[IGSREPORT-17065] Wk 1514 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jan 29 05:08:07 PST 2009
******************************************************************************
IGS Electronic Report 29 Jan 05:08:10 PST 2009 Message Number 17065
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1514 (Jan 11, 2009 - Jan 17, 2009)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the centers
absolute deviation to the unweighted average orbit after removing small
differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1514.
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:
igl1514[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1514 in the SP3 format.
igl15147.sum Combination Report for GPS Week 1514.
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 | 303.6 ns
1 | 291.9 ns
2 | 281.7 ns
3 | 287.7 ns
4 | 283.9 ns
5 | 288.0 ns
6 | 186.3 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 | R06
0 | COD | R06
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 1.1514, 1a.1514).
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 2.1514.0-6)
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 3.1514.0-6).
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 1514 summary. (Jan 11, 2009 - Jan 17, 2009)
Table 1.1514.a GPS week : 1514 MJD: 54842.0-54848.0
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| 0 -2 10 -9 4 -8 -.08 42 46 | 0 89 2575 2730
| 1 0 3 38 28 100 .04 | 0 702
cod 244| -1 2 -5 24 13 26 -.09 82 15 | --- --- --- ---
| 1 2 2 21 23 30 .03 | --- ---
esx 128| 1 0 -2 -39 15 1 .46 32 29 | 97115 2374 6478 14549
| 1 2 4 51 42 86 .05 | 43853 6173
iac n/a| 1 -3 -1 -2 -22 -20 -.12 26 26 | 275438 -836 6263 11719
| 1 2 7 33 26 42 .04 | 40513 2096
mcc n/a| 3 -5 25 71 -2 833 -.31 311 311 | --- --- --- ---
| 14 14 19 225 225 465 .42 | --- ---
Table 1.1514.b GPS week : 1514 MJD: 54842.0-54848.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R02 | --- --- --- --- 0 0 53 |
R03 | 0 176 190 98 45 27 17 |
R04 | 16 27 18 14 18 15 13 |
R06 | 38 --- --- --- --- --- 0 |
R07 | 35 16 8 8 10 9 7 |
R09 | 0 --- --- --- --- --- --- |
R10 | 10 12 9 10 12 11 10 |
R11 | 15 13 10 14 16 12 12 |
R13 | 12 15 13 12 8 8 10 |
R14 | 9 14 10 16 10 9 9 |
R15 | 15 14 10 9 12 11 12 |
R17 | 13 12 15 14 17 16 16 |
R18 | 13 12 11 11 9 10 11 |
R19 | 14 12 11 12 13 11 11 |
R20 | 18 14 16 20 14 19 18 |
R21 | 11 10 10 15 17 11 12 |
R22 | 11 10 12 13 15 18 11 |
R23 | 25 19 19 21 14 11 14 |
R24 | 25 11 17 14 13 12 13 |
Table 1.1514.c GPS week : 1514 MJD: 54842.0-54848.0
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 1514 0 | -37 -69 218 -1101 -3717 -20750 88.3 6240 6240 | 303558 0
brd 1514 1 | -30 -10 330 -3977 -1756 -23570 92.3 3446 3446 | 291947 0
brd 1514 2 | -5 30 198 -1609 -4207 -28810 90.4 3339 3339 | 281683 0
brd 1514 3 | 8 155 98 -1181 -1713 -23290 88.0 3243 3243 | 287715 0
brd 1514 4 | -32 112 -55 -165 -1243 -17410 90.2 2505 2505 | 283944 0
