[IGSREPORT-17374] Wk 1528 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu May 7 05:40:55 PDT 2009
******************************************************************************
IGS Electronic Report 07 May 05:41:17 PDT 2009 Message Number 17374
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1528 (Apr 19, 2009 - Apr 25, 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 2.1528.
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:
igl1528[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1528 in the SP3 format.
igl15287.sum Combination Report for GPS Week 1528.
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 | 221.8 ns
1 | 223.4 ns
2 | 227.7 ns
3 | 227.5 ns
4 | 151.8 ns
5 | 227.7 ns
6 | 233.7 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
3 | BKG | R07
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 1.1528, 1a.1528).
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 2.1528.0-6)
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 3.1528.0-6).
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 1528 summary. (Apr 19, 2009 - Apr 25, 2009)
Table 1.1528.a GPS week : 1528 MJD: 54940.0-54946.0
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 88| 2 0 -3 13 -21 103 -.16 25 24 | 0 -954 6657 7860
| 1 2 3 44 83 98 .04 | 0 4258
cod 233| -3 0 -2 17 1 23 -.09 18 16 | --- --- --- ---
| 1 1 1 30 41 42 .03 | --- ---
esx 121| -1 -1 2 -28 -7 -27 .38 28 26 | 97694 -3234 6794 13452
| 1 2 4 39 34 58 .06 | 26417 6306
iac n/a| 2 0 8 -6 6 -123 -.05 26 26 | 217399 93 6919 14334
| 2 2 5 27 39 33 .05 | 27227 3879
mcc n/a| 1 0 65 -13 34 82 -.26 108 108 | --- --- --- ---
| 14 13 12 103 62 445 .48 | --- ---
Table 1.1528.b GPS week : 1528 MJD: 54940.0-54946.0
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 | 9 12 19 15 10 12 10 |
R03 | 13 12 14 19 15 13 12 |
R04 | 10 13 9 19 16 15 18 |
R06 | 18 17 21 19 20 19 30 |
R07 | 9 11 13 43 --- 0 0 |
R08 | 13 14 14 15 10 13 16 |
R10 | 16 18 25 14 16 14 8 |
R11 | 13 11 16 13 14 13 13 |
R13 | 14 12 12 13 12 11 12 |
R14 | 10 11 20 13 14 16 15 |
R15 | 14 11 10 10 12 13 10 |
R17 | 17 13 9 14 13 14 13 |
R18 | 14 15 13 11 9 8 12 |
R19 | 12 13 12 14 11 13 8 |
R20 | 10 15 12 12 15 14 12 |
R21 | 11 8 12 12 10 10 13 |
R22 | 19 11 10 12 12 15 15 |
R23 | 18 19 22 19 14 15 13 |
R24 | 65 78 41 34 16 17 14 |
Table 1.1528.c GPS week : 1528 MJD: 54940.0-54946.0
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 1528 0 | 19 42 197 23 498 -14770 91.0 2198 2198 | 221767 0
brd 1528 1 | -118 -5523 -605 65269 -1108 -16280 84.6 >>>>> >>>>> | 223395 0
brd 1528 2 | 26 41 292 -359 -567 -15000 88.5 3364 3364 | 227669 0
brd 1528 3 | -49 92 391 -1853 2535 -13360 85.9 5119 5119 | 227502 0
brd 1528 4 | 64 -71 430 -1561 1476 -11920 84.2 8630 8630 | 151816 0
brd 1528 5 | 5 47 305 -931 3633 -9605 88.4 5620 5620 | 227677 0
brd 1528 6 | -34 -58 228 -1227 2310 -12660 86.9 5064 5064 | 233678 0
-------------+------------------------------------------------------------+----------------
