[IGSREPORT-17574] Wk 1537 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 9 05:08:03 PDT 2009
******************************************************************************
IGS Electronic Report 09 Jul 05:08:26 PDT 2009 Message Number 17574
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1537 (Jun 21, 2009 - Jun 27, 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 2.1537.
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:
igl1537[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1537 in the SP3 format.
igl15377.sum Combination Report for GPS Week 1537.
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 | 132.6 ns
1 | 59.3 ns
2 | 188.7 ns
3 | 195.9 ns
4 | 87.4 ns
5 | 138.0 ns
6 | 129.8 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 1.1537, 1a.1537).
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 2.1537.0-6)
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 3.1537.0-6).
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 1537 summary. (Jun 21, 2009 - Jun 27, 2009)
Table 1.1537.a GPS week : 1537 MJD: 55003.0-55009.0
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 104| 1 0 -9 -17 -22 -43 -.13 42 41 | 0 652 3651 4148
| 2 2 5 29 24 212 .05 | 0 705
cod 236| -3 0 0 1 -10 97 -.12 20 17 | --- --- --- ---
| 1 0 2 23 22 69 .04 | --- ---
esx 126| 3 -1 4 72 43 81 .31 27 25 | 34354 -149 4941 9634
| 1 2 7 53 41 66 .07 | 51135 6591
iac n/a| 0 1 2 -44 -24 -164 .00 34 34 | 133679 -1484 4950 9722
| 1 1 4 29 27 132 .03 | 50761 2414
mcc n/a| -4 -6 46 -19 -70 142 .05 200 200 | --- --- --- ---
| 17 16 30 233 169 430 .74 | --- ---
Table 1.1537.b GPS week : 1537 MJD: 55003.0-55009.0
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 | 19 22 23 26 21 20 15 |
R03 | 19 26 20 27 23 21 18 |
R07 | 26 23 21 21 19 17 18 |
R08 | 25 24 29 28 21 25 15 |
R10 | 16 15 17 18 12 19 29 |
R11 | 13 14 13 10 12 13 14 |
R13 | 12 13 13 11 11 13 10 |
R14 | 11 15 13 13 12 16 17 |
R15 | 14 15 15 18 19 11 13 |
R17 | 18 15 16 18 18 17 11 |
R18 | 11 16 15 16 16 14 15 |
R19 | 10 10 12 15 12 12 9 |
R20 | 15 15 15 15 15 17 15 |
R21 | 14 12 11 11 13 13 12 |
R22 | 15 15 12 9 18 11 16 |
R23 | 19 18 19 23 18 22 20 |
R24 | 13 16 18 25 12 21 17 |
Table 1.1537.c GPS week : 1537 MJD: 55003.0-55009.0
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 1537 0 | -120 -32 310 -380 -1738 -18250 87.9 1776 1776 | 132578 0
brd 1537 1 | -58 -4 321 -1240 -41 -16580 90.0 1812 1812 | 59288 0
brd 1537 2 | -112 -57 318 -14 -1078 -9062 87.3 1808 1808 | 188688 0
brd 1537 3 | 7 -13 351 -253 509 -7692 88.4 2061 2061 | 195868 0
brd 1537 4 | -31 -64 430 -5 -963 -9496 89.1 2108 2108 | 87373 0
brd 1537 5 | -57 -5 371 -1821 1242 -9980 90.3 2322 2322 | 138016 0
brd 1537 6 | 153 31 378 -956 1787 -14390 86.7 2141 2141 | 129806 0
-------------+------------------------------------------------------------+----------------