brd 1514 5 | -17 115 77 199 -1388 -17880 91.4 3036 3036 | 287973 0
brd 1514 6 | -34 -16 57 253 583 -12830 91.7 2975 2975 | 186347 0
-------------+------------------------------------------------------------+----------------
brd 1514 mean| -21 45 132 -1082 -1920 -20648 90.3 3540 3540 | 274738 0
brd 1514 sdev| 17 83 126 1468 1609 5186 1.6 1229 1229 | 39615 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 2.1514.0 GPS week: 1514 Day: 0 MJD: 54842
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| 0 -1 12 37 50 61 -.15 166 202 | 0 102 1928 1985
cod 244| -1 6 -9 -4 16 64 -.13 479 23 | --- --- --- ---
esx 128| -1 0 4 -109 -51 -27 .46 33 31 | 114452 12255 7715 34778
iac n/a| 2 -4 -3 49 29 -70 -.04 28 28 | 305047 -474 6340 14240
mcc n/a| 23 3 11 37 410 1000 .16 194 194 | --- --- --- ---
Table 2.1514.1 GPS week: 1514 Day: 1 MJD: 54843
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 9 -31 2 34 -.04 27 24 | 0 1478 3492 3801
cod 244| -2 4 -6 24 -10 -4 -.09 14 13 | --- --- --- ---
esx 128| 3 -2 -9 -68 0 54 .43 41 34 | 122219 5362 7303 15038
iac n/a| 2 -5 7 11 -32 -42 -.12 27 27 | 295147 -3340 7295 15253
mcc n/a| -5 -2 6 0 107 1094 -.40 314 314 | --- --- --- ---
Table 2.1514.2 GPS week: 1514 Day: 2 MJD: 54844
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| 0 -1 6 -55 -3 125 -.08 20 18 | 0 24 2321 2479
cod 244| 0 3 -6 49 26 -8 -.07 16 14 | --- --- --- ---
esx 128| 0 -1 -5 4 10 -137 .44 29 25 | 112597 3242 6470 9955
iac n/a| -1 -3 7 -20 -24 -61 -.11 27 27 | 282208 83 6464 10052
mcc n/a| -9 -3 3 46 -203 1305 -.18 401 401 | --- --- --- ---
Table 2.1514.3 GPS week: 1514 Day: 3 MJD: 54845
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| -2 -3 9 -48 -45 23 -.08 21 20 | 0 -28 2277 2353
cod 244| 0 2 -1 56 57 12 -.12 20 17 | --- --- --- ---
esx 128| 4 2 -4 8 89 -75 .54 35 33 | 122024 -6636 5016 11454
iac n/a| 0 -3 -4 -50 -59 19 -.15 23 23 | 289243 -2490 5014 11775
mcc n/a| 0 3 46 -69 -39 1297 -1.01 574 574 | --- --- --- ---
Table 2.1514.4 GPS week: 1514 Day: 4 MJD: 54846
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| 0 -1 14 -13 18 -96 -.08 22 21 | 0 122 2160 2211
cod 244| -1 1 -1 18 1 48 -.11 15 13 | --- --- --- ---
esx 128| 2 0 -6 19 17 53 .50 33 30 | 106664 3217 5497 8513
iac n/a| 0 -3 -11 -15 -31 -38 -.15 27 27 | 282460 2481 5515 8613
mcc n/a| -1 12 51 -180 67 186 -.72 338 338 | --- --- --- ---
Table 2.1514.5 GPS week: 1514 Day: 5 MJD: 54847
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| 0 -1 13 30 1 -170 -.06 21 19 | 0 -194 2327 2402
cod 244| 0 0 -4 17 6 58 -.05 14 12 | --- --- --- ---
esx 128| 1 2 0 -89 5 115 .39 29 26 | 102839 -3871 5585 10343
iac n/a| 1 -4 -5 28 -21 12 -.10 25 25 | 288654 -2685 5593 10786
mcc n/a| -8 -21 40 530 -103 262 .03 149 149 | --- --- --- ---
Table 2.1514.6 GPS week: 1514 Day: 6 MJD: 54848
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 5 18 7 -41 -.10 20 19 | 0 -876 3523 3884
