[IGSREPORT-19293] Wk 1613 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Dec 23 06:35:15 PST 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1613 (Dec 05, 2010 - Dec 11, 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 2.1613.
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:
igl1613[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1613 in the SP3 format.
igl16137.sum Combination Report for GPS Week 1613.
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 | 358.9 ns
1 | 318.6 ns
2 | 359.6 ns
3 | 333.7 ns
4 | 330.8 ns
5 | 330.7 ns
6 | 355.8 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 1.1613, 1a.1613).
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 2.1613.0-6)
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 3.1613.0-6).
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 1613 summary. (Dec 05, 2010 - Dec 11, 2010)
Table 1.1613.a GPS week : 1613 MJD: 55535.0-55541.0
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 136| 2 0 11 23 4 -37 -.15 44 40 | 0 1350 5148 5793
| 1 2 2 47 23 73 .04 | 0 1272
cod 236| -1 0 0 38 -13 5 -.11 17 13 | --- --- --- ---
| 0 0 2 10 7 16 .03 | --- ---
esx 152| 0 -1 -2 -71 36 10 .34 28 26 | 30559 -3838 5733 12364
| 1 1 1 57 43 57 .04 | 17479 6851
gfz 194| 1 -1 0 -32 -56 30 -.30 35 35 | --- --- --- ---
| 2 1 3 50 88 61 .04 | --- ---
iac n/a| 3 0 -3 -30 11 65 -.11 38 38 | 341883 -1375 5718 12413
| 1 1 7 38 21 49 .04 | 17580 2492
mcc n/a| 3 -2 58 53 125 1625 .27 222 222 | --- --- --- ---
| 11 11 20 175 156 368 .57 | --- ---
Table 1.1613.b GPS week : 1613 MJD: 55535.0-55541.0
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 | 20 20 21 25 24 21 19 |
R02 | 23 25 30 26 18 18 19 |
R05 | 27 33 26 26 22 31 18 |
R06 | 37 36 33 25 22 23 23 |
R07 | 25 23 20 19 20 17 17 |
R08 | 27 21 25 32 27 20 17 |
R09 | 12 13 11 10 13 12 11 |
R10 | 12 10 11 12 11 15 9 |
R11 | 33 24 23 14 18 15 14 |
R12 | 10 11 10 11 9 14 10 |
R13 | 13 15 18 11 10 9 14 |
R15 | 13 12 13 11 12 12 10 |
R16 | 10 11 11 15 11 9 8 |
R18 | 9 7 16 14 11 16 11 |
R19 | 10 13 10 11 16 12 11 |
R20 | 11 18 17 17 14 17 19 |
R21 | 13 20 16 7 11 10 16 |
R22 | 10 17 17 10 7 12 7 |
R23 | 12 9 12 11 8 12 12 |
R24 | 13 19 11 18 9 13 11 |
Table 1.1613.c GPS week : 1613 MJD: 55535.0-55541.0
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 1613 0 | 61 26 239 -1053 -174 -15630 83.4 2410 2410 | 358887 0
brd 1613 1 | -20 -2 177 -1040 1197 -14570 86.5 2178 2178 | 318643 0
brd 1613 2 | 84 -70 150 -721 -174 -14260 90.2 2336 2336 | 359599 0
brd 1613 3 | -8 113 9 -740 164 -17050 87.9 2739 2739 | 333662 0
brd 1613 4 | -119 33 178 -4696 -1528 -16980 87.8 2662 2662 | 330805 0
brd 1613 5 | -32 -48 234 437 1417 -10580 86.5 2172 2172 | 330732 0
brd 1613 6 | 164 -51 219 1363 3826 -9730 86.3 1703 1703 | 355837 0
