[IGSREPORT-18306] Wk 1569 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Fri Feb 19 06:49:27 PST 2010
******************************************************************************
IGS Electronic Report 19 Feb 06:49:51 PST 2010 Message Number 18306
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1569 (Jan 31, 2010 - Feb 06, 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 2.1569.
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:
igl1569[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1569 in the SP3 format.
igl15697.sum Combination Report for GPS Week 1569.
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 | 430.3 ns
1 | 378.2 ns
2 | 339.0 ns
3 | 334.5 ns
4 | 332.7 ns
5 | 454.6 ns
6 | 339.6 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 1.1569, 1a.1569).
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 2.1569.0-6)
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 3.1569.0-6).
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 1569 summary. (Jan 31, 2010 - Feb 06, 2010)
Table 1.1569.a GPS week : 1569 MJD: 55227.0-55233.0
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 128| 0 0 1 -42 -5 -34 -.11 22 21 | 0 268 2154 2307
| 1 1 3 41 20 159 .04 | 0 531
cod 242| 0 0 -4 50 -13 19 -.11 16 15 | --- --- --- ---
| 0 1 2 33 19 37 .04 | --- ---
esx 130| 0 0 -1 -10 42 31 .39 26 24 | 20487 -1291 4288 8868
| 2 2 3 38 13 59 .03 | 51435 2175
iac n/a| 1 2 7 -36 2 -44 -.11 27 27 | 1739965 3002 146458 150226
| 1 1 6 43 23 106 .04 | 3642603 9563
mcc n/a| 6 2 23 -29 0 434 -.21 117 117 | --- --- --- ---
| 8 11 24 70 81 782 .24 | --- ---
Table 1.1569.b GPS week : 1569 MJD: 55227.0-55233.0
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 | 12 11 11 11 10 9 13 |
R02 | 15 12 10 7 11 13 8 |
R03 | 13 11 12 10 12 12 10 |
R04 | 11 12 10 12 13 13 13 |
R05 | 14 17 15 12 10 10 13 |
R07 | 22 24 10 7 12 15 14 |
R08 | 13 11 10 11 10 11 15 |
R10 | 14 15 16 12 12 11 9 |
R11 | 8 10 12 14 10 11 16 |
R13 | 17 9 8 11 12 18 11 |
R14 | 13 9 8 12 12 14 16 |
R15 | 13 11 8 8 10 19 18 |
R17 | 16 12 16 18 13 16 16 |
R18 | 17 12 9 10 11 12 11 |
R19 | 17 11 12 15 14 17 15 |
R20 | 16 16 17 20 17 16 16 |
R21 | 11 14 15 15 14 13 12 |
R23 | 15 16 12 12 13 14 18 |
Table 1.1569.c GPS week : 1569 MJD: 55227.0-55233.0
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 1569 0 | -24 52 4 -5675 -219 -13690 87.1 2299 2299 | 430283 0
brd 1569 1 | 9 -59 -182 -305 1818 -12670 82.8 2400 2400 | 378229 0
brd 1569 2 | 51 162 24 2806 3876 -11040 85.4 2287 2287 | 339018 0
brd 1569 3 | -45 -60 -73 3538 1412 -9760 87.0 2566 2566 | 334480 0
brd 1569 4 | 164 150 -28 -1477 -1257 -12020 88.8 4472 4472 | 332710 0
brd 1569 5 | 87 6 -142 1334 -1445 -11720 87.3 3806 3806 | 454553 0
brd 1569 6 | -116 -30 -80 618 -2314 -18560 86.5 2625 2625 | 339553 0
-------------+------------------------------------------------------------+----------------
