[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: October 20th 2011

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 ET - UTC (sec) : 66 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


299/12:43:09 828 -5 8 7 3 7 3
N/A -4 4 -0 0 218 2
000/00:02:19 656 -0 3 0 0 204 8

Coasting Arc #1 (Orbit 2035)
---------------------------------------

Vector Time (GMT): 2011/292/17:21:47
765
Vector Time (MET): N/A
Weight (LBS)     : 871443
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2222465
51                 A    =         6772844
56  meter
 Y    =        6395952
69  meter          E    =           
0008040
 Z    =         311159
95                 I    =           51
33034
 XDOT =      -4438
607112                 Wp   =            5
21443
 YDOT =       1833
959268  meter/sec      RA   =          252
94629  deg
 ZDOT =      -5974
498308                 TA   =          171
41485
                                          MA   =          171
40109
                                          Ha   =            216
034  n
mi
                                          Hp   =            204
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7291553
52                 X    =         2149267
96
 Y    =       20984096
75  feet           Y    =         6420396
40  meter
 Z    =        1020865
98                 Z    =          321778
79
 XDOT =     -14562
359292                 XDOT =       -4429
761603
 YDOT =       6016
926731  feet/sec       YDOT =        1784
373309  meter/sec
 ZDOT =     -19601
372402                 ZDOT =       -5996
039840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17823945
95                 X    =        -5432738
73
 Y    =       13255811
09  feet           Y    =         4040371
22  meter
 Z    =        1063794
93                 Z    =          324244
69
 XDOT =      -9112
653229                 XDOT =       -2777
536704
 YDOT =     -10667
849583  feet/sec       YDOT =       -3251
560553  meter/sec
 ZDOT =     -19689
192998                 ZDOT =       -6001
266026


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   11292
75613047  
00016717  00000-0  10270-3 0  9005
2 25544  51
6419 253
6552 0018653 331
8740  28
1406 15
59797036 20369


Satellite: ISS
Catalog Number: 25544
Epoch time:      11292
75613047   =   yrday
fracday
Element set:     900
Inclination:       51
6419  deg
RA of node:       253
6552  deg
Eccentricity:     
0018653     
Arg of perigee:   331
8740  deg
Mean anomaly:      28
1406  deg
Mean motion:   15
59797036  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2036
Checksum:              308


Coasting Arc #2 (Orbit 2051)
---------------------------------------

Vector Time (GMT): 2011/293/17:21:47
765
Vector Time (MET): N/A
Weight (LBS)     : 871443
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         241587
49                 A    =         6768628
33  meter
 Y    =       -5999850
86  meter          E    =           
0019108
 Z    =        3097287
48                 I    =           51
32627
 XDOT =       5300
358472                 Wp   =           16
10214
 YDOT =       2716
999836  meter/sec      RA   =          247
92161  deg
 ZDOT =       4860
621419                 TA   =           19
85475
                                          MA   =           19
78048
                                          Ha   =            216
186  n
mi
                                          Hp   =            203
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         792609
87                 X    =          293614
86
 Y    =      -19684550
07  feet           Y    =        -5996858
24  meter
 Z    =       10161704
32                 Z    =         3098587
77
 XDOT =      17389
627534                 XDOT =        5245
970293
 YDOT =       8914
041456  feet/sec       YDOT =        2775
967818  meter/sec
 ZDOT =      15946
920666                 ZDOT =        4886
238531

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18900993
32                 X    =         5761022
77
 Y    =       -5545147
65  feet           Y    =        -1690161
01  meter
 Z    =       10167288
99                 Z    =         3098989
68
 XDOT =      -3378
676465                 XDOT =       -1029
820586
 YDOT =      17848
739862  feet/sec       YDOT =        5440
295910  meter/sec
 ZDOT =      16051
125047                 ZDOT =        4892
382914


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   11293
78118733  
00016717  00000-0  10270-3 0  9012
2 25544  51
6416 248
4998 0018859 336
0765  23
9512 15
59852748 20525


