[IGSREPORT-17419] Wk 1530 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu May 21 05:11:49 PDT 2009
******************************************************************************
IGS Electronic Report 21 May 05:12:12 PDT 2009 Message Number 17419
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1530 (May 03, 2009 - May 09, 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 2.1530.
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:
igl1530[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1530 in the SP3 format.
igl15307.sum Combination Report for GPS Week 1530.
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 | 148.5 ns
1 | 225.7 ns
2 | 224.6 ns
3 | 223.5 ns
4 | 159.1 ns
5 | 166.4 ns
6 | 150.2 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 1.1530, 1a.1530).
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 2.1530.0-6)
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 3.1530.0-6).
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 1530 summary. (May 03, 2009 - May 09, 2009)
Table 1.1530.a GPS week : 1530 MJD: 54954.0-54960.0
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| 2 0 -5 11 23 116 -.14 32 29 | 0 1071 4725 5279
| 1 2 4 23 38 204 .05 | 0 675
cod 237| -2 0 5 -2 -3 32 -.10 21 17 | --- --- --- ---
| 1 1 2 15 21 70 .04 | --- ---
esx 123| -2 0 11 -4 -39 27 .47 34 27 | 62624 -3956 7966 14121
| 1 1 6 46 44 88 .07 | 39393 5115
iac n/a| 2 0 -12 3 13 -205 -.12 33 33 | 187415 -2468 7983 14511
| 1 2 7 26 28 54 .06 | 35947 3775
mcc n/a| 6 10 91 142 48 -150 .50 170 170 | --- --- --- ---
| 11 14 25 219 104 605 .46 | --- ---
Table 1.1530.b GPS week : 1530 MJD: 54954.0-54960.0
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 | 8 12 10 11 12 8 11 |
R03 | 10 9 13 13 17 14 13 |
R04 | 2248 0 0 0 0 53 14 |
R06 | 17 19 25 22 27 17 28 |
R07 | 40 17 15 10 12 14 13 |
R08 | 12 12 20 11 14 12 19 |
R10 | 21 24 22 24 26 31 32 |
R11 | 13 17 21 22 18 18 18 |
R13 | 13 19 18 20 20 24 24 |
R14 | 16 19 23 25 21 23 28 |
R15 | 15 15 37 16 16 18 26 |
R17 | 11 12 16 18 21 16 14 |
R18 | 13 13 10 12 15 12 12 |
R19 | 15 10 13 11 14 12 13 |
R20 | 19 13 17 17 16 14 10 |
R21 | 14 21 14 11 15 13 14 |
R22 | 14 10 11 10 14 15 13 |
R23 | 15 17 19 16 16 13 13 |
R24 | 15 14 15 16 19 12 14 |
Table 1.1530.c GPS week : 1530 MJD: 54954.0-54960.0
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 1530 0 | -30 -130 233 1027 -1997 -14610 89.7 3964 3964 | 148469 0
brd 1530 1 | -100 128 0 -797 499 -27650 228.9 >>>>> >>>>> | 225678 0
brd 1530 2 | -27 67 423 -1039 3076 -10440 93.8 5982 5982 | 224582 0
brd 1530 3 | -88 1 206 398 -96 -9536 90.8 4940 4940 | 223517 0
brd 1530 4 | -5 -12 276 -1889 -2854 -10610 90.2 3467 3467 | 159052 0
brd 1530 5 | 26 -123 235 459 -368 -15470 91.8 3405 3405 | 166442 0
brd 1530 6 | 88 22 458 -1173 -2270 -12510 87.7 3442 3442 | 150212 0
-------------+------------------------------------------------------------+----------------
brd 1530 mean| -19 -6 262 -430 -573 -14403 110.4 >>>>> >>>>> | 185421 0
