[IGSREPORT-18011] Wk 1556 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Nov 19 06:17:29 PST 2009
******************************************************************************
IGS Electronic Report 19 Nov 06:17:52 PST 2009 Message Number 18011
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1556 (Nov 01, 2009 - Nov 07, 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 2.1556.
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:
igl1556[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1556 in the SP3 format.
igl15567.sum Combination Report for GPS Week 1556.
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 | 506.1 ns
1 | 492.4 ns
2 | 414.2 ns
3 | 405.2 ns
4 | 502.1 ns
5 | 432.7 ns
6 | 503.6 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 | COD | R24
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 1.1556, 1a.1556).
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 2.1556.0-6)
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 3.1556.0-6).
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 1556 summary. (Nov 01, 2009 - Nov 07, 2009)
Table 1.1556.a GPS week : 1556 MJD: 55136.0-55142.0
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 110| 0 0 2 -8 -25 -25 -.19 30 28 | 0 -195 3208 3535
| 1 2 4 36 62 152 .06 | 0 1041
cod 232| -1 0 -9 18 1 77 -.16 27 15 | --- --- --- ---
| 1 0 1 20 33 28 .03 | --- ---
esx 127| 0 0 -2 0 12 -9 .38 25 24 | 112013 -2384 4908 10260
| 2 1 4 22 35 77 .04 | 48128 6620
iac n/a| 1 1 19 -55 -22 -105 -.00 34 34 | 462595 1161 4908 9479
| 2 1 6 37 32 63 .07 | 43545 3654
mcc n/a| 0 5 11 21 -65 387 .16 168 168 | --- --- --- ---
| 7 10 16 162 182 487 .37 | --- ---
Table 1.1556.b GPS week : 1556 MJD: 55136.0-55142.0
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 12 12 11 11 7 11 |
R03 | 14 13 11 14 10 11 10 |
R07 | 12 10 10 12 9 10 10 |
R08 | 11 14 11 10 8 8 11 |
R10 | 21 16 17 18 19 27 33 |
R11 | 22 21 20 23 24 23 19 |
R13 | 16 14 18 20 20 19 24 |
R14 | 16 15 17 15 19 24 25 |
R15 | 20 18 20 16 14 17 20 |
R17 | 15 10 15 14 12 11 12 |
R18 | 14 10 13 10 9 14 10 |
R19 | 12 10 9 11 13 16 11 |
R20 | 16 16 15 10 13 12 15 |
R21 | 17 9 12 9 12 16 11 |
R23 | 16 16 11 11 11 15 17 |
R24 | 15 34 --- --- --- --- --- |
Table 1.1556.c GPS week : 1556 MJD: 55136.0-55142.0
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 1556 0 | -7 -8 92 238 1379 -20280 87.0 2072 2072 | 506055 0
brd 1556 1 | 7737 ---- 926 -170000 -16329 505700 48.3 >>>>> >>>>> | 492409 0
brd 1556 2 | 87 -94 234 -413 -1115 -22670 89.6 2841 2841 | 414185 0
brd 1556 3 | 246 25 140 -2468 5 -19980 85.1 2728 2728 | 405181 0
brd 1556 4 | 59 113 246 -1584 134 -14710 86.9 2502 2502 | 502108 0
brd 1556 5 | -12 -17 107 -46 3489 -7889 89.1 2323 2323 | 432668 0
