[IGSREPORT-16873] Wk 1505 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Nov 27 08:15:51 PST 2008
******************************************************************************
IGS Electronic Report 27 Nov 08:15:53 PST 2008 Message Number 16873
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1505 (Nov 09, 2008 - Nov 15, 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 2.1505.
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:
igl1505[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1505 in the SP3 format.
igl15057.sum Combination Report for GPS Week 1505.
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 | 540.6 ns
1 | 531.8 ns
2 | 524.7 ns
3 | 514.2 ns
4 | 512.7 ns
5 | 509.5 ns
6 | 443.3 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
----+--------+---------------
3 | BKG | R22
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 1.1505, 1a.1505).
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 2.1505.0-6)
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 3.1505.0-6).
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 1505 summary. (Nov 09, 2008 - Nov 15, 2008)
Table 1.1505.a GPS week : 1505 MJD: 54779.0-54785.0
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 76| 0 0 4 16 0 -115 -.13 33 30 | 0 158 2484 2583
| 1 1 4 28 30 180 .06 | 0 281
cod 244| -3 0 -4 -2 18 31 -.10 23 20 | --- --- --- ---
| 1 1 3 24 13 56 .04 | --- ---
esx 124| 1 0 -6 25 19 62 .42 43 39 | 139482 3838 6755 27305
| 1 4 5 44 57 77 .08 | 29457 4147
iac n/a| 1 0 6 -11 -19 14 .01 35 35 | 512412 -1057 5844 12713
| 2 1 7 32 25 106 .03 | 32232 1989
mcc n/a| -3 -11 0 353 -124 -416 .67 296 296 | --- --- --- ---
| 25 21 45 432 248 2005 .65 | --- ---
Table 1.1505.b GPS week : 1505 MJD: 54779.0-54785.0
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 | 14 18 17 20 19 18 21 |
R06 | 21 20 23 15 30 31 23 |
R07 | 12 16 10 13 12 15 17 |
R09 | 0 0 0 --- 0 --- 0 |
R10 | 14 11 15 18 22 27 30 |
R11 | 24 13 17 15 14 25 25 |
R13 | 19 16 18 14 18 23 25 |
R14 | 16 18 20 23 21 23 24 |
R15 | 17 21 20 22 25 21 26 |
R17 | 19 19 12 18 15 15 18 |
R18 | 23 15 14 12 15 14 14 |
R19 | 14 10 19 12 15 16 17 |
R20 | 11 16 14 17 14 14 16 |
R21 | 20 24 18 16 24 24 18 |
R22 | 159 343 241 48 43 17 16 |
R23 | 21 18 17 13 12 16 15 |
R24 | 16 14 22 16 28 14 21 |
Table 1.1505.c GPS week : 1505 MJD: 54779.0-54785.0
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 1505 0 | -29 63 -169 151 -1747 -8677 92.3 5073 5073 | 540620 0
brd 1505 1 | 21 224 -130 -3797 2007 -12480 90.3 5089 5089 | 531773 0
brd 1505 2 | -198 55 -186 -2126 1587 -17670 99.2 3702 3702 | 524731 0
brd 1505 3 | -25 -188 -80 -110 2072 -18100 94.2 4228 4228 | 514219 0
brd 1505 4 | 189 -181 86 4360 2627 -18600 92.2 4288 4288 | 512673 0
brd 1505 5 | -69 38 211 610 6653 -21400 88.9 5725 5725 | 509516 0
brd 1505 6 | 196 -32 239 668 1464 -18220 86.2 6017 6017 | 443319 0
