[IGSREPORT-18233] Wk 1566 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jan 28 05:03:48 PST 2010
******************************************************************************
IGS Electronic Report 28 Jan 05:04:11 PST 2010 Message Number 18233
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1566 (Jan 10, 2010 - Jan 16, 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 2.1566.
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:
igl1566[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1566 in the SP3 format.
igl15667.sum Combination Report for GPS Week 1566.
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 | 399.5 ns
1 | 421.9 ns
2 | 475.2 ns
3 | 426.7 ns
4 | 463.1 ns
5 | 385.9 ns
6 | 471.9 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 1.1566, 1a.1566).
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 2.1566.0-6)
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 3.1566.0-6).
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 1566 summary. (Jan 10, 2010 - Jan 16, 2010)
Table 1.1566.a GPS week : 1566 MJD: 55206.0-55212.0
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 129| 0 1 5 -1 0 28 -.10 19 19 | 0 -430 2220 2437
| 0 1 1 38 39 122 .04 | 0 894
cod 239| -1 -1 -4 48 -12 18 -.12 12 12 | --- --- --- ---
| 0 1 1 18 23 50 .02 | --- ---
esx 140| -1 0 -2 -85 28 -31 .43 23 22 | 88770 1823 4272 10293
| 2 2 1 26 43 53 .04 | 38452 6136
iac n/a| 1 1 3 -30 -12 -43 -.08 24 24 | 435062 -553 4282 8995
| 1 1 5 22 27 90 .04 | 35364 2903
mcc n/a| 8 0 49 -119 -101 -119 -.71 180 180 | --- --- --- ---
| 8 10 33 143 123 1037 .79 | --- ---
Table 1.1566.b GPS week : 1566 MJD: 55206.0-55212.0
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 | 9 11 9 10 11 8 11 |
R03 | 16 8 11 10 8 11 7 |
R04 | --- --- --- --- --- --- 0 |
R05 | 13 8 7 11 11 11 7 |
R07 | 9 9 8 9 10 10 10 |
R08 | 9 7 11 10 11 9 7 |
R10 | 14 14 11 14 9 11 10 |
R11 | 15 13 13 12 12 9 11 |
R13 | 7 13 13 12 13 9 11 |
R14 | 9 9 13 12 10 10 8 |
R15 | 12 11 15 12 11 13 12 |
R17 | 14 12 13 13 14 12 13 |
R18 | 10 8 9 10 7 11 10 |
R19 | 13 10 6 9 10 8 9 |
R20 | 16 15 12 10 9 10 18 |
R21 | 12 9 15 15 9 8 13 |
R23 | 28 27 61 80 48 53 55 |
Table 1.1566.c GPS week : 1566 MJD: 55206.0-55212.0
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 1566 0 | 18 9 57 -54 3634 -13990 83.5 2546 2546 | 399469 0
brd 1566 1 | 104 -41 -42 2789 2255 -17050 86.2 2415 2415 | 421921 0
brd 1566 2 | 78 -78 42 1306 934 -17320 87.3 1804 1804 | 475209 0
brd 1566 3 | -18 55 140 1055 -906 -21880 85.5 2369 2369 | 426704 0
brd 1566 4 | 45 42 159 575 -480 -27370 86.7 2930 2930 | 463064 0
brd 1566 5 | -87 6 -57 -2033 495 -22000 88.0 2784 2784 | 385930 0
brd 1566 6 | 194 41 80 -1369 3476 -12390 85.1 2522 2522 | 471859 0
