[IGSREPORT-17964] Wk 1554 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Nov 5 05:37:03 PST 2009
******************************************************************************
IGS Electronic Report 05 Nov 05:37:26 PST 2009 Message Number 17964
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1554 (Oct 18, 2009 - Oct 24, 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 2.1554.
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:
igl1554[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1554 in the SP3 format.
igl15547.sum Combination Report for GPS Week 1554.
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 | 179.2 ns
1 | 185.7 ns
2 | 76.4 ns
3 | 79.4 ns
4 | 182.5 ns
5 | 68.2 ns
6 | 188.2 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 1.1554, 1a.1554).
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 2.1554.0-6)
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 3.1554.0-6).
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 1554 summary. (Oct 18, 2009 - Oct 24, 2009)
Table 1.1554.a GPS week : 1554 MJD: 55122.0-55128.0
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 100| 0 0 -4 -8 -18 44 -.13 26 24 | 0 463 3651 4119
| 1 1 7 21 20 239 .02 | 0 1569
cod 224| 0 0 -1 16 3 76 -.13 18 15 | --- --- --- ---
| 1 2 1 17 23 50 .05 | --- ---
esx 126| 0 -1 2 17 20 -5 .43 24 23 | 87274 -989 4905 9858
| 0 2 5 14 40 87 .05 | 58124 4431
iac n/a| 0 0 4 -47 -11 -144 -.12 24 24 | 137613 -269 4896 10056
| 1 1 4 24 14 94 .04 | 58205 2237
mcc n/a| -1 2 21 -83 -16 1210 -.08 123 123 | --- --- --- ---
| 5 7 42 83 79 806 .42 | --- ---
Table 1.1554.b GPS week : 1554 MJD: 55122.0-55128.0
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 | 14 11 10 9 11 8 13 |
R03 | 12 11 12 13 13 11 9 |
R07 | 13 9 11 11 13 14 11 |
R08 | 10 11 9 9 13 10 11 |
R10 | 10 14 11 11 25 31 15 |
R11 | 17 14 16 14 13 28 29 |
R13 | 9 14 11 11 10 13 14 |
R14 | 12 14 10 11 15 17 13 |
R15 | 12 11 11 10 27 20 15 |
R17 | 10 13 10 9 11 11 12 |
R18 | 13 12 9 8 12 14 11 |
R19 | 11 9 11 9 12 8 9 |
R20 | 16 14 14 10 10 11 12 |
R21 | 12 14 13 9 10 11 12 |
R23 | 12 17 11 11 12 21 20 |
R24 | 11 14 14 13 11 15 12 |
Table 1.1554.c GPS week : 1554 MJD: 55122.0-55128.0
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 1554 0 | -40 -57 198 -206 -5638 -24530 87.6 2089 2089 | 179227 0
brd 1554 1 | 4576 ---- 2400 -121900 -34320 138100 25.1 >>>>> >>>>> | 185699 0
brd 1554 2 | -5 -29 202 -725 -1139 -17470 86.8 2031 2031 | 76416 0
brd 1554 3 | 53 -4 2 -1428 -357 -15460 87.8 2091 2091 | 79407 0
brd 1554 4 | -48 29 -56 -1282 -706 -10970 91.0 2292 2292 | 182533 0
brd 1554 5 | 156 120 2 478 -775 -7724 89.4 2497 2497 | 68165 0
brd 1554 6 | 51 -113 148 3735 739 -3277 88.2 2813 2813 | 188213 0
