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

 
Date: June 3rd 2011

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15338 57 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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


153/22:38:26 098 -5 3 7 3 7 4
N/A 2 0 -1 3 189 3
000/00:16:52 195 -4 7 -0 0 183 9

163/14:26:50 821 -9 2 9 5 9 5
N/A 1 3 -0 0 191 9
000/00:33:41 641 -2 2 -0 3 190 2

163/18:35:10 758 3 6 8 5 8 6
N/A 5 3 -0 5 201 5
000/00:40:21 516 -5 7 0 4 193 2

166/15:04:46 247 8 8 9 8 9 8
N/A -3 9 0 3 205 1
000/00:29:32 493 1 9 0 6 196 1

166/19:08:05 798 -8 5 9 4 9 4
N/A -1 3 0 2 206 3
000/00:36:11 597 3 8 -0 3 205 2

Coasting Arc #1 (Orbit 3843)
---------------------------------------

Vector Time (GMT): 2011/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905423
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4184892
48                 A    =         6715788
50  meter
 Y    =        1011789
95  meter          E    =           
0014123
 Z    =       -5165309
54                 I    =           51
32976
 XDOT =      -3015
636090                 Wp   =           75
47346
 YDOT =      -6995
923991  meter/sec      RA   =          240
17388  deg
 ZDOT =       1078
820158                 TA   =          204
83810
                                          MA   =          204
90614
                                          Ha   =            188
294  n
mi
                                          Hp   =            181
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13729962
19                 X    =        -4170803
08
 Y    =        3319520
84  feet           Y    =          965071
53  meter
 Z    =      -16946553
61                 Z    =        -5185605
57
 XDOT =      -9893
819192                 XDOT =       -2942
422957
 YDOT =     -22952
506533  feet/sec       YDOT =       -7029
237476  meter/sec
 ZDOT =       3539
436213                 ZDOT =        1064
346790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1825021
82                 X    =         -556266
65
 Y    =       13907097
55  feet           Y    =         4238883
33  meter
 Z    =      -17028760
75                 Z    =        -5190366
28
 XDOT =     -23969
728832                 XDOT =       -7305
973348
 YDOT =       1093
193923  feet/sec       YDOT =         333
205508  meter/sec
 ZDOT =       3481
124636                 ZDOT =        1061
046789


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   11152
51408285  
00016717  00000-0  10270-3 0  9000
2 25544  51
6487 241
0311 0005688 353
1195   6
9890 15
75642848 38440


Satellite: ISS
Catalog Number: 25544
Epoch time:      11152
51408285   =   yrday
fracday
Element set:     900
Inclination:       51
6487  deg
RA of node:       241
0311  deg
Eccentricity:     
0005688     
Arg of perigee:   353
1195  deg
Mean anomaly:       6
9890  deg
Mean motion:   15
75642848  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3844
Checksum:              314


Coasting Arc #2 (Orbit 3859)
---------------------------------------

Vector Time (GMT): 2011/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905423
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2704125
28                 A    =         6726416
66  meter
 Y    =        5971164
23  meter          E    =           
0004884
 Z    =       -1510366
28                 I    =           51
38120
 XDOT =      -5037
273482                 Wp   =          101
97332
 YDOT =        828
098617  meter/sec      RA   =          235
02942  deg
 ZDOT =      -5761
455852                 TA   =           94
72776
                                          MA   =           94
67199
                                          Ha   =            188
385  n
mi
                                          Hp   =            180
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8871802
11                 X    =         2644490
73
 Y    =       19590433
84  feet           Y    =         6001070
22  meter
 Z    =       -4955269
96                 Z    =        -1497373
41
 XDOT =     -16526
487802                 XDOT =       -5018
170774
 YDOT =       2716
858979  feet/sec       YDOT =         771
876541  meter/sec
 ZDOT =     -18902
414213                 ZDOT =       -5785
880545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21458246
83                 X    =         6540473
63
 Y    =       -1598082
82  feet           Y    =         -487095
64  meter
 Z    =       -4902901
73                 Z    =        -1494404
45
 XDOT =      -3228
342438                 XDOT =        -983
998775
 YDOT =      14777
612406  feet/sec       YDOT =        4504
216261  meter/sec
 ZDOT =     -19001
339303                 ZDOT =       -5791
608219


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   11153
52884435  
00016717  00000-0  10270-3 0  9018
2 25544  51
6477 235
8082 0005677 357
3225   2
7907 15
75681732 38609


Satellite: ISS
Catalog Number: 25544
Epoch time:      11153
52884435   =   yrday
fracday
Element set:     901
Inclination:       51
6477  deg
RA of node:       235
8082  deg
Eccentricity:     
0005677     
Arg of perigee:   357
3225  deg
Mean anomaly:       2
7907  deg
Mean motion:   15
75681732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3860
Checksum:              321


