[IGSREPORT-17089] Wk 1515 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Feb 5 06:16:08 PST 2009
******************************************************************************
IGS Electronic Report 05 Feb 06:16:16 PST 2009 Message Number 17089
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1515 (Jan 18, 2009 - Jan 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 2.1515.
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:
igl1515[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1515 in the SP3 format.
igl15157.sum Combination Report for GPS Week 1515.
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 | 278.7 ns
1 | 270.3 ns
2 | 269.3 ns
3 | 270.2 ns
4 | 278.0 ns
5 | 164.3 ns
6 | 275.9 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
----+--------+---------------
0 | ESX | R03
1 | ESX | R03
2 | ESX | R03
3 | ESX | R03
4 | ESX | R03
5 | ESX | R03
6 | ESX | R03
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 1.1515, 1a.1515).
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 2.1515.0-6)
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 3.1515.0-6).
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 1515 summary. (Jan 18, 2009 - Jan 24, 2009)
Table 1.1515.a GPS week : 1515 MJD: 54849.0-54855.0
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 89| 0 0 5 4 30 -106 -.08 21 20 | 0 287 2436 2559
| 1 1 2 30 29 139 .02 | 0 563
cod 237| -1 1 -3 20 -8 75 -.08 15 14 | --- --- --- ---
| 1 1 3 19 26 47 .02 | --- ---
esx 134| 0 1 -2 -53 -21 -20 .44 95 45 | 88583 -1907 5978 11475
| 2 2 4 61 35 108 .07 | 42197 3102
iac n/a| 0 -2 1 -18 -5 -6 -.04 24 24 | 259149 -1058 5979 11504
| 1 1 5 23 12 61 .04 | 40453 2125
mcc n/a| 8 -33 15 -117 -2 2229 .63 477 477 | --- --- --- ---
| 22 40 25 329 214 2344 1.18 | --- ---
Table 1.1515.b GPS week : 1515 MJD: 54849.0-54855.0
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 | 40 20 15 9 8 11 10 |
R03 | 16 13 14 13 12 12 13 |
R04 | 14 11 13 14 14 16 17 |
R06 | 0 0 0 0 0 0 0 |
R07 | 10 11 14 9 9 14 10 |
R10 | 13 12 8 10 22 10 11 |
R11 | 11 16 9 10 12 13 18 |
R13 | 10 13 13 8 13 9 12 |
R14 | 9 10 11 10 10 9 9 |
R15 | 17 11 12 9 10 16 11 |
R17 | 17 17 10 9 13 14 15 |
R18 | 12 12 11 7 11 9 10 |
R19 | 11 12 10 12 12 9 11 |
R20 | 13 15 14 12 26 20 16 |
R21 | 10 12 15 14 10 15 10 |
R22 | 11 15 11 10 17 16 11 |
R23 | 15 21 15 20 21 16 25 |
R24 | 18 13 22 0 0 33 33 |
Table 1.1515.c GPS week : 1515 MJD: 54849.0-54855.0
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 1515 0 | 40 75 -89 -614 -1941 -12530 91.2 3982 3982 | 278675 0
brd 1515 1 | -53 -36 -4 -3411 -2070 -10360 91.8 3556 3556 | 270271 0
brd 1515 2 | 128 105 59 -1818 -919 -9276 89.3 2931 2931 | 269319 0
brd 1515 3 | 18 36 64 -1897 -420 -9561 90.4 2837 2837 | 270238 0
brd 1515 4 | 76 47 157 -145 2865 -6183 90.7 2349 2349 | 277988 0
brd 1515 5 | -73 62 283 -1756 1656 -11600 89.9 2527 2527 | 164288 0