brd 1530 sdev| 65 94 151 1063 2034 6245 52.3 >>>>> >>>>> | 37117 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 2.1530.0 GPS week: 1530 Day: 0 MJD: 54954
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 -2 0 38 -36 254 -.14 27 25 | 0 2455 4069 4472
cod 237| -2 1 3 -14 43 -45 -.11 18 16 | --- --- --- ---
esx 123| -1 0 5 -47 -46 -43 .46 25 22 | 23370 -2155 6820 10740
iac n/a| 5 -1 -7 53 -25 -192 -.08 31 31 | 150159 -4453 6861 10056
mcc n/a| 9 10 121 436 80 393 .56 191 191 | --- --- --- ---
Table 2.1530.1 GPS week: 1530 Day: 1 MJD: 54955
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 -3 -15 10 -43 -.12 26 25 | 0 447 4642 5136
cod 237| -1 2 1 -14 -10 102 -.09 22 18 | --- --- --- ---
esx 123| 0 1 5 32 9 122 .45 33 27 | 100863 3033 7159 15776
iac n/a| 0 0 -4 12 -7 -157 -.08 27 27 | 226374 573 7208 16448
mcc n/a| 12 5 110 195 82 667 .72 155 155 | --- --- --- ---
Table 2.1530.2 GPS week: 1530 Day: 2 MJD: 54956
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 -8 9 42 141 -.13 30 28 | 0 977 4717 5319
cod 237| -4 0 6 7 -1 82 -.05 23 19 | --- --- --- ---
esx 123| -2 2 19 -54 -91 -26 .47 47 32 | 111515 -9210 8933 13360
iac n/a| 2 0 -10 9 -12 -258 -.04 31 31 | 227997 -6260 8942 13466
mcc n/a| -7 41 99 -160 -65 237 .54 153 153 | --- --- --- ---
Table 2.1530.3 GPS week: 1530 Day: 3 MJD: 54957
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| 4 -3 -10 23 5 264 -.08 32 27 | 0 1295 5136 5739
cod 237| -3 1 5 -3 -26 -41 -.15 21 17 | --- --- --- ---
esx 123| -1 3 9 -24 30 -30 .35 27 23 | 100599 -1102 6755 13242
iac n/a| 2 0 -8 -7 24 -220 -.09 36 36 | 222021 770 6748 14751
mcc n/a| 24 1 42 269 -129 -126 -.05 187 187 | --- --- --- ---
Table 2.1530.4 GPS week: 1530 Day: 4 MJD: 54958
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 -1 -10 11 88 -275 -.09 37 33 | 0 1043 6225 6869
cod 237| 0 0 8 17 -12 104 -.06 20 18 | --- --- --- ---
esx 123| -1 -1 8 -35 -79 168 .44 37 30 | 34525 -2649 7784 12649
iac n/a| 1 6 -12 -30 29 -117 -.20 35 35 | 160733 -373 7821 13516
mcc n/a| 9 -2 91 287 107 -691 .11 160 160 | --- --- --- ---
Table 2.1530.5 GPS week: 1530 Day: 5 MJD: 54959
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 5 -3 34 20 218 -.17 31 31 | 0 691 4022 4609
cod 237| -1 -1 5 -22 -4 -34 -.13 19 15 | --- --- --- ---
esx 123| -4 -2 19 57 -61 53 .54 37 31 | 36789 -3457 7461 12812
iac n/a| 2 -1 -22 -2 50 -221 -.13 32 32 | 166225 688 7438 12194
mcc n/a| -6 12 78 80 119 -642 1.35 170 170 | --- --- --- ---
Table 2.1530.6 GPS week: 1530 Day: 6 MJD: 54960
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 -3 -24 31 257 -.24 41 37 | 0 593 4267 4811
cod 237| -3 2 7 14 -11 59 -.12 23 17 | --- --- --- ---
esx 123| -3 0 13 41 -34 -48 .58 33 28 | 30711 -12155 10852 20268
iac n/a| 2 0 -23 -10 37 -272 -.19 36 36 | 158399 -8222 10868 21151
mcc n/a| 3 6 97 -113 147 -890 .29 174 174 | --- --- --- ---
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 3.1530.0 GPS week: 1530 Day: 0 MJD: 54954
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 655 14 6 18 17 --- 8 | 41 33 33 46 --- 35