-------------+------------------------------------------------------------+----------------
brd 1613 mean| 18 0 172 -921 675 -14114 86.9 2314 2314 | 341166 0
brd 1613 sdev| 92 64 79 1889 1698 2917 2.1 347 347 | 16577 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 2.1613.0 GPS week: 1613 Day: 0 MJD: 55535
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 136| 0 2 11 -22 39 -88 -.15 60 51 | 0 1524 4485 4777
cod 236| 0 0 -1 50 -17 3 -.11 17 11 | --- --- --- ---
esx 152| 0 -2 -1 -41 -14 39 .32 29 26 | 51101 2128 4731 11344
gfz 194| 1 -1 -2 -96 -24 -41 -.36 43 44 | --- --- --- ---
iac n/a| 2 2 3 -77 27 42 -.09 39 39 | 361126 -2751 4642 11922
mcc n/a| 1 -16 89 339 244 934 1.32 262 262 | --- --- --- ---
Table 2.1613.1 GPS week: 1613 Day: 1 MJD: 55536
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 136| 0 -1 11 13 24 -39 -.20 55 41 | 0 2770 4868 5739
cod 236| -1 0 2 33 -20 0 -.13 21 15 | --- --- --- ---
esx 152| 1 -1 -1 -55 8 57 .30 25 23 | 16692 -6756 4667 13576
gfz 194| 0 0 0 -55 27 0 -.32 40 30 | --- --- --- ---
iac n/a| 4 0 -10 -31 20 -14 -.18 42 42 | 319901 -4249 4662 13021
mcc n/a| 22 14 47 -127 385 2058 -.02 169 169 | --- --- --- ---
Table 2.1613.2 GPS week: 1613 Day: 2 MJD: 55537
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 136| 0 0 11 15 3 113 -.15 43 36 | 0 1924 3786 4338
cod 236| -1 -1 2 33 -16 6 -.17 18 15 | --- --- --- ---
esx 152| 0 -2 -1 -2 34 -98 .29 30 28 | 50236 -1515 4628 14656
gfz 194| 0 1 0 29 39 42 -.28 35 41 | --- --- --- ---
iac n/a| 2 2 -16 -31 27 100 -.08 45 45 | 360771 -1263 4618 15492
mcc n/a| 0 -15 51 52 -37 1795 -.56 258 258 | --- --- --- ---
Table 2.1613.3 GPS week: 1613 Day: 3 MJD: 55538
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 136| 3 4 11 31 -11 -73 -.12 48 48 | 0 2502 6530 7201
cod 236| -2 0 0 41 -4 -23 -.07 18 14 | --- --- --- ---
esx 152| -1 0 -1 -82 79 28 .32 28 26 | 31474 -17908 10864 15776
gfz 194| 6 -3 1 34 -2 -43 -.32 31 24 | --- --- --- ---
iac n/a| 3 0 0 -58 3 139 -.14 35 35 | 337627 -3843 10890 16115
mcc n/a| 0 0 49 158 75 1740 .20 168 168 | --- --- --- ---
Table 2.1613.4 GPS week: 1613 Day: 4 MJD: 55539
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 136| 2 0 10 11 -33 -109 -.09 32 30 | 0 -979 7610 8574
cod 236| -3 0 -3 54 -2 21 -.11 16 12 | --- --- --- ---
esx 152| -1 -2 0 -79 29 61 .37 29 29 | 9563 -2317 6706 12516
gfz 194| 2 -2 1 -43 -188 49 -.29 32 36 | --- --- --- ---
iac n/a| 2 2 1 -33 -19 71 -.08 34 34 | 326475 2718 6706 12299
mcc n/a| -5 3 28 -184 -62 1563 .54 160 160 | --- --- --- ---
Table 2.1613.5 GPS week: 1613 Day: 5 MJD: 55540
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 136| 4 1 14 -6 -1 -46 -.19 37 38 | 0 637 4027 4526
