[IGSREPORT-18478] Wk 1577 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 15 04:21:24 PDT 2010
******************************************************************************
IGS Electronic Report 15 Apr 04:21:37 PDT 2010 Message Number 18478
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1577 (Mar 28, 2010 - Apr 03, 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 2.1577.
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:
igl1577[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1577 in the SP3 format.
igl15777.sum Combination Report for GPS Week 1577.
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 | 455.2 ns
1 | 401.7 ns
2 | 458.5 ns
3 | 365.5 ns
4 | 365.7 ns
5 | 401.4 ns
6 | 394.4 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 1.1577, 1a.1577).
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 2.1577.0-6)
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 3.1577.0-6).
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 1577 summary. (Mar 28, 2010 - Apr 03, 2010)
Table 1.1577.a GPS week : 1577 MJD: 55283.0-55289.0
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 132| 2 0 3 15 16 0 -.13 24 24 | 0 1 1739 1792
| 1 0 2 30 25 64 .04 | 0 63
cod 250| -2 1 -1 52 -17 -4 -.10 15 15 | --- --- --- ---
| 1 1 1 26 16 63 .02 | --- ---
esx 142| 0 0 -7 -59 -2 -24 .43 23 22 | 79368 84 4220 9818
| 1 1 4 28 32 61 .04 | 35112 2638
iac n/a| 3 0 5 -15 30 35 -.18 23 23 | 1218589 -796 4268 149778
| 0 1 7 27 12 117 .04 | 2169417 1234
mcc n/a| 5 3 44 -36 87 -191 .14 175 175 | --- --- --- ---
| 12 7 13 275 248 1093 .38 | --- ---
Table 1.1577.b GPS week : 1577 MJD: 55283.0-55289.0
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 | 17 13 13 11 12 12 12 |
R02 | 10 13 16 14 13 13 11 |
R03 | 11 8 8 9 13 11 11 |
R04 | 20 15 12 6 10 12 11 |
R05 | 16 12 16 12 8 11 8 |
R07 | 11 14 12 10 12 8 14 |
R08 | 11 15 12 11 11 10 12 |
R10 | 13 15 12 10 15 11 9 |
R11 | 15 14 12 10 12 15 14 |
R13 | 10 17 13 13 13 10 14 |
R14 | 15 15 15 15 11 14 15 |
R15 | 45 25 16 12 15 14 15 |
R17 | 12 14 12 15 10 12 12 |
R18 | 8 10 9 10 16 11 11 |
R19 | 10 12 8 10 9 10 8 |
R20 | 14 15 12 9 11 11 16 |
R21 | 9 11 13 10 11 12 12 |
R22 | 18 13 9 10 10 11 9 |
R23 | 22 17 16 14 12 13 7 |
R24 | 15 11 11 10 10 10 12 |
Table 1.1577.c GPS week : 1577 MJD: 55283.0-55289.0
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 1577 0 | -8 -60 221 1888 -629 -24250 87.9 1884 1884 | 455177 0
brd 1577 1 | -132 16 270 1560 -1832 -20760 84.9 1730 1730 | 401684 0
brd 1577 2 | -25 13 207 -726 1336 -21330 84.9 1464 1464 | 458467 0
brd 1577 3 | 32 1 244 263 2037 -21640 87.4 1582 1582 | 365502 0
brd 1577 4 | -41 -61 190 -1753 -2157 -19890 85.7 1955 1955 | 365670 0
brd 1577 5 | 25 -4 213 -2468 -882 -16390 85.2 1706 1706 | 401400 0
brd 1577 6 | 82 -152 193 621 -414 -14290 85.8 1731 1731 | 394401 0
-------------+------------------------------------------------------------+----------------
brd 1577 mean| -9 -35 220 -87 -363 -19792 86.0 1721 1721 | 406043 0
