26 19 --- 17
R08 | 1548 16 13 20 17 158 9 | 20 31 34 26 113 24
R10 | 2859 17 13 25 17 --- 10 | 21 19 31 16 --- 15
R11 | 2890 22 21 39 26 165 15 | 12 27 48 18 84 19
R13 | 1041 19 9 30 25 --- 11 | 19 19 44 25 --- 20
R14 | 1777 22 12 22 32 --- 12 | 21 16 24 40 --- 18
R15 | 2499 13 10 10 19 94 7 | 27 23 22 32 43 23
R17 | 1635 30 14 28 45 --- 16 | 36 36 43 42 --- 35
R18 | 891 17 13 23 20 --- 10 | 22 25 33 39 --- 25
R19 | 1739 16 7 25 23 --- 10 | 23 26 31 36 --- 24
R20 | 1354 34 9 22 36 --- 14 | 13 29 24 20 --- 19
R21 | 635 19 10 20 35 --- 11 | 26 28 37 25 --- 26
R23 | 2364 24 10 29 48 --- 15 | 40 52 59 58 --- 48
------+------------------------------------+--------------------------------
RMS | 2028 22 12 24 29 142 |T 23 60 34 31 80 41
WRMS | 2028 22 11 23 29 142 |NE 23 60 34 31 80 41
MEDI | 1739 19 12 23 26 158 |MD 22 25 33 26 84 20
Table 3.1568.2 GPS week: 1568 Day: 2 MJD: 55222
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 9286 --- 29 --- 62 --- 42 | --- 50 --- 49 --- 49
R02 | 1730 13 12 9 22 --- 8 | 21 33 27 34 --- 25
XR03 | 1163 15 11 --- 30 --- 13 | 24 37 --- 38 --- 31
R04 | 1667 19 20 18 36 --- 13 | 30 27 30 33 --- 24
XR05 |19486 1848 1447 --- --- --- 1635 | 895 9999 --- --- --- 9999
R07 | 8727 11 9 23 14 --- 8 | 26 25 34 36 --- 27
R08 | 1125 8 13 27 25 82 10 | 35 38 54 28 45 36
R10 | 2204 14 12 24 21 --- 10 | 16 21 30 21 --- 17
R11 | 2205 13 18 42 19 207 13 | 21 22 53 22 50 20
R13 | 1610 16 11 15 14 --- 8 | 26 19 39 21 --- 22
R14 | 1510 16 12 25 21 --- 10 | 20 11 34 36 --- 18
R15 | 2443 11 9 17 26 63 9 | 16 26 25 26 21 17
R17 | 1930 21 12 21 28 --- 11 | 28 29 37 43 --- 29
R18 | 1963 17 10 20 15 --- 8 | 37 39 36 34 --- 35
R19 | 1344 24 20 49 21 --- 16 | 51 44 49 37 --- 39
R20 | 1583 17 12 25 47 --- 14 | 24 22 33 31 --- 18
R21 | 1169 12 13 35 26 --- 12 | 35 35 46 37 --- 34
R23 | 1660 30 17 28 36 --- 15 | 56 80 93 76 --- 73
------+------------------------------------+--------------------------------
RMS | 2826 17 14 27 26 134 |T 80 32 41 35 38 30
WRMS | 2826 16 14 26 26 134 |NE 80 32 41 35 38 30
MEDI | 1667 16 12 24 25 82 |MD 26 29 36 34 45 27
Table 3.1568.3 GPS week: 1568 Day: 3 MJD: 55223
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 5761 75 31 --- 86 --- 43 | 51 73 --- 82 --- 63
R02 | 1205 14 11 33 16 --- 10 | 32 35 32 36 --- 29
R03 | 1905 12 10 28 30 --- 10 | 29 30 9999 32 --- 27
R04 | 1368 14 10 33 29 --- 11 | 46 34 47 36 --- 36
XR05 | 1455 361 26 --- 66 --- 42 | 341 504 --- 37 --- 282
R07 | 5253 19 11 17 16 --- 8 | 30 28 31 30 --- 23
R08 | 857 17 10 13 20 100 8 | 20 29 36 30 53 24
R10 | 1529 13 12 35 17 --- 10 | 15 21 32 18 --- 13
R11 | 1373 18 14 49 17 204 13 | 20 27 59 18 46 19
R13 | 1589 21 11 44 16 --- 12 | 26 17 51 28 --- 21
R14 | 3235 10 7 34 24 --- 10 | 22 19 34 30 --- 15
R15 | 1569 14 8 28 24 79 9 | 43 42 42 31 41 36
R17 | 2237 16 10 16 27 --- 9 | 35 44 48 44 --- 38
R18 | 4488 6 9 24 20 --- 8 | 29 36 33 35 --- 30
R19 | 676 18 8 17 42 --- 12 | 24 23 26 44 --- 21
R20 | 1668 28 8 33 47 --- 15 | 13 22 39 34 --- 17
R21 | 1692 17 11 41 27 --- 12 | 41 38 38 36 --- 31
R23 | 1724 21 19 86 36 --- 22 | 73 75 113 93 --- 77
------+------------------------------------+--------------------------------
RMS | 2361 17 11 37 27 139 |T 49 60 44 38 46 44
WRMS | 2361 17 10 31 27 139 |NE 49 60 44 38 46 44
MEDI | 1589 17 10 33 24 100 |MD 29 30 38 34 46 27
Table 3.1568.4 GPS week: 1568 Day: 4 MJD: 55224
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 7417 38 24 --- 31 --- 22 | 39 44 --- 61 --- 34
R02 | 1530 15 7 22 23 --- 9 | 19 25 51 36 --- 26
