[IGSREPORT-16996] Wk 1511 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Fri Jan 9 05:51:33 PST 2009
******************************************************************************
IGS Electronic Report 09 Jan 05:51:36 PST 2009 Message Number 16996
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1511 (Dec 21, 2008 - Dec 27, 2008)
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 2.1511.
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:
igl1511[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1511 in the SP3 format.
igl15117.sum Combination Report for GPS Week 1511.
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 | 317.0 ns
1 | 305.1 ns
2 | 303.1 ns
3 | 314.5 ns
4 | 302.8 ns
5 | 302.5 ns
6 | 344.3 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
----+--------+---------------
0 | BKG | R23
1 | BKG | R23
6 | BKG | R04
6 | IAC | R10
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 1.1511, 1a.1511).
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 2.1511.0-6)
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 3.1511.0-6).
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 1511 summary. (Dec 21, 2008 - Dec 27, 2008)
Table 1.1511.a GPS week : 1511 MJD: 54821.0-54827.0
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 87| 3 0 18 23 -38 -77 -.14 63 33 | 0 -54 2476 2559
| 1 2 4 48 44 135 .05 | 0 90
cod 242| -3 0 -7 39 21 11 -.08 24 16 | --- --- --- ---
| 1 0 2 19 12 31 .06 | --- ---
esx 132| -1 0 -6 -61 17 3 .34 39 27 | 57130 6966 7552 14685
| 1 3 3 39 26 51 .10 | 26552 7571
iac n/a| 6 -2 9 -18 -49 21 -.15 59 59 | 311541 -128 7359 14234
| 3 2 6 45 24 41 .07 | 17590 6044
mcc n/a| 6 4 19 32 -77 1935 -.01 64 64 | --- --- --- ---
| 7 14 11 171 111 660 .34 | --- ---
Table 1.1511.b GPS week : 1511 MJD: 54821.0-54827.0
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
------+------------------------------------+------------------------------------------
R04 | 18 21 35 42 36 61 62 |
R06 | 20 16 17 17 16 28 25 |
R07 | 20 21 23 28 15 28 26 |
R10 | 10 13 16 17 18 16 32 |
R11 | 9 10 14 16 12 15 15 |
R13 | 13 10 9 10 20 15 16 |
R14 | 11 9 9 10 9 12 11 |
R15 | 12 11 10 13 17 17 15 |
R17 | 14 15 12 13 14 18 36 |
R18 | 14 14 17 14 13 15 21 |
R19 | 12 13 16 14 11 16 36 |
R20 | 14 17 16 21 16 21 24 |
R21 | 11 12 15 18 16 15 17 |
R22 | 17 9 11 15 15 18 12 |
R23 | 24 149 42 24 20 20 17 |
R24 | 16 18 18 20 18 27 24 |
Table 1.1511.c GPS week : 1511 MJD: 54821.0-54827.0
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 1511 0 | -147 -79 299 -1251 1267 -23520 99.5 3477 3477 | 317008 0
brd 1511 1 | 113 -223 36 -3029 4509 -22610 84.7 5122 5122 | 305131 0
brd 1511 2 | 130 70 161 -29 -2481 -22680 87.9 3889 3889 | 303141 0
brd 1511 3 | 95 94 94 -1219 108 -28000 91.2 3605 3605 | 314508 0
brd 1511 4 | 110 -136 253 2297 -498 -37660 95.2 3817 3817 | 302757 0