brd 1577 sdev| 68 60 28 1637 1547 3377 1.2 166 166 | 37885 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 2.1577.0 GPS week: 1577 Day: 0 MJD: 55283
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 132| 4 0 4 7 15 77 -.18 27 26 | 0 29 1597 1641
cod 250| -5 3 -4 37 -6 48 -.12 19 17 | --- --- --- ---
esx 142| 0 0 -5 -50 -31 -88 .36 24 23 | 127662 849 3365 9756
iac n/a| 4 -1 6 -11 47 -71 -.19 26 26 | 6137879 221 3583 999999
mcc n/a| 23 6 46 81 -320 1336 -.21 150 150 | --- --- --- ---
Table 2.1577.1 GPS week: 1577 Day: 1 MJD: 55284
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 132| 3 0 6 30 -3 49 -.19 25 25 | 0 9 1711 1788
cod 250| -1 2 1 15 -5 31 -.10 19 18 | --- --- --- ---
esx 142| -1 -1 -1 -60 27 -49 .44 24 23 | 61894 -4525 3950 11351
iac n/a| 3 0 -3 10 17 -33 -.22 24 24 | 403743 -2824 4017 7966
mcc n/a| 0 1 18 2 40 958 .56 170 170 | --- --- --- ---
Table 2.1577.2 GPS week: 1577 Day: 2 MJD: 55285
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 132| 3 0 4 1 40 -79 -.12 21 22 | 0 -97 1899 1939
cod 250| -2 1 0 65 -11 24 -.11 16 14 | --- --- --- ---
esx 142| 1 0 -3 -24 -62 38 .43 23 23 | 126322 2935 4713 12352
iac n/a| 3 0 -3 -27 43 57 -.11 26 26 | 457912 98 4730 8547
mcc n/a| 15 5 59 -133 281 -1179 -.36 161 161 | --- --- --- ---
Table 2.1577.3 GPS week: 1577 Day: 3 MJD: 55286
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 132| 3 1 5 67 50 23 -.06 23 24 | 0 -30 1712 1768
cod 250| -1 0 -1 29 -38 -30 -.07 11 12 | --- --- --- ---
esx 142| -2 0 -3 -118 26 -36 .48 25 22 | 44014 2240 4690 11945
iac n/a| 3 0 5 14 26 91 -.16 22 22 | 366367 -611 4682 9807
mcc n/a| 15 5 57 97 352 -593 .62 183 183 | --- --- --- ---
Table 2.1577.4 GPS week: 1577 Day: 4 MJD: 55287
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 132| 2 0 -1 33 26 46 -.14 25 25 | 0 9 2015 2064
cod 250| -2 1 -2 55 -33 -136 -.07 15 15 | --- --- --- ---
esx 142| 0 0 -11 -46 12 -78 .43 21 21 | 43684 -2008 5227 8344
iac n/a| 3 -1 16 -65 40 248 -.23 20 20 | 367081 -2250 5287 8418
mcc n/a| -7 14 40 409 316 -1112 .03 198 198 | --- --- --- ---
Table 2.1577.5 GPS week: 1577 Day: 5 MJD: 55288
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 132| 1 -1 3 -14 14 -49 -.11 21 21 | 0 -25 1547 1600
cod 250| -1 0 -1 92 -29 -3 -.11 16 16 | --- --- --- ---
esx 142| 0 1 -14 -58 5 -39 .47 23 23 | 73873 -537 3735 7654
iac n/a| 1 0 10 -4 22 51 -.17 19 19 | 401709 -317 3719 6903
mcc n/a| -6 -4 48 -422 -115 -1233 .36 197 197 | --- --- --- ---
Table 2.1577.6 GPS week: 1577 Day: 6 MJD: 55289
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 132| 0 1 0 -20 -25 -71 -.11 26 27 | 0 112 1696 1750
cod 250| -2 0 -1 68 4 32 -.12 12 13 | --- --- --- ---
esx 142| 1 -4 -8 -59 5 80 .42 23 22 | 78127 1635 3861 7324
iac n/a| 2 4 6 -24 17 -94 -.19 24 24 | 395432 106 3863 6807
mcc n/a| 0 -4 40 -290 58 484 -.01 163 163 | --- --- --- ---
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 3.1577.0 GPS week: 1577 Day: 0 MJD: 55283
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1230 20 30 33 29 --- 16 | 46 42 61 54 --- 45
R02 | 3927 19 15 21 14 --- 10 | 42 58 35 50 --- 46
R03 | 1364 14 15 24 21 --- 11 | 39 43 43 38 --- 38
