[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 23rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
There are no maneuvers
Coasting Arc #1 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2011/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4128115
78 A = 6726340
90 meter
Y = 937238
14 meter E =
0015340
Z = -5240451
37 I = 51
29940
XDOT = -2274
050359 Wp = 89
79052
YDOT = -7326
308664 meter/sec RA = 249
86834 deg
ZDOT = 482
348480 TA = 184
81427
MA = 184
82904
Ha = 193
623 n
mi
Hp = 186
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13543686
93 X = -4112832
18
Y = 3074928
29 feet Y = 891159
94 meter
Z = -17193081
92 Z = -5260468
72
XDOT = -7460
795142 XDOT = -2194
300330
YDOT = -24036
445749 feet/sec YDOT = -7351
292515 meter/sec
ZDOT = 1582
508136 ZDOT = 471
495655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13545434
95 X = -4128648
57
Y = 2573396
65 feet Y = 784371
30 meter
Z = -17273897
29 Z = -5265083
89
XDOT = -6385
417707 XDOT = -1946
275317
YDOT = -23309
274183 feet/sec YDOT = -7104
666771 meter/sec
ZDOT = 1538
802565 ZDOT = 469
027022
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 11080
51512531
00016717 00000-0 10270-3 0 9000
2 25544 51
6422 250
6713 0001133 23
3047 336
8166 15
71839746 27107
Satellite: ISS
Catalog Number: 25544
Epoch time: 11080
51512531 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 250
6713 deg
Eccentricity:
0001133
Arg of perigee: 23
3047 deg
Mean anomaly: 336
8166 deg
Mean motion: 15
71839746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2710
Checksum: 271
Coasting Arc #2 (Orbit 2725)
---------------------------------------
Vector Time (GMT): 2011/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3051789
62 A = 6738060
79 meter
Y = 5996296
38 meter E =
0012182
Z = 249787
22 I = 51
35134
XDOT = -4182
867955 Wp = 126
55478
YDOT = 2387
122708 meter/sec RA = 244
72764 deg
ZDOT = -6004
436608 TA = 50
72245
MA = 50
61446
Ha = 193
485 n
mi
Hp = 186
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10012433
12 X = 2983297
65
Y = 19672888
39 feet Y = 6030040
40 meter
Z = 819511
88 Z = 264445
98
XDOT = -13723
320062 XDOT = -4180
081840
YDOT = 7831
767415 feet/sec YDOT = 2340
362438 meter/sec
ZDOT = -19699
595169 ZDOT = -6024
750418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9613648
28 X = 2930239
99
Y = 19868285
75 feet Y = 6055853
50 meter
Z = 878602
68 Z = 267798
10
XDOT = -12309
664412 XDOT = -3751
985713
YDOT = 6857
490860 feet/sec YDOT = 2090
163214 meter/sec
ZDOT = -19781
631259 ZDOT = -6029
441208
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 11081
53233999
00016717 00000-0 10270-3 0 9012
2 25544 51
6422 245
4635 0001367 15
3255 344
7948 15
71923781 27269
Satellite: ISS
Catalog Number: 25544
Epoch time: 11081
53233999 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 245
4635 deg
Eccentricity:
0001367
Arg of perigee: 15
3255 deg
Mean anomaly: 344
7948 deg
Mean motion: 15
71923781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2726
Checksum: 315
Coasting Arc #3 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2011/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2968611
25 A = 6726447
67 meter
Y = -3113833
10 meter E =
0003802
Z = 5167702
65 I = 51
32635
XDOT = 4566
051770 Wp = 104
21663
YDOT = 6110
109313 meter/sec RA = 239
59818 deg
ZDOT = 1057
126091 TA = 335
64712
MA = 335
66508
Ha = 193
459 n
mi
Hp = 186
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9739538
21 X = 2978106
34
Y = -10215987
86 feet Y = -3080582
91 meter
Z = 16954405
00 Z = 5182147
38
XDOT = 14980
484810 XDOT = 4492
252681
YDOT = 20046
290396 feet/sec YDOT = 6160