-------------+------------------------------------------------------------+----------------
brd 1566 mean| 47 5 54 323 1344 -18857 86.1 2481 2481 | 434879 0
brd 1566 sdev| 90 49 82 1643 1821 5206 1.5 359 359 | 35760 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 2.1566.0 GPS week: 1566 Day: 0 MJD: 55206
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 129| 1 2 6 8 39 190 -.10 20 20 | 0 -1 1781 1838
cod 239| 0 0 0 38 -45 -54 -.13 14 14 | --- --- --- ---
esx 140| -4 0 -2 -74 -1 -102 .37 25 24 | 56459 -3319 4724 16808
iac n/a| 3 0 -4 5 13 -32 -.04 27 27 | 401319 -4127 4763 9728
mcc n/a| 1 3 7 -3 -55 31 -.54 108 108 | --- --- --- ---
Table 2.1566.1 GPS week: 1566 Day: 1 MJD: 55207
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 129| 1 0 7 63 68 -115 -.06 19 19 | 0 -1632 2228 2356
cod 239| -2 0 -6 25 -15 2 -.11 11 10 | --- --- --- ---
esx 140| -1 -1 -3 -122 -34 26 .45 24 23 | 68052 7195 3602 8728
iac n/a| 3 1 4 -10 18 83 -.09 22 22 | 419976 2007 3612 8486
mcc n/a| 5 8 28 -43 29 547 -.07 93 93 | --- --- --- ---
Table 2.1566.2 GPS week: 1566 Day: 2 MJD: 55208
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 129| 1 1 6 3 -8 73 -.11 18 18 | 0 349 1703 1816
cod 239| -2 0 -3 45 6 1 -.14 14 14 | --- --- --- ---
esx 140| 2 -4 -3 -112 46 -92 .45 24 23 | 132600 2480 4002 8528
iac n/a| 0 3 -3 -34 -26 58 -.08 24 24 | 476844 -2773 4010 8230
mcc n/a| -1 12 46 1 -168 1394 -.25 119 119 | --- --- --- ---
Table 2.1566.3 GPS week: 1566 Day: 3 MJD: 55209
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 129| 0 1 6 -1 -43 62 -.04 21 21 | 0 59 1942 2082
cod 239| 0 0 -5 52 -2 -10 -.10 12 12 | --- --- --- ---
esx 140| -2 -1 -4 -84 96 15 .47 26 24 | 88836 5802 3754 8782
iac n/a| 2 1 6 -55 -33 -51 -.02 22 22 | 425050 1287 3751 8470
mcc n/a| 12 -2 77 -214 -134 -1234 -2.07 372 372 | --- --- --- ---
Table 2.1566.4 GPS week: 1566 Day: 4 MJD: 55210
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 129| 0 0 3 -58 -20 135 -.12 20 20 | 0 204 2577 2872
cod 239| -2 -2 -5 77 0 23 -.08 10 10 | --- --- --- ---
esx 140| 0 3 0 -78 63 -63 .40 21 21 | 126731 9185 5141 10854
iac n/a| 0 1 10 -57 -56 -176 -.16 24 24 | 462691 3249 5138 9592
mcc n/a| 10 1 20 -122 -271 -1478 -1.41 172 172 | --- --- --- ---
Table 2.1566.5 GPS week: 1566 Day: 5 MJD: 55211
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 129| 1 2 5 -37 -30 -135 -.14 18 19 | 0 -1795 3294 3918
cod 239| -1 -3 -3 66 12 95 -.14 11 10 | --- --- --- ---
esx 140| -2 0 -3 -84 17 -3 .43 19 19 | 31810 -7860 4691 10669
iac n/a| 1 3 7 -33 -2 -107 -.08 23 23 | 388109 -3426 4696 10741
mcc n/a| 24 -20 62 -54 72 -598 .18 171 171 | --- --- --- ---
Table 2.1566.6 GPS week: 1566 Day: 6 MJD: 55212
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 129| 0 2 5 10 -3 -10 -.12 15 15 | 0 -194 2017 2182
