[IGSREPORT-17990] Wk 1555 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Nov 12 09:37:28 PST 2009
******************************************************************************
IGS Electronic Report 12 Nov 09:37:31 PST 2009 Message Number 17990
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1555 (Oct 25, 2009 - Oct 31, 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 2.1555.
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:
igl1555[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1555 in the SP3 format.
igl15557.sum Combination Report for GPS Week 1555.
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 | 142.3 ns
1 | 185.2 ns
2 | 188.7 ns
3 | 190.1 ns
4 | 502.1 ns
5 | 505.3 ns
6 | 503.3 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 1.1555, 1a.1555).
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 2.1555.0-6)
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 3.1555.0-6).
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 1555 summary. (Oct 25, 2009 - Oct 31, 2009)
Table 1.1555.a GPS week : 1555 MJD: 55129.0-55135.0
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 104| 0 0 -3 7 -13 104 -.16 26 25 | 0 2481 9029 9426
| 0 1 4 29 20 84 .06 | 0 6548
cod 230| -1 0 -6 3 -4 45 -.13 16 14 | --- --- --- ---
| 1 1 2 23 28 31 .03 | --- ---
esx 129| 0 0 -1 -1 43 3 .39 25 23 | 144757 -46334 14489 22514
| 1 1 5 50 34 58 .08 | 34502 115925
iac n/a| 0 0 15 -44 -21 -182 -.03 28 28 | 262964 -2003 14480 22730
| 1 1 3 47 27 85 .05 | 124103 153669
mcc n/a| -28 -10 -1 54 159 -650 .73 252 252 | --- --- --- ---
| 48 22 18 149 300 825 1.66 | --- ---
Table 1.1555.b GPS week : 1555 MJD: 55129.0-55135.0
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 | 10 12 13 11 10 10 14 |
R03 | 8 8 16 13 9 15 12 |
R07 | 12 10 10 8 18 13 15 |
R08 | 12 10 9 10 9 11 10 |
R10 | 13 10 10 10 14 16 16 |
R11 | 17 17 19 16 17 17 16 |
R13 | 13 17 17 15 16 18 20 |
R14 | 11 14 15 17 17 17 17 |
R15 | 15 13 13 14 17 17 19 |
R17 | 10 16 12 10 13 12 17 |
R18 | 10 12 9 9 9 12 14 |
R19 | 10 10 12 11 12 12 9 |
R20 | 9 12 13 10 13 13 11 |
R21 | 10 14 14 11 16 15 14 |
R23 | 14 10 15 11 13 15 15 |
R24 | 19 12 10 14 11 25 16 |
Table 1.1555.c GPS week : 1555 MJD: 55129.0-55135.0
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 1555 0 | 31 -19 244 2190 -141 -1306 92.6 2880 2880 | 142334 0
brd 1555 1 | -154 -48 142 -4774 79 662 88.5 2465 2465 | 185200 0
brd 1555 2 | 96 48 148 -599 -754 -7037 89.6 1923 1923 | 188746 0
brd 1555 3 | 66 51 31 -1832 984 -10700 90.0 1885 1885 | 190102 0
brd 1555 4 | 38 38 90 52 439 -12960 91.2 2542 2542 | 502055 0
brd 1555 5 | -17 -44 65 -200 -1336 -11960 90.6 3131 3131 | 505322 0
brd 1555 6 | 30 64 22 45 202 -14640 90.8 2388 2388 | 503288 0