-------------+------------------------------------------------------------+----------------
brd 1505 mean| 12 -2 -4 -34 2094 -16449 91.9 4874 4874 | 510978 0
brd 1505 sdev| 141 146 181 2542 2465 4332 4.1 841 841 | 31868 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 2.1505.0 GPS week: 1505 Day: 0 MJD: 54779
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 76| 2 2 1 -26 -9 141 -.04 24 23 | 0 764 2510 2683
cod 244| -5 -1 -1 30 36 4 -.12 25 24 | --- --- --- ---
esx 124| 1 0 1 65 35 -56 .37 49 43 | 170524 -507 7554 38466
iac n/a| 2 2 -1 -27 -42 -73 -.00 28 28 | 542990 -4642 6207 11293
mcc n/a| 9 -36 19 812 -500 -1055 -.41 358 358 | --- --- --- ---
Table 2.1505.1 GPS week: 1505 Day: 1 MJD: 54780
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 76| 0 -1 6 -17 -13 -50 -.18 27 26 | 0 226 2257 2430
cod 244| -1 1 -5 -17 38 -44 -.07 19 16 | --- --- --- ---
esx 124| 3 3 -2 -17 -14 123 .48 40 33 | 160904 -572 7203 36202
iac n/a| -3 0 0 16 -48 -32 .04 35 35 | 532974 -2462 6258 13231
mcc n/a| 39 -14 72 1087 -216 1163 1.63 265 265 | --- --- --- ---
Table 2.1505.2 GPS week: 1505 Day: 2 MJD: 54781
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 76| -1 0 10 36 -19 -68 -.11 30 26 | 0 -9 2323 2413
cod 244| -1 0 -4 -31 14 22 -.11 19 17 | --- --- --- ---
esx 124| 0 -4 -6 -23 103 21 .45 39 35 | 145914 11623 7177 28783
iac n/a| 1 1 0 26 -34 51 -.01 35 35 | 524786 51 5769 10053
mcc n/a| -38 32 13 -67 -165 -4249 .33 385 385 | --- --- --- ---
Table 2.1505.3 GPS week: 1505 Day: 3 MJD: 54782
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 76| 1 0 8 34 -44 -338 -.20 26 24 | 0 63 2785 2852
cod 244| -3 0 -3 -8 16 52 -.10 20 18 | --- --- --- ---
esx 124| 2 -5 -15 6 41 127 .56 42 43 | 149892 2823 6965 14409
iac n/a| 1 0 3 6 -24 234 .03 31 31 | 516697 899 6880 13197
mcc n/a| -26 -7 -29 82 270 -1369 .68 257 257 | --- --- --- ---
Table 2.1505.4 GPS week: 1505 Day: 4 MJD: 54783
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 76| -1 -1 0 10 45 40 -.20 38 30 | 0 -63 2856 2920
cod 244| -2 1 -4 -9 5 1 -.18 30 24 | --- --- --- ---
esx 124| 1 0 -12 28 -74 32 .40 42 37 | 133683 3409 6999 29751
iac n/a| 2 -1 12 -3 16 -62 -.03 42 42 | 516593 -1645 5786 18349
mcc n/a| -7 -27 -60 71 21 279 1.14 225 225 | --- --- --- ---
Table 2.1505.5 GPS week: 1505 Day: 5 MJD: 54784
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 76| 1 -3 0 44 4 -224 -.11 41 37 | 0 64 2271 2333
cod 244| -2 1 -1 31 2 47 -.09 20 19 | --- --- --- ---
esx 124| 0 0 -4 100 -10 162 .42 51 45 | 135872 5321 4453 15505
iac n/a| 3 0 11 -67 11 -34 .05 36 36 | 508801 636 4537 10913
mcc n/a| 3 -11 -35 144 -287 852 .87 221 221 | --- --- --- ---
Table 2.1505.6 GPS week: 1505 Day: 6 MJD: 54785
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 76| 1 -2 2 30 31 -309 -.08 45 42 | 0 66 2386 2450
cod 244| -5 -1 -12 -11 18 134 -.07 24 22 | --- --- --- ---
esx 124| 1 5 -3 16 58 27 .29 40 38 | 79587 4775 6934 28025