cod 236| 0 0 -1 31 -15 29 -.10 15 13 | --- --- --- ---
esx 152| 0 0 -5 -54 11 18 .40 28 25 | 13814 1497 4431 9098
gfz 194| 0 -4 0 -77 -127 103 -.25 29 27 | --- --- --- ---
iac n/a| 5 0 -7 -25 36 39 -.13 39 39 | 329815 630 4430 9047
mcc n/a| 14 -6 72 88 148 1419 .13 283 283 | --- --- --- ---
Table 2.1613.6 GPS week: 1613 Day: 6 MJD: 55541
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 136| 3 -1 6 122 10 -21 -.19 35 35 | 0 1074 4735 5399
cod 236| -1 0 -1 24 -21 3 -.12 13 11 | --- --- --- ---
esx 152| 0 0 -3 -186 109 -31 .38 26 26 | 41035 -1998 4106 9587
gfz 194| 0 0 7 -16 -123 101 -.29 33 45 | --- --- --- ---
iac n/a| 1 -2 2 47 -13 76 -.07 33 33 | 357472 -870 4083 8999
mcc n/a| -9 3 69 48 126 1872 .28 255 255 | --- --- --- ---
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 3.1613.0 GPS week: 1613 Day: 0 MJD: 55535
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
XR01E |13077 37 15 --- 44 42 --- 20 | 26 26 --- 47 50 --- 25
R02E | 4654 54 33 32 27 52 --- 23 | 47 62 74 61 71 --- 59
R05E | 2143 101 27 29 26 45 311 27 | 36 25 38 41 55 175 28
R06E | 2382 143 21 57 47 54 --- 37 | 76 91 122 98 129 --- 100
R07E | 1152 65 16 43 104 65 --- 25 | 45 28 41 64 60 --- 26
R08E | 2113 99 26 26 25 53 189 27 | 39 37 39 50 68 104 38
R09M | 1053 27 9 25 42 27 --- 11 | 33 39 57 60 38 --- 39
R10 | 1875 35 7 22 25 25 --- 11 | 28 22 28 27 29 --- 22
R11M | 3166 98 29 51 45 71 350 32 | 63 112 139 133 90 170 104
R12 | 1393 26 5 14 27 25 --- 9 | 27 30 38 42 31 --- 29
R13 | 1718 26 12 28 30 24 --- 12 | 31 30 37 45 22 --- 27
R15 | 3584 26 15 15 18 35 150 12 | 29 26 43 27 31 81 29
R16M | 939 17 11 19 16 23 --- 9 | 30 28 38 32 29 --- 28
R18M | 1228 26 11 14 36 18 309 9 | 52 63 69 81 63 234 61
R19M | 4649 31 7 12 59 21 --- 9 | 66 77 73 72 75 --- 73
R20 | 3620 35 12 17 36 19 --- 11 | 26 52 53 67 60 --- 46
R21 | 868 21 7 25 25 34 --- 12 | 51 73 85 84 60 --- 69
R22M | 817 19 12 22 30 21 --- 10 | 54 68 74 84 62 --- 65
R23 | 663 27 9 12 73 37 197 12 | 43 41 43 60 72 133 45
R24 | 1127 38 7 29 14 19 --- 12 | 28 50 63 57 61 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 2410 59 17 29 43 39 262 |T 41 49 60 61 57 149 48
WRMS | 2410 51 11 26 44 39 262 |NE 31 40 49 49 42 81 38
MEDI | 1718 31 12 25 30 27 197 |MD 36 39 53 60 60 133 39
Table 3.1613.1 GPS week: 1613 Day: 1 MJD: 55536
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1238 58 16 26 33 47 --- 20 | 30 35 46 39 53 --- 33
R02E | 4114 69 27 26 30 63 --- 25 | 49 55 55 51 69 --- 51
R05E | 1953 116 32 35 29 47 123 32 | 34 44 50 41 51 97 36
R06E | 1816 122 43 35 49 60 --- 36 | 54 45 51 43 76 --- 44
R07E | 1613 50 17 39 55 61 --- 23 | 27 23 37 46 52 --- 24
R08E | 1697 65 11 32 46 46 135 21 | 53 41 44 53 58 68 43
R09 | 1659 21 12 24 30 36 --- 13 | 30 31 38 41 33 --- 28