Satellite: ISS
Catalog Number: 25544
Epoch time:      11293
78118733   =   yrday
fracday
Element set:     901
Inclination:       51
6416  deg
RA of node:       248
4998  deg
Eccentricity:     
0018859     
Arg of perigee:   336
0765  deg
Mean anomaly:      23
9512  deg
Mean motion:   15
59852748  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2052
Checksum:              341


Coasting Arc #3 (Orbit 2066)
---------------------------------------

Vector Time (GMT): 2011/294/17:21:47
765
Vector Time (MET): N/A
Weight (LBS)     : 871443
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2842562
80                 A    =         6761314
24  meter
 Y    =        3416865
61  meter          E    =           
0021468
 Z    =       -5105611
88                 I    =           51
31437
 XDOT =      -4473
545720                 Wp   =           18
19788
 YDOT =      -6037
900033  meter/sec      RA   =          242
85920  deg
 ZDOT =      -1531
826888                 TA   =          236
87302
                                          MA   =          237
07923
                                          Ha   =            216
239  n
mi
                                          Hp   =            203
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9325993
43                 X    =        -2855757
24
 Y    =       11210188
99  feet           Y    =         3385004
22  meter
 Z    =      -16750695
13                 Z    =        -5119453
43
 XDOT =     -14676
987271                 XDOT =       -4398
254844
 YDOT =     -19809
383312  feet/sec       YDOT =       -6087
505088  meter/sec
 ZDOT =      -5025
678765                 ZDOT =       -1553
376280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13642540
30                 X    =        -4158246
28
 Y    =       -4962489
16  feet           Y    =        -1512566
70  meter
 Z    =      -16807232
78                 Z    =        -5122844
55
 XDOT =      13435
362910                 XDOT =        4095
098615
 YDOT =     -19415
337028  feet/sec       YDOT =       -5917
794726  meter/sec
 ZDOT =      -5113
170653                 ZDOT =       -1558
494415


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   11294
74214919  
00016717  00000-0  10270-3 0  9023
2 25544  51
6410 243
6674 0018851 339
1880  20
8506 15
59936537 20675


Satellite: ISS
Catalog Number: 25544
Epoch time:      11294
74214919   =   yrday
fracday
Element set:     902
Inclination:       51
6410  deg
RA of node:       243
6674  deg
Eccentricity:     
0018851     
Arg of perigee:   339
1880  deg
Mean anomaly:      20
8506  deg
Mean motion:   15
59936537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2067
Checksum:              322


Coasting Arc #4 (Orbit 2082)
---------------------------------------

Vector Time (GMT): 2011/295/17:21:47
765
Vector Time (MET): N/A
Weight (LBS)     : 871443
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4768599
62                 A    =         6762424
30  meter
 Y    =         380680
91  meter          E    =           
0021541
 Z    =        4787795
63                 I    =           51
33396
 XDOT =       2000
458797                 Wp   =            1
91134
 YDOT =       6961
993224  meter/sec      RA   =          237
77580  deg
 ZDOT =      -2524
492401                 TA   =          113
13061
                                          MA   =          112
90348
                                          Ha   =            216
275  n
mi
                                          Hp   =            202
936

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15645011
89                 X    =         4740729
86
 Y    =        1248953
13  feet           Y    =          433850
88  meter
 Z    =       15707990
92                 Z    =         4810894
01
 XDOT =       6563
185031                 XDOT =        1934
723398
 YDOT =      22841
185118  feet/sec       YDOT =        6983
995826  meter/sec
 ZDOT =      -8282
455385                 ZDOT =       -2514
934315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4261842
56                 X    =         1299009
61
 Y    =       15006625
90  feet           Y    =         4574019
57  meter
 Z    =       15802061
15                 Z    =         4816468
24
 XDOT =     -17996
610450                 XDOT =       -5485
366865
 YDOT =      13865
627150  feet/sec       YDOT =        4226
243155  meter/sec
 ZDOT =      -8243
836953                 ZDOT =       -2512
721503


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   11295
76714616  
00016717  00000-0  10270-3 0  9036
2 25544  51
6413 238
5119 0018824 342
6857  17
3654 15
60000562 20833