iac n/a| 1 0 19 -27 -15 18 .00 39 39 | 444046 -241 5471 11955
mcc n/a| -7 -15 21 341 5 1465 .46 360 360 | --- --- --- ---
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 3.1505.0 GPS week: 1505 Day: 0 MJD: 54779
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2649 11 23 42 19 --- 13 | 40 38 50 35 --- 35
R06 | 8419 38 36 49 20 --- 20 | 67 84 102 78 --- 77
R07 | 1700 24 17 28 16 --- 12 | 30 31 44 31 --- 29
XR09E |17797 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 2104 21 21 30 22 --- 13 | 33 37 40 39 --- 30
R11E | 3779 26 26 81 39 447 24 | 37 47 56 46 111 34
R13E | 4727 26 18 59 32 --- 19 | 55 62 83 69 --- 59
R14E | 1294 14 19 40 35 --- 15 | 33 37 39 31 --- 25
R15E | 4914 22 15 40 37 365 16 | 40 34 52 42 53 33
R17 |10546 37 22 52 18 --- 18 | 44 54 77 46 --- 46
R18 | 9016 24 36 63 37 --- 22 | 76 97 86 56 --- 73
R19 | 2049 15 22 42 22 --- 14 | 65 65 74 57 --- 62
R20 | 1580 13 12 36 18 --- 11 | 57 58 60 60 --- 55
R21 | 4615 22 37 34 40 --- 19 | 225 234 236 231 --- 230
XR22 |15029 --- 146 --- 172 --- 158 | --- 127 --- 212 --- 130
R23 | 2763 12 26 73 30 --- 20 | 58 39 111 40 --- 50
R24 | 3190 30 26 27 22 226 15 | 291 274 278 282 214 280
------+------------------------------------+--------------------------------
RMS | 5073 24 25 49 28 358 |T 76 82 92 84 126 78
WRMS | 5073 23 24 43 28 358 |NE 95 100 111 102 214 97
MEDI | 3779 22 22 40 22 365 |MD 55 54 74 46 111 50
Table 3.1505.1 GPS week: 1505 Day: 1 MJD: 54780
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 4771 30 23 31 40 --- 17 | 40 46 53 28 --- 36
R06 |12006 33 17 56 35 --- 20 | 105 114 136 126 --- 115
R07 | 2971 27 27 25 33 --- 16 | 28 39 44 39 --- 29
XR09E |11314 --- --- 10 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 1970 7 14 27 24 --- 10 | 13 19 35 29 --- 16
R11E | 2131 20 16 22 33 349 13 | 26 39 49 42 318 29
R13E | 6478 25 20 38 30 --- 15 | 45 44 48 49 --- 37
R14E | 1589 23 18 44 44 --- 18 | 33 38 66 45 --- 34
R15E | 5510 24 28 52 46 127 21 | 22 37 43 43 138 20
R17 | 3455 44 13 46 28 --- 19 | 23 32 60 41 --- 28
R18 | 9938 21 20 26 36 --- 14 | 40 51 61 32 --- 42
R19 | 1395 20 11 24 18 --- 10 | 49 45 45 41 --- 44
R20 | 2098 27 20 25 41 --- 16 | 63 62 60 53 --- 55
R21 | 2096 27 22 73 42 --- 23 | 159 162 170 152 --- 158
XR22 |14565 --- 243 --- 483 --- 343 | --- 178 --- 469 --- 135
R23 | 2035 24 16 38 49 --- 18 | 38 51 76 42 --- 47
R24 | 1942 34 12 29 12 268 13 | 230 221 243 224 348 228
------+------------------------------------+--------------------------------
RMS | 5088 27 19 40 35 265 |T 60 73 79 90 268 65
WRMS | 5088 26 16 33 35 265 |NE 77 91 94 113 348 83
MEDI | 2971 25 18 29 35 268 |MD 40 45 60 42 318 37
Table 3.1505.2 GPS week: 1505 Day: 2 MJD: 54781
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 5169 25 21 46 28 --- 17 | 34 42 65 48 --- 34
R06 | 8718 53 27 47 31 --- 22 | 73 127 122 87 --- 101
R07 | 4282 11 11 23 22 --- 9 | 27 30 25 32 --- 24