-------------+------------------------------------------------------------+----------------
brd 1554 mean| 677 -6197 414 -17332 -6028 8381 79.4 >>>>> >>>>> | 137094 0
brd 1554 sdev| 1720 16373 881 46143 12638 57614 24.0 >>>>> >>>>> | 58560 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 2.1554.0 GPS week: 1554 Day: 0 MJD: 55122
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 100| 1 -1 -1 11 -26 89 -.13 23 24 | 0 -947 2795 2964
cod 224| -2 1 -1 3 8 15 -.14 16 15 | --- --- --- ---
esx 126| 0 1 5 -4 -27 42 .45 24 21 | 131929 3125 4699 9066
iac n/a| 0 -1 0 -35 5 -214 -.09 24 24 | 178808 2193 4732 9572
mcc n/a| 2 0 31 66 -38 315 -.08 92 92 | --- --- --- ---
Table 2.1554.1 GPS week: 1554 Day: 1 MJD: 55123
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 100| 0 0 0 -16 -10 -52 -.13 24 24 | 0 -44 4373 4706
cod 224| 0 -2 -2 24 27 89 -.10 13 13 | --- --- --- ---
esx 126| 0 1 -3 31 -15 -16 .43 29 25 | 143965 -8431 5630 10652
iac n/a| 0 3 10 -78 10 -119 -.08 24 24 | 187669 -2928 5610 10895
mcc n/a| -1 11 49 -90 -48 713 -.30 99 99 | --- --- --- ---
Table 2.1554.2 GPS week: 1554 Day: 2 MJD: 55124
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 100| 1 1 0 -40 -34 -87 -.13 22 22 | 0 1922 3832 4636
cod 224| 0 0 -2 32 16 49 -.10 15 14 | --- --- --- ---
esx 126| 0 -1 0 16 46 97 .37 21 20 | 28878 3032 4238 10432
iac n/a| 1 0 8 -64 -18 -143 -.17 22 22 | 76325 885 4204 10510
mcc n/a| -6 0 34 -169 -75 550 -.56 109 109 | --- --- --- ---
Table 2.1554.3 GPS week: 1554 Day: 3 MJD: 55125
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 100| 2 0 -4 -9 -15 357 -.08 19 18 | 0 773 2762 3204
cod 224| 0 2 0 21 3 35 -.12 14 14 | --- --- --- ---
esx 126| 0 -3 0 11 45 -108 .48 22 23 | 39150 -3801 4113 9553
iac n/a| 2 0 4 -61 -9 -284 -.13 18 18 | 81124 -1745 4102 9574
mcc n/a| -8 -9 91 -131 78 918 .78 435 435 | --- --- --- ---
Table 2.1554.4 GPS week: 1554 Day: 4 MJD: 55126
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 100| -2 -1 0 18 -38 355 -.15 32 30 | 0 -1309 3782 4389
cod 224| 1 -1 -3 -17 28 76 -.22 21 18 | --- --- --- ---
esx 126| 1 2 -4 6 -1 -131 .40 20 18 | 129586 -1893 4267 8439
iac n/a| 0 -1 5 -10 -14 -181 -.16 26 26 | 183238 -1740 4272 8619
mcc n/a| -4 0 -27 -156 86 1520 -.04 50 50 | --- --- --- ---
Table 2.1554.5 GPS week: 1554 Day: 5 MJD: 55127
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 100| 1 1 -5 -27 -27 -286 -.15 29 24 | 0 -209 2571 2699
cod 224| -3 -2 0 26 -34 170 -.15 24 17 | --- --- --- ---
esx 126| 0 -5 4 30 86 70 .49 29 29 | 10151 -2317 4206 8994
iac n/a| 0 2 1 -57 -27 9 -.15 31 31 | 69272 -1428 4158 9336
mcc n/a| 2 12 -14 -85 -127 1945 -.26 33 33 | --- --- --- ---
Table 2.1554.6 GPS week: 1554 Day: 6 MJD: 55128
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 100| -2 1 -20 3 23 -65 -.14 32 29 | 0 3055 5443 6239