Satellite: ISS
Catalog Number: 25544
Epoch time:      11295
76714616   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:       238
5119  deg
Eccentricity:     
0018824     
Arg of perigee:   342
6857  deg
Mean anomaly:      17
3654  deg
Mean motion:   15
60000562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2083
Checksum:              303


Coasting Arc #5 (Orbit 2097)
---------------------------------------

Vector Time (GMT): 2011/296/17:21:47
765
Vector Time (MET): N/A
Weight (LBS)     : 871443
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5139413
68                 A    =         6770046
69  meter
 Y    =       -3747747
02  meter          E    =           
0022409
 Z    =       -2277699
83                 I    =           51
37571
 XDOT =       1441
282678                 Wp   =          359
18998
 YDOT =      -5258
296416  meter/sec      RA   =          232
72509  deg
 ZDOT =       5421
285511                 TA   =          335
24623
                                          MA   =          335
35359
                                          Ha   =            216
404  n
mi
                                          Hp   =            202
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16861593
44                 X    =        -5086058
84
 Y    =      -12295757
94  feet           Y    =        -3804920
98  meter
 Z    =       -7472768
47                 Z    =        -2302537
52
 XDOT =       4728
617709                 XDOT =        1473
638844
 YDOT =     -17251
628660  feet/sec       YDOT =       -5241
997692  meter/sec
 ZDOT =      17786
369786                 ZDOT =        5428
366448

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5300251
53                 X    =         1615516
66
 Y    =      -20146624
07  feet           Y    =        -6140691
02  meter
 Z    =       -7573779
63                 Z    =        -2308488
03
 XDOT =      16277
229562                 XDOT =        4961
299570
 YDOT =      -2389
147213  feet/sec       YDOT =        -728
212071  meter/sec
 ZDOT =      17815
446297                 ZDOT =        5430
148031


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   11296
72805459  
00016717  00000-0  10270-3 0  9040
2 25544  51
6405 233
6783 0018823 346
1383  13
9254 15
59995748 20980


Satellite: ISS
Catalog Number: 25544
Epoch time:      11296
72805459   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       233
6783  deg
Eccentricity:     
0018823     
Arg of perigee:   346
1383  deg
Mean anomaly:      13
9254  deg
Mean motion:   15
59995748  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2098
Checksum:              344


Coasting Arc #6 (Orbit 2113)
---------------------------------------

Vector Time (GMT): 2011/297/17:21:47
765
Vector Time (MET): N/A
Weight (LBS)     : 871443
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3636239
65                 A    =         6771476
56  meter
 Y    =        5566549
73  meter          E    =           
0011472
 Z    =       -1322597
15                 I    =           51
39983
 XDOT =      -4712
420250                 Wp   =           11
07607
 YDOT =       1699
722411  meter/sec      RA   =          227
70925  deg
 ZDOT =      -5799
484811                 TA   =          183
37992
                                          MA   =          183
38768
                                          Ha   =            216
548  n
mi
                                          Hp   =            202
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11929920
10                 X    =         3580148
20
 Y    =       18262958
43  feet           Y    =         5606898
64  meter
 Z    =       -4339229
51                 Z    =        -1305068
70
 XDOT =     -15460
696358                 XDOT =       -4702
903220
 YDOT =       5576
517096  feet/sec       YDOT =        1647
077923  meter/sec
 ZDOT =     -19027
181137                 ZDOT =       -5822
355243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12322234
83                 X    =        -3755817
18
 Y    =       18017593
95  feet           Y    =         5491762
64  meter
 Z    =       -4268066
75                 Z    =        -1300906
74
 XDOT =      -9693
080306                 XDOT =       -2954
450877
 YDOT =     -11160
508822  feet/sec       YDOT =       -3401
723089  meter/sec
 ZDOT =     -19120
422155                 ZDOT =       -5827
904673


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   11297
75299311  
00016717  00000-0  10270-3 0  9059
2 25544  51
6403 228
5232 0018618 349
9351  10
1429 15
60036424 21149