brd 1569 mean| 18 31 -68 119 267 -12780 86.4 2922 2922 | 372689 0
brd 1569 sdev| 92 93 75 3080 2194 2831 1.9 862 862 | 50562 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 2.1569.0 GPS week: 1569 Day: 0 MJD: 55227
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 128| 0 0 4 -91 -6 99 -.14 21 20 | 0 741 2291 2419
cod 242| -1 0 -1 80 -15 19 -.09 19 17 | --- --- --- ---
esx 130| 0 0 -2 27 43 0 .43 30 27 | 76221 2389 4898 9615
iac n/a| 0 4 -2 -22 22 -188 -.12 29 29 | 9999999 24401 999999 999999
mcc n/a| 7 -11 3 -113 -18 -311 .05 110 110 | --- --- --- ---
Table 2.1569.1 GPS week: 1569 Day: 1 MJD: 55228
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 128| 0 2 0 -35 -24 34 -.06 17 17 | 0 -126 2067 2296
cod 242| 0 0 -5 39 5 18 -.06 17 17 | --- --- --- ---
esx 130| -1 3 5 12 46 3 .34 27 26 | 32541 -3431 4075 8213
iac n/a| 2 0 1 -33 -1 -133 -.08 27 27 | 378362 1513 4115 7008
mcc n/a| 5 0 15 -17 0 31 -.39 102 102 | --- --- --- ---
Table 2.1569.2 GPS week: 1569 Day: 2 MJD: 55229
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 128| 1 0 4 6 -12 -109 -.08 20 20 | 0 -478 2090 2221
cod 242| 0 0 -4 13 -14 65 -.08 13 12 | --- --- --- ---
esx 130| -1 3 -2 -55 38 -16 .39 27 25 | -14549 -2365 3909 7971
iac n/a| 1 2 5 -1 31 -16 -.16 26 26 | 338016 189 3934 8457
mcc n/a| -1 -1 25 45 -32 -210 -.14 73 73 | --- --- --- ---
Table 2.1569.3 GPS week: 1569 Day: 3 MJD: 55230
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 128| -1 -1 2 -6 29 26 -.06 22 21 | 0 -235 2262 2422
cod 242| 0 0 -6 22 -36 -24 -.11 14 13 | --- --- --- ---
esx 130| -2 -2 0 -63 18 -7 .36 27 25 | -25943 -1454 4034 10206
iac n/a| 0 0 9 -15 11 42 -.12 26 26 | 334362 -323 4034 10078
mcc n/a| 5 7 1 6 -35 53 -.13 77 77 | --- --- --- ---
Table 2.1569.4 GPS week: 1569 Day: 4 MJD: 55231
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 128| 0 1 -2 -92 10 103 -.09 23 22 | 0 492 1964 2129
cod 242| 0 0 -5 87 -36 -26 -.18 14 15 | --- --- --- ---
esx 130| 1 -1 -2 32 59 25 .42 20 19 | -21780 -1121 4603 8233
iac n/a| 1 2 17 -95 -40 -89 -.07 27 27 | 333800 -1141 4632 8045
mcc n/a| 2 -2 11 -87 -45 486 -.25 99 99 | --- --- --- ---
Table 2.1569.5 GPS week: 1569 Day: 5 MJD: 55232
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 128| -3 1 0 -65 -29 -45 -.16 25 25 | 0 803 2282 2438
cod 242| -1 1 -2 88 -8 19 -.16 19 17 | --- --- --- ---
esx 130| 0 -1 -3 -5 55 64 .40 24 22 | 102714 -3644 4193 7943
iac n/a| 1 2 6 -95 7 -51 -.04 27 27 | 456404 -3563 4203 8326
mcc n/a| 25 3 31 56 -44 1243 -.62 136 136 | --- --- --- ---
Table 2.1569.6 GPS week: 1569 Day: 6 MJD: 55233
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 128| -2 0 -3 -11 -5 -352 -.15 25 24 | 0 682 2123 2224
cod 242| 0 -1 -7 24 14 65 -.12 20 17 | --- --- --- ---
esx 130| 2 0 -1 -17 38 152 .41 26 22 | -5795 588 4307 9895
iac n/a| 0 4 11 11 -12 126 -.16 24 24 | 338812 -61 4295 9674
mcc n/a| 2 23 72 -100 181 1751 .01 221 221 | --- --- --- ---
