[IGSREPORT-16262] Wk 1478 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu May 22 08:44:43 PDT 2008
******************************************************************************
IGS Electronic Report 22 May 08:44:51 PDT 2008 Message Number 16262
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1478 (May 04, 2008 - May 10, 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 2.1478.
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:
igl1478[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1478 in the SP3 format.
igl14787.sum Combination Report for GPS Week 1478.
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 | 1016.1 ns
1 | 936.5 ns
2 | 949.4 ns
3 | 1013.1 ns
4 | 1016.9 ns
5 | 1013.6 ns
6 | 927.5 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 | R06 R08
1 | ESX | R08 R13
1 | IAC | R01
2 | ESX | R07 R13
2 | IAC | R01
3 | COD | R01
3 | ESX | R09 R15
4 | ESX | R09 R19
6 | ESX | R09
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 1.1478, 1a.1478).
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 2.1478.0-6)
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 3.1478.0-6).
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 1478 summary. (May 04, 2008 - May 10, 2008)
Table 1.1478.a GPS week : 1478 MJD: 54590.0-54596.0
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 67| 2 -1 -6 18 28 35 -.06 34 31 | 0 229 3411 3595
| 2 3 4 54 29 110 .04 | 0 305
cod 206| -6 0 -4 -43 1 22 -.09 34 31 | --- --- --- ---
| 2 4 2 59 48 69 .04 | --- ---
esx 114| 0 2 3 -2 -72 65 .37 420 1105 | -18083 3678 13177 29013
| 2 3 5 46 73 89 .10 | 36577 9764
iac n/a| 4 0 8 3 9 -83 -.03 36 36 | 982801 2828 14507 31372
| 2 4 2 31 32 108 .09 | 39632 13922
mcc n/a| 2 -9 24 -86 21 292 .34 233 233 | --- --- --- ---
| 16 17 33 236 352 1290 .96 | --- ---
Table 1.1478.b GPS week : 1478 MJD: 54590.0-54596.0
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 | 68 532 467 210 77 35 23 |
R04 | 17 14 14 25 16 18 16 |
R06 | 19 30 26 42 26 20 38 |
R07 | 21 22 14 37 35 76 90 |
R08 | 14 16 35 22 22 41 32 |
R09 | 22 28 26 31 25 21 20 |
R10 | 18 19 16 17 14 14 17 |
R11 | 22 23 25 19 22 23 18 |
R13 | 19 19 21 20 27 20 18 |
R14 | 13 11 14 20 16 17 17 |
R15 | 17 17 21 18 27 23 20 |
R17 | 36 28 31 27 16 23 17 |
R19 | 21 22 28 25 16 21 16 |
R20 | 22 14 16 15 13 18 14 |
R23 | 21 29 28 20 23 24 17 |
R24 | 17 22 31 23 26 19 12 |
Table 1.1478.c GPS week : 1478 MJD: 54590.0-54596.0
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 1478 0 | -27 479 471 -5411 4462 -31050 96.5 5469 5469 | 1016135 0
brd 1478 1 | 21 270 412 -4106 -466 -27530 91.0 >>>>> >>>>> | 936465 0
brd 1478 2 | 209 11 374 -5362 -1649 -9326 95.8 7660 7660 | 949406 0
brd 1478 3 | 4 138 230 -1761 2790 -12500 98.6 5618 5618 | 1013099 0
brd 1478 4 | -30 189 275 -2376 -470 -4207 97.3 9121 9121 | 1016941 0
brd 1478 5 | 157 -77 115 -4945 4364 -6092 95.1 6099 6099 | 1013558 0
