[IGSREPORT-16711] Wk 1497 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Tue Oct 14 05:02:30 PDT 2008
******************************************************************************
IGS Electronic Report 14 Oct 05:02:37 PDT 2008 Message Number 16711
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1497 (Sep 14, 2008 - Sep 20, 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 2.1497.
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:
igl1497[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1497 in the SP3 format.
igl14977.sum Combination Report for GPS Week 1497.
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 | 650.3 ns
1 | 586.2 ns
2 | 649.7 ns
3 | 536.3 ns
4 | 563.5 ns
5 | 609.8 ns
6 | 650.6 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 1.1497, 1a.1497).
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 2.1497.0-6)
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 3.1497.0-6).
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 1497 summary. (Sep 14, 2008 - Sep 20, 2008)
Table 1.1497.a GPS week : 1497 MJD: 54723.0-54729.0
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 62| 1 -1 -2 36 -21 -118 -.03 63 39 | 0 -15 2237 2336
| 2 2 5 42 59 220 .09 | 0 338
cod 212| -5 0 0 0 -18 92 -.17 44 25 | --- --- --- ---
| 2 2 4 60 56 63 .06 | --- ---
esx 127| 3 1 10 -29 87 45 .35 58 43 | 102801 2172 7604 23711
| 3 4 9 33 38 126 .07 | 43069 4789
iac n/a| 2 0 -7 8 -9 38 -.12 54 54 | 609344 -735 6460 14615
| 3 3 4 40 53 192 .10 | 45760 4023
mcc n/a| 10 7 54 92 25 -1570 .34 222 222 | --- --- --- ---
| 12 18 20 195 119 2225 1.05 | --- ---
Table 1.1497.b GPS week : 1497 MJD: 54723.0-54729.0
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 | 0 0 0 0 0 0 0 |
R04 | 22 17 57 46 43 21 32 |
R06 | 29 20 23 19 29 23 24 |
R07 | 15 15 17 11 13 13 17 |
R09 | 0 0 0 0 0 --- 0 |
R10 | 19 15 18 20 17 14 16 |
R11 | 20 19 15 15 17 16 19 |
R13 | 13 12 16 20 24 15 19 |
R14 | 19 14 10 11 15 13 18 |
R15 | 15 16 9 11 13 13 14 |
R17 | 31 32 40 31 27 25 29 |
R19 | 32 40 58 34 43 49 32 |
R20 | 30 32 38 22 19 29 22 |
R23 | 41 48 35 47 51 44 42 |
R24 | 24 106 175 20 18 15 18 |
Table 1.1497.c GPS week : 1497 MJD: 54723.0-54729.0
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 1497 0 | 139 79 227 1167 2244 -16610 91.6 4157 4157 | 650260 0
brd 1497 1 | 292 208 751 7404 2420 -54560 <<<< >>>>> >>>>> | 586228 0
brd 1497 2 | -176 -221 195 -818 387 -12880 99.2 2704 2704 | 649719 0
brd 1497 3 | -125 222 76 -4742 1014 -11520 100.4 2807 2807 | 536257 0
brd 1497 4 | 166 115 76 -824 4075 -8579 98.5 4294 4294 | 563499 0
brd 1497 5 | 133 30 198 6740 -532 -3696 95.1 4125 4125 | 609818 0
brd 1497 6 | -133 47 309 -1084 4399 -5527 92.5 4354 4354 | 650627 0