Satellite: ISS
Catalog Number: 25544
Epoch time:      11297
75299311   =   yrday
fracday
Element set:     905
Inclination:       51
6403  deg
RA of node:       228
5232  deg
Eccentricity:     
0018618     
Arg of perigee:   349
9351  deg
Mean anomaly:      10
1429  deg
Mean motion:   15
60036424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2114
Checksum:              292


Coasting Arc #7 (Orbit 2129)
---------------------------------------

Vector Time (GMT): 2011/298/17:21:47
765
Vector Time (MET): N/A
Weight (LBS)     : 871443
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -545680
92                 A    =         6764167
52  meter
 Y    =       -5176507
58  meter          E    =           
0017204
 Z    =        4303819
56                 I    =           51
39650
 XDOT =       6490
702904                 Wp   =           25
21554
 YDOT =       2202
425102  meter/sec      RA   =          222
67228  deg
 ZDOT =       3482
145536                 TA   =           29
41166
                                          MA   =           29
31496
                                          Ha   =            216
664  n
mi
                                          Hp   =            202
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1790291
74                 X    =         -508663
34
 Y    =      -16983292
59  feet           Y    =        -5182402
43  meter
 Z    =       14120142
91                 Z    =         4301258
87
 XDOT =      21294
957034                 XDOT =        6448
676483
 YDOT =       7225
804139  feet/sec       YDOT =        2274
773395  meter/sec
 ZDOT =      11424
361995                 ZDOT =        3513
575910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14840083
07                 X    =         4523257
32
 Y    =       -8467433
99  feet           Y    =        -2580873
88  meter
 Z    =       14109936
34                 Z    =         4300708
60
 XDOT =       1182
629571                 XDOT =         360
465493
 YDOT =      21267
504322  feet/sec       YDOT =        6482
335317  meter/sec
 ZDOT =      11552
310111                 ZDOT =        3521
144122


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   11298
77790090  
00016717  00000-0  10270-3 0  9063
2 25544  51
6399 223
3661 0018718 353
9155   6
1770 15
60074124 21301


Satellite: ISS
Catalog Number: 25544
Epoch time:      11298
77790090   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       223
3661  deg
Eccentricity:     
0018718     
Arg of perigee:   353
9155  deg
Mean anomaly:       6
1770  deg
Mean motion:   15
60074124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2130
Checksum:              308


Coasting Arc #8 (Orbit 2141)
---------------------------------------

Vector Time (GMT): 2011/299/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2775647
20                 A    =         6763813
44  meter
 Y    =        3185685
70  meter          E    =           
0019765
 Z    =       -5288473
63                 I    =           51
40309
 XDOT =      -5908
068006                 Wp   =           24
96906
 YDOT =      -4889
157313  meter/sec      RA   =          218
57423  deg
 ZDOT =        173
517783                 TA   =          246
58551
                                          MA   =          246
79347
                                          Ha   =            218
248  n
mi
                                          Hp   =            204
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9106454
07                 X    =        -2785372
71
 Y    =       10451724
73  feet           Y    =         3154592
06  meter
 Z    =      -17350635
28                 Z    =        -5301981
89
 XDOT =     -19383
425216                 XDOT =       -5853
800319
 YDOT =     -16040
542366  feet/sec       YDOT =       -4954
921515  meter/sec
 ZDOT =        569
284064                 ZDOT =         144
947668

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -985124
21                 X    =         -300265
86
 Y    =      -13757831
96  feet           Y    =        -4193387
18  meter
 Z    =      -17405809
09                 Z    =        -5305290
61
 XDOT =      24054
172435                 XDOT =        7331
711758
 YDOT =      -2221
892439  feet/sec       YDOT =        -677
232816  meter/sec
 ZDOT =        453
100300                 ZDOT =         138
104971


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   11299
54656439  
00016717  00000-0  10270-3 0  9078
2 25544  51
6416 219
5010 0019415 339
9494  20
0896 15
58791079 21420