R03 | 2238 14 12 11 22 --- 8 | 30 35 9999 31 --- 32
R04 | 1137 13 11 17 24 --- 9 | 22 28 24 24 --- 20
XR05 | 1538 69 45 --- 44 --- 38 | 189 257 --- 33 --- 148
XR07 |15380 29 46 --- 71 --- 33 | 34 49 --- 50 --- 30
R08 | 1178 14 10 14 24 146 8 | 24 22 26 24 32 19
R10 | 2169 12 20 33 18 --- 12 | 8 20 45 22 --- 16
R11 | 2172 14 11 26 25 183 10 | 13 17 40 27 20 19
R13 | 1511 15 16 34 33 --- 13 | 13 22 48 22 --- 19
R14 | 3625 18 14 25 31 --- 12 | 22 24 32 44 --- 23
R15 | 3180 17 13 26 23 143 11 | 22 22 21 23 20 15
R17 | 1913 16 10 7 25 --- 8 | 35 38 39 44 --- 37
R18 | 4540 19 11 21 20 --- 10 | 42 34 39 28 --- 33
R19 | 474 16 10 21 23 --- 9 | 36 39 35 46 --- 36
R20 | 2162 18 14 18 40 --- 12 | 15 17 20 19 --- 12
R21 | 1443 11 10 23 28 --- 10 | 29 40 37 33 --- 34
R23 | 1497 30 14 26 44 --- 16 | 67 79 85 96 --- 78
------+------------------------------------+--------------------------------
RMS | 2287 17 12 23 28 158 |T 36 45 38 36 24 35
WRMS | 2287 16 12 22 28 158 |NE 36 45 38 36 24 35
MEDI | 1913 16 12 22 25 146 |MD 24 28 37 31 20 26
Table 3.1568.5 GPS week: 1568 Day: 5 MJD: 55225
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 2667 60 34 --- 55 --- 33 | 47 32 --- 43 --- 27
R02 | 3036 12 6 13 10 --- 5 | 23 29 28 25 --- 25
R03 | 1779 17 14 27 21 --- 11 | 23 30 9999 32 --- 26
R04 | 1247 12 8 27 21 --- 9 | 45 37 43 39 --- 38
XR05 | 2449 41 26 --- 48 --- 25 | 128 204 --- 23 --- 106
XR07 | 7731 68 19 --- 55 --- 31 | 52 32 --- 38 --- 22
R08 | 1863 21 9 22 31 201 11 | 35 26 31 25 39 25
R10 | 3119 24 11 29 24 --- 12 | 30 14 28 20 --- 13
R11 | 2995 14 13 27 23 171 11 | 18 21 25 17 31 14
R13 | 2138 14 11 18 28 --- 10 | 15 23 31 29 --- 20
R14 | 3722 30 10 24 25 --- 12 | 12 18 30 19 --- 13
R15 | 5267 18 11 24 19 200 10 | 34 30 39 32 36 29
R17 | 887 24 13 18 24 --- 11 | 32 32 47 34 --- 32
R18 | 2784 22 7 19 14 --- 8 | 30 28 38 27 --- 28
R19 | 630 18 8 15 20 --- 8 | 28 19 25 25 --- 20
R20 | 1315 13 7 20 25 --- 9 | 22 28 51 42 --- 31
R21 | 1050 27 8 15 24 --- 10 | 21 21 24 31 --- 19
R23 | 2605 37 15 28 39 --- 16 | 45 57 62 75 --- 57
------+------------------------------------+--------------------------------
RMS | 2593 21 11 22 24 191 |T 35 37 35 32 35 30
WRMS | 2593 20 10 22 24 191 |NE 35 37 35 32 35 30
MEDI | 2449 21 11 22 24 200 |MD 30 28 31 29 36 25
Table 3.1568.6 GPS week: 1568 Day: 6 MJD: 55226
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1677 36 29 63 37 --- 24 | 37 57 18 45 --- 45
R02 | 3056 21 14 31 25 --- 13 | 33 30 30 30 --- 23
R03 | 849 12 12 10 20 --- 8 | 28 34 9999 26 --- 27
R04 | 1453 9 15 13 32 --- 10 | 30 24 32 32 --- 26
R05 | 3732 27 31 26 31 --- 16 | 93 262 31 34 --- 135
XR07 |14107 58 16 --- 49 --- 29 | 41 33 --- 58 --- 33
R08 | 2272 16 12 20 35 332 12 | 25 37 31 23 37 27
R10 | 1947 26 11 27 16 --- 12 | 27 28 41 24 --- 23
R11 | 2275 22 15 12 21 219 10 | 12 31 25 27 36 17
R13 | 2601 24 24 35 25 --- 15 | 19 16 31 19 --- 14
R14 | 2942 18 14 16 22 --- 10 | 14 21 34 25 --- 17
R15 | 6212 23 10 18 19 263 10 | 22 27 37 30 24 24
R17 | 1310 30 17 31 29 --- 15 | 57 51 53 66 --- 52
R18 | 961 44 13 37 28 --- 18 | 80 59 43 74 --- 61
R19 | 1090 25 19 33 27 --- 15 | 68 47 39 60 --- 51
R20 | 1551 31 23 22 45 --- 17 | 42 30 52 45 --- 38
R21 | 1163 48 22 25 20 --- 17 | 61 29 25 37 --- 30
R23 | 1557 26 17 30 40 --- 16 | 63 75 84 94 --- 76
------+------------------------------------+--------------------------------
RMS | 2509 28 19 29 29 275 |T 41 49 37 41 32 39
WRMS | 2509 24 17 24 29 275 |NE 41 49 37 41 32 39
MEDI | 1677 25 15 26 27 263 |MD 33 31 32 32 36 27
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