[IGSREPORT-17618] Wk 1539 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 23 05:54:31 PDT 2009
******************************************************************************
IGS Electronic Report 23 Jul 05:55:03 PDT 2009 Message Number 17618
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1539 (Jul 05, 2009 - Jul 11, 2009)
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 2.1539.
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:
igl1539[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1539 in the SP3 format.
igl15397.sum Combination Report for GPS Week 1539.
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 | 194.9 ns
1 | 196.2 ns
2 | 201.0 ns
3 | 195.3 ns
4 | 195.9 ns
5 | 191.7 ns
6 | 72.9 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 1.1539, 1a.1539).
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 2.1539.0-6)
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 3.1539.0-6).
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 1539 summary. (Jul 05, 2009 - Jul 11, 2009)
Table 1.1539.a GPS week : 1539 MJD: 55017.0-55023.0
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 107| 2 -1 -13 -2 -15 90 -.10 31 29 | 0 -277 3441 3916
| 2 1 5 22 31 202 .04 | 0 438
cod 235| -4 0 2 5 -6 50 -.12 17 15 | --- --- --- ---
| 2 1 2 17 18 41 .04 | --- ---
esx 129| 2 0 1 41 60 31 .38 29 25 | 89370 -423 5861 10614
| 2 2 6 20 42 73 .04 | 46540 5324
iac n/a| 2 0 5 -20 -23 -196 -.06 27 27 | 178215 -824 5869 10414
| 1 1 6 23 20 71 .04 | 46250 2969
mcc n/a| 0 20 29 -40 23 1454 -.26 3271 3271 | --- --- --- ---
| 25 33 38 210 204 2209 1.81 | --- ---
Table 1.1539.b GPS week : 1539 MJD: 55017.0-55023.0
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
------+------------------------------------+------------------------------------------
R02 | 12 15 12 14 17 17 9 |
R03 | 16 13 15 13 28 27 12 |
R07 | 18 17 13 11 7 9 11 |
R08 | 15 14 14 13 13 15 11 |
R10 | 13 11 15 14 10 22 21 |
R11 | 13 10 10 16 12 12 18 |
R13 | 14 12 11 11 10 11 10 |
R14 | 13 14 13 11 12 9 14 |
R15 | 14 12 18 16 19 15 17 |
R17 | 15 13 17 13 17 18 15 |
R18 | 12 8 11 10 10 12 15 |
R19 | 14 11 7 12 11 8 9 |
R20 | 14 18 16 18 15 18 12 |
R21 | 12 17 14 14 13 12 9 |
R22 | 10 12 12 19 12 12 8 |
R23 | 23 19 20 18 20 18 20 |
R24 | 17 14 13 15 18 23 16 |
Table 1.1539.c GPS week : 1539 MJD: 55017.0-55023.0
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 1539 0 | -51 -25 386 -1543 547 -20280 87.4 2224 2224 | 194947 0
brd 1539 1 | -61 -47 439 -61 1300 -12570 89.8 1882 1882 | 196249 0
brd 1539 2 | 13 -52 305 957 2222 -7686 89.8 1741 1741 | 200958 0
brd 1539 3 | 86 76 397 -576 415 -9095 86.0 1602 1602 | 195303 0
brd 1539 4 | -21 37 385 -370 -63 -12570 87.9 1842 1842 | 195867 0
brd 1539 5 | -3 107 415 -866 792 -16050 87.6 2205 2205 | 191735 0
brd 1539 6 | 26 -2 631 -105 -99 -22550 89.3 2377 2377 | 72886 0