brd 1556 6 | 0 -7 144 -1267 3308 -5695 87.6 2220 2220 | 503583 0
-------------+------------------------------------------------------------+----------------
brd 1556 mean| 1158 -8164 270 -25077 -1304 59210 81.9 >>>>> >>>>> | 465169 0
brd 1556 sdev| 2902 21605 295 63911 6844 196988 14.9 >>>>> >>>>> | 45658 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 2.1556.0 GPS week: 1556 Day: 0 MJD: 55136
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 110| 2 0 0 -43 82 -28 -.24 33 30 | 0 -1047 3602 3937
cod 232| -3 0 -6 31 -51 63 -.14 19 17 | --- --- --- ---
esx 127| 3 0 -5 32 -43 18 .40 26 24 | 158416 103 6916 14234
iac n/a| 3 0 13 -100 13 -130 .05 32 32 | 490971 4346 6907 15053
mcc n/a| 9 -8 -3 114 132 555 .42 69 69 | --- --- --- ---
Table 2.1556.1 GPS week: 1556 Day: 1 MJD: 55137
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 110| 0 2 5 40 -33 83 -.20 32 30 | 0 -901 3253 3505
cod 232| 0 0 -9 9 32 58 -.17 79 11 | --- --- --- ---
esx 127| 1 0 -1 -30 15 -98 .39 23 20 | 153231 8048 6395 9841
iac n/a| 4 3 23 -6 -69 -91 .04 35 35 | 489796 5691 6404 9431
mcc n/a| -2 11 5 -84 -81 -351 -.03 110 110 | --- --- --- ---
Table 2.1556.2 GPS week: 1556 Day: 2 MJD: 55138
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 110| 1 3 -2 -62 -36 -32 -.09 28 27 | 0 -1122 2895 3047
cod 232| -2 0 -12 31 8 92 -.13 14 14 | --- --- --- ---
esx 127| 1 2 7 -15 53 57 .31 29 29 | 72077 -14147 4170 10243
iac n/a| 2 2 21 -82 -57 -181 .05 33 33 | 415003 -3905 4168 9189
mcc n/a| 1 6 21 -101 -24 -246 .06 271 271 | --- --- --- ---
Table 2.1556.3 GPS week: 1556 Day: 3 MJD: 55139
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 110| 1 -3 7 -23 -88 82 -.19 29 27 | 0 1761 3464 3997
cod 232| 0 0 -10 -7 -1 63 -.13 17 14 | --- --- --- ---
esx 127| -2 0 -4 22 37 -33 .35 21 20 | 46807 -1356 4533 9653
iac n/a| 1 1 16 -33 -35 -131 -.07 32 32 | 402997 3249 4550 8383
mcc n/a| -2 21 38 -45 -14 588 .41 340 340 | --- --- --- ---
Table 2.1556.4 GPS week: 1556 Day: 4 MJD: 55140
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 110| 0 1 6 17 -84 -34 -.12 28 25 | 0 454 3446 3947
cod 232| 0 0 -9 -5 43 97 -.16 18 15 | --- --- --- ---
esx 127| -1 0 -2 3 38 -54 .39 21 20 | 148071 -5060 4102 8594
iac n/a| -2 1 16 -21 -13 -142 -.13 35 35 | 502821 -2398 4095 7248
mcc n/a| -11 11 22 352 -453 933 -.56 200 200 | --- --- --- ---
Table 2.1556.5 GPS week: 1556 Day: 5 MJD: 55141
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 110| 1 0 1 17 -50 -344 -.23 32 31 | 0 -550 2734 2999
cod 232| -2 0 -9 47 6 125 -.20 22 16 | --- --- --- ---
esx 127| 0 0 -5 4 10 116 .38 23 22 | 65820 -2931 4463 9472
iac n/a| 1 1 30 -96 -7 14 -.00 40 40 | 434140 -1170 4457 8743
mcc n/a| 7 0 4 -27 -22 679 .45 79 79 | --- --- --- ---