-------------+------------------------------------------------------------+----------------
brd 1497 mean| 42 68 262 1120 2001 -16196 -16.4 >>>>> >>>>> | 606629 0
brd 1497 sdev| 183 147 231 4431 1838 17478 297.9 >>>>> >>>>> | 46430 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 2.1497.0 GPS week: 1497 Day: 0 MJD: 54723
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 62| 2 4 -7 24 28 -167 .05 50 40 | 0 22 2026 2119
cod 212| -4 -2 2 -18 -112 186 -.17 30 26 | --- --- --- ---
esx 127| 2 -2 -1 -25 91 66 .40 53 44 | 126624 5946 8637 21055
iac n/a| -2 4 -3 25 12 -195 -.03 44 44 | 650981 4906 7563 14253
mcc n/a| 3 -9 36 105 90 -1116 -1.08 133 133 | --- --- --- ---
Table 2.1497.1 GPS week: 1497 Day: 1 MJD: 54724
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 62| 0 -4 -2 38 92 -112 -.09 80 44 | 0 -622 1630 1739
cod 212| -6 -1 4 4 -69 90 -.24 49 28 | --- --- --- ---
esx 127| 6 2 1 -14 63 -25 .42 56 36 | 81481 857 10345 26163
iac n/a| 7 0 -6 77 51 -2 -.10 85 85 | 592140 -5120 7825 18725
mcc n/a| 8 1 34 79 143 -836 -.16 160 160 | --- --- --- ---
Table 2.1497.2 GPS week: 1497 Day: 2 MJD: 54725
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 62| 5 -2 -5 0 -69 17 .06 152 48 | 0 -59 2209 2263
cod 212| -9 2 3 71 -2 39 -.08 82 25 | --- --- --- ---
esx 127| 0 -2 8 -71 54 -92 .23 104 42 | 143444 7818 6857 24757
iac n/a| 4 1 -6 -13 31 65 .02 80 80 | 652618 -851 6368 12543
mcc n/a| 17 -2 69 515 145 -766 1.15 379 379 | --- --- --- ---
Table 2.1497.3 GPS week: 1497 Day: 3 MJD: 54726
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 62| 4 -4 3 11 -44 108 .06 47 42 | 0 422 1948 2025
cod 212| -3 0 2 18 19 62 -.25 31 20 | --- --- --- ---
esx 127| -1 2 19 -2 56 -104 .41 49 45 | 34422 -1498 6909 26761
iac n/a| 6 2 -15 -30 -107 -23 -.18 44 44 | 540207 -1803 4720 12496
mcc n/a| 33 45 61 -71 -79 -6552 2.15 263 263 | --- --- --- ---
Table 2.1497.4 GPS week: 1497 Day: 4 MJD: 54727
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 62| 1 0 1 4 -63 72 -.06 51 38 | 0 319 2380 2520
cod 212| -5 -5 3 54 26 41 -.17 46 22 | --- --- --- ---
esx 127| 3 1 6 -42 113 74 .36 45 56 | 67668 6768 4808 19484
iac n/a| 2 2 -9 3 -17 -112 -.13 40 40 | 563612 3786 4795 15602
mcc n/a| -4 10 86 34 45 -798 .20 198 198 | --- --- --- ---
Table 2.1497.5 GPS week: 1497 Day: 5 MJD: 54728
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 62| 0 -2 1 57 -41 -209 -.07 32 30 | 0 -130 3215 3387
cod 212| -4 1 -9 -22 42 48 -.11 32 22 | --- --- --- ---
esx 127| 3 2 11 -70 75 207 .37 48 34 | 113957 -5030 8281 22655
iac n/a| 0 -3 -1 36 -45 144 -.27 40 40 | 614505 -5673 7896 19361
mcc n/a| 5 16 63 -1 10 -941 -.26 150 150 | --- --- --- ---
Table 2.1497.6 GPS week: 1497 Day: 6 MJD: 54729