-------------+------------------------------------------------------------+----------------
brd 1539 mean| -1 13 422 -366 730 -14400 88.2 1981 1981 | 178277 0
brd 1539 sdev| 50 62 100 773 816 5532 1.4 287 287 | 46552 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 2.1539.0 GPS week: 1539 Day: 0 MJD: 55017
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 107| 3 -2 -11 22 -58 70 -.18 28 27 | 0 -839 3988 4500
cod 235| 0 1 0 -8 12 61 -.14 17 17 | --- --- --- ---
esx 129| -1 0 -4 58 94 37 .34 28 26 | 107712 -7274 6202 10654
iac n/a| 1 -2 17 -2 -10 -203 -.08 30 30 | 196687 -4038 6221 10724
mcc n/a| 41 40 -33 316 -334 -557 -3.45 >>>> >>>> | --- --- --- ---
Table 2.1539.1 GPS week: 1539 Day: 1 MJD: 55018
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 107| 3 -1 -7 -29 -3 159 -.06 27 24 | 0 334 3167 3549
cod 235| -2 1 4 -14 -2 54 -.11 14 12 | --- --- --- ---
esx 129| 0 0 3 57 120 -9 .45 30 27 | 110790 4404 4419 10728
iac n/a| 2 0 0 -4 -26 -297 .01 29 29 | 194821 1951 4427 9974
mcc n/a| 7 76 22 -48 -58 316 .54 502 502 | --- --- --- ---
Table 2.1539.2 GPS week: 1539 Day: 2 MJD: 55019
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 107| 3 0 -19 -5 -18 414 -.11 33 33 | 0 -102 3220 3695
cod 235| -3 0 3 -2 -1 3 -.11 13 12 | --- --- --- ---
esx 129| 2 -3 6 69 11 -68 .40 28 25 | 110973 -4384 6289 10428
iac n/a| 2 0 0 -7 -24 -292 -.10 29 29 | 201966 -3260 6311 10547
mcc n/a| -28 29 65 52 87 3853 1.43 361 361 | --- --- --- ---
Table 2.1539.3 GPS week: 1539 Day: 3 MJD: 55020
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 107| -2 -2 -14 26 -42 55 -.11 36 35 | 0 -113 2623 3029
cod 235| -6 1 1 0 -26 56 -.14 17 16 | --- --- --- ---
esx 129| 5 -1 0 14 83 47 .37 24 22 | 102500 3165 5473 10055
iac n/a| 3 0 4 -1 -27 -166 -.12 24 24 | 195233 1162 5476 10223
mcc n/a| -28 31 85 -333 166 5321 -2.07 366 366 | --- --- --- ---
Table 2.1539.4 GPS week: 1539 Day: 4 MJD: 55021
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 107| 4 0 -9 8 37 -256 -.06 35 29 | 0 -830 3768 4162
cod 235| -4 0 2 30 -33 122 -.19 16 14 | --- --- --- ---
esx 129| 3 -2 -5 26 7 148 .41 27 25 | 110642 -5563 6947 11348
iac n/a| 1 0 10 -23 12 -145 -.03 29 29 | 196128 -4250 6931 10894
mcc n/a| 16 1 30 -245 316 446 1.08 438 438 | --- --- --- ---
Table 2.1539.5 GPS week: 1539 Day: 5 MJD: 55022
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 107| 0 0 -21 -11 2 14 -.07 33 29 | 0 -403 3554 4037
cod 235| -3 -1 -1 6 16 55 -.06 20 17 | --- --- --- ---
esx 129| 2 0 12 33 43 92 .36 34 30 | 98600 6216 6629 10891
iac n/a| 0 0 5 -45 -51 -137 -.04 25 25 | 188988 2738 6666 10769
mcc n/a| -9 -14 12 -4 31 360 .02 553 553 | --- --- --- ---
Table 2.1539.6 GPS week: 1539 Day: 6 MJD: 55023
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 107| 1 0 -11 -29 -22 178 -.10 24 24 | 0 12 3772 4444
cod 235| -7 -1 4 28 -10 -3 -.08 18 15 | --- --- --- ---
