[IGSREPORT-16018] Wk 1467 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Fri Mar 7 07:02:20 PST 2008
******************************************************************************
IGS Electronic Report 07 Mar 07:02:22 PST 2008 Message Number 16018
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1467 (Feb 17, 2008 - Feb 23, 2008)
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 2.1467.
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:
igl1467[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1467 in the SP3 format.
igl14677.sum Combination Report for GPS Week 1467.
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 | 1271.0 ns
1 | 1246.8 ns
2 | 1278.6 ns
3 | 1236.3 ns
4 | 1239.7 ns
5 | 1274.4 ns
6 | 1214.9 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 | COD | R08
2 | ESX | R19
3 | ESX | R19
4 | ESX | R07 R11
5 | ESX | R17
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 1.1467, 1a.1467).
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 2.1467.0-6)
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 3.1467.0-6).
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 1467 summary. (Feb 17, 2008 - Feb 23, 2008)
Table 1.1467.a GPS week : 1467 MJD: 54513.0-54519.0
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 65| 0 0 0 7 45 8 -.11 36 33 | 0 180 2724 2841
| 2 2 8 25 24 75 .10 | 0 214
cod 176| 0 0 3 33 -11 34 -.06 61 27 | --- --- --- ---
| 1 2 5 51 22 78 .05 | --- ---
esx 111| 1 1 3 -20 -41 -21 .39 103 102 | 2862 1105 8833 24887
| 4 5 6 44 78 156 .15 | 25095 8181
iac n/a| 0 0 -8 -16 12 -36 -.03 37 37 | 1250334 -2007 8812 18571
| 2 2 6 31 58 57 .08 | 24641 6295
mcc n/a| -13 -6 6 224 272 665 .57 220 220 | --- --- --- ---
| 32 19 35 173 153 453 1.10 | --- ---
Table 1.1467.b GPS week : 1467 MJD: 54513.0-54519.0
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 | 27 14 24 23 16 19 22 |
R04 | 16 14 27 24 18 37 21 |
R06 | 18 17 19 21 13 15 17 |
R07 | 0 0 0 0 38 27 17 |
R08 | 67 39 58 42 43 38 42 |
R09 | 20 33 27 20 26 47 23 |
R10 | 14 14 16 22 24 17 15 |
R11 | 15 18 19 21 20 30 39 |
R13 | 30 21 23 25 26 13 20 |
R14 | 14 13 13 16 16 16 15 |
R15 | 29 33 38 37 20 23 23 |
R17 | 17 17 23 26 23 17 17 |
R19 | 24 32 17 21 16 23 23 |
R20 | 24 18 16 24 20 16 18 |
R23 | 21 17 19 17 23 22 15 |
R24 | 0 0 0 21 30 22 25 |
Table 1.1467.c GPS week : 1467 MJD: 54513.0-54519.0
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 1467 0 | 307 100 192 2305 2947 -8016 95.1 7019 7019 | 1271045 0
brd 1467 1 | 121 -135 302 4140 2482 -12490 94.3 6754 6754 | 1246798 0
brd 1467 2 | 51 -85 -85 1798 5846 -10750 95.6 7672 7672 | 1278551 0
brd 1467 3 | 86 121 195 649 5879 -19570 94.0 6961 6961 | 1236312 0
brd 1467 4 | 42 58 156 1030 6645 -22700 95.2 6219 6219 | 1239745 0
brd 1467 5 | 34 42 353 1690 3410 -13860 98.0 5761 5761 | 1274409 0
