[IGSREPORT-18498] Wk 1578 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 22 05:49:20 PDT 2010
******************************************************************************
IGS Electronic Report 22 Apr 05:49:33 PDT 2010 Message Number 18498
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1578 (Apr 04, 2010 - Apr 10, 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 2.1578.
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:
igl1578[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1578 in the SP3 format.
igl15787.sum Combination Report for GPS Week 1578.
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 | 446.8 ns
1 | 404.0 ns
2 | 453.8 ns
3 | 367.6 ns
4 | 394.5 ns
5 | 402.3 ns
6 | 369.9 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 1.1578, 1a.1578).
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 2.1578.0-6)
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 3.1578.0-6).
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 1578 summary. (Apr 04, 2010 - Apr 10, 2010)
Table 1.1578.a GPS week : 1578 MJD: 55290.0-55296.0
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 131| 2 0 2 6 11 -29 -.11 23 23 | 0 -34 1697 1747
| 1 0 5 25 49 155 .05 | 0 61
cod 247| -3 0 0 45 -13 54 -.07 13 13 | --- --- --- ---
| 1 1 2 17 22 42 .03 | --- ---
esx 140| 0 0 -1 -61 23 -15 .42 26 25 | 78214 -2611 3879 8896
| 2 1 3 17 27 70 .06 | 39417 2486
iac n/a| 2 -1 0 -23 6 -54 -.13 22 22 | 406469 -681 3877 8601
| 0 1 7 18 15 66 .04 | 34234 819
mcc n/a| 3 -10 23 60 15 385 -.43 192 192 | --- --- --- ---
| 10 12 18 118 228 933 .63 | --- ---
Table 1.1578.b GPS week : 1578 MJD: 55290.0-55296.0
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 | 11 15 10 12 12 11 10 |
R02 | 16 13 11 11 10 9 11 |
R03 | 10 15 11 11 13 10 11 |
R04 | 10 9 9 12 12 9 9 |
R05 | 10 14 9 13 11 12 12 |
R07 | 10 9 9 12 16 11 11 |
R08 | 8 11 12 11 10 10 11 |
R10 | 13 12 14 12 12 15 9 |
R11 | 15 15 12 10 15 11 11 |
R13 | 14 9 12 10 9 10 12 |
R14 | 14 15 20 21 19 15 14 |
R15 | 8 11 14 12 13 11 14 |
R17 | 10 11 12 11 11 9 11 |
R18 | 13 13 12 12 12 13 13 |
R19 | 11 11 12 8 9 11 10 |
R20 | 12 14 14 15 15 9 12 |
R21 | 11 10 12 10 15 13 12 |
R22 | 12 14 14 14 14 11 12 |
R23 | 8 12 9 10 12 11 10 |
R24 | 9 12 13 12 9 11 10 |
Table 1.1578.c GPS week : 1578 MJD: 55290.0-55296.0
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 1578 0 | 38 27 310 -1068 1273 -16030 87.7 1608 1608 | 446815 0
brd 1578 1 | -101 -18 304 775 1579 -16090 89.1 1838 1838 | 404023 0
brd 1578 2 | 63 -30 253 1685 3529 -19030 86.6 1758 1758 | 453797 0
brd 1578 3 | 20 -24 309 874 1475 -16700 86.2 1693 1693 | 367564 0
brd 1578 4 | 33 -47 258 -186 -770 -18780 88.4 1726 1726 | 394457 0
brd 1578 5 | -8 -48 257 -639 -1516 -19920 85.6 1682 1682 | 402286 0
brd 1578 6 | 50 19 183 -576 -1240 -21980 85.9 1759 1759 | 369886 0
-------------+------------------------------------------------------------+----------------
brd 1578 mean| 13 -17 268 123 618 -18361 87.1 1723 1723 | 405546 0
