[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: May 21st 2013

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 29062 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2013/140/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4096210
22                 A    =         6798690
47  meter
 Y    =       -5049224
92  meter          E    =           
0013821
 Z    =       -1957272
03                 I    =           51
34015
 XDOT =       2831
499510                 Wp   =            1
21401
 YDOT =      -4448
759654  meter/sec      RA   =          244
88454  deg
 ZDOT =       5565
044248                 TA   =          337
12285
                                          MA   =          337
18436
                                          Ha   =            228
113  n
mi
                                          Hp   =            221
048

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13439009
90                 X    =        -4029936
22
 Y    =      -16565698
55  feet           Y    =        -5094660
73  meter
 Z    =       -6421496
15                 Z    =        -1977010
45
 XDOT =       9289
696554                 XDOT =        2854
002179
 YDOT =     -14595
668155  feet/sec       YDOT =       -4416
970323  meter/sec
 ZDOT =      18258
019186                 ZDOT =        5578
854196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21044743
09                 X    =        -6414437
69
 Y    =       -3330547
98  feet           Y    =        -1015151
03  meter
 Z    =       -6503168
98                 Z    =        -1982165
91
 XDOT =      -3200
686475                 XDOT =        -975
569238
 YDOT =     -15449
385979  feet/sec       YDOT =       -4708
972846  meter/sec
 ZDOT =      18316
182675                 ZDOT =        5582
772479


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13140
46110433  
00016717  00000-0  10270-3 0  9008
2 25544  51
6485 245
8109 0009551 334
4780  25
5898 15
50344770 30409


Satellite: ISS
Catalog Number: 25544
Epoch time:      13140
46110433   =   yrday
fracday
Element set:     900
Inclination:       51
6485  deg
RA of node:       245
8109  deg
Eccentricity:     
0009551     
Arg of perigee:   334
4780  deg
Mean anomaly:      25
5898  deg
Mean motion:   15
50344770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              291


Coasting Arc #2 (Orbit 3055)
---------------------------------------

Vector Time (GMT): 2013/141/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4307777
40                 A    =         6799237
47  meter
 Y    =        5041753
40  meter          E    =           
0009009
 Z    =        1500263
33                 I    =           51
35629
 XDOT =      -2879
715261                 Wp   =           75
33802
 YDOT =       4176
397852  meter/sec      RA   =          239
90995  deg
 ZDOT =      -5735
204822                 TA   =           88
25152
                                          MA   =           88
14833
                                          Ha   =            228
252  n
mi
                                          Hp   =            220
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14133127
96                 X    =         4243791
26
 Y    =       16541185
70  feet           Y    =         5089567
88  meter
 Z    =        4922123
79                 Z    =         1521035
22
 XDOT =      -9447
884713                 XDOT =       -2898
342029
 YDOT =      13702
092690  feet/sec       YDOT =        4144
091060  meter/sec
 ZDOT =     -18816
288786                 ZDOT =       -5749
239612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21596311
95                 X    =         6582555
88
 Y    =        2470125
78  feet           Y    =          752894
34  meter
 Z    =        5008115
60                 Z    =         1526473
64
 XDOT =       2706
792936                 XDOT =         825
030487
 YDOT =      14808
075194  feet/sec       YDOT =        4513
501319  meter/sec
 ZDOT =     -18875
354952                 ZDOT =       -5753
208190


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13141
49242995  
00016717  00000-0  10270-3 0  9012
2 25544  51
6485 240
6991 0009483 338
1802  21
8944 15
50388494 30560


Satellite: ISS
Catalog Number: 25544
Epoch time:      13141
49242995   =   yrday
fracday
Element set:     901
Inclination:       51
6485  deg
RA of node:       240
6991  deg
Eccentricity:     
0009483     
Arg of perigee:   338
1802  deg
Mean anomaly:      21
8944  deg
Mean motion:   15
50388494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3056
Checksum:              326


Coasting Arc #3 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2013/142/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4507372
94                 A    =         6799671
34  meter
 Y    =       -4967901
66  meter          E    =           
0016998
 Z    =       -1045503
78                 I    =           51
37494
 XDOT =       2976
007807                 Wp   =           10
30065
 YDOT =      -3929
797461  meter/sec      RA   =          234
93639  deg
 ZDOT =       5874
196553                 TA   =          338
33062
                                          MA   =          338
40246
                                          Ha   =            228
381  n
mi
                                          Hp   =            220
467

