[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 17th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 1016)
---------------------------------------
Vector Time (GMT): 2011/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4669336
80 A = 6761367
91 meter
Y = 1011331
08 meter E =
0023602
Z = -4805268
32 I = 51
39294
XDOT = -3902
820982 Wp = 92
68342
YDOT = -6092
102915 meter/sec RA = 221
20766 deg
ZDOT = 2519
893397 TA = 202
15707
MA = 202
25924
Ha = 215
864 n
mi
Hp = 200
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15319346
46 X = -4656956
05
Y = 3318015
36 feet Y = 959184
83 meter
Z = -15765316
03 Z = -4827921
42
XDOT = -12804
530782 XDOT = -3846
648756
YDOT = -19987
214287 feet/sec YDOT = -6135
432514 meter/sec
ZDOT = 8267
366788 ZDOT = 2501
070470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14127326
40 X = 4306009
09
Y = 6572444
63 feet Y = 2003281
12 meter
Z = -15857440
27 Z = -4833347
79
XDOT = -1383
256824 XDOT = -421
616680
YDOT = 22660
145154 feet/sec YDOT = 6906
812243 meter/sec
ZDOT = 8191
064715 ZDOT = 2496
636525
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 11227
51167546
00016717 00000-0 10270-3 0 9005
2 25544 51
6360 222
1624 0012729 78
2164 282
0419 15
60348811 10173
Satellite: ISS
Catalog Number: 25544
Epoch time: 11227
51167546 = yrday
fracday
Element set: 900
Inclination: 51
6360 deg
RA of node: 222
1624 deg
Eccentricity:
0012729
Arg of perigee: 78
2164 deg
Mean anomaly: 282
0419 deg
Mean motion: 15
60348811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1017
Checksum: 282
Coasting Arc #2 (Orbit 1032)
---------------------------------------
Vector Time (GMT): 2011/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5997079
42 A = 6769141
19 meter
Y = 2289604
26 meter E =
0025891
Z = 2120102
73 I = 51
44283
XDOT = -85
383314 Wp = 96
40352
YDOT = 5366
090606 meter/sec RA = 216
15904 deg
ZDOT = -5498
746544 TA = 59
95316
MA = 59
69659
Ha = 215
752 n
mi
Hp = 200
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19675457
42 X = 5960732
01
Y = 7511824
99 feet Y = 2356464
09 meter
Z = 6955717
62 Z = 2149147
67
XDOT = -280
128982 XDOT = -118
670197
YDOT = 17605
284142 feet/sec YDOT = 5364
949519 meter/sec
ZDOT = -18040
507035 ZDOT = -5499
242339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11389258
72 X = -3471446
06
Y = -17668628
93 feet Y = -5385398
10 meter
Z = 7073717
85 Z = 2156069
20
XDOT = 9260
998457 XDOT = 2822
752330
YDOT = -13263
983339 feet/sec YDOT = -4042
862122 meter/sec
ZDOT = -18042
706848 ZDOT = -5499
417047
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 11228
53637930
00016717 00000-0 10270-3 0 9018
2 25544 51
6358 217
0041 0012741 81
4293 278
8306 15
60413623 10339
Satellite: ISS
Catalog Number: 25544
Epoch time: 11228
53637930 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 217
0041 deg
Eccentricity:
0012741
Arg of perigee: 81
4293 deg
Mean anomaly: 278
8306 deg
Mean motion: 15
60413623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1033
Checksum: 281
Coasting Arc #3 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2011/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4890142
19 A = 6770020
91 meter
Y = -4401493
86 meter E =
0026025
Z = 1554317
84 I = 51
47112
XDOT = 4311
296103 Wp = 73
98551
YDOT = -2736
579692 meter/sec RA = 211
14694 deg
ZDOT = 5741
894347 TA = 303
10608
MA = 303
35562
Ha = 215
720 n
mi
Hp = 200
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16043773
59 X = -4848110
87
Y = -14440596
66 feet Y = -4455943
36 meter
Z = 5099467
98 Z = 1530664
09
XDOT = 14144
672255 XDOT = 4313
683948
YDOT = -8978
279830 feet/sec YDOT = -2688
354617 meter/sec