esx 129| 3 3 0 26 60 -24 .36 28 22 | -15625 473 5068 10196
iac n/a| 4 1 2 -61 -40 -132 -.04 25 25 | 73683 -77 5056 9771
mcc n/a| -2 -18 20 -19 -42 443 .64 456 456 | --- --- --- ---
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 3.1539.0 GPS week: 1539 Day: 0 MJD: 55017
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2438 21 12 25 27 --- 12 | 41 51 60 49 --- 49
R03E | 4447 28 10 33 37 --- 15 | 49 56 76 67 --- 58
R07E | 4119 39 24 33 25 --- 17 | 54 55 57 65 --- 55
R08E | 1947 18 22 24 35 652 14 | 26 37 33 36 238 27
R10 | 3042 19 20 31 18 --- 13 | 28 27 40 29 --- 23
R11 | 1130 14 17 39 14 >>>> 13 | 31 28 37 30 9999 26
R13 | 1430 29 19 28 20 --- 14 | 26 38 41 41 --- 33
R14 | 2496 17 22 21 30 --- 13 | 35 33 33 41 --- 29
R15 | 1227 30 12 25 28 118 13 | 23 32 43 29 33 26
R17 | 637 28 9 26 40 --- 14 | 49 57 63 28 --- 49
R18 | 1076 16 17 18 29 --- 11 | 28 37 35 33 --- 30
R19 | 1279 32 16 19 26 --- 13 | 38 59 64 39 --- 49
R20 | 2800 35 14 20 29 --- 14 | 41 41 38 44 --- 34
R21 | 1410 28 10 22 24 --- 12 | 26 42 53 50 --- 39
R22 | 792 17 10 25 19 --- 10 | 32 35 36 43 --- 32
R23 | 1425 38 29 39 52 --- 22 | 46 51 53 42 --- 40
R24 | 1257 42 12 31 32 --- 17 | 219 195 186 201 --- 199
------+------------------------------------+--------------------------------
RMS | 2223 28 17 28 30 >>>> |T 46 51 55 51 135 46
WRMS | 2223 26 17 26 30 >>>> |NE 47 51 55 50 33 46
MEDI | 1425 28 16 25 28 652 |MD 35 41 43 41 33 34
Table 3.1539.1 GPS week: 1539 Day: 1 MJD: 55018
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2438 15 11 31 46 --- 15 | 32 33 46 35 --- 30
R03E | 2289 17 12 34 28 --- 12 | 38 41 55 53 --- 41
R07E | 2930 44 21 32 24 --- 17 | 45 58 68 54 --- 52
R08E | 1679 28 18 26 27 641 13 | 37 37 38 34 137 31
R10 | 3659 12 10 24 32 --- 11 | 43 25 44 25 --- 25
R11 | 1535 15 14 23 15 562 9 | 35 26 40 33 9999 29
R13 | 1286 28 14 21 19 --- 11 | 18 24 32 27 --- 20
R14 | 2196 18 17 36 25 --- 13 | 27 32 31 37 --- 22
R15 | 1490 26 11 17 30 165 12 | 28 23 33 21 34 20
R17 | 882 20 18 23 32 --- 13 | 35 43 42 24 --- 35
R18 | 795 12 8 22 13 --- 8 | 28 30 37 31 --- 28
R19 | 1240 27 9 13 28 --- 11 | 23 33 30 25 --- 26
R20 | 2672 23 17 32 52 --- 17 | 47 47 54 67 --- 45
R21 | 1314 43 14 38 29 --- 17 | 31 44 67 47 --- 40
R22 | 489 28 8 27 18 --- 11 | 23 34 53 30 --- 30
R23 | 688 25 17 56 35 --- 18 | 28 29 61 49 --- 27
R24 | 803 40 12 23 16 --- 13 | 149 158 170 156 --- 158
------+------------------------------------+--------------------------------
RMS | 1882 27 14 30 29 501 |T 39 42 53 44 85 38
WRMS | 1882 24 12 27 29 501 |NE 39 42 53 44 34 38
MEDI | 1490 25 14 26 28 562 |MD 32 33 44 34 34 30
Table 3.1539.2 GPS week: 1539 Day: 2 MJD: 55019
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2159 22 12 22 30 --- 12 | 40 41 44 33 --- 36
R03E | 1955 31 14 32 34 --- 15 | 60 60 74 60 --- 60
R07 | 2274 36 13 29 17 --- 13 | 61 83 96 68 --- 75