R10 | 1615 21 12 12 22 26 --- 9 | 25 40 40 45 40 --- 34
R11 | 3623 74 39 27 52 29 246 24 | 90 108 98 102 90 96 89
R12 | 1104 16 7 17 22 33 --- 10 | 31 37 46 50 33 --- 36
R13 | 1852 30 16 28 24 30 --- 14 | 21 22 29 32 19 --- 17
R15 | 4298 19 16 16 25 33 164 12 | 23 19 35 35 22 69 22
R16 | 1330 17 15 17 27 26 --- 10 | 27 32 46 42 34 --- 34
R18 | 1163 20 5 12 33 10 --- 6 | 35 39 40 39 46 --- 39
R19 | 3205 34 18 20 64 21 --- 12 | 56 49 61 76 59 --- 53
R20 | 1916 57 10 30 63 29 --- 17 | 19 30 44 59 30 --- 28
R21 | 1318 31 23 25 18 59 --- 19 | 33 61 56 55 30 --- 46
R22 | 789 30 20 25 34 47 --- 17 | 34 53 60 62 38 --- 45
R23M | 886 13 12 15 49 21 149 9 | 35 47 47 75 43 56 43
R24 | 1391 42 13 15 37 60 --- 18 | 22 35 46 69 83 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 2177 55 21 25 40 42 169 |T 36 42 48 52 47 77 39
WRMS | 2177 41 15 23 30 42 169 |NE 24 34 42 49 36 69 32
MEDI | 1615 31 16 25 33 33 149 |MD 31 39 46 46 43 69 36
Table 3.1613.2 GPS week: 1613 Day: 2 MJD: 55537
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 832 53 16 30 38 52 --- 20 | 41 43 33 44 50 --- 37
R02E | 2102 68 39 21 26 83 --- 29 | 50 61 53 53 90 --- 54
R05E | 2017 68 29 38 31 53 90 25 | 35 35 53 36 45 56 31
R06E | 1849 96 22 50 46 62 --- 32 | 63 34 43 48 53 --- 35
R07E | 2445 38 16 33 60 57 --- 19 | 23 27 32 40 48 --- 21
R08E | 1015 65 14 50 41 52 148 25 | 59 55 46 69 80 51 53
R09 | 1814 17 10 15 26 36 --- 10 | 37 37 49 38 39 --- 38
R10 | 1000 16 14 12 14 31 --- 10 | 23 22 27 24 32 --- 21
R11 | 3729 44 24 55 51 31 191 22 | 103 104 126 124 112 97 106
R12 | 1968 20 9 16 38 26 --- 9 | 23 34 46 53 37 --- 33
R13 | 3446 31 16 46 30 31 --- 18 | 29 33 60 43 25 --- 33
R15 | 3734 28 12 17 33 34 179 12 | 24 33 47 39 28 51 30
R16 | 881 19 9 18 34 30 --- 10 | 32 25 37 37 32 --- 27
R18 | 4695 25 18 24 20 48 536 16 | 37 56 60 55 37 366 46
R19 | 2315 23 11 19 29 14 --- 9 | 40 55 52 55 45 --- 46
R20 | 1279 35 12 14 28 57 --- 16 | 34 36 48 63 73 --- 42
R21 | 795 20 23 10 23 54 --- 16 | 29 52 43 38 40 --- 39
R22 | 1441 33 23 21 27 45 --- 16 | 30 52 53 54 37 --- 42
R23 | 1966 16 15 18 36 36 116 12 | 25 42 47 62 29 69 36
R24 | 2294 32 11 14 33 19 --- 10 | 24 48 50 66 61 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 2336 43 18 30 35 45 258 |T 38 44 50 52 49 115 40
WRMS | 2336 36 15 28 41 45 258 |NE 26 36 45 46 42 51 34
MEDI | 1966 31 15 19 31 36 148 |MD 32 37 47 48 40 56 37
Table 3.1613.3 GPS week: 1613 Day: 3 MJD: 55538
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 962 56 29 31 36 64 --- 25 | 63 53 54 73 78 --- 57
R02E | 1481 71 20 47 36 54 --- 26 | 50 60 79 68 76 --- 60
R05E | 2325 84 23 24 30 55 82 26 | 41 32 44 36 53 58 29
R06E | 3674 85 25 28 26 43 --- 25 | 89 59 47 66 71 --- 57
R07E | 4719 54 15 28 34 42 --- 19 | 37 25 34 36 54 --- 29