Satellite: ISS
Catalog Number: 25544
Epoch time:      11299
54656439   =   yrday
fracday
Element set:     907
Inclination:       51
6416  deg
RA of node:       219
5010  deg
Eccentricity:     
0019415     
Arg of perigee:   339
9494  deg
Mean anomaly:      20
0896  deg
Mean motion:   15
58791079  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2142
Checksum:              332


Coasting Arc #9 (Orbit 2157)
---------------------------------------

Vector Time (GMT): 2011/300/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5283672
90                 A    =         6768065
90  meter
 Y    =        -523339
49  meter          E    =           
0021820
 Z    =        4207519
23                 I    =           51
44164
 XDOT =       3485
360108                 Wp   =           11
33107
 YDOT =       5782
084415  meter/sec      RA   =          213
51607  deg
 ZDOT =      -3633
405577                 TA   =          116
08491
                                          MA   =          115
86018
                                          Ha   =            218
377  n
mi
                                          Hp   =            204
519

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17334884
84                 X    =         5268692
34
 Y    =       -1716993
07  feet           Y    =         -464337
90  meter
 Z    =       13804196
95                 Z    =         4233151
65
 XDOT =      11434
908492                 XDOT =        3438
095579
 YDOT =      18970
093226  feet/sec       YDOT =        5820
795508  meter/sec
 ZDOT =     -11920
621971                 ZDOT =       -3616
588142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10791718
86                 X    =        -3289315
91
 Y    =       13567982
84  feet           Y    =         4135521
17  meter
 Z    =       13908659
07                 Z    =         4239359
28
 XDOT =     -20633
838539                 XDOT =       -6289
193987
 YDOT =      -4180
983503  feet/sec       YDOT =       -1274
363772  meter/sec
 ZDOT =     -11852
356258                 ZDOT =       -3612
598187


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   11300
57231196  
00016717  00000-0  10270-3 0  9084
2 25544  51
6411 214
3514 0019411 343
6764  16
3764 15
58826015 21583


Satellite: ISS
Catalog Number: 25544
Epoch time:      11300
57231196   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:       214
3514  deg
Eccentricity:     
0019411     
Arg of perigee:   343
6764  deg
Mean anomaly:      16
3764  deg
Mean motion:   15
58826015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2158
Checksum:              291


Coasting Arc #10 (Orbit 2172)
---------------------------------------

Vector Time (GMT): 2011/301/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6267972
14                 A    =         6774482
17  meter
 Y    =       -1978964
76  meter          E    =           
0025211
 Z    =       -1571932
27                 I    =           51
48979
 XDOT =        177
754633                 Wp   =            1
50446
 YDOT =      -5105
966602  meter/sec      RA   =          208
49253  deg
 ZDOT =       5746
098692                 TA   =          341
20340
                                          MA   =          341
29632
                                          Ha   =            218
419  n
mi
                                          Hp   =            204
333

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20564213
06                 X    =        -6237740
75
 Y    =       -6492666
52  feet           Y    =        -2048888
01  meter
 Z    =       -5157258
12                 Z    =        -1602309
43
 XDOT =        583
184490                 XDOT =         206
923133
 YDOT =     -16751
858929  feet/sec       YDOT =       -5103
815801  meter/sec
 ZDOT =      18852
029831                 ZDOT =        5747
033053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18787650
19                 X    =         5726475
78
 Y    =      -10524951
69  feet           Y    =        -3208005
27  meter
 Z    =       -5280954
54                 Z    =        -1609634
94
 XDOT =      11123
305702                 XDOT =        3390
383578
 YDOT =      10437
674964  feet/sec       YDOT =        3181
403329  meter/sec
 ZDOT =      18856
066890                 ZDOT =        5747
329188


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   11301
53392381  
00016717  00000-0  10270-3 0  9096
2 25544  51
6416 209
5231 0019411 346
9873  13
0778 15
58869249 21739


Satellite: ISS
Catalog Number: 25544
Epoch time:      11301
53392381   =   yrday
fracday
Element set:     909
Inclination:       51
6416  deg
RA of node:       209
5231  deg
Eccentricity:     
0019411     
Arg of perigee:   346
9873  deg
Mean anomaly:      13
0778  deg
Mean motion:   15
58869249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2173
Checksum:              319