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 62| 1 -1 -9 122 -53 -536 -.17 30 30 | 0 -59 2254 2299
cod 212| -7 0 0 -111 -34 177 -.19 41 33 | --- --- --- ---
esx 127| 8 9 25 17 160 192 .27 54 42 | 152011 345 7397 25107
iac n/a| 0 -4 -5 -37 5 393 -.13 43 43 | 651346 -392 6058 9326
mcc n/a| 6 -6 34 -14 -179 17 .37 273 273 | --- --- --- ---
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 3.1497.0 GPS week: 1497 Day: 0 MJD: 54723
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 13 --- --- --- 0 | --- 43 --- --- --- 44
R04 | 2406 34 25 47 44 --- 21 | 51 70 47 44 --- 48
R06 | 8030 69 23 74 25 --- 28 | 144 115 111 128 --- 115
R07 | 4914 33 21 20 31 --- 15 | 24 39 34 28 --- 25
XR09 | 9169 --- --- 9 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1977 19 26 44 40 --- 19 | 38 39 34 58 --- 30
R11 | 9031 26 35 44 33 118 20 | 23 46 29 50 56 34
R13 | 1503 21 22 17 25 --- 12 | 38 38 22 37 --- 29
R14 | 1942 38 26 22 42 --- 18 | 23 20 33 39 --- 17
R15 | 1172 16 26 23 32 147 15 | 33 55 37 34 33 39
R17E | 4293 65 38 63 53 --- 31 | 48 49 42 35 --- 28
R19E | 1484 82 28 50 59 --- 31 | 66 31 22 60 --- 35
R20E | 1818 53 38 54 63 --- 29 | 73 51 50 75 --- 53
R23E | 1165 81 37 108 58 --- 41 | 62 40 122 74 --- 54
R24E | 3475 40 34 42 48 --- 23 | 530 629 602 578 --- 589
------+------------------------------------+--------------------------------
RMS | 4157 50 30 53 44 133 |T 88 90 91 95 44 81
WRMS | 4157 40 26 44 44 133 |NE 46 51 43 52 44 42
MEDI | 1977 38 26 44 42 118 |MD 48 43 37 50 33 35
Table 3.1497.1 GPS week: 1497 Day: 1 MJD: 54724
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 9 --- --- --- 0 | --- 70 --- --- --- 71
R04 |>>>>> 51 13 21 29 --- 17 | 75 59 42 48 --- 51
R06 |>>>>> 54 28 24 26 --- 19 | 182 208 205 212 --- 202
R07 |>>>>> 36 23 26 16 --- 15 | 32 57 40 33 --- 39
XR09 |>>>>> --- --- 8 --- --- 0 | --- --- 9999 --- --- 9999
R10 |>>>>> 28 25 26 20 --- 14 | 36 38 45 46 --- 37
R11 |>>>>> 23 29 44 25 138 18 | 24 37 43 40 113 31
R13 |>>>>> 22 20 20 21 --- 12 | 42 55 39 49 --- 41
R14 |>>>>> 35 16 26 17 --- 13 | 37 24 21 27 --- 22
R15 |>>>>> 28 23 33 23 179 15 | 25 41 54 24 53 34
R17E |>>>>> 60 44 45 73 --- 31 | 27 40 65 53 --- 26
R19E |>>>>> 77 48 61 93 --- 39 | 40 48 34 82 --- 36
R20E |>>>>> 75 38 43 66 --- 31 | 56 52 52 73 --- 43
R23E |>>>>> 112 56 80 91 --- 48 | 69 51 80 100 --- 44
R24E |>>>>> 214 136 141 254 --- 105 | 431 614 611 361 --- 508
------+------------------------------------+--------------------------------
RMS |>>>>> 80 49 56 85 160 |T 82 99 102 88 83 84
WRMS |>>>>> 44 28 36 85 160 |NE 56 65 61 59 83 58
MEDI |>>>>> 51 25 26 26 138 |MD 40 51 45 49 53 39
Table 3.1497.2 GPS week: 1497 Day: 2 MJD: 54725
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 8 --- --- --- 0 | --- 55 --- --- --- 57
