[IGSREPORT-18972] Wk 1599 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 16 05:57:51 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1599 (Aug 29, 2010 - Sep 04, 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 2.1599.
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:
igl1599[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1599 in the SP3 format.
igl15997.sum Combination Report for GPS Week 1599.
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 | 227.9 ns
1 | 211.6 ns
2 | 218.0 ns
3 | 224.7 ns
4 | 239.1 ns
5 | 244.5 ns
6 | 402.5 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 1.1599, 1a.1599).
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 2.1599.0-6)
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 3.1599.0-6).
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 1599 summary. (Aug 29, 2010 - Sep 04, 2010)
Table 1.1599.a GPS week : 1599 MJD: 55437.0-55443.0
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 124| 1 0 -6 10 -42 -78 -.14 27 25 | 0 16 1798 1881
| 1 0 1 26 30 100 .04 | 0 159
cod 230| -1 0 6 24 -4 53 -.13 20 20 | --- --- --- ---
| 1 1 3 22 15 49 .06 | --- ---
esx 131| 0 -1 6 -14 75 83 .40 30 24 | -73420 -1363 4130 8644
| 1 2 2 20 28 50 .07 | 64168 4923
gfz 194| 0 0 6 -68 -15 100 -.16 33 31 | 100551 -2941 4171 8475
| 1 2 3 59 58 35 .10 | 69510 4392
iac n/a| 0 0 -10 -34 -29 -63 -.12 34 34 | 252971 -232 4129 8909
| 1 0 5 30 24 43 .04 | 67256 2513
mcc n/a| 1 0 33 -62 -36 430 -.42 93 93 | --- --- --- ---
| 7 7 16 70 45 188 .44 | --- ---
Table 1.1599.b GPS week : 1599 MJD: 55437.0-55443.0
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 11 14 10 14 43 50 |
R02 | 10 13 11 10 11 11 12 |
R03 | 19 20 17 17 19 17 16 |
R04 | 14 14 13 13 12 12 13 |
R05 | 11 15 15 14 12 11 11 |
R07 | 11 10 12 17 17 14 13 |
R08 | 14 11 9 10 13 14 13 |
R10 | 13 11 11 12 12 13 11 |
R11 | 22 18 13 20 24 20 15 |
R13 | 8 8 11 10 14 14 15 |
R14 | 9 16 13 14 14 13 9 |
R15 | 13 12 11 16 12 16 11 |
R17 | 16 16 14 15 12 12 16 |
R18 | 17 18 17 15 15 10 13 |
R19 | 19 20 21 19 18 14 15 |
R20 | 17 26 24 23 25 16 17 |
R21 | 15 15 13 15 19 12 9 |
R22 | 18 15 15 16 24 14 11 |
R23 | 18 17 12 15 16 17 15 |
R24 | 18 14 12 12 14 13 14 |
Table 1.1599.c GPS week : 1599 MJD: 55437.0-55443.0
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 1599 0 | -32 5 310 -1904 298 -10100 86.3 1824 1824 | 227871 0
brd 1599 1 | -13 -43 354 -79 447 -14890 87.8 1571 1571 | 211573 0
brd 1599 2 | -32 -134 526 -408 41 -19610 88.0 1665 1665 | 217967 0
brd 1599 3 | 122 48 322 702 3067 -23000 89.4 1826 1826 | 224658 0
brd 1599 4 | -55 -103 261 -448 -323 -21770 85.7 2070 2070 | 239055 0
brd 1599 5 | 91 2 390 -255 -222 -20290 86.3 2230 2230 | 244467 0
brd 1599 6 | 124 47 283 1577 -2037 -14100 85.2 2803 2803 | 402481 0