Coasting Arc #3 (Orbit 3866)
---------------------------------------

Vector Time (GMT): 2011/153/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         375403
92                 A    =         6725293
25  meter
 Y    =        5528686
40  meter          E    =           
0005102
 Z    =       -3816426
43                 I    =           51
36850
 XDOT =      -6012
516048                 Wp   =           68
40491
 YDOT =      -2443
709518  meter/sec      RA   =          232
72039  deg
 ZDOT =      -4134
092326                 TA   =          158
15469
                                          MA   =          158
13292
                                          Ha   =            189
315  n
mi
                                          Hp   =            183
944

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1231640
16                 X    =          332092
77
 Y    =       18138734
90  feet           Y    =         5532642
88  meter
 Z    =      -12521084
08                 Z    =        -3814706
97
 XDOT =     -19726
102520                 XDOT =       -5964
660394
 YDOT =      -8017
419678  feet/sec       YDOT =       -2510
676845  meter/sec
 ZDOT =     -13563
295033                 ZDOT =       -4163
185434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15094607
92                 X    =        -4600836
49
 Y    =      -10141611
14  feet           Y    =        -3091163
08  meter
 Z    =      -12514340
69                 Z    =        -3814371
04
 XDOT =      17676
139248                 XDOT =        5387
687243
 YDOT =      -9437
510337  feet/sec       YDOT =       -2876
553151  meter/sec
 ZDOT =     -13680
998707                 ZDOT =       -4169
968406


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   11153
97281777  
00016717  00000-0  10270-3 0  9028
2 25544  51
6450 233
5236 0001371 282
0921  78
0089 15
74196594 38670


Satellite: ISS
Catalog Number: 25544
Epoch time:      11153
97281777   =   yrday
fracday
Element set:     902
Inclination:       51
6450  deg
RA of node:       233
5236  deg
Eccentricity:     
0001371     
Arg of perigee:   282
0921  deg
Mean anomaly:      78
0089  deg
Mean motion:   15
74196594  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3867
Checksum:              322


Coasting Arc #4 (Orbit 3882)
---------------------------------------

Vector Time (GMT): 2011/154/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5438111
80                 A    =         6725988
24  meter
 Y    =        1749346
41  meter          E    =           
0010822
 Z    =        3542181
71                 I    =           51
38997
 XDOT =        896
872890                 Wp   =           84
31183
 YDOT =       6229
989110  meter/sec      RA   =          227
51324  deg
 ZDOT =      -4440
996378                 TA   =           53
28072
                                          MA   =           53
18136
                                          Ha   =            189
197  n
mi
                                          Hp   =            183
883

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17841574
13                 X    =         5400938
82
 Y    =        5739325
50  feet           Y    =         1809950
24  meter
 Z    =       11621331
08                 Z    =         3568510
07
 XDOT =       2942
496357                 XDOT =         848
714851
 YDOT =      20439
596817  feet/sec       YDOT =        6239
749967  meter/sec
 ZDOT =     -14570
198090                 ZDOT =       -4436
755297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15285062
91                 X    =        -4658887
18
 Y    =       10730357
92  feet           Y    =         3270613
09  meter
 Z    =       11727882
65                 Z    =         3574658
63
 XDOT =     -17358
822468                 XDOT =       -5290
969088
 YDOT =      -8775
899488  feet/sec       YDOT =       -2674
894164  meter/sec
 ZDOT =     -14553
264717                 ZDOT =       -4435
835086


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   11154
98851667  
00016717  00000-0  10270-3 0  9032
2 25544  51
6441 228
3067 0001377 286
1889  73
9123 15
74220667 38838


Satellite: ISS
Catalog Number: 25544
Epoch time:      11154
98851667   =   yrday
fracday
Element set:     903
Inclination:       51
6441  deg
RA of node:       228
3067  deg
Eccentricity:     
0001377     
Arg of perigee:   286
1889  deg
Mean anomaly:      73
9123  deg
Mean motion:   15
74220667  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3883
Checksum:              334