cod 239| 0 -3 -3 33 -45 67 -.13 15 14 | --- --- --- ---
esx 140| 1 1 -1 -43 13 2 .40 19 18 | 116905 -716 3994 7688
iac n/a| 1 0 0 -25 0 -81 -.09 26 26 | 471448 -90 4004 7724
mcc n/a| 4 1 103 -397 -186 499 -.84 221 221 | --- --- --- ---
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 3.1566.0 GPS week: 1566 Day: 0 MJD: 55206
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1414 14 8 14 22 --- 8 | 34 29 31 32 --- 29
R03 | 1476 35 10 27 39 --- 16 | 39 33 35 34 --- 31
R05 | 4718 15 10 31 35 --- 13 | 31 22 31 42 --- 27
R07 | 1536 10 9 21 21 --- 8 | 19 20 23 33 --- 19
R08 | 2552 14 10 24 14 98 9 | 17 23 33 26 45 21
R10 | 3502 29 16 22 26 --- 13 | 37 23 31 20 --- 20
R11 | 2271 22 13 36 32 157 14 | 26 25 49 31 26 24
R13 | 2398 13 8 15 13 --- 7 | 28 24 32 26 --- 24
R14 | 5250 13 5 18 24 --- 8 | 22 24 37 28 --- 24
R15 | 1598 18 16 23 27 31 11 | 21 35 33 20 104 25
R17 | 1618 16 25 13 39 --- 14 | 38 49 45 41 --- 41
R18 | 732 17 18 15 16 --- 10 | 34 32 28 27 --- 27
R19 | 593 19 12 34 20 --- 12 | 49 63 76 63 --- 59
R20 | 2018 29 16 39 31 --- 16 | 22 24 39 32 --- 22
R21 | 1000 13 18 22 30 --- 12 | 31 46 52 33 --- 38
XR23 | ---- --- 19 --- 39 --- 27 | --- 52 --- 47 --- 46
------+------------------------------------+--------------------------------
RMS | 2545 20 14 25 27 108 |T 29 32 38 33 58 29
WRMS | 2545 20 14 24 27 108 |NE 29 32 38 33 58 29
MEDI | 1618 16 12 22 26 98 |MD 31 25 33 32 45 25
Table 3.1566.1 GPS week: 1566 Day: 1 MJD: 55207
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1348 24 12 23 18 --- 10 | 23 21 23 25 --- 17
R03 | 1699 14 8 17 19 --- 8 | 19 25 39 27 --- 23
R05 | 3068 12 8 18 16 --- 7 | 31 22 26 39 --- 24
R07 | 1260 17 8 17 21 --- 8 | 22 18 29 30 --- 19
R08 | 2848 13 6 11 17 60 6 | 18 23 25 29 52 19
R10 | 2375 30 17 33 20 --- 14 | 29 28 37 24 --- 21
R11 | 2625 19 15 30 27 143 12 | 19 31 44 23 31 23
R13 | 2799 28 12 33 14 --- 12 | 26 21 28 15 --- 17
R14 | 4484 14 11 20 19 --- 9 | 19 26 33 25 --- 23
R15 | 2741 19 11 21 29 46 11 | 23 26 34 20 74 22
R17 | 1638 20 9 31 28 --- 12 | 20 36 54 23 --- 29
R18 | 1298 8 8 15 19 --- 7 | 26 22 34 22 --- 22
R19 | 656 21 8 20 24 --- 10 | 58 54 58 60 --- 54
R20 | 3192 22 14 32 35 --- 14 | 31 29 47 30 --- 29
R21 | 815 14 10 20 18 --- 8 | 23 35 46 28 --- 31
XR23 | ---- --- 18 --- 38 --- 26 | --- 47 --- 61 --- 49
------+------------------------------------+--------------------------------
RMS | 2415 19 11 24 22 93 |T 25 29 37 30 52 26
WRMS | 2415 19 10 23 22 93 |NE 25 29 37 30 52 26
MEDI | 2375 19 10 20 19 60 |MD 23 26 34 25 52 23
Table 3.1566.2 GPS week: 1566 Day: 2 MJD: 55208
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1155 19 12 19 12 --- 9 | 24 26 39 27 --- 26
R03 | 1296 19 13 24 19 --- 10 | 33 33 50 33 --- 32
R05 | 1698 12 9 11 18 --- 7 | 30 26 34 36 --- 28