cod 244| 0 2 -4 10 -4 10 -.09 15 13 | --- --- --- ---
esx 128| 0 1 0 -44 37 26 .44 25 24 | -987 3049 7760 11763
iac n/a| 2 0 -2 -17 -19 35 -.15 26 26 | 185313 568 7621 11319
mcc n/a| 23 -29 20 136 -258 688 -.09 208 208 | --- --- --- ---
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 3.1514.0 GPS week: 1514 Day: 0 MJD: 54842
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR03E | ---- --- 8 --- --- --- 0 | --- 153 --- --- --- 175
R04E | 3715 28 26 34 22 --- 15 | 75 83 97 78 --- 79
R06E |21093 651 1915 30 42 --- 38 | 2 9999 6 2 --- 9999
R07 | 952 84 61 57 41 --- 35 | 65 150 157 96 --- 110
XR09 |13169 --- --- 10 --- --- 0 | --- --- 3 --- --- 5
R10 | 1213 16 11 28 15 --- 10 | 28 28 34 29 --- 28
R11 | 1653 31 20 38 9 97 14 | 26 34 63 41 41 37
R13 | 1828 18 17 31 17 --- 12 | 26 29 57 32 --- 28
R14 | 2296 17 12 21 9 --- 8 | 26 29 42 30 --- 28
R15 | 2724 19 24 37 21 87 14 | 24 30 45 29 32 25
R17 | 1080 24 13 29 23 --- 12 | 39 58 64 46 --- 50
R18 | 989 32 22 25 13 --- 13 | 26 48 53 34 --- 37
R19 | 1055 31 18 26 20 --- 13 | 42 69 71 52 --- 57
R20 | 1717 28 26 38 29 --- 17 | 34 62 42 54 --- 46
R21 | 902 20 15 24 19 --- 11 | 52 60 68 69 --- 61
R22 | 670 21 14 30 11 --- 11 | 56 72 52 64 --- 60
R23 | 1199 50 27 21 57 --- 24 | 48 46 54 35 --- 38
R24 |11580 50 44 34 40 309 24 | 206 255 246 227 146 234
------+------------------------------------+--------------------------------
RMS | 6239 166 479 33 28 194 |T 48 75 67 57 73 64
WRMS | 6239 202 23 31 28 194 |NE 49 69 70 59 73 56
MEDI | 1653 28 20 30 20 97 |MD 34 58 54 41 41 46
Table 3.1514.1 GPS week: 1514 Day: 1 MJD: 54843
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR03E | ---- --- 123 --- 247 --- 175 | --- 155 --- 168 --- 142
R04E | 3567 47 24 90 39 --- 27 | 95 111 163 95 --- 106
R07 | 968 36 9 44 31 --- 16 | 53 56 84 74 --- 59
R10 | 1903 21 14 32 21 --- 12 | 27 42 58 33 --- 36
R11 | 759 33 13 27 18 90 12 | 21 33 37 26 38 26
R13 | 1921 29 10 54 14 --- 15 | 20 27 69 29 --- 29
R14 | 2521 19 14 29 35 --- 13 | 27 26 45 29 --- 25
R15 | 2093 19 12 35 34 75 13 | 16 18 33 26 22 14
R17 | 1236 12 17 34 24 --- 12 | 37 52 38 27 --- 37
R18 | 1147 19 12 39 13 --- 11 | 23 38 63 28 --- 32
R19 | 1272 19 12 30 23 --- 11 | 57 69 55 52 --- 58
R20 | 1715 30 18 26 25 --- 13 | 24 33 46 35 --- 26
R21 | 2383 20 8 30 18 --- 10 | 26 43 49 44 --- 38
R22 | 847 21 9 23 20 --- 10 | 63 52 41 40 --- 48
R23 | 1281 39 18 44 41 --- 19 | 62 46 73 56 --- 52
R24 |11418 21 12 22 22 532 10 | 212 212 211 200 247 208
------+------------------------------------+--------------------------------
RMS | 3446 27 14 41 27 314 |T 50 63 71 60 102 58
WRMS | 3446 24 12 34 27 314 |NE 47 53 64 49 102 49
MEDI | 1715 21 12 32 23 90 |MD 27 43 55 35 38 37
Table 3.1514.2 GPS week: 1514 Day: 2 MJD: 54844
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR03E | ---- --- 136 --- 264 --- 189 | --- 172 --- 228 --- 166
R04 | 3273 33 22 38 34 --- 18 | 61 84 88 82 --- 74