Table 2.1556.6 GPS week: 1556 Day: 6 MJD: 55142
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 110| 0 0 -1 -6 33 95 -.25 32 26 | 0 38 3064 3315
cod 232| -3 1 -8 22 -31 44 -.18 22 17 | --- --- --- ---
esx 127| 0 2 -2 -18 -25 -74 .43 33 32 | 139675 -1345 3781 9787
iac n/a| 0 -2 16 -48 13 -73 .03 33 33 | 502439 2317 3780 8308
mcc n/a| 4 -4 -5 -58 3 553 .38 105 105 | --- --- --- ---
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 3.1556.0 GPS week: 1556 Day: 0 MJD: 55136
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1417 18 12 20 33 --- 12 | 26 33 36 45 --- 30
R03 | 2521 27 20 23 27 --- 14 | 26 42 50 48 --- 37
R07 | 3160 29 18 16 14 --- 11 | 28 33 27 32 --- 25
R08 | 1415 17 17 18 20 67 10 | 23 30 37 38 33 29
R10E | 2756 42 21 29 52 --- 20 | 35 51 61 51 --- 44
R11E | 956 56 24 27 44 88 21 | 180 190 182 191 111 184
R13E | 2685 27 22 24 37 --- 15 | 36 32 40 40 --- 30
R14E | 1732 21 24 27 38 --- 16 | 36 32 46 50 --- 35
R15E | 2829 39 22 33 43 47 19 | 37 34 29 57 58 30
R17 | 1274 29 16 22 35 --- 14 | 51 53 48 35 --- 44
R18 | 1955 28 14 31 24 --- 14 | 35 43 56 38 --- 40
R19 | 1504 16 18 13 32 --- 12 | 44 53 53 45 --- 46
R20 | 3110 49 15 18 19 --- 15 | 51 38 40 38 --- 33
R21 | 970 38 18 41 13 --- 17 | 26 44 77 50 --- 46
R23 | 965 32 23 31 25 --- 16 | 35 46 44 42 --- 36
R24 | 1527 28 17 28 29 --- 14 | 13 46 32 9 --- 23
------+------------------------------------+--------------------------------
RMS | 2071 33 19 26 32 69 |T 42 50 53 50 67 44
WRMS | 2071 30 17 24 32 69 |NE 32 41 45 38 33 35
MEDI | 1527 28 18 24 29 67 |MD 35 42 44 42 58 35
Table 3.1556.1 GPS week: 1556 Day: 1 MJD: 55137
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 27 6 26 22 --- 11 | 28 37 41 40 --- 35
R03 |>>>>> 30 17 22 26 --- 13 | 23 27 26 34 --- 21
R07 |>>>>> 27 13 11 19 --- 10 | 20 27 24 29 --- 21
R08 |>>>>> 29 7 17 42 35 13 | 25 25 38 34 39 24
R10E |45835 27 19 19 46 --- 15 | 31 23 40 44 --- 23
R11E |>>>>> 52 15 29 53 170 20 | 152 150 160 159 54 152
R13E |>>>>> 26 20 18 35 --- 13 | 49 35 37 34 --- 31
R14E |>>>>> 25 18 23 40 --- 14 | 27 42 44 46 --- 35
R15E |>>>>> 40 15 20 49 77 17 | 42 34 36 63 32 36
R17 |>>>>> 12 17 14 22 --- 9 | 27 37 23 16 --- 25
R18 |>>>>> 23 10 11 23 --- 9 | 22 29 26 27 --- 23
R19 |>>>>> 17 8 21 26 --- 10 | 35 28 19 32 --- 24
R20 |>>>>> 27 24 30 35 --- 16 | 32 30 64 46 --- 39
R21 |>>>>> 18 6 19 14 --- 8 | 23 29 38 32 --- 28
R23 |>>>>> 40 15 25 31 --- 15 | 23 52 61 38 --- 42
R24 |>>>>> 55 312 42 48 --- 34 | 14 134 54 6 --- 28
------+------------------------------------+--------------------------------
RMS |>>>>> 32 79 23 35 110 |T 35 46 45 42 41 36
WRMS |>>>>> 30 11 20 35 110 |NE 24 41 37 30 39 28
MEDI |>>>>> 27 15 20 31 77 |MD 27 30 38 34 39 28
Table 3.1556.2 GPS week: 1556 Day: 2 MJD: 55138