R08E | 1002 36 16 22 29 470 14 | 23 32 41 34 230 27
R10 | 4085 28 20 16 40 --- 15 | 39 44 44 36 --- 35
R11 | 1251 23 10 17 24 236 10 | 34 25 31 30 9999 24
R13 | 1082 22 11 23 26 --- 11 | 26 24 36 26 --- 23
R14 | 2439 34 12 28 23 --- 13 | 30 31 47 33 --- 30
R15 | 853 61 10 29 23 337 17 | 36 26 34 22 28 21
R17 | 979 41 16 20 44 --- 16 | 54 48 37 15 --- 39
R18 | 1133 33 11 20 15 --- 11 | 32 27 33 14 --- 20
R19 | 1150 20 7 12 14 --- 7 | 28 25 25 22 --- 21
R20 | 1739 28 13 33 41 --- 16 | 38 30 60 46 --- 34
R21 | 1250 25 17 33 21 --- 13 | 41 39 57 47 --- 39
R22 | 738 28 5 26 24 --- 11 | 30 26 48 32 --- 27
R23 | 960 39 17 57 27 --- 20 | 40 28 57 26 --- 17
R24 | 1058 26 10 23 36 --- 13 | 80 66 70 68 --- 67
------+------------------------------------+--------------------------------
RMS | 1740 33 13 28 29 361 |T 40 38 49 36 129 35
WRMS | 1740 33 12 25 29 361 |NE 39 33 44 32 28 30
MEDI | 1150 28 12 23 26 337 |MD 38 31 44 33 28 30
Table 3.1539.3 GPS week: 1539 Day: 3 MJD: 55020
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1603 33 16 28 22 --- 14 | 48 56 61 51 --- 49
R03E | 3367 37 14 20 18 --- 12 | 54 69 76 65 --- 65
R07 | 2760 31 11 13 24 --- 11 | 62 62 68 60 --- 62
R08E | 829 26 13 25 25 469 12 | 51 54 64 47 395 50
R10 | 2070 42 18 26 14 --- 14 | 34 29 34 19 --- 19
R11 | 1208 25 17 28 37 141 15 | 30 41 58 53 9999 42
R13 | 982 32 8 17 17 --- 10 | 25 33 45 37 --- 33
R14 | 1821 27 15 16 18 --- 10 | 36 38 41 39 --- 36
R15 | 1199 44 18 20 33 402 16 | 33 35 41 36 63 32
R17 | 925 35 12 15 29 --- 13 | 42 43 52 29 --- 39
R18 | 1048 29 11 21 9 --- 10 | 35 35 35 29 --- 30
R19 | 996 34 11 23 16 --- 11 | 23 34 47 25 --- 30
R20 | 973 50 18 36 18 --- 17 | 68 43 56 39 --- 43
R21 | 1115 40 18 22 22 --- 14 | 50 59 62 46 --- 50
R22 | 1105 42 33 32 26 --- 19 | 42 43 52 49 --- 34
R23 | 1212 32 28 25 37 --- 17 | 43 39 31 26 --- 27
R24 | 1451 41 13 29 22 --- 14 | 118 140 162 137 --- 140
------+------------------------------------+--------------------------------
RMS | 1601 36 17 24 24 366 |T 46 50 57 46 229 45
WRMS | 1601 35 16 22 24 366 |NE 44 47 55 43 63 42
MEDI | 1199 34 15 23 22 402 |MD 42 43 52 39 63 39
Table 3.1539.4 GPS week: 1539 Day: 4 MJD: 55021
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1996 29 23 31 36 --- 17 | 38 64 65 47 --- 48
R03E | 3208 79 29 51 40 --- 28 | 90 103 123 110 --- 98
R07 | 3215 12 8 14 17 --- 7 | 59 59 57 66 --- 58
R08E | 1214 20 11 27 29 739 12 | 25 42 58 40 403 38
R10 | 1981 15 14 16 21 --- 9 | 42 34 44 27 --- 33
R11 | 871 20 17 19 26 82 11 | 32 33 44 40 9999 32
R13 | 1228 14 15 15 23 --- 10 | 30 24 25 27 --- 21
R14 | 1654 27 15 23 17 --- 11 | 35 35 33 25 --- 26
R15 | 943 44 13 31 44 149 18 | 31 23 50 39 42 26
R17 | 917 41 16 43 20 --- 17 | 41 45 69 52 --- 48
R18 | 1304 14 10 23 20 --- 9 | 34 29 29 32 --- 25
R19 | 650 16 11 23 23 --- 10 | 37 34 27 25 --- 26
R20 | 703 31 18 27 28 --- 14 | 25 35 22 37 --- 23
