[IGSREPORT-18371] Wk 1572 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 11 05:41:06 PST 2010
******************************************************************************
IGS Electronic Report 11 Mar 07:49:15 PST 2010 Message Number 18371
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1572 (Feb 21, 2010 - Feb 27, 2010)
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 2.1572.
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:
igl1572[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1572 in the SP3 format.
igl15727.sum Combination Report for GPS Week 1572.
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 | 486.3 ns
1 | 434.4 ns
2 | 409.0 ns
3 | 403.6 ns
4 | 485.5 ns
5 | 479.3 ns
6 | 474.8 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 1.1572, 1a.1572).
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 2.1572.0-6)
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 3.1572.0-6).
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 1572 summary. (Feb 21, 2010 - Feb 27, 2010)
Table 1.1572.a GPS week : 1572 MJD: 55248.0-55254.0
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 130| 1 0 0 9 -24 -83 -.22 37 33 | 0 -7 1672 1749
| 0 1 3 42 36 85 .04 | 0 77
cod 244| -1 0 -4 -5 -21 41 -.20 20 17 | --- --- --- ---
| 1 1 1 17 20 50 .06 | --- ---
esx 130| 0 0 -8 18 51 61 .35 27 24 | 107679 -177 4417 8685
| 1 2 2 25 24 64 .04 | 38502 3431
iac n/a| 0 0 23 -34 12 -76 .09 41 41 | 453562 -650 4462 8991
| 2 3 5 26 32 65 .06 | 36758 1590
mcc n/a| 7 -7 38 34 -8 -1042 -.26 168 168 | --- --- --- ---
| 14 16 17 91 127 734 .82 | --- ---
Table 1.1572.b GPS week : 1572 MJD: 55248.0-55254.0
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 | 14 18 14 10 10 13 11 |
R02 | 14 14 14 9 13 14 23 |
R03 | 14 15 14 13 11 12 25 |
R04 | 12 17 20 14 13 14 33 |
R05 | 15 14 14 11 17 16 15 |
R07 | 16 14 12 8 16 14 13 |
R08 | 13 17 14 10 9 13 12 |
R10 | 13 11 15 15 29 12 12 |
R11 | 14 14 12 11 14 10 14 |
R13 | 15 14 13 9 10 13 11 |
R14 | 26 15 12 12 7 9 17 |
R15 | 10 14 9 10 9 14 33 |
R17 | 24 22 14 19 19 16 17 |
R18 | 17 21 17 16 20 18 29 |
R19 | 28 24 20 17 18 19 30 |
R20 | 26 35 29 23 23 23 31 |
R21 | 17 16 17 17 22 18 19 |
R23 | 23 23 14 18 18 27 23 |
Table 1.1572.c GPS week : 1572 MJD: 55248.0-55254.0
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 1572 0 | 67 96 105 -350 2138 -12240 89.1 2319 2319 | 486320 0
brd 1572 1 | -50 87 86 169 -1200 -13010 89.1 2289 2289 | 434386 0
brd 1572 2 | 0 -11 52 1775 -517 -11240 90.6 2172 2172 | 409015 0
brd 1572 3 | -9 14 28 -1094 393 -6499 89.2 2177 2177 | 403566 0
brd 1572 4 | 32 19 -49 -1124 -489 -5338 88.7 1833 1833 | 485507 0
brd 1572 5 | -43 36 166 -457 2600 -8537 89.1 1863 1863 | 479279 0
brd 1572 6 | 115 -20 216 -354 2107 -9774 84.7 1958 1958 | 474753 0
-------------+------------------------------------------------------------+----------------
brd 1572 mean| 16 31 86 -205 718 -9519 88.6 2087 2087 | 453260 0