R03 | 3559 22 10 17 21 --- 10 | 43 29 36 33 --- 31
XR04 | ---- 2817 1793 --- --- --- 2247 | 4 9999 --- --- --- 9999
R06 | 6044 43 16 21 38 --- 17 | 62 66 60 58 --- 60
XR07 |13023 75 47 --- 43 --- 39 | 55 53 --- 50 --- 47
R08 | 1999 18 15 16 32 107 11 | 51 42 38 52 58 43
R10E | 1494 37 35 40 32 --- 21 | 47 51 51 41 --- 37
R11E | 1966 18 8 22 37 244 12 | 44 27 44 40 48 34
R13E | 890 20 19 19 28 --- 12 | 29 24 33 35 --- 23
R14E | 2801 22 24 34 32 --- 16 | 35 23 53 32 --- 24
R15E | 1737 39 9 28 23 197 15 | 55 33 32 30 25 31
R17 | 1419 19 12 12 31 --- 11 | 40 53 53 38 --- 44
R18 | 3057 28 10 17 32 --- 12 | 39 50 51 36 --- 41
R19 | 2304 37 23 8 26 --- 14 | 43 52 47 36 --- 39
R20 | 1419 26 24 31 48 --- 18 | 20 38 55 21 --- 31
R21 | 2290 29 13 28 23 --- 13 | 36 44 42 29 --- 34
R22 | 887 16 17 34 23 --- 13 | 35 47 40 33 --- 34
R23 | 1982 19 26 17 38 --- 15 | 39 50 37 27 --- 34
R24 |12927 24 17 30 30 --- 14 | 102 115 123 105 --- 111
------+------------------------------------+--------------------------------
RMS | 3964 27 18 25 31 191 |T 43 46 48 41 43 40
WRMS | 3964 25 16 22 31 191 |NE 43 51 51 43 58 44
MEDI | 1982 24 17 21 31 197 |MD 41 44 44 36 48 34
Table 3.1530.1 GPS week: 1530 Day: 1 MJD: 54955
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 21 11 21 27 --- 12 | 32 30 32 42 --- 29
R03 |>>>>> 16 12 22 13 --- 9 | 29 25 29 21 --- 22
XR04 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R06 |>>>>> 36 23 42 26 --- 18 | 64 93 110 64 --- 76
R07 |>>>>> 24 34 26 27 --- 16 | 44 67 40 31 --- 41
R08 |>>>>> 22 18 18 20 103 11 | 30 39 26 41 53 30
R10E | 2998 40 22 63 36 --- 23 | 69 34 68 49 --- 40
R11E |>>>>> 23 26 37 34 159 17 | 20 21 44 41 68 26
R13E |>>>>> 42 30 26 30 --- 19 | 36 29 45 42 --- 26
R14E |>>>>> 27 18 40 41 --- 18 | 29 21 47 40 --- 20
R15E |>>>>> 21 20 27 35 191 15 | 21 24 32 24 30 12
R17 |>>>>> 21 18 19 25 --- 12 | 30 30 30 24 --- 24
R18 |>>>>> 23 17 27 21 --- 12 | 14 37 40 50 --- 30
R19 |>>>>> 10 14 25 17 --- 10 | 25 29 54 26 --- 29
R20 |>>>>> 21 26 29 13 --- 13 | 18 20 33 20 --- 10
R21 |>>>>> 38 22 57 20 --- 20 | 43 37 51 15 --- 22
R22 |>>>>> 20 14 18 17 --- 10 | 32 31 29 25 --- 25
R23 |>>>>> 23 31 34 22 --- 16 | 48 55 46 51 --- 46
R24 |>>>>> 16 25 9 35 --- 14 | 84 80 84 88 --- 81
------+------------------------------------+--------------------------------
RMS |>>>>> 26 22 33 27 155 |T 37 39 46 38 50 32
WRMS |>>>>> 25 18 27 27 155 |NE 37 44 46 38 53 35
MEDI |>>>>> 22 20 26 25 159 |MD 30 30 40 40 53 26
Table 3.1530.2 GPS week: 1530 Day: 2 MJD: 54956
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2144 16 14 16 20 --- 9 | 38 30 38 44 --- 34
R03 | 2012 15 16 29 29 --- 13 | 24 26 37 34 --- 20
XR04 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R06 | 4760 61 28 43 38 --- 25 | 145 172 185 182 --- 167
R07 |12540 13 21 36 29 --- 14 | 23 26 53 35 --- 26
R08 | 1349 42 29 40 27 136 20 | 42 52 54 43 48 41
R10E | 2039 37 24 39 48 --- 21 | 43 35 56 52 --- 32
R11E | 2460 44 22 36 42 178 21 | 51 33 44 47 128 33
R13E | 1277 32 19 40 35 --- 17 | 30 27 56 48 --- 30