-------------+------------------------------------------------------------+----------------
brd 1555 mean| 12 12 106 -731 -74 -8277 90.4 2459 2459 | 316721 0
brd 1555 sdev| 81 48 78 2144 768 5942 1.3 457 457 | 175520 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 2.1555.0 GPS week: 1555 Day: 0 MJD: 55129
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 104| 1 0 -10 2 2 203 -.08 27 24 | 0 -680 2272 2459
cod 230| -1 0 -3 12 -10 43 -.13 12 11 | --- --- --- ---
esx 129| 0 0 0 -14 83 -41 .42 23 21 | 89614 -2262 3807 8925
iac n/a| 1 0 15 -30 -71 -230 -.06 26 26 | 144152 -1224 3784 8838
mcc n/a| -114 -6 25 -58 429 -1214 -1.89 536 536 | --- --- --- ---
Table 2.1555.1 GPS week: 1555 Day: 1 MJD: 55130
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 104| 0 0 -5 -12 -39 85 -.10 26 25 | 0 -640 1885 1971
cod 230| 0 0 -6 40 28 45 -.06 15 14 | --- --- --- ---
esx 129| -1 1 6 14 38 31 .28 25 24 | 131482 -1352 3596 8378
iac n/a| 1 0 7 -69 -46 -140 -.05 22 22 | 184563 795 3588 8903
mcc n/a| -81 -41 3 235 647 -2228 1.72 407 407 | --- --- --- ---
Table 2.1555.2 GPS week: 1555 Day: 2 MJD: 55131
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 104| 0 0 4 56 -11 176 -.20 24 25 | 0 863 2028 2225
cod 230| -1 1 -7 -13 -12 65 -.14 14 14 | --- --- --- ---
esx 129| 2 0 -1 -68 10 15 .40 27 23 | 126192 -2868 3178 9902
iac n/a| 0 0 15 27 7 -315 -.04 29 29 | 188424 -754 3188 10200
mcc n/a| -5 -45 -27 278 296 -595 2.91 222 222 | --- --- --- ---
Table 2.1555.3 GPS week: 1555 Day: 3 MJD: 55132
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 104| 0 1 -2 40 -22 31 -.16 26 25 | 0 17274 48657 50312
cod 230| -2 -2 -9 -8 18 53 -.14 13 12 | --- --- --- ---
esx 129| 0 0 3 -46 1 41 .51 21 20 | 201961 -309209 77476 100312
iac n/a| 0 0 16 -5 -7 -208 -.12 28 28 | 263157 -307770 77445 101594
mcc n/a| 0 7 -21 69 24 201 2.30 357 357 | --- --- --- ---
Table 2.1555.4 GPS week: 1555 Day: 4 MJD: 55133
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 104| 1 0 -2 -12 -22 -26 -.23 26 26 | 0 33 3591 3889
cod 230| -4 0 -7 5 -24 87 -.15 17 15 | --- --- --- ---
esx 129| 0 1 -8 30 88 51 .40 24 21 | 157363 -4790 4894 11670
iac n/a| 2 0 17 -65 -18 -165 .05 28 28 | 190862 204358 4904 11135
mcc n/a| -3 5 5 -110 -104 -282 -.15 96 96 | --- --- --- ---
Table 2.1555.5 GPS week: 1555 Day: 5 MJD: 55134
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 104| 0 0 -3 -1 -25 171 -.21 27 25 | 0 -74 2712 2985
cod 230| 0 0 -6 19 18 -16 -.14 21 17 | --- --- --- ---
esx 129| -1 1 -9 -12 25 -110 .45 30 27 | 152271 -317 4386 9301
iac n/a| 0 0 18 -50 -8 -36 .01 27 27 | 400608 69012 4387 9366
mcc n/a| 5 4 -3 4 -57 -365 -.00 77 77 | --- --- --- ---
Table 2.1555.6 GPS week: 1555 Day: 6 MJD: 55135
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 104| 0 1 -7 -23 21 86 -.16 28 26 | 0 595 2059 2142