R07 | 1793 12 10 20 16 --- 8 | 49 49 55 43 --- 46
R10 | 3452 16 12 20 16 --- 9 | 23 37 43 34 --- 31
R11 | 1581 18 11 17 23 80 10 | 30 39 36 39 43 32
R13 | 1570 14 15 35 31 --- 13 | 29 35 49 29 --- 29
R14 | 3319 15 16 20 22 --- 10 | 27 29 30 27 --- 24
R15 | 2099 17 11 10 26 65 9 | 18 31 33 31 41 24
R17 | 1428 23 15 39 26 --- 14 | 23 49 70 28 --- 38
R18 | 1312 9 13 36 11 --- 10 | 37 42 28 36 --- 34
R19 | 966 15 13 17 28 --- 10 | 46 64 69 59 --- 56
R20 | 1714 20 22 33 35 --- 15 | 30 48 57 44 --- 39
R21 | 3118 11 9 23 28 --- 10 | 27 38 48 22 --- 29
R22 | 802 10 12 27 31 --- 11 | 39 41 60 66 --- 46
R23 | 1568 29 28 37 40 --- 19 | 34 44 51 35 --- 33
R24 |10026 37 19 41 17 687 17 | 88 125 137 110 577 112
------+------------------------------------+--------------------------------
RMS | 3338 20 16 29 27 401 |T 37 57 56 57 220 50
WRMS | 3338 18 14 25 27 401 |NE 35 47 54 43 220 40
MEDI | 1714 16 13 27 26 80 |MD 30 42 51 36 43 34
Table 3.1514.3 GPS week: 1514 Day: 3 MJD: 54845
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR03E | ---- --- 87 --- 109 --- 98 | --- 190 --- 110 --- 135
R04 | 3941 20 25 28 20 --- 13 | 122 119 137 132 --- 125
R07 | 2277 15 11 17 14 --- 8 | 52 50 65 51 --- 51
R10 | 4188 17 10 28 17 --- 10 | 29 31 46 37 --- 32
R11 | 2421 24 16 36 24 78 14 | 25 42 48 28 68 28
R13 | 1457 18 13 32 23 --- 12 | 21 30 38 28 --- 25
R14 | 2444 10 25 55 16 --- 16 | 28 37 63 29 --- 31
R15 | 3635 15 11 17 19 90 9 | 21 34 30 28 25 24
R17 | 1820 17 22 22 32 --- 14 | 50 54 57 44 --- 49
R18 | 1011 21 9 30 15 --- 10 | 25 42 68 40 --- 39
R19 | 920 18 18 26 19 --- 11 | 44 64 59 49 --- 51
R20 | 1537 27 30 50 30 --- 19 | 26 45 62 26 --- 29
R21 | 2726 21 14 53 14 --- 15 | 36 32 66 29 --- 31
R22 | 886 23 13 34 22 --- 13 | 29 45 58 27 --- 34
R23 | 2249 37 35 28 39 --- 20 | 46 32 60 47 --- 35
R24 | 8456 20 20 35 24 986 14 | 117 129 158 134 699 130
------+------------------------------------+--------------------------------
RMS | 3243 21 20 35 23 573 |T 44 61 67 52 264 53
WRMS | 3243 20 17 33 23 573 |NE 39 47 62 42 264 42
MEDI | 2277 20 16 30 20 90 |MD 29 42 60 37 68 34
Table 3.1514.4 GPS week: 1514 Day: 4 MJD: 54846
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | ---- --- 3 --- --- --- 0 | --- 60 --- --- --- 61
XR03 |10841 84 42 --- 70 --- 45 | 486 84 --- 85 --- 98
R04 | 3200 29 24 52 22 --- 18 | 69 84 79 76 --- 73
R07 | 1993 18 7 28 13 --- 9 | 33 34 43 35 --- 32
R10 | 3787 22 13 27 25 --- 12 | 19 21 34 37 --- 21
R11 | 2931 21 22 40 31 71 16 | 24 29 36 36 37 21
R13 | 1585 15 6 21 13 --- 8 | 30 31 46 29 --- 31
R14 | 1660 19 8 29 15 --- 10 | 23 25 30 23 --- 21
R15 | 4397 17 13 37 16 132 11 | 19 29 45 27 26 24
R17 | 2618 19 15 51 35 --- 16 | 35 37 85 42 --- 43
R18 | 698 18 8 19 20 --- 9 | 34 38 56 36 --- 38
R19 | 591 33 9 19 27 --- 13 | 28 43 48 56 --- 38
R20 | 1893 15 16 16 45 --- 14 | 29 36 57 32 --- 35
R21 | 1601 20 8 41 46 --- 16 | 46 41 82 28 --- 41