brd 1578 sdev| 55 30 45 1001 1848 2217 1.3 72 72 | 33866 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 2.1578.0 GPS week: 1578 Day: 0 MJD: 55290
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 131| 1 0 1 -34 -54 -200 -.17 19 20 | 0 -12 1763 1812
cod 247| 0 0 -4 56 21 106 -.06 13 11 | --- --- --- ---
esx 140| 0 0 -3 -45 46 34 .51 29 28 | 130554 -4075 3949 10591
iac n/a| 2 -2 8 -47 7 -25 -.13 21 21 | 447941 -1200 3972 8898
mcc n/a| -10 2 48 31 -364 1513 -.68 235 235 | --- --- --- ---
Table 2.1578.1 GPS week: 1578 Day: 1 MJD: 55291
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 131| 4 -1 11 5 -35 84 -.10 27 26 | 0 -70 1616 1666
cod 247| -2 2 0 36 7 36 -.07 13 11 | --- --- --- ---
esx 140| -2 0 -6 -57 52 -112 .48 32 29 | 82123 1395 3865 9362
iac n/a| 3 -2 -1 -25 -13 -83 -.12 21 21 | 404283 448 3858 8466
mcc n/a| 3 3 9 161 152 1441 -.40 225 225 | --- --- --- ---
Table 2.1578.2 GPS week: 1578 Day: 2 MJD: 55292
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 131| 3 0 9 13 18 236 -.14 26 26 | 0 -86 1484 1533
cod 247| -2 0 4 31 -33 -6 -.08 14 13 | --- --- --- ---
esx 140| 0 -1 0 -64 6 -104 .39 26 24 | 130053 -2493 3659 9297
iac n/a| 3 0 -14 -6 26 -125 -.14 23 23 | 455727 -1400 3664 8641
mcc n/a| 5 0 -4 30 154 1085 -.46 191 191 | --- --- --- ---
Table 2.1578.3 GPS week: 1578 Day: 3 MJD: 55293
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 131| 2 0 0 25 91 15 -.11 25 25 | 0 -87 1829 1890
cod 247| -5 0 1 62 -45 22 -.12 13 13 | --- --- --- ---
esx 140| 4 -3 -3 -72 -17 41 .43 22 20 | 34746 -5195 4309 8813
iac n/a| 2 0 1 -9 18 -137 -.17 27 27 | 368757 -483 4277 9121
mcc n/a| 2 -10 40 -136 -181 -44 -.80 191 191 | --- --- --- ---
Table 2.1578.4 GPS week: 1578 Day: 4 MJD: 55294
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 131| 2 0 -2 18 41 -148 -.01 25 25 | 0 13 2015 2053
cod 247| -2 1 0 54 -17 92 -.09 15 15 | --- --- --- ---
esx 140| 0 0 0 -38 10 -44 .34 25 23 | 59884 -2838 3814 7454
iac n/a| 1 -1 5 -39 -14 47 -.20 24 24 | 395578 -1846 3822 7909
mcc n/a| -7 -22 32 103 241 -368 .37 193 193 | --- --- --- ---
Table 2.1578.5 GPS week: 1578 Day: 5 MJD: 55295
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 131| 1 0 -3 -19 30 -153 -.11 20 20 | 0 74 1483 1540
cod 247| -4 2 0 61 -7 91 -.05 12 12 | --- --- --- ---
esx 140| 0 1 3 -60 16 37 .40 25 24 | 72152 -70 3717 8895
iac n/a| 3 -2 0 -36 5 -3 -.10 21 21 | 402973 -107 3701 8773
mcc n/a| 15 -28 22 229 188 -178 .33 168 168 | --- --- --- ---
Table 2.1578.6 GPS week: 1578 Day: 6 MJD: 55296
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 131| 3 0 3 36 -12 -39 -.16 22 22 | 0 -70 1693 1739
cod 247| -3 0 -1 18 -19 37 -.03 13 12 | --- --- --- ---
esx 140| 0 0 0 -91 51 42 .38 25 25 | 37986 -5001 3844 7865
iac n/a| 3 0 1 0 16 -51 -.07 20 20 | 370030 -185 3848 8399
mcc n/a| 15 -16 15 5 -84 -746 -1.39 141 141 | --- --- --- ---
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 3.1578.0 GPS week: 1578 Day: 0 MJD: 55290
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1046 20 19 16 21 --- 11 | 41 62 50 40 --- 48
R02 | 1145 20 9 56 24 --- 15 | 51 55 52 52 --- 50
