[IGSREPORT-18327] Wk 1570 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Feb 25 06:42:31 PST 2010
******************************************************************************
IGS Electronic Report 25 Feb 06:42:55 PST 2010 Message Number 18327
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1570 (Feb 07, 2010 - Feb 13, 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 2.1570.
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:
igl1570[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1570 in the SP3 format.
igl15707.sum Combination Report for GPS Week 1570.
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 | 336.2 ns
1 | 361.9 ns
2 | 442.0 ns
3 | 391.9 ns
4 | 552.4 ns
5 | 488.4 ns
6 | 471.8 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 1.1570, 1a.1570).
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 2.1570.0-6)
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 3.1570.0-6).
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 1570 summary. (Feb 07, 2010 - Feb 13, 2010)
Table 1.1570.a GPS week : 1570 MJD: 55234.0-55240.0
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 129| 0 2 -1 0 -15 24 -.12 25 24 | 0 -248 2312 2524
| 0 1 5 12 34 161 .03 | 0 720
cod 241| -1 -1 -2 40 -23 26 -.14 20 17 | --- --- --- ---
| 1 0 3 11 20 57 .03 | --- ---
esx 133| 0 0 -5 -16 60 -23 .43 26 23 | 81896 303 4839 10052
| 1 2 4 33 34 65 .05 | 75416 5173
iac n/a| 1 2 10 -33 -1 -18 -.11 25 25 | 434588 332 4845 9911
| 1 2 7 23 18 38 .02 | 76484 1490
mcc n/a| 12 -3 74 20 78 -291 -.88 215 215 | --- --- --- ---
| 15 13 26 151 150 328 .60 | --- ---
Table 1.1570.b GPS week : 1570 MJD: 55234.0-55240.0
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 | 13 12 12 13 13 16 15 |
R02 | 11 16 9 14 12 10 8 |
R03 | 13 16 12 10 10 11 13 |
R04 | 14 13 10 13 11 16 25 |
R05 | 14 15 14 18 12 12 12 |
R07 | 13 11 11 13 10 9 11 |
R08 | 17 10 10 15 12 13 15 |
R10 | 9 13 15 13 12 14 12 |
R11 | 18 14 10 17 16 13 14 |
R13 | 12 13 11 9 11 10 14 |
R14 | 11 8 7 8 9 15 13 |
R15 | 19 12 12 8 12 14 13 |
R17 | 13 11 14 17 19 26 16 |
R18 | 9 11 8 10 17 19 10 |
R19 | 16 12 14 13 15 16 14 |
R20 | 16 16 11 17 18 22 19 |
R21 | 9 9 12 11 23 31 14 |
R23 | 16 19 15 14 16 16 14 |
Table 1.1570.c GPS week : 1570 MJD: 55234.0-55240.0
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 1570 0 | -48 -3 -17 1123 340 -14930 88.5 2170 2170 | 336200 0
brd 1570 1 | 96 -141 30 1903 -1659 -16470 89.3 2296 2296 | 361874 0
brd 1570 2 | 124 68 -44 -1179 -1185 -6072 89.0 1985 1985 | 442009 0
brd 1570 3 | 3 -63 34 -1904 -1716 -5242 86.7 1923 1923 | 391935 0
brd 1570 4 | 52 123 -2 -3265 3387 -8769 86.8 2127 2127 | 552373 0
brd 1570 5 | 113 21 64 792 3823 -13220 86.6 2457 2457 | 488368 0
brd 1570 6 | 13 4 159 1180 853 -16280 87.5 2477 2477 | 471758 0
-------------+------------------------------------------------------------+----------------
brd 1570 mean| 50 1 31 -192 549 -11569 87.8 2204 2204 | 434931 0