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14787968
97                 X    =        -4446406
91
 Y    =      -16298889
96  feet           Y    =        -5017965
02  meter
 Z    =       -3430130
51                 Z    =        -1067252
79
 XDOT =       9763
805140                 XDOT =        2991
194595
 YDOT =     -12893
036290  feet/sec       YDOT =       -3896
433209  meter/sec
 ZDOT =      19272
298402                 ZDOT =        5888
690758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21944763
96                 X    =        -6688764
06
 Y    =       -1462552
63  feet           Y    =         -445786
04  meter
 Z    =       -3520214
48                 Z    =        -1072961
37
 XDOT =      -2127
414589                 XDOT =        -648
435967
 YDOT =     -14372
416006  feet/sec       YDOT =       -4380
712399  meter/sec
 ZDOT =      19333
251595                 ZDOT =        5892
775086


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13142
45927491  
00016717  00000-0  10270-3 0  9021
2 25544  51
6493 235
9067 0009736 342
3494  17
7317 15
50411827 30717


Satellite: ISS
Catalog Number: 25544
Epoch time:      13142
45927491   =   yrday
fracday
Element set:     902
Inclination:       51
6493  deg
RA of node:       235
9067  deg
Eccentricity:     
0009736     
Arg of perigee:   342
3494  deg
Mean anomaly:      17
7317  deg
Mean motion:   15
50411827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3071
Checksum:              312


Coasting Arc #4 (Orbit 3086)
---------------------------------------

Vector Time (GMT): 2013/143/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4683261
20                 A    =         6799868
85  meter
 Y    =        4900348
22  meter          E    =           
0007889
 Z    =         543021
22                 I    =           51
39407
 XDOT =      -3131
021020                 Wp   =           81
73003
 YDOT =       3660
143888  meter/sec      RA   =          229
96508  deg
 ZDOT =      -5951
060232                 TA   =           92
40482
                                          MA   =           92
31449
                                          Ha   =            228
477  n
mi
                                          Hp   =            220
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15365030
20                 X    =         4625478
47
 Y    =       16077257
92  feet           Y    =         4952396
28  meter
 Z    =        1781565
70                 Z    =          565632
59
 XDOT =     -10272
378673                 XDOT =       -3142
807532
 YDOT =      12008
346089  feet/sec       YDOT =        3625
065351  meter/sec
 ZDOT =     -19524
475827                 ZDOT =       -5966
299172

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22225137
81                 X    =         6774222
00
 Y    =         512824
49  feet           Y    =          156308
90  meter
 Z    =        1875263
21                 Z    =          571580
23
 XDOT =       1348
532715                 XDOT =         411
032771
 YDOT =      14047
713844  feet/sec       YDOT =        4281
743180  meter/sec
 ZDOT =     -19588
505997                 ZDOT =       -5970
576628


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13143
49055334  
00016717  00000-0  10270-3 0  9035
2 25544  51
6490 230
7952 0009628 346
0400  14
0484 15
50460440 30875


Satellite: ISS
Catalog Number: 25544
Epoch time:      13143
49055334   =   yrday
fracday
Element set:     903
Inclination:       51
6490  deg
RA of node:       230
7952  deg
Eccentricity:     
0009628     
Arg of perigee:   346
0400  deg
Mean anomaly:      14
0484  deg
Mean motion:   15
50460440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3087
Checksum:              284


Coasting Arc #5 (Orbit 3101)
---------------------------------------

Vector Time (GMT): 2013/144/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4829535
19                 A    =         6799953
92  meter
 Y    =       -4769189
73  meter          E    =           
0019379
 Z    =         -52650
41                 I    =           51
41541
 XDOT =       3332
010901                 Wp   =           20
59919
 YDOT =      -3432
733188  meter/sec      RA   =          224
99440  deg
 ZDOT =       5995
372676                 TA   =          338
83224
                                          MA   =          338
91233
                                          Ha   =            228
618  n
mi
                                          Hp   =            219
901