brd 1537 mean| -31 -20 354 -667 -40 -12207 88.5 2004 2004 | 133088 0
brd 1537 sdev| 92 33 42 690 1297 4143 1.3 208 208 | 49336 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 2.1537.0 GPS week: 1537 Day: 0 MJD: 55003
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 104| 1 0 -7 -30 -42 182 -.21 45 46 | 0 1288 4370 4829
cod 236| -2 0 0 38 -41 87 -.12 20 17 | --- --- --- ---
esx 126| 4 0 2 28 114 133 .36 24 23 | 30967 -2098 5163 9134
iac n/a| 0 1 0 -50 -24 -358 -.01 30 30 | 133938 -3416 5220 9382
mcc n/a| -25 3 41 19 -275 -211 .33 53 53 | --- --- --- ---
Table 2.1537.1 GPS week: 1537 Day: 1 MJD: 55004
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 104| 0 2 -15 -49 -21 17 -.08 48 40 | 0 696 3664 4527
cod 236| -2 0 0 22 -36 85 -.19 17 14 | --- --- --- ---
esx 126| 4 -1 13 0 -1 38 .42 27 25 | -37048 10701 4350 10030
iac n/a| 3 3 0 17 31 -198 -.02 35 35 | 57414 1116 4364 9693
mcc n/a| 5 -7 47 -73 13 -138 .06 72 72 | --- --- --- ---
Table 2.1537.2 GPS week: 1537 Day: 2 MJD: 55005
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 104| 4 -1 -12 33 -2 57 -.13 48 48 | 0 1682 3939 4558
cod 236| -2 0 0 -25 -11 18 -.12 19 16 | --- --- --- ---
esx 126| 1 2 0 60 31 -43 .21 23 22 | 92562 373 4600 10505
iac n/a| 0 0 12 -44 -34 48 .00 37 37 | 191584 -1115 4614 10846
mcc n/a| -25 -24 -8 -488 -169 432 -.49 403 403 | --- --- --- ---
Table 2.1537.3 GPS week: 1537 Day: 3 MJD: 55006
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 104| 3 0 -15 -42 -19 55 -.17 49 43 | 0 837 3088 3426
cod 236| -3 -2 -1 -7 -6 46 -.07 20 17 | --- --- --- ---
esx 126| 3 0 12 168 13 117 .24 33 32 | 99794 -9725 4385 8550
iac n/a| 1 -2 0 -69 -18 -141 -.02 36 36 | 196414 -3908 4381 9409
mcc n/a| -12 -2 34 102 51 -130 .62 124 124 | --- --- --- ---
Table 2.1537.4 GPS week: 1537 Day: 4 MJD: 55007
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 104| 3 3 -6 7 -64 73 -.09 39 41 | 0 231 4092 4581
cod 236| -4 0 -1 -19 15 60 -.07 19 15 | --- --- --- ---
esx 126| 4 -3 8 93 85 76 .32 28 26 | -18368 5170 5931 9824
iac n/a| 2 1 0 -63 -31 -256 -.04 32 32 | 85623 2401 5955 9675
mcc n/a| -1 -30 45 107 203 469 1.17 176 176 | --- --- --- ---
Table 2.1537.5 GPS week: 1537 Day: 5 MJD: 55008
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 104| -1 0 -7 -14 7 -332 -.10 34 34 | 0 257 3133 3639
cod 236| -5 0 6 -10 17 168 -.10 22 22 | --- --- --- ---
esx 126| 3 -3 -4 93 29 94 .26 28 25 | 44084 -4400 4575 9217
iac n/a| -1 1 2 -57 -57 -58 .03 34 34 | 139878 -3101 4589 9446
mcc n/a| 22 3 71 246 -89 835 -1.08 281 281 | --- --- --- ---
Table 2.1537.6 GPS week: 1537 Day: 6 MJD: 55009
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 104| 1 -4 -2 -30 -16 -358 -.12 33 34 | 0 -421 3277 3482
cod 236| -5 0 1 10 -8 214 -.15 21 18 | --- --- --- ---
esx 126| 0 0 -1 65 33 152 .35 25 23 | 28492 -1070 5588 10184