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 3.1569.0 GPS week: 1569 Day: 0 MJD: 55227
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1991 15 13 23 28 --- 11 | 47 50 45 30 --- 41
R02 | 1990 14 23 40 20 --- 14 | 30 32 41 28 --- 28
R03 | 1231 22 15 27 26 --- 12 | 35 39 36 28 --- 31
R04 | 2138 21 11 24 16 --- 10 | 33 34 41 37 --- 34
R05 | 3590 16 26 32 22 --- 14 | 35 45 47 28 --- 34
XR07 |14416 32 30 --- 27 --- 21 | 30 33 --- 34 --- 26
R08 | 3073 13 17 20 38 120 13 | 34 45 37 22 42 32
R10 | 2116 19 21 31 26 --- 14 | 28 29 56 32 --- 29
R11 | 1928 13 6 19 15 112 7 | 14 18 31 21 36 14
R13 | 1270 25 20 36 35 --- 16 | 14 22 51 32 --- 21
R14 | 2234 14 20 24 30 --- 13 | 24 27 43 32 --- 27
R15 | 5305 29 19 19 20 97 13 | 20 21 27 24 14 17
R17 | 975 16 18 25 46 --- 15 | 71 73 63 73 --- 69
R18 | 1119 30 18 41 27 --- 17 | 88 82 100 94 --- 88
R19 | 879 20 24 49 23 --- 17 | 75 67 78 82 --- 71
R20 | 1595 22 20 31 39 --- 16 | 42 45 58 45 --- 44
R21 | 1724 22 10 15 25 --- 10 | 108 111 104 114 --- 109
R23 | 1433 27 20 28 31 --- 15 | 67 78 98 95 --- 81
------+------------------------------------+--------------------------------
RMS | 2299 21 19 30 29 110 |T 44 47 56 47 30 44
WRMS | 2299 20 17 27 29 110 |NE 44 47 56 47 30 44
MEDI | 1928 20 19 27 26 112 |MD 34 39 47 32 36 32
Table 3.1569.1 GPS week: 1569 Day: 1 MJD: 55228
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2409 9 11 28 30 --- 11 | 26 28 37 27 --- 24
R02 | 1347 8 22 31 15 --- 11 | 29 23 42 27 --- 25
R03 | 2275 13 11 34 17 --- 11 | 26 31 31 27 --- 25
R04 | 1751 15 12 33 25 --- 12 | 36 53 62 37 --- 44
R05 | 1274 36 19 32 22 --- 16 | 40 28 32 29 --- 24
XR07 | 6468 21 37 --- 42 --- 23 | 26 48 --- 25 --- 24
R08 | 3899 13 18 14 28 119 10 | 21 31 24 32 35 22
R10 | 3291 24 23 27 25 --- 14 | 16 27 35 23 --- 15
R11 | 1452 14 14 15 27 94 10 | 26 30 28 24 54 24
R13 | 1100 10 10 22 21 --- 9 | 17 16 34 18 --- 17
R14 | 3738 9 11 24 21 --- 9 | 30 29 30 32 --- 26
R15 | 3267 9 20 22 23 92 10 | 20 26 36 39 32 26
R17 | 1434 15 16 21 30 --- 11 | 27 32 36 49 --- 32
R18 | 1026 17 16 23 28 --- 12 | 56 61 71 66 --- 60
R19 | 784 15 13 20 30 --- 11 | 52 55 68 56 --- 53
R20 | 1431 22 19 23 46 --- 16 | 34 43 42 39 --- 38
R21 | 3693 13 21 43 17 --- 14 | 65 86 84 69 --- 73
R23 | 2648 20 21 37 32 --- 15 | 48 58 91 67 --- 60
------+------------------------------------+--------------------------------
RMS | 2400 17 17 27 27 102 |T 33 39 46 38 40 34
WRMS | 2400 17 17 26 27 102 |NE 33 39 46 38 40 34
MEDI | 1751 14 16 24 25 94 |MD 27 31 36 32 35 25
Table 3.1569.2 GPS week: 1569 Day: 2 MJD: 55229
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1420 15 12 26 24 --- 10 | 39 33 30 26 --- 28
R02 | 2273 14 13 24 21 --- 10 | 31 24 47 34 --- 27
R03 | 2027 15 13 28 28 --- 11 | 34 42 42 28 --- 34
R04 | 2088 16 10 25 21 --- 10 | 35 40 38 35 --- 35
R05 | 2053 29 14 36 28 --- 15 | 37 31 56 32 --- 31
R07 | 3633 20 14 18 15 --- 10 | 31 39 29 33 --- 31