brd 1515 6 | 126 -93 356 0 457 -18600 91.1 2636 2636 | 275935 0
-------------+------------------------------------------------------------+----------------
brd 1515 mean| 37 28 118 -1377 -53 -11158 90.6 2974 2974 | 258102 0
brd 1515 sdev| 80 69 158 1206 1835 3850 .8 588 588 | 41551 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 2.1515.0 GPS week: 1515 Day: 0 MJD: 54849
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 89| 2 0 5 38 11 -177 -.11 21 22 | 0 732 3018 3275
cod 237| -3 2 -7 -6 19 92 -.07 15 15 | --- --- --- ---
esx 134| 0 0 5 -121 -25 124 .35 90 45 | 105990 -4446 9372 12769
iac n/a| 1 -2 3 19 -10 -44 .00 23 23 | 280393 -1868 9412 12971
mcc n/a| 2 4 4 81 -180 -68 1.08 141 141 | --- --- --- ---
Table 2.1515.1 GPS week: 1515 Day: 1 MJD: 54850
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 89| 0 -2 5 30 3 137 -.07 21 22 | 0 1384 3927 4201
cod 237| -1 2 -6 37 -5 -21 -.10 15 15 | --- --- --- ---
esx 134| 3 0 -4 -102 47 -168 .54 97 38 | 92604 1085 7399 17417
iac n/a| -2 0 7 -24 -12 -45 -.03 27 27 | 273418 -1387 7427 18208
mcc n/a| -3 -25 -12 -13 54 322 1.66 133 133 | --- --- --- ---
Table 2.1515.2 GPS week: 1515 Day: 2 MJD: 54851
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 89| 3 -2 9 -17 -8 -107 -.06 21 20 | 0 11 2029 2076
cod 237| -2 2 -5 10 20 85 -.11 14 13 | --- --- --- ---
esx 134| 2 0 0 -24 -5 -43 .50 106 44 | 103973 1921 4491 9837
iac n/a| 1 -3 0 -31 -18 17 -.10 22 22 | 269882 -1387 4421 8906
mcc n/a| 6 -4 17 -57 35 1085 .87 108 108 | --- --- --- ---
Table 2.1515.3 GPS week: 1515 Day: 3 MJD: 54852
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 89| 0 1 2 -47 60 -128 -.09 16 15 | 0 51 1946 2009
cod 237| 0 0 -4 51 -37 97 -.10 13 11 | --- --- --- ---
esx 134| 0 0 0 36 -68 82 .42 96 40 | 108681 -6199 5020 9964
iac n/a| -1 0 5 -49 12 -95 -.03 23 23 | 271428 -566 5007 10321
mcc n/a| 30 -22 20 -71 -13 1319 .50 105 105 | --- --- --- ---
Table 2.1515.4 GPS week: 1515 Day: 4 MJD: 54853
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 89| -1 -1 3 19 53 -114 -.09 18 18 | 0 -173 1876 1939
cod 237| 0 1 -4 18 -42 87 -.05 19 17 | --- --- --- ---
esx 134| -2 5 -5 -57 -27 53 .36 96 43 | 98765 -1738 5202 9230
iac n/a| 1 -2 7 -1 -1 -14 -.04 26 26 | 276467 449 5195 9677
mcc n/a| -28 -95 11 256 -225 6702 -1.92 736 736 | --- --- --- ---
Table 2.1515.5 GPS week: 1515 Day: 5 MJD: 54854
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 89| 1 1 10 -10 64 -33 -.08 23 22 | 0 8 1998 2108
cod 237| 0 1 1 10 -26 56 -.08 15 13 | --- --- --- ---
esx 134| -4 3 -9 6 -34 -98 .41 88 42 | -5665 -4137 5914 9988
iac n/a| -1 -2 -4 -4 11 78 -.02 24 24 | 167740 -4757 5910 9732
mcc n/a| 38 -85 3 -781 419 3517 .85 1066 1066 | --- --- --- ---
Table 2.1515.6 GPS week: 1515 Day: 6 MJD: 54855
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 89| 0 0 4 22 30 -323 -.06 26 23 | 0 0 2262 2307
cod 237| -1 0 1 24 12 129 -.08 15 12 | --- --- --- ---