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15844931
72                 X    =        -4775590
37
 Y    =      -15646947
92  feet           Y    =        -4822895
00  meter
 Z    =        -172737
55                 Z    =          -75981
80
 XDOT =      10931
794293                 XDOT =        3341
024294
 YDOT =     -11262
247991  feet/sec       YDOT =       -3395
422735  meter/sec
 ZDOT =      19669
857862                 ZDOT =        6011
581192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22261507
68                 X    =        -6785307
54
 Y    =         520905
66  feet           Y    =          158772
04  meter
 Z    =        -269465
23                 Z    =          -82133
00
 XDOT =       -548
347092                 XDOT =        -167
136194
 YDOT =     -13975
279015  feet/sec       YDOT =       -4259
665044  meter/sec
 ZDOT =      19737
910910                 ZDOT =        6016
115245


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13144
45735455  
00016717  00000-0  10270-3 0  9042
2 25544  51
6495 226
0026 0009878 350
1116   9
9839 15
50481794 31027


Satellite: ISS
Catalog Number: 25544
Epoch time:      13144
45735455   =   yrday
fracday
Element set:     904
Inclination:       51
6495  deg
RA of node:       226
0026  deg
Eccentricity:     
0009878     
Arg of perigee:   350
1116  deg
Mean anomaly:       9
9839  deg
Mean motion:   15
50481794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3102
Checksum:              313


Coasting Arc #6 (Orbit 3117)
---------------------------------------

Vector Time (GMT): 2013/145/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4941019
76                 A    =         6799717
09  meter
 Y    =        4648775
73  meter          E    =           
0006532
 Z    =        -479237
28                 I    =           51
43622
 XDOT =      -3581
295513                 Wp   =           77
49371
 YDOT =       3198
846465  meter/sec      RA   =          220
02595  deg
 ZDOT =      -5961
432640                 TA   =          107
67672
                                          MA   =          107
60539
                                          Ha   =            228
688  n
mi
                                          Hp   =            219
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16210694
75                 X    =         4890996
96
 Y    =       15251888
86  feet           Y    =         4703749
69  meter
 Z    =       -1572300
79                 Z    =         -455354
77
 XDOT =     -11749
657195                 XDOT =       -3587
839999
 YDOT =      10494
903100  feet/sec       YDOT =        3158
762296  meter/sec
 ZDOT =     -19558
506038                 ZDOT =       -5978
846066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22217329
73                 X    =         6771842
10
 Y    =       -1448680
36  feet           Y    =         -441557
77  meter
 Z    =       -1473245
67                 Z    =         -449045
28
 XDOT =       -370
550824                 XDOT =        -112
943891
 YDOT =      14040
795422  feet/sec       YDOT =        4279
634445  meter/sec
 ZDOT =     -19631
565264                 ZDOT =       -5983
701092


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13145
48858686  
00016717  00000-0  10270-3 0  9059
2 25544  51
6482 220
8908 0009785 353
8243   6
2785 15
50529644 31186


Satellite: ISS
Catalog Number: 25544
Epoch time:      13145
48858686   =   yrday
fracday
Element set:     905
Inclination:       51
6482  deg
RA of node:       220
8908  deg
Eccentricity:     
0009785     
Arg of perigee:   353
8243  deg
Mean anomaly:       6
2785  deg
Mean motion:   15
50529644  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3118
Checksum:              339


Coasting Arc #7 (Orbit 3133)
---------------------------------------

Vector Time (GMT): 2013/146/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5005966
21                 A    =         6799356
00  meter
 Y    =       -4474096
74  meter          E    =           
0020626
 Z    =         987888
49                 I    =           51
45942
 XDOT =       3870
410438                 Wp   =           31
59708
 YDOT =      -3020
436783  meter/sec      RA   =          215
05772  deg
 ZDOT =       5894
628438                 TA   =          339
12900
                                          MA   =          339
21308
                                          Ha   =            228
822  n
mi
                                          Hp   =            219
354