R08E | 1512 106 34 27 50 54 145 31 | 25 58 52 45 62 49 43
R09 | 1237 19 10 17 23 27 --- 10 | 39 28 45 44 27 --- 30
R10 | 2489 28 12 25 17 19 --- 11 | 30 29 47 34 37 --- 30
R11 | 3397 26 21 28 37 20 208 13 | 163 168 176 157 154 124 165
R12 | 2707 18 16 25 34 16 --- 11 | 36 51 46 57 42 --- 43
R13 | 2380 19 10 25 28 21 --- 10 | 26 32 40 49 29 --- 28
R15 | 4392 20 11 19 22 26 192 10 | 20 20 33 37 25 56 18
R16 | 515 24 14 34 27 35 --- 15 | 28 33 59 48 21 --- 32
R18 | 5103 29 6 36 32 28 197 14 | 40 52 83 52 34 218 52
R19 | 1790 19 7 24 24 26 --- 10 | 56 64 70 57 57 --- 62
R20 | 1227 46 16 30 26 37 --- 17 | 24 36 55 50 46 --- 36
R21 | 989 19 7 12 17 13 --- 7 | 61 65 52 72 64 --- 61
R22 | 1523 28 16 14 36 10 --- 10 | 29 55 46 54 47 --- 47
R23 | 2540 18 18 22 26 20 150 11 | 38 47 55 30 50 89 45
R24 | 3335 45 10 44 36 29 --- 18 | 28 41 74 61 28 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 2739 48 18 28 31 35 168 |T 46 50 59 56 52 99 48
WRMS | 2739 48 14 26 24 35 168 |NE 32 39 49 51 38 56 36
MEDI | 2325 28 15 25 28 27 150 |MD 37 47 52 50 47 58 43
Table 3.1613.4 GPS week: 1613 Day: 4 MJD: 55539
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2087 45 18 42 34 66 --- 24 | 26 30 41 51 67 --- 31
R02E | 978 33 16 25 27 50 --- 17 | 71 68 73 72 88 --- 70
R05E | 870 59 17 32 29 49 79 22 | 39 28 39 27 52 38 26
R06E | 3940 45 32 23 24 50 --- 21 | 43 75 70 68 75 --- 62
R07E | 3783 41 23 39 51 36 --- 19 | 29 36 43 43 43 --- 25
R08E | 1152 68 30 45 43 48 156 26 | 60 57 52 56 64 46 47
R09 | 1659 20 15 28 33 26 --- 12 | 30 28 40 42 29 --- 27
R10 | 4021 16 13 27 24 23 --- 11 | 21 29 48 36 39 --- 28
R11 | 2960 28 15 47 40 30 190 17 | 155 151 170 173 138 108 151
R12 | 2504 13 10 11 16 28 --- 9 | 22 35 36 34 32 --- 31
R13 | 1373 15 10 27 27 17 --- 10 | 25 28 43 44 36 --- 27
R15 | 3110 18 12 30 34 25 121 12 | 22 20 46 35 26 62 22
R16 | 558 17 11 28 34 15 --- 10 | 30 29 49 48 20 --- 28
R18 | 4021 28 18 9 39 14 188 10 | 32 59 43 39 40 341 45
R19 | 3242 28 7 40 29 35 --- 15 | 52 59 93 44 42 --- 60
R20 | 2623 22 17 16 29 38 --- 13 | 38 42 45 42 39 --- 38
R21 | 929 26 8 26 41 15 --- 11 | 28 45 61 78 48 --- 44
R22 | 1721 13 9 16 23 13 --- 7 | 58 57 40 55 57 --- 52
R23 | 2092 10 9 20 13 19 190 8 | 104 106 87 97 110 125 101
R24 | 4105 15 11 16 34 20 --- 8 | 12 25 23 44 32 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 2661 32 16 29 32 34 160 |T 44 50 57 56 53 120 46
WRMS | 2661 30 12 29 36 34 160 |NE 24 32 43 44 36 62 29
MEDI | 2092 22 13 27 29 26 156 |MD 30 36 45 44 42 62 31
Table 3.1613.5 GPS week: 1613 Day: 5 MJD: 55540
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2696 47 20 27 24 61 --- 21 | 27 40 33 40 54 --- 32
R02E | 1418 33 16 29 36 51 --- 17 | 33 31 40 46 56 --- 30