R03 | 1296 18 14 28 13 --- 10 | 53 64 60 64 --- 59
R04 | 2606 15 9 26 19 --- 9 | 33 46 60 39 --- 41
R05 | 1365 24 14 15 16 --- 10 | 35 47 42 40 --- 39
R07 | 967 17 12 27 15 --- 10 | 55 41 39 43 --- 42
R08 | 2530 15 8 18 14 87 7 | 53 50 54 48 79 47
R10 | 1598 26 15 28 24 --- 13 | 24 24 36 45 --- 27
R11 | 2564 35 21 23 25 382 15 | 41 45 52 41 11 42
R13 | 763 18 18 44 12 --- 13 | 20 26 29 29 --- 21
R14 | 656 18 15 41 26 --- 14 | 41 57 66 54 --- 50
R15 | 1447 13 7 15 21 111 8 | 31 45 44 44 43 40
R17 | 749 21 12 16 20 --- 10 | 39 47 44 42 --- 42
R18 | 1660 17 6 29 33 --- 12 | 23 22 42 38 --- 25
R19 | 1431 14 11 17 30 --- 10 | 25 23 23 25 --- 20
R20 | 2610 16 10 37 22 --- 12 | 20 36 50 28 --- 29
R21 | 1676 17 14 28 17 --- 10 | 31 23 48 31 --- 27
R22 | 1592 17 13 34 19 --- 11 | 60 62 81 53 --- 60
R23 | 702 12 7 22 15 --- 7 | 44 39 47 39 --- 39
R24 | 1181 20 8 16 19 --- 9 | 39 39 33 38 --- 34
------+------------------------------------+--------------------------------
RMS | 1608 19 13 29 21 235 |T 37 42 47 41 44 39
WRMS | 1608 20 11 28 21 235 |NE 37 42 47 41 44 39
MEDI | 1365 17 12 26 19 111 |MD 39 45 47 40 43 40
Table 3.1578.1 GPS week: 1578 Day: 1 MJD: 55291
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1485 37 24 30 15 --- 15 | 36 64 53 46 --- 51
R02 | 998 20 15 41 20 --- 13 | 25 35 42 25 --- 28
R03 | 1157 35 12 41 21 --- 14 | 52 54 42 58 --- 51
R04 | 1715 14 10 19 19 --- 8 | 22 36 38 22 --- 29
R05 | 2213 14 8 37 34 --- 13 | 29 27 58 25 --- 24
R07 | 1720 21 7 23 14 --- 9 | 29 31 40 34 --- 31
R08 | 3561 21 11 33 14 132 10 | 20 25 47 32 65 26
R10 | 1957 33 9 25 20 --- 12 | 17 22 38 28 --- 20
R11 | 1285 40 11 28 28 354 14 | 36 38 49 32 10 35
R13 | 2098 19 12 16 18 --- 9 | 16 29 38 27 --- 23
R14 | 797 28 14 50 17 --- 15 | 29 31 49 36 --- 30
R15 | 2971 30 11 23 18 92 11 | 34 36 41 30 39 32
R17 | 686 22 12 25 20 --- 10 | 39 37 41 35 --- 33
R18 | 2441 23 13 31 29 --- 13 | 29 34 41 46 --- 31
R19 | 740 21 10 22 23 --- 10 | 25 27 37 21 --- 22
R20 | 2083 37 13 37 19 --- 14 | 30 24 41 11 --- 15
R21 | 1762 20 9 29 14 --- 9 | 33 34 31 27 --- 27
R22 | 901 20 19 40 22 --- 13 | 51 63 65 51 --- 55
R23 | 711 30 12 32 12 --- 11 | 29 39 55 43 --- 38
R24 | 2109 24 10 35 22 --- 12 | 24 36 40 37 --- 30
------+------------------------------------+--------------------------------
RMS | 1838 26 13 32 21 224 |T 30 36 44 33 38 31
WRMS | 1838 26 11 29 21 224 |NE 30 36 44 33 38 31
MEDI | 1715 22 11 30 19 132 |MD 29 34 41 32 39 30
Table 3.1578.2 GPS week: 1578 Day: 2 MJD: 55292
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1085 21 11 26 15 --- 10 | 44 40 60 46 --- 43
R02 | 1062 25 13 19 23 --- 11 | 46 45 42 35 --- 40
R03 | 1494 24 13 22 17 --- 10 | 51 55 43 68 --- 53
R04 | 1905 15 9 18 17 --- 8 | 44 35 42 46 --- 39
R05 | 1563 21 10 18 18 --- 9 | 32 44 43 36 --- 37
R07 | 2131 19 10 19 15 --- 9 | 26 28 30 38 --- 26
R08 | 4194 26 13 20 23 188 11 | 32 35 41 54 154 35
R10 | 2349 26 16 32 25 --- 14 | 20 25 43 36 --- 26
R11 | 898 24 13 29 23 265 12 | 35 39 45 31 10 33
R13 | 2538 28 9 26 19 --- 11 | 20 27 42 34 --- 26