R14E | 2263 25 37 60 34 --- 22 | 30 26 84 31 --- 27
R15E | 3572 37 25 136 37 141 37 | 28 34 131 23 74 29
R17 | 905 22 23 23 36 --- 15 | 32 48 53 33 --- 36
R18 | 1264 15 11 20 19 --- 9 | 25 31 45 38 --- 29
R19 | 1115 8 22 17 30 --- 12 | 36 26 53 64 --- 40
R20 | 1373 35 26 36 19 --- 17 | 15 48 63 31 --- 29
R21 | 3282 16 18 41 17 --- 13 | 38 31 79 34 --- 37
R22 | 1862 12 18 25 18 --- 10 | 41 47 39 44 --- 39
R23 | 2308 40 26 31 32 --- 18 | 30 63 79 46 --- 46
R24 |19972 17 22 38 26 --- 14 | 64 70 65 73 --- 65
------+------------------------------------+--------------------------------
RMS | 5982 30 23 47 31 153 |T 40 45 67 50 83 42
WRMS | 5982 28 19 32 31 153 |NE 42 51 64 53 48 46
MEDI | 2039 22 22 36 29 141 |MD 32 33 54 43 74 33
Table 3.1530.3 GPS week: 1530 Day: 3 MJD: 54957
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2144 18 13 23 19 --- 10 | 37 33 44 32 --- 33
R03 | 2333 22 15 24 27 --- 12 | 29 30 37 36 --- 27
XR04 | ---- --- 5 --- --- --- 0 | --- 9999 --- --- --- 9999
R06 | 4594 61 31 25 31 --- 22 | 157 174 189 163 --- 167
R07 |11967 20 15 17 20 --- 10 | 53 41 42 45 --- 44
R08 | 1703 24 14 17 18 212 10 | 29 35 46 25 149 29
R10E | 1308 47 16 21 72 --- 23 | 94 65 62 69 --- 65
R11E | 2152 45 23 37 49 194 22 | 36 61 82 61 191 51
R13E | 1410 26 23 38 50 --- 20 | 25 36 61 72 --- 39
R14E | 1802 44 25 53 46 --- 24 | 23 31 69 42 --- 29
R15E | 2299 25 24 35 22 149 16 | 27 33 75 32 95 34
R17 | 1054 32 28 19 43 --- 17 | 67 93 71 67 --- 75
R18 | 1433 13 18 17 33 --- 12 | 29 43 41 28 --- 30
R19 | 940 25 10 21 20 --- 11 | 29 52 56 34 --- 42
R20 | 2282 25 22 19 49 --- 17 | 27 40 52 53 --- 35
R21 | 2997 17 16 21 22 --- 11 | 40 44 34 36 --- 34
R22 | 1763 17 16 11 25 --- 10 | 34 31 28 22 --- 21
R23 | 1611 30 24 28 30 --- 16 | 34 40 57 46 --- 37
R24 |14874 34 25 23 26 --- 15 | 93 106 94 107 --- 97
------+------------------------------------+--------------------------------
RMS | 4940 32 21 27 36 187 |T 47 54 63 53 145 49
WRMS | 4940 27 17 23 36 187 |NE 50 58 60 53 149 51
MEDI | 1802 25 18 21 27 194 |MD 34 40 56 42 149 35
Table 3.1530.4 GPS week: 1530 Day: 4 MJD: 54958
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 889 14 13 27 30 --- 12 | 51 41 49 38 --- 39
R03 | 3737 25 14 46 31 --- 16 | 39 32 60 27 --- 30
XR04 | ---- --- 7 --- --- --- 0 | --- 424 --- --- --- 445
R06 | 3496 67 30 60 33 --- 27 | 85 120 123 108 --- 106
R07 |10732 31 15 19 20 --- 12 | 35 39 37 31 --- 33
R08 | 1133 33 18 27 22 214 14 | 35 41 35 38 56 33
R10E | 975 43 28 60 56 --- 26 | 64 58 50 50 --- 40
R11E | 1172 27 17 31 46 143 17 | 69 82 76 73 79 71
R13E | 1378 40 24 34 44 --- 20 | 48 23 49 52 --- 27
R14E | 1852 44 26 35 46 --- 21 | 41 46 44 44 --- 34
R15E | 2812 29 11 27 42 102 15 | 37 40 45 42 31 33
R17 | 1808 55 8 52 23 --- 20 | 47 82 119 77 --- 77
R18 | 1512 24 21 35 29 --- 15 | 31 48 47 35 --- 35
R19 | 1042 19 22 25 26 --- 13 | 38 35 34 42 --- 30
R20 | 2636 27 15 41 29 --- 15 | 43 39 40 33 --- 28
R21 | 1458 33 18 29 27 --- 15 | 44 35 42 27 --- 27
R22 | 1399 18 24 12 35 --- 14 | 31 55 40 43 --- 37