Coasting Arc #11 (Orbit 2188)
---------------------------------------

Vector Time (GMT): 2011/302/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5362426
74                 A    =         6774356
68  meter
 Y    =        3794734
01  meter          E    =           
0012943
 Z    =       -1689052
27                 I    =           51
51633
 XDOT =      -4038
172117                 Wp   =            7
37719
 YDOT =       3172
626450  meter/sec      RA   =          203
49099  deg
 ZDOT =      -5684
892632                 TA   =          191
17165
                                          MA   =          191
20041
                                          Ha   =            218
604  n
mi
                                          Hp   =            204
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17593263
59                 X    =         5327800
01
 Y    =       12449914
73  feet           Y    =         3854506
39  meter
 Z    =       -5541510
06                 Z    =        -1663085
08
 XDOT =     -13248
596186                 XDOT =       -4045
732175
 YDOT =      10408
879429  feet/sec       YDOT =        3127
427009  meter/sec
 ZDOT =     -18651
222547                 ZDOT =       -5704
528758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21063443
46                 X    =        -6420137
57
 Y    =        4691959
67  feet           Y    =         1430109
31  meter
 Z    =       -5435853
08                 Z    =        -1656848
02
 XDOT =       1457
924668                 XDOT =         444
375439
 YDOT =     -15186
113979  feet/sec       YDOT =       -4628
727541  meter/sec
 ZDOT =     -18731
393297                 ZDOT =       -5709
328677


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   11302
55961590  
00016717  00000-0  10270-3 0  9105
2 25544  51
6413 204
3731 0019296 350
4991   9
5797 15
58885834 21892


Satellite: ISS
Catalog Number: 25544
Epoch time:      11302
55961590   =   yrday
fracday
Element set:     910
Inclination:       51
6413  deg
RA of node:       204
3731  deg
Eccentricity:     
0019296     
Arg of perigee:   350
4991  deg
Mean anomaly:       9
5797  deg
Mean motion:   15
58885834  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2189
Checksum:              331


Coasting Arc #12 (Orbit 2204)
---------------------------------------

Vector Time (GMT): 2011/303/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2628201
88                 A    =         6767476
96  meter
 Y    =       -4490368
89  meter          E    =           
0017956
 Z    =        4311029
19                 I    =           51
52166
 XDOT =       6817
227021                 Wp   =           24
94624
 YDOT =       -648
607476  meter/sec      RA   =          198
46920  deg
 ZDOT =       3491
188210                 TA   =           29
64118
                                          MA   =           29
53954
                                          Ha   =            218
763  n
mi
                                          Hp   =            203
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8622709
58                 X    =        -2598736
88
 Y    =      -14732181
39  feet           Y    =        -4519594
42  meter
 Z    =       14143796
55                 Z    =         4298332
63
 XDOT =      22366
230383                 XDOT =        6807
013377
 YDOT =      -2127
977285  feet/sec       YDOT =        -572
430275  meter/sec
 ZDOT =      11454
029559                 ZDOT =        3524
281983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16818735
77                 X    =         5126350
66
 Y    =        3158152
57  feet           Y    =          962604
90  meter
 Z    =       14092248
55                 Z    =         4295317
36
 XDOT =     -12862
840144                 XDOT =       -3920
593676
 YDOT =      16945
991613  feet/sec       YDOT =        5165
138244  meter/sec
 ZDOT =      11588
951490                 ZDOT =        3532
312414


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   11303
58527943  
00016717  00000-0  10270-3 0  9110
2 25544  51
6411 199
2221 0019406 354
6785   5
4161 15
58939437 22054


Satellite: ISS
Catalog Number: 25544
Epoch time:      11303
58527943   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       199
2221  deg
Eccentricity:     
0019406     
Arg of perigee:   354
6785  deg
Mean anomaly:       5
4161  deg
Mean motion:   15
58939437  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2205
Checksum:              308