brd 1511 5 | -1 -82 296 499 3123 -32100 88.4 3981 3981 | 302462 0
brd 1511 6 | 33 -112 54 -485 -644 -26770 88.8 4237 4237 | 344317 0
-------------+------------------------------------------------------------+----------------
brd 1511 mean| 47 -66 170 -459 769 -27620 90.8 4018 4018 | 312760 0
brd 1511 sdev| 98 113 112 1658 2393 5598 5.0 545 545 | 15131 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 2.1511.0 GPS week: 1511 Day: 0 MJD: 54821
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 87| 4 0 12 -17 -66 -41 -.18 64 29 | 0 -75 2914 2981
cod 242| -4 0 -4 45 34 3 -.03 14 11 | --- --- --- ---
esx 132| -2 -1 -10 -51 4 -18 .26 32 25 | 40554 -151 6525 17177
iac n/a| 6 -2 7 -67 -38 76 -.17 31 31 | 315081 -2498 6430 16546
mcc n/a| 15 1 34 -227 116 2642 -.55 51 51 | --- --- --- ---
Table 2.1511.1 GPS week: 1511 Day: 1 MJD: 54822
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 87| 3 -1 15 3 -12 27 -.15 127 27 | 0 7 2230 2320
cod 242| -1 0 -11 37 3 37 .00 48 15 | --- --- --- ---
esx 132| -3 3 -10 -48 1 -87 .27 65 25 | 31781 7953 7135 17521
iac n/a| 4 -2 10 12 -39 -10 -.19 69 69 | 301649 -145 6938 16697
mcc n/a| 13 3 25 -36 -113 2243 -.07 64 64 | --- --- --- ---
Table 2.1511.2 GPS week: 1511 Day: 2 MJD: 54823
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 87| 4 0 14 16 -47 -72 -.13 46 27 | 0 -140 2194 2300
cod 242| -4 1 -7 29 20 6 -.09 21 15 | --- --- --- ---
esx 132| 0 -1 -3 -6 31 24 .41 32 24 | 32807 18835 13059 15467
iac n/a| 8 0 15 21 -20 51 -.13 46 46 | 296370 10976 12481 14906
mcc n/a| 0 5 6 -75 -117 2326 -.02 57 57 | --- --- --- ---
Table 2.1511.3 GPS week: 1511 Day: 3 MJD: 54824
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 87| 1 -2 19 -26 -6 80 -.03 47 36 | 0 -89 2429 2490
cod 242| -1 0 -8 75 25 -21 -.14 21 18 | --- --- --- ---
esx 132| -1 3 -4 -42 3 -21 .51 37 31 | 66458 7081 5633 12879
iac n/a| 1 -2 1 -65 -53 -34 -.27 40 40 | 316150 172 5619 12953
mcc n/a| -5 3 13 146 -219 2542 -.30 45 45 | --- --- --- ---
Table 2.1511.4 GPS week: 1511 Day: 4 MJD: 54825
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 87| 5 0 20 4 10 -298 -.20 50 34 | 0 -177 3007 3094
cod 242| -4 0 -3 39 29 51 -.05 16 15 | --- --- --- ---
esx 132| -2 -4 -3 -57 0 68 .31 32 27 | 60328 362 8089 12548
iac n/a| 7 1 2 -59 -74 59 -.12 34 34 | 305813 -7728 7713 12540
mcc n/a| 9 -20 33 -27 1 1584 .25 111 111 | --- --- --- ---
Table 2.1511.5 GPS week: 1511 Day: 5 MJD: 54826
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 87| 4 2 25 87 -28 -220 -.17 70 43 | 0 35 2178 2257
cod 242| -3 1 -6 35 5 32 -.14 28 18 | --- --- --- ---
esx 132| -1 -4 -11 -130 9 41 .25 31 30 | 59693 14677 5576 14259
iac n/a| 11 -1 13 39 -32 17 -.04 49 49 | 298314 3125 5529 13991
mcc n/a| 3 26 20 264 -51 1104 .19 63 63 | --- --- --- ---
Table 2.1511.6 GPS week: 1511 Day: 6 MJD: 54827