-------------+------------------------------------------------------------+----------------
brd 1599 mean| 29 -25 349 -116 181 -17680 87.0 1998 1998 | 252581 0
brd 1599 sdev| 79 71 88 1076 1515 4719 1.5 420 420 | 67068 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 2.1599.0 GPS week: 1599 Day: 0 MJD: 55437
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 124| 0 0 -5 10 -53 -129 -.13 26 24 | 0 -139 1592 1663
cod 230| 0 0 9 21 19 115 -.14 20 22 | --- --- --- ---
esx 131| -2 -3 6 -20 54 74 .45 27 24 | -88373 289 3495 8262
gfz 194| 1 3 9 -95 -25 131 -.21 32 34 | 71235 -1822 3503 7814
iac n/a| 1 0 -14 -38 -29 -80 -.16 32 32 | 228467 -654 3499 8338
mcc n/a| 5 -4 48 11 -79 288 -.22 87 87 | --- --- --- ---
Table 2.1599.1 GPS week: 1599 Day: 1 MJD: 55438
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 124| 1 0 -4 40 -4 32 -.13 29 27 | 0 245 1755 1822
cod 230| 0 -1 8 12 -20 -19 -.18 19 18 | --- --- --- ---
esx 131| -2 0 4 -37 39 103 .47 27 25 | -115714 -1137 3928 9729
gfz 194| 0 0 10 -29 55 74 -.15 30 22 | 57033 -2849 3921 9808
iac n/a| 2 0 -14 -15 -17 -80 -.14 33 33 | 212392 468 3924 10299
mcc n/a| 0 9 56 21 26 795 .03 82 82 | --- --- --- ---
Table 2.1599.2 GPS week: 1599 Day: 2 MJD: 55439
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 124| 1 1 -5 29 -88 -187 -.14 24 22 | 0 -107 1950 2051
cod 230| 0 0 10 14 -1 52 -.22 19 19 | --- --- --- ---
esx 131| 0 0 4 -30 124 152 .43 23 22 | -107594 -4538 4903 8535
gfz 194| 0 4 10 -84 -113 111 -.26 32 30 | 66236 -5685 4909 8232
iac n/a| -2 1 -17 -17 -47 9 -.13 34 34 | 218777 -3192 4912 8966
mcc n/a| -5 -5 44 -74 -56 409 -.51 111 111 | --- --- --- ---
Table 2.1599.3 GPS week: 1599 Day: 3 MJD: 55440
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 124| 0 0 -5 -38 -57 -38 -.10 25 24 | 0 159 1695 1765
cod 230| 0 0 4 62 -7 37 -.07 19 17 | --- --- --- ---
esx 131| -1 -4 9 18 95 76 .32 28 27 | -97809 7065 4684 9252
gfz 194| 3 -2 1 -168 -49 54 -.19 32 22 | 68593 5070 4688 9080
iac n/a| 0 0 -9 -66 -61 -89 -.15 32 32 | 223893 3010 4660 9461
mcc n/a| 1 9 26 -112 23 253 -.30 96 96 | --- --- --- ---
Table 2.1599.4 GPS week: 1599 Day: 4 MJD: 55441
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 124| 1 1 -9 0 -58 -176 -.20 28 28 | 0 74 1828 1927
cod 230| -2 1 2 41 -27 119 -.12 21 24 | --- --- --- ---
esx 131| 0 -3 10 0 83 65 .46 29 24 | -84816 -7026 3532 8558
gfz 194| -1 1 6 -78 19 157 -.03 28 24 | 91704 -7961 3524 8474
iac n/a| 1 0 -6 -68 15 -32 -.09 37 37 | 240989 -2595 3537 9218
mcc n/a| -9 1 13 -181 -51 477 -.01 89 89 | --- --- --- ---
Table 2.1599.5 GPS week: 1599 Day: 5 MJD: 55442
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 124| 3 0 -6 0 -13 -117 -.12 25 24 | 0 55 1813 1890
cod 230| -3 1 3 22 2 37 -.09 19 23 | --- --- --- ---