esx 134| 1 3 -2 -108 -32 -95 .49 90 63 | 115737 159 4452 11121
iac n/a| 2 -4 -5 -35 -16 56 -.08 23 23 | 274720 2109 4486 10716
mcc n/a| 15 -6 67 -234 -107 2732 1.37 1049 1049 | --- --- --- ---
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 3.1515.0 GPS week: 1515 Day: 0 MJD: 54849
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 6843 84 42 --- 37 --- 40 | 71 36 --- 44 --- 41
R03 | 9869 21 16 332 29 --- 15 | 31 42 269 49 --- 39
R04 | 6561 21 15 40 27 --- 14 | 93 97 106 84 --- 92
XR06 | ---- --- --- --- --- --- 0 | 68 9999 --- --- --- 0
R07 | 3674 22 14 19 16 --- 10 | 23 33 33 38 --- 29
R10 | 1222 11 19 47 14 --- 13 | 25 24 38 27 --- 24
R11 | 3677 17 11 26 25 164 10 | 23 30 41 39 46 27
R13 | 2885 21 12 25 16 --- 10 | 18 42 49 28 --- 31
R14 | 1290 14 8 35 9 --- 9 | 19 29 42 26 --- 25
R15 | 2496 20 13 55 33 113 16 | 23 28 46 29 215 25
R17 | 2040 29 17 58 22 --- 17 | 38 49 52 47 --- 43
R18 | 635 14 18 26 26 --- 12 | 34 24 37 48 --- 32
R19 | 1937 13 17 28 19 --- 10 | 44 52 35 42 --- 43
R20 | 1344 22 13 33 27 --- 13 | 31 46 52 47 --- 42
R21 | 1513 12 13 26 18 --- 9 | 45 51 65 53 --- 50
R22 | 951 14 12 32 19 --- 10 | 57 62 65 62 --- 59
R23 | 1297 27 12 28 35 --- 14 | 49 61 68 52 --- 55
R24 | 7310 41 18 52 18 --- 18 | 26 9999 57 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 3981 21 15 90 23 141 |T 39 44 65 44 130 41
WRMS | 3981 22 15 45 23 141 |NE 39 44 65 44 130 41
MEDI | 2040 21 14 32 22 113 |MD 31 42 49 44 46 39
Table 3.1515.1 GPS week: 1515 Day: 1 MJD: 54850
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 5491 32 24 --- 28 --- 19 | 38 33 --- 33 --- 28
R03 | 7603 17 13 365 24 --- 12 | 33 28 196 37 --- 29
R04 | 5768 20 11 25 20 --- 10 | 49 59 59 57 --- 54
XR06 | ---- --- --- --- --- --- 0 | 58 9999 --- --- --- 0
R07 | 2447 20 9 26 23 --- 11 | 21 22 39 27 --- 20
R10 | 1868 14 14 38 20 --- 12 | 21 28 42 21 --- 21
R11 | 1718 25 14 58 19 158 16 | 23 24 85 33 43 30
R13 | 2753 24 13 35 22 --- 13 | 25 22 47 21 --- 20
R14 | 2903 15 9 26 24 --- 10 | 21 22 40 19 --- 19
R15 | 3536 13 13 33 21 101 11 | 31 17 40 23 221 19
R17 | 1890 34 15 47 23 --- 16 | 29 37 57 33 --- 33
R18 | 795 15 14 27 26 --- 11 | 24 28 35 41 --- 24
R19 | 1648 15 11 38 19 --- 11 | 33 37 21 39 --- 30
R20 | 1651 20 20 27 39 --- 15 | 29 39 42 40 --- 33
R21 | 1390 20 13 35 21 --- 12 | 36 53 80 49 --- 49
R22 | 683 20 19 43 25 --- 14 | 61 50 61 46 --- 47
R23 | 923 30 23 33 57 --- 21 | 23 41 31 29 --- 26
R24 | 7571 24 15 30 26 --- 13 | 27 9999 52 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 3555 21 15 97 27 133 |T 32 33 57 34 132 30
WRMS | 3555 22 15 38 27 133 |NE 32 33 57 34 132 30
MEDI | 1890 20 14 33 23 101 |MD 29 28 42 33 43 28
Table 3.1515.2 GPS week: 1515 Day: 2 MJD: 54851
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 4897 25 16 --- 24 --- 15 | 30 35 --- 37 --- 31
R03 | 7590 19 14 397 25 --- 13 | 27 32 237 34 --- 28
R04 | 1759 20 17 29 25 --- 12 | 67 71 78 78 --- 70