ZDOT = 18838
236046 ZDOT = 5762
844215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4785200
68 X = 1458529
17
Y = 21071436
45 feet Y = 6422573
83 meter
Z = 5003448
48 Z = 1525051
10
XDOT = -15102
698390 XDOT = -4603
302469
YDOT = -1121
449189 feet/sec YDOT = -341
817713 meter/sec
ZDOT = 18923
502107 ZDOT = 5767
883442
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 11229
56107153
00016717 00000-0 10270-3 0 9022
2 25544 51
6358 211
8478 0012657 86
5131 273
7472 15
60453553 10499
Satellite: ISS
Catalog Number: 25544
Epoch time: 11229
56107153 = yrday
fracday
Element set: 902
Inclination: 51
6358 deg
RA of node: 211
8478 deg
Eccentricity:
0012657
Arg of perigee: 86
5131 deg
Mean anomaly: 273
7472 deg
Mean motion: 15
60453553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 305
Coasting Arc #4 (Orbit 1063)
---------------------------------------
Vector Time (GMT): 2011/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1572567
99 A = 6762427
54 meter
Y = 4787753
39 meter E =
0022176
Z = -4530201
43 I = 51
47186
XDOT = -6968
626826 Wp = 80
96182
YDOT = -651
359681 meter/sec RA = 206
10947 deg
ZDOT = -3117
051727 TA = 157
75097
MA = 157
65461
Ha = 215
812 n
mi
Hp = 200
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5159343
78 X = 1540920
18
Y = 15707852
32 feet Y = 4805161
73 meter
Z = -14862865
57 Z = -4522638
97
XDOT = -22862
948903 XDOT = -6945
683355
YDOT = -2137
006826 feet/sec YDOT = -729
158918 meter/sec
ZDOT = -10226
547660 ZDOT = -3150
849210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4511141
18 X = 1374995
83
Y = -15934660
93 feet Y = -4856884
65 meter
Z = -14832276
03 Z = -4520877
73
XDOT = 16473
216055 XDOT = 5021
036254
YDOT = 14281
048326 feet/sec YDOT = 4352
863530 meter/sec
ZDOT = -10363
942893 ZDOT = -3158
929794
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 11230
52171390
00016717 00000-0 10270-3 0 9035
2 25544 51
6359 207
0115 0012741 89
0448 271
2168 15
60411402 10647
Satellite: ISS
Catalog Number: 25544
Epoch time: 11230
52171390 = yrday
fracday
Element set: 903
Inclination: 51
6359 deg
RA of node: 207
0115 deg
Eccentricity:
0012741
Arg of perigee: 89
0448 deg
Mean anomaly: 271
2168 deg
Mean motion: 15
60411402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1064
Checksum: 266
Coasting Arc #5 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2011/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2575137
84 A = 6759364
61 meter
Y = -3444225
33 meter E =
0015712
Z = 5201560
36 I = 51
48971
XDOT = 6774
065500 Wp = 85
21205
YDOT = 3490
461613 meter/sec RA = 201
03559 deg
ZDOT = -1038
435866 TA = 14
74709
MA = 14
70131
Ha = 215
657 n
mi
Hp = 200
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8448614
96 X = 2588192
41
Y = -11299951
86 feet Y = -3415355
49 meter
Z = 17065486
74 Z = 5214102
04
XDOT = 22224
624345 XDOT = 6739
575506
YDOT = 11451
645713 feet/sec YDOT = 3566
020489 meter/sec
ZDOT = -3406
941817 ZDOT = -1005
611557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13178793
24 X = -4016896
18
Y = 4862134
64 feet Y = 1481978
64 meter
Z = 17116597
21 Z = 5217138
83
XDOT = -11950
982683 XDOT = -3642
659522
YDOT = -20822
898824 feet/sec YDOT = -6346
819562 meter/sec
ZDOT = -3273
586654 ZDOT = -997
789212
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 11231
54638579
00016717 00000-0 10270-3 0 9046
2 25544 51
6359 201
8546 0012617 92
4469 267
8132 15
60435403 10807
Satellite: ISS
Catalog Number: 25544
Epoch time: 11231
54638579 = yrday
fracday
Element set: 904
Inclination: 51
6359 deg
RA of node: 201
8546 deg
Eccentricity:
0012617
Arg of perigee: 92
4469 deg
Mean anomaly: 267
8132 deg
Mean motion: 15