Coasting Arc #5 (Orbit 3898)
---------------------------------------

Vector Time (GMT): 2011/155/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1158159
24                 A    =         6724660
60  meter
 Y    =       -5318531
02  meter          E    =           
0009712
 Z    =        3941679
92                 I    =           51
40751
 XDOT =       6411
460723                 Wp   =           98
94809
 YDOT =       1558
242799  meter/sec      RA   =          222
41022  deg
 ZDOT =       3976
573249                 TA   =          309
67724
                                          MA   =          309
76286
                                          Ha   =            189
235  n
mi
                                          Hp   =            183
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3799735
02                 X    =        -1117748
22
 Y    =      -17449248
77  feet           Y    =        -5331256
94  meter
 Z    =       12932020
72                 Z    =         3936150
92
 XDOT =      21034
976124                 XDOT =        6374
242237
 YDOT =       5112
345141  feet/sec       YDOT =        1629
730918  meter/sec
 ZDOT =      13046
500162                 ZDOT =        4007
629857

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16389586
21                 X    =         4995545
88
 Y    =        7132267
06  feet           Y    =         2173915
00  meter
 Z    =       12909828
01                 Z    =         3934915
58
 XDOT =     -15945
254044                 XDOT =       -4860
113433
 YDOT =      12740
501358  feet/sec       YDOT =        3883
304814  meter/sec
 ZDOT =      13172
224313                 ZDOT =        4014
893970


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   11156
00418314  
00016717  00000-0  10270-3 0  9046
2 25544  51
6442 223
0888 0001423 294
3360  65
7655 15
74272716 38997


Satellite: ISS
Catalog Number: 25544
Epoch time:      11156
00418314   =   yrday
fracday
Element set:     904
Inclination:       51
6442  deg
RA of node:       223
0888  deg
Eccentricity:     
0001423     
Arg of perigee:   294
3360  deg
Mean anomaly:      65
7655  deg
Mean motion:   15
74272716  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3899
Checksum:              307


Coasting Arc #6 (Orbit 3913)
---------------------------------------

Vector Time (GMT): 2011/156/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5733919
69                 A    =         6726138
47  meter
 Y    =        -966791
22  meter          E    =           
0003686
 Z    =       -3383123
00                 I    =           51
43720
 XDOT =      -1718
942127                 Wp   =           80
83559
 YDOT =      -5919
041759  meter/sec      RA   =          217
20526  deg
 ZDOT =       4609
688087                 TA   =          239
13815
                                          MA   =          239
17441
                                          Ha   =            189
090  n
mi
                                          Hp   =            183
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18812072
46                 X    =        -5706248
19
 Y    =       -3171887
21  feet           Y    =        -1030756
20  meter
 Z    =      -11099484
91                 Z    =        -3410911
14
 XDOT =      -5639
573907                 XDOT =       -1675
019397
 YDOT =     -19419
428343  feet/sec       YDOT =       -5938
019076  meter/sec
 ZDOT =      15123
648581                 ZDOT =        4601
443373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13364579
84                 X    =         4073523
94
 Y    =      -13521552
30  feet           Y    =        -4121369
14  meter
 Z    =      -11212008
44                 Z    =        -3417420
17
 XDOT =      18200
848757                 XDOT =        5547
618701
 YDOT =       5489
653654  feet/sec       YDOT =        1673
246434  meter/sec
 ZDOT =      15090
468250                 ZDOT =        4599
574723


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   11156
95634147  
00016717  00000-0  10270-3 0  9055
2 25544  51
6445 218
1970 0001513 299
4126  60
6886 15
74336097 39144


Satellite: ISS
Catalog Number: 25544
Epoch time:      11156
95634147   =   yrday
fracday
Element set:     905
Inclination:       51
6445  deg
RA of node:       218
1970  deg
Eccentricity:     
0001513     
Arg of perigee:   299
4126  deg
Mean anomaly:      60
6886  deg
Mean motion:   15
74336097  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3914
Checksum:              323


Coasting Arc #7 (Orbit 3929)
---------------------------------------

Vector Time (GMT): 2011/157/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1796235
79                 A    =         6723739
34  meter
 Y    =        5004649
17  meter          E    =           
0006854
 Z    =       -4122750
47                 I    =           51
45473
 XDOT =      -6689
635111                 Wp   =           59
64411
 YDOT =       -679
185194  meter/sec      RA   =          212
10446  deg
 ZDOT =      -3740
276827                 TA   =          171
93329
                                          MA   =          171
92226
                                          Ha   =            189
059  n
mi
                                          Hp   =            183
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5893162
05                 X    =         1760166
78
 Y    =       16419452
66  feet           Y    =         5024534
59  meter
 Z    =      -13526084
22                 Z    =        -4114111
43
 XDOT =     -21947
621754                 XDOT =       -6663
373675
 YDOT =      -2228
297882  feet/sec       YDOT =        -753
845474  meter/sec
 ZDOT =     -12271
249432                 ZDOT =       -3772
711154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16947062
09                 X    =        -5165464
53
 Y    =       -4250368
72  feet           Y    =        -1295512
39  meter
 Z    =      -13491263
51                 Z    =        -4112137
12
 XDOT =      13791
297917                 XDOT =        4203
587605
 YDOT =     -15633
613029  feet/sec       YDOT =       -4765
125251  meter/sec
 ZDOT =     -12402
618352                 ZDOT =       -3780
318074