brd 1478 6 | -112 14 389 146 591 -10590 101.1 7210 7210 | 927451 0
-------------+------------------------------------------------------------+----------------
brd 1478 mean| 31 146 324 -3402 1374 -14470 96.5 >>>>> >>>>> | 981865 0
brd 1478 sdev| 112 189 123 2124 2483 10538 3.1 >>>>> >>>>> | 41754 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 2.1478.0 GPS week: 1478 Day: 0 MJD: 54590
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 67| 2 0 -6 -12 11 110 -.14 32 30 | 0 45 2718 2860
cod 206| -4 -5 -3 1 -58 43 -.14 29 28 | --- --- --- ---
esx 114| -2 0 0 -21 57 -79 .45 2300 7416 | 9090 18185 21927 30599
iac n/a| 2 3 11 -7 21 -66 -.02 40 40 | 1019314 31504 31698 60837
mcc n/a| 2 0 31 0 -224 1343 -.18 235 235 | --- --- --- ---
Table 2.1478.1 GPS week: 1478 Day: 1 MJD: 54591
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 67| -2 -1 1 26 66 88 -.03 34 30 | 0 -337 5942 6358
cod 206| 0 -1 -1 -86 -18 15 -.05 35 30 | --- --- --- ---
esx 114| 1 3 -6 -19 -24 136 .40 73 44 | -54291 3343 13871 48209
iac n/a| 3 -1 4 22 -11 -144 -.06 35 35 | 945672 509 14039 48714
mcc n/a| 14 -8 33 -207 -101 1108 .24 211 211 | --- --- --- ---
Table 2.1478.2 GPS week: 1478 Day: 2 MJD: 54592
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 67| 6 -8 -8 110 37 145 -.08 39 31 | 0 422 2824 2909
cod 206| -6 6 -7 -130 81 -57 -.01 37 38 | --- --- --- ---
esx 114| 1 5 9 49 -130 167 .21 73 51 | -47643 3895 12163 21610
iac n/a| 4 -8 5 21 -1 -232 -.13 38 38 | 949470 -3138 12880 16577
mcc n/a| 8 -7 -31 278 380 -1447 .73 253 253 | --- --- --- ---
Table 2.1478.3 GPS week: 1478 Day: 3 MJD: 54593
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 67| 1 0 -9 1 35 -86 -.02 33 29 | 0 560 3016 3147
cod 206| -9 -1 -7 -19 37 161 -.10 41 31 | --- --- --- ---
esx 114| 3 7 9 6 -145 148 .25 283 70 | 14101 -1204 8150 22201
iac n/a| 4 0 9 -17 -29 -94 -.13 38 38 | 1017728 -4335 8161 21791
mcc n/a| 27 -21 49 -320 496 370 1.45 206 206 | --- --- --- ---
Table 2.1478.4 GPS week: 1478 Day: 4 MJD: 54594
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 67| 3 -2 -10 47 20 -82 -.08 36 35 | 0 346 3376 3489
cod 206| -6 -3 -2 -82 -15 17 -.11 35 32 | --- --- --- ---
esx 114| 2 4 6 51 -109 37 .48 85 56 | 15544 -7171 9510 24398
iac n/a| 1 0 6 55 67 22 -.08 31 31 | 1014359 -1557 7737 20046
mcc n/a| -18 18 70 -292 197 -1625 1.44 294 294 | --- --- --- ---
Table 2.1478.5 GPS week: 1478 Day: 5 MJD: 54595
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 67| 5 1 -5 20 49 147 -.06 25 25 | 0 147 2600 2816
cod 206| -7 2 -3 -34 -36 -27 -.11 38 34 | --- --- --- ---
esx 114| -4 -2 7 -83 -117 32 .37 63 55 | 4136 14818 14351 29147
iac n/a| 3 2 9 -14 -6 -154 .10 36 36 | 1004325 8156 14509 26865
mcc n/a| -18 -9 14 -225 -103 993 -.06 197 197 | --- --- --- ---
Table 2.1478.6 GPS week: 1478 Day: 6 MJD: 54596