XR04 |13632 131 54 --- 69 --- 56 | 167 110 --- 48 --- 77
R06 | 2452 58 29 55 26 --- 23 | 122 152 199 154 --- 154
R07 | 1560 34 17 50 13 --- 16 | 23 27 47 18 --- 13
XR09 | 8278 --- --- 9 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1891 45 23 38 25 --- 18 | 44 35 38 24 --- 22
R11 | 1206 26 23 33 19 147 14 | 43 47 48 34 102 37
R13 | 4974 21 21 36 29 --- 16 | 33 46 56 41 --- 36
R14 | 1888 29 13 18 13 --- 10 | 26 26 30 32 --- 22
R15 | 4333 18 10 17 16 163 9 | 50 28 48 23 72 31
R17E | 1639 74 43 93 71 --- 40 | 27 45 116 58 --- 42
XR19E | 708 146 58 --- 54 --- 57 | 145 43 --- 75 --- 63
R20E | 1318 76 60 55 71 --- 38 | 56 81 64 86 --- 62
R23E | 2338 101 40 50 55 --- 34 | 59 76 87 115 --- 71
R24E | 3156 473 252 310 234 619 175 | 357 686 734 431 318 524
------+------------------------------------+--------------------------------
RMS | 2703 152 82 104 80 379 |T 88 104 133 87 164 86
WRMS | 2703 48 25 42 80 379 |NE 63 58 66 46 87 49
MEDI | 1891 58 23 38 29 163 |MD 50 46 56 48 102 42
Table 3.1497.3 GPS week: 1497 Day: 3 MJD: 54726
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 58 --- --- --- 58
XR04 |14163 --- 39 --- 53 --- 46 | --- 77 --- 102 --- 81
R06 | 3207 22 32 49 24 --- 19 | 307 295 307 323 --- 307
R07 | 1416 17 20 22 17 --- 11 | 40 42 56 38 --- 39
XR09 |11746 --- --- 14 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2220 27 27 41 44 --- 20 | 60 50 46 77 --- 50
XR11 | 3192 --- 17 25 23 380 15 | --- 40 35 23 68 28
R13 | 4911 26 23 60 21 --- 19 | 41 45 50 57 --- 39
R14 | 3596 16 16 27 17 --- 11 | 46 42 42 28 --- 35
XR15 | 8729 --- 10 17 17 359 10 | --- 32 40 32 48 31
R17E | 2189 61 40 29 70 --- 30 | 27 52 29 76 --- 31
XR19E | 1024 --- 29 --- 39 --- 34 | --- 21 --- 46 --- 28
R20E | 2000 44 29 44 38 --- 22 | 70 56 48 77 --- 52
R23E | 973 103 56 91 75 --- 46 | 69 55 100 109 --- 63
R24E | 2627 36 16 44 43 263 20 | 375 374 362 375 53 371
------+------------------------------------+--------------------------------
RMS | 2807 47 31 49 44 263 |T 115 88 101 104 56 86
WRMS | 2807 42 20 45 44 263 |NE 98 75 82 85 58 74
MEDI | 2627 27 23 29 38 359 |MD 60 50 48 76 53 39
Table 3.1497.4 GPS week: 1497 Day: 4 MJD: 54727
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 34 --- --- --- 34
R04 | 9872 86 85 57 67 --- 43 | 128 86 116 70 --- 76
R06 | 3727 42 56 54 47 --- 29 | 128 148 129 121 --- 125
R07 | 2135 18 24 30 13 --- 12 | 26 32 53 27 --- 28
XR09 |16006 --- --- 10 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2228 37 27 31 18 --- 16 | 21 37 57 34 --- 33
R11 | 1403 38 24 29 27 104 17 | 49 35 37 25 44 28
R13 | 1422 52 15 62 19 --- 23 | 56 52 47 37 --- 38
R14 | 5949 12 14 32 33 --- 14 | 26 16 36 39 --- 21
R15 | 4031 21 21 24 24 69 13 | 52 38 44 38 42 37