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   11157
97194705  
00016717  00000-0  10270-3 0  9060
2 25544  51
6447 212
9789 0001647 304
1871  55
9136 15
74382708 39308


Satellite: ISS
Catalog Number: 25544
Epoch time:      11157
97194705   =   yrday
fracday
Element set:     906
Inclination:       51
6447  deg
RA of node:       212
9789  deg
Eccentricity:     
0001647     
Arg of perigee:   304
1871  deg
Mean anomaly:      55
9136  deg
Mean motion:   15
74382708  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3930
Checksum:              332


Coasting Arc #8 (Orbit 3945)
---------------------------------------

Vector Time (GMT): 2011/158/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5938292
72                 A    =         6726590
08  meter
 Y    =         208933
79  meter          E    =           
0011765
 Z    =        3142847
66                 I    =           51
49136
 XDOT =       2370
700479                 Wp   =           89
25045
 YDOT =       5512
619190  meter/sec      RA   =          206
90367  deg
 ZDOT =      -4830
141864                 TA   =           54
05863
                                          MA   =           53
94954
                                          Ha   =            189
007  n
mi
                                          Hp   =            183
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19482587
65                 X    =         5920247
72
 Y    =         685478
31  feet           Y    =          275238
17  meter
 Z    =       10311180
00                 Z    =         3171651
94
 XDOT =       7777
888709                 XDOT =        2332
344953
 YDOT =      18086
020964  feet/sec       YDOT =        5538
915832  meter/sec
 ZDOT =     -15846
922125                 ZDOT =       -4818
717665

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11176976
45                 X    =        -3406742
42
 Y    =       15896421
93  feet           Y    =         4845229
40  meter
 Z    =       10427871
41                 Z    =         3178415
21
 XDOT =     -18291
211118                 XDOT =       -5575
161149
 YDOT =      -2462
248604  feet/sec       YDOT =        -750
493374  meter/sec
 ZDOT =     -15800
826438                 ZDOT =       -4816
091898


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   11158
98752288  
00016717  00000-0  10270-3 0  9079
2 25544  51
6445 207
7606 0001562 311
5638  48
5392 15
74418778 39461


Satellite: ISS
Catalog Number: 25544
Epoch time:      11158
98752288   =   yrday
fracday
Element set:     907
Inclination:       51
6445  deg
RA of node:       207
7606  deg
Eccentricity:     
0001562     
Arg of perigee:   311
5638  deg
Mean anomaly:      48
5392  deg
Mean motion:   15
74418778  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3946
Checksum:              344


Coasting Arc #9 (Orbit 3961)
---------------------------------------

Vector Time (GMT): 2011/159/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2303774
93                 A    =         6722839
61  meter
 Y    =       -4612210
46  meter          E    =           
0008340
 Z    =        4308894
57                 I    =           51
50724
 XDOT =       6883
646420                 Wp   =          103
35679
 YDOT =       -204
529917  meter/sec      RA   =          201
80392  deg
 ZDOT =       3453
971879                 TA   =          311
66236
                                          MA   =          311
73373
                                          Ha   =            189
086  n
mi
                                          Hp   =            183
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7558316
72                 X    =        -2272960
89
 Y    =      -15131924
07  feet           Y    =        -4637800
76  meter
 Z    =       14136793
22                 Z    =         4297777
28
 XDOT =      22584
141798                 XDOT =        6868
643153
 YDOT =       -671
029912  feet/sec       YDOT =        -127
636997  meter/sec
 ZDOT =      11331
928738                 ZDOT =        3487
376135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16879422
02                 X    =         5144847
83
 Y    =        1567026
87  feet           Y    =          477629
79  meter
 Z    =       14091903
32                 Z    =         4295212
13
 XDOT =     -11283
574940                 XDOT =       -3439
233642
 YDOT =      18198
413493  feet/sec       YDOT =        5546
876433  meter/sec
 ZDOT =      11467
282108                 ZDOT =        3495
227586


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   11160
00306694  
00016717  00000-0  10270-3 0  9082
2 25544  51
6449 202
5417 0001661 316
7308  43
3725 15
74457222 39627


Satellite: ISS
Catalog Number: 25544
Epoch time:      11160
00306694   =   yrday
fracday
Element set:     908
Inclination:       51
6449  deg
RA of node:       202
5417  deg
Eccentricity:     
0001661     
Arg of perigee:   316
7308  deg
Mean anomaly:      43
3725  deg
Mean motion:   15
74457222  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3962
Checksum:              293