cod 224| 1 0 1 21 -20 96 -.08 21 15 | --- --- --- ---
esx 126| 0 -3 12 33 6 6 .38 26 23 | 127259 3357 7187 11873
iac n/a| 0 1 0 -26 -25 -81 -.09 22 22 | 186859 2876 7200 11889
mcc n/a| 8 4 -14 -17 8 2513 -.10 42 42 | --- --- --- ---
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 3.1554.0 GPS week: 1554 Day: 0 MJD: 55122
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 781 35 13 27 16 --- 13 | 23 35 54 43 --- 36
R03 | 1125 22 20 11 23 --- 11 | 28 46 32 33 --- 34
R07 | 4337 21 18 19 30 --- 13 | 27 34 30 39 --- 30
R08 | 1427 14 12 21 22 103 10 | 26 24 39 33 34 26
R10 | 3259 20 14 18 19 --- 10 | 65 73 76 80 --- 72
R11 | 948 35 12 40 28 108 17 | 55 50 72 51 84 53
R13 | 1430 21 10 13 17 --- 9 | 27 33 33 29 --- 28
R14 | 1836 20 16 22 27 --- 12 | 52 65 55 57 --- 56
R15 | 2195 19 13 25 27 54 12 | 60 66 64 73 79 64
R17 | 1911 21 11 14 24 --- 10 | 39 47 47 56 --- 45
R18 | 1033 13 16 32 24 --- 12 | 27 39 41 39 --- 34
R19 | 763 21 16 21 20 --- 11 | 54 46 41 43 --- 44
R20 | 1901 34 19 37 22 --- 16 | 26 33 46 35 --- 31
R21 | 2662 9 23 21 25 --- 12 | 28 39 42 31 --- 32
R23 | 1183 15 15 15 32 --- 11 | 53 68 68 79 --- 65
R24 | 2810 21 15 19 17 --- 10 | 54 55 50 57 --- 51
------+------------------------------------+--------------------------------
RMS | 2088 23 16 24 24 92 |T 40 47 49 48 65 43
WRMS | 2088 24 15 21 24 92 |NE 35 42 44 44 34 38
MEDI | 1430 21 15 21 23 103 |MD 28 46 46 43 79 36
Table 3.1554.1 GPS week: 1554 Day: 1 MJD: 55123
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 17 9 28 23 --- 11 | 33 42 45 55 --- 41
R03 |>>>>> 26 14 21 19 --- 11 | 26 33 38 42 --- 32
R07 |>>>>> 17 13 15 19 --- 9 | 30 28 29 29 --- 26
R08 |>>>>> 11 16 16 27 113 10 | 29 26 39 33 18 28
R10 |>>>>> 16 15 25 37 --- 13 | 44 55 64 62 --- 53
R11 |>>>>> 31 8 22 32 113 13 | 59 47 47 59 64 51
R13 |>>>>> 30 17 28 23 --- 13 | 19 29 37 27 --- 21
R14 |>>>>> 30 15 31 20 --- 13 | 51 45 67 47 --- 48
R15 |>>>>> 27 12 11 22 64 10 | 38 44 50 49 76 43
R17 |>>>>> 23 14 19 32 --- 12 | 28 38 56 57 --- 41
R18 |>>>>> 27 8 28 18 --- 11 | 25 30 43 24 --- 25
R19 |>>>>> 10 11 22 17 --- 8 | 27 41 36 25 --- 31
R20 |>>>>> 24 15 38 22 --- 13 | 26 30 38 38 --- 26
R21 |>>>>> 28 12 41 17 --- 14 | 33 22 36 21 --- 18
R23 |>>>>> 30 11 55 21 --- 17 | 35 57 98 50 --- 56
R24 |>>>>> 24 17 32 26 --- 13 | 34 57 55 38 --- 43
------+------------------------------------+--------------------------------
RMS |>>>>> 24 13 29 24 99 |T 33 39 48 41 52 36
WRMS |>>>>> 24 13 25 24 99 |NE 29 36 46 37 18 33
MEDI |>>>>> 24 13 25 22 113 |MD 30 38 43 38 64 32
Table 3.1554.2 GPS week: 1554 Day: 2 MJD: 55124
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 781 23 13 12 19 --- 9 | 28 25 35 34 --- 26
R03 | 1106 26 13 19 27 --- 12 | 23 39 48 50 --- 36