XR09E |14795 --- --- 10 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 2326 21 13 41 29 --- 14 | 27 26 50 44 --- 27
R11E | 2811 26 16 44 32 448 16 | 28 35 69 40 318 34
R13E | 2729 23 13 53 31 --- 17 | 51 44 66 56 --- 43
R14E | 1362 20 25 46 47 --- 19 | 35 43 41 57 --- 36
R15E | 2434 24 17 40 58 301 20 | 23 35 57 70 80 35
R17 | 2768 22 11 27 21 --- 11 | 41 51 63 38 --- 46
R18 | 3623 39 16 17 16 --- 14 | 29 46 49 45 --- 36
R19 | 1023 26 25 54 31 --- 19 | 31 40 56 53 --- 34
R20 | 1026 21 21 20 32 --- 13 | 52 54 65 47 --- 51
R21 | 2158 31 21 28 45 --- 18 | 200 214 205 201 --- 205
XR22 |17338 --- 173 --- 335 --- 241 | --- 148 --- 383 --- 159
R23 | 4917 26 19 42 33 --- 16 | 34 49 58 30 --- 37
R24 | 2047 50 25 35 45 393 22 | 215 253 239 263 427 242
------+------------------------------------+--------------------------------
RMS | 3701 30 19 39 35 385 |T 60 77 82 93 275 71
WRMS | 3701 26 17 35 35 385 |NE 73 95 94 111 427 88
MEDI | 2768 25 19 40 31 393 |MD 34 44 63 48 318 36
Table 3.1505.3 GPS week: 1505 Day: 3 MJD: 54782
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2932 27 27 62 21 --- 19 | 37 42 75 48 --- 38
R06 |11924 20 24 30 32 --- 15 | 133 148 139 131 --- 138
R07 | 3468 22 17 38 14 --- 13 | 33 37 65 48 --- 38
R10E | 3749 22 18 58 30 --- 18 | 41 31 31 35 --- 25
R11E | 1927 27 18 34 23 314 14 | 35 47 56 53 147 42
R13E | 2099 23 17 17 33 --- 13 | 42 37 33 45 --- 32
R14E | 2368 27 23 67 49 --- 23 | 33 23 70 55 --- 26
R15E | 5862 25 26 48 52 153 21 | 34 30 51 71 47 32
R17 | 2206 15 23 52 37 --- 18 | 42 45 79 31 --- 40
R18 | 1589 15 9 38 23 --- 12 | 38 43 74 45 --- 44
R19 | 1361 27 14 22 15 --- 11 | 71 61 68 50 --- 59
R20 | 1528 39 19 39 21 --- 17 | 51 50 73 36 --- 41
R21 | 2593 39 20 18 27 --- 15 | 134 151 159 158 --- 148
XR22 |14501 426 37 --- 59 --- 47 | 67 100 --- 191 --- 115
R23 | 4754 15 16 36 23 --- 12 | 27 30 52 30 --- 26
R24 | 1513 26 24 22 32 278 15 | 114 110 119 117 263 112
------+------------------------------------+--------------------------------
RMS | 4228 26 20 42 31 257 |T 58 61 76 71 152 59
WRMS | 4228 24 18 43 31 257 |NE 67 74 90 80 263 72
MEDI | 2368 25 19 38 27 278 |MD 41 43 70 48 147 40
Table 3.1505.4 GPS week: 1505 Day: 4 MJD: 54783
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2251 36 28 39 26 --- 18 | 29 40 66 41 --- 39
R06 | 9468 49 54 69 25 --- 29 | 64 153 136 141 --- 117
R07 | 3253 22 21 21 14 --- 11 | 31 31 44 28 --- 26
XR09E | 5494 --- --- 10 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 3620 22 26 61 39 --- 22 | 38 49 57 57 --- 41
R11E | 1371 22 21 28 24 228 13 | 36 31 30 29 85 22
R13E | 2696 32 21 38 36 --- 18 | 31 22 41 43 --- 24
R14E | 3931 28 28 35 50 --- 20 | 35 55 46 76 --- 46
R15E | 4939 41 21 50 58 103 25 | 34 25 51 63 40 28
R17 | 2381 27 15 40 20 --- 15 | 35 48 95 56 --- 53
R18 | 1783 24 23 28 25 --- 14 | 38 58 66 40 --- 46
R19 | 1399 14 20 43 23 --- 15 | 46 36 81 29 --- 41
R20 | 1532 34 20 23 13 --- 13 | 47 68 72 49 --- 57