Coasting Arc #10 (Orbit 3976)
---------------------------------------

Vector Time (GMT): 2011/160/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6057436
45                 A    =         6727043
49  meter
 Y    =         569592
86  meter          E    =           
0004371
 Z    =       -2868101
29                 I    =           51
55112
 XDOT =      -2866
041471                 Wp   =           42
18897
 YDOT =      -5046
123406  meter/sec      RA   =          196
60835  deg
 ZDOT =       5058
575439                 TA   =          284
82321
                                          MA   =          284
87163
                                          Ha   =            188
883  n
mi
                                          Hp   =            183
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19873479
17                 X    =        -6049422
78
 Y    =        1868742
98  feet           Y    =          501899
99  meter
 Z    =       -9409781
12                 Z    =        -2897508
90
 XDOT =      -9403
023199                 XDOT =       -2833
975461
 YDOT =     -16555
522985  feet/sec       YDOT =       -5077
994393  meter/sec
 ZDOT =      16596
376112                 ZDOT =        5044
729591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8641630
93                 X    =         2633969
11
 Y    =      -17930767
88  feet           Y    =        -5465298
05  meter
 Z    =       -9528962
88                 Z    =        -2904427
88
 XDOT =      17775
946630                 XDOT =        5418
108533
 YDOT =       -209
950159  feet/sec       YDOT =         -63
992808  meter/sec
 ZDOT =      16540
439731                 ZDOT =        5041
526030


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   11160
95511071  
00016717  00000-0  10270-3 0  9094
2 25544  51
6448 197
6491 0001862 317
2861  42
8158 15
74512647 39778


Satellite: ISS
Catalog Number: 25544
Epoch time:      11160
95511071   =   yrday
fracday
Element set:     909
Inclination:       51
6448  deg
RA of node:       197
6491  deg
Eccentricity:     
0001862     
Arg of perigee:   317
2861  deg
Mean anomaly:      42
8158  deg
Mean motion:   15
74512647  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3977
Checksum:              326


Coasting Arc #11 (Orbit 3992)
---------------------------------------

Vector Time (GMT): 2011/161/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2650488
27                 A    =         6721721
26  meter
 Y    =        4209141
27  meter          E    =           
0009479
 Z    =       -4530482
78                 I    =           51
56257
 XDOT =      -6968
278203                 Wp   =           59
10796
 YDOT =       1074
416794  meter/sec      RA   =          191
50969  deg
 ZDOT =      -3078
440250                 TA   =          180
17149
                                          MA   =          180
17181
                                          Ha   =            188
872  n
mi
                                          Hp   =            183
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8695827
64                 X    =         2625232
27
 Y    =       13809518
60  feet           Y    =         4238639
91  meter
 Z    =      -14863788
66                 Z    =        -4517667
51
 XDOT =     -22861
805127                 XDOT =       -6964
820020
 YDOT =       3524
989480  feet/sec       YDOT =         996
512935  meter/sec
 ZDOT =     -10099
869588                 ZDOT =       -3112
283887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16352789
14                 X    =        -4984330
13
 Y    =         665927
21  feet           Y    =          202974
61  meter
 Z    =      -14811997
30                 Z    =        -4514696
78
 XDOT =       8446
067929                 XDOT =        2574
361505
 YDOT =     -20296
593620  feet/sec       YDOT =       -6186
401735  meter/sec
 ZDOT =     -10237
055591                 ZDOT =       -3120
254544


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   11161
97059494  
00016717  00000-0  10270-3 0  9105
2 25544  51
6441 192
4301 0001914 319
1011  41
0008 15
74562500 39936


Satellite: ISS
Catalog Number: 25544
Epoch time:      11161
97059494   =   yrday
fracday
Element set:     910
Inclination:       51
6441  deg
RA of node:       192
4301  deg
Eccentricity:     
0001914     
Arg of perigee:   319
1011  deg
Mean anomaly:      41
0008  deg
Mean motion:   15
74562500  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3993
Checksum:              275