60435403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 307
Coasting Arc #6 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2011/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5798576
05 A = 6766219
44 meter
Y = 1089621
28 meter E =
0017417
Z = -3328567
95 I = 51
54159
XDOT = -3594
252844 Wp = 93
99754
YDOT = -4894
825190 meter/sec RA = 195
97832 deg
ZDOT = 4679
015854 TA = 227
13770
MA = 227
28412
Ha = 215
709 n
mi
Hp = 200
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19024199
64 X = -5794159
97
Y = 3574872
96 feet Y = 1024802
74 meter
Z = -10920498
54 Z = -3356726
52
XDOT = -11792
168124 XDOT = -3561
980480
YDOT = -16059
137762 feet/sec YDOT = -4934
837856 meter/sec
ZDOT = 15351
101883 ZDOT = 4661
633502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17932834
29 X = 5465927
89
Y = 7113259
36 feet Y = 2168121
45 meter
Z = -11035042
94 Z = -3363481
09
XDOT = 1978
608968 XDOT = 603
080013
YDOT = 18616
677070 feet/sec YDOT = 5674
363171 meter/sec
ZDOT = 15280
576852 ZDOT = 4657
519825
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 11232
50700523
00016717 00000-0 10270-3 0 9053
2 25544 51
6360 197
0200 0012662 95
7005 264
5595 15
60437944 10959
Satellite: ISS
Catalog Number: 25544
Epoch time: 11232
50700523 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 197
0200 deg
Eccentricity:
0012662
Arg of perigee: 95
7005 deg
Mean anomaly: 264
5595 deg
Mean motion: 15
60437944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 286
Coasting Arc #7 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2011/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6590244
40 A = 6770919
60 meter
Y = 1499862
32 meter E =
0022984
Z = -275949
62 I = 51
58754
XDOT = -1283
426844 Wp = 117
64739
YDOT = 4605
743053 meter/sec RA = 190
96620 deg
ZDOT = -6010
240297 TA = 65
33695
MA = 65
09777
Ha = 215
652 n
mi
Hp = 200
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21621536
75 X = 6574323
35
Y = 4920808
13 feet Y = 1573469
44 meter
Z = -905346
51 Z = -243973
09
XDOT = -4210
717991 XDOT = -1305
637314
YDOT = 15110
705554 feet/sec YDOT = 4591
266857 meter/sec
ZDOT = -19718
636146 ZDOT = -6016
529050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15915092
57 X = -4850920
22
Y = -15447767
47 feet Y = -4708479
53 meter
Z = -775348
41 Z = -236326
20
XDOT = 10224
927269 XDOT = 3116
557832
YDOT = -9618
787302 feet/sec YDOT = -2931
806370 meter/sec
ZDOT = -19744
364700 ZDOT = -6018
082361
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 11233
53165476
00016717 00000-0 10270-3 0 9060
2 25544 51
6366 191
8618 0012571 99
4398 260
8179 15
60475326 11117
Satellite: ISS
Catalog Number: 25544
Epoch time: 11233
53165476 = yrday
fracday
Element set: 906
Inclination: 51
6366 deg
RA of node: 191
8618 deg
Eccentricity:
0012571
Arg of perigee: 99
4398 deg
Mean anomaly: 260
8179 deg
Mean motion: 15
60475326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 321
Coasting Arc #8 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2011/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4528035
88 A = 6765100
56 meter
Y = -3405032
83 meter E =
0024300
Z = 3680168
16 I = 51
59848
XDOT = 5680
466397 Wp = 99
74670
YDOT = -2852
033338 meter/sec RA = 185
95337 deg
ZDOT = 4322
078430 TA = 304
28922
MA = 304
51904
Ha = 215
593 n
mi
Hp = 200
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14855760
75 X = -4507501
04
Y = -11171367
54 feet Y = -3455553
34 meter
Z = 12074042
51 Z = 3658220
96
XDOT = 18636
700776 XDOT = 5690
940506
YDOT = -9357
064756 feet/sec YDOT = -2788
452417 meter/sec
ZDOT = 14180
047343 ZDOT = 4349
699285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7240312