R04 | 1406 46 22 35 37 --- 20 | 26 51 81 79 --- 55
R05 | 1040 43 13 28 19 --- 15 | 31 43 61 49 --- 41
R07 | 1581 20 18 16 19 --- 10 | 32 47 50 44 --- 42
R08 | 1541 17 20 17 21 122 11 | 37 60 57 50 51 49
R10 | 3489 20 21 17 29 --- 12 | 35 38 40 40 --- 34
R11 | 2456 28 18 29 30 174 15 | 57 62 62 58 82 56
R13 | 1088 18 14 20 17 --- 10 | 41 36 44 39 --- 37
R14 | 1429 20 16 36 26 --- 14 | 28 39 66 38 --- 39
XR15 | 1139 --- 37 --- 55 165 45 | --- 62 --- 65 52 59
R17 | 1694 23 14 14 28 --- 11 | 55 60 64 68 --- 60
R18 | 2153 15 12 14 17 --- 8 | 31 30 32 32 --- 29
R19 | 837 17 10 19 19 --- 9 | 30 32 34 30 --- 29
R20 | 1044 28 18 26 26 --- 14 | 24 27 28 22 --- 18
R21 | 1114 12 10 17 20 --- 8 | 25 29 42 28 --- 28
R22 | 1096 30 29 27 34 --- 17 | 224 208 197 211 --- 208
R23 | 1741 53 27 29 40 --- 21 | 81 93 90 103 --- 88
R24 | 2123 27 20 22 36 --- 15 | 69 75 70 72 --- 69
------+------------------------------------+--------------------------------
RMS | 1884 27 19 24 26 150 |T 50 56 60 58 61 53
WRMS | 1884 26 17 23 26 150 |NE 50 56 60 58 61 53
MEDI | 1406 20 18 22 26 165 |MD 37 43 57 49 52 42
Table 3.1577.1 GPS week: 1577 Day: 1 MJD: 55284
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 780 16 21 25 22 --- 12 | 32 31 54 33 --- 35
R02 | 2781 12 24 27 22 --- 13 | 47 59 57 39 --- 49
R03 | 1231 16 13 15 12 --- 8 | 27 38 37 27 --- 31
R04 | 730 25 15 24 36 --- 14 | 26 36 43 57 --- 38
R05 | 1384 30 7 17 21 --- 11 | 21 33 45 49 --- 34
R07 | 2288 20 24 33 14 --- 14 | 38 49 60 47 --- 45
R08 | 2291 22 30 18 26 169 14 | 32 59 45 34 109 42
R10 | 3829 34 23 23 23 --- 15 | 44 49 46 35 --- 40
R11 | 900 27 23 25 18 172 13 | 34 63 50 44 169 44
R13 | 1149 44 14 33 19 --- 16 | 32 40 67 27 --- 36
R14 | 1097 30 11 32 30 --- 15 | 34 32 40 45 --- 32
XR15 | 2653 41 28 --- 37 180 25 | 37 66 --- 73 59 70
R17 | 1135 23 17 21 32 --- 13 | 47 63 57 57 --- 54
R18 | 1114 15 17 12 20 --- 9 | 28 34 30 27 --- 27
R19 | 549 11 16 25 24 --- 11 | 33 38 40 28 --- 31
R20 | 2022 26 22 21 30 --- 14 | 26 32 49 31 --- 29
R21 | 848 20 14 19 23 --- 11 | 34 34 51 30 --- 34
R22 | 2003 24 20 26 20 --- 13 | 140 135 119 137 --- 132
R23 | 1089 36 15 30 34 --- 16 | 72 81 92 96 --- 82
R24 | 1787 21 15 19 18 --- 10 | 61 60 63 65 --- 60
------+------------------------------------+--------------------------------
RMS | 1729 25 19 24 24 170 |T 42 51 55 49 112 47
WRMS | 1729 25 17 23 24 170 |NE 42 51 55 49 112 47
MEDI | 1149 23 17 24 22 172 |MD 34 40 50 39 109 38
Table 3.1577.2 GPS week: 1577 Day: 2 MJD: 55285
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1609 22 17 31 19 --- 13 | 31 38 34 28 --- 27
R02 | 1837 15 14 44 34 --- 16 | 51 52 85 37 --- 53
R03 | 1694 9 12 21 11 --- 8 | 43 45 48 39 --- 43
R04 | 786 27 13 17 24 --- 11 | 25 36 39 33 --- 29
R05 | 1003 35 12 27 31 --- 15 | 22 36 54 56 --- 36
R07 | 1859 26 13 20 20 --- 11 | 35 50 64 39 --- 45
R08 | 1572 19 22 16 24 83 12 | 32 51 52 42 73 42
R10 | 1946 11 13 28 24 --- 11 | 39 60 62 49 --- 51
R11 | 1025 16 17 18 29 239 11 | 68 81 92 96 121 82
R13 | 1591 23 16 22 30 --- 13 | 45 75 83 68 --- 66