XR06 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R07 | 1655 27 13 32 24 --- 13 | 26 31 39 39 --- 28
R10 | 2598 16 8 15 17 --- 8 | 23 27 31 27 --- 24
R11 | 918 15 10 22 13 124 8 | 28 26 44 29 40 27
R13 | 1835 18 11 42 22 --- 13 | 24 27 51 28 --- 26
R14 | 5471 15 10 27 22 --- 10 | 23 22 42 25 --- 23
R15 | 3516 21 10 37 16 88 12 | 37 28 47 26 125 26
R17 | 1257 22 11 18 19 --- 10 | 29 44 43 48 --- 38
R18 | 1713 18 15 23 18 --- 10 | 31 34 37 24 --- 26
R19 | 1008 20 12 25 15 --- 10 | 50 42 49 40 --- 41
R20 | 1639 24 13 42 23 --- 14 | 31 34 39 27 --- 23
R21 | 1635 21 28 32 25 --- 15 | 42 49 66 48 --- 45
R22 | 709 18 16 29 17 --- 11 | 34 42 46 40 --- 36
R23 | 882 29 15 28 33 --- 15 | 49 49 66 51 --- 47
XR24 | 7366 --- 9 --- 33 --- 21 | --- 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 2931 21 14 106 22 108 |T 34 37 61 37 82 33
WRMS | 2931 20 13 44 22 108 |NE 34 37 61 37 82 33
MEDI | 1713 20 12 29 22 88 |MD 30 34 46 34 40 28
Table 3.1515.3 GPS week: 1515 Day: 3 MJD: 54852
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 4479 12 11 19 19 --- 8 | 49 38 16 38 --- 37
R03 | 6596 17 16 365 20 --- 12 | 34 43 210 37 --- 35
R04 | 2001 20 14 41 29 --- 14 | 35 33 51 47 --- 33
XR06 | ---- --- 7 --- --- --- 0 | --- 9999 --- --- --- 9999
R07 | 1445 12 10 21 20 --- 8 | 24 33 38 34 --- 28
R10 | 3117 16 14 22 20 --- 10 | 25 36 32 25 --- 26
R11 | 847 14 13 33 11 130 10 | 29 27 48 25 101 26
R13 | 1070 12 10 19 19 --- 8 | 23 24 29 29 --- 22
R14 | 5719 15 12 23 23 --- 10 | 30 22 38 27 --- 22
R15 | 2093 15 10 17 21 71 8 | 26 27 42 30 461 27
R17 | 652 17 5 17 23 --- 9 | 48 54 47 61 --- 52
R18 | 1685 12 6 21 10 --- 6 | 27 22 24 20 --- 20
R19 | 743 18 11 44 14 --- 12 | 35 38 64 37 --- 37
R20 | 1022 18 9 26 32 --- 11 | 19 27 28 22 --- 19
R21 | 1772 11 13 49 25 --- 13 | 28 32 58 37 --- 26
R22 | 660 9 15 21 26 --- 10 | 33 43 41 30 --- 34
R23 | 1417 24 23 63 40 --- 20 | 39 43 84 43 --- 40
XR24 |>>>>> --- 7 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 2837 16 13 96 23 105 |T 31 33 53 33 281 30
WRMS | 2837 15 11 40 23 105 |NE 31 33 53 33 281 30
MEDI | 1685 15 11 22 20 71 |MD 29 33 41 30 101 27
Table 3.1515.4 GPS week: 1515 Day: 4 MJD: 54853
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2821 12 9 17 18 --- 8 | 37 27 25 38 --- 30
R03 | 4174 17 17 351 17 --- 12 | 30 36 189 48 --- 35
R04 | 2100 21 23 22 25 --- 13 | 53 56 59 54 --- 50
XR06 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R07 | 1742 14 12 24 14 --- 9 | 25 26 38 31 --- 26
R10 | 2870 31 17 76 22 --- 21 | 20 35 91 23 --- 30
R11 | 945 11 16 34 25 231 12 | 21 22 37 34 75 21
R13 | 1146 19 11 22 33 --- 12 | 18 28 29 41 --- 24
R14 | 5682 13 16 28 15 --- 10 | 13 23 34 25 --- 17
R15 | 1904 12 14 24 16 1015 9 | 30 25 30 23 431 19
R17 | 937 19 12 33 29 --- 13 | 48 46 71 48 --- 49
R18 | 1312 16 9 30 19 --- 10 | 24 20 31 33 --- 22
R19 | 718 22 7 28 21 --- 11 | 50 37 49 33 --- 39