R14 | 793 50 10 44 36 --- 20 | 31 48 59 43 --- 40
R15 | 1327 27 23 25 23 65 14 | 35 46 33 41 79 35
R17 | 1000 29 7 27 18 --- 11 | 34 37 37 40 --- 33
R18 | 1329 17 12 18 34 --- 12 | 15 20 25 47 --- 22
R19 | 672 14 13 33 21 --- 11 | 20 22 48 37 --- 26
R20 | 897 28 23 20 25 --- 14 | 18 41 39 34 --- 28
R21 | 1480 20 11 27 28 --- 12 | 24 27 31 28 --- 21
R22 | 970 23 16 35 25 --- 14 | 22 43 47 33 --- 31
R23 | 1038 18 11 15 19 --- 9 | 31 38 36 48 --- 36
R24 | 2379 34 16 19 16 --- 12 | 25 44 47 44 --- 35
------+------------------------------------+--------------------------------
RMS | 1758 26 14 26 23 191 |T 30 36 41 40 81 33
WRMS | 1758 26 13 24 23 191 |NE 30 36 41 40 81 33
MEDI | 1327 24 12 22 21 188 |MD 31 38 42 38 79 33
Table 3.1578.3 GPS week: 1578 Day: 3 MJD: 55293
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1605 27 10 14 31 --- 11 | 56 67 53 54 --- 57
R02 | 1138 13 13 28 23 --- 11 | 40 44 48 26 --- 37
R03 | 1126 25 11 20 20 --- 11 | 49 46 59 44 --- 46
R04 | 1863 24 18 21 23 --- 12 | 31 32 26 34 --- 26
R05 | 1225 33 10 22 23 --- 12 | 31 25 34 43 --- 27
R07 | 3140 20 10 25 25 --- 11 | 21 18 43 25 --- 20
R08 | 3079 28 10 10 24 199 10 | 24 29 31 38 116 26
R10 | 3248 22 14 23 27 --- 12 | 22 29 28 43 --- 24
R11 | 1019 21 12 12 26 --- 10 | 33 46 42 37 --- 36
R13 | 1979 18 11 20 20 --- 9 | 21 25 37 25 --- 23
R14 | 678 47 17 27 56 --- 20 | 33 49 52 41 --- 40
R15 | 1077 25 11 21 25 183 11 | 32 35 46 46 81 34
R17 | 1194 21 14 24 15 --- 10 | 55 62 69 56 --- 58
R18 | 1340 22 19 11 28 --- 11 | 22 32 28 26 --- 23
R19 | 500 16 8 14 19 --- 8 | 28 26 31 28 --- 24
R20 | 1020 23 13 41 25 --- 15 | 25 30 70 28 --- 34
R21 | 606 20 13 18 22 --- 10 | 32 28 39 22 --- 26
R22 | 702 24 16 30 31 --- 14 | 40 45 28 31 --- 31
R23 | 1513 18 11 22 21 --- 10 | 29 36 38 39 --- 31
R24 | 1743 28 15 16 21 --- 11 | 40 43 35 37 --- 35
------+------------------------------------+--------------------------------
RMS | 1692 25 13 22 27 191 |T 33 37 41 36 98 32
WRMS | 1692 25 13 20 27 191 |NE 33 37 41 36 98 32
MEDI | 1194 22 12 21 23 183 |MD 31 32 38 37 81 31
Table 3.1578.4 GPS week: 1578 Day: 4 MJD: 55294
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1707 23 17 19 23 --- 11 | 27 43 37 28 --- 31
R02 | 963 19 15 13 19 --- 9 | 37 35 44 22 --- 32
R03 | 1614 8 22 23 28 --- 12 | 27 21 42 29 --- 22
R04 | 2194 17 19 23 22 --- 11 | 28 31 30 19 --- 22
R05 | 1123 25 12 23 11 --- 10 | 30 31 21 31 --- 25
R07 | 2437 40 15 18 33 --- 15 | 21 28 25 33 --- 20
R08 | 3223 19 10 18 24 193 10 | 21 27 24 45 56 27
R10 | 3011 17 9 33 20 --- 12 | 26 28 48 32 --- 27
R11 | 930 31 22 29 18 --- 14 | 36 41 50 37 --- 37
R13 | 821 18 12 19 18 --- 9 | 18 23 32 23 --- 21
R14 | 951 47 13 25 45 --- 19 | 22 32 45 43 --- 30
R15 | 2100 24 16 27 25 193 13 | 19 34 40 31 47 25
R17 | 1495 15 13 28 22 --- 11 | 63 60 66 53 --- 57
R18 | 2273 18 19 24 22 --- 12 | 27 38 26 38 --- 26
R19 | 853 14 13 19 18 --- 9 | 32 36 30 40 --- 31
R20 | 859 37 12 29 21 --- 14 | 15 25 41 30 --- 20
R21 | 624 31 9 34 26 --- 14 | 41 32 50 35 --- 33
R22 | 824 21 17 28 33 --- 14 | 40 39 58 64 --- 44