brd 1572 sdev| 59 45 88 983 1541 2892 1.8 200 200 | 36640 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 2.1572.0 GPS week: 1572 Day: 0 MJD: 55248
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 130| 0 -1 -7 51 -39 -117 -.23 34 32 | 0 -53 1822 1887
cod 244| -3 1 -6 -5 -38 40 -.10 23 22 | --- --- --- ---
esx 130| 1 -3 -6 -15 52 98 .35 31 25 | 135405 983 5718 9233
iac n/a| 1 7 29 -34 27 -34 .15 38 38 | 486465 1026 5694 9698
mcc n/a| 12 -15 30 13 9 -1311 -.86 153 153 | --- --- --- ---
Table 2.1572.1 GPS week: 1572 Day: 1 MJD: 55249
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 130| 2 1 2 50 -13 -10 -.23 34 34 | 0 -88 1675 1753
cod 244| -1 -4 -2 -42 -23 -20 -.24 27 21 | --- --- --- ---
esx 130| 0 3 -8 37 101 83 .41 28 24 | 86580 -383 4054 9943
iac n/a| 0 0 12 -14 -45 -57 .07 41 41 | 435871 -3297 4075 10303
mcc n/a| 8 -7 60 -113 196 -1250 -.47 130 130 | --- --- --- ---
Table 2.1572.2 GPS week: 1572 Day: 2 MJD: 55250
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 130| 1 0 0 26 -54 48 -.25 36 31 | 0 -14 1490 1550
cod 244| 0 0 -4 -3 8 -13 -.18 15 14 | --- --- --- ---
esx 130| 0 3 -7 7 42 92 .31 25 23 | 58012 -495 3833 9296
iac n/a| 1 0 23 -7 -11 -179 .14 39 39 | 408075 96 3806 9101
mcc n/a| 23 4 37 -21 -174 -753 .61 122 122 | --- --- --- ---
Table 2.1572.3 GPS week: 1572 Day: 3 MJD: 55251
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 130| 1 0 1 -6 21 -123 -.17 23 23 | 0 92 1551 1660
cod 244| -1 1 -5 -5 -20 100 -.16 19 15 | --- --- --- ---
esx 130| -2 -1 -8 41 34 56 .31 22 20 | 58802 -1722 4232 8215
iac n/a| 0 2 27 -78 1 -69 .01 39 39 | 403828 406 4306 8428
mcc n/a| -14 15 19 7 28 -408 -.53 128 128 | --- --- --- ---
Table 2.1572.4 GPS week: 1572 Day: 4 MJD: 55252
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 130| 2 0 -1 -23 17 -130 -.21 25 25 | 0 -95 1836 1901
cod 244| 0 0 -3 -1 -53 82 -.23 18 14 | --- --- --- ---
esx 130| 1 0 -12 42 34 142 .38 32 28 | 140666 -220 5422 9753
iac n/a| -3 0 23 -59 29 -126 .14 44 44 | 484876 -1395 5537 10327
mcc n/a| -10 -24 18 154 51 40 -1.52 195 195 | --- --- --- ---
Table 2.1572.5 GPS week: 1572 Day: 5 MJD: 55253
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 130| 0 0 3 31 -19 -42 -.27 26 26 | 0 86 1692 1768
cod 244| -2 0 -5 8 -15 88 -.21 18 17 | --- --- --- ---
esx 130| 0 0 -4 -15 32 -50 .38 24 23 | 136635 6055 4156 7001
iac n/a| 1 -3 22 -14 47 -91 .08 50 50 | 479134 556 4279 7466
mcc n/a| 15 -30 47 122 -158 -1422 .28 205 205 | --- --- --- ---
Table 2.1572.6 GPS week: 1572 Day: 6 MJD: 55254
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 130| 2 2 0 -62 -79 -204 -.15 80 59 | 0 19 1638 1727
cod 244| -3 0 -3 13 -10 8 -.27 21 15 | --- --- --- ---
esx 130| 0 -1 -12 29 62 9 .33 26 22 | 137656 -5463 3510 7355
iac n/a| 2 -1 24 -34 37 22 .05 38 38 | 476686 -1944 3542 7619
mcc n/a| 18 5 59 80 -10 -2191 .71 242 242 | --- --- --- ---