R07 | 2077 8 9 23 15 --- 8 | 19 19 36 24 --- 21
R08 | 1298 17 9 28 21 143 10 | 20 21 29 30 135 17
R10 | 1152 18 12 21 24 --- 10 | 29 25 32 33 --- 25
R11 | 1679 17 12 27 36 126 13 | 28 26 39 36 66 24
R13 | 2599 25 9 30 30 --- 13 | 28 30 48 26 --- 29
R14 | 3120 20 23 28 15 --- 13 | 24 29 50 36 --- 29
R15 | 2686 16 22 19 40 77 14 | 28 26 40 34 208 27
R17 | 1162 18 19 32 17 --- 12 | 28 51 26 49 --- 36
R18 | 972 20 6 21 16 --- 9 | 21 24 37 29 --- 21
R19 | 888 6 10 11 14 --- 6 | 38 48 44 44 --- 42
R20 | 2063 18 6 20 35 --- 11 | 17 20 27 26 --- 17
R21 | 1309 22 16 35 30 --- 14 | 21 41 58 41 --- 33
XR23 | ---- --- 44 --- 83 --- 60 | --- 72 --- 58 --- 58
------+------------------------------------+--------------------------------
RMS | 1804 18 14 24 24 119 |T 25 32 39 35 136 29
WRMS | 1804 18 14 23 24 119 |NE 25 32 39 35 136 29
MEDI | 1309 18 12 23 19 126 |MD 28 26 39 33 135 27
Table 3.1566.3 GPS week: 1566 Day: 3 MJD: 55209
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1171 23 9 24 16 --- 10 | 24 25 40 27 --- 25
R03 | 1008 16 14 22 17 --- 10 | 27 30 36 39 --- 29
R05 | 4522 19 9 23 27 --- 11 | 26 34 45 45 --- 34
R07 | 4437 15 8 14 21 --- 8 | 15 23 31 33 --- 22
R08 | 1179 22 10 16 22 144 10 | 25 34 25 41 115 29
R10 | 1240 26 11 40 18 --- 13 | 22 23 47 31 --- 22
R11 | 869 21 9 35 19 195 12 | 30 24 43 24 78 24
R13 | 2601 17 9 33 21 --- 11 | 23 31 60 24 --- 27
R14 | 2693 20 18 29 20 --- 12 | 37 33 49 34 --- 33
R15 | 4232 18 16 18 32 597 12 | 35 31 39 27 209 29
R17 | 1251 14 13 33 29 --- 13 | 39 53 74 33 --- 48
R18 | 1226 17 16 22 13 --- 9 | 34 40 23 31 --- 30
R19 | 728 19 11 17 16 --- 9 | 33 43 46 37 --- 37
R20 | 1350 24 11 15 16 --- 9 | 29 23 29 28 --- 22
R21 | 793 33 15 31 28 --- 15 | 33 34 23 29 --- 22
XR23 | 6564 --- 59 --- 107 --- 80 | --- 101 --- 80 --- 87
------+------------------------------------+--------------------------------
RMS | 2369 21 12 26 22 372 |T 28 36 40 35 134 32
WRMS | 2369 21 12 24 22 372 |NE 28 36 40 35 134 32
MEDI | 1240 19 11 23 20 195 |MD 29 31 40 31 115 29
Table 3.1566.4 GPS week: 1566 Day: 4 MJD: 55210
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2811 27 9 14 25 --- 10 | 25 24 24 35 --- 21
R03 | 1064 12 8 15 24 --- 8 | 25 33 26 31 --- 25
R05 | 5926 20 13 17 28 --- 11 | 23 35 39 31 --- 29
R07 | 3221 14 11 25 23 --- 10 | 32 29 40 39 --- 30
R08 | 815 31 9 15 19 109 10 | 20 22 32 28 60 19
R10 | 1623 19 9 18 21 --- 9 | 24 26 39 35 --- 26
R11 | 1460 26 9 26 23 218 11 | 20 27 35 32 41 21
R13 | 2515 19 16 22 33 --- 12 | 25 31 33 21 --- 22
R14 | 4540 18 9 26 19 --- 10 | 25 26 39 22 --- 21
R15 | 5424 13 12 22 27 --- 10 | 21 23 35 23 --- 18
R17 | 2223 22 10 33 36 --- 14 | 52 50 55 36 --- 44
R18 | 1549 13 9 12 18 --- 7 | 26 28 37 25 --- 26
R19 | 1051 21 9 20 17 --- 9 | 29 38 41 37 --- 34