esx 131| 0 -1 4 0 55 121 .34 38 24 | -89539 1667 3640 7414
gfz 194| 1 0 4 -45 38 99 -.02 44 47 | 93861 -795 3967 7279
iac n/a| 1 0 -2 -51 -35 -46 -.10 33 33 | 242870 2987 3694 7322
mcc n/a| 4 -10 27 -67 -30 505 -.74 84 84 | --- --- --- ---
Table 2.1599.6 GPS week: 1599 Day: 6 MJD: 55443
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 124| 2 0 -6 28 -23 67 -.17 31 24 | 0 -172 1954 2050
cod 230| -3 0 4 -6 4 31 -.09 18 17 | --- --- --- ---
esx 131| 0 1 5 -31 73 -6 .33 37 25 | 69902 -5867 4728 8761
gfz 194| 0 -3 4 23 -32 75 -.26 34 41 | 255196 -6545 4690 8644
iac n/a| 1 0 -5 14 -31 -125 -.04 34 34 | 403415 -1649 4683 8759
mcc n/a| 13 -5 15 -32 -86 286 -1.21 99 99 | --- --- --- ---
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 3.1599.0 GPS week: 1599 Day: 0 MJD: 55437
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 965 12 25 23 22 25 --- 12 | 31 62 41 47 29 --- 40
R02 | 780 17 13 16 21 21 --- 10 | 17 31 34 18 18 --- 20
R03 | 1753 27 35 32 34 37 --- 19 | 46 42 59 62 46 --- 43
R04 | 1160 15 24 33 16 19 --- 13 | 36 54 39 42 31 --- 38
R05 | 1122 16 19 21 24 12 --- 10 | 33 54 43 43 35 --- 41
R07 | 967 11 20 21 38 17 --- 10 | 32 58 43 46 36 --- 41
R08 | 2302 28 15 27 36 24 55 13 | 36 54 48 43 30 24 41
R10 | 1323 30 13 21 34 24 --- 13 | 20 24 36 29 23 --- 22
R11 | 1411 42 24 33 38 50 --- 21 | 53 59 74 72 65 --- 60
R13 | 1310 12 10 17 30 14 --- 7 | 24 24 25 38 26 --- 22
R14 | 952 10 12 15 29 23 --- 9 | 13 15 17 24 15 --- 11
R15 | 1685 26 12 15 23 33 55 12 | 18 14 24 25 22 19 13
R17E | 2796 25 21 31 41 35 --- 16 | 42 43 42 38 54 --- 38
R18E | 1827 33 14 27 25 39 --- 16 | 15 20 36 35 51 --- 22
R19E | 3742 32 26 32 30 42 --- 19 | 36 52 55 44 59 --- 42
R20E | 2750 25 20 36 41 37 --- 17 | 93 101 110 99 110 --- 99
R21E | 2039 30 17 29 43 28 --- 15 | 33 31 43 60 40 --- 32
R22E | 880 27 23 32 32 40 --- 17 | 29 23 35 34 37 --- 24
R23E | 1157 38 25 25 30 38 130 18 | 59 51 66 50 65 63 56
R24E | 2205 28 21 32 41 42 --- 17 | 26 26 27 37 42 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 1823 26 20 27 32 32 87 |T 34 41 44 44 41 35 36
WRMS | 1823 24 22 24 34 32 87 |NE 29 40 40 40 31 21 32
MEDI | 1323 26 20 27 30 28 55 |MD 32 42 41 42 36 24 38
Table 3.1599.1 GPS week: 1599 Day: 1 MJD: 55438
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1407 21 18 10 14 23 --- 10 | 24 52 54 38 27 --- 39
R02 | 856 16 18 28 32 25 --- 12 | 13 19 33 31 12 --- 11
R03 | 2074 33 26 47 40 30 --- 20 | 29 32 51 56 44 --- 33
R04 | 1127 21 18 31 14 20 --- 13 | 18 29 39 37 24 --- 23
R05 | 1284 19 25 29 23 30 --- 15 | 32 40 38 29 25 --- 28
R07 | 1308 26 17 10 34 12 --- 10 | 10 34 34 45 28 --- 25
R08 | 1328 25 19 11 21 20 64 11 | 20 37 30 44 41 13 29
R10 | 1429 22 16 17 24 21 --- 11 | 13 21 23 25 16 --- 13