brd 1570 sdev| 64 85 66 1928 2306 4801 1.1 216 216 | 76363 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 2.1570.0 GPS week: 1570 Day: 0 MJD: 55234
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 129| 0 4 -1 -12 41 146 -.10 27 27 | 0 -981 2559 2955
cod 241| -3 -1 -7 19 -30 -32 -.17 19 18 | --- --- --- ---
esx 133| 2 0 -5 11 52 -54 .51 26 23 | -16215 -1227 4929 8492
iac n/a| 0 1 14 -43 12 -34 -.12 24 24 | 337636 -1955 4943 8940
mcc n/a| 12 -20 95 196 34 4 -.31 133 133 | --- --- --- ---
Table 2.1570.1 GPS week: 1570 Day: 1 MJD: 55235
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 129| 0 1 2 20 -32 118 -.15 20 20 | 0 -945 2127 2293
cod 241| 0 -1 -4 52 6 -28 -.13 19 17 | --- --- --- ---
esx 133| 0 2 -6 -43 -2 -6 .41 23 23 | 4123 8565 4945 9021
iac n/a| 0 1 14 -34 20 -81 -.11 27 27 | 360054 1896 4933 9026
mcc n/a| 40 11 117 91 242 -636 -1.43 277 277 | --- --- --- ---
Table 2.1570.2 GPS week: 1570 Day: 2 MJD: 55236
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 129| 0 0 -3 12 -47 -151 -.13 18 18 | 0 817 2638 2860
cod 241| 1 -1 -4 46 -12 92 -.10 16 15 | --- --- --- ---
esx 133| -1 1 -5 -40 86 27 .37 20 20 | 102948 -4466 5314 9042
iac n/a| 1 1 19 -46 -6 16 -.13 26 26 | 444181 -231 5340 8951
mcc n/a| 0 0 81 123 -67 -85 -1.36 191 191 | --- --- --- ---
Table 2.1570.3 GPS week: 1570 Day: 3 MJD: 55237
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 129| 0 0 -4 -1 -46 286 -.09 23 23 | 0 259 2502 2721
cod 241| -1 0 -2 39 -17 -24 -.12 18 19 | --- --- --- ---
esx 133| 2 0 -6 8 43 -157 .36 25 21 | 46260 -6638 5118 12780
iac n/a| 0 -1 15 -57 -11 -37 -.09 25 25 | 388723 1373 5111 13099
mcc n/a| 4 -13 53 40 -98 -768 -1.30 279 279 | --- --- --- ---
Table 2.1570.4 GPS week: 1570 Day: 4 MJD: 55238
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 129| 0 2 7 -12 24 -34 -.09 25 23 | 0 -690 2790 3025
cod 241| 0 -2 -1 33 -54 11 -.13 18 13 | --- --- --- ---
esx 133| 0 0 -13 -55 84 10 .46 29 27 | 200036 4635 4662 11759
iac n/a| 0 1 9 14 4 33 -.08 27 27 | 551770 2031 4671 11346
mcc n/a| 2 -10 41 -266 259 -470 .05 206 206 | --- --- --- ---
Table 2.1570.5 GPS week: 1570 Day: 5 MJD: 55239
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 129| 0 2 -2 -7 -27 -86 -.09 32 27 | 0 -581 1890 1999
cod 241| -3 0 2 53 -39 91 -.16 25 20 | --- --- --- ---
esx 133| 0 -3 1 33 59 -15 .44 32 27 | 127145 861 4809 9398
iac n/a| 2 4 -1 -46 6 0 -.14 24 24 | 487464 3 4827 8661
mcc n/a| 0 14 73 31 -13 43 -.55 179 179 | --- --- --- ---
Table 2.1570.6 GPS week: 1570 Day: 6 MJD: 55240
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 129| 0 1 -7 5 -20 -110 -.18 28 27 | 0 381 1682 1819
cod 241| -2 0 2 38 -13 72 -.17 23 17 | --- --- --- ---
esx 133| 2 -5 0 -27 98 32 .47 25 24 | 108978 396 4099 9873
iac n/a| 4 5 2 -24 -35 -26 -.12 23 23 | 472289 -791 4090 9354
mcc n/a| 25 -8 56 -72 189 -128 -1.24 242 242 | --- --- --- ---