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 3.1572.0 GPS week: 1572 Day: 0 MJD: 55248
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1282 27 17 7 38 --- 13 | 43 39 36 37 --- 33
R02 | 858 26 14 13 39 --- 13 | 30 36 43 33 --- 33
R03 | 654 27 23 18 30 --- 14 | 32 43 37 32 --- 33
R04 | 981 18 16 26 23 --- 12 | 31 41 34 22 --- 34
R05 | 867 15 23 18 41 --- 14 | 40 42 39 43 --- 34
R07 | 1853 13 30 26 36 --- 15 | 23 37 34 37 --- 26
R08 | 924 30 17 17 21 117 12 | 37 36 30 40 61 32
R10 | 2524 23 17 17 30 --- 12 | 28 24 24 28 --- 19
R11 | 2166 25 19 25 26 211 13 | 29 32 44 46 64 33
R13 | 1441 24 23 27 30 --- 15 | 22 41 37 38 --- 29
R14 | 1631 35 25 72 27 --- 26 | 29 31 71 34 --- 24
R15 | 4459 12 16 18 22 111 10 | 24 24 27 18 27 16
R17E | 963 49 44 28 41 --- 23 | 25 37 24 39 --- 25
R18E | 2265 30 23 26 41 --- 17 | 43 36 32 42 --- 27
R19E | 1704 73 21 47 47 --- 28 | 38 32 33 47 --- 28
R20E | 1136 41 29 46 64 --- 25 | 36 38 45 60 --- 28
R21E | 972 21 21 22 53 --- 17 | 30 23 30 48 --- 21
R23E | 6412 55 23 37 40 --- 22 | 51 46 56 58 --- 47
------+------------------------------------+--------------------------------
RMS | 2319 34 23 31 38 153 |T 32 35 37 39 50 29
WRMS | 2319 32 22 25 38 153 |NE 30 35 38 34 50 28
MEDI | 1282 26 21 25 36 117 |MD 30 36 34 38 61 28
Table 3.1572.1 GPS week: 1572 Day: 1 MJD: 55249
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 709 35 17 28 46 --- 18 | 41 31 44 29 --- 29
R02 | 1553 23 17 20 39 --- 14 | 32 34 42 22 --- 28
R03 | 806 22 22 23 38 --- 15 | 27 35 34 38 --- 29
XR04 |10287 --- 20 13 38 --- 16 | --- 25 36 20 --- 31
R05 | 1087 27 13 28 23 --- 13 | 27 28 53 27 --- 30
R07 | 1067 13 26 31 20 --- 14 | 16 24 34 21 --- 12
R08 | 1685 35 12 34 32 97 16 | 24 26 63 41 37 32
R10 | 1853 27 10 16 22 --- 10 | 15 16 31 24 --- 14
R11 | 1227 13 24 28 22 170 13 | 17 37 31 30 56 23
R13 | 2094 28 10 15 43 --- 14 | 21 23 30 26 --- 19
R14 | 1960 27 22 27 23 --- 14 | 27 27 47 34 --- 24
R15 | 4713 26 13 21 34 112 13 | 37 20 33 33 22 18
R17E | 1954 43 30 33 46 --- 21 | 26 22 36 40 --- 19
R18E | 2562 20 35 27 58 --- 20 | 32 46 35 39 --- 28
R19E | 623 63 29 20 46 --- 23 | 32 21 24 43 --- 21
R20E | 1619 58 71 41 66 --- 35 | 48 95 57 59 --- 51
R21E | 1305 25 18 25 46 --- 16 | 31 31 36 41 --- 21
R23E | 5462 41 26 42 52 --- 23 | 43 48 62 32 --- 37
------+------------------------------------+--------------------------------
RMS | 2288 34 27 28 41 130 |T 29 32 40 33 38 25
WRMS | 2288 34 21 24 41 130 |NE 25 27 39 28 38 24
MEDI | 1619 27 20 27 38 112 |MD 27 27 36 32 37 24
Table 3.1572.2 GPS week: 1572 Day: 2 MJD: 55250
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1549 36 13 26 24 --- 13 | 26 31 30 21 --- 23
R02 | 2787 38 10 13 42 --- 14 | 61 27 37 27 --- 30
R03 | 1294 10 15 22 46 --- 13 | 36 47 36 15 --- 33
R04 | 2526 58 16 19 52 --- 20 | 56 38 40 14 --- 36
R05 | 1180 32 16 18 34 --- 13 | 28 37 54 61 --- 40
R07 | 1790 22 10 28 20 --- 11 | 31 29 50 24 --- 31
R08 | 1398 22 16 34 24 83 14 | 33 30 48 42 33 30