R14 | 1191 28 11 18 43 --- 15 | 29 27 26 31 --- 23
R15 | 2312 39 20 24 19 118 15 | 35 78 48 87 44 74
R17 | 628 25 16 10 28 --- 11 | 44 51 52 66 --- 51
R18 | 1543 15 13 17 16 --- 8 | 46 42 53 39 --- 42
R19 | 618 12 9 14 20 --- 8 | 29 27 29 27 --- 25
R20 | 1580 14 13 26 31 --- 12 | 39 31 51 29 --- 34
R21 | 937 12 15 28 31 --- 12 | 31 28 53 25 --- 31
R22 | 1701 14 10 21 19 --- 9 | 75 73 71 73 --- 72
R23 | 968 24 29 24 28 --- 15 | 83 88 71 73 --- 77
R24 | 1406 14 16 22 23 --- 11 | 85 88 85 79 --- 84
------+------------------------------------+--------------------------------
RMS | 1464 21 16 23 26 161 |T 44 52 57 50 79 49
WRMS | 1464 22 14 23 26 161 |NE 44 52 57 50 79 49
MEDI | 1543 16 13 21 24 118 |MD 39 50 53 39 73 43
Table 3.1577.3 GPS week: 1577 Day: 3 MJD: 55286
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1866 29 16 16 14 --- 11 | 36 46 48 36 --- 40
R02 | 1033 19 16 36 27 --- 13 | 40 48 35 30 --- 35
R03 | 1142 9 11 17 22 --- 9 | 32 43 48 26 --- 37
R04 | 1721 16 9 10 8 --- 6 | 28 42 38 34 --- 37
R05 | 678 26 10 13 33 --- 12 | 28 36 40 52 --- 37
R07 | 1148 18 13 26 14 --- 10 | 43 55 65 40 --- 50
R08 | 878 30 12 22 14 124 11 | 33 52 62 42 68 47
R10 | 739 18 14 18 22 --- 10 | 81 91 97 81 --- 86
R11 | 992 23 9 25 17 261 10 | 65 76 88 73 102 74
R13 | 905 32 9 36 17 --- 13 | 76 89 119 87 --- 91
R14 | 1052 35 10 27 36 --- 15 | 40 50 63 57 --- 50
R15 | 2710 29 12 22 24 132 12 | 39 49 36 46 31 42
R17 | 846 26 9 42 30 --- 15 | 71 79 80 83 --- 76
R18 | 3625 20 13 26 14 --- 10 | 41 48 59 47 --- 46
R19 | 1462 27 9 17 19 --- 10 | 39 44 46 54 --- 43
R20 | 1326 22 11 10 21 --- 9 | 27 27 21 27 --- 21
R21 | 712 21 8 28 16 --- 10 | 41 40 65 44 --- 44
R22 | 1689 14 7 24 21 --- 9 | 95 89 88 100 --- 91
R23 | 944 22 16 35 25 --- 13 | 54 74 73 62 --- 62
R24 | 2427 15 7 24 21 --- 9 | 51 51 55 52 --- 49
------+------------------------------------+--------------------------------
RMS | 1582 23 11 25 22 183 |T 48 56 61 53 67 52
WRMS | 1582 24 12 22 22 183 |NE 48 56 61 53 67 52
MEDI | 1052 22 10 24 21 132 |MD 40 49 59 47 68 46
Table 3.1577.4 GPS week: 1577 Day: 4 MJD: 55287
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1855 32 23 12 14 --- 12 | 25 42 28 19 --- 23
R02 | 1099 36 19 19 12 --- 12 | 35 42 37 33 --- 31
R03 | 1155 15 20 32 19 --- 13 | 26 40 22 17 --- 20
R04 | 1787 19 13 17 17 --- 9 | 26 41 45 25 --- 32
R05 | 1090 15 8 18 14 --- 8 | 24 38 38 27 --- 30
R07 | 989 14 17 27 18 --- 11 | 37 38 20 35 --- 29
R08 | 2605 31 11 15 19 181 11 | 22 39 38 40 73 32
R10 | 982 27 21 20 33 --- 14 | 42 61 59 54 --- 51
R11 | 777 33 11 21 20 279 12 | 46 71 79 54 100 62
R13 | 612 32 20 16 18 --- 12 | 28 53 36 42 --- 37
R14 | 988 19 12 18 27 --- 11 | 27 32 28 45 --- 28
R15 | 4608 33 14 24 29 82 14 | 31 49 40 48 30 43
R17 | 1774 19 15 21 17 --- 10 | 66 58 63 56 --- 58
R18 | 3870 44 11 25 27 --- 15 | 69 48 43 37 --- 44
R19 | 2084 19 12 18 12 --- 9 | 37 30 39 46 --- 34
R20 | 1354 16 14 18 23 --- 10 | 33 20 30 29 --- 21
R21 | 742 23 13 25 14 --- 11 | 19 28 30 26 --- 18
R22 | 2073 17 15 21 17 --- 10 | 86 74 69 84 --- 75