R05E | 810 94 17 49 42 60 124 31 | 41 29 42 50 56 47 25
R06E | 1813 64 24 25 24 48 --- 22 | 45 35 34 31 46 --- 32
R07E | 2896 34 20 20 52 50 --- 17 | 22 37 29 36 49 --- 27
R08E | 1895 54 20 28 33 45 135 20 | 48 27 24 30 44 44 21
R09 | 1701 30 11 25 23 21 --- 12 | 39 48 43 38 39 --- 40
R10 | 3569 17 19 17 28 47 --- 14 | 21 28 25 34 35 --- 22
R11 | 3358 25 18 28 40 34 133 14 | 114 121 117 130 130 221 118
R12 | 1479 18 11 23 17 45 --- 13 | 32 31 32 28 25 --- 26
R13 | 2989 11 12 16 15 25 --- 9 | 29 38 38 33 27 --- 32
R15 | 1394 26 9 15 17 33 155 11 | 17 20 30 27 22 87 18
R16 | 726 17 11 14 19 20 --- 8 | 18 32 38 43 23 --- 26
R18 | 3449 34 10 43 14 24 550 16 | 30 39 79 38 39 518 43
R19 | 2364 10 10 24 19 36 --- 11 | 43 44 57 44 27 --- 42
R20 | 1777 41 13 31 29 39 --- 16 | 29 39 55 54 52 --- 40
R21 | 739 23 7 22 27 20 --- 10 | 39 50 59 50 54 --- 50
R22 | 958 19 14 29 32 26 --- 12 | 28 34 50 52 42 --- 35
R23 | 915 19 12 27 35 26 321 11 | 107 111 118 119 113 235 111
R24 | 2387 21 13 32 31 22 --- 12 | 19 21 45 39 32 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2172 37 15 28 29 39 283 |T 39 42 49 48 48 192 39
WRMS | 2172 38 13 25 27 39 283 |NE 26 32 40 37 35 87 30
MEDI | 1777 25 13 25 27 34 135 |MD 30 35 40 39 42 87 32
Table 3.1613.6 GPS week: 1613 Day: 6 MJD: 55541
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2021 35 16 30 27 55 --- 18 | 32 33 45 38 60 --- 34
R02E | 747 52 16 24 23 45 --- 18 | 75 53 50 49 69 --- 54
R05E | 903 44 15 33 35 43 266 18 | 28 26 50 38 50 39 25
R06E | 1015 71 16 37 39 44 --- 22 | 76 76 78 78 89 --- 75
R07E | 1557 40 13 28 60 46 --- 17 | 23 20 34 45 42 --- 18
R08E | 2272 34 18 25 27 48 90 17 | 36 35 54 39 56 50 34
R09 | 1924 22 11 22 27 26 --- 11 | 39 45 60 46 37 --- 43
R10 | 922 12 8 19 30 24 --- 8 | 23 26 33 33 37 --- 26
R11 | 1966 36 12 31 18 23 105 13 | 242 244 260 241 236 212 245
R12 | 1969 16 12 19 36 22 --- 9 | 29 32 37 31 24 --- 28
R13 | 3747 26 18 20 24 37 --- 14 | 29 34 44 44 30 --- 32
R15 | 824 17 8 23 31 24 150 10 | 20 29 34 25 28 54 25
R16 | 659 14 9 17 31 15 --- 7 | 22 29 37 41 19 --- 25
R18 | 1522 35 8 17 25 22 446 11 | 37 62 76 67 66 354 59
R19 | 1452 36 8 24 20 13 --- 11 | 47 64 75 58 63 --- 61
R20 | 1633 49 15 41 55 32 --- 18 | 19 46 75 77 66 --- 50
R21 | 776 43 5 41 24 21 --- 15 | 40 75 105 79 66 --- 72
R22 | 2594 21 5 14 19 15 --- 7 | 39 62 62 64 64 --- 57
R23 | 910 26 14 14 24 31 283 11 | 112 112 108 115 111 264 110
R24 | 1111 18 13 26 53 16 --- 10 | 23 35 48 52 35 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1703 35 13 26 33 33 255 |T 49 56 68 63 62 162 55
WRMS | 1703 35 11 26 45 33 255 |NE 26 39 53 48 40 54 38
MEDI | 1452 34 12 24 27 24 150 |MD 32 35 50 46 56 54 34
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