R10 | 1610 30 23 22 33 --- 15 | 26 25 36 44 --- 24
R11 | 1403 17 10 27 26 170 11 | 22 17 35 26 40 18
R13 | 2495 22 11 24 37 --- 13 | 21 18 37 24 --- 21
R14 | 987 28 10 16 30 --- 11 | 30 29 33 23 --- 25
R15 | 2960 15 7 19 22 96 8 | 26 21 33 25 21 21
R17E | 2052 17 16 19 46 --- 13 | 40 31 34 40 --- 29
R18E | 1740 26 20 26 47 --- 16 | 38 31 40 50 --- 32
R19E | 1170 56 23 20 43 --- 19 | 36 21 25 40 --- 20
R20E | 1618 80 21 49 57 --- 28 | 46 42 43 45 --- 26
R21E | 2580 50 11 27 35 --- 17 | 26 22 42 47 --- 27
R23E | 4660 12 12 17 54 --- 14 | 42 36 45 48 --- 37
------+------------------------------------+--------------------------------
RMS | 2172 36 15 25 39 122 |T 34 29 38 34 31 27
WRMS | 2172 31 14 23 39 122 |NE 33 29 39 28 31 27
MEDI | 1618 26 13 22 35 96 |MD 31 29 37 27 33 27
Table 3.1572.3 GPS week: 1572 Day: 3 MJD: 55251
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1291 15 13 12 29 --- 9 | 29 41 39 26 --- 33
R02 | 3513 12 11 19 22 --- 9 | 32 41 57 31 --- 39
R03 | 1309 16 13 27 33 --- 12 | 47 43 59 28 --- 44
XR04 | 2236 16 17 23 --- --- 13 | 34 27 57 --- --- 31
R05 | 1943 19 19 13 30 --- 11 | 34 42 35 34 --- 31
R07 | 1896 17 10 10 20 --- 8 | 40 34 34 26 --- 31
R08 | 1143 6 17 19 20 143 9 | 21 33 30 27 51 24
R10 | 1563 30 20 24 32 --- 15 | 19 32 37 46 --- 24
R11 | 745 22 12 13 30 144 11 | 30 40 48 46 63 37
R13 | 1649 18 9 13 23 --- 9 | 27 27 29 27 --- 24
R14 | 1293 14 19 21 30 --- 12 | 44 36 34 42 --- 31
R15 | 2864 16 11 19 28 91 10 | 31 28 37 29 23 25
R17E | 1995 16 29 27 63 --- 19 | 23 39 36 44 --- 24
R18E | 2892 21 15 21 55 --- 15 | 43 33 41 45 --- 32
R19E | 1355 27 16 27 52 --- 17 | 31 20 33 53 --- 25
R20E | 1784 42 38 34 47 --- 23 | 33 44 65 57 --- 40
R21E | 2374 40 21 25 32 --- 17 | 30 33 39 39 --- 26
R23E | 4188 22 20 25 64 --- 18 | 40 42 40 55 --- 37
------+------------------------------------+--------------------------------
RMS | 2176 23 19 22 39 128 |T 32 35 41 38 45 31
WRMS | 2176 23 15 20 39 128 |NE 32 35 41 32 45 31
MEDI | 1784 17 16 21 30 143 |MD 31 34 37 39 51 31
Table 3.1572.4 GPS week: 1572 Day: 4 MJD: 55252
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 963 14 8 14 32 --- 9 | 35 40 38 30 --- 35
R02 | 2247 14 19 30 25 --- 12 | 32 37 34 23 --- 26
R03 | 703 19 14 16 25 --- 10 | 20 39 40 31 --- 29
XR04 | 2222 14 12 26 --- --- 12 | 25 28 42 --- --- 27
R05 | 1247 45 11 22 35 --- 17 | 21 39 50 29 --- 32
R07 | 2367 33 15 33 25 --- 15 | 21 32 63 50 --- 35
R08 | 762 16 11 15 18 166 8 | 22 30 36 34 43 26
R10 | 1617 36 31 86 24 --- 29 | 24 34 88 26 --- 24
R11 | 830 17 18 35 27 252 14 | 33 33 49 33 104 31
R13 | 801 16 14 19 21 --- 10 | 22 28 41 28 --- 26
R14 | 3372 11 10 12 14 --- 6 | 37 35 31 27 --- 31
R15 | 2403 12 13 11 27 152 9 | 33 28 31 40 69 29
R17E | 1666 22 20 29 62 --- 18 | 33 27 53 54 --- 33
R18E | 2573 24 19 27 71 --- 19 | 48 40 48 80 --- 43
R19E | 488 24 22 16 62 --- 17 | 30 24 22 48 --- 20