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 87| 3 3 20 96 -120 -15 -.15 40 36 | 0 60 2384 2475
cod 242| -5 1 -7 10 29 -31 -.09 20 18 | --- --- --- ---
esx 132| 0 0 -5 -90 71 16 .36 41 30 | 108290 10 6853 12944
iac n/a| 7 -6 18 -11 -90 -6 -.13 144 144 | 347416 -4804 6803 12005
mcc n/a| 9 14 6 184 -159 1107 .47 55 55 | --- --- --- ---
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 3.1511.0 GPS week: 1511 Day: 0 MJD: 54821
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 1877 31 13 46 41 --- 18 | 217 229 36 58 --- 222
R06E | 9125 28 22 58 28 --- 19 | 27 52 78 44 --- 42
R07E | 1822 46 19 33 47 --- 20 | 24 41 54 60 --- 37
R10 | 2613 20 9 19 22 --- 9 | 30 30 35 51 --- 29
R11 | 1814 16 10 15 20 59 8 | 26 30 32 31 37 26
R13 | 1011 20 14 23 34 --- 12 | 27 34 50 36 --- 34
R14 | 1859 10 13 23 28 --- 11 | 22 26 35 31 --- 25
R15 | 3103 15 10 29 33 42 12 | 30 35 40 39 32 33
R17 | 1520 24 11 33 31 --- 13 | 40 61 76 44 --- 54
R18 | 1696 42 15 13 23 --- 13 | 25 54 40 55 --- 41
R19 | 1502 28 9 21 24 --- 11 | 42 78 73 81 --- 68
R20 | 5138 32 8 16 39 --- 13 | 34 55 57 66 --- 50
R21 | 4195 25 11 21 24 --- 11 | 48 75 71 75 --- 67
R22 | 3174 42 14 40 19 --- 16 | 51 83 108 81 --- 80
R23 | 2773 231 22 52 32 --- 24 | 773 980 960 944 --- 962
R24 | 3135 40 18 28 31 --- 16 | 75 101 103 79 --- 90
------+------------------------------------+--------------------------------
RMS | 3476 64 14 32 31 51 |T 93 122 115 110 34 116
WRMS | 3476 29 11 25 31 51 |NE 130 168 175 160 34 163
MEDI | 1877 28 13 23 28 42 |MD 30 54 54 55 32 42
Table 3.1511.1 GPS week: 1511 Day: 1 MJD: 54822
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2161 40 30 34 43 --- 21 | 129 142 68 67 --- 146
R06E | 9646 32 26 29 26 --- 16 | 32 42 50 26 --- 32
R07E | 1696 37 23 34 54 --- 21 | 33 38 47 71 --- 39
R10 | 3512 18 12 17 37 --- 12 | 20 23 43 41 --- 22
R11 | 1674 17 13 23 19 58 10 | 22 30 43 21 27 24
XR13 | 1462 --- 13 11 17 --- 9 | --- 24 31 25 --- 24
R14 | 1729 10 10 18 19 --- 8 | 18 19 28 22 --- 19
R15 | 2658 16 10 22 25 69 10 | 23 28 40 34 32 28
R17 | 2033 27 11 42 24 --- 15 | 28 47 71 51 --- 44
R18 | 1107 33 16 26 16 --- 13 | 15 45 51 37 --- 35
R19 | 917 27 23 22 13 --- 12 | 20 50 29 39 --- 32
R20 | 4552 33 17 16 46 --- 17 | 20 35 33 31 --- 26
R21 | 3584 13 14 29 24 --- 11 | 42 35 41 17 --- 30
R22 | 1991 16 7 24 16 --- 9 | 53 48 53 56 --- 50
R23 |11411 484 176 229 243 --- 149 | 730 9999 940 817 --- 944
R24 | 9682 27 23 53 16 --- 18 | 50 63 55 52 --- 49
------+------------------------------------+--------------------------------
RMS | 5121 127 48 65 69 64 |T 82 44 101 87 29 96
WRMS | 5121 27 15 25 69 64 |NE 132 37 157 134 29 147
MEDI | 2033 27 14 24 24 58 |MD 28 38 43 37 27 32
Table 3.1511.2 GPS week: 1511 Day: 2 MJD: 54823
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2541 105 32 39 68 --- 34 | 119 130 75 97 --- 134