R23 | 1500 16 16 24 22 --- 11 | 68 78 77 92 --- 77
R24 | 1654 14 14 23 17 --- 10 | 82 79 70 75 --- 74
------+------------------------------------+--------------------------------
RMS | 1955 25 15 21 20 198 |T 41 48 44 44 67 40
WRMS | 1955 25 15 21 20 198 |NE 41 48 44 44 67 40
MEDI | 1354 19 14 20 18 181 |MD 33 42 38 40 73 32
Table 3.1577.5 GPS week: 1577 Day: 5 MJD: 55288
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 836 21 16 29 11 --- 11 | 26 36 45 25 --- 29
R02 | 857 22 24 17 21 --- 12 | 21 34 23 22 --- 20
R03 | 1306 19 14 24 17 --- 10 | 25 40 32 24 --- 28
R04 | 1177 22 15 28 13 --- 11 | 16 29 42 22 --- 24
R05 | 892 14 20 16 23 --- 11 | 27 27 42 43 --- 31
R07 | 1365 13 13 13 13 --- 7 | 35 29 42 43 --- 34
R08 | 2992 19 8 25 15 212 10 | 23 28 53 36 93 31
R10 | 1304 18 17 20 22 --- 11 | 48 62 61 62 --- 56
R11 | 982 29 22 31 22 262 15 | 50 67 62 50 211 54
R13 | 785 13 16 24 17 --- 10 | 47 54 72 60 --- 56
R14 | 1602 29 12 25 26 --- 13 | 37 48 34 50 --- 39
R15 | 3039 31 9 29 24 51 13 | 40 48 26 42 22 34
R17 | 1325 16 16 18 27 --- 11 | 58 61 48 55 --- 54
R18 | 2212 17 12 33 11 --- 11 | 38 36 47 27 --- 34
R19 | 1678 13 14 21 19 --- 9 | 33 34 21 33 --- 28
R20 | 2103 17 14 15 26 --- 10 | 27 33 34 17 --- 24
R21 | 1254 18 19 22 20 --- 11 | 37 34 44 40 --- 36
R22 | 2338 27 13 15 17 --- 10 | 91 83 82 81 --- 82
R23 | 1970 29 17 32 11 --- 13 | 65 62 62 66 --- 60
R24 | 1457 19 10 16 19 --- 9 | 62 59 56 63 --- 58
------+------------------------------------+--------------------------------
RMS | 1705 21 16 23 19 197 |T 40 45 46 43 108 40
WRMS | 1705 21 16 23 19 197 |NE 40 45 46 43 108 40
MEDI | 1325 19 14 22 19 212 |MD 37 36 44 42 93 34
Table 3.1577.6 GPS week: 1577 Day: 6 MJD: 55289
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 811 30 12 16 26 --- 11 | 26 47 45 36 --- 38
R02 | 863 21 16 25 14 --- 11 | 20 45 33 27 --- 30
R03 | 1461 35 10 17 14 --- 11 | 39 44 33 24 --- 31
R04 | 2410 11 14 28 18 --- 10 | 27 42 40 29 --- 31
R05 | 1161 19 8 12 18 --- 8 | 29 41 49 36 --- 38
R07 | 1867 20 21 32 23 --- 14 | 41 52 45 36 --- 41
R08 | 2828 26 11 28 22 89 12 | 25 47 48 40 163 37
R10 | 771 22 9 15 19 --- 9 | 42 34 35 43 --- 35
R11 | 2160 37 8 30 21 252 13 | 47 59 67 42 167 53
R13 | 645 35 8 18 38 --- 14 | 38 33 42 48 --- 37
R14 | 1167 32 14 23 36 --- 14 | 30 37 36 53 --- 35
R15 | 1515 42 15 28 25 89 15 | 24 30 32 40 38 26
R17 | 624 24 12 20 29 --- 12 | 50 57 59 66 --- 56
R18 | 2452 26 7 18 29 --- 11 | 42 49 52 43 --- 44
R19 | 2133 18 11 16 13 --- 8 | 37 37 32 42 --- 34
R20 | 2694 33 8 22 45 --- 15 | 26 22 33 18 --- 18
R21 | 1319 18 17 29 12 --- 11 | 29 28 51 31 --- 30
R22 | 1681 12 9 18 23 --- 9 | 114 108 107 103 --- 107
R23 | 1652 12 6 12 17 --- 6 | 77 87 83 90 --- 83
R24 | 1703 13 19 29 13 --- 11 | 72 80 69 76 --- 73
------+------------------------------------+--------------------------------
RMS | 1731 26 12 23 24 163 |T 41 48 49 46 122 43
WRMS | 1731 27 13 22 24 163 |NE 41 48 49 46 122 43
MEDI | 1515 22 11 20 21 89 |MD 37 44 45 40 163 37
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