[IGSREPORT-16080] Wk 1470 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 27 05:23:25 PDT 2008
******************************************************************************
IGS Electronic Report 27 Mar 05:23:36 PDT 2008 Message Number 16080
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1470 (Mar 09, 2008 - Mar 15, 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 2.1470.
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:
igl1470[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1470 in the SP3 format.
igl14707.sum Combination Report for GPS Week 1470.
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 | 1207.4 ns
1 | 1221.6 ns
2 | 1187.6 ns
3 | 1136.7 ns
4 | 1223.1 ns
5 | 1128.0 ns
6 | 1197.8 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 | R09 R13
1 | ESX | R08 R13
2 | ESX | R09 R13
3 | ESX | R13
4 | ESX | R09 R23
5 | ESX | R09 R11
6 | ESX | R09 R11 R13
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 1.1470, 1a.1470).
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 2.1470.0-6)
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 3.1470.0-6).
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 1470 summary. (Mar 09, 2008 - Mar 15, 2008)
Table 1.1470.a GPS week : 1470 MJD: 54534.0-54540.0
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 66| 0 0 -1 8 11 -52 -.14 42 36 | 0 -38 2619 2742
| 3 2 5 22 35 253 .11 | 0 380
cod 178| -2 2 0 -12 -31 93 -.15 34 36 | --- --- --- ---
| 2 2 3 40 26 121 .05 | --- ---
esx 110| 1 -2 5 40 48 5 .23 3441 62 | -43013 1291 8732 20420
| 6 3 8 76 49 152 .12 | 37699 4645
iac n/a| 0 0 -1 -16 7 -96 .16 52 52 | 2397693 -4473 291621 297611
| 2 3 8 29 28 99 .11 | 2057008 6084
mcc n/a| -13 -11 24 11 -88 112 .42 321 321 | --- --- --- ---
| 21 16 36 192 233 868 .30 | --- ---
Table 1.1470.b GPS week : 1470 MJD: 54534.0-54540.0
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 | 16 19 20 21 21 11 20 |
R04 | 18 20 26 16 15 15 21 |
R06 | 20 18 19 24 22 18 18 |
R07 | 24 17 26 18 21 31 46 |
R08 | 38 29 50 19 46 77 92 |
R09 | 25 25 30 24 29 32 30 |
R10 | 17 18 19 20 15 20 31 |
R11 | 37 33 16 62 18 21 25 |
R13 | 27 26 24 29 27 23 23 |
R14 | 15 23 20 21 17 17 13 |
R15 | 16 26 28 38 22 21 19 |
R17E | 24 22 20 63 45 37 49 |
R19E | 32 23 22 29 33 28 42 |
R20E | 21 30 32 29 30 25 26 |
R23E | 26 30 30 54 56 64 55 |
R24E | 23 22 25 21 17 17 16 |
Table 1.1470.c GPS week : 1470 MJD: 54534.0-54540.0
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 1470 0 | 11 -81 362 7063 4181 -12530 99.0 7715 7715 | 1207391 0
brd 1470 1 | -115 244 258 -3186 -532 -5343 94.2 5521 5521 | 1221617 0
brd 1470 2 | 136 135 38 -794 936 -17220 94.3 4652 4652 | 1187644 0
brd 1470 3 | -65 -12 157 -1603 412 -24940 99.5 5962 5962 | 1136739 0
brd 1470 4 | 5 35 173 -4024 -1465 -22090 93.9 6638 6638 | 1223109 0
brd 1470 5 | 111 -37 648 4895 -2525 -26510 88.5 7718 7718 | 1127964 0