R20 | 1718 22 5 17 18 --- 9 | 26 24 33 27 --- 23
R21 | 1008 15 10 19 16 --- 8 | 39 34 19 16 --- 25
XR23 | 1847 --- 29 --- 76 --- 47 | --- 45 --- 71 --- 46
------+------------------------------------+--------------------------------
RMS | 2929 20 10 21 24 172 |T 27 30 35 31 50 26
WRMS | 2929 20 10 21 24 172 |NE 27 30 35 31 50 26
MEDI | 1718 19 9 19 23 109 |MD 25 28 35 31 41 25
Table 3.1566.5 GPS week: 1566 Day: 5 MJD: 55211
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1738 16 8 19 13 --- 8 | 21 20 34 21 --- 20
R03 | 1224 10 12 18 32 --- 10 | 30 37 29 32 --- 27
R05 | 4507 15 14 14 31 --- 10 | 27 32 37 37 --- 30
R07 | 2476 19 8 15 25 --- 9 | 30 27 31 25 --- 24
R08 | 1910 18 6 18 17 150 8 | 22 31 29 35 37 27
R10 | 2676 25 12 19 21 --- 11 | 18 33 38 25 --- 25
R11 | 1112 15 8 18 21 189 8 | 19 30 42 34 28 27
R13 | 1365 19 7 20 18 --- 9 | 23 22 29 17 --- 19
R14 | 4354 18 10 23 15 --- 9 | 18 23 30 18 --- 17
R15 | 5517 24 14 21 31 --- 12 | 19 27 40 22 --- 20
R17 | 1810 24 11 24 30 --- 12 | 27 32 41 36 --- 30
R18 | 2094 23 15 25 16 --- 11 | 38 37 41 33 --- 34
R19 | 1068 15 11 18 13 --- 8 | 36 42 36 39 --- 37
R20 | 3544 17 11 16 23 --- 9 | 32 26 33 25 --- 26
R21 | 788 11 10 13 22 --- 8 | 26 25 28 19 --- 21
XR23 | 2970 --- 36 --- 79 --- 53 | --- 47 --- 35 --- 34
------+------------------------------------+--------------------------------
RMS | 2784 18 11 19 23 171 |T 25 30 34 28 32 26
WRMS | 2784 19 10 19 23 171 |NE 25 30 34 28 32 26
MEDI | 1910 18 11 18 21 150 |MD 26 30 34 25 28 26
Table 3.1566.6 GPS week: 1566 Day: 6 MJD: 55212
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1296 14 13 18 28 --- 10 | 28 32 34 28 --- 28
R03 | 1362 11 8 15 16 --- 7 | 38 36 33 37 --- 34
XR04 | ---- --- 6 --- --- --- 0 | --- 4 --- --- --- 5
R05 | 1330 11 10 9 18 --- 7 | 30 26 33 31 --- 27
R07 | 3623 18 12 22 18 --- 10 | 36 31 41 38 --- 33
R08 | 1557 11 6 11 20 265 7 | 23 32 29 37 51 27
R10 | 4045 11 18 22 12 --- 9 | 26 29 31 26 --- 23
R11 | 1891 13 18 23 20 166 11 | 28 29 44 33 40 29
R13 | 739 20 13 27 14 --- 11 | 21 30 29 26 --- 23
R14 | 1774 11 15 16 15 --- 8 | 18 27 35 24 --- 23
R15 | 5902 20 18 27 15 --- 12 | 25 23 37 19 --- 20
R17 | 1521 17 17 11 42 --- 13 | 35 40 42 47 --- 38
R18 | 1099 10 13 19 24 --- 9 | 28 32 26 28 --- 26
R19 | 1045 12 14 18 18 --- 9 | 62 65 76 68 --- 66
R20 | 3315 24 21 22 54 --- 17 | 21 26 32 30 --- 23
R21 | 692 17 15 19 39 --- 12 | 27 37 31 30 --- 30
XR23 | 2241 --- 40 --- 74 --- 54 | --- 80 --- 42 --- 60
------+------------------------------------+--------------------------------
RMS | 2522 15 15 19 26 221 |T 29 34 36 34 45 30
WRMS | 2522 15 14 18 26 221 |NE 29 34 36 34 45 30
MEDI | 1521 13 14 19 18 166 |MD 28 31 33 30 40 27
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