R06E | 8455 27 28 17 42 --- 16 | 33 46 48 41 --- 37
R07E | 1658 31 28 33 70 --- 22 | 36 57 45 89 --- 48
R10 | 3388 23 18 27 41 --- 15 | 26 31 39 38 --- 29
R11 | 1936 26 14 32 21 58 13 | 27 25 45 23 27 25
XR13 | 1266 --- 11 13 15 --- 9 | --- 25 33 27 --- 25
R14 | 1242 17 10 15 25 --- 9 | 24 26 34 26 --- 25
R15 | 1287 14 13 12 28 56 9 | 25 37 41 35 36 33
R17 | 1003 15 14 27 27 --- 12 | 34 55 30 68 --- 44
R18 | 1075 24 10 39 44 --- 17 | 44 50 67 34 --- 48
R19 | 602 33 6 41 25 --- 16 | 55 65 102 58 --- 71
R20 | 3507 41 20 12 41 --- 16 | 21 64 43 49 --- 45
R21 | 2209 29 22 25 28 --- 14 | 35 66 60 37 --- 51
R22 | 1451 14 14 18 29 --- 10 | 37 49 50 31 --- 42
R23 | 4932 109 36 69 92 --- 42 | 273 300 301 327 --- 289
R24 | 9033 31 28 29 41 --- 18 | 64 84 118 105 --- 89
------+------------------------------------+--------------------------------
RMS | 3889 46 21 32 46 57 |T 56 69 70 67 31 64
WRMS | 3889 27 15 24 46 57 |NE 69 75 81 80 31 71
MEDI | 1658 27 14 27 29 56 |MD 35 50 45 38 27 44
Table 3.1511.3 GPS week: 1511 Day: 3 MJD: 54824
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4333 130 27 61 70 --- 42 | 148 172 96 56 --- 152
R06E | 8713 24 21 29 41 --- 16 | 27 35 53 40 --- 29
R07E | 4838 55 31 36 72 --- 27 | 29 45 50 67 --- 35
R10 | 2518 22 23 34 38 --- 17 | 34 35 42 48 --- 31
R11 | 1845 20 10 43 34 42 15 | 22 37 75 25 55 35
XR13 | 1162 --- 9 18 17 --- 10 | --- 36 47 37 --- 37
R14 | 2477 24 7 21 19 --- 10 | 29 30 42 34 --- 30
R15 | 1184 27 13 18 32 47 12 | 27 39 51 44 38 38
R17 | 978 19 15 22 31 --- 12 | 64 63 54 73 --- 59
R18 | 1823 21 18 39 16 --- 14 | 24 40 43 39 --- 29
R19 | 734 34 11 34 22 --- 14 | 39 68 92 67 --- 64
R20 | 1656 60 17 22 43 --- 20 | 38 57 46 72 --- 48
R21 | 1277 41 28 34 23 --- 18 | 35 78 49 60 --- 54
R22 | 1685 35 9 38 20 --- 15 | 48 64 89 79 --- 66
R23 | 1798 14 37 63 37 --- 24 | 316 394 359 346 --- 367
R24 | 6651 40 26 27 47 --- 20 | 77 96 100 115 --- 93
------+------------------------------------+--------------------------------
RMS | 3604 47 21 37 40 45 |T 63 80 80 75 46 72
WRMS | 3604 36 18 31 40 45 |NE 83 94 102 94 46 90
MEDI | 1798 27 17 34 32 42 |MD 35 45 51 56 38 38
Table 3.1511.4 GPS week: 1511 Day: 4 MJD: 54825
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3408 143 23 38 44 --- 35 | 208 264 44 39 --- 243
R06E |10495 23 18 36 37 --- 16 | 37 31 52 47 --- 33
R07E | 3619 43 12 26 33 --- 15 | 33 32 52 39 --- 33
R10 | 1817 24 18 31 51 --- 17 | 29 32 54 60 --- 32
R11 | 1883 23 14 21 27 110 11 | 24 32 37 22 53 23
R13 | 2144 28 16 59 34 --- 20 | 37 35 88 38 --- 42
R14 | 2358 28 7 15 18 --- 9 | 28 29 32 32 --- 27
R15 | 2421 48 11 30 34 112 16 | 21 21 37 29 65 22
R17 | 1910 26 17 22 32 --- 13 | 30 51 57 39 --- 43
R18 | 2587 24 13 29 27 --- 12 | 35 56 41 62 --- 48
R19 | 1640 31 14 16 20 --- 11 | 39 56 45 52 --- 47
R20 | 1952 44 11 21 40 --- 15 | 25 38 48 67 --- 41