brd 1470 6 | -21 137 323 -1139 -454 -19830 99.4 8602 8602 | 1197808 0
-------------+------------------------------------------------------------+----------------
brd 1470 mean| 8 60 280 173 78 -18351 95.5 6686 6686 | 1186038 0
brd 1470 sdev| 90 116 195 4172 2140 7422 4.0 1403 1403 | 38816 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 2.1470.0 GPS week: 1470 Day: 0 MJD: 54534
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 66| -6 1 3 16 -37 173 -.12 31 30 | 0 14 2833 2926
cod 178| 0 0 6 57 22 -30 -.20 29 25 | --- --- --- ---
esx 110| 2 -4 0 -83 138 -90 .24 412 59 | -29438 -428 8367 25220
iac n/a| 0 2 -11 -15 29 -65 .19 45 45 | 1205884 -3516 7798 20581
mcc n/a| -54 -19 59 -240 -448 -765 .67 670 670 | --- --- --- ---
Table 2.1470.1 GPS week: 1470 Day: 1 MJD: 54535
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 66| 0 0 3 5 -27 71 .04 31 31 | 0 210 2745 2814
cod 178| -3 3 0 -28 -29 46 -.11 31 30 | --- --- --- ---
esx 110| 9 0 1 92 48 -111 .08 180 56 | -8676 4242 8248 20358
iac n/a| 1 -5 -11 -20 -1 -97 .27 51 51 | 1225299 -3701 7913 15347
mcc n/a| -19 12 -5 23 -255 -540 .28 343 343 | --- --- --- ---
Table 2.1470.2 GPS week: 1470 Day: 2 MJD: 54536
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 66| -3 0 4 26 50 -504 -.10 44 43 | 0 237 2481 2601
cod 178| 0 3 1 -17 -59 226 -.21 29 27 | --- --- --- ---
esx 110| 8 -5 -5 114 5 249 .46 5578 61 | -38214 389 11399 19211
iac n/a| -3 2 4 -38 49 103 .06 42 42 | 1188983 -1374 10458 17674
mcc n/a| -26 -36 -30 15 299 1615 .62 233 233 | --- --- --- ---
Table 2.1470.3 GPS week: 1470 Day: 3 MJD: 54537
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 66| 0 -1 0 -6 28 207 -.27 38 37 | 0 -325 2386 2444
cod 178| -2 3 0 -18 -26 -39 -.12 38 32 | --- --- --- ---
esx 110| 3 -6 11 62 71 -115 .20 397 59 | -89012 -7807 9305 19913
iac n/a| -3 0 -5 -41 -29 -138 .30 48 48 | 1134667 -1141 8884 13586
mcc n/a| -8 -6 56 338 -47 -426 .61 127 127 | --- --- --- ---
Table 2.1470.4 GPS week: 1470 Day: 4 MJD: 54538
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 66| 2 -4 -6 -7 22 2 -.19 38 28 | 0 -17 2550 2639
cod 178| -3 3 0 21 -46 37 -.19 37 44 | --- --- --- ---
esx 110| -8 2 16 -47 56 175 .16 9509 86 | -7745 3684 7323 22788
iac n/a| 2 -1 -1 -18 16 -155 .19 59 59 | 1219628 3677 6298 16092
mcc n/a| 8 -24 61 161 -143 -195 .58 194 194 | --- --- --- ---
Table 2.1470.5 GPS week: 1470 Day: 5 MJD: 54539
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 66| 0 1 -9 -20 47 -263 -.07 59 36 | 0 354 2322 2407
cod 178| -4 4 -4 -67 -50 149 -.08 29 26 | --- --- --- ---
esx 110| 0 1 12 93 -13 38 .30 4663 53 | -102085 2465 6996 17074
iac n/a| 1 -5 8 46 9 -109 .04 54 54 | 5225004 -13090 999999 999999
mcc n/a| 2 -10 20 -93 29 161 .37 317 317 | --- --- --- ---
Table 2.1470.6 GPS week: 1470 Day: 6 MJD: 54540