Coasting Arc #13 (Orbit 2219)
---------------------------------------

Vector Time (GMT): 2011/304/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1010743
31                 A    =         6763174
93  meter
 Y    =        4089767
08  meter          E    =           
0024031
 Z    =       -5303042
46                 I    =           51
53679
 XDOT =      -7449
049236                 Wp   =           36
46986
 YDOT =      -1811
153700  meter/sec      RA   =          193
41629  deg
 ZDOT =         42
000792                 TA   =          233
81975
                                          MA   =          234
04225
                                          Ha   =            218
750  n
mi
                                          Hp   =            203
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3316086
97                 X    =        -1030639
25
 Y    =       13417870
99  feet           Y    =         4078353
19  meter
 Z    =      -17398433
27                 Z    =        -5308000
95
 XDOT =     -24439
137912                 XDOT =       -7428
446957
 YDOT =      -5942
105314  feet/sec       YDOT =       -1894
338339  meter/sec
 ZDOT =        137
797874                 ZDOT =           5
862906

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8168062
65                 X    =        -2489625
50
 Y    =      -11117922
99  feet           Y    =        -3388742
93  meter
 Z    =      -17418832
22                 Z    =        -5309260
06
 XDOT =      19512
115928                 XDOT =        5947
292935
 YDOT =     -14222
635788  feet/sec       YDOT =       -4335
059388  meter/sec
 ZDOT =         -9
441103                 ZDOT =          -2
877648


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   11304
54681226  
00016717  00000-0  10270-3 0  9123
2 25544  51
6407 194
3935 0019425 357
7530   2
3535 15
59011613 22206


Satellite: ISS
Catalog Number: 25544
Epoch time:      11304
54681226   =   yrday
fracday
Element set:     912
Inclination:       51
6407  deg
RA of node:       194
3935  deg
Eccentricity:     
0019425     
Arg of perigee:   357
7530  deg
Mean anomaly:       2
3535  deg
Mean motion:   15
59011613  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2220
Checksum:              283


Coasting Arc #14 (Orbit 2235)
---------------------------------------

Vector Time (GMT): 2011/305/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4516400
49                 A    =         6767237
09  meter
 Y    =       -2734261
54  meter          E    =           
0024468
 Z    =        4239115
37                 I    =           51
58093
 XDOT =       5659
760138                 Wp   =           24
28145
 YDOT =       3719
460285  meter/sec      RA   =          188
36452  deg
 ZDOT =      -3601
628310                 TA   =          102
67423
                                          MA   =          102
40057
                                          Ha   =            218
771  n
mi
                                          Hp   =            203
054

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14817586
90                 X    =         4526046
83
 Y    =       -8970674
36  feet           Y    =        -2683702
48  meter
 Z    =       13907858
81                 Z    =         4261079
64
 XDOT =      18568
766858                 XDOT =        5635
243963
 YDOT =      12202
953691  feet/sec       YDOT =        3782
614136  meter/sec
 ZDOT =     -11816
365847                 ZDOT =       -3574
192482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2376063
04                 X    =         -724224
01
 Y    =       17084665
75  feet           Y    =         5207406
12  meter
 Z    =       13997533
27                 Z    =         4266448
14
 XDOT =     -19997
236385                 XDOT =       -6095
157650
 YDOT =       6886
707411  feet/sec       YDOT =        2099
068419  meter/sec
 ZDOT =     -11704
672552                 ZDOT =       -3567
584194


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   11305
57242048  
00016717  00000-0  10270-3 0  9133
2 25544  51
6408 189
2423 0019502   1
2585 358
8616 15
59075779 22368


Satellite: ISS
Catalog Number: 25544
Epoch time:      11305
57242048   =   yrday
fracday
Element set:     913
Inclination:       51
6408  deg
RA of node:       189
2423  deg
Eccentricity:     
0019502     
Arg of perigee:     1
2585  deg
Mean anomaly:     358
8616  deg
Mean motion:   15
59075779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2236
Checksum:              315