757097 meter/sec
ZDOT = 3468
261454 ZDOT = 1079
128353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9665612
14 X = 2946078
58
Y = -10189146
07 feet Y = -3105651
72 meter
Z = 17012763
03 Z = 5185490
17
XDOT = 14162
071768 XDOT = 4316
599475
YDOT = 19382
082746 feet/sec YDOT = 5907
658821 meter/sec
ZDOT = 3557
002086 ZDOT = 1084
174236
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 11082
54952910
00016717 00000-0 10270-3 0 9026
2 25544 51
6424 240
2560 0001293 25
2206 334
9019 15
71909107 27429
Satellite: ISS
Catalog Number: 25544
Epoch time: 11082
54952910 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 240
2560 deg
Eccentricity:
0001293
Arg of perigee: 25
2206 deg
Mean anomaly: 334
9019 deg
Mean motion: 15
71909107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 279
Coasting Arc #4 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2011/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4757838
33 A = 6736845
83 meter
Y = -4498354
44 meter E =
0009274
Z = -1569552
04 I = 51
37975
XDOT = 2398
063749 Wp = 36
75564
YDOT = -4530
710027 meter/sec RA = 234
43440 deg
ZDOT = 5740
525620 TA = 305
88536
MA = 305
97142
Ha = 193
455 n
mi
Hp = 186
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15609705
82 X = -4699558
70
Y = -14758380
71 feet Y = -4551233
68 meter
Z = -5149448
95 Z = -1592523
78
XDOT = 7867
663220 XDOT = 2420
662457
YDOT = -14864
534209 feet/sec YDOT = -4503
766843 meter/sec
ZDOT = 18833
745471 ZDOT = 5752
230435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15790854
29 X = -4813052
39
Y = -14531292
96 feet Y = -4429138
09 meter
Z = -5242135
78 Z = -1597802
99
XDOT = 6479
025303 XDOT = 1974
806912
YDOT = -13823
104814 feet/sec YDOT = -4213
282347 meter/sec
ZDOT = 18881
064808 ZDOT = 5754
948554
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 11083
50311418
00016717 00000-0 10270-3 0 9036
2 25544 51
6436 235
3744 0001251 30
5573 329
5662 15
71970538 27577
Satellite: ISS
Catalog Number: 25544
Epoch time: 11083
50311418 = yrday
fracday
Element set: 903
Inclination: 51
6436 deg
RA of node: 235
3744 deg
Eccentricity:
0001251
Arg of perigee: 30
5573 deg
Mean anomaly: 329
5662 deg
Mean motion: 15
71970538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 297
Coasting Arc #5 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2011/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1109276
64 A = 6727797
33 meter
Y = 4594851
70 meter E =
0012842
Z = -4799616
17 I = 51
36851
XDOT = -6061
945110 Wp = 68
35018
YDOT = -4035
228949 meter/sec RA = 229
33055 deg
ZDOT = -2462
671056 TA = 177
44249
MA = 177
43592
Ha = 193
440 n
mi
Hp = 186
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3639359
06 X = -1137259
22
Y = 15074972
76 feet Y = 4582290
47 meter
Z = -15746772
23 Z = -4805073
12
XDOT = -19888
271359 XDOT = -6004
408759
YDOT = -13238
940121 feet/sec YDOT = -4102
695673 meter/sec
ZDOT = -8079
629450 ZDOT = -2491
979855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3065637
94 X = -934406
44
Y = 15179106
83 feet Y = 4626591
76 meter
Z = -15768866
59 Z = -4806350
54
XDOT = -19142
272027 XDOT = -5834
564514
YDOT = -12380
388836 feet/sec YDOT = -3773
542517 meter/sec
ZDOT = -8197
922917 ZDOT = -2498
726905
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 11084
52024293
00016717 00000-0 10270-3 0 9042
2 25544 51
6437 230
1676 0001379 31
0787 329
0456 15
72027895 27733
Satellite: ISS
Catalog Number: 25544
Epoch time: 11084
52024293 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 230
1676 deg
Eccentricity:
0001379
Arg of perigee: 31
0787 deg
Mean anomaly: 329
0456 deg
Mean motion: 15