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 66| 3 -1 -6 47 -5 -57 -.26 55 45 | 0 -739 3022 3364
cod 178| -2 0 0 -35 -31 263 -.15 44 66 | --- --- --- ---
esx 110| -2 -4 2 54 31 -109 .18 3350 57 | -25921 6498 9490 18380
iac n/a| 3 3 6 -24 -22 -212 .03 64 64 | 5584390 -12170 999999 999999
mcc n/a| 2 2 7 -125 -52 937 -.18 364 364 | --- --- --- ---
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 3.1470.0 GPS week: 1470 Day: 0 MJD: 54534
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5395 19 25 37 32 --- 15 | 37 60 50 26 --- 36
R04 | 4758 22 19 53 41 --- 18 | 47 68 69 51 --- 50
R06 | 2100 27 30 55 32 --- 19 | 38 53 49 60 --- 41
R07 | 9459 20 42 84 24 274 24 | 25 41 43 31 114 27
R08 | 6458 42 32 156 50 --- 38 | 45 66 168 24 --- 33
R09 |13522 41 31 1548 33 --- 25 | 57 40 9999 35 --- 37
R10 | 1383 32 25 37 26 --- 17 | 42 47 53 44 --- 40
R11 |10402 33 38 141 62 --- 36 | 41 39 773 64 --- 42
R13 |12845 28 38 485 45 --- 26 | 26 52 9999 36 --- 30
R14 | 2917 29 18 36 20 --- 14 | 32 43 46 47 --- 35
R15 | 7056 25 18 51 25 472 15 | 37 38 66 29 65 32
R17E |10913 39 25 84 33 --- 24 | 36 53 113 70 --- 50
R19E | 2080 28 36 65 88 --- 31 | 49 52 45 58 --- 45
R20E | 2088 26 23 53 53 --- 21 | 80 75 71 93 --- 73
R23E | 5702 39 25 91 39 --- 26 | 38 53 9999 66 --- 46
R24E | 9402 31 25 39 63 1025 23 | 53 52 58 84 168 54
------+------------------------------------+--------------------------------
RMS | 7715 31 29 412 45 670 |T 42 52 123 51 115 41
WRMS | 7715 30 25 59 45 670 |NE 38 49 146 40 89 36
MEDI | 5702 28 25 55 33 472 |MD 38 52 58 47 114 40
Table 3.1470.1 GPS week: 1470 Day: 1 MJD: 54535
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5015 29 22 52 32 --- 19 | 50 35 69 22 --- 33
R04 | 3355 26 34 30 45 --- 19 | 45 55 52 25 --- 36
R06 | 1340 22 26 38 44 --- 18 | 39 37 55 49 --- 33
R07 | 5541 25 28 40 30 177 17 | 55 40 53 26 74 33
R08 | 5617 38 46 573 31 --- 28 | 26 79 236 38 --- 50
R09 | 8898 24 36 48 69 --- 24 | 42 61 981 43 --- 36
R10 | 1683 24 34 35 33 --- 18 | 54 50 42 43 --- 41
R11 | 3200 19 38 120 47 --- 33 | 29 38 750 44 --- 21
R13 | 8778 38 35 370 38 --- 26 | 34 55 9999 39 --- 36
R14 | 1923 35 33 59 37 --- 23 | 30 68 44 54 --- 39
R15 | 5749 27 28 91 33 320 26 | 40 46 102 43 41 38
R17E |11150 32 25 65 38 --- 22 | 45 63 117 58 --- 58
R19E | 1749 38 21 47 56 --- 22 | 33 32 57 63 --- 32
R20E | 1285 35 25 44 99 --- 30 | 59 54 75 44 --- 52
R23E | 1840 50 22 88 50 --- 29 | 50 42 9999 69 --- 44
R24E | 6982 25 22 25 73 469 21 | 49 59 51 81 143 52
------+------------------------------------+--------------------------------
RMS | 5521 31 31 180 51 343 |T 42 50 191 46 86 39
WRMS | 5521 31 30 56 51 343 |NE 40 51 238 38 57 36
MEDI | 3355 27 28 48 38 320 |MD 42 50 57 43 74 36
Table 3.1470.2 GPS week: 1470 Day: 2 MJD: 54536
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4266 51 21 34 33 --- 20 | 48 41 43 18 --- 26
R04 | 4418 42 24 56 61 --- 25 | 66 29 61 34 --- 26