34 X = 2206847
20
Y = 17181849
51 feet Y = 5237027
73 meter
Z = 11984886
62 Z = 3652993
44
XDOT = -19483
493670 XDOT = -5938
568871
YDOT = -1824
479795 feet/sec YDOT = -556
101441 meter/sec
ZDOT = 14292
488388 ZDOT = 4356
350461
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 11234
55629131
00016717 00000-0 10270-3 0 9077
2 25544 51
6369 186
7053 0012505 103
9581 256
2966 15
60521287 11276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11234
55629131 = yrday
fracday
Element set: 907
Inclination: 51
6369 deg
RA of node: 186
7053 deg
Eccentricity:
0012505
Arg of perigee: 103
9581 deg
Mean anomaly: 256
2966 deg
Mean motion: 15
60521287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 307
Coasting Arc #9 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2011/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 423264
11 A = 6758955
45 meter
Y = 4204801
12 meter E =
0026820
Z = -5297682
54 I = 51
60810
XDOT = -7643
433638 Wp = 96
06477
YDOT = 226
009725 meter/sec RA = 180
89549 deg
ZDOT = -435
961745 TA = 169
79790
MA = 169
74335
Ha = 215
515 n
mi
Hp = 200
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1388661
79 X = 401948
64
Y = 13795279
25 feet Y = 4209415
27 meter
Z = -17380848
22 Z = -5295678
00
XDOT = -25076
882015 XDOT = -7643
275045
YDOT = 741
501724 feet/sec YDOT = 140
537083 meter/sec
ZDOT = -1430
320687 ZDOT = -473
092734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5461084
66 X = 1664538
60
Y = -12755124
30 feet Y = -3887761
89 meter
Z = -17372833
80 Z = -5295239
74
XDOT = 21282
092445 XDOT = 6486
781777
YDOT = 11244
906587 feet/sec YDOT = 3427
447528 meter/sec
ZDOT = -1581
375559 ZDOT = -482
003270
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 11235
51687930
00016717 00000-0 10270-3 0 9086
2 25544 51
6369 181
8692 0012445 106
8442 253
4080 15
60499382 11425
Satellite: ISS
Catalog Number: 25544
Epoch time: 11235
51687930 = yrday
fracday
Element set: 908
Inclination: 51
6369 deg
RA of node: 181
8692 deg
Eccentricity:
0012445
Arg of perigee: 106
8442 deg
Mean anomaly: 253
4080 deg
Mean motion: 15
60499382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 315
Coasting Arc #10 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2011/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3861101
04 A = 6763133
17 meter
Y = -3611268
62 meter E =
0021388
Z = 4198399
64 I = 51
65340
XDOT = 6298
699714 Wp = 94
52552
YDOT = 2451
710650 meter/sec RA = 175
83418 deg
ZDOT = -3669
430925 TA = 33
01182
MA = 32
87847
Ha = 215
370 n
mi
Hp = 200
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12667654
34 X = 3880801
23
Y = -11847994
16 feet Y = -3567981
39 meter
Z = 13774277
03 Z = 4217204
35
XDOT = 20665
025310 XDOT = 6288
641239
YDOT = 8043
670111 feet/sec YDOT = 2522
090411 meter/sec
ZDOT = -12038
815371 ZDOT = -3638
856667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16702525
93 X = -5090929
90
Y = 4444461
06 feet Y = 1354671
73 meter
Z = 13850903
71 Z = 4221755
45
XDOT = -14100
398193 XDOT = -4297
801369
YDOT = -15712
937084 feet/sec YDOT = -4789
303223 meter/sec
ZDOT = -11914
505356 ZDOT = -3631
541233
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 11236
54149364
00016717 00000-0 10270-3 0 9095
2 25544 51
6374 176
7120 0012441 110
5116 249
7377 15
60531665 11581
Satellite: ISS
Catalog Number: 25544
Epoch time: 11236
54149364 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 176
7120 deg
Eccentricity:
0012441
Arg of perigee: 110
5116 deg
Mean anomaly: 249
7377 deg
Mean motion: 15
60531665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1158
Checksum: 300
Coasting Arc #11 (Orbit 1172)