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1490 13 9 37 18 --- 11 | 22 23 49 27 --- 24
R03 | 1930 22 11 24 25 --- 11 | 37 34 40 50 --- 34
R07 | 3971 19 13 22 18 --- 10 | 41 33 28 31 --- 29
R08 | 920 23 8 29 16 36 10 | 19 24 44 30 25 25
R10E | 4300 30 19 20 49 --- 16 | 39 37 28 52 --- 33
R11E | 1807 45 12 30 52 456 19 | 90 110 113 120 55 106
R13E | 896 39 16 28 47 --- 17 | 36 42 53 42 --- 37
R14E | 5764 32 16 30 44 --- 16 | 54 50 40 56 --- 44
R15E | 2438 48 19 29 46 107 19 | 27 27 34 46 34 22
R17 | 1226 28 23 31 25 --- 15 | 38 63 31 47 --- 45
R18 | 3470 11 11 37 28 --- 12 | 35 37 55 25 --- 32
R19 | 2950 18 10 22 16 --- 9 | 57 58 54 49 --- 53
R20 | 1390 24 11 35 37 --- 14 | 29 22 33 20 --- 15
R21 | 1154 20 11 35 19 --- 12 | 31 37 45 44 --- 34
R23 | 3355 17 17 23 18 --- 10 | 44 46 45 47 --- 42
------+------------------------------------+--------------------------------
RMS | 2841 28 14 29 33 271 |T 39 42 46 45 38 38
WRMS | 2841 27 14 29 33 271 |NE 35 37 42 37 25 33
MEDI | 1930 23 12 29 25 107 |MD 37 37 44 46 34 34
Table 3.1556.3 GPS week: 1556 Day: 3 MJD: 55139
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1319 20 9 24 20 --- 10 | 41 43 53 48 --- 43
R03 | 3445 36 11 28 20 --- 14 | 30 31 39 32 --- 28
R07 | 5118 18 18 18 26 --- 11 | 39 30 29 22 --- 24
R08 | 1242 22 11 16 18 43 9 | 22 34 38 31 37 30
R10E | 2630 40 23 22 42 --- 18 | 64 49 54 59 --- 48
R11E | 1734 46 19 30 61 574 22 | 191 172 172 177 60 173
R13E | 1796 38 26 23 50 --- 19 | 53 56 48 63 --- 46
R14E | 4623 19 22 22 37 --- 14 | 32 34 47 48 --- 33
R15E | 2939 38 13 20 39 125 15 | 43 41 46 58 36 42
R17 | 1414 37 20 20 17 --- 13 | 28 67 62 50 --- 53
R18 | 865 10 14 16 24 --- 9 | 41 53 53 28 --- 43
R19 | 1252 22 14 22 19 --- 11 | 41 43 66 51 --- 49
R20 | 1718 22 13 16 19 --- 10 | 44 49 57 64 --- 50
R21 | 1096 21 8 13 18 --- 8 | 36 44 40 41 --- 38
R23 | 4318 20 15 22 18 --- 11 | 29 31 40 23 --- 26
------+------------------------------------+--------------------------------
RMS | 2728 29 17 21 32 340 |T 48 51 56 53 44 48
WRMS | 2728 27 14 20 32 340 |NE 35 42 47 39 37 38
MEDI | 1734 22 14 22 20 125 |MD 41 43 48 48 37 43
Table 3.1556.4 GPS week: 1556 Day: 4 MJD: 55140
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1564 30 18 7 16 --- 11 | 26 43 37 41 --- 34
R03 | 3338 23 10 18 22 --- 10 | 38 38 37 46 --- 37
R07 | 3534 16 14 17 16 --- 9 | 30 22 28 26 --- 23
R08 | 591 16 11 14 14 91 8 | 22 20 32 20 59 20
R10E | 1511 44 19 29 41 --- 19 | 34 30 36 49 --- 26
R11E | 882 52 24 33 62 313 24 | 109 130 130 132 119 121
R13E | 1896 27 22 29 58 --- 19 | 18 36 45 53 --- 27
R14E | 3081 25 30 23 55 --- 19 | 34 47 40 46 --- 30
R15E | 4856 26 19 16 34 119 13 | 38 26 34 46 57 29