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16423773
67                 X    =        -4960362
79
 Y    =      -14678795
08  feet           Y    =        -4529821
76  meter
 Z    =        3241103
98                 Z    =          963679
84
 XDOT =      12698
196975                 XDOT =        3875
263109
 YDOT =      -9909
569499  feet/sec       YDOT =       -2977
129073  meter/sec
 ZDOT =      19339
332147                 ZDOT =        5913
442151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21913055
44                 X    =        -6679099
30
 Y    =        2380428
60  feet           Y    =          725554
64  meter
 Z    =        3140649
97                 Z    =          957270
11
 XDOT =       1239
882052                 XDOT =         377
916050
 YDOT =     -14378
595545  feet/sec       YDOT =       -4382
595922  meter/sec
 ZDOT =      19418
221683                 ZDOT =        5918
673969


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13146
51979558  
00016717  00000-0  10270-3 0  9067
2 25544  51
6484 215
7781 0009984 357
9530   2
1578 15
50556136 31344


Satellite: ISS
Catalog Number: 25544
Epoch time:      13146
51979558   =   yrday
fracday
Element set:     906
Inclination:       51
6484  deg
RA of node:       215
7781  deg
Eccentricity:     
0009984     
Arg of perigee:   357
9530  deg
Mean anomaly:       2
1578  deg
Mean motion:   15
50556136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3134
Checksum:              335


Coasting Arc #8 (Orbit 3148)
---------------------------------------

Vector Time (GMT): 2013/147/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5027641
51                 A    =         6798656
80  meter
 Y    =        4319016
76  meter          E    =           
0006315
 Z    =       -1527945
10                 I    =           51
48164
 XDOT =      -4187
919427                 Wp   =           57
81506
 YDOT =       2850
582167  meter/sec      RA   =          210
09125  deg
 ZDOT =      -5736
645801                 TA   =          138
86980
                                          MA   =          138
82219
                                          Ha   =            228
883  n
mi
                                          Hp   =            219
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16494886
83                 X    =         4986394
05
 Y    =       14170002
48  feet           Y    =         4375008
59  meter
 Z    =       -5012943
24                 Z    =        -1503620
73
 XDOT =     -13739
893134                 XDOT =       -4191
616755
 YDOT =       9352
303699  feet/sec       YDOT =        2803
730301  meter/sec
 ZDOT =     -18821
016409                 ZDOT =       -5756
999066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21539031
13                 X    =         6565096
69
 Y    =       -3153182
78  feet           Y    =         -961090
11  meter
 Z    =       -4911968
84                 Z    =        -1497168
10
 XDOT =      -2127
743989                 XDOT =        -648
536368
 YDOT =      14843
680903  feet/sec       YDOT =        4524
353939  meter/sec
 ZDOT =     -18906
319907                 ZDOT =       -5762
646308


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13147
48653223  
00016717  00000-0  10270-3 0  9073
2 25544  51
6469 210
9852 0009959   1
5684 358
5497 15
50598297 31495


Satellite: ISS
Catalog Number: 25544
Epoch time:      13147
48653223   =   yrday
fracday
Element set:     907
Inclination:       51
6469  deg
RA of node:       210
9852  deg
Eccentricity:     
0009959     
Arg of perigee:     1
5684  deg
Mean anomaly:     358
5497  deg
Mean motion:   15
50598297  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3149
Checksum:              352


Coasting Arc #9 (Orbit 3164)
---------------------------------------

Vector Time (GMT): 2013/148/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4988699
40                 A    =         6797830
23  meter
 Y    =       -4124826
63  meter          E    =           
0020548
 Z    =        2032532
53                 I    =           51
50637
 XDOT =       4535
956186                 Wp   =           42
79706
 YDOT =      -2744
152107  meter/sec      RA   =          205
12496  deg
 ZDOT =       5545
961490                 TA   =          339
70746
                                          MA   =          339
78900
                                          Ha   =            229
005  n
mi
                                          Hp   =            218
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16367124
01                 X    =        -4952077
44
 Y    =      -13532895
77  feet           Y    =        -4180408
89  meter
 Z    =        6668413
81                 Z    =         2008386
29
 XDOT =      14881
746018                 XDOT =        4539
363934
 YDOT =      -9003
123710  feet/sec       YDOT =       -2693
409796  meter/sec
 ZDOT =      18195
411711                 ZDOT =        5568
004750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20918330
90                 X    =        -6375907
26
 Y    =        3843530
40  feet           Y    =         1171508
07  meter
 Z    =        6568140
21                 Z    =         2001969
14
 XDOT =       2900
193358                 XDOT =         883
978936
 YDOT =     -15571
080144  feet/sec       YDOT =       -4746
065228  meter/sec
 ZDOT =      18287
765990                 ZDOT =        5574
111074