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 67| 0 0 -5 -67 -24 -71 -.05 37 35 | 0 421 3403 3589
cod 206| -7 -3 -3 43 25 4 -.08 25 21 | --- --- --- ---
esx 114| 1 0 0 -1 -35 17 .41 62 43 | -67521 -6114 12267 26927
iac n/a| 10 3 11 -36 29 83 .07 35 35 | 928740 -11343 12528 24778
mcc n/a| 0 -38 0 165 -497 1307 -1.25 235 235 | --- --- --- ---
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 3.1478.0 GPS week: 1478 Day: 0 MJD: 54590
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 4954 60 100 --- 120 --- 67 | 222 331 --- 9999 --- 233
R04 | 4004 29 16 43 29 --- 17 | 33 56 73 50 --- 49
R06 |13123 27 25 8903 30 --- 19 | 93 105 9999 125 --- 103
R07 | 1877 33 25 54 27 143 20 | 45 49 45 53 75 43
R08 | 4892 19 19 162 20 --- 14 | 31 31 142 38 --- 29
R09 | 4912 27 37 43 45 --- 22 | 44 64 151 57 --- 52
R10 | 4823 39 24 37 19 --- 18 | 34 31 43 45 --- 33
R11 | 6623 37 26 40 49 --- 22 | 43 48 46 34 --- 36
R13 | 4750 33 23 33 41 --- 19 | 47 53 68 45 --- 50
R14 | 2763 18 10 35 24 --- 13 | 29 27 34 27 --- 25
R15 | 2856 25 19 39 32 289 16 | 55 52 48 74 81 55
R17 | 1970 65 38 46 93 --- 36 | 66 64 62 81 --- 48
R19 | 5128 24 45 37 33 --- 20 | 27 58 71 35 --- 35
R20 | 1978 21 37 56 31 --- 21 | 31 47 66 28 --- 30
R23 | 7039 20 45 27 47 --- 21 | 36 39 60 42 --- 37
R24 | 4422 37 19 35 27 248 17 | 146 154 161 161 100 153
------+------------------------------------+--------------------------------
RMS | 5468 32 29 2299 40 235 |T 61 75 76 59 85 63
WRMS | 5468 30 28 7415 40 235 |NE 61 75 76 59 85 63
MEDI | 4750 27 25 40 31 248 |MD 43 52 62 45 81 43
Table 3.1478.1 GPS week: 1478 Day: 1 MJD: 54591
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |>>>>> 553 510 --- 3394 --- 531 | 651 532 --- 9999 --- 420
R04 |>>>>> 35 20 17 20 --- 14 | 37 58 50 71 --- 51
R06 |>>>>> 59 28 78 31 --- 29 | 107 144 9999 112 --- 124
R07 | 2818 38 43 47 18 76 21 | 41 53 73 38 39 32
R08 |>>>>> 15 26 203 23 --- 15 | 23 35 141 24 --- 26
R09 |>>>>> 37 59 30 56 --- 28 | 67 90 235 81 --- 76
R10 |>>>>> 39 40 21 26 --- 19 | 32 36 42 33 --- 31
R11 |>>>>> 28 34 53 42 --- 23 | 44 57 88 55 --- 52
R13 |>>>>> 22 33 122 22 --- 18 | 67 54 126 67 --- 56
R14 |>>>>> 12 16 26 18 --- 10 | 30 25 38 31 --- 25
R15 |>>>>> 11 27 41 29 270 16 | 38 43 44 52 86 37
R17 |>>>>> 42 47 32 61 --- 27 | 24 68 61 45 --- 36
R19 |>>>>> 17 28 59 38 --- 21 | 19 20 74 54 --- 28
R20 |>>>>> 20 12 37 21 --- 13 | 14 30 56 34 --- 27
R23 |>>>>> 54 54 39 50 --- 29 | 52 35 40 39 --- 31
R24 |>>>>> 40 30 51 32 235 22 | 101 137 150 133 70 125
------+------------------------------------+--------------------------------
RMS |>>>>> 34 35 73 35 211 |T 84 88 87 57 65 73
WRMS |>>>>> 30 30 44 35 211 |NE 84 88 87 57 65 73
MEDI |>>>>> 35 30 41 29 235 |MD 38 53 61 52 70 36
Table 3.1478.2 GPS week: 1478 Day: 2 MJD: 54592
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |17554 494 441 --- >>>> --- 467 | 729 803 --- 9999 --- 587