brd 1528 mean| -12 -775 177 8480 1253 -13370 87.1 >>>>> >>>>> | 216214 0
brd 1528 sdev| 60 2094 354 25050 1728 2231 2.4 >>>>> >>>>> | 28648 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 2.1528.0 GPS week: 1528 Day: 0 MJD: 54940
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 88| 6 3 -4 6 29 5 -.23 31 29 | 0 521 4619 5164
cod 233| -5 0 -4 30 -38 82 -.07 15 14 | --- --- --- ---
esx 121| -1 -3 1 -21 34 -26 .32 27 25 | 113449 -4130 6111 12650
iac n/a| 4 0 12 -17 36 -147 .02 25 25 | 221505 772 6117 13293
mcc n/a| 13 14 60 66 -44 750 .26 83 83 | --- --- --- ---
Table 2.1528.1 GPS week: 1528 Day: 1 MJD: 54941
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 88| 2 -2 -6 43 -7 223 -.18 27 25 | 0 1035 4178 4506
cod 233| -3 0 -4 -21 -9 23 -.07 16 15 | --- --- --- ---
esx 121| -1 2 5 25 -32 -41 .38 27 26 | 117443 -15203 6090 8684
iac n/a| 4 -2 9 -11 12 -164 -.02 23 23 | 225450 -3966 6087 9268
mcc n/a| -7 10 38 -88 -16 -398 .06 123 123 | --- --- --- ---
Table 2.1528.2 GPS week: 1528 Day: 2 MJD: 54942
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 88| 1 0 -5 84 -194 239 -.16 25 26 | 0 -2539 5581 6069
cod 233| -2 1 -1 -12 66 -59 -.12 25 20 | --- --- --- ---
esx 121| -2 -1 6 -48 38 -50 .33 27 23 | 106676 2452 5788 10485
iac n/a| 0 0 4 -22 70 -111 -.07 27 27 | 223738 5180 7293 11166
mcc n/a| 0 9 68 -181 -16 -186 -.30 100 100 | --- --- --- ---
Table 2.1528.3 GPS week: 1528 Day: 3 MJD: 54943
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 88| 0 -4 -6 -29 -46 147 -.11 26 25 | 0 2870 5052 5620
cod 233| -3 2 0 54 43 17 -.11 19 16 | --- --- --- ---
esx 121| 0 0 6 -20 -26 -9 .31 28 25 | 96494 2999 6248 11364
iac n/a| 1 -1 5 -23 6 -146 -.09 28 28 | 228028 1639 5709 11964
mcc n/a| -21 -4 70 -64 112 173 .23 93 93 | --- --- --- ---
Table 2.1528.4 GPS week: 1528 Day: 4 MJD: 54944
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 88| 3 0 -3 -21 -19 47 -.12 24 23 | 0 542 4234 4823
cod 233| -4 -1 0 47 9 31 -.13 16 14 | --- --- --- ---
esx 121| 0 0 -4 -7 -10 42 .46 29 27 | 39734 -1168 7052 21323
iac n/a| 5 3 15 -32 -35 -120 -.11 25 25 | 156510 2308 7021 23081
mcc n/a| -2 -12 68 88 77 526 -.36 108 108 | --- --- --- ---
Table 2.1528.5 GPS week: 1528 Day: 5 MJD: 54945
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 88| 0 0 -3 42 29 44 -.16 20 20 | 0 -9910 17421 22674
cod 233| -1 1 -3 -4 -10 33 -.06 16 14 | --- --- --- ---
esx 121| 1 -2 4 -102 -54 -135 .40 31 30 | 105147 -6837 9545 18916
iac n/a| 2 0 9 39 -8 -65 -.02 31 31 | 232529 -6194 9473 19631
mcc n/a| 19 -21 69 94 97 113 -1.02 106 106 | --- --- --- ---
Table 2.1528.6 GPS week: 1528 Day: 6 MJD: 54946
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 88| 2 1 3 -32 57 20 -.13 22 21 | 0 799 5518 6170
cod 233| -2 -1 -1 29 -49 36 -.08 21 19 | --- --- --- ---
esx 121| -4 -5 -2 -28 -3 26 .44 29 24 | 104916 -755 6728 10746
iac n/a| 0 5 0 24 -39 -108 -.09 25 25 | 234038 916 6734 11938
mcc n/a| 10 0 77 -13 29 -401 -.70 142 142 | --- --- --- ---
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 3.1528.0 GPS week: 1528 Day: 0 MJD: 54940