R20 | 966 28 33 78 42 --- 25 | 16 31 94 25 --- 26
R21 | 840 11 21 22 14 --- 10 | 31 45 47 31 --- 36
R22 | 949 20 31 42 27 --- 17 | 26 36 53 31 --- 23
R23 | 1853 16 30 50 51 --- 21 | 36 37 89 45 --- 42
XR24 |>>>>> --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 2349 18 19 96 26 736 |T 29 33 60 35 253 30
WRMS | 2349 18 17 43 26 736 |NE 29 33 60 35 253 30
MEDI | 1742 16 14 28 21 231 |MD 26 31 47 33 75 26
Table 3.1515.5 GPS week: 1515 Day: 5 MJD: 54854
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1544 21 10 24 23 --- 11 | 41 28 29 33 --- 28
R03 | 2905 15 13 327 23 --- 12 | 33 38 134 47 --- 37
R04 | 1586 31 16 48 21 --- 16 | 22 31 66 27 --- 29
XR06 | ---- --- 3 --- --- --- 0 | --- 558 --- --- --- 9999
R07 | 3806 20 20 35 23 --- 13 | 30 36 48 39 --- 31
R10 | 3939 13 9 26 22 --- 9 | 22 31 44 31 --- 27
R11 | 2082 20 17 40 16 171 13 | 19 24 45 30 58 23
R13 | 1022 15 11 22 16 --- 9 | 25 22 25 42 --- 25
R14 | 5544 19 8 23 13 --- 9 | 19 27 34 19 --- 19
R15 | 1725 31 20 45 20 1497 16 | 16 28 48 23 197 20
R17 | 1319 30 11 29 25 --- 13 | 23 40 63 35 --- 36
R18 | 809 17 7 28 14 --- 9 | 15 21 47 20 --- 20
R19 | 1881 12 11 25 12 --- 8 | 36 41 39 43 --- 37
R20 | 1759 36 14 31 54 --- 20 | 43 38 55 25 --- 34
R21 | 1068 20 19 46 21 --- 14 | 29 27 61 23 --- 26
R22 | 1195 31 18 43 21 --- 15 | 34 30 51 22 --- 25
R23 | 2850 20 23 37 35 --- 16 | 35 25 42 34 --- 24
XR24 |>>>>> --- 23 --- 44 --- 33 | --- 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 2527 23 15 88 24 1065 |T 27 61 51 30 127 27
WRMS | 2527 22 13 42 24 1065 |NE 27 61 51 30 127 27
MEDI | 1759 20 13 31 21 171 |MD 25 30 47 30 58 26
Table 3.1515.6 GPS week: 1515 Day: 6 MJD: 54855
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1431 22 11 22 14 --- 9 | 42 41 24 45 --- 41
R03 | 2777 16 14 335 22 --- 12 | 29 41 226 39 --- 35
R04 | 1312 35 22 39 25 --- 16 | 44 28 31 40 --- 28
XR06 | ---- --- 7 --- --- --- 0 | --- 688 --- --- --- 9999
R07 | 3374 23 8 24 16 --- 9 | 22 30 35 38 --- 29
R10 | 4615 18 14 27 18 --- 10 | 20 33 31 22 --- 24
R11 | 2883 35 16 56 27 128 18 | 27 32 28 29 49 27
R13 | 981 17 10 43 14 --- 12 | 26 37 51 35 --- 34
R14 | 3262 19 11 23 14 --- 9 | 29 28 27 29 --- 26
R15 | 2714 19 13 28 18 1477 10 | 24 30 32 30 331 27
R17 | 2914 22 17 26 36 --- 14 | 34 39 53 52 --- 41
R18 | 1718 20 12 25 16 --- 10 | 25 31 44 37 --- 30
R19 | 1984 22 13 22 21 --- 11 | 49 55 51 56 --- 51
R20 | 3064 47 9 28 24 --- 15 | 44 42 41 40 --- 39
R21 | 1584 12 16 22 21 --- 10 | 43 39 49 42 --- 41
R22 | 1484 19 11 25 21 --- 10 | 43 43 45 27 --- 37
R23 | 3196 42 26 69 42 --- 24 | 60 72 111 74 --- 70
XR24 |>>>>> --- 24 --- 42 --- 32 | --- 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 2636 26 15 90 23 1048 |T 35 77 54 39 190 36
WRMS | 2636 23 12 63 23 1048 |NE 35 77 54 39 190 36
MEDI | 2777 20 13 26 21 128 |MD 29 39 41 38 49 34
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