R22 | 1100 24 18 37 26 --- 14 | 26 31 53 27 --- 24
R23 | 1243 23 18 28 26 --- 13 | 36 35 27 28 --- 26
R24 | 3968 30 21 22 14 565 13 | 94 131 119 111 312 115
------+------------------------------------+--------------------------------
RMS | 2504 22 15 33 27 338 |T 64 46 56 44 125 43
WRMS | 2504 21 13 30 27 338 |NE 34 40 54 39 125 36
MEDI | 1893 20 13 28 25 132 |MD 30 36 48 35 37 35
Table 3.1514.5 GPS week: 1514 Day: 5 MJD: 54847
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | ---- --- 4 --- --- --- 0 | --- 29 --- --- --- 35
XR03 | 3467 47 32 --- 37 --- 27 | 487 96 --- 83 --- 98
R04 | 1401 33 24 22 26 --- 15 | 121 130 145 127 --- 128
R07 | 1595 18 8 19 17 --- 8 | 39 46 51 45 --- 43
R10 | 4352 15 12 27 22 --- 10 | 23 26 40 27 --- 24
R11 | 3216 23 12 31 13 83 11 | 23 30 50 29 29 28
R13 | 1771 15 8 15 16 --- 7 | 24 26 39 27 --- 26
R14 | 1485 22 5 19 16 --- 9 | 23 27 56 29 --- 30
R15 | 2126 13 7 30 26 127 11 | 24 25 29 28 20 21
R17 | 1988 24 16 26 45 --- 16 | 15 32 36 39 --- 28
R18 | 789 14 14 24 19 --- 10 | 23 24 38 25 --- 22
R19 | 683 18 12 24 20 --- 10 | 18 30 47 39 --- 28
R20 | 1356 24 22 47 38 --- 18 | 20 28 41 18 --- 20
R21 | 1089 15 14 24 21 --- 10 | 37 57 58 40 --- 47
R22 | 1397 19 18 51 38 --- 18 | 23 34 63 21 --- 25
R23 | 953 23 11 20 20 --- 10 | 19 27 31 34 --- 22
R24 | 9148 25 15 24 20 209 12 | 77 83 81 80 211 78
------+------------------------------------+--------------------------------
RMS | 3036 21 14 29 25 149 |T 62 44 53 43 86 41
WRMS | 3036 19 12 26 25 149 |NE 27 35 47 34 86 31
MEDI | 1485 19 12 24 20 127 |MD 23 30 47 29 29 28
Table 3.1514.6 GPS week: 1514 Day: 6 MJD: 54848
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 6357 103 49 --- 70 --- 53 | 23 45 --- 26 --- 47
XR03 | 6763 19 11 --- 39 --- 16 | 482 82 --- 74 --- 80
R04 | 1503 23 12 31 26 --- 13 | 104 105 124 106 --- 108
XR06 | ---- --- 3 --- --- --- 0 | --- 9999 --- --- --- 9999
R07 | 4577 9 9 15 13 --- 6 | 36 41 36 47 --- 38
R10 | 3334 10 14 24 18 --- 9 | 24 20 33 31 --- 24
R11 | 3571 15 13 33 20 106 11 | 30 32 34 33 36 29
R13 | 2876 15 12 21 22 --- 10 | 27 34 36 26 --- 27
R14 | 1248 18 10 16 13 --- 8 | 30 29 35 28 --- 27
R15 | 2039 20 16 27 24 125 12 | 34 30 40 25 25 27
R17 | 1965 19 21 20 44 --- 15 | 29 48 60 50 --- 43
R18 | 869 17 15 24 22 --- 11 | 23 40 36 34 --- 30
R19 | 1529 13 18 18 24 --- 10 | 40 51 53 66 --- 49
R20 | 1133 41 10 22 44 --- 17 | 31 39 45 40 --- 35
R21 | 889 16 17 33 14 --- 12 | 41 51 57 43 --- 45
R22 | 796 20 15 13 24 --- 10 | 46 51 52 32 --- 43
R23 | 1075 25 11 35 28 --- 14 | 50 49 61 56 --- 50
R24 | 7798 17 19 29 27 321 13 | 120 142 135 129 301 130
------+------------------------------------+--------------------------------
RMS | 2974 20 15 25 26 208 |T 68 52 55 49 120 48
WRMS | 2974 19 13 24 26 208 |NE 40 46 50 45 120 42
MEDI | 1965 18 13 24 24 125 |MD 34 45 45 40 36 43
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