iac n/a| 0 2 0 -45 -40 -188 .06 32 32 | 130904 -2365 5528 9604
mcc n/a| 4 16 90 -54 -223 -259 -.24 294 294 | --- --- --- ---
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 3.1537.0 GPS week: 1537 Day: 0 MJD: 55003
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1065 46 18 31 40 --- 18 | 68 55 76 60 --- 58
R03E | 2905 45 26 25 38 --- 18 | 75 58 54 62 --- 56
R07E | 2127 81 26 29 49 --- 25 | 43 32 53 50 --- 36
R08E | 636 87 25 30 33 --- 24 | 49 73 67 77 --- 66
R10 | 1470 40 29 21 21 --- 16 | 41 65 44 54 --- 49
R11 | 715 29 22 18 24 --- 13 | 31 42 63 37 --- 41
R13 | 2845 26 13 28 16 --- 12 | 38 45 42 33 --- 37
R14 | 1914 24 14 24 17 --- 11 | 43 43 68 43 --- 46
R15 | 2322 30 15 19 33 53 13 | 34 34 44 41 43 36
R17 | 684 42 20 17 42 --- 17 | 73 86 92 62 --- 78
R18 | 1127 32 11 17 20 --- 11 | 53 62 65 71 --- 62
R19 | 1737 26 6 19 17 --- 9 | 49 49 63 52 --- 51
R20 | 887 43 13 24 30 --- 15 | 39 41 55 53 --- 40
R21 | 917 34 22 23 22 --- 14 | 35 62 62 42 --- 50
R22 | 760 31 16 28 29 --- 14 | 39 55 66 40 --- 49
R23 | 2004 56 23 33 28 --- 19 | 57 60 66 72 --- 58
R24 | 2885 19 17 21 29 --- 12 | 76 96 101 76 --- 89
------+------------------------------------+--------------------------------
RMS | 1776 45 20 24 30 53 |T 49 56 63 54 43 53
WRMS | 1776 46 17 23 30 53 |NE 52 59 67 54 43 57
MEDI | 1470 34 18 24 29 53 |MD 43 55 63 53 43 50
Table 3.1537.1 GPS week: 1537 Day: 1 MJD: 55004
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1471 66 20 25 49 --- 21 | 70 55 69 66 --- 57
R03E | 2071 86 17 33 56 --- 26 | 54 39 44 58 --- 35
R07E | 3318 65 30 23 51 --- 23 | 43 66 63 55 --- 53
R08E | 1354 85 20 29 40 --- 23 | 47 47 64 49 --- 43
R10M | 872 37 16 25 31 --- 14 | 33 49 43 31 --- 37
R11 | 737 26 14 20 37 --- 13 | 22 50 59 39 --- 42
R13 | 1437 23 13 24 30 --- 12 | 21 28 30 20 --- 20
R14 | 1285 33 22 29 25 --- 15 | 26 35 41 28 --- 26
R15 | 4408 46 13 24 31 72 15 | 37 40 47 41 72 39
R17 | 696 35 10 35 29 --- 15 | 40 59 92 58 --- 63
R18 | 732 49 11 20 33 --- 15 | 38 52 67 88 --- 59
R19 | 959 13 8 18 26 --- 9 | 22 27 35 45 --- 28
R20M | 1387 19 17 27 39 --- 14 | 20 30 46 31 --- 27
R21M | 595 37 12 17 22 --- 11 | 24 38 44 34 --- 33
R22 | 676 33 13 38 22 --- 15 | 29 41 68 33 --- 40
R23 | 1567 25 25 30 41 --- 17 | 31 50 41 31 --- 31
R24 | 2221 49 21 27 15 --- 16 | 45 77 93 70 --- 72
------+------------------------------------+--------------------------------
RMS | 1812 48 17 27 35 72 |T 35 46 55 45 72 41
WRMS | 1812 40 14 25 35 72 |NE 32 45 57 50 72 43
MEDI | 1354 37 16 25 31 72 |MD 33 47 47 41 72 39
Table 3.1537.2 GPS week: 1537 Day: 2 MJD: 55005
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1375 63 22 28 59 --- 23 | 62 52 57 65 --- 50
R03E | 3067 57 27 25 41 --- 20 | 60 35 61 56 --- 41
R07E | 3831 76 16 25 38 --- 21 | 33 31 44 34 --- 27
R08E | 914 105 24 19 64 340 29 | 40 49 49 65 303 44
R10 | 1796 46 26 19 31 --- 16 | 48 57 45 51 --- 48