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2186 19 9 23 15 --- 9 | 22 32 48 30 --- 30
R03 | 1802 27 17 30 19 --- 13 | 28 35 36 26 --- 28
R04 | 2115 21 14 15 18 --- 9 | 40 39 29 35 --- 33
R06 | 4406 39 15 42 34 --- 18 | 189 189 179 195 --- 187
R07 | 1983 15 10 18 17 --- 8 | 19 9999 18 12 --- 9999
R08 | 1250 24 23 20 20 74 13 | 38 38 23 27 34 30
R10 | 1699 42 11 39 20 --- 16 | 30 31 55 40 --- 31
R11 | 1040 35 10 20 25 57 13 | 38 24 32 22 53 22
R13 | 1328 43 9 29 16 --- 14 | 92 71 67 70 --- 72
R14 | 1252 19 13 23 18 --- 10 | 37 41 49 42 --- 38
R15 | 2076 30 16 25 25 109 13 | 40 43 41 41 106 38
R17 | 799 35 22 20 41 --- 17 | 60 56 70 71 --- 60
R18 | 1568 34 16 27 25 --- 14 | 35 39 53 34 --- 35
R19 | 2365 20 14 15 32 --- 12 | 43 42 39 45 --- 40
R20 | 3535 20 16 13 15 --- 9 | 20 31 23 17 --- 20
R21 | 2835 21 12 27 13 --- 10 | 18 25 34 24 --- 21
R22 | 1746 37 17 40 37 --- 18 | 28 42 50 27 --- 32
R23 | 2382 49 15 29 34 --- 18 | 55 50 69 74 --- 56
XR24 | 9488 --- 50 --- 83 --- 64 | --- 247 --- 189 --- 218
------+------------------------------------+--------------------------------
RMS | 2198 31 15 27 25 83 |T 46 59 50 53 64 55
WRMS | 2198 29 14 25 25 83 |NE 46 59 50 53 64 55
MEDI | 1983 27 15 23 20 74 |MD 37 39 41 35 53 33
Table 3.1528.1 GPS week: 1528 Day: 1 MJD: 54941
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 20 12 31 22 --- 12 | 25 34 58 32 --- 33
R03 |>>>>> 15 15 21 27 --- 11 | 27 37 33 27 --- 26
R04 |>>>>> 32 15 28 19 --- 13 | 48 28 34 30 --- 30
R06 |>>>>> 45 20 35 15 --- 17 | 160 178 202 190 --- 181
R07 |>>>>> 25 10 13 26 --- 11 | 15 9999 15 19 --- 9999
R08 |>>>>> 19 22 34 15 72 13 | 42 43 46 36 37 39
R10 | 8857 51 25 29 19 --- 18 | 34 34 41 34 --- 30
R11 |>>>>> 20 12 30 14 71 11 | 24 23 33 26 61 19
R13 |>>>>> 29 11 28 18 --- 12 | 35 42 42 41 --- 38
R14 |>>>>> 19 16 20 22 --- 11 | 35 59 38 47 --- 42
R15 |>>>>> 16 13 19 26 187 11 | 39 35 40 47 115 37
R17 |>>>>> 20 13 23 30 --- 12 | 48 46 43 60 --- 46
R18 |>>>>> 17 23 34 26 --- 15 | 17 35 35 27 --- 21
R19 |>>>>> 26 9 31 25 --- 13 | 38 52 63 53 --- 49
R20 |>>>>> 22 21 31 28 --- 14 | 18 19 34 27 --- 17
R21 |>>>>> 17 10 15 12 --- 7 | 17 25 25 19 --- 19
R22 |>>>>> 20 14 22 22 --- 11 | 19 45 41 48 --- 33
R23 |>>>>> 36 20 33 41 --- 18 | 49 63 66 67 --- 57
XR24 |13622 --- 65 --- 93 --- 78 | --- 232 --- 195 --- 203
------+------------------------------------+--------------------------------
RMS |>>>>> 27 16 27 23 123 |T 38 57 49 53 71 51
WRMS |>>>>> 25 15 26 23 123 |NE 38 57 49 53 71 51
MEDI |>>>>> 20 15 28 22 72 |MD 34 37 40 36 61 33
Table 3.1528.2 GPS week: 1528 Day: 2 MJD: 54942
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 744 28 17 38 42 --- 18 | 26 29 61 30 --- 29
R03 | 4612 21 25 28 24 --- 14 | 33 47 25 35 --- 30
R04 | 1687 14 12 14 17 --- 8 | 35 28 38 32 --- 29
R06 | 9926 30 34 32 44 --- 20 | 128 120 138 148 --- 131
R07 | 869 10 24 16 31 --- 12 | 21 9999 20 20 --- 9999
R08 | 2174 25 22 25 23 78 13 | 38 36 40 41 27 33
R10 | 1442 58 50 24 30 --- 25 | 34 41 40 33 --- 27