R17E | 2755 33 48 35 59 --- 26 | 25 49 46 61 --- 29
XR19E | 1666 --- 45 --- 41 --- 43 | --- 19 --- 63 --- 45
R20E | 4012 34 25 34 34 --- 18 | 42 35 54 48 --- 29
R23E | 2895 114 95 82 54 --- 50 | 71 107 97 87 --- 73
R24E | 3561 33 23 28 37 319 17 | 260 272 266 284 57 269
------+------------------------------------+--------------------------------
RMS | 4294 51 46 45 40 197 |T 73 68 81 71 47 61
WRMS | 4294 38 22 56 40 197 |NE 60 53 64 48 43 46
MEDI | 2895 34 24 32 34 104 |MD 49 37 53 48 44 34
Table 3.1497.5 GPS week: 1497 Day: 5 MJD: 54728
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 54 --- --- --- 56
R04 | 2169 29 19 66 24 --- 21 | 66 49 44 49 --- 40
R06 | 2391 30 52 33 34 --- 22 | 268 256 234 261 --- 253
R07 | 1688 25 14 28 20 --- 12 | 23 33 53 35 --- 31
R10 | 2231 31 15 30 19 --- 14 | 42 33 31 38 --- 32
R11 | 3244 18 24 35 30 105 15 | 20 14 41 29 42 15
R13 | 6289 26 18 26 33 --- 15 | 15 32 41 33 --- 15
R14 | 2866 21 13 31 23 --- 12 | 41 29 27 33 --- 28
R15 | 7955 16 19 30 24 70 12 | 28 45 32 37 72 33
R17E | 5744 37 39 35 58 --- 24 | 32 48 29 53 --- 28
XR19E | 1084 88 44 --- 71 --- 49 | 47 21 --- 48 --- 34
R20E | 3742 45 35 39 74 --- 28 | 18 45 49 67 --- 28
R23E | 1328 57 68 114 62 --- 44 | 76 66 101 100 --- 63
R24E | 3944 22 17 27 38 228 15 | 219 242 224 245 119 230
------+------------------------------------+--------------------------------
RMS | 4124 32 32 48 40 150 |T 68 69 75 79 77 63
WRMS | 4124 30 22 34 40 150 |NE 62 60 62 64 57 55
MEDI | 2866 29 19 31 33 105 |MD 41 45 41 48 72 32
Table 3.1497.6 GPS week: 1497 Day: 6 MJD: 54729
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 12 --- --- --- 0 | --- 70 --- --- --- 68
R04 | 2171 35 78 36 53 --- 31 | 47 117 36 47 --- 54
R06 | 4436 34 35 52 47 --- 23 | 272 291 309 290 --- 285
R07 | 1415 33 20 41 17 --- 16 | 22 28 33 20 --- 19
XR09 | 9744 --- --- 21 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1271 27 18 31 32 --- 15 | 49 37 24 33 --- 32
R11 | 1342 21 16 62 29 84 19 | 49 33 83 29 53 35
R13 | 2325 36 29 36 29 --- 19 | 33 36 47 29 --- 21
R14 | 2606 12 21 43 45 --- 17 | 36 18 53 22 --- 22
R15 | 6830 17 15 42 21 115 13 | 45 50 36 48 82 40
R17E | 8654 39 64 48 48 --- 29 | 48 65 27 45 --- 36
XR19E | 1891 48 24 --- 60 --- 32 | 32 27 --- 53 --- 26
R20E | 2516 26 30 49 47 --- 21 | 32 40 53 49 --- 30
R23E | 1747 41 67 112 75 --- 41 | 55 65 98 83 --- 43
R24E | 7380 17 22 48 38 451 17 | 347 373 387 345 154 363
------+------------------------------------+--------------------------------
RMS | 4353 30 41 54 43 273 |T 82 89 98 84 96 76
WRMS | 4353 30 33 42 43 273 |NE 69 75 77 64 67 64
MEDI | 2325 33 22 43 45 115 |MD 47 40 47 47 82 35
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