R23 | 1415 37 14 26 36 --- 16 | 48 14 28 42 --- 18
R24 | 6135 47 22 37 26 --- 18 | 61 114 128 86 --- 97
------+------------------------------------+--------------------------------
RMS | 3466 37 20 37 35 160 |T 47 72 58 49 55 65
WRMS | 3466 33 18 30 35 160 |NE 45 79 60 48 56 73
MEDI | 1458 31 18 31 30 143 |MD 43 41 45 42 56 34
Table 3.1530.5 GPS week: 1530 Day: 5 MJD: 54959
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1012 13 8 18 14 --- 7 | 25 25 27 24 --- 22
R03 | 3738 24 13 34 27 --- 13 | 19 30 39 29 --- 22
XR04 | ---- --- 39 --- 70 --- 52 | --- 168 --- 54 --- 207
R06 | 5199 47 16 23 32 --- 17 | 104 110 90 95 --- 98
R07 |10049 39 12 30 13 --- 13 | 37 34 39 37 --- 36
R08 | 1650 16 16 26 27 226 12 | 26 38 40 22 55 27
R10E | 1330 47 36 82 53 --- 30 | 40 49 102 44 --- 43
R11E | 1105 28 26 39 35 169 18 | 51 70 68 69 100 61
R13E | 1481 33 30 47 55 --- 23 | 41 41 70 76 --- 44
R14E | 2212 46 25 41 48 --- 22 | 34 47 49 36 --- 30
R15E | 2790 40 17 38 35 85 18 | 43 33 36 38 47 27
R17 | 2027 27 19 26 39 --- 16 | 74 82 74 59 --- 71
R18 | 1431 30 13 23 14 --- 11 | 33 50 69 45 --- 47
R19 | 1287 18 12 31 22 --- 11 | 47 52 52 49 --- 48
R20 | 2688 26 12 39 23 --- 14 | 25 29 42 27 --- 25
R21 | 1323 32 12 28 22 --- 13 | 19 41 52 32 --- 31
R22 | 1582 24 13 41 25 --- 14 | 20 34 67 33 --- 31
R23 | 3655 18 13 24 32 --- 12 | 49 32 33 55 --- 35
R24 | 3524 26 16 22 18 --- 11 | 192 169 165 180 --- 174
------+------------------------------------+--------------------------------
RMS | 3405 31 19 37 32 170 |T 48 59 61 52 67 56
WRMS | 3405 31 15 31 32 170 |NE 51 63 60 52 55 62
MEDI | 1650 27 16 30 27 169 |MD 37 41 52 44 55 36
Table 3.1530.6 GPS week: 1530 Day: 6 MJD: 54960
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1150 16 15 24 21 --- 11 | 36 36 46 38 --- 36
R03 | 3561 20 15 30 23 --- 12 | 27 35 33 39 --- 31
XR04 | ---- --- 10 --- 18 --- 14 | --- 289 --- 45 --- 286
R06 | 9694 69 35 40 51 --- 27 | 123 74 84 116 --- 90
R07 | 5944 37 11 23 17 --- 12 | 37 32 28 34 --- 31
R08 | 1674 53 17 37 25 258 19 | 32 34 64 33 55 35
R10E | 1185 52 50 48 71 --- 32 | 41 66 58 39 --- 39
R11E | 1502 41 22 29 36 139 18 | 96 89 111 79 116 91
R13E | 1068 55 22 46 49 --- 24 | 43 41 48 57 --- 36
R14E | 2261 49 29 55 61 --- 27 | 48 35 42 51 --- 28
R15E | 3637 65 24 49 46 71 26 | 59 32 34 43 50 26
R17 | 2657 14 23 23 31 --- 13 | 58 83 82 52 --- 68
R18 | 1453 35 19 14 14 --- 12 | 35 59 54 38 --- 47
R19 | 2210 16 15 30 28 --- 13 | 42 57 55 39 --- 48
R20 | 3444 24 11 15 16 --- 9 | 29 46 49 31 --- 38
R21 | 1327 32 27 18 18 --- 14 | 25 59 44 26 --- 37
R22 | 1424 29 12 20 31 --- 13 | 30 46 61 59 --- 46
R23 | 2083 20 16 27 29 --- 13 | 26 28 44 35 --- 28
R24 | 3153 36 11 24 23 --- 13 | 191 190 188 191 --- 189
------+------------------------------------+--------------------------------
RMS | 3442 41 23 33 36 174 |T 54 70 62 55 73 64
WRMS | 3442 37 17 28 36 174 |NE 53 76 64 55 55 72
MEDI | 2083 35 17 27 28 139 |MD 37 46 49 39 55 38
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