cod 230| 0 -1 -4 -29 -50 41 -.13 19 18 | --- --- --- ---
esx 129| 0 2 -2 84 58 36 .29 25 23 | 154421 -3542 4088 9110
iac n/a| -1 3 17 -119 -4 -177 -.01 33 33 | 468988 21559 4068 9076
mcc n/a| 0 4 7 -38 -119 -67 .23 71 71 | --- --- --- ---
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 3.1555.0 GPS week: 1555 Day: 0 MJD: 55129
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3117 17 11 20 19 --- 9 | 25 31 32 42 --- 30
R03 | 3022 19 6 14 18 --- 8 | 30 25 33 32 --- 26
R07 | 1310 18 14 17 36 --- 12 | 30 28 23 30 --- 21
R08 | 3385 18 15 18 31 162 11 | 25 26 30 28 83 23
R10E | 1053 26 15 23 28 --- 12 | 51 48 46 52 --- 46
R11E | 1957 42 9 37 30 --- 16 | 50 58 80 54 --- 58
R13E | 844 36 16 14 26 --- 13 | 58 68 69 51 --- 62
R14E | 2524 25 14 17 25 --- 11 | 33 33 40 23 --- 28
R15E | 1969 41 11 20 36 740 15 | 33 24 35 30 87 23
R17 | 1771 23 8 20 18 --- 9 | 37 46 44 45 --- 41
R18 | 5057 23 8 19 20 --- 9 | 47 36 31 42 --- 35
R19 | 2937 20 9 19 24 --- 10 | 42 47 51 50 --- 44
R20 | 2482 20 11 11 18 --- 8 | 25 29 32 35 --- 27
R21 | 2048 16 5 27 23 --- 10 | 34 40 30 42 --- 34
R23 | 1571 38 7 30 25 --- 14 | 65 71 88 67 --- 72
R24 | 5879 35 24 43 30 --- 18 | 237 242 247 241 --- 240
------+------------------------------------+--------------------------------
RMS | 2879 27 12 23 26 536 |T 51 53 56 54 85 50
WRMS | 2879 24 11 21 26 536 |NE 54 56 58 59 83 53
MEDI | 2048 23 11 19 25 162 |MD 34 36 35 42 83 34
Table 3.1555.1 GPS week: 1555 Day: 1 MJD: 55130
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2082 32 9 17 24 --- 11 | 24 31 34 33 --- 27
R03 | 2108 13 8 18 14 --- 7 | 30 33 38 31 --- 29
R07 | 2408 21 12 24 16 --- 10 | 26 24 35 25 --- 23
R08 | 2709 15 13 16 24 241 10 | 20 25 33 19 33 22
R10E | 1497 23 6 22 18 --- 10 | 36 44 44 48 --- 41
R11E | 992 37 14 39 32 --- 17 | 34 35 62 44 --- 38
R13E | 1850 36 23 33 24 --- 16 | 48 53 53 37 --- 45
R14E | 1788 19 19 27 29 --- 13 | 25 25 37 27 --- 18
R15E | 2305 32 12 13 30 523 12 | 25 20 26 28 85 19
R17 | 2254 31 20 33 27 --- 15 | 17 26 35 26 --- 15
R18 | 3546 22 10 31 17 --- 11 | 31 40 43 50 --- 37
R19 | 2237 23 14 15 19 --- 10 | 28 33 29 42 --- 30
R20 | 1938 18 14 28 20 --- 11 | 14 23 38 22 --- 18
R21 | 1551 13 25 29 21 --- 13 | 19 35 48 26 --- 28
R23 | 1089 25 10 18 16 --- 10 | 54 61 64 63 --- 58
R24 | 5487 31 13 25 17 --- 12 | 212 204 195 195 --- 201
------+------------------------------------+--------------------------------
RMS | 2465 26 15 25 22 407 |T 40 44 50 44 59 40
WRMS | 2465 25 14 24 22 407 |NE 43 48 53 48 33 44
MEDI | 2082 23 13 24 20 241 |MD 26 33 38 31 33 28
Table 3.1555.2 GPS week: 1555 Day: 2 MJD: 55131
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1702 21 14 24 32 --- 13 | 29 28 38 45 --- 29
R03 | 1399 26 16 39 33 --- 16 | 32 28 55 54 --- 35