72027895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 309
Coasting Arc #6 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2011/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5643998
64 A = 6734486
62 meter
Y = 2472667
62 meter E =
0014167
Z = 2703140
24 I = 51
41166
XDOT = -22
667251 Wp = 96
13998
YDOT = 5715
708114 meter/sec RA = 224
14908 deg
ZDOT = -5159
405310 TA = 52
93241
MA = 52
80296
Ha = 193
355 n
mi
Hp = 186
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18517055
90 X = 5602798
11
Y = 8112426
58 feet Y = 2535551
97 meter
Z = 8868570
33 Z = 2730458
28
XDOT = -74
367620 XDOT = -61
516540
YDOT = 18752
323209 feet/sec YDOT = 5715
237219 meter/sec
ZDOT = -16927
182774 ZDOT = -5159
610009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18838126
07 X = 5741860
83
Y = 7200656
14 feet Y = 2194759
99 meter
Z = 8978859
68 Z = 2736756
43
XDOT = 1468
455353 XDOT = 447
585192
YDOT = 17354
218831 feet/sec YDOT = 5289
565900 meter/sec
ZDOT = -16928
078838 ZDOT = -5159
678430
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 11085
53734178
00016717 00000-0 10270-3 0 9055
2 25544 51
6431 224
9589 0001332 33
7465 326
3782 15
72049334 27893
Satellite: ISS
Catalog Number: 25544
Epoch time: 11085
53734178 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 224
9589 deg
Eccentricity:
0001332
Arg of perigee: 33
7465 deg
Mean anomaly: 326
3782 deg
Mean motion: 15
72049334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 322
Coasting Arc #7 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2011/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1107059
85 A = 6729991
59 meter
Y = -5169000
19 meter E =
0010814
Z = 4157029
46 I = 51
42105
XDOT = 6582
367800 Wp = 98
51955
YDOT = 1559
239045 meter/sec RA = 219
06069 deg
ZDOT = 3682
038624 TA = 313
73384
MA = 313
82333
Ha = 193
278 n
mi
Hp = 186
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3632086
13 X = -1069370
63
Y = -16958662
05 feet Y = -5181169
06 meter
Z = 13638548
08 Z = 4151743
25
XDOT = 21595
694882 XDOT = 6546
556460
YDOT = 5115
613664 feet/sec YDOT = 1632
647027 meter/sec
ZDOT = 12080
179214 ZDOT = 3713
928228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4825586
28 X = -1470838
70
Y = -16675800
53 feet Y = -5082784
00 meter
Z = 13617255
82 Z = 4150539
57
XDOT = 20597
937322 XDOT = 6278
251296
YDOT = 4035
226777 feet/sec YDOT = 1229
937122 meter/sec
ZDOT = 12208
956092 ZDOT = 3721
289817
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 11086
55440810
00016717 00000-0 10270-3 0 9066
2 25544 51
6442 219
7512 0001354 32
2634 327
8611 15
72140070 28054
Satellite: ISS
Catalog Number: 25544
Epoch time: 11086
55440810 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 219
7512 deg
Eccentricity:
0001354
Arg of perigee: 32
2634 deg
Mean anomaly: 327
8611 deg
Mean motion: 15
72140070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 274
Coasting Arc #8 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2011/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5638232
85 A = 6731507
67 meter
Y = -259192
04 meter E =
0006529
Z = -3673860
73 I = 51
45120
XDOT = -2537
031809 Wp = 89
52546
YDOT = -5841
902159 meter/sec RA = 213
87469 deg
ZDOT = 4312
354158 TA = 226
24517
MA = 226
29922
Ha = 193
272 n
mi
Hp = 186
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18498139
27 X = -5617068
80
Y = -850367
58 feet Y = -322124
09 meter
Z = -12053348
84 Z = -3701199
39
XDOT = -8323
595174 XDOT = -2492
466290
YDOT = -19166
345667 feet/sec YDOT = -5870
023313 meter/sec
ZDOT = 14148
143564 ZDOT = 4300
138105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18432598