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13148
51769569  
00016717  00000-0  10270-3 0  9080
2 25544  51
6472 205
8718 0010082   5
4901 354
6358 15
50630309 31659


Satellite: ISS
Catalog Number: 25544
Epoch time:      13148
51769569   =   yrday
fracday
Element set:     908
Inclination:       51
6472  deg
RA of node:       205
8718  deg
Eccentricity:     
0010082     
Arg of perigee:     5
4901  deg
Mean anomaly:     354
6358  deg
Mean motion:   15
50630309  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3165
Checksum:              313


Coasting Arc #10 (Orbit 3179)
---------------------------------------

Vector Time (GMT): 2013/149/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4903306
89                 A    =         6796718
21  meter
 Y    =        3962784
07  meter          E    =           
0008703
 Z    =       -2554976
25                 I    =           51
53029
 XDOT =      -4884
147317                 Wp   =           40
94876
 YDOT =       2656
443166  meter/sec      RA   =          200
15994  deg
 ZDOT =      -5256
881267                 TA   =          167
71862
                                          MA   =          167
69739
                                          Ha   =            229
059  n
mi
                                          Hp   =            218
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16086964
85                 X    =         4871041
14
 Y    =       13001260
06  feet           Y    =         4017435
79  meter
 Z    =       -8382468
01                 Z    =        -2531234
40
 XDOT =     -16024
105371                 XDOT =       -4887
952731
 YDOT =       8715
364719  feet/sec       YDOT =        2601
804805  meter/sec
 ZDOT =     -17246
985785                 ZDOT =       -5280
616993

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20266421
32                 X    =         6177205
22
 Y    =       -4328861
83  feet           Y    =        -1319437
09  meter
 Z    =       -8283845
31                 Z    =        -2524916
05
 XDOT =      -3588
375939                 XDOT =       -1093
736986
 YDOT =      16370
949854  feet/sec       YDOT =        4989
865515  meter/sec
 ZDOT =     -17346
404144                 ZDOT =       -5287
183983


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13149
48439122  
00016717  00000-0  10270-3 0  9097
2 25544  51
6463 201
0780 0010134   9
3188 350
8149 15
50666934 31800


Satellite: ISS
Catalog Number: 25544
Epoch time:      13149
48439122   =   yrday
fracday
Element set:     909
Inclination:       51
6463  deg
RA of node:       201
0780  deg
Eccentricity:     
0010134     
Arg of perigee:     9
3188  deg
Mean anomaly:     350
8149  deg
Mean motion:   15
50666934  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3180
Checksum:              301


Coasting Arc #11 (Orbit 3195)
---------------------------------------

Vector Time (GMT): 2013/150/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4747882
50                 A    =         6795504
99  meter
 Y    =       -3780992
35  meter          E    =           
0019162
 Z    =        3028707
21                 I    =           51
55598
 XDOT =       5251
782196                 Wp   =           53
44384
 YDOT =      -2633
178097  meter/sec      RA   =          195
19549  deg
 ZDOT =       4935
083445                 TA   =          341
31264
                                          MA   =          341
38290
                                          Ha   =            229
181  n
mi
                                          Hp   =            218
301

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15577042
31                 X    =        -4719962
40
 Y    =      -12404830
55  feet           Y    =        -3833930
31  meter
 Z    =        9936703
45                 Z    =         3005709
92
 XDOT =      17230
256550                 XDOT =        5256
863330
 YDOT =      -8639
035752  feet/sec       YDOT =       -2574
421351  meter/sec
 ZDOT =      16191
218653                 ZDOT =        4960
608267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19410810
84                 X    =        -5916415
14
 Y    =        4651267
54  feet           Y    =         1417706
35  meter
 Z    =        9841152
20                 Z    =         2999583
19
 XDOT =       4112
685793                 XDOT =        1253
546630
 YDOT =     -17394
176411  feet/sec       YDOT =       -5301
744970  meter/sec
 ZDOT =      16298
113113                 ZDOT =        4967
664877


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13150
51551036  
00016717  00000-0  10270-3 0  9104
2 25544  51
6466 195
9643 0010203  13
1435 346
9980 15
50701872 31964