R07 | 2939 19 8 18 23 --- 9 | 27 16 32 29 --- 21
R08 | 1507 17 6 21 18 190 9 | 31 21 29 34 86 24
R10E | 994 11 9 22 25 --- 9 | 51 51 60 38 --- 47
R11E | 957 32 12 43 45 --- 18 | 35 35 66 41 --- 35
R13E | 2334 40 11 28 37 --- 16 | 45 40 57 47 --- 42
R14E | 1728 29 22 25 32 --- 15 | 26 28 32 22 --- 20
R15E | 4031 20 14 28 29 251 12 | 20 32 42 28 65 23
R17 | 1611 18 15 21 30 --- 11 | 30 43 45 45 --- 39
R18 | 2731 15 8 15 22 --- 8 | 28 39 33 48 --- 34
R19 | 1060 20 20 15 24 --- 11 | 35 62 51 20 --- 45
R20 | 878 23 16 18 31 --- 12 | 23 30 26 37 --- 22
R21 | 616 31 17 24 27 --- 14 | 19 39 43 26 --- 26
R23 | 1275 26 14 42 16 --- 14 | 57 57 98 54 --- 64
R24 | 1682 21 11 19 19 --- 10 | 260 267 268 276 --- 266
------+------------------------------------+--------------------------------
RMS | 1922 24 14 27 29 222 |T 46 51 60 52 75 48
WRMS | 1922 25 14 23 29 222 |NE 51 57 65 60 86 55
MEDI | 1507 21 14 22 27 190 |MD 30 35 43 38 65 34
Table 3.1555.3 GPS week: 1555 Day: 3 MJD: 55132
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1147 20 7 15 36 --- 11 | 18 24 30 50 --- 25
R03 | 841 26 11 23 36 --- 13 | 21 24 31 34 --- 21
R07 | 3833 15 12 13 13 --- 7 | 22 33 29 29 --- 27
R08 | 2567 17 13 13 23 198 9 | 36 30 34 35 161 30
R10E | 722 22 9 18 25 --- 10 | 36 62 70 64 --- 57
R11E | 946 20 13 36 39 572 15 | 40 47 68 42 95 41
R13E | 1597 30 11 25 44 --- 15 | 50 42 70 60 --- 50
R14E | 2929 48 15 16 39 --- 16 | 30 20 37 37 --- 23
R15E | 1262 33 13 27 29 126 14 | 25 28 51 37 153 30
R17 | 1330 14 12 23 14 --- 9 | 50 45 65 50 --- 49
R18 | 1551 18 8 16 24 --- 9 | 52 54 55 55 --- 52
R19 | 703 17 16 23 21 --- 11 | 39 56 48 29 --- 44
R20 | 2129 20 14 17 18 --- 9 | 28 48 48 28 --- 38
R21 | 857 23 13 23 19 --- 11 | 17 33 33 32 --- 25
R23 | 1320 26 12 14 27 --- 11 | 44 38 47 52 --- 40
R24 | 2775 40 17 18 20 --- 14 | 134 157 151 151 --- 149
------+------------------------------------+--------------------------------
RMS | 1884 26 13 21 28 357 |T 40 46 54 49 136 43
WRMS | 1884 25 12 20 28 357 |NE 41 49 51 49 161 45
MEDI | 1320 20 12 18 24 198 |MD 36 38 48 37 153 38
Table 3.1555.4 GPS week: 1555 Day: 4 MJD: 55133
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1291 12 7 15 30 --- 10 | 25 19 26 35 --- 22
R03 | 1338 15 11 16 20 --- 9 | 22 29 39 25 --- 26
R07 | 6962 32 27 29 36 --- 17 | 45 34 54 42 --- 34
R08 | 3328 14 13 9 23 131 9 | 23 26 28 34 149 24
R10E | 1657 32 18 26 18 --- 14 | 61 65 68 66 --- 62
R11E | 1803 26 16 38 37 55 17 | 37 32 61 41 112 36
R13E | 1426 28 22 24 38 --- 16 | 28 36 46 35 --- 30
R14E | 3372 32 16 25 41 --- 16 | 29 34 35 40 --- 29
R15E | 2359 33 21 31 35 86 17 | 30 29 37 45 85 27
R17 | 1233 28 13 21 27 --- 13 | 42 48 49 36 --- 41
R18 | 1195 17 14 14 13 --- 8 | 32 21 35 35 --- 27
R19 | 785 28 16 16 21 --- 11 | 53 65 74 57 --- 61