R07 | 1808 19 19 15 17 --- 10 | 23 28 33 24 --- 23
R08 | 1181 10 14 22 16 141 9 | 31 20 19 18 45 16
R10 | 4061 17 13 14 27 --- 10 | 47 55 60 62 --- 53
R11 | 918 42 12 32 20 114 16 | 50 52 51 40 152 44
R13 | 1175 23 10 25 18 --- 11 | 29 30 46 27 --- 29
R14 | 1418 17 9 16 23 --- 9 | 50 52 50 59 --- 51
R15 | 1359 18 17 21 22 53 11 | 42 49 63 59 156 50
R17 | 988 17 12 13 25 --- 10 | 47 45 50 61 --- 49
R18 | 1310 21 8 16 15 --- 8 | 35 42 50 41 --- 40
R19 | 659 15 16 18 23 --- 10 | 27 37 32 39 --- 31
R20 | 2100 17 23 29 24 --- 13 | 24 35 47 22 --- 27
R21 | 1387 24 23 26 17 --- 13 | 37 34 46 39 --- 33
R23 | 2921 16 13 24 24 --- 11 | 41 52 45 54 --- 46
R24 | 4351 21 13 26 32 --- 13 | 57 64 43 64 --- 53
------+------------------------------------+--------------------------------
RMS | 2031 22 15 21 22 109 |T 36 41 44 43 117 37
WRMS | 2031 22 14 20 22 109 |NE 33 38 40 40 45 34
MEDI | 1310 18 13 19 22 114 |MD 35 39 46 40 152 36
Table 3.1554.3 GPS week: 1554 Day: 3 MJD: 55125
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2671 12 13 18 16 --- 8 | 30 36 51 50 --- 39
R03 | 1113 21 22 24 22 --- 13 | 25 38 41 33 --- 30
R07 | 1977 19 20 14 20 --- 11 | 28 26 32 32 --- 24
R08 | 1472 18 13 16 16 118 9 | 45 29 34 29 45 31
R10 | 3546 17 11 28 21 --- 11 | 85 65 70 76 --- 71
R11 | 2071 28 9 38 12 445 13 | 79 61 59 65 140 63
R13 | 2056 18 7 23 22 --- 10 | 32 22 22 35 --- 23
R14 | 2292 20 17 16 23 --- 11 | 51 55 52 51 --- 49
R15 | 3367 17 11 22 17 597 9 | 71 67 78 78 156 70
R17 | 1658 18 14 15 14 --- 8 | 45 43 42 39 --- 39
R18 | 1747 16 12 16 11 --- 8 | 39 37 30 35 --- 33
R19 | 991 17 14 12 15 --- 8 | 31 42 39 39 --- 36
R20 | 1361 19 11 19 22 --- 10 | 22 34 43 32 --- 27
R21 | 950 11 11 18 18 --- 8 | 38 33 29 30 --- 29
R23 | 2195 17 15 22 19 --- 10 | 39 43 36 38 --- 34
R24 | 1860 22 15 28 21 --- 12 | 33 46 57 60 --- 43
------+------------------------------------+--------------------------------
RMS | 2091 19 14 22 18 435 |T 43 42 44 45 113 40
WRMS | 2091 18 14 23 18 435 |NE 34 37 39 37 45 33
MEDI | 1860 18 13 18 18 445 |MD 38 38 41 38 140 34
Table 3.1554.4 GPS week: 1554 Day: 4 MJD: 55126
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 4266 19 21 11 20 --- 10 | 24 27 21 22 --- 17
R03 | 1290 31 19 20 22 --- 13 | 16 32 29 20 --- 21
R07 | 1957 30 18 17 22 --- 12 | 27 28 39 38 --- 28
R08 | 1005 35 25 8 15 50 12 | 33 44 27 31 28 28
R10 | 3676 59 33 38 45 --- 25 | 68 96 113 110 --- 92
R11 | 1186 27 16 20 24 --- 12 | 54 56 54 60 --- 52
R13 | 1052 19 14 14 22 --- 10 | 31 24 34 37 --- 27
R14 | 3162 43 19 17 26 --- 15 | 38 72 74 64 --- 60
R15 | 4420 58 35 38 55 --- 26 | 41 111 116 78 --- 85
R17 | 886 20 18 19 17 --- 10 | 42 47 41 43 --- 38
R18 | 1415 24 14 19 23 --- 11 | 37 31 36 16 --- 24
R19 | 1548 23 19 13 24 --- 11 | 31 38 30 22 --- 25