R21 | 8132 67 21 48 19 --- 24 | 173 213 234 196 --- 202
R22 | 1857 41 66 42 118 --- 43 | 69 110 42 148 --- 73
R23 | 5120 17 14 25 24 --- 11 | 42 36 55 42 --- 37
R24 | 4216 72 29 55 35 298 28 | 180 235 248 234 108 220
------+------------------------------------+--------------------------------
RMS | 4287 38 30 42 42 225 |T 58 75 85 79 77 67
WRMS | 4287 30 24 37 42 225 |NE 68 93 103 91 108 82
MEDI | 3253 28 21 39 25 228 |MD 38 48 57 49 85 41
Table 3.1505.5 GPS week: 1505 Day: 5 MJD: 54784
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1242 38 24 32 31 --- 17 | 26 39 51 44 --- 32
R06 |12685 89 10 61 55 --- 30 | 145 194 218 216 --- 192
R07 | 1325 29 9 46 21 --- 14 | 25 27 55 36 --- 26
R10E | 2572 47 24 72 55 --- 27 | 36 42 75 68 --- 40
R11E | 2629 28 31 79 35 165 24 | 39 39 58 42 58 30
R13E | 3016 39 22 62 48 --- 23 | 41 20 58 46 --- 23
R14E | 4540 50 21 45 47 --- 22 | 36 46 61 69 --- 43
R15E | 8768 29 27 29 53 67 20 | 28 25 39 63 26 27
R17 | 2600 23 22 44 19 --- 15 | 61 39 60 40 --- 44
R18 | 5399 21 20 36 24 --- 14 | 65 59 68 65 --- 60
R19 | 1380 34 17 44 23 --- 16 | 54 52 44 38 --- 43
R20 | 1999 40 15 25 22 --- 14 | 34 39 40 28 --- 31
R21 | 5131 52 16 69 37 --- 23 | 277 290 291 304 --- 289
R22 | 8610 35 16 52 23 --- 17 | 40 122 63 67 --- 94
R23 | 1246 35 20 44 19 --- 16 | 23 44 59 17 --- 26
R24 | 9811 23 16 32 28 338 13 | 270 267 248 237 74 256
------+------------------------------------+--------------------------------
RMS | 5725 41 20 51 36 221 |T 75 84 93 86 52 78
WRMS | 5725 37 19 45 36 221 |NE 92 106 108 99 74 99
MEDI | 2629 35 20 44 28 165 |MD 39 42 59 46 58 40
Table 3.1505.6 GPS week: 1505 Day: 6 MJD: 54785
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1589 39 30 48 25 --- 20 | 34 52 70 43 --- 40
R06 |14225 67 17 43 36 --- 23 | 90 121 125 131 --- 115
R07 | 4713 38 20 31 31 --- 16 | 33 35 48 30 --- 30
XR09E |15568 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 3299 64 34 48 68 --- 30 | 65 98 79 86 --- 75
R11E | 2297 31 27 58 53 166 24 | 30 33 74 50 116 34
R13E | 1950 53 31 45 45 --- 24 | 61 32 65 51 --- 36
R14E | 5942 54 23 41 51 --- 23 | 42 43 44 61 --- 35
R15E | 9016 50 39 29 56 53 25 | 58 24 29 64 46 31
R17 | 1617 23 26 44 25 --- 17 | 51 63 67 46 --- 49
R18 | 2857 30 16 27 27 --- 14 | 71 71 86 68 --- 69
R19 | 1261 33 22 43 14 --- 16 | 71 61 101 65 --- 69
R20 | 2315 33 19 31 27 --- 15 | 47 44 43 43 --- 37
R21 | 2303 50 14 27 33 --- 17 | 316 315 312 314 --- 313
R22 | 5423 30 19 39 24 --- 16 | 52 125 34 154 --- 107
R23 | 806 33 16 38 19 --- 15 | 44 25 46 21 --- 23
R24 |12749 56 21 28 43 599 21 | 281 302 299 281 204 291
------+------------------------------------+--------------------------------
RMS | 6017 45 24 40 39 360 |T 84 90 95 94 122 84
WRMS | 6017 42 22 38 39 360 |NE 99 110 111 108 204 103
MEDI | 2857 38 21 39 31 166 |MD 52 52 67 61 116 40
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