Coasting Arc #12 (Orbit 4008)
---------------------------------------

Vector Time (GMT): 2011/162/22:46:52
195
Vector Time (MET): N/A
Weight (LBS)     : 904691
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6100897
80                 A    =         6727590
15  meter
 Y    =       -1315390
72  meter          E    =           
0012510
 Z    =        2498317
02                 I    =           51
61375
 XDOT =       3173
215435                 Wp   =           98
35589
 YDOT =       4586
532591  meter/sec      RA   =          186
32169  deg
 ZDOT =      -5313
357025                 TA   =           53
34233
                                          MA   =           53
22740
                                          Ha   =            188
821  n
mi
                                          Hp   =            183
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20016068
91                 X    =         6103016
83
 Y    =       -4315586
35  feet           Y    =        -1247155
25  meter
 Z    =        8196578
17                 Z    =         2527960
46
 XDOT =      10410
811796                 XDOT =        3147
503680
 YDOT =      15047
679103  feet/sec       YDOT =        4621
874348  meter/sec
 ZDOT =     -17432
273703                 ZDOT =       -5298
003243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5955658
95                 X    =        -1815284
85
 Y    =       19540029
52  feet           Y    =         5955801
00  meter
 Z    =        8316764
20                 Z    =         2534949
73
 XDOT =     -16838
064795                 XDOT =       -5132
242150
 YDOT =       2289
715123  feet/sec       YDOT =         697
905169  meter/sec
 ZDOT =     -17370
204953                 ZDOT =       -5294
438470


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   11162
98604871  
00016717  00000-0  10270-3 0  9113
2 25544  51
6442 187
2113 0001892 327
2556  32
8490 15
74630033 40098


Satellite: ISS
Catalog Number: 25544
Epoch time:      11162
98604871   =   yrday
fracday
Element set:     911
Inclination:       51
6442  deg
RA of node:       187
2113  deg
Eccentricity:     
0001892     
Arg of perigee:   327
2556  deg
Mean anomaly:      32
8490  deg
Mean motion:   15
74630033  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4009
Checksum:              295


Coasting Arc #13 (Orbit 4018)
---------------------------------------

Vector Time (GMT): 2011/163/14:43:41
641
Vector Time (MET): N/A
Weight (LBS)     : 903229
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5333971
42                 A    =         6734202
52  meter
 Y    =        2382988
07  meter          E    =           
0005895
 Z    =       -3346015
73                 I    =           51
62312
 XDOT =      -4688
791896                 Wp   =          257
03421
 YDOT =      -3935
496481  meter/sec      RA   =          182
90026  deg
 ZDOT =       4663
541678                 TA   =           63
62195
                                          MA   =           63
56144
                                          Ha   =            191
938  n
mi
                                          Hp   =            190
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17499906
23                 X    =        -5343967
51
 Y    =        7818202
33  feet           Y    =         2323284
97  meter
 Z    =      -10977741
89                 Z    =        -3371952
35
 XDOT =     -15383
175513                 XDOT =       -4667
090798
 YDOT =     -12911
733862  feet/sec       YDOT =       -3987
808761  meter/sec
 ZDOT =      15300
333590                 ZDOT =        4640
815419

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15625538
34                 X    =         4762664
09
 Y    =       10995115
64  feet           Y    =         3351311
25  meter
 Z    =      -11082951
16                 Z    =        -3378083
51
 XDOT =      -2394
114436                 XDOT =        -729
726080
 YDOT =      18758
992042  feet/sec       YDOT =        5717
740774  meter/sec
 ZDOT =      15208
358232                 ZDOT =        4635
507589


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   11163
62070908  
00016717  00000-0  10270-3 0  9124
2 25544  51
6404 183
9483 0010687 262
5080  97
4868 15
71552440 40193


Satellite: ISS
Catalog Number: 25544
Epoch time:      11163
62070908   =   yrday
fracday
Element set:     912
Inclination:       51
6404  deg
RA of node:       183
9483  deg
Eccentricity:     
0010687     
Arg of perigee:   262
5080  deg
Mean anomaly:      97
4868  deg
Mean motion:   15
71552440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4019
Checksum:              311


Coasting Arc #14 (Orbit 4021)
---------------------------------------

Vector Time (GMT): 2011/163/18:55:21
516
Vector Time (MET): N/A
Weight (LBS)     : 901478
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4216096
85                 A    =         6742502
26  meter
 Y    =        3357795
66  meter          E    =           
0008786
 Z    =       -4046110
33                 I    =           51
62326
 XDOT =      -5993
587023                 Wp   =          170
04383
 YDOT =       2860
377964  meter/sec      RA   =          182
05788  deg
 ZDOT =      -3881
352654                 TA   =           59
93546
                                          MA   =           59
84835
                                          Ha   =            201
512  n
mi
                                          Hp   =            193
156