Satellite: ISS
Catalog Number: 25544
Epoch time:      13150
51551036   =   yrday
fracday
Element set:     910
Inclination:       51
6466  deg
RA of node:       195
9643  deg
Eccentricity:     
0010203     
Arg of perigee:    13
1435  deg
Mean anomaly:     346
9980  deg
Mean motion:   15
50701872  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3196
Checksum:              292


Coasting Arc #12 (Orbit 3210)
---------------------------------------

Vector Time (GMT): 2013/151/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4550339
57                 A    =         6794123
21  meter
 Y    =        3645738
39  meter          E    =           
0012837
 Z    =       -3504513
22                 I    =           51
58155
 XDOT =      -5586
215177                 Wp   =           38
92189
 YDOT =       2630
932450  meter/sec      RA   =          190
23179  deg
 ZDOT =      -4515
585871                 TA   =          182
18834
                                          MA   =          182
19396
                                          Ha   =            229
211  n
mi
                                          Hp   =            218
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14928935
60                 X    =         4526257
96
 Y    =       11961083
96  feet           Y    =         3696488
75  meter
 Z    =      -11497746
80                 Z    =        -3482466
28
 XDOT =     -18327
477616                 XDOT =       -5593
284105
 YDOT =       8631
668143  feet/sec       YDOT =        2568
424651  meter/sec
 ZDOT =     -14814
914275                 ZDOT =       -4542
740258

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18588722
58                 X    =         5665842
64
 Y    =       -4743237
52  feet           Y    =        -1445738
80  meter
 Z    =      -11406135
17                 Z    =        -3476590
00
 XDOT =      -4468
321183                 XDOT =       -1361
944296
 YDOT =      18393
553509  feet/sec       YDOT =        5606
355110  meter/sec
 ZDOT =     -14928
622258                 ZDOT =       -4550
244064


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13151
48216514  
00016717  00000-0  10270-3 0  9111
2 25544  51
6467 191
1702 0010286  17
0655 343
0840 15
50734319 32110


Satellite: ISS
Catalog Number: 25544
Epoch time:      13151
48216514   =   yrday
fracday
Element set:     911
Inclination:       51
6467  deg
RA of node:       191
1702  deg
Eccentricity:     
0010286     
Arg of perigee:    17
0655  deg
Mean anomaly:     343
0840  deg
Mean motion:   15
50734319  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3211
Checksum:              275


Coasting Arc #13 (Orbit 3226)
---------------------------------------

Vector Time (GMT): 2013/152/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4279240
11                 A    =         6792696
07  meter
 Y    =       -3511894
99  meter          E    =           
0016736
 Z    =        3917408
98                 I    =           51
60727
 XDOT =       5928
770081                 Wp   =           62
11419
 YDOT =      -2686
126052  meter/sec      RA   =          185
26893  deg
 ZDOT =       4062
702617                 TA   =          345
36276
                                          MA   =          345
41116
                                          Ha   =            229
345  n
mi
                                          Hp   =            217
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14039501
68                 X    =        -4258681
12
 Y    =      -11521965
18  feet           Y    =        -3559633
44  meter
 Z    =       12852391
66                 Z    =         3896670
42
 XDOT =      19451
345410                 XDOT =        5938
630664
 YDOT =      -8812
749514  feet/sec       YDOT =       -2619
771922  meter/sec
 ZDOT =      13329
076827                 ZDOT =        4091
527992

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17630133
69                 X    =        -5373664
75
 Y    =        4609698
80  feet           Y    =         1405036
19  meter
 Z    =       12766218
07                 Z    =         3891143
27
 XDOT =       4640
014816                 XDOT =        1414
276516
 YDOT =     -19553
387610  feet/sec       YDOT =       -5959
872543  meter/sec
 ZDOT =      13449
779748                 ZDOT =        4099
492867


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13152
51324043  
00016717  00000-0  10270-3 0  9124
2 25544  51
6465 186
0565 0010353  20
9814 339
1760 15
50770711 32273


Satellite: ISS
Catalog Number: 25544
Epoch time:      13152
51324043   =   yrday
fracday
Element set:     912
Inclination:       51
6465  deg
RA of node:       186
0565  deg
Eccentricity:     
0010353     
Arg of perigee:    20
9814  deg
Mean anomaly:     339
1760  deg
Mean motion:   15
50770711  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3227
Checksum:              281