R21 | 2446 43 11 42 22 --- 16 | 31 51 96 69 --- 60
R22 | 2476 36 16 28 31 --- 15 | 39 72 48 82 --- 61
R23 | 2226 47 22 32 43 --- 19 | 327 350 342 346 --- 345
R24 | 6434 46 17 35 35 --- 17 | 69 99 124 82 --- 94
------+------------------------------------+--------------------------------
RMS | 3816 50 16 32 34 111 |T 63 78 74 69 59 74
WRMS | 3816 34 15 27 34 111 |NE 71 86 95 83 59 82
MEDI | 2358 31 14 29 33 110 |MD 33 38 48 47 53 42
Table 3.1511.5 GPS week: 1511 Day: 5 MJD: 54826
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3138 220 78 35 65 --- 60 | 228 279 56 45 --- 218
R06E |12169 56 31 41 73 --- 27 | 38 39 72 62 --- 44
R07E | 2228 88 18 52 42 --- 28 | 21 35 32 53 --- 29
R10 | 847 22 18 20 51 --- 16 | 26 29 37 87 --- 26
R11 | 2553 22 18 24 45 47 15 | 17 21 43 37 18 21
R13 | 2536 20 11 33 38 --- 15 | 23 26 51 33 --- 27
R14 | 1657 22 11 16 37 --- 12 | 22 32 39 38 --- 29
R15 | 1573 32 14 27 50 75 17 | 24 36 51 40 36 34
R17 | 1998 20 25 30 51 --- 18 | 34 46 69 42 --- 42
R18 | 1896 17 17 30 40 --- 15 | 27 49 45 41 --- 38
R19 | 1407 32 19 13 51 --- 16 | 39 50 54 70 --- 48
R20 | 1739 45 17 24 67 --- 21 | 21 37 35 83 --- 35
R21 | 2738 46 10 28 25 --- 15 | 23 53 79 59 --- 55
R22 | 2610 56 18 29 27 --- 18 | 20 61 80 51 --- 56
R23 | 3341 40 27 32 45 --- 19 | 238 269 256 250 --- 258
R24 | 5808 75 32 40 51 --- 27 | 78 114 132 77 --- 99
------+------------------------------------+--------------------------------
RMS | 3981 70 28 31 49 63 |T 54 73 70 66 27 66
WRMS | 3981 43 18 30 49 63 |NE 57 75 90 71 27 70
MEDI | 2228 32 18 29 45 47 |MD 24 39 51 51 18 38
Table 3.1511.6 GPS week: 1511 Day: 6 MJD: 54827
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR04E |16378 1018 17 --- 135 --- 62 | 601 933 --- 42 --- 934
R06E |14103 47 24 50 66 --- 25 | 65 58 59 55 --- 53
R07E | 4401 59 26 45 65 --- 26 | 35 38 44 49 --- 32
R10M | 1489 67 21 48 482 --- 32 | 89 47 46 412 --- 49
R11 | 1869 20 15 21 62 66 15 | 30 21 34 31 31 22
R13 | 1748 25 14 34 52 --- 16 | 34 31 63 53 --- 38
R14 | 1235 20 12 17 35 --- 11 | 33 43 39 45 --- 37
R15 | 1616 25 15 24 47 41 14 | 25 30 41 29 46 24
R17 | 2101 45 21 96 95 --- 35 | 61 75 117 58 --- 72
R18M | 902 25 26 44 61 --- 20 | 42 73 83 48 --- 59
R19M | 1071 44 27 32 164 --- 35 | 42 80 83 151 --- 72
R20M | 1485 32 19 21 104 --- 23 | 41 61 61 137 --- 61
R21M | 2205 38 13 22 52 --- 16 | 40 76 84 100 --- 70
R22 | 2153 24 17 14 28 --- 11 | 46 82 77 68 --- 71
R23 | 3823 28 16 27 57 --- 16 | 317 363 346 348 --- 349
R24 | 2321 58 26 37 44 --- 23 | 119 163 151 128 --- 142
------+------------------------------------+--------------------------------
RMS | 4237 40 20 40 144 55 |T 101 135 88 109 38 130
WRMS | 4237 36 18 30 144 55 |NE 83 101 108 95 38 94
MEDI | 1869 32 17 32 61 41 |MD 42 61 63 55 31 59
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