R11M | 1401 28 17 18 33 591 13 | 33 38 55 39 515 40
R13 | 1289 31 11 25 24 --- 12 | 30 40 53 30 --- 37
R14 | 2742 30 15 21 27 --- 12 | 45 42 51 37 --- 39
R15 | 2047 38 16 25 33 150 15 | 37 36 67 37 48 42
R17 | 927 45 14 28 26 --- 15 | 54 59 87 72 --- 68
R18 | 1511 45 20 19 24 --- 14 | 51 90 85 63 --- 78
R19 | 496 25 15 11 36 --- 12 | 39 40 45 71 --- 44
R20 | 853 33 20 18 35 --- 14 | 25 36 43 44 --- 32
R21 | 771 24 12 16 24 --- 10 | 34 42 43 45 --- 38
R22M | 501 32 8 22 25 --- 12 | 55 53 54 51 --- 50
R23M | 934 37 21 21 54 --- 18 | 51 59 70 101 --- 65
R24 | 2085 33 22 38 31 --- 17 | 132 145 150 145 --- 140
------+------------------------------------+--------------------------------
RMS | 1808 48 19 23 37 403 |T 48 53 62 59 288 51
WRMS | 1808 48 16 22 37 403 |NE 55 64 76 65 48 64
MEDI | 1375 37 17 21 33 340 |MD 45 42 54 51 303 44
Table 3.1537.3 GPS week: 1537 Day: 3 MJD: 55006
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1221 86 23 39 44 --- 26 | 51 41 53 41 --- 38
R03E | 3850 95 23 40 39 --- 27 | 50 37 48 33 --- 30
R07E | 2158 44 28 29 45 --- 20 | 46 40 57 38 --- 37
R08E | 1399 76 25 40 61 105 27 | 34 40 56 66 42 37
R10 | 1587 44 14 33 39 --- 18 | 58 64 52 71 --- 57
R11 | 1785 17 10 21 20 154 9 | 28 26 49 44 35 32
R13 | 1305 27 18 19 16 --- 11 | 24 40 37 31 --- 30
R14 | 4210 28 17 15 28 --- 12 | 30 37 38 30 --- 27
R15 | 2985 37 16 32 44 107 18 | 36 35 47 48 41 35
R17 | 1089 42 17 34 39 --- 18 | 46 70 81 40 --- 58
R18 | 2332 38 16 38 18 --- 15 | 38 71 83 70 --- 67
R19 | 437 29 19 38 19 --- 15 | 36 47 85 54 --- 53
R20 | 1724 30 20 32 24 --- 14 | 49 47 77 65 --- 55
R21 | 1201 19 14 26 16 --- 10 | 21 38 48 31 --- 32
R22 | 567 22 9 16 18 --- 9 | 96 93 90 100 --- 93
R23 | 940 50 19 32 58 --- 22 | 62 78 99 101 --- 80
R24 | 1669 58 31 57 30 --- 24 | 54 112 136 81 --- 99
------+------------------------------------+--------------------------------
RMS | 2061 49 20 33 36 124 |T 44 53 66 55 39 50
WRMS | 2061 43 17 32 36 124 |NE 37 58 72 50 41 52
MEDI | 1587 38 18 32 30 107 |MD 46 41 56 48 41 38
Table 3.1537.4 GPS week: 1537 Day: 4 MJD: 55007
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1019 58 19 26 44 --- 20 | 44 17 26 42 --- 21
R03E | 2571 68 24 32 41 --- 23 | 57 32 40 42 --- 29
R07E | 2748 46 28 32 30 --- 19 | 49 38 39 28 --- 30
R08E | 1198 41 30 34 43 180 21 | 47 37 34 34 45 29
R10 | 1051 24 11 21 28 --- 12 | 47 46 46 50 --- 45
R11 | 1074 29 15 24 18 215 12 | 34 34 52 36 29 33
R13 | 2257 25 15 19 21 --- 11 | 28 24 32 32 --- 22
R14 | 5400 27 12 25 18 --- 11 | 43 21 37 28 --- 26
R15 | 1634 42 23 28 43 121 19 | 29 30 36 32 26 22
R17 | 1325 20 24 19 49 --- 17 | 58 59 58 31 --- 46
R18 | 2720 31 16 38 29 --- 16 | 53 49 73 47 --- 51
R19 | 652 34 9 21 20 --- 11 | 46 42 41 56 --- 43
R20 | 1625 36 15 36 20 --- 15 | 54 51 80 63 --- 58
R21 | 1798 30 14 28 20 --- 13 | 45 43 73 67 --- 53