brd 1467 6 | -44 -170 -61 5256 635 -14970 96.7 5989 5989 | 1214875 0
-------------+------------------------------------------------------------+----------------
brd 1467 mean| 85 -9 150 2409 3977 -14622 95.5 6625 6625 | 1251676 0
brd 1467 sdev| 110 118 167 1683 2198 5059 1.4 670 670 | 23702 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 2.1467.0 GPS week: 1467 Day: 0 MJD: 54513
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 65| 4 0 13 1 41 28 -.07 35 35 | 0 531 2880 3081
cod 176| -1 0 0 18 -13 -121 -.06 250 33 | --- --- --- ---
esx 111| 1 7 0 -41 -45 191 .28 84 84 | 7295 -5638 7802 27901
iac n/a| -2 -2 -11 -22 25 -9 .05 27 27 | 1270618 -11002 8116 22092
mcc n/a| 3 -41 -41 238 203 563 .78 106 106 | --- --- --- ---
Table 2.1467.1 GPS week: 1467 Day: 1 MJD: 54514
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 65| 2 -2 7 5 57 -86 -.12 33 33 | 0 -62 2768 2883
cod 176| 0 0 -4 33 -54 59 -.05 23 22 | --- --- --- ---
esx 111| -7 5 0 -31 40 157 .21 87 87 | -11558 13572 10824 38024
iac n/a| 5 1 0 -16 47 -22 .04 35 35 | 1236650 6465 10815 25977
mcc n/a| 14 -21 -22 558 315 843 -.67 122 122 | --- --- --- ---
Table 2.1467.2 GPS week: 1467 Day: 2 MJD: 54515
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 65| -2 0 -8 -27 47 -60 -.04 35 34 | 0 119 2927 3029
cod 176| 0 0 5 129 17 116 -.02 31 27 | --- --- --- ---
esx 111| 3 0 1 -30 -127 -84 .31 168 168 | 45176 -5339 8089 23318
iac n/a| -1 -1 -1 -60 53 62 -.03 42 42 | 1281974 -5437 7804 12904
mcc n/a| 9 5 14 80 439 360 -.39 172 172 | --- --- --- ---
Table 2.1467.3 GPS week: 1467 Day: 3 MJD: 54516
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 65| -2 -2 -6 33 -5 63 -.32 39 34 | 0 36 3222 3315
cod 176| -4 -1 9 40 -20 18 -.15 31 28 | --- --- --- ---
esx 111| 0 2 2 -39 -135 -154 .67 114 116 | -20088 -2981 8629 26387
iac n/a| -1 -1 -15 17 98 -47 -.17 48 48 | 1232155 -2769 8065 22522
mcc n/a| -10 -11 36 186 37 1226 -.22 145 145 | --- --- --- ---
Table 2.1467.4 GPS week: 1467 Day: 4 MJD: 54517
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 65| -2 0 -9 23 52 -37 -.14 40 34 | 0 79 2605 2769
cod 176| -1 1 9 -17 4 53 -.11 27 25 | --- --- --- ---
esx 111| 3 -1 1 31 74 54 .45 100 100 | -11831 7724 5800 20231
iac n/a| -1 -3 -5 3 -45 -31 -.12 35 35 | 1238055 2868 5431 15464
mcc n/a| -48 11 -20 107 342 1000 1.21 209 209 | --- --- --- ---
Table 2.1467.5 GPS week: 1467 Day: 5 MJD: 54518
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 65| 0 6 3 38 71 23 -.04 41 33 | 0 141 2081 2147
cod 176| 2 -5 4 -24 -13 98 -.04 28 26 | --- --- --- ---
esx 111| 3 2 1 -79 -34 -103 .37 96 88 | 27924 7168 10330 19157
iac n/a| -1 4 -13 17 -55 -112 -.02 41 41 | 1274122 2862 10983 15613
mcc n/a| -68 0 54 324 434 808 2.48 499 499 | --- --- --- ---
Table 2.1467.6 GPS week: 1467 Day: 6 MJD: 54519
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 65| -2 1 2 -20 52 131 -.03 31 31 | 0 419 2588 2667