R20 | 2206 21 16 20 12 --- 10 | 30 36 34 23 --- 27
R21 | 1323 18 17 15 17 --- 9 | 27 44 51 31 --- 36
R23 | 1024 20 20 18 25 --- 12 | 43 37 52 25 --- 30
R24 | 952 26 19 15 15 --- 11 | 36 50 34 44 --- 38
------+------------------------------------+--------------------------------
RMS | 2291 32 21 20 26 50 |T 36 48 49 41 28 39
WRMS | 2291 30 18 18 26 50 |NE 31 37 35 28 28 28
MEDI | 1323 24 19 17 22 50 |MD 33 38 36 31 28 28
Table 3.1554.5 GPS week: 1554 Day: 5 MJD: 55127
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 5567 12 8 11 19 --- 7 | 21 33 35 32 --- 26
R03 | 1735 18 11 28 15 --- 11 | 24 15 38 19 --- 16
R07 | 1964 15 11 31 37 --- 14 | 15 18 39 27 --- 18
R08 | 1551 13 16 19 18 32 9 | 43 36 40 40 21 34
R10E | 3247 62 40 54 60 --- 31 | 56 120 135 87 --- 92
R11E | 994 46 51 41 56 --- 28 | 74 123 116 85 --- 92
R13E | 1026 22 19 21 26 --- 12 | 30 26 34 35 --- 22
R14E | 2090 33 21 33 29 --- 17 | 35 61 65 51 --- 47
R15E | 2466 43 32 27 31 --- 19 | 67 95 108 77 --- 83
R17 | 2237 16 18 18 25 --- 11 | 36 39 49 32 --- 35
R18 | 2174 18 24 30 20 --- 13 | 44 30 43 35 --- 32
R19 | 3077 15 11 11 16 --- 8 | 35 33 41 33 --- 32
R20 | 2629 14 22 18 19 --- 10 | 34 24 36 27 --- 21
R21 | 2310 13 14 19 30 --- 11 | 47 37 47 25 --- 34
R23 | 1175 42 19 47 28 --- 20 | 46 26 51 25 --- 28
R24 | 1897 24 27 18 33 --- 15 | 71 92 90 103 --- 86
------+------------------------------------+--------------------------------
RMS | 2496 29 24 29 31 32 |T 42 50 60 45 21 43
WRMS | 2496 24 17 29 31 32 |NE 37 34 46 36 21 32
MEDI | 2090 18 19 21 26 32 |MD 36 33 43 33 21 32
Table 3.1554.6 GPS week: 1554 Day: 6 MJD: 55128
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 5570 26 13 29 23 --- 13 | 21 28 41 31 --- 26
R03 | 3158 20 12 15 12 --- 8 | 20 29 27 22 --- 21
R07 | 1642 18 17 17 20 --- 10 | 24 24 29 28 --- 23
R08 | 2947 27 18 15 15 42 10 | 33 37 37 48 27 38
R10E | 1864 32 18 30 23 --- 14 | 60 66 71 79 --- 66
R11E | 1744 61 51 38 51 --- 29 | 64 68 64 68 --- 59
R13E | 792 29 17 31 23 --- 14 | 27 34 44 41 --- 31
R14E | 2306 29 18 23 20 --- 12 | 37 46 47 46 --- 39
R15E | 1158 31 27 17 23 --- 14 | 53 75 68 63 --- 63
R17 | 2569 30 19 14 18 --- 11 | 42 56 54 49 --- 48
R18 | 2818 30 12 22 15 --- 11 | 46 27 39 34 --- 31
R19 | 3664 21 13 17 11 --- 8 | 50 39 38 36 --- 37
R20 | 2697 37 14 21 14 --- 12 | 37 24 33 22 --- 23
R21 | 2375 28 13 27 12 --- 11 | 63 46 51 48 --- 47
R23 | 981 44 26 49 20 --- 20 | 61 54 46 49 --- 48
R24 | 4308 28 11 26 14 --- 11 | 67 75 82 76 --- 72
------+------------------------------------+--------------------------------
RMS | 2813 32 21 26 22 42 |T 44 45 48 46 27 42
WRMS | 2813 29 15 23 22 42 |NE 42 39 43 40 27 37
MEDI | 2375 29 17 22 18 42 |MD 42 39 44 46 27 38
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