R22 | 887 49 14 40 22 --- 17 | 160 155 163 151 --- 155
R23 | 1417 48 20 20 37 --- 17 | 89 77 62 84 --- 74
R24 | 1192 16 9 23 31 --- 11 | 106 98 70 81 --- 87
------+------------------------------------+--------------------------------
RMS | 2107 39 19 28 32 176 |T 58 50 56 53 33 48
WRMS | 2107 41 15 26 32 176 |NE 51 46 49 43 26 42
MEDI | 1417 34 15 26 29 180 |MD 47 42 46 42 29 43
Table 3.1537.5 GPS week: 1537 Day: 5 MJD: 55008
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1722 33 27 21 53 --- 19 | 32 28 38 60 --- 33
R03E | 4856 45 25 28 48 --- 21 | 55 27 45 53 --- 34
R07E | 3803 34 16 25 43 --- 17 | 51 45 50 31 --- 36
R08E | 1205 64 19 47 35 340 24 | 38 28 52 47 37 28
R10 | 1875 43 26 27 36 --- 19 | 31 34 32 27 --- 24
R11 | 1175 27 16 25 21 315 13 | 25 26 43 33 23 26
R13 | 2083 19 21 24 19 --- 12 | 24 39 41 27 --- 26
R14 | 3559 24 25 34 21 --- 15 | 36 32 41 26 --- 29
R15 | 2363 21 18 17 23 148 11 | 20 29 32 49 34 30
R17 | 1374 23 33 19 34 --- 16 | 55 55 37 37 --- 39
R18 | 2956 20 31 16 20 --- 13 | 26 36 36 27 --- 25
R19 | 1006 19 14 20 29 --- 11 | 28 32 33 21 --- 24
R20 | 2136 34 18 27 40 --- 17 | 42 45 31 50 --- 35
R21 | 1053 25 14 29 18 --- 12 | 55 39 30 46 --- 36
R22 | 991 24 16 19 18 --- 11 | 237 241 240 246 --- 241
R23 | 1429 39 25 41 45 --- 21 | 153 157 137 149 --- 148
R24 | 1167 44 24 38 36 --- 20 | 38 52 55 37 --- 40
------+------------------------------------+--------------------------------
RMS | 2322 34 22 28 34 281 |T 55 55 57 56 31 50
WRMS | 2322 34 22 25 34 281 |NE 32 39 39 32 34 30
MEDI | 1722 27 21 25 34 315 |MD 38 36 41 37 34 33
Table 3.1537.6 GPS week: 1537 Day: 6 MJD: 55009
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 3991 23 22 16 38 --- 14 | 41 37 43 47 --- 38
R03E | 2582 21 21 18 58 --- 18 | 48 37 38 50 --- 34
R07E | 3749 34 28 28 38 --- 18 | 39 56 55 48 --- 43
R08E | 3294 31 12 26 32 352 14 | 36 34 53 59 44 40
R10 | 1169 64 43 49 41 --- 28 | 67 63 74 69 --- 61
R11 | 927 39 17 18 17 332 13 | 39 26 41 30 31 29
R13 | 2379 22 11 18 15 --- 9 | 24 30 35 33 --- 26
R14 | 1165 23 29 32 28 --- 16 | 34 35 55 27 --- 33
R15 | 1345 24 21 20 27 155 13 | 22 37 32 36 29 28
R17 | 858 23 18 11 21 --- 10 | 63 57 53 45 --- 51
R18 | 2559 46 13 21 12 --- 14 | 43 67 71 54 --- 59
R19 | 1146 18 14 15 17 --- 9 | 53 57 55 44 --- 51
R20 | 2031 36 12 25 30 --- 14 | 39 43 47 54 --- 42
R21 | 1641 17 16 26 18 --- 11 | 45 54 51 50 --- 47
R22 | 767 32 20 24 33 --- 15 | 293 287 294 301 --- 292
R23 | 1217 43 26 33 40 --- 20 | 196 196 221 208 --- 202
R24 | 1355 30 20 20 46 --- 17 | 54 76 68 59 --- 62
------+------------------------------------+--------------------------------
RMS | 2140 33 21 25 32 294 |T 66 70 75 71 34 66
WRMS | 2140 34 18 23 32 294 |NE 41 51 52 42 29 44
MEDI | 1355 30 20 21 30 332 |MD 43 54 53 50 31 43
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