---------------------------------------
Vector Time (GMT): 2011/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6430209
72 A = 6770264
92 meter
Y = 1857697
48 meter E =
0017454
Z = -1023133
27 I = 51
70736
XDOT = -2189
967321 Wp = 82
20649
YDOT = -4373
561396 meter/sec RA = 170
81791 deg
ZDOT = 5910
981185 TA = 266
69315
MA = 266
89284
Ha = 215
366 n
mi
Hp = 200
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21096488
59 X = -6445534
84
Y = 6094808
01 feet Y = 1785705
28 meter
Z = -3356736
44 Z = -1054407
84
XDOT = -7184
932155 XDOT = -2169
612485
YDOT = -14348
954712 feet/sec YDOT = -4397
937230 meter/sec
ZDOT = 19392
982891 ZDOT = 5900
391895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21517338
04 X = 6558484
64
Y = 4282723
54 feet Y = 1305374
14 meter
Z = -3484054
73 Z = -1061939
88
XDOT = 195
938101 XDOT = 59
721933
YDOT = 14529
564780 feet/sec YDOT = 4428
611345 meter/sec
ZDOT = 19350
038365 ZDOT = 5897
891694
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 11237
50205851
00016717 00000-0 10270-3 0 9108
2 25544 51
6373 171
8768 0012393 114
0114 246
2340 15
60539762 11732
Satellite: ISS
Catalog Number: 25544
Epoch time: 11237
50205851 = yrday
fracday
Element set: 910
Inclination: 51
6373 deg
RA of node: 171
8768 deg
Eccentricity:
0012393
Arg of perigee: 114
0114 deg
Mean anomaly: 246
2340 deg
Mean motion: 15
60539762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1173
Checksum: 284
Coasting Arc #12 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2011/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6150219
67 A = 6767534
17 meter
Y = 677344
65 meter E =
0017239
Z = -2742053
60 I = 51
72940
XDOT = -2830
450248 Wp = 119
75931
YDOT = 4918
824675 meter/sec RA = 165
82059 deg
ZDOT = -5166
078933 TA = 91
30963
MA = 91
11214
Ha = 215
356 n
mi
Hp = 200
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20177886
07 X = 6155508
49
Y = 2222259
35 feet Y = 746149
72 meter
Z = -8996238
85 Z = -2712163
63
XDOT = -9286
254095 XDOT = -2860
147798
YDOT = 16137
876230 feet/sec YDOT = 4887
006778 meter/sec
ZDOT = -16949
077863 ZDOT = -5179
901124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17133919
29 X = -5222418
60
Y = -10985796
32 feet Y = -3348470
72 meter
Z = -8874622
54 Z = -2704984
95
XDOT = 14600
169142 XDOT = 4450
131555
YDOT = -9121
265399 feet/sec YDOT = -2780
161694 meter/sec
ZDOT = -17005
486955 ZDOT = -5183
272424
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 11238
52664928
00016717 00000-0 10270-3 0 9116
2 25544 51
6386 166
7184 0012387 117
7274 242
5140 15
60570386 11892
Satellite: ISS
Catalog Number: 25544
Epoch time: 11238
52664928 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 166
7184 deg
Eccentricity:
0012387
Arg of perigee: 117
7274 deg
Mean anomaly: 242
5140 deg
Mean motion: 15
60570386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1189
Checksum: 322
Coasting Arc #13 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2011/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3228530
75 A = 6759658
07 meter
Y = -3098574
94 meter E =
0017843
Z = 5056195
24 I = 51
73269
XDOT = 6458
199159 Wp = 123
25975
YDOT = -3759
220583 meter/sec RA = 160
78636 deg
ZDOT = 1805
829976 TA = 309
25261
MA = 309
41080
Ha = 215
265 n
mi
Hp = 200
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10592292
50 X = -3218203
47
Y = -10165928
27 feet Y = -3134620
43 meter
Z = 16588567
05 Z = 5040536
57
XDOT = 21188
317451 XDOT = 6490
983310
YDOT = -12333
400863 feet/sec YDOT = -3686
817691 meter/sec
ZDOT = 5924
639029 ZDOT = 1837
282955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5294902
12 X = 1613886
17
Y = 13770034