Coasting Arc #15 (Orbit 2250)
---------------------------------------

Vector Time (GMT): 2011/306/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6519907
81                 A    =         6773921
80  meter
 Y    =         856282
56  meter          E    =           
0026527
 Z    =       -1560916
59                 I    =           51
63297
 XDOT =      -1984
098917                 Wp   =           14
53780
 YDOT =      -4686
235417  meter/sec      RA   =          183
34906  deg
 ZDOT =       5763
027819                 TA   =          328
33088
                                          MA   =          328
49021
                                          Ha   =            218
872  n
mi
                                          Hp   =            202
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21390773
66                 X    =        -6521415
64
 Y    =        2809325
99  feet           Y    =          783364
51  meter
 Z    =       -5121117
41                 Z    =        -1592594
22
 XDOT =      -6509
510881                 XDOT =       -1959
545010
 YDOT =     -15374
788113  feet/sec       YDOT =       -4708
285478  meter/sec
 ZDOT =      18907
571585                 ZDOT =        5753
448683

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11022661
53                 X    =         3359707
23
 Y    =      -18509953
43  feet           Y    =        -5641833
80  meter
 Z    =       -5250324
83                 Z    =        -1600299
01
 XDOT =      14822
948494                 XDOT =        4518
034701
 YDOT =       3516
953607  feet/sec       YDOT =        1071
967459  meter/sec
 ZDOT =      18868
719904                 ZDOT =        5751
185827


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   11306
53390475  
00016717  00000-0  10270-3 0  9149
2 25544  51
6405 184
4129 0019472   4
6573 355
4760 15
59066736 22518


Satellite: ISS
Catalog Number: 25544
Epoch time:      11306
53390475   =   yrday
fracday
Element set:     914
Inclination:       51
6405  deg
RA of node:       184
4129  deg
Eccentricity:     
0019472     
Arg of perigee:     4
6573  deg
Mean anomaly:     355
4760  deg
Mean motion:   15
59066736  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2251
Checksum:              311


Coasting Arc #16 (Orbit 2266)
---------------------------------------

Vector Time (GMT): 2011/307/12:44:19
656
Vector Time (MET): N/A
Weight (LBS)     : 870759
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6429853
33                 A    =         6773635
54  meter
 Y    =        1225119
93  meter          E    =           
0015083
 Z    =       -1781708
91                 I    =           51
66204
 XDOT =      -2433
457475                 Wp   =           29
84724
 YDOT =       4549
126299  meter/sec      RA   =          178
35651  deg
 ZDOT =      -5661
733906                 TA   =          169
71627
                                          MA   =          169
68538
                                          Ha   =            218
971  n
mi
                                          Hp   =            202
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21095319
33                 X    =         6424331
21
 Y    =        4019422
33  feet           Y    =         1296991
56  meter
 Z    =       -5845501
68                 Z    =        -1750485
87
 XDOT =      -7983
784367                 XDOT =       -2456
641926
 YDOT =      14924
955050  feet/sec       YDOT =        4521
784105  meter/sec
 ZDOT =     -18575
242475                 ZDOT =       -5673
612178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15996843
07                 X    =        -4875837
77
 Y    =       14378491
89  feet           Y    =         4382564
33  meter
 Z    =       -5718227
52                 Z    =        -1742915
75
 XDOT =      -6058
376239                 XDOT =       -1846
593077
 YDOT =     -14136
369157  feet/sec       YDOT =       -4308
765319  meter/sec
 ZDOT =     -18623
883524                 ZDOT =       -5676
559698


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   11307
55946107  
00016717  00000-0  10270-3 0  9152
2 25544  51
6401 179
2618 0019277   8
2859 351
8611 15
59091496 22672


Satellite: ISS
Catalog Number: 25544
Epoch time:      11307
55946107   =   yrday
fracday
Element set:     915
Inclination:       51
6401  deg
RA of node:       179
2618  deg
Eccentricity:     
0019277     
Arg of perigee:     8
2859  deg
Mean anomaly:     351
8611  deg
Mean motion:   15
59091496  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2267
Checksum:              328

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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