R21 | 1108 29 13 27 19 --- 12 | 50 44 61 48 --- 44
R22 | 884 27 9 17 29 --- 11 | 37 35 39 45 --- 32
R23 | 1811 32 24 29 51 --- 19 | 43 34 35 38 --- 29
R24 | 3608 61 17 23 19 --- 18 | 81 95 90 93 --- 83
------+------------------------------------+--------------------------------
RMS | 1842 35 16 27 29 438 |T 42 45 51 46 222 40
WRMS | 1842 29 14 25 29 438 |NE 39 38 43 40 42 34
MEDI | 1228 27 15 23 23 149 |MD 37 35 44 40 42 32
Table 3.1539.5 GPS week: 1539 Day: 5 MJD: 55022
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 3064 27 21 41 31 --- 17 | 54 74 83 55 --- 62
R03 | 1987 66 39 51 31 --- 26 | 84 139 160 108 --- 119
R07 | 2996 20 10 15 17 --- 9 | 53 46 41 54 --- 46
R08 | 761 32 18 25 27 944 14 | 44 44 62 38 340 42
R10 | 2040 28 30 60 29 --- 21 | 17 36 50 29 --- 19
R11 | 2905 11 18 30 18 83 11 | 22 26 44 25 9999 23
R13 | 2793 18 19 13 22 --- 11 | 21 29 29 31 --- 24
R14 | 4102 21 12 16 12 --- 8 | 26 27 29 34 --- 25
R15 | 1186 41 12 22 28 139 15 | 18 17 33 28 27 17
R17 | 797 43 16 38 31 --- 18 | 28 28 40 28 --- 26
R18 | 1741 31 11 25 17 --- 12 | 24 26 46 40 --- 28
R19 | 582 14 14 15 11 --- 7 | 29 28 36 28 --- 28
R20 | 975 44 20 34 25 --- 17 | 45 39 49 42 --- 36
R21 | 805 19 17 27 20 --- 12 | 39 48 39 24 --- 35
R22 | 544 19 14 33 13 --- 11 | 46 36 60 36 --- 39
R23 | 1614 24 23 29 41 --- 17 | 22 39 43 39 --- 32
R24 | 3547 51 17 58 33 --- 22 | 66 77 87 75 --- 69
------+------------------------------------+--------------------------------
RMS | 2204 33 20 34 25 553 |T 37 44 54 42 183 39
WRMS | 2204 29 17 30 25 553 |NE 31 35 45 35 27 30
MEDI | 1741 27 17 29 25 139 |MD 29 36 44 36 27 32
Table 3.1539.6 GPS week: 1539 Day: 6 MJD: 55023
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3355 14 10 13 20 --- 8 | 51 60 59 52 --- 55
R03 | 2991 16 16 19 29 --- 12 | 55 62 72 68 --- 62
R07 | 1632 21 12 28 15 --- 11 | 55 61 66 63 --- 59
R08 | 2174 15 12 16 26 768 10 | 39 34 39 34 219 32
R10 | 3096 27 29 55 28 --- 20 | 25 35 64 28 --- 33
R11 | 3574 33 15 47 26 111 17 | 28 26 42 30 9999 24
R13 | 3201 15 16 15 18 --- 9 | 21 28 32 31 --- 23
R14 | 3436 17 15 30 29 --- 13 | 33 33 49 30 --- 31
R15 | 1709 42 21 24 29 149 17 | 31 25 39 32 30 24
R17 | 866 31 10 22 37 --- 15 | 36 48 53 41 --- 43
R18 | 1193 11 28 38 16 --- 14 | 18 36 50 34 --- 28
R19 | 1089 18 13 19 14 --- 9 | 30 37 37 30 --- 31
R20 | 1960 28 12 21 23 --- 12 | 22 25 39 44 --- 27
R21 | 630 20 15 13 11 --- 9 | 42 43 46 40 --- 39
R22 | 1130 18 8 16 11 --- 8 | 38 30 38 36 --- 31
R23 | 1254 21 29 40 45 --- 20 | 32 36 37 37 --- 30
R24 | 3258 36 26 21 20 --- 15 | 79 81 76 88 --- 80
------+------------------------------------+--------------------------------
RMS | 2376 24 18 28 25 456 |T 37 41 49 42 124 38
WRMS | 2376 24 15 22 25 456 |NE 33 37 46 38 30 34
MEDI | 1960 20 15 21 23 149 |MD 33 36 46 36 30 31
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