01 feet Y = 4197106
37 meter
Z = 16524935
39 Z = 5036800
31
XDOT = -23394
053844 XDOT = -7130
507612
YDOT = 1675
845670 feet/sec YDOT = 510
797760 meter/sec
ZDOT = 6052
771482 ZDOT = 1844
884748
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 11239
55122670
00016717 00000-0 10270-3 0 9124
2 25544 51
6388 161
5613 0012311 122
2610 237
9741 15
60614033 12058
Satellite: ISS
Catalog Number: 25544
Epoch time: 11239
55122670 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 161
5613 deg
Eccentricity:
0012311
Arg of perigee: 122
2610 deg
Mean anomaly: 237
9741 deg
Mean motion: 15
60614033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 266
Coasting Arc #14 (Orbit 1219)
---------------------------------------
Vector Time (GMT): 2011/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -995011
97 A = 6760586
11 meter
Y = 4634585
93 meter E =
0023801
Z = -4842904
53 I = 51
76479
XDOT = -7162
254535 Wp = 116
92730
YDOT = 1072
126796 meter/sec RA = 155
72642 deg
ZDOT = 2496
474747 TA = 177
59184
MA = 177
58036
Ha = 215
143 n
mi
Hp = 200
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3264474
96 X = -1023237
39
Y = 15205334
42 feet Y = 4623301
00 meter
Z = -15888794
38 Z = -4847807
02
XDOT = -23498
210416 XDOT = -7185
838123
YDOT = 3517
476365 feet/sec YDOT = 991
902373 meter/sec
ZDOT = 8190
533946 ZDOT = 2461
623895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9173003
86 X = 2795931
58
Y = -12532990
20 feet Y = -3820055
41 meter
Z = -15908894
84 Z = -4849031
15
XDOT = 21980
053232 XDOT = 6699
520225
YDOT = 5866
280822 feet/sec YDOT = 1788
042395 meter/sec
ZDOT = 8048
645746 ZDOT = 2453
227223
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 11240
51175927
00016717 00000-0 10270-3 0 9136
2 25544 51
6395 156
7255 0012296 125
1006 235
1305 15
60598839 12205
Satellite: ISS
Catalog Number: 25544
Epoch time: 11240
51175927 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 156
7255 deg
Eccentricity:
0012296
Arg of perigee: 125
1006 deg
Mean anomaly: 235
1305 deg
Mean motion: 15
60598839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1220
Checksum: 295
Coasting Arc #15 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2011/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4596068
36 A = 6768624
50 meter
Y = -4478973
92 meter E =
0025936
Z = 2107246
50 I = 51
81901
XDOT = 4804
740735 Wp = 119
18419
YDOT = 2303
587688 meter/sec RA = 150
70339 deg
ZDOT = -5544
435513 TA = 37
43280
MA = 37
25243
Ha = 215
072 n
mi
Hp = 200
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15078964
44 X = 4635575
08
Y = -14694796
33 feet Y = -4427356
82 meter
Z = 6913538
39 Z = 2129670
13
XDOT = 15763
585087 XDOT = 4805
557884
YDOT = 7557
702387 feet/sec YDOT = 2357
321371 meter/sec
ZDOT = -18190
405225 ZDOT = -5521
092672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19641815
23 X = -5986825
28
Y = 7499259
83 feet Y = 2285774
40 meter
Z = 7004956
64 Z = 2135110
78
XDOT = -11009
451214 XDOT = -3355
680730
YDOT = -11815
583713 feet/sec YDOT = -3601
389916 meter/sec
ZDOT = -18095
457822 ZDOT = -5515
495544
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 11241
53631459
00016717 00000-0 10270-3 0 9147
2 25544 51
6396 151
5677 0012345 129
1501 231
0754 15
60605488 12365
Satellite: ISS
Catalog Number: 25544
Epoch time: 11241
53631459 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 151
5677 deg
Eccentricity:
0012345
Arg of perigee: 129
1501 deg
Mean anomaly: 231
0754 deg
Mean motion: 15
60605488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 296
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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