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13832338
75                 X    =         4197891
44
 Y    =       11016389
98  feet           Y    =         3404841
45  meter
 Z    =      -13274640
20                 Z    =        -4025672
03
 XDOT =     -19663
999419                 XDOT =       -6006
271766
 YDOT =       9384
442138  feet/sec       YDOT =        2793
283709  meter/sec
 ZDOT =     -12734
096635                 ZDOT =       -3910
500161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14611798
02                 X    =        -4453676
04
 Y    =      -10068723
96  feet           Y    =        -3068947
06  meter
 Z    =      -13191916
92                 Z    =        -4020896
28
 XDOT =      18187
430666                 XDOT =        5543
528867
 YDOT =      -9596
865211  feet/sec       YDOT =       -2925
124516  meter/sec
 ZDOT =     -12852
339958                 ZDOT =       -3917
393219


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   11163
81156945  
00016717  00000-0  10270-3 0  9132
2 25544  51
6424 182
9734 0012103 205
7375 154
3184 15
67935606 40226


Satellite: ISS
Catalog Number: 25544
Epoch time:      11163
81156945   =   yrday
fracday
Element set:     913
Inclination:       51
6424  deg
RA of node:       182
9734  deg
Eccentricity:     
0012103     
Arg of perigee:   205
7375  deg
Mean anomaly:     154
3184  deg
Mean motion:   15
67935606  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4022
Checksum:              302


Coasting Arc #15 (Orbit 4037)
---------------------------------------

Vector Time (GMT): 2011/164/18:55:21
516
Vector Time (MET): N/A
Weight (LBS)     : 901478
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2976259
76                 A    =         6739959
43  meter
 Y    =       -3851365
53  meter          E    =           
0006980
 Z    =        4658099
13                 I    =           51
64496
 XDOT =       6892
527282                 Wp   =          171
33354
 YDOT =       1887
527650  meter/sec      RA   =          176
92233  deg
 ZDOT =      -2849
519437                 TA   =          306
81925
                                          MA   =          306
88326
                                          Ha   =            201
173  n
mi
                                          Hp   =            193
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9764631
74                 X    =         2996476
89
 Y    =      -12635713
68  feet           Y    =        -3817970
98  meter
 Z    =       15282477
46                 Z    =         4672606
33
 XDOT =      22613
278484                 XDOT =        6884
750864
 YDOT =       6192
676016  feet/sec       YDOT =        1964
561105  meter/sec
 ZDOT =      -9348
817051                 ZDOT =       -2816
053833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8584149
07                 X    =        -2616448
64
 Y    =       13398373
78  feet           Y    =         4083824
33  meter
 Z    =       15341426
77                 Z    =         4676066
88
 XDOT =     -22129
774869                 XDOT =       -6745
155380
 YDOT =      -3652
155173  feet/sec       YDOT =       -1113
176897  meter/sec
 ZDOT =      -9213
222359                 ZDOT =       -2808
190175


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   11164
83133132  
00016717  00000-0  10270-3 0  9149
2 25544  51
6415 177
7840 0012089 209
8597 150
1875 15
67962752 40380


Satellite: ISS
Catalog Number: 25544
Epoch time:      11164
83133132   =   yrday
fracday
Element set:     914
Inclination:       51
6415  deg
RA of node:       177
7840  deg
Eccentricity:     
0012089     
Arg of perigee:   209
8597  deg
Mean anomaly:     150
1875  deg
Mean motion:   15
67962752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4038
Checksum:              323


Coasting Arc #16 (Orbit 4053)
---------------------------------------

Vector Time (GMT): 2011/165/18:55:21
516
Vector Time (MET): N/A
Weight (LBS)     : 901478
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6705690
85                 A    =         6749218
66  meter
 Y    =         467772
03  meter          E    =           
0003979
 Z    =         615868
38                 I    =           51
70671
 XDOT =        217
568856                 Wp   =          116
76926
 YDOT =      -4808
367547  meter/sec      RA   =          171
86127  deg
 ZDOT =       5989
567652                 TA   =          249
90641
                                          MA   =          249
94923
                                          Ha   =            201
003  n
mi
                                          Hp   =            193
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22000298
07                 X    =        -6713414
97
 Y    =        1534685
15  feet           Y    =          392741
62  meter
 Z    =        2020565
55                 Z    =          583273
35
 XDOT =        713
808584                 XDOT =         242
224458
 YDOT =     -15775
484077  feet/sec       YDOT =       -4805
797870  meter/sec
 ZDOT =      19650
812507                 ZDOT =        5990
683556

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21745916
40                 X    =         6628155
32
 Y    =       -3741676
94  feet           Y    =        -1140463
13  meter
 Z    =        1888394
07                 Z    =          575582
51
 XDOT =        721
452541                 XDOT =         219
898734
 YDOT =      14168
688217  feet/sec       YDOT =        4318
616169  meter/sec
 ZDOT =      19655
515718                 ZDOT =        5991
001191