85 X = -5618256
13
Y = 685183
37 feet Y = 208843
89 meter
Z = -12163770
93 Z = -3707517
38
XDOT = -9923
639717 XDOT = -3024
725386
YDOT = -17055
612655 feet/sec YDOT = -5198
550737 meter/sec
ZDOT = 14098
859390 ZDOT = 4297
332342
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 11087
50788197
00016717 00000-0 10270-3 0 9076
2 25544 51
6444 214
8692 0001543 31
8633 328
2622 15
72141985 28205
Satellite: ISS
Catalog Number: 25544
Epoch time: 11087
50788197 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 214
8692 deg
Eccentricity:
0001543
Arg of perigee: 31
8633 deg
Mean anomaly: 328
2622 deg
Mean motion: 15
72141985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 315
Coasting Arc #9 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2011/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3260063
62 A = 6732468
03 meter
Y = 4842805
80 meter E =
0005796
Z = -3359377
06 I = 51
48113
XDOT = -6072
787655 Wp = 79
89628
YDOT = 874
899845 meter/sec RA = 208
79183 deg
ZDOT = -4637
803000 TA = 139
70739
MA = 139
66443
Ha = 193
265 n
mi
Hp = 186
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10695746
79 X = 3221987
14
Y = 15888470
48 feet Y = 4879048
62 meter
Z = -11021578
27 Z = -3343632
82
XDOT = -19923
844011 XDOT = -6059
590349
YDOT = 2870
406315 feet/sec YDOT = 807
063640 meter/sec
ZDOT = -15215
889107 ZDOT = -4667
272157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12301291
38 X = 3749433
61
Y = 14728124
50 feet Y = 4489132
35 meter
Z = -10958022
64 Z = -3340005
30
XDOT = -18370
445932 XDOT = -5599
311920
YDOT = 3948
140908 feet/sec YDOT = 1203
393349 meter/sec
ZDOT = -15334
936880 ZDOT = -4674
088761
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 11088
52488992
00016717 00000-0 10270-3 0 9080
2 25544 51
6448 209
6605 0001542 36
7074 323
4193 15
72199299 28365
Satellite: ISS
Catalog Number: 25544
Epoch time: 11088
52488992 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 209
6605 deg
Eccentricity:
0001542
Arg of perigee: 36
7074 deg
Mean anomaly: 323
4193 deg
Mean motion: 15
72199299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 339
Coasting Arc #10 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2011/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4797982
93 A = 6728741
70 meter
Y = -1713656
26 meter E =
0010807
Z = 4389446
96 I = 51
49707
XDOT = 4831
124531 Wp = 65
16807
YDOT = 4994
276938 meter/sec RA = 203
61067 deg
ZDOT = -3320
140798 TA = 58
31407
MA = 58
20874
Ha = 193
192 n
mi
Hp = 186
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15741413
80 X = 4795465
90
Y = -5622231
81 feet Y = -1660015
93 meter
Z = 14401072
69 Z = 4412749
30
XDOT = 15850
146098 XDOT = 4791
046943
YDOT = 16385
423026 feet/sec YDOT = 5048
077079 meter/sec
ZDOT = -10892
850387 ZDOT = -3296
769370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14886481
46 X = 4537399
55
Y = -7421164
76 feet Y = -2261971
02 meter
Z = 14495222
57 Z = 4418143
84
XDOT = 17187
894143 XDOT = 5238
870135
YDOT = 13317
134102 feet/sec YDOT = 4059
062474 meter/sec
ZDOT = -10798
474382 ZDOT = -3291
374992
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 11089
54186769
00016717 00000-0 10270-3 0 9091
2 25544 51
6454 204
4525 0001732 42
0157 318
1138 15
72228667 28529
Satellite: ISS
Catalog Number: 25544
Epoch time: 11089
54186769 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 204
4525 deg
Eccentricity:
0001732
Arg of perigee: 42
0157 deg
Mean anomaly: 318
1138 deg
Mean motion: 15
72228667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 314
Coasting Arc #11 (Orbit 2867)
---------------------------------------