R04 | 2448 22 30 24 21 --- 14 | 32 53 51 28 --- 36
R06 |11072 65 39 43 26 --- 26 | 67 65 983 56 --- 48
R07 | 1670 18 21 152 18 132 13 | 35 37 96 29 67 23
R08 | 5121 33 56 98 41 --- 34 | 34 26 157 44 --- 36
R09 |17261 38 47 45 45 --- 25 | 51 70 171 73 --- 62
R10 | 3109 36 25 22 26 --- 16 | 38 38 46 54 --- 40
R11 | 7034 39 38 46 47 --- 24 | 50 53 74 59 --- 47
R13 | 9636 34 19 144 33 --- 20 | 44 39 116 43 --- 36
R14 | 4136 17 25 33 20 --- 14 | 29 42 33 24 --- 22
R15 |11893 29 21 54 35 184 20 | 51 56 100 72 74 60
R17 | 5765 43 41 74 58 --- 31 | 47 72 95 71 --- 56
R19 | 4474 31 41 81 31 --- 28 | 36 30 73 58 --- 45
R20 | 1954 24 29 38 17 --- 16 | 43 28 66 34 --- 35
R23 | 3674 25 64 22 59 --- 27 | 58 79 63 34 --- 50
R24 | 6582 78 21 43 54 375 30 | 120 93 100 78 168 89
------+------------------------------------+--------------------------------
RMS | 7659 39 37 73 38 253 |T 91 99 148 50 103 79
WRMS | 7659 31 38 51 38 253 |NE 91 99 148 50 103 79
MEDI | 5121 33 30 45 33 184 |MD 44 53 95 54 74 45
Table 3.1478.3 GPS week: 1478 Day: 3 MJD: 54593
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |26903 124 902 --- 275 --- 209 | 250 898 --- 9999 --- 313
R04 | 1289 19 42 66 49 --- 25 | 45 54 90 85 --- 57
R06 | 8627 70 78 79 68 --- 42 | 78 177 435 124 --- 118
R07 | 1543 20 82 104 44 106 36 | 33 88 85 44 82 35
R08 | 6537 24 39 60 32 --- 21 | 46 48 99 49 --- 41
R09 |13192 45 39 1065 46 --- 31 | 71 77 988 80 --- 74
R10 | 1916 23 26 38 31 --- 16 | 34 42 52 38 --- 30
R11 | 6481 32 27 46 32 --- 19 | 45 44 61 53 --- 40
R13 | 6691 31 32 40 37 --- 20 | 59 64 78 88 --- 62
R14 | 2768 17 22 75 23 --- 20 | 28 44 63 31 --- 28
R15 | 5368 22 24 118 28 151 17 | 59 40 110 66 124 52
R17 | 4968 38 39 83 28 --- 26 | 27 42 94 36 --- 25
R19 | 2672 31 26 87 27 --- 24 | 32 37 55 29 --- 26
R20 | 1261 28 25 32 16 --- 14 | 29 35 29 26 --- 17
R23 | 3199 28 26 49 37 --- 19 | 25 43 69 41 --- 26
R24 | 2763 37 37 51 37 306 23 | 138 152 150 190 125 155
------+------------------------------------+--------------------------------
RMS | 5618 33 41 283 38 206 |T 62 117 163 65 110 68
WRMS | 5618 29 31 70 38 206 |NE 62 117 163 65 110 68
MEDI | 3199 28 32 66 32 151 |MD 45 44 85 49 124 40
Table 3.1478.4 GPS week: 1478 Day: 4 MJD: 54594
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |10551 82 72 --- --- --- 77 | 100 274 --- --- --- 83
R04 | 1426 30 28 36 19 --- 16 | 24 33 52 42 --- 29
R06 | 4331 49 43 54 37 --- 26 | 63 65 348 85 --- 60
R07 | 7476 58 77 55 42 230 34 | 33 95 84 77 41 51
R08 | 5990 25 35 69 28 --- 22 | 28 50 66 41 --- 30
R09 |15809 42 26 198 34 --- 24 | 64 65 285 65 --- 62
R10 | 3572 25 22 36 19 --- 14 | 39 48 46 34 --- 36
R11 |19048 31 21 73 24 --- 21 | 50 63 98 60 --- 50
R13 |14279 48 54 49 37 --- 27 | 35 52 49 39 --- 29
R14 | 1749 19 33 32 27 --- 16 | 22 40 35 29 --- 21
R15 |10928 32 25 90 41 111 27 | 36 29 103 69 50 45