R11 | 961 34 28 22 27 73 16 | 30 23 40 29 39 24
R13 | 666 23 14 21 22 --- 11 | 59 32 41 42 --- 39
R14 | 1219 19 44 46 20 --- 20 | 37 58 43 41 --- 36
R15 | 1247 9 10 18 27 136 10 | 35 32 43 36 66 33
R17 | 1664 18 12 14 14 --- 8 | 56 58 58 63 --- 55
R18 | 1061 18 23 28 21 --- 13 | 24 36 38 41 --- 29
R19 | 924 25 14 18 22 --- 11 | 38 34 29 47 --- 32
R20 | 1823 21 16 25 17 --- 11 | 21 32 50 36 --- 29
R21 | 1657 24 12 20 25 --- 12 | 18 25 45 41 --- 27
R22 | 1549 17 12 17 17 --- 9 | 24 24 32 28 --- 23
R23 | 7433 22 37 44 44 --- 21 | 56 47 84 61 --- 56
XR24 |15691 --- 39 --- 41 --- 40 | --- 134 --- 98 --- 117
------+------------------------------------+--------------------------------
RMS | 3363 25 25 27 27 100 |T 39 46 48 47 44 43
WRMS | 3363 26 20 23 27 100 |NE 39 46 48 47 44 43
MEDI | 1549 21 22 22 24 78 |MD 34 34 40 41 39 30
Table 3.1528.3 GPS week: 1528 Day: 3 MJD: 54943
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 761 27 14 39 18 --- 14 | 28 31 64 26 --- 32
R03 | 5214 31 8 28 56 --- 19 | 32 40 47 60 --- 39
R04 | 5365 34 22 49 18 --- 18 | 48 44 34 36 --- 32
R06 |17806 25 35 24 38 --- 18 | 171 168 158 173 --- 165
XR07 |15893 416 17 --- 65 --- 43 | 21 9999 --- 18 --- 9999
R08 | 2267 31 19 29 25 81 15 | 45 43 62 35 29 42
R10 | 1280 22 17 31 30 --- 14 | 43 36 57 53 --- 41
R11 | 1200 28 17 20 23 74 12 | 27 22 28 31 41 19
R13 | 1168 23 16 27 21 --- 12 | 28 29 36 38 --- 26
R14 | 2599 16 20 27 22 --- 12 | 44 43 60 54 --- 45
R15 | 923 9 12 25 21 119 10 | 33 35 36 41 54 32
R17 | 2436 21 16 31 28 --- 14 | 60 55 61 59 --- 56
R18 | 953 27 13 24 11 --- 11 | 22 34 52 35 --- 31
R19 | 694 25 21 24 25 --- 13 | 32 52 34 43 --- 38
R20 | 2977 23 16 20 21 --- 11 | 29 31 27 30 --- 24
R21 | 815 21 13 30 20 --- 12 | 37 33 56 30 --- 35
R22 | 935 26 12 13 29 --- 12 | 19 28 31 53 --- 29
R23 | 6070 36 34 22 38 --- 19 | 50 66 68 51 --- 50
XR24 |27109 --- 29 63 51 --- 33 | --- 56 55 52 --- 44
------+------------------------------------+--------------------------------
RMS | 5118 26 19 28 28 93 |T 42 47 53 48 41 43
WRMS | 5118 25 16 25 28 93 |NE 42 47 53 48 41 43
MEDI | 2267 25 17 27 25 81 |MD 32 36 52 41 41 35
Table 3.1528.4 GPS week: 1528 Day: 4 MJD: 54944
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 653 14 10 22 24 --- 10 | 16 23 43 32 --- 23
R03 | 3906 17 9 38 34 --- 14 | 20 25 42 27 --- 21
R04 | 893 29 10 24 43 --- 16 | 39 44 53 61 --- 46
R06 |18748 43 31 34 27 --- 19 | 106 132 142 126 --- 123
R08 | 1561 21 14 13 22 112 10 | 47 44 44 37 28 42
R10 | 1502 16 19 42 27 --- 15 | 40 29 46 46 --- 31
R11 | 790 34 12 26 21 48 13 | 24 31 47 43 35 32
R13 | 2252 22 17 23 17 --- 11 | 38 34 45 34 --- 33
R14 | 2697 20 19 36 24 --- 14 | 23 35 54 47 --- 28
R15 | 1099 20 12 23 25 141 11 | 27 23 31 41 37 24
R17 | 2996 15 21 23 30 --- 13 | 39 42 50 43 --- 39
R18 | 1695 16 9 20 14 --- 8 | 22 25 31 36 --- 24
R19 | 908 26 7 19 21 --- 10 | 37 49 58 62 --- 49
R20 | 2491 30 17 38 19 --- 15 | 23 43 54 31 --- 33
R21 | 1043 18 15 19 19 --- 10 | 14 33 29 32 --- 21