Vector Time (GMT): 2011/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5056872
23 A = 6734506
90 meter
Y = -3719397
29 meter E =
0015460
Z = 2417829
58 I = 51
54625
XDOT = 4710
000732 Wp = 70
79558
YDOT = -2907
321776 meter/sec RA = 198
52473 deg
ZDOT = 5355
769028 TA = 316
52512
MA = 316
64691
Ha = 193
218 n
mi
Hp = 185
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16590788
14 X = -5026650
64
Y = -12202747
01 feet Y = -3775777
05 meter
Z = 7932511
74 Z = 2393337
37
XDOT = 15452
758308 XDOT = 4716
143798
YDOT = -9538
457269 feet/sec YDOT = -2854
616744 meter/sec
ZDOT = 17571
420695 ZDOT = 5378
665225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18127979
80 X = -5525408
24
Y = -9853794
25 feet Y = -3003436
49 meter
Z = 7833588
94 Z = 2387677
91
XDOT = 13206
543090 XDOT = 4025
354334
YDOT = -10193
364772 feet/sec YDOT = -3106
937583 meter/sec
ZDOT = 17663
943149 ZDOT = 5383
969872
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 11090
55881190
00016717 00000-0 10270-3 0 9106
2 25544 51
6461 199
2436 0001787 41
7873 318
3425 15
72314918 28683
Satellite: ISS
Catalog Number: 25544
Epoch time: 11090
55881190 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 199
2436 deg
Eccentricity:
0001787
Arg of perigee: 41
7873 deg
Mean anomaly: 318
3425 deg
Mean motion: 15
72314918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2868
Checksum: 323
Coasting Arc #12 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2011/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3308694
22 A = 6726299
47 meter
Y = 3217630
42 meter E =
0013525
Z = -4905315
52 I = 51
54905
XDOT = -6549
107595 Wp = 99
21275
YDOT = -3362
687030 meter/sec RA = 193
35825 deg
ZDOT = 2214
763474 TA = 192
35423
MA = 192
38743
Ha = 193
114 n
mi
Hp = 185
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10855295
99 X = -3320599
46
Y = 10556530
24 feet Y = 3180563
46 meter
Z = -16093554
86 Z = -4921418
35
XDOT = -21486
573474 XDOT = -6521
777501
YDOT = -11032
437763 feet/sec YDOT = -3435
770058 meter/sec
ZDOT = 7266
284365 ZDOT = 2183
014872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9035126
78 X = -2753906
64
Y = 12064212
78 feet Y = 3677172
05 meter
Z = -16158636
82 Z = -4925152
50
XDOT = -22072
965923 XDOT = -6727
840013
YDOT = -6983
683329 feet/sec YDOT = -2128
626679 meter/sec
ZDOT = 7138
033934 ZDOT = 2175
672743
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 11091
51217089
00016717 00000-0 10270-3 0 9114
2 25544 51
6463 194
3615 0001895 42
6739 317
4570 15
72375781 28834
Satellite: ISS
Catalog Number: 25544
Epoch time: 11091
51217089 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 194
3615 deg
Eccentricity:
0001895
Arg of perigee: 42
6739 deg
Mean anomaly: 317
4570 deg
Mean motion: 15
72375781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 322
Coasting Arc #13 (Orbit 2898)
---------------------------------------
Vector Time (GMT): 2011/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6236783
68 A = 6735873
43 meter
Y = 2075473
35 meter E =
0008509
Z = -1461181
21 I = 51
61106
XDOT = -2762
726348 Wp = 130
41998
YDOT = 4239
962294 meter/sec RA = 188
26243 deg
ZDOT = -5797
193732 TA = 65
65253
MA = 65
56372
Ha = 193
138 n
mi
Hp = 185
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20461888
71 X = 6220209
95
Y = 6809295
77 feet Y = 2145124
02 meter
Z = -4793901
62 Z = -1430923
46
XDOT = -9064
062821 XDOT = -2781
771397
YDOT = 13910
637449 feet/sec YDOT = 4208
960671 meter/sec
ZDOT = -19019
664476 ZDOT = -5810
661776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21344575
21 X = 6505826
52
Y = 3259080
40 feet Y = 993367
71 meter
Z = -4671658
73 Z = -1423921