R08 | 1860 12 11 17 28 81 9 | 34 32 34 43 37 32
R10 | 2904 26 20 35 28 --- 15 | 30 29 53 29 --- 29
R11 | 1544 21 16 25 21 73 11 | 16 28 37 26 48 20
R13 | 783 12 8 18 21 --- 8 | 27 12 32 18 --- 17
R14 | 3676 13 12 17 16 --- 8 | 27 27 29 26 --- 23
R15 | 2070 13 12 12 20 64 8 | 24 22 37 34 35 24
R17 | 2340 22 17 36 36 --- 15 | 34 33 58 44 --- 35
R18 | 997 17 10 10 26 --- 9 | 105 111 113 127 --- 112
R19 | 1052 16 9 29 30 --- 12 | 60 67 62 72 --- 62
R20 | 2590 36 12 27 41 --- 16 | 41 47 54 45 --- 45
R21 | 1449 12 13 45 29 --- 14 | 132 143 172 135 --- 144
R23 | 3464 23 10 22 30 --- 11 | 58 73 78 77 --- 68
------+------------------------------------+--------------------------------
RMS | 2287 20 13 27 26 73 |T 44 46 55 48 40 44
WRMS | 2287 20 12 25 26 73 |NE 44 46 55 48 40 44
MEDI | 2053 16 12 25 26 73 |MD 34 33 42 34 37 31
Table 3.1569.3 GPS week: 1569 Day: 3 MJD: 55230
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1217 24 10 22 19 --- 10 | 27 35 35 35 --- 29
R02 | 1648 9 10 16 13 --- 7 | 31 30 32 19 --- 27
R03 | 1395 12 9 23 24 --- 9 | 29 35 43 27 --- 30
R04 | 1818 16 16 22 31 --- 12 | 49 59 59 50 --- 53
R05 | 1974 18 18 24 22 --- 11 | 26 32 32 29 --- 22
R07 | 2772 12 6 14 19 --- 7 | 23 33 22 34 --- 27
R08 | 1643 17 12 29 17 45 10 | 35 40 37 37 28 34
R10 | 3493 25 12 14 29 --- 11 | 24 20 32 23 --- 19
R11 | 3149 17 18 39 21 114 13 | 27 22 53 27 45 23
R13 | 1824 19 13 27 18 --- 11 | 12 21 25 19 --- 14
R14 | 1441 22 15 25 22 --- 11 | 22 18 34 22 --- 16
R15 | 1619 14 8 19 15 51 8 | 18 20 28 26 25 19
R17 | 2072 17 21 50 35 --- 17 | 25 28 50 39 --- 21
R18 | 670 22 7 16 23 --- 9 | 60 67 64 74 --- 64
R19 | 1655 28 21 28 27 --- 14 | 36 61 47 50 --- 48
R20 | 4959 41 8 35 54 --- 19 | 31 44 63 45 --- 40
R21 | 1914 33 13 30 32 --- 15 | 63 84 104 71 --- 78
R23 | 5376 21 16 22 24 --- 11 | 71 85 91 84 --- 81
------+------------------------------------+--------------------------------
RMS | 2566 22 14 27 26 77 |T 33 40 47 39 32 35
WRMS | 2566 21 13 25 26 77 |NE 33 40 47 39 32 35
MEDI | 1818 18 12 23 22 51 |MD 27 33 37 34 28 27
Table 3.1569.4 GPS week: 1569 Day: 4 MJD: 55231
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 785 19 11 19 18 --- 9 | 30 34 31 36 --- 29
R02 | 1451 19 17 17 26 --- 11 | 16 28 39 29 --- 24
R03 | 1852 11 17 24 25 --- 11 | 29 35 32 24 --- 27
R04 | 929 17 20 19 34 --- 13 | 19 41 41 29 --- 30
R05 | 3620 12 15 9 27 --- 9 | 27 37 32 26 --- 30
R07 |15052 28 14 23 21 --- 12 | 55 35 32 27 --- 35
R08 | 1546 10 11 11 32 77 9 | 21 31 30 31 26 22
R10 | 4466 17 19 17 30 --- 12 | 24 17 33 30 --- 19
R11 | 3626 19 13 19 20 149 10 | 28 17 39 23 33 21
R13 | 2183 28 10 26 20 --- 12 | 19 24 37 23 --- 20
R14 | 1886 19 19 17 30 --- 12 | 20 26 24 21 --- 15
R15 | 1752 16 14 22 19 36 10 | 25 18 24 25 19 14
R17 | 730 28 16 20 23 --- 12 | 20 26 33 39 --- 22
R18 | 970 25 9 17 23 --- 10 | 119 126 141 146 --- 130
R19 | 1462 33 10 22 29 --- 13 | 76 85 91 89 --- 83