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 3.1570.0 GPS week: 1570 Day: 0 MJD: 55234
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1357 26 8 32 19 --- 12 | 36 39 48 31 --- 34
R02 | 2251 14 19 21 22 --- 11 | 26 36 41 24 --- 28
R03 | 868 19 16 23 27 --- 12 | 28 27 33 33 --- 22
R04 | 1101 32 27 13 15 --- 13 | 36 39 43 37 --- 36
R05 | 1155 21 28 17 23 --- 13 | 41 57 42 30 --- 39
R07 | 1431 21 20 29 20 --- 13 | 42 43 32 28 --- 32
R08 | 1574 25 27 41 24 122 17 | 46 36 50 33 60 35
R10 | 4047 20 11 14 14 --- 8 | 22 32 37 40 --- 31
R11 | 780 42 16 33 31 93 18 | 26 30 44 31 60 19
R13 | 873 23 21 23 17 --- 12 | 28 16 36 28 --- 21
R14 | 2194 24 14 20 16 --- 10 | 21 15 29 19 --- 15
R15 | 5380 49 15 32 28 171 18 | 37 29 42 38 92 27
R17 | 2571 21 17 19 28 --- 12 | 37 48 56 59 --- 48
R18 | 1258 14 11 18 19 --- 9 | 37 41 48 46 --- 41
R19 | 2028 26 25 28 29 --- 15 | 30 30 37 29 --- 26
R20 | 1493 29 20 37 25 --- 16 | 27 23 42 27 --- 25
R21 | 1204 15 12 15 18 --- 8 | 56 59 60 57 --- 57
R23 | 1591 29 17 25 37 --- 16 | 62 72 85 94 --- 76
------+------------------------------------+--------------------------------
RMS | 2170 27 19 26 24 133 |T 35 37 44 38 70 34
WRMS | 2170 27 18 23 24 133 |NE 32 32 39 30 70 27
MEDI | 1431 23 17 23 22 122 |MD 36 36 42 31 60 31
Table 3.1570.1 GPS week: 1570 Day: 1 MJD: 55235
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1189 14 20 16 31 --- 12 | 25 34 36 21 --- 26
R02 | 1447 14 18 30 44 --- 15 | 20 28 30 33 --- 19
R03 | 1413 15 33 29 28 --- 15 | 22 35 35 20 --- 17
R04 | 1271 28 25 12 16 --- 12 | 31 40 42 32 --- 30
R05 | 924 17 29 21 33 --- 14 | 44 40 28 35 --- 33
R07 | 2743 21 12 22 16 --- 10 | 31 20 22 24 --- 19
R08 | 2534 9 11 22 24 198 9 | 31 29 50 34 47 33
R10 | 3104 23 21 18 25 --- 12 | 28 27 31 43 --- 27
R11 | 828 27 13 26 26 91 13 | 28 15 36 26 83 20
R13 | 942 25 16 28 16 --- 13 | 26 13 33 26 --- 19
R14 | 3777 9 10 17 18 --- 8 | 13 18 26 24 --- 16
R15 | 3736 20 11 24 27 428 12 | 33 28 42 40 228 31
R17 | 1227 21 12 17 28 --- 11 | 18 32 35 43 --- 29
R18 | 1401 18 14 18 25 --- 11 | 28 28 31 24 --- 25
R19 | 1738 11 19 19 33 --- 12 | 26 33 45 20 --- 27
R20 | 2474 27 18 35 26 --- 15 | 22 22 31 20 --- 18
R21 | 2825 15 10 18 17 --- 9 | 54 45 56 46 --- 48
R23 | 3592 33 29 27 40 --- 18 | 47 56 62 72 --- 54
------+------------------------------------+--------------------------------
RMS | 2296 20 19 23 27 277 |T 29 30 37 32 119 27
WRMS | 2296 20 17 23 27 277 |NE 27 26 33 29 119 23
MEDI | 1447 18 16 21 26 198 |MD 28 28 35 26 83 26
Table 3.1570.2 GPS week: 1570 Day: 2 MJD: 55236
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 974 20 14 20 30 --- 12 | 33 37 40 26 --- 31
R02 | 1570 8 16 17 19 --- 9 | 25 27 30 21 --- 20
R03 | 1170 17 22 20 26 --- 12 | 33 40 31 28 --- 27
R04 | 2030 10 14 20 22 --- 9 | 31 30 38 27 --- 28
R05 | 1421 31 19 22 24 --- 14 | 40 37 40 21 --- 26
R07 | 2287 18 17 17 21 --- 10 | 30 30 35 32 --- 25