R23 | 1494 14 18 27 19 --- 11 | 31 42 45 50 --- 38
R24 | 1629 10 14 20 16 --- 9 | 25 34 37 40 --- 31
------+------------------------------------+--------------------------------
RMS | 1726 25 15 25 24 193 |T 29 34 39 36 51 29
WRMS | 1726 25 15 23 24 193 |NE 29 34 39 36 51 29
MEDI | 1494 19 14 23 22 193 |MD 27 32 40 33 47 27
Table 3.1578.5 GPS week: 1578 Day: 5 MJD: 55295
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1072 22 10 28 13 --- 10 | 37 39 51 26 --- 35
R02 | 928 15 11 23 11 --- 8 | 25 32 32 32 --- 26
R03 | 1543 12 12 27 17 --- 10 | 30 34 31 26 --- 27
R04 | 1396 5 12 26 14 --- 9 | 22 18 44 25 --- 23
R05 | 1880 20 13 34 11 --- 11 | 41 39 26 31 --- 30
R07 | 1195 22 11 13 24 --- 10 | 14 25 33 48 --- 27
R08 | 2175 26 13 13 13 173 10 | 21 33 34 29 45 27
R10 | 1776 19 19 41 25 --- 15 | 23 44 54 33 --- 34
R11 | 799 23 14 18 23 --- 11 | 30 39 43 33 --- 34
R13 | 1269 19 12 21 18 --- 9 | 22 27 38 23 --- 23
R14 | 721 25 9 24 40 --- 14 | 27 34 43 36 --- 28
R15 | 3547 23 7 24 21 162 10 | 25 25 29 26 31 20
R17 | 1937 13 12 15 21 --- 9 | 53 43 55 38 --- 45
R18 | 3049 21 14 23 33 --- 13 | 22 32 50 31 --- 26
R19 | 1473 19 14 26 18 --- 11 | 24 31 50 39 --- 33
R20 | 1147 12 13 15 20 --- 8 | 26 26 23 15 --- 15
R21 | 1323 30 15 23 21 --- 12 | 35 35 44 40 --- 33
R22 | 1245 18 9 27 23 --- 11 | 30 36 52 36 --- 34
R23 | 657 16 14 28 20 --- 11 | 41 43 53 49 --- 42
R24 | 1326 20 9 25 20 --- 10 | 58 60 40 39 --- 49
------+------------------------------------+--------------------------------
RMS | 1682 20 12 25 21 168 |T 30 34 41 32 38 30
WRMS | 1682 20 12 24 21 168 |NE 30 34 41 32 38 30
MEDI | 1323 19 12 24 20 162 |MD 26 34 43 32 31 28
Table 3.1578.6 GPS week: 1578 Day: 6 MJD: 55296
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 998 16 13 23 17 --- 10 | 33 41 36 29 --- 33
R02 | 1478 26 18 23 8 --- 11 | 23 34 31 27 --- 28
R03 | 1178 19 12 22 21 --- 10 | 23 30 37 26 --- 24
R04 | 1791 12 9 26 15 --- 9 | 28 33 40 27 --- 29
R05 | 2039 16 21 28 17 --- 12 | 30 44 37 33 --- 34
R07 | 1241 25 8 13 28 --- 11 | 26 25 27 35 --- 26
R08 | 1118 26 14 20 19 153 11 | 34 34 36 39 46 32
R10 | 1300 17 9 17 19 --- 9 | 28 36 31 40 --- 31
R11 | 954 21 12 26 16 --- 10 | 46 50 48 34 --- 42
R13 | 1131 17 14 35 17 --- 12 | 22 25 48 28 --- 27
R14 | 1052 31 17 27 27 --- 14 | 32 34 47 44 --- 34
R15 | 4302 33 11 38 17 127 14 | 30 30 31 32 53 27
R17 | 1567 23 10 19 22 --- 10 | 54 61 59 60 --- 57
R18 | 3596 25 12 31 21 --- 12 | 42 34 39 34 --- 32
R19 | 1174 23 8 22 17 --- 10 | 34 39 42 43 --- 37
R20 | 1673 25 10 28 19 --- 11 | 16 29 45 14 --- 22
R21 | 1208 15 16 24 25 --- 11 | 37 44 30 33 --- 33
R22 | 1011 24 10 29 23 --- 12 | 38 39 39 37 --- 34
R23 | 804 22 9 22 15 --- 9 | 47 49 60 49 --- 48
R24 | 973 19 13 17 23 --- 10 | 54 61 64 60 --- 58
------+------------------------------------+--------------------------------
RMS | 1759 22 13 25 20 141 |T 33 38 41 36 49 34
WRMS | 1759 22 12 25 20 141 |NE 33 38 41 36 49 34
MEDI | 1178 22 12 23 19 127 |MD 32 34 39 34 46 32
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