R06 | 2203 29 27 44 38 --- 19 | 78 46 56 59 --- 51
R07 | 2047 62 45 34 26 136 26 | 49 74 57 34 164 39
R08 | 4242 71 29 214 34 --- 49 | 54 42 163 36 --- 37
R09 |10144 56 43 3909 24 --- 30 | 65 64 9999 37 --- 43
R10 | 1349 27 29 42 39 --- 19 | 48 47 63 49 --- 40
R11 | 3937 31 11 51 21 --- 15 | 55 44 540 54 --- 43
R13 | 7385 51 23 >>>> 28 --- 24 | 25 47 9999 56 --- 36
R14 | 1911 24 25 70 25 --- 19 | 59 51 34 46 --- 40
R15 | 2887 24 31 111 31 253 27 | 44 44 100 54 113 35
R17E | 7528 29 21 60 37 --- 19 | 36 45 71 50 --- 23
XR19E | 1490 31 25 --- 37 --- 21 | 36 53 --- 59 --- 42
R20E | 2048 50 34 74 71 --- 31 | 39 39 76 70 --- 37
R23E | 1773 43 27 97 54 --- 29 | 63 60 9999 79 --- 56
R24E | 3019 37 25 50 62 283 24 | 76 55 60 75 234 59
------+------------------------------------+--------------------------------
RMS | 4652 44 29 5577 42 233 |T 52 48 110 50 170 39
WRMS | 4652 43 27 61 42 233 |NE 53 48 124 43 138 37
MEDI | 2887 37 25 60 34 253 |MD 49 46 61 50 164 39
Table 3.1470.3 GPS week: 1470 Day: 3 MJD: 54537
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5298 39 34 30 36 --- 21 | 34 45 36 37 --- 28
R04 | 7496 18 23 51 31 --- 16 | 52 42 38 39 --- 32
R06 | 2200 25 23 77 53 --- 23 | 38 44 66 73 --- 38
R07 | 2958 25 26 34 39 104 17 | 41 88 51 41 87 53
R08 | 5577 24 34 54 31 --- 19 | 72 41 103 41 --- 23
R09 |11803 31 27 72 50 --- 23 | 33 55 9999 78 --- 46
R10 | 1910 20 31 66 35 --- 20 | 38 44 55 67 --- 43
R11 | 6500 59 31 309 47 --- 61 | 36 55 758 48 --- 49
R13 | 9197 31 46 1439 44 --- 29 | 26 52 9999 39 --- 27
R14 | 2082 18 39 50 41 --- 20 | 26 57 48 20 --- 25
R15 | 4908 31 32 185 36 106 38 | 38 46 161 42 112 36
R17E | 9589 53 79 289 54 --- 63 | 43 109 291 63 --- 70
XR19E | 2007 30 24 --- 62 --- 28 | 59 39 --- 56 --- 42
R20E | 1923 39 34 79 62 --- 28 | 68 72 92 87 --- 61
R23E | 1234 73 47 219 78 --- 53 | 49 57 9999 90 --- 51
R24E | 2970 28 22 41 56 161 21 | 47 42 47 47 284 36
------+------------------------------------+--------------------------------
RMS | 5962 38 38 397 48 127 |T 43 55 145 54 161 41
WRMS | 5962 37 32 59 48 127 |NE 39 51 146 47 99 36
MEDI | 2970 30 31 72 44 106 |MD 38 46 55 47 112 38
Table 3.1470.4 GPS week: 1470 Day: 4 MJD: 54538
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5687 22 29 66 34 --- 21 | 24 21 55 41 --- 15
R04 | 9800 15 28 28 30 --- 14 | 28 45 34 24 --- 23
R06 | 4397 26 20 70 36 --- 21 | 45 59 73 74 --- 51
R07 | 4098 30 31 53 39 83 21 | 29 45 58 32 40 23
R08 | 7225 92 56 113 48 --- 45 | 99 22 148 34 --- 53
R09 | 9029 43 41 1883 37 --- 29 | 51 59 9999 76 --- 45
R10 | 1715 25 26 35 20 --- 15 | 23 44 53 25 --- 29
R11 | 5627 21 18 43 48 --- 18 | 27 30 9999 78 --- 38
R13 | 7034 30 41 82 40 --- 27 | 43 53 9999 39 --- 36
R14 | 1826 27 25 28 37 --- 16 | 15 33 41 23 --- 16
R15 | 9902 20 31 46 54 145 21 | 39 40 85 32 44 35