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   11165
85107233  
00016717  00000-0  10270-3 0  9156
2 25544  51
6418 172
5930 0012067 213
8832 146
1558 15
67978886 40545


Satellite: ISS
Catalog Number: 25544
Epoch time:      11165
85107233   =   yrday
fracday
Element set:     915
Inclination:       51
6418  deg
RA of node:       172
5930  deg
Eccentricity:     
0012067     
Arg of perigee:   213
8832  deg
Mean anomaly:     146
1558  deg
Mean motion:   15
67978886  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4054
Checksum:              325


Coasting Arc #17 (Orbit 4066)
---------------------------------------

Vector Time (GMT): 2011/166/15:19:32
493
Vector Time (MET): N/A
Weight (LBS)     : 900197
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3405429
75                 A    =         6749555
74  meter
 Y    =       -4096348
21  meter          E    =           
0012469
 Z    =        4131909
75                 I    =           51
70493
 XDOT =       6511
939760                 Wp   =          108
78922
 YDOT =       1605
825212  meter/sec      RA   =          167
50585  deg
 ZDOT =      -3769
681118                 TA   =           19
86534
                                          MA   =           19
81682
                                          Ha   =            205
121  n
mi
                                          Hp   =            196
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11172669
79                 X    =         3430910
77
 Y    =      -13439462
63  feet           Y    =        -4058124
98  meter
 Z    =       13556134
34                 Z    =         4148514
38
 XDOT =      21364
631757                 XDOT =        6511
811526
 YDOT =       5268
455419  feet/sec       YDOT =        1678
645715  meter/sec
 ZDOT =     -12367
720205                 ZDOT =       -3738
046146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17398595
11                 X    =        -5303091
79
 Y    =         949915
18  feet           Y    =          289534
15  meter
 Z    =       13623620
44                 Z    =         4152479
51
 XDOT =     -10583
884223                 XDOT =       -3225
967911
 YDOT =     -18066
980726  feet/sec       YDOT =       -5506
815725  meter/sec
 ZDOT =     -12239
501841                 ZDOT =       -3730
600161


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   11166
67970212  
00016717  00000-0  10270-3 0  9163
2 25544  51
6387 168
3752 0006827 164
4635 195
6734 15
65320494 40677


Satellite: ISS
Catalog Number: 25544
Epoch time:      11166
67970212   =   yrday
fracday
Element set:     916
Inclination:       51
6387  deg
RA of node:       168
3752  deg
Eccentricity:     
0006827     
Arg of perigee:   164
4635  deg
Mean anomaly:     195
6734  deg
Mean motion:   15
65320494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4067
Checksum:              334


Coasting Arc #18 (Orbit 4069)
---------------------------------------

Vector Time (GMT): 2011/166/19:26:11
597
Vector Time (MET): N/A
Weight (LBS)     : 898627
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6613107
00                 A    =         6765771
54  meter
 Y    =         501672
14  meter          E    =           
0007830
 Z    =        1313137
78                 I    =           51
73469
 XDOT =        789
046642                 Wp   =           36
27016
 YDOT =      -4923
096859  meter/sec      RA   =          166
67694  deg
 ZDOT =       5842
984019                 TA   =          338
05205
                                          MA   =          338
08556
                                          Ha   =            206
291  n
mi
                                          Hp   =            205
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21696545
28                 X    =        -6624604
26
 Y    =        1645905
97  feet           Y    =          427655
81  meter
 Z    =        4308194
80                 Z    =         1280983
55
 XDOT =       2588
735701                 XDOT =         815
654930
 YDOT =     -16151
892581  feet/sec       YDOT =       -4914
125658  meter/sec
 ZDOT =      19169
895074                 ZDOT =        5846
880842

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20619213
79                 X    =         6284736
36
 Y    =       -7028779
33  feet           Y    =        -2142371
94  meter
 Z    =        4177787
70                 Z    =         1273389
69
 XDOT =       1133
626245                 XDOT =         345
529279
 YDOT =      14752
562276  feet/sec       YDOT =        4496
580982  meter/sec
 ZDOT =      19185
883359                 ZDOT =        5847
857248


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   11166
87136542  
00016717  00000-0  10270-3 0  9176
2 25544  51
6411 167
4063 0007317 264
1441  95
8881 15
62027894 40701


Satellite: ISS
Catalog Number: 25544
Epoch time:      11166
87136542   =   yrday
fracday
Element set:     917
Inclination:       51
6411  deg
RA of node:       167
4063  deg
Eccentricity:     
0007317     
Arg of perigee:   264
1441  deg
Mean anomaly:      95
8881  deg
Mean motion:   15
62027894  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4070
Checksum:              311

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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