R11 | 1035 31 16 22 47 54 --- 18 | 45 57 60 61 28 --- 45
R13 | 1358 13 13 12 21 13 --- 7 | 29 28 30 35 21 --- 25
R14 | 1649 29 17 24 24 39 --- 15 | 19 30 49 38 19 --- 27
R15 | 1577 23 10 25 25 22 46 11 | 17 21 32 28 32 12 22
R17E | 1068 21 17 30 22 41 --- 15 | 26 21 41 29 43 --- 25
R18E | 1330 39 14 32 29 39 --- 17 | 17 23 35 37 47 --- 21
R19E | 2538 50 26 18 19 41 --- 20 | 44 64 67 65 82 --- 55
R20E | 2257 61 27 42 47 51 --- 26 | 79 92 105 96 107 --- 91
R21E | 1771 26 25 21 29 29 --- 14 | 26 31 37 41 43 --- 27
R22E | 1419 21 20 31 25 30 --- 15 | 29 17 44 30 47 --- 25
R23E | 755 21 23 27 24 43 118 16 | 40 54 52 44 55 45 46
R24E | 2362 13 12 30 46 38 --- 14 | 23 18 30 44 34 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 1570 29 19 27 30 33 82 |T 27 36 44 42 38 23 31
WRMS | 1570 27 18 25 22 33 82 |NE 22 33 39 38 26 12 26
MEDI | 1358 22 18 25 24 30 64 |MD 24 30 38 38 32 13 25
Table 3.1599.2 GPS week: 1599 Day: 2 MJD: 55439
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1651 13 29 27 13 21 --- 14 | 27 55 37 40 24 --- 31
R02 | 903 19 14 18 20 23 --- 10 | 15 30 25 23 17 --- 18
R03 | 1417 32 23 20 28 45 --- 17 | 32 34 42 35 20 --- 24
R04 | 531 14 23 14 26 36 --- 12 | 28 33 27 25 31 --- 22
R05 | 1227 22 29 26 35 25 --- 15 | 23 46 41 46 24 --- 28
R07 | 1359 29 16 19 52 17 --- 12 | 26 49 55 43 32 --- 38
R08 | 1363 14 12 20 28 15 81 9 | 39 40 36 43 30 17 33
R10 | 984 15 10 20 27 27 --- 10 | 17 18 31 40 26 --- 19
R11 | 1559 19 19 21 58 29 --- 12 | 40 38 48 58 32 --- 34
R13 | 1542 21 20 14 14 19 --- 11 | 30 23 38 38 31 --- 27
R14 | 3416 21 21 13 23 36 --- 13 | 19 28 33 36 23 --- 22
R15 | 1999 13 12 24 25 22 39 10 | 19 24 29 30 31 13 20
R17E | 1510 17 9 24 21 45 --- 14 | 30 25 34 36 41 --- 27
R18E | 1711 28 24 24 26 43 --- 16 | 27 23 24 31 48 --- 21
R19E | 1826 36 29 34 31 47 --- 20 | 40 55 71 41 55 --- 49
R20E | 2309 46 19 38 42 66 --- 24 | 69 67 81 84 115 --- 73
R21E | 937 22 10 23 35 34 --- 12 | 25 20 33 38 37 --- 18
R22E | 1397 22 15 31 33 37 --- 15 | 21 18 45 40 39 --- 20
R23E | 1059 21 17 13 43 29 170 11 | 57 53 61 53 79 42 58
R24E | 2268 24 13 20 29 26 --- 12 | 28 20 32 45 30 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1665 24 19 23 32 34 111 |T 30 34 41 41 38 24 30
WRMS | 1665 22 19 22 30 34 111 |NE 26 34 36 38 26 15 26
MEDI | 1417 21 17 20 28 29 81 |MD 27 30 36 40 31 17 24
Table 3.1599.3 GPS week: 1599 Day: 3 MJD: 55440
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2427 19 12 22 17 14 --- 10 | 45 47 56 49 36 --- 43
R02 | 2090 10 15 16 15 22 --- 9 | 24 37 32 38 35 --- 29
R03 | 880 39 20 22 16 34 --- 16 | 47 44 45 38 25 --- 34
R04 | 715 19 17 13 15 38 --- 13 | 32 43 37 26 25 --- 31
R05 | 924 21 24 24 22 26 --- 14 | 25 45 30 31 35 --- 30
R07 | 1478 22 26 41 52 21 --- 16 | 40 61 55 87 37 --- 43