R17 | 1039 24 19 21 20 --- 12 | 33 53 54 30 --- 41
R18 | 1085 20 9 15 12 --- 8 | 26 49 48 42 --- 42
R19 | 846 27 11 15 34 --- 12 | 48 58 59 70 --- 55
R20 | 1560 14 13 27 32 --- 12 | 36 37 32 54 --- 35
R21 | 1205 30 20 14 11 --- 11 | 36 55 54 47 --- 46
R23 | 4567 15 15 19 28 --- 11 | 39 37 49 45 --- 39
------+------------------------------------+--------------------------------
RMS | 2502 28 18 21 35 200 |T 37 45 47 49 78 40
WRMS | 2502 25 15 20 35 200 |NE 33 41 43 42 59 37
MEDI | 1560 25 18 18 28 119 |MD 34 38 40 46 59 35
Table 3.1556.5 GPS week: 1556 Day: 5 MJD: 55141
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1411 10 11 11 18 --- 7 | 46 30 38 41 --- 36
R03 | 1329 25 15 13 18 --- 10 | 30 29 30 40 --- 28
R07 | 896 24 12 13 18 --- 9 | 41 28 26 24 --- 25
R08 | 481 13 13 11 20 85 8 | 23 29 35 21 41 23
R10E | 1713 74 36 25 46 --- 26 | 63 54 53 43 --- 44
R11E | 645 34 27 30 73 104 23 | 217 202 209 214 126 206
R13E | 1263 23 16 27 63 --- 19 | 56 46 46 70 --- 44
R14E | 3831 30 42 35 58 --- 23 | 37 57 34 61 --- 32
R15E | 6241 34 14 27 45 24 17 | 29 23 26 53 49 21
R17 | 865 20 16 16 28 --- 11 | 44 37 39 28 --- 34
R18 | 1420 38 8 23 25 --- 14 | 31 37 45 48 --- 36
R19 | 989 30 18 12 49 --- 15 | 54 37 38 67 --- 41
R20 | 2299 24 17 18 27 --- 12 | 43 43 66 48 --- 48
R21 | 1084 30 23 31 14 --- 15 | 49 51 53 28 --- 41
R23 | 2707 16 24 28 30 --- 14 | 46 25 61 35 --- 38
------+------------------------------------+--------------------------------
RMS | 2322 32 22 23 40 79 |T 53 48 53 54 72 46
WRMS | 2322 31 16 22 40 79 |NE 40 34 43 38 41 35
MEDI | 1329 25 16 23 28 85 |MD 44 37 39 43 49 36
Table 3.1556.6 GPS week: 1556 Day: 6 MJD: 55142
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 694 20 15 23 20 --- 11 | 39 37 43 48 --- 36
R03 | 797 13 14 22 21 --- 10 | 34 31 37 41 --- 30
R07 | 2026 17 16 16 19 --- 9 | 31 21 31 24 --- 22
R08 | 617 17 17 16 22 89 10 | 26 24 30 30 29 21
R10E | 1377 84 26 73 29 --- 32 | 59 28 38 42 --- 33
R11E | 794 29 24 31 47 156 19 | 184 169 178 179 115 175
R13E | 1556 33 36 40 55 --- 24 | 45 34 35 56 --- 31
R14E | 2132 39 37 36 57 --- 24 | 50 23 36 62 --- 31
R15E | 6812 26 23 32 52 31 19 | 37 18 29 65 32 27
R17 | 711 17 18 16 28 --- 11 | 42 57 45 28 --- 43
R18 | 2422 22 11 16 21 --- 10 | 37 50 48 48 --- 45
R19 | 870 21 15 27 12 --- 11 | 45 36 56 43 --- 42
R20 | 1075 22 21 29 29 --- 14 | 32 42 35 36 --- 31
R21 | 1114 25 15 13 17 --- 10 | 50 65 58 47 --- 54
R23 | 1691 30 23 44 16 --- 17 | 31 30 66 39 --- 33
------+------------------------------------+--------------------------------
RMS | 2219 32 22 33 33 105 |T 49 44 51 52 58 43
WRMS | 2219 26 17 32 33 105 |NE 36 39 44 38 29 35
MEDI | 1114 22 18 27 22 89 |MD 39 34 38 43 32 33
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