58
XDOT = -6240
609137 XDOT = -1902
137665
YDOT = 13662
631162 feet/sec YDOT = 4164
369978 meter/sec
ZDOT = -19074
111180 ZDOT = -5813
789088
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 11092
52905708
00016717 00000-0 10270-3 0 9129
2 25544 51
6460 189
1525 0001899 44
5065 315
6249 15
72391719 28999
Satellite: ISS
Catalog Number: 25544
Epoch time: 11092
52905708 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 189
1525 deg
Eccentricity:
0001899
Arg of perigee: 44
5065 deg
Mean anomaly: 315
6249 deg
Mean motion: 15
72391719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2899
Checksum: 332
Coasting Arc #14 (Orbit 2914)
---------------------------------------
Vector Time (GMT): 2011/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1450314
61 A = 6724801
50 meter
Y = -4031774
77 meter E =
0005673
Z = 5179782
40 I = 51
60566
XDOT = 7513
985245 Wp = 52
30359
YDOT = 1282
738650 meter/sec RA = 183
11424 deg
ZDOT = -1101
210416 TA = 48
23198
MA = 48
18351
Ha = 192
953 n
mi
Hp = 185
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4758250
02 X = 1470128
37
Y = -13227607
51 feet Y = -4015445
14 meter
Z = 16994036
75 Z = 5186876
60
XDOT = 24652
182561 XDOT = 7504
432453
YDOT = 4208
460137 feet/sec YDOT = 1366
711063 meter/sec
ZDOT = -3612
895067 ZDOT = -1064
730720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2123008
77 X = 647093
07
Y = -13860998
11 feet Y = -4224832
22 meter
Z = 17022731
68 Z = 5188528
62
XDOT = 24015
047340 XDOT = 7319
786429
YDOT = -594
748585 feet/sec YDOT = -181
279369 meter/sec
ZDOT = -3465
498285 ZDOT = -1056
283877
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 11093
54591099
00016717 00000-0 10270-3 0 9137
2 25544 51
6465 183
9432 0001995 43
1536 316
9782 15
72478369 29150
Satellite: ISS
Catalog Number: 25544
Epoch time: 11093
54591099 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 183
9432 deg
Eccentricity:
0001995
Arg of perigee: 43
1536 deg
Mean anomaly: 316
9782 deg
Mean motion: 15
72478369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2915
Checksum: 341
Coasting Arc #15 (Orbit 2930)
---------------------------------------
Vector Time (GMT): 2011/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6711628
64 A = 6736461
43 meter
Y = -134818
18 meter E =
0015193
Z = 466027
89 I = 51
67497
XDOT = 521
955441 Wp = 49
44917
YDOT = -4777
287990 meter/sec RA = 178
00505 deg
ZDOT = 6017
015562 TA = 315
61543
MA = 315
73711
Ha = 193
090 n
mi
Hp = 185
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22019778
99 X = -6711886
14
Y = -442316
85 feet Y = -209873
08 meter
Z = 1528962
89 Z = 433421
99
XDOT = 1712
452235 XDOT = 546
107438
YDOT = -15673
517027 feet/sec YDOT = -4771
315571 meter/sec
ZDOT = 19740
864704 ZDOT = 6019
610343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21662493
57 X = -6602728
04
Y = 4023460
85 feet Y = 1226350
87 meter
Z = 1397202
05 Z = 425867
19
XDOT = -1316
003364 XDOT = -401
117825
YDOT = -14091
526090 feet/sec YDOT = -4295
097152 meter/sec
ZDOT = 19751
387772 ZDOT = 6020
222993
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 11094
56273740
00016717 00000-0 10270-3 0 9141
2 25544 51
6461 178
7346 0002194 46
4525 313
6819 15
72469862 29319
Satellite: ISS
Catalog Number: 25544
Epoch time: 11094
56273740 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 178
7346 deg
Eccentricity:
0002194
Arg of perigee: 46
4525 deg
Mean anomaly: 313
6819 deg
Mean motion: 15
72469862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2931
Checksum: 324
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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