R08 | 2367 25 13 13 23 18 87 10 | 27 47 47 49 31 29 36
R10 | 1332 19 11 26 26 23 --- 11 | 18 17 35 35 20 --- 14
R11 | 1154 39 22 31 34 49 --- 20 | 36 44 47 46 44 --- 37
R13 | 1775 19 12 21 32 15 --- 9 | 17 28 29 47 33 --- 24
R14 | 1796 25 23 28 21 20 --- 14 | 34 27 46 24 25 --- 30
R15 | 3211 23 20 39 23 23 61 15 | 30 24 26 30 31 14 22
R17E | 781 21 16 28 31 41 --- 15 | 36 36 33 40 35 --- 28
R18E | 2886 18 24 17 34 38 --- 14 | 28 31 25 29 36 --- 16
R19E | 1114 28 23 31 33 49 --- 18 | 71 77 66 62 89 --- 72
R20E | 1148 42 19 53 59 45 --- 23 | 70 83 113 116 101 --- 85
R21E | 3278 21 14 28 37 39 --- 15 | 29 17 41 35 45 --- 24
R22E | 976 23 18 30 47 36 --- 15 | 23 26 44 41 46 --- 24
R23E | 860 29 24 19 24 30 127 14 | 50 79 72 68 62 61 64
R24E | 1659 21 15 17 26 26 --- 11 | 16 23 31 38 28 --- 16
------+-----------------------------------------+-------------------------------------
RMS | 1826 25 19 28 32 32 96 |T 34 41 45 46 40 34 35
WRMS | 1826 24 17 27 22 32 96 |NE 31 38 40 41 31 21 31
MEDI | 1332 21 18 24 26 26 87 |MD 30 37 41 38 35 29 30
Table 3.1599.4 GPS week: 1599 Day: 4 MJD: 55441
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3489 36 19 15 29 24 --- 14 | 22 52 71 59 51 --- 43
R02 | 3035 9 12 20 13 30 --- 10 | 21 30 35 36 42 --- 28
R03 | 1409 44 34 19 34 31 --- 19 | 35 42 38 44 29 --- 21
R04 | 603 26 16 20 16 21 --- 12 | 25 50 67 46 47 --- 46
R05 | 957 21 15 15 29 33 --- 12 | 32 45 45 42 48 --- 40
R07 | 1655 13 36 32 29 23 --- 16 | 32 64 30 40 32 --- 38
R08 | 2823 17 23 26 19 23 68 13 | 40 45 38 32 24 29 33
R10 | 1456 13 16 12 18 36 --- 11 | 13 15 18 20 37 --- 13
R11 | 1178 53 19 46 24 45 --- 24 | 32 42 73 54 38 --- 43
R13 | 1555 28 10 32 26 25 --- 14 | 15 25 36 36 22 --- 20
R14 | 1413 30 18 14 22 34 --- 14 | 12 24 20 26 37 --- 15
R15 | 3800 17 18 18 22 29 98 11 | 12 25 22 27 19 20 15
R17E | 1720 25 14 21 28 24 --- 12 | 28 23 20 28 34 --- 16
R18E | 2136 33 17 24 23 27 --- 14 | 24 22 33 26 34 --- 19
R19E | 1453 35 19 27 44 42 --- 17 | 19 42 78 71 61 --- 43
R20E | 1283 30 28 48 47 69 --- 25 | 62 66 70 85 102 --- 66
R21E | 2480 27 19 27 29 59 --- 19 | 16 25 39 35 59 --- 20
R22E | 1783 31 32 58 33 43 --- 24 | 27 38 68 38 53 --- 30
R23E | 2513 17 19 21 32 52 99 16 | 66 66 76 74 107 87 73
R24E | 989 18 21 25 23 33 --- 14 | 21 38 39 37 34 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2069 28 21 29 28 37 89 |T 27 38 45 42 45 45 32
WRMS | 2069 28 24 24 24 37 89 |NE 24 38 41 38 35 24 29
MEDI | 1555 26 19 21 26 31 98 |MD 24 38 38 37 37 29 28
Table 3.1599.5 GPS week: 1599 Day: 5 MJD: 55442
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3016 52 16 129 129 77 --- 42 | 45 42 169 63 24 --- 48
R02 | 2298 18 9 26 19 18 --- 10 | 11 19 48 24 17 --- 19