R20E | 1611 38 29 36 64 --- 23 | 34 37 39 63 --- 27
R21E | 1574 30 19 38 73 --- 22 | 34 26 42 61 --- 24
R23E | 2664 26 22 23 56 --- 17 | 31 38 39 54 --- 33
------+------------------------------------+--------------------------------
RMS | 1833 25 18 32 44 195 |T 29 33 43 41 72 29
WRMS | 1833 25 14 28 44 195 |NE 27 33 45 31 72 29
MEDI | 1611 19 15 23 27 166 |MD 31 33 40 34 69 29
Table 3.1572.5 GPS week: 1572 Day: 5 MJD: 55253
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2160 25 18 25 21 --- 13 | 19 47 53 29 --- 36
R02 | 1147 15 22 21 41 --- 13 | 32 49 36 16 --- 35
R03 | 1182 18 14 23 37 --- 12 | 35 48 44 30 --- 40
XR04 | 2290 20 18 20 --- --- 13 | 31 33 16 --- --- 20
R05 | 1992 30 16 23 52 --- 16 | 40 26 42 43 --- 31
R07 | 2054 32 19 14 35 --- 14 | 33 53 44 64 --- 43
R08 | 548 16 12 12 52 207 12 | 27 36 43 60 80 36
R10 | 1380 24 13 18 35 --- 12 | 32 20 40 21 --- 23
R11 | 1309 12 11 23 24 263 10 | 28 28 29 34 55 24
R13 | 1467 26 19 20 26 --- 12 | 40 36 39 28 --- 31
R14 | 4267 17 10 11 24 --- 8 | 58 30 28 32 --- 31
R15 | 2125 16 23 29 22 119 13 | 45 24 31 28 67 18
R17E | 1157 16 15 24 62 --- 15 | 18 25 27 56 --- 21
R18E | 2062 22 18 25 66 --- 17 | 39 36 43 55 --- 31
R19E | 867 19 17 25 78 --- 18 | 27 31 29 63 --- 22
R20E | 1490 39 25 27 82 --- 23 | 27 38 46 62 --- 29
R21E | 1131 21 21 24 66 --- 17 | 18 31 32 58 --- 20
R23E | 2191 53 23 48 68 --- 26 | 49 38 66 64 --- 43
------+------------------------------------+--------------------------------
RMS | 1863 26 18 24 50 205 |T 33 34 38 43 67 29
WRMS | 1863 26 17 23 50 205 |NE 35 35 37 35 67 30
MEDI | 1467 20 18 23 41 207 |MD 32 33 39 43 67 31
Table 3.1572.6 GPS week: 1572 Day: 6 MJD: 55254
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2476 33 12 9 26 --- 10 | 44 58 60 68 --- 56
R02 | 899 100 18 35 22 --- 23 | 58 51 71 33 --- 44
R03 | 995 103 19 34 37 --- 24 | 63 49 75 27 --- 49
XR04 | 2574 108 19 36 --- --- 32 | 49 44 39 --- --- 37
R05 | 1278 59 15 23 19 --- 15 | 51 49 41 38 --- 38
R07 | 2992 37 13 14 31 --- 12 | 36 61 64 50 --- 55
R08 | 762 28 12 12 32 234 11 | 45 46 36 33 50 38
R10 | 2292 28 13 21 28 --- 12 | 27 27 26 24 --- 20
R11 | 1482 31 17 23 29 301 13 | 28 33 47 48 82 33
R13 | 1714 24 12 18 26 --- 11 | 22 26 39 25 --- 25
R14 | 3885 76 10 17 23 --- 16 | 47 36 30 30 --- 30
R15 | 1731 171 17 29 24 173 33 | 52 36 32 47 35 34
R17E | 1557 43 17 26 41 --- 17 | 23 25 28 48 --- 27
R18E | 1565 108 26 32 61 --- 29 | 84 76 85 76 --- 73
R19E | 1559 117 38 24 55 --- 30 | 73 34 44 60 --- 37
R20E | 2329 104 37 39 63 --- 31 | 78 47 54 66 --- 50
R21E | 1652 55 20 27 45 --- 19 | 33 30 42 59 --- 32
R23E | 1458 67 32 30 45 --- 23 | 68 58 53 61 --- 56
------+------------------------------------+--------------------------------
RMS | 1958 80 21 26 38 242 |T 48 43 48 46 55 40
WRMS | 1958 59 15 22 38 242 |NE 43 43 46 38 55 38
MEDI | 1565 59 17 24 31 234 |MD 47 44 42 48 50 37
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