cod 176| 0 0 0 51 -1 19 -.01 34 26 | --- --- --- ---
esx 111| 6 -7 18 47 -61 -209 .42 72 72 | -16884 -6768 10363 19193
iac n/a| 0 1 -13 -51 -35 -90 .03 34 34 | 1218769 -7039 10475 15430
mcc n/a| 4 10 23 75 131 -141 .79 289 289 | --- --- --- ---
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 3.1467.0 GPS week: 1467 Day: 0 MJD: 54513
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1795 30 42 99 24 --- 26 | 45 49 82 52 --- 39
R04 | 1451 20 18 44 29 --- 15 | 53 50 52 42 --- 45
R06 | 4502 34 24 52 24 --- 18 | 25 49 58 48 --- 38
XR07 | ---- --- 7 --- --- 669 0 | --- 9999 --- --- 60 9999
R08 | 9376 56 929 208 32 --- 67 | 25 482 65 23 --- 23
R09 |13842 36 29 39 33 --- 19 | 46 41 79 55 --- 38
R10 | 904 24 17 39 22 --- 14 | 13 33 34 28 --- 20
R11 | 8245 24 23 39 23 --- 14 | 19 41 60 36 --- 28
R13 |13366 46 27 106 38 --- 29 | 24 26 117 35 --- 29
R14 | 5062 22 12 46 17 --- 13 | 21 26 52 35 --- 24
R15 | 3649 44 43 103 18 106 28 | 50 37 95 39 54 28
R17 | 7975 16 24 51 28 --- 16 | 31 34 64 49 --- 35
R19 | 2504 49 46 45 28 --- 24 | 316 311 302 299 --- 303
R20 | 1150 43 41 62 24 --- 23 | 22 56 53 49 --- 32
R23 | 5188 22 33 71 27 --- 21 | 77 90 100 77 --- 79
XR24 | ---- --- 6 --- --- --- 0 | --- 230 --- --- --- 227
------+------------------------------------+--------------------------------
RMS | 7018 35 250 84 27 106 |T 54 103 86 61 57 65
WRMS | 7018 35 33 84 27 106 |NE 54 103 86 61 57 65
MEDI | 4502 30 24 51 24 106 |MD 25 49 64 42 54 35
Table 3.1467.1 GPS week: 1467 Day: 1 MJD: 54514
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4233 21 19 35 25 --- 13 | 26 46 60 49 --- 37
R04 | 733 22 11 48 23 --- 13 | 59 65 49 40 --- 49
R06 | 4158 30 16 32 39 --- 16 | 20 26 48 39 --- 25
XR07 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R08 | 6112 36 39 186 22 --- 38 | 25 186 115 24 --- 32
R09 |15206 51 24 121 56 --- 32 | 38 36 98 49 --- 22
R10 | 1667 30 13 36 25 --- 14 | 18 27 47 16 --- 15
R11 | 4741 22 17 67 30 --- 17 | 21 28 79 46 --- 27
R13 |12141 21 22 76 42 --- 21 | 24 39 57 41 --- 25
R14 | 1915 26 14 40 16 --- 12 | 33 21 49 23 --- 24
R15 | 7483 57 41 92 59 122 32 | 35 51 115 22 42 27
R17 | 7296 23 17 36 42 --- 16 | 36 50 66 39 --- 37
R19 | 2431 41 24 153 22 --- 32 | 278 235 184 252 --- 243
R20 | 1419 23 29 45 35 --- 18 | 19 28 48 50 --- 24
R23 | 6387 25 17 55 30 --- 16 | 51 50 77 61 --- 51
XR24 | ---- --- 5 --- --- --- 0 | --- 248 --- --- --- 247
------+------------------------------------+--------------------------------
RMS | 6754 33 23 87 35 122 |T 48 75 78 53 42 59
WRMS | 6754 33 22 87 35 122 |NE 48 75 78 53 42 59
MEDI | 4233 25 17 48 30 122 |MD 26 46 60 40 42 27
Table 3.1467.2 GPS week: 1467 Day: 2 MJD: 54515
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7801 25 48 24 53 --- 24 | 26 46 38 32 --- 25
R04 | 1839 28 60 38 51 --- 27 | 21 63 47 40 --- 32