R22 | 680 22 7 34 13 --- 11 | 25 25 49 29 --- 24
R23 | 3591 12 24 33 25 --- 14 | 46 69 43 53 --- 53
R24 |30336 32 19 31 27 --- 15 | 10 57 68 61 --- 57
------+------------------------------------+--------------------------------
RMS | 8629 24 16 29 25 108 |T 33 42 51 46 33 39
WRMS | 8629 23 14 27 25 108 |NE 33 42 51 46 33 39
MEDI | 1561 20 14 24 24 112 |MD 25 34 46 41 35 32
Table 3.1528.5 GPS week: 1528 Day: 5 MJD: 54945
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 648 17 11 28 28 --- 11 | 18 31 55 32 --- 27
R03 | 6997 14 10 36 31 --- 12 | 27 34 34 44 --- 27
R04 | 1743 22 11 39 35 --- 15 | 26 24 30 46 --- 26
R06 |16363 31 18 52 31 --- 18 | 117 96 80 107 --- 100
XR07 | ---- --- 3 --- --- --- 0 | --- 9999 --- --- --- 9999
R08 | 1306 32 8 26 22 137 13 | 25 15 29 25 18 16
R10 | 2900 13 22 29 28 --- 13 | 50 48 36 44 --- 41
R11 | 515 23 14 31 19 43 12 | 22 35 45 27 25 27
R13 | 2623 18 11 19 26 --- 10 | 27 28 35 25 --- 24
R14 | 2013 28 16 31 41 --- 16 | 43 60 59 79 --- 53
R15 | 1070 16 15 21 36 113 12 | 19 37 41 27 36 27
R17 | 3753 17 19 33 27 --- 13 | 43 37 50 37 --- 36
R18 | 1823 13 9 17 17 --- 7 | 16 17 28 31 --- 18
R19 | 641 17 19 29 23 --- 12 | 34 46 37 57 --- 39
R20 | 1661 24 15 25 33 --- 13 | 18 29 37 26 --- 23
R21 | 838 10 16 22 21 --- 9 | 48 48 42 50 --- 44
R22 | 771 15 20 36 37 --- 15 | 16 31 28 39 --- 21
R23 | 2998 21 20 35 34 --- 15 | 34 52 72 34 --- 44
R24 |13965 21 18 31 50 --- 16 | 8 65 76 63 --- 64
------+------------------------------------+--------------------------------
RMS | 5620 20 16 31 31 105 |T 32 40 45 44 26 36
WRMS | 5620 20 14 30 31 105 |NE 32 40 45 44 26 36
MEDI | 1743 17 15 29 28 113 |MD 26 35 37 37 25 27
Table 3.1528.6 GPS week: 1528 Day: 6 MJD: 54946
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 823 11 14 16 27 --- 10 | 26 26 27 35 --- 26
R03 | 4700 20 16 27 18 --- 12 | 25 39 52 26 --- 29
R04 | 2479 25 22 43 31 --- 17 | 37 46 32 35 --- 31
R06 |13674 46 37 66 53 --- 29 | 79 78 71 89 --- 73
XR07 | ---- --- 4 --- --- --- 0 | --- 9999 --- --- --- 9999
R08 | 599 32 22 20 29 180 15 | 27 18 28 29 25 18
R10 | 3064 12 12 16 17 --- 8 | 39 33 35 44 --- 34
R11 | 548 11 15 28 29 125 12 | 25 29 32 29 31 24
R13 | 1971 21 8 27 19 --- 11 | 28 25 39 28 --- 25
R14 | 1346 32 30 20 13 --- 15 | 27 54 55 49 --- 42
R15 | 916 6 20 14 25 110 10 | 24 27 31 36 40 25
R17 | 3782 18 30 20 16 --- 12 | 62 45 58 47 --- 50
R18 | 2199 20 19 25 16 --- 11 | 43 32 46 43 --- 37
R19 | 673 12 16 9 16 --- 8 | 33 40 33 45 --- 35
R20 | 910 20 19 20 24 --- 12 | 16 30 25 19 --- 18
R21 | 757 17 20 31 19 --- 12 | 36 35 63 47 --- 42
R22 | 1401 17 23 34 24 --- 14 | 41 40 47 28 --- 33
R23 | 1484 24 19 25 20 --- 13 | 57 48 44 43 --- 44
R24 |14281 20 21 28 26 --- 13 | 9 72 39 74 --- 57
------+------------------------------------+--------------------------------
RMS | 5064 22 21 29 25 142 |T 35 39 42 41 32 35
WRMS | 5064 21 19 24 25 142 |NE 35 39 42 41 32 35
MEDI | 1401 20 19 25 20 125 |MD 28 35 39 36 31 33
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