R20 | 1513 23 21 22 17 --- 12 | 22 39 40 29 --- 28
R21 | 863 31 15 38 24 --- 16 | 25 27 49 15 --- 20
R23 | 1013 20 22 21 21 --- 12 | 66 50 68 59 --- 57
R24 | 2781 19 13 23 22 --- 11 | 294 305 300 305 --- 301
------+------------------------------------+--------------------------------
RMS | 2541 25 17 24 28 96 |T 52 53 63 56 115 51
WRMS | 2541 26 15 21 28 96 |NE 59 60 69 61 149 58
MEDI | 1426 26 16 22 23 86 |MD 30 34 46 36 112 29
Table 3.1555.5 GPS week: 1555 Day: 5 MJD: 55134
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1345 19 10 19 21 --- 10 | 16 28 43 29 --- 25
R03 | 4985 29 21 30 22 --- 15 | 24 34 56 27 --- 31
R07 | 8348 28 19 11 24 --- 12 | 31 25 23 29 --- 20
R08 | 2965 20 16 21 19 76 11 | 30 31 38 35 68 28
R10E | 1371 41 18 26 19 --- 15 | 35 45 37 39 --- 34
R11E | 1268 26 20 33 39 68 17 | 48 43 62 41 47 42
R13E | 906 30 24 33 37 --- 17 | 35 49 68 48 --- 43
R14E | 1808 28 23 27 35 --- 16 | 32 35 37 37 --- 25
R15E | 2186 30 24 20 39 85 16 | 20 37 33 48 58 27
R17 | 1066 21 9 25 29 --- 12 | 35 42 64 23 --- 37
R18 | 1713 8 10 35 19 --- 11 | 44 37 58 43 --- 41
R19 | 782 19 14 25 22 --- 11 | 23 38 60 44 --- 37
R20 | 5586 18 28 26 13 --- 13 | 37 60 54 38 --- 45
R21 | 710 14 25 39 17 --- 14 | 22 37 39 22 --- 25
R23 | 932 15 26 31 26 --- 14 | 38 47 78 63 --- 51
R24 | 1423 51 28 55 35 --- 24 | 157 183 197 160 --- 170
------+------------------------------------+--------------------------------
RMS | 3130 27 21 30 27 77 |T 39 48 59 45 57 42
WRMS | 3130 25 17 27 27 77 |NE 41 51 64 46 68 46
MEDI | 1371 21 20 26 22 76 |MD 32 37 54 38 58 34
Table 3.1555.6 GPS week: 1555 Day: 6 MJD: 55135
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1780 28 16 29 21 --- 13 | 31 30 39 39 --- 27
R03 | 1974 21 12 18 30 --- 11 | 29 34 38 37 --- 31
R07 | 5507 35 18 27 20 --- 14 | 43 31 34 45 --- 30
R08 | 2007 14 16 17 21 54 10 | 26 32 40 35 45 30
R10E | 2667 31 20 24 40 --- 16 | 35 41 51 44 --- 37
R11E | 1016 23 22 29 39 93 16 | 26 31 51 39 49 29
R13E | 1655 30 20 40 50 --- 20 | 51 60 60 59 --- 52
R14E | 1747 31 18 28 39 --- 16 | 40 24 34 47 --- 26
R15E | 2293 30 15 29 53 60 18 | 31 26 36 57 60 28
R17 | 1063 41 20 23 34 --- 17 | 47 63 52 38 --- 50
R18 | 880 20 25 27 22 --- 14 | 44 40 43 35 --- 37
R19 | 1428 16 17 11 17 --- 9 | 39 47 47 34 --- 41
R20 | 4838 28 11 15 15 --- 10 | 27 41 48 43 --- 38
R21 | 828 18 19 20 37 --- 13 | 42 55 40 63 --- 45
R23 | 733 36 21 17 29 --- 15 | 48 51 61 54 --- 50
R24 | 1432 28 22 25 34 --- 15 | 201 205 202 205 --- 202
------+------------------------------------+--------------------------------
RMS | 2388 28 19 25 33 71 |T 47 50 54 54 51 47
WRMS | 2388 26 18 23 33 71 |NE 52 57 58 57 45 52
MEDI | 1655 28 18 24 30 60 |MD 39 40 43 43 49 37
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