R08 | 1622 13 18 19 21 200 10 | 38 33 26 29 99 27
R10 | 3596 25 16 29 33 --- 14 | 45 28 45 53 --- 35
R11 | 1584 16 12 18 18 182 9 | 20 16 26 28 64 14
R13 | 1054 17 9 11 33 --- 10 | 28 21 26 21 --- 18
R14 | 1520 7 8 16 17 --- 7 | 28 18 34 15 --- 21
R15 | 1800 15 21 23 19 --- 11 | 33 15 31 41 --- 25
R17 | 853 23 16 18 39 --- 14 | 45 34 44 36 --- 33
R18 | 1375 11 12 14 17 --- 7 | 37 29 42 38 --- 33
R19 | 2066 13 31 19 24 --- 13 | 27 38 30 30 --- 24
R20 | 3921 22 10 14 28 --- 10 | 21 19 24 26 --- 14
R21 | 1930 15 14 24 29 --- 12 | 34 47 60 39 --- 41
R23 | 2003 28 13 24 38 --- 14 | 46 59 74 83 --- 60
------+------------------------------------+--------------------------------
RMS | 1984 18 16 20 26 191 |T 33 31 37 33 81 27
WRMS | 1984 18 15 20 26 191 |NE 32 27 33 28 81 24
MEDI | 1584 16 14 19 24 182 |MD 33 30 34 28 64 26
Table 3.1570.3 GPS week: 1570 Day: 3 MJD: 55237
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 904 29 13 19 28 --- 13 | 25 42 39 45 --- 35
R02 | 1538 27 15 27 25 --- 13 | 50 47 58 41 --- 44
R03 | 1438 16 19 18 15 --- 10 | 37 47 32 27 --- 33
R04 | 2434 21 16 21 31 --- 13 | 28 48 42 38 --- 32
R05 | 938 32 24 44 17 --- 17 | 34 36 70 42 --- 36
R07 | 1520 22 19 21 30 --- 13 | 26 37 33 44 --- 28
R08 | 755 24 20 32 24 200 14 | 33 42 35 45 140 32
R10 | 4538 28 17 17 23 --- 12 | 19 26 34 24 --- 20
R11 | 2948 22 24 43 20 348 16 | 17 30 64 32 163 27
R13 | 1873 14 6 21 20 --- 9 | 44 35 45 29 --- 34
R14 | 1322 14 12 10 18 --- 8 | 21 21 19 18 --- 15
R15 | 1529 14 9 12 18 270 7 | 12 30 29 42 219 25
R17 | 988 29 33 20 33 --- 17 | 42 35 56 59 --- 40
R18 | 1225 16 16 11 25 --- 10 | 42 52 50 47 --- 46
R19 | 1044 14 25 17 26 --- 12 | 23 35 50 33 --- 31
R20 | 2617 29 20 35 31 --- 16 | 25 23 32 27 --- 19
R21 | 1574 23 11 23 17 --- 11 | 61 60 81 58 --- 63
R23 | 1346 29 13 25 29 --- 14 | 52 69 84 85 --- 70
------+------------------------------------+--------------------------------
RMS | 1922 23 18 25 25 279 |T 32 39 47 40 174 35
WRMS | 1922 23 19 21 25 279 |NE 28 35 41 35 174 29
MEDI | 1438 22 16 21 24 270 |MD 28 36 42 41 163 32
Table 3.1570.4 GPS week: 1570 Day: 4 MJD: 55238
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 840 25 9 36 13 --- 12 | 46 49 78 49 --- 51
R02 | 1787 28 12 22 15 --- 11 | 51 39 33 32 --- 36
R03 | 964 14 15 21 16 --- 9 | 30 44 49 39 --- 39
R04 | 1803 15 13 19 26 --- 10 | 29 49 49 24 --- 35
R05 | 1215 16 11 24 30 --- 11 | 18 29 38 35 --- 23
R07 | 2016 20 13 20 19 --- 10 | 24 33 45 19 --- 27
R08 | 1273 24 19 14 20 199 11 | 25 41 45 31 46 31
R10 | 2364 19 13 23 27 --- 11 | 25 27 42 24 --- 25
R11 | 3189 17 20 46 21 216 15 | 14 16 55 22 56 13
R13 | 1631 17 9 28 23 --- 11 | 15 23 29 24 --- 17
R14 | 2197 18 11 15 19 --- 9 | 15 29 35 29 --- 22
R15 | 3564 17 9 28 28 204 12 | 11 20 30 20 59 16
R17 | 1525 29 32 31 40 --- 19 | 31 53 55 64 --- 41
R18 | 889 36 25 24 27 --- 16 | 37 64 54 46 --- 45
R19 | 566 34 11 33 23 --- 14 | 54 47 48 40 --- 42