R06 | 1382 32 20 26 45 --- 18 | 23 34 40 47 --- 31
XR07 | ---- --- 10 --- --- --- 0 | --- 9999 --- --- --- 9999
R08 | 5991 68 32 238 41 --- 57 | 63 100 182 30 --- 56
R09 | 9765 21 28 95 44 --- 26 | 39 44 95 50 --- 38
R10 | 3090 23 23 35 29 --- 15 | 11 29 49 24 --- 16
R11 | 9225 30 12 50 43 --- 19 | 20 30 82 60 --- 29
R13 |11439 20 36 49 56 --- 23 | 32 49 59 63 --- 33
R14 | 1326 14 16 29 31 --- 12 | 13 11 33 35 --- 12
R15 |15725 74 20 114 59 171 38 | 40 29 99 42 53 27
R17 | 9392 25 27 82 30 --- 22 | 38 38 74 35 --- 33
R19 | 2329 20 25 548 27 --- 17 | 242 242 620 244 --- 245
R20 | 1143 13 28 38 33 --- 16 | 32 53 66 65 --- 47
R23 | 7559 36 32 33 30 --- 19 | 71 59 81 59 --- 60
XR24 | ---- --- 10 --- --- --- 0 | --- 165 --- --- --- 161
------+------------------------------------+--------------------------------
RMS | 7672 35 31 168 42 171 |T 47 66 111 59 53 56
WRMS | 7672 34 27 168 42 171 |NE 47 66 111 59 53 56
MEDI | 5991 25 25 38 41 171 |MD 32 46 66 42 53 33
Table 3.1467.3 GPS week: 1467 Day: 3 MJD: 54516
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9170 34 29 34 63 --- 23 | 46 74 83 77 --- 64
R04 | 1245 13 39 34 63 --- 23 | 56 66 63 41 --- 51
R06 | 2455 31 27 55 39 --- 21 | 28 44 63 42 --- 32
XR07 | ---- --- 7 --- --- 332 0 | --- 9999 --- --- 61 9999
R08 | 4642 99 50 70 64 --- 42 | 72 123 140 39 --- 47
R09 | 9121 24 39 42 27 --- 19 | 36 46 28 28 --- 21
R10 | 1134 34 28 54 40 --- 21 | 24 52 58 41 --- 31
R11 |12391 29 22 30 60 --- 21 | 17 33 61 52 --- 25
R13 |11806 43 15 80 33 --- 25 | 21 47 97 36 --- 38
R14 | 1303 17 30 20 37 --- 16 | 39 26 31 50 --- 27
R15 | 7038 49 30 131 39 145 37 | 64 35 144 44 97 35
R17 | 9891 27 17 84 50 --- 25 | 66 67 133 100 --- 78
R19 | 1568 29 27 364 35 --- 21 | 165 163 329 154 --- 157
R20 | 1154 17 35 46 65 --- 24 | 24 34 38 59 --- 24
R23 | 5907 26 21 48 25 --- 17 | 69 59 96 89 --- 70
XR24 |11213 24 18 --- --- --- 21 | 48 221 --- --- --- 208
------+------------------------------------+--------------------------------
RMS | 6961 39 31 114 48 145 |T 51 72 97 60 79 60
WRMS | 6961 34 28 116 48 145 |NE 51 72 97 60 79 60
MEDI | 5907 29 27 48 39 145 |MD 46 52 63 44 61 38
Table 3.1467.4 GPS week: 1467 Day: 4 MJD: 54517
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4264 16 19 34 37 --- 15 | 60 64 63 71 --- 62
R04 | 4474 48 22 25 27 --- 18 | 70 32 23 29 --- 23
R06 | 4113 22 20 27 24 --- 13 | 47 50 47 42 --- 43
XR07 | 5593 50 28 446 --- 130 38 | 14 9999 330 --- 49 9999
R08 | 4177 88 53 130 40 --- 42 | 61 81 69 46 --- 53
R09 |13380 27 42 50 53 --- 25 | 37 53 108 52 --- 47
R10 | 1856 33 41 55 36 --- 23 | 21 65 42 44 --- 36
R11 | 4296 15 24 295 40 --- 20 | 36 32 266 75 --- 44
R13 |10067 27 22 96 34 --- 25 | 21 24 88 27 --- 22
R14 | 2254 33 19 36 26 --- 16 | 31 22 47 29 --- 17
R15 | 5889 52 15 58 14 209 20 | 73 36 52 35 127 31