R20 | 4721 45 11 24 36 --- 17 | 36 55 60 47 --- 49
R21 | 2407 18 12 29 35 --- 13 | 146 157 176 142 --- 156
R23 | 5883 22 11 21 35 --- 12 | 71 69 84 61 --- 70
------+------------------------------------+--------------------------------
RMS | 4471 23 14 20 27 99 |T 43 47 54 47 26 44
WRMS | 4471 22 15 19 27 99 |NE 43 47 54 47 26 44
MEDI | 1852 19 13 19 26 77 |MD 27 34 33 29 26 27
Table 3.1569.5 GPS week: 1569 Day: 5 MJD: 55232
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1726 24 11 13 13 --- 9 | 18 29 39 33 --- 26
R02 | 1832 18 20 26 19 --- 12 | 22 23 36 28 --- 21
R03 | 1048 15 23 21 20 --- 12 | 23 32 36 21 --- 24
R04 | 1841 26 18 20 26 --- 13 | 32 33 35 29 --- 26
R05 | 3550 15 17 16 21 --- 10 | 19 28 25 26 --- 22
R07 |12273 28 16 22 34 --- 14 | 48 43 38 19 --- 36
R08 | 1460 28 11 13 21 150 11 | 30 31 43 29 19 29
R10 | 4497 19 16 10 28 --- 10 | 21 19 24 21 --- 16
R11 | 1582 16 16 12 26 170 10 | 14 19 33 37 24 20
R13 | 1825 26 21 45 28 --- 18 | 24 17 60 21 --- 19
R14 | 2735 32 12 30 14 --- 13 | 14 19 28 26 --- 12
R15 | 2194 40 19 20 48 67 18 | 31 26 23 24 17 17
R17 | 931 25 25 33 21 --- 15 | 35 27 60 32 --- 33
R18 | 1598 27 15 21 18 --- 11 | 54 76 91 80 --- 74
R19 | 969 21 33 29 31 --- 17 | 38 47 67 62 --- 50
R20 | 4575 25 21 29 33 --- 15 | 26 45 57 33 --- 37
R21 | 1116 28 19 19 22 --- 12 | 59 88 95 71 --- 78
R23 | 4431 21 15 22 35 --- 13 | 57 58 57 78 --- 59
------+------------------------------------+--------------------------------
RMS | 3806 25 19 24 27 136 |T 31 36 47 37 20 33
WRMS | 3806 25 17 22 27 136 |NE 31 36 47 37 20 33
MEDI | 1825 25 17 21 22 150 |MD 26 29 38 29 19 26
Table 3.1569.6 GPS week: 1569 Day: 6 MJD: 55233
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1872 26 18 22 19 --- 12 | 55 45 35 37 --- 41
R02 | 1187 11 8 22 13 --- 8 | 28 37 49 31 --- 34
R03 | 1064 23 14 12 18 --- 10 | 28 45 40 30 --- 34
R04 | 2403 28 23 16 17 --- 12 | 43 42 47 39 --- 40
R05 | 1906 17 19 28 22 --- 12 | 31 49 48 32 --- 37
R07 | 2481 15 27 22 25 --- 13 | 41 48 26 29 --- 34
R08 | 1572 29 18 18 33 228 14 | 44 43 33 30 26 32
R10 | 4921 18 11 17 17 --- 9 | 17 31 44 38 --- 30
R11 | 1007 30 21 34 27 265 16 | 23 20 51 37 41 23
R13 | 1596 21 14 23 16 --- 10 | 31 19 41 26 --- 22
R14 | 1511 30 17 39 16 --- 15 | 22 23 47 21 --- 21
R15 | 6076 43 25 25 29 157 18 | 48 31 31 21 15 24
R17 | 2410 31 13 41 21 --- 16 | 33 44 46 47 --- 41
R18 | 1079 19 12 24 20 --- 11 | 72 74 89 74 --- 76
R19 | 1805 13 31 21 29 --- 14 | 41 53 48 43 --- 43
R20 | 4040 20 27 41 17 --- 16 | 25 37 53 34 --- 31
R21 | 979 15 22 13 26 --- 11 | 75 78 87 86 --- 81
R23 | 2340 30 26 28 41 --- 18 | 67 78 91 105 --- 83
------+------------------------------------+--------------------------------
RMS | 2625 25 20 26 24 221 |T 40 44 50 42 27 40
WRMS | 2625 24 17 22 24 221 |NE 40 44 50 42 27 40
MEDI | 1805 21 18 22 20 228 |MD 33 43 47 34 26 34
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