R17 |10433 29 26 40 16 --- 15 | 39 53 54 52 --- 38
R19 | 6189 19 20 169 24 --- 15 | 23 41 121 48 --- 40
R20 | 5366 16 18 38 20 --- 13 | 27 28 39 21 --- 21
R23 | 1150 47 17 66 25 --- 22 | 44 58 70 38 --- 37
R24 | 2476 41 30 62 50 441 26 | 136 154 147 180 73 152
------+------------------------------------+--------------------------------
RMS | 9121 36 35 85 31 294 |T 47 71 106 58 54 49
WRMS | 9121 35 32 56 31 294 |NE 47 71 106 58 54 49
MEDI | 5990 31 26 55 27 230 |MD 36 52 70 48 50 38
Table 3.1478.5 GPS week: 1478 Day: 5 MJD: 54595
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 3174 24 50 --- 68 --- 34 | 77 161 --- 9999 --- 44
R04 | 2183 24 33 35 35 --- 18 | 30 45 47 39 --- 33
R06 | 2749 16 43 40 40 --- 20 | 42 63 411 32 --- 37
XR07 | ---- 92 118 --- 115 395 76 | 51 134 --- 174 75 102
R08 | 3916 24 91 125 45 --- 40 | 46 63 63 51 --- 24
R09 | 8142 27 20 73 26 --- 20 | 34 41 116 46 --- 31
R10 | 3434 18 23 42 17 --- 14 | 30 29 58 38 --- 28
R11 | 5582 23 29 77 38 --- 23 | 26 38 82 47 --- 35
R13 |15828 25 29 53 39 --- 20 | 42 37 77 53 --- 36
R14 | 1808 19 37 40 22 --- 16 | 21 43 46 34 --- 23
R15 | 5030 26 25 40 58 197 22 | 27 40 56 79 67 40
R17 | 6990 25 22 83 34 --- 23 | 22 28 98 50 --- 32
R19 | 5476 36 27 53 34 --- 21 | 32 42 70 69 --- 42
R20 | 4754 14 20 64 28 --- 17 | 32 20 64 23 --- 22
R23 | 1329 40 41 58 29 --- 23 | 16 64 70 30 --- 29
R24 | 1201 24 35 41 34 --- 18 | 222 192 225 200 --- 206
------+------------------------------------+--------------------------------
RMS | 6098 25 38 63 36 197 |T 46 65 105 64 71 47
WRMS | 6098 25 34 55 36 197 |NE 46 65 105 64 71 47
MEDI | 3916 24 29 53 34 197 |MD 32 42 70 47 67 33
Table 3.1478.6 GPS week: 1478 Day: 6 MJD: 54596
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 3263 34 26 --- 40 --- 23 | 92 107 --- 9999 --- 64
R04 | 1596 28 19 36 31 --- 16 | 36 32 55 46 --- 37
R06 | 3417 83 38 102 40 --- 38 | 135 77 415 129 --- 93
XR07 | ---- 78 138 --- 147 --- 90 | 68 58 --- 125 --- 66
R08 | 3484 63 47 57 57 --- 32 | 42 68 43 55 --- 39
R09 | 9275 29 22 158 34 --- 20 | 33 38 145 41 --- 33
R10 | 5246 25 30 27 35 --- 17 | 45 50 46 50 --- 44
R11 |12020 23 19 47 35 --- 17 | 48 40 41 52 --- 39
R13 |17728 30 26 43 30 --- 18 | 51 55 55 48 --- 45
R14 | 3480 26 18 33 37 --- 16 | 34 36 60 27 --- 33
R15 | 8931 38 21 33 45 235 20 | 42 49 63 69 66 50
R17 | 3503 29 17 36 34 --- 16 | 29 40 83 59 --- 43
R19 | 2542 28 23 42 22 --- 16 | 51 54 86 57 --- 54
R20 | 3127 23 17 27 29 --- 13 | 24 28 54 46 --- 31
R23 | 2632 16 14 48 33 --- 16 | 27 37 58 28 --- 25
R24 | 1348 19 19 27 15 --- 11 | 221 212 220 223 --- 218
------+------------------------------------+--------------------------------
RMS | 7210 37 25 62 35 235 |T 61 61 101 70 66 57
WRMS | 7210 35 21 43 35 235 |NE 61 61 101 70 66 57
MEDI | 3480 28 21 36 34 235 |MD 42 49 58 52 66 43
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