R20 | 2494 24 18 33 46 --- 17 | 37 35 44 36 --- 32
R21 | 890 48 28 46 42 --- 23 | 59 110 128 97 --- 92
R23 | 4443 26 23 33 32 --- 16 | 66 77 82 91 --- 75
------+------------------------------------+--------------------------------
RMS | 2126 25 18 29 27 206 |T 32 43 52 40 53 36
WRMS | 2126 23 13 27 27 206 |NE 24 31 43 29 53 27
MEDI | 1631 20 13 24 23 204 |MD 29 39 45 32 56 32
Table 3.1570.5 GPS week: 1570 Day: 5 MJD: 55239
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 948 31 31 23 19 --- 15 | 28 55 37 47 --- 39
R02 | 1964 17 15 24 7 --- 9 | 21 35 50 36 --- 33
R03 | 1188 30 13 18 15 --- 11 | 19 34 37 39 --- 29
R04 | 1073 23 39 26 15 --- 16 | 33 23 50 32 --- 30
R05 | 1065 23 17 22 18 --- 11 | 46 38 41 49 --- 39
R07 | 2811 9 13 15 18 --- 8 | 32 34 31 24 --- 26
R08 | 1257 28 20 22 19 243 12 | 44 39 36 30 62 33
R10 | 2168 23 26 22 22 --- 13 | 16 34 24 26 --- 16
R11 | 1342 19 15 28 23 140 12 | 23 18 35 23 86 16
R13 | 1777 18 13 19 17 --- 9 | 28 21 25 27 --- 22
R14 | 1498 21 24 40 18 --- 15 | 14 32 47 21 --- 21
R15 | 7395 18 25 23 28 133 14 | 21 15 40 36 90 25
R17E | 1836 55 27 61 32 --- 25 | 52 80 122 69 --- 72
R18E | 762 36 22 48 19 --- 18 | 54 84 82 66 --- 69
R19E | 787 30 17 26 32 --- 15 | 27 44 52 41 --- 35
R20E | 2287 39 31 33 43 --- 21 | 20 31 44 30 --- 26
R21E | 1146 72 49 53 36 --- 30 | 87 128 136 100 --- 106
R23E | 3607 28 24 32 27 --- 16 | 60 60 80 74 --- 66
------+------------------------------------+--------------------------------
RMS | 2457 32 25 32 24 179 |T 34 44 53 42 79 39
WRMS | 2457 27 20 27 24 179 |NE 26 32 36 32 79 27
MEDI | 1342 23 22 24 19 140 |MD 28 34 41 36 86 30
Table 3.1570.6 GPS week: 1570 Day: 6 MJD: 55240
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 964 30 16 32 22 --- 14 | 46 47 59 41 --- 45
R02 | 2025 17 9 18 11 --- 8 | 29 35 39 33 --- 32
R03 | 1234 36 12 18 18 --- 12 | 31 46 56 47 --- 42
R04M | 2725 37 61 19 37 --- 25 | 35 53 42 42 --- 31
R05 | 1475 23 14 25 16 --- 11 | 33 35 54 44 --- 38
R07 | 4721 19 17 20 17 --- 10 | 45 45 33 30 --- 35
R08 | 1720 44 13 13 25 365 14 | 80 48 44 35 57 46
R10 | 1330 10 17 30 21 --- 12 | 17 22 40 22 --- 20
R11 | 711 15 26 34 17 177 14 | 20 19 49 20 66 18
R13 | 1335 32 11 30 19 --- 13 | 18 11 32 18 --- 13
R14 | 1110 28 15 29 19 --- 13 | 25 35 38 30 --- 28
R15 | 6371 21 21 16 26 108 12 | 29 26 28 24 103 19
R17E | 2260 32 24 28 25 --- 15 | 59 83 73 69 --- 68
R18E | 1511 22 15 15 17 --- 10 | 59 68 77 65 --- 66
R19E | 1021 28 21 26 19 --- 13 | 41 38 33 43 --- 34
R20E | 1652 37 23 31 38 --- 18 | 39 41 32 39 --- 34
R21E | 964 30 23 22 22 --- 14 | 88 97 89 99 --- 92
R23E | 3327 24 17 26 28 --- 14 | 72 74 93 88 --- 80
------+------------------------------------+--------------------------------
RMS | 2477 28 23 25 23 242 |T 42 45 50 43 75 41
WRMS | 2477 27 17 24 23 242 |NE 33 33 42 31 75 30
MEDI | 1475 28 17 25 19 177 |MD 35 41 42 39 66 34
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