R03 | 2495 35 17 36 49 24 --- 16 | 21 30 51 59 28 --- 25
R04 | 1522 10 23 25 22 20 --- 11 | 24 45 26 42 33 --- 30
R05 | 691 19 16 23 22 19 --- 11 | 34 41 35 37 47 --- 37
R07 | 1862 33 21 12 27 21 --- 13 | 18 44 51 44 39 --- 36
R08 | 1762 19 29 18 24 28 63 14 | 22 40 18 24 16 15 20
R10 | 1366 19 11 29 25 26 --- 12 | 13 18 41 35 29 --- 21
R11 | 1487 42 20 34 27 39 --- 19 | 37 46 36 36 47 --- 37
R13 | 2453 17 24 24 29 31 --- 14 | 18 26 23 32 22 --- 16
R14 | 1444 24 22 23 20 24 --- 13 | 25 43 34 38 23 --- 27
R15 | 4840 20 32 26 25 26 105 15 | 19 22 31 31 23 14 18
R17E | 2646 23 12 14 27 32 --- 12 | 25 27 29 38 35 --- 25
R18E | 1698 20 14 17 41 20 --- 10 | 16 22 26 45 30 --- 16
R19E | 1095 20 16 35 30 24 --- 13 | 61 51 77 60 68 --- 60
R20E | 2375 26 22 30 84 33 --- 16 | 57 61 85 108 87 --- 67
R21E | 2066 18 18 16 38 26 --- 11 | 21 15 21 37 42 --- 18
R22E | 1122 21 17 25 32 33 --- 13 | 21 22 38 30 50 --- 27
R23E | 3242 22 18 35 26 44 78 17 | 35 35 32 31 56 47 29
R24E | 1051 11 14 24 24 35 --- 12 | 17 19 31 28 41 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 2230 25 19 38 44 33 84 |T 27 33 45 42 37 25 29
WRMS | 2230 24 23 24 47 33 84 |NE 23 34 46 38 29 14 27
MEDI | 1762 20 17 25 27 26 78 |MD 21 30 34 37 33 15 25
Table 3.1599.6 GPS week: 1599 Day: 6 MJD: 55443
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1349 104 46 119 69 87 --- 50 | 54 63 72 57 50 --- 46
R02 | 1418 14 14 34 26 16 --- 11 | 20 30 30 21 20 --- 20
R03 | 3421 24 18 48 24 14 --- 15 | 23 38 43 36 24 --- 26
R04 | 5860 14 16 21 27 35 --- 12 | 25 49 44 50 25 --- 34
R05 | 906 11 17 18 19 29 --- 11 | 40 57 44 55 45 --- 46
R07 | 1764 25 15 26 21 28 --- 13 | 34 65 44 57 62 --- 51
R08 | 1356 13 23 29 31 18 83 12 | 44 67 40 43 37 14 48
R10 | 1105 17 11 21 12 25 --- 10 | 25 17 20 25 26 --- 18
R11 | 2013 20 19 27 29 38 --- 15 | 46 56 64 50 51 --- 51
R13 | 4237 32 8 31 42 30 --- 14 | 24 22 38 51 24 --- 23
R14 | 3177 10 14 13 12 24 --- 9 | 22 22 35 30 35 --- 25
R15 | 4524 23 12 19 37 20 82 10 | 20 18 25 31 19 19 16
R17E | 2576 32 13 29 33 37 --- 15 | 33 37 35 31 44 --- 32
R18E | 3743 18 12 18 29 37 --- 12 | 21 16 34 28 33 --- 17
R19E | 1006 32 17 32 40 24 --- 15 | 28 45 58 61 39 --- 38
R20E | 2137 32 14 33 42 37 --- 16 | 64 68 92 88 91 --- 74
R21E | 2793 13 8 19 31 20 --- 8 | 19 21 29 39 27 --- 17
R22E | 1151 12 14 22 31 28 --- 11 | 15 24 30 26 34 --- 17
R23E | 3163 28 13 31 46 36 126 15 | 32 41 58 41 38 78 35
R24E | 1505 13 18 24 36 37 --- 13 | 13 23 25 30 35 --- 15
------+-----------------------------------------+-------------------------------------
RMS | 2802 31 18 37 34 34 99 |T 30 38 43 42 37 37 32
WRMS | 2802 24 17 25 41 34 99 |NE 31 42 41 42 34 16 33
MEDI | 2013 18 14 26 31 28 83 |MD 25 37 38 39 35 19 26
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