R17E | 8619 36 40 89 136 --- 44 | 43 50 134 98 --- 40
XR19E | 1480 36 33 --- 71 --- 32 | 41 56 --- 75 --- 43
R20E | 2097 24 40 92 53 --- 29 | 52 85 81 78 --- 63
R23E | 9881 60 69 >>>> 113 --- 56 | 42 44 9999 115 --- 42
R24E | 896 18 19 39 44 291 17 | 44 38 48 41 127 35
------+------------------------------------+--------------------------------
RMS | 6637 38 37 9509 59 194 |T 40 45 73 55 70 36
WRMS | 6637 28 44 86 59 194 |NE 38 41 68 43 42 33
MEDI | 5627 26 31 66 40 145 |MD 41 44 58 41 44 36
Table 3.1470.5 GPS week: 1470 Day: 5 MJD: 54539
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4548 24 13 19 20 --- 10 | 30 27 56 25 --- 23
R04 | 8907 34 13 35 25 --- 14 | 52 39 44 18 --- 34
R06 |10378 20 22 46 38 --- 17 | 29 36 58 34 --- 30
R07 | 3035 46 53 58 55 73 30 | 40 67 68 29 49 33
R08 | 8611 187 53 226 71 --- 77 | 158 19 222 31 --- 58
R09 |11238 46 18 >>>> 71 --- 31 | 29 21 9999 82 --- 28
R10 | 1648 37 20 42 45 --- 19 | 40 30 65 45 --- 31
R11 | 6966 26 21 424 44 --- 21 | 23 26 9999 55 --- 19
R13 |12960 36 28 63 42 --- 23 | 23 46 9999 41 --- 28
R14 | 1465 35 11 41 36 --- 17 | 27 26 49 30 --- 20
R15 | 6438 12 18 55 54 90 20 | 19 30 67 38 45 23
R17E |12200 44 46 67 98 --- 36 | 35 52 81 91 --- 39
XR19E | 1590 48 29 --- 44 --- 27 | 66 53 --- 55 --- 51
R20E | 1705 30 27 66 57 --- 24 | 92 58 96 96 --- 75
XR23E | 2611 99 80 --- 99 --- 64 | 97 89 --- 87 --- 68
R24E | 1359 26 20 32 42 537 17 | 27 41 41 46 108 30
------+------------------------------------+--------------------------------
RMS | 7717 59 29 4663 54 317 |T 49 41 77 50 67 36
WRMS | 7717 36 26 53 54 317 |NE 42 33 78 38 47 29
MEDI | 4548 35 21 55 44 90 |MD 30 36 65 41 49 30
Table 3.1470.6 GPS week: 1470 Day: 6 MJD: 54540
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4596 37 32 41 31 --- 20 | 28 42 50 28 --- 28
R04 | 5150 41 26 46 33 --- 20 | 55 27 31 28 --- 24
R06 | 9517 32 17 26 44 --- 17 | 40 58 63 73 --- 53
R07 | 2957 73 64 107 80 83 45 | 48 73 91 47 51 36
R08 | 9918 133 115 276 119 --- 91 | 73 32 199 31 --- 29
R09 |14993 49 25 402 51 --- 29 | 51 32 9999 53 --- 32
R10 | 1110 60 36 80 41 --- 30 | 25 54 58 47 --- 34
R11 |11022 27 22 >>>> 54 --- 24 | 27 31 9999 85 --- 38
R13 | 8351 31 34 1605 28 --- 22 | 19 54 9999 23 --- 26
R14 | 1358 25 19 21 26 --- 13 | 19 39 28 16 --- 22
R15 |13123 23 17 57 32 52 18 | 37 38 46 20 55 28
R17E |13904 69 43 93 131 --- 48 | 41 30 123 92 --- 42
XR19E | 1090 71 31 --- 74 --- 41 | 69 47 --- 69 --- 43
R20E | 1830 33 33 51 62 --- 25 | 95 80 74 101 --- 83
XR23E | 5698 66 82 --- 86 --- 55 | 69 88 --- 59 --- 50
R24E | 1596 21 20 30 40 624 16 | 43 37 53 60 172 42
------+------------------------------------+--------------------------------
RMS | 8602 55 44 3349 64 364 |T 46 47 74 52 92 38
WRMS | 8602 45 66 57 64 364 |NE 38 43 70 41 53 31
MEDI | 5150 37 31 57 44 83 |MD 41 39 58 47 55 34
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