R17 |10362 22 15 84 37 --- 22 | 46 47 71 51 --- 47
R19 | 1169 24 19 53 14 --- 15 | 254 242 237 271 --- 253
R20 | 1218 40 18 35 43 --- 19 | 33 41 63 56 --- 43
R23 | 4075 45 20 55 45 --- 22 | 51 47 99 81 --- 60
XR24 | 5470 43 25 67 --- 1043 29 | 25 109 88 --- 564 98
------+------------------------------------+--------------------------------
RMS | 6219 40 27 100 35 209 |T 55 63 105 64 246 58
WRMS | 6219 34 25 100 35 209 |NE 55 63 105 64 246 58
MEDI | 4264 33 20 55 36 209 |MD 37 47 69 46 127 44
Table 3.1467.5 GPS week: 1467 Day: 5 MJD: 54518
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4845 28 18 62 31 --- 18 | 39 48 68 28 --- 37
R04 | 5202 100 34 43 57 --- 36 | 102 50 30 24 --- 45
R06 | 5143 21 22 48 19 --- 15 | 45 61 52 62 --- 50
XR07 | 2891 39 28 57 --- 115 27 | 28 9999 166 --- 41 9999
R08 | 2887 44 43 153 31 --- 38 | 53 137 100 32 --- 36
R09 | 7961 51 43 160 89 --- 46 | 30 51 152 53 --- 35
R10 | 1881 32 28 29 24 --- 16 | 18 34 46 24 --- 18
R11 | 7230 25 41 115 29 --- 30 | 16 42 124 31 --- 20
R13 |11802 21 15 14 31 --- 12 | 16 21 36 15 --- 12
R14 | 1257 16 24 35 36 --- 16 | 18 22 49 34 --- 23
R15 | 5765 34 18 84 34 209 23 | 29 51 98 56 47 43
R17 | 9502 25 23 219 25 --- 17 | 45 38 193 61 --- 39
R19 | 1325 41 36 60 32 --- 23 | 171 202 174 182 --- 182
R20 | 1008 29 12 55 22 --- 16 | 30 38 68 39 --- 35
R23 | 3876 32 26 47 49 --- 21 | 40 42 75 73 --- 48
R24 | 3334 44 19 47 45 674 21 | 22 87 58 19 40 77
------+------------------------------------+--------------------------------
RMS | 5761 41 28 96 41 499 |T 43 61 93 48 42 46
WRMS | 5761 33 26 88 41 499 |NE 43 61 93 48 42 46
MEDI | 3876 32 24 55 31 209 |MD 30 48 68 34 41 37
Table 3.1467.6 GPS week: 1467 Day: 6 MJD: 54519
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5614 29 22 84 27 --- 22 | 55 63 71 50 --- 51
R04 | 7610 32 24 55 39 --- 20 | 52 54 81 31 --- 41
R06 | 1288 22 13 57 33 --- 17 | 49 45 51 46 --- 44
R07 | 4349 21 23 49 28 67 16 | 27 9999 96 6 33 9999
R08 | 3016 48 80 125 46 --- 41 | 70 186 109 41 --- 71
R09 |10683 22 41 40 49 --- 22 | 34 48 68 55 --- 34
R10 | 1407 19 11 57 20 --- 14 | 24 43 81 32 --- 33
R11 | 8033 45 48 151 36 --- 38 | 16 56 122 49 --- 38
R13 |11455 30 36 35 35 --- 19 | 30 48 43 33 --- 23
R14 | 1147 27 14 34 31 --- 15 | 16 19 42 43 --- 23
R15 | 3313 34 33 49 47 238 22 | 38 51 68 59 61 41
R17 | 9992 20 21 55 29 --- 17 | 36 30 70 45 --- 32
R19 | 2622 30 38 79 18 --- 23 | 248 237 220 235 --- 236
R20 | 1808 32 11 53 31 --- 18 | 24 42 59 46 --- 36
R23 | 4399 19 15 48 28 --- 15 | 75 74 76 100 --- 79
R24 | 1120 39 43 65 33 435 25 | 18 60 52 22 43 61
------+------------------------------------+--------------------------------
RMS | 5989 31 34 72 34 289 |T 50 70 81 55 45 56
WRMS | 5989 31 26 72 34 289 |NE 50 70 81 55 45 56
MEDI | 3313 29 23 55 31 238 |MD 34 51 70 45 43 41
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