Coasting Arc #14 (Orbit 3241)
---------------------------------------

Vector Time (GMT): 2013/153/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3979069
31                 A    =         6791278
82  meter
 Y    =        3437899
34  meter          E    =           
0017301
 Z    =       -4315908
71                 I    =           51
63410
 XDOT =      -6204
462776                 Wp   =           44
98810
 YDOT =       2755
167470  meter/sec      RA   =          180
30648  deg
 ZDOT =      -3522
283668                 TA   =          189
02473
                                          MA   =          189
05587
                                          Ha   =            229
330  n
mi
                                          Hp   =            217
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13054689
35                 X    =         3961295
95
 Y    =       11279197
30  feet           Y    =         3482296
70  meter
 Z    =      -14159805
49                 Z    =        -4296621
53
 XDOT =     -20355
849001                 XDOT =       -6217
700069
 YDOT =       9039
263354  feet/sec       YDOT =        2685
711465  meter/sec
 ZDOT =     -11556
048781                 ZDOT =       -3552
456635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16787378
76                 X    =         5116793
05
 Y    =       -4253458
10  feet           Y    =        -1296454
03  meter
 Z    =      -14079677
05                 Z    =        -4291485
57
 XDOT =      -4596
614130                 XDOT =       -1401
047987
 YDOT =      20564
811011  feet/sec       YDOT =        6268
154396  meter/sec
 ZDOT =     -11682
399845                 ZDOT =       -3560
795473


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13153
47985400  
00016717  00000-0  10270-3 0  9131
2 25544  51
6472 181
2621 0010396  24
6840 335
4807 15
50798999 32424


Satellite: ISS
Catalog Number: 25544
Epoch time:      13153
47985400   =   yrday
fracday
Element set:     913
Inclination:       51
6472  deg
RA of node:       181
2621  deg
Eccentricity:     
0010396     
Arg of perigee:    24
6840  deg
Mean anomaly:     335
4807  deg
Mean motion:   15
50798999  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3242
Checksum:              319


Coasting Arc #15 (Orbit 3257)
---------------------------------------

Vector Time (GMT): 2013/154/10:58:21
532
Vector Time (MET): N/A
Weight (LBS)     : 879644
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3608161
49                 A    =         6789885
53  meter
 Y    =       -3385273
32  meter          E    =           
0013880
 Z    =        4636412
03                 I    =           51
65944
 XDOT =       6478
142131                 Wp   =           66
07142
 YDOT =      -2866
197772  meter/sec      RA   =          175
34465  deg
 ZDOT =       2947
220918                 TA   =          354
59714
                                          MA   =          354
61210
                                          Ha   =            229
470  n
mi
                                          Hp   =            217
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11837800
15                 X    =        -3592561
16
 Y    =      -11106539
76  feet           Y    =        -3425535
17  meter
 Z    =       15211325
57                 Z    =         4618921
35
 XDOT =      21253
747149                 XDOT =        6495
394131
 YDOT =      -9403
535997  feet/sec       YDOT =       -2793
658856  meter/sec
 ZDOT =       9669
359968                 ZDOT =        2978
733213

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15889148
33                 X    =        -4843012
41
 Y    =        3637064
61  feet           Y    =         1108577
29  meter
 Z    =       15138688
51                 Z    =         4614272
26
 XDOT =       4385
422502                 XDOT =        1336
676779
 YDOT =     -21658
062238  feet/sec       YDOT =       -6601
377370  meter/sec
 ZDOT =       9801
332396                 ZDOT =        2987
446114


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   13154
51088519  
00016717  00000-0  10270-3 0  9143
2 25544  51
6461 176
1480 0010495  28
7597 331
4131 15
50838748 32582


Satellite: ISS
Catalog Number: 25544
Epoch time:      13154
51088519   =   yrday
fracday
Element set:     914
Inclination:       51
6461  deg
RA of node:       176
1480  deg
Eccentricity:     
0010495     
Arg of perigee:    28
7597  deg
Mean anomaly:     331
4131  deg
Mean motion:   15
50838748  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3258
Checksum:              319

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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