[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 30th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25564 29 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
272/16:46:24
542 8
3 8
7 8
8
N/A 0
5 -0
8 211
4
000/00:02:49
084 3
0 0
4 205
6
Coasting Arc #1 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2011/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2677849
45 A = 6756705
31 meter
Y = -3720714
95 meter E =
0002122
Z = -4965507
13 I = 51
59788
XDOT = 7031
593509 Wp = 92
98106
YDOT = -2268
323314 meter/sec RA = 355
09850 deg
ZDOT = -2093
265861 TA = 156
66877
MA = 156
65914
Ha = 208
199 n
mi
Hp = 205
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8785595
30 X = -2611922
75
Y = -12207070
04 feet Y = -3750292
10 meter
Z = -16291033
89 Z = -4978355
87
XDOT = 23069
532511 XDOT = 7066
604599
YDOT = -7442
005625 feet/sec YDOT = -2189
496148 meter/sec
ZDOT = -6867
670146 ZDOT = -2059
020631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10131616
86 X = 3088116
82
Y = 11038546
36 feet Y = 3364548
93 meter
Z = -16343128
93 Z = -4981385
70
XDOT = -21206
516605 XDOT = -6463
746261
YDOT = 9507
179835 feet/sec YDOT = 2897
788414 meter/sec
ZDOT = -6728
075814 ZDOT = -2050
717508
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 11272
51954033
00016717 00000-0 10270-3 0 9000
2 25544 51
6409 355
5016 0010770 251
3132 108
6856 15
61726048 17208
Satellite: ISS
Catalog Number: 25544
Epoch time: 11272
51954033 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 355
5016 deg
Eccentricity:
0010770
Arg of perigee: 251
3132 deg
Mean anomaly: 108
6856 deg
Mean motion: 15
61726048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 282
Coasting Arc #2 (Orbit 1722)
---------------------------------------
Vector Time (GMT): 2011/272/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2356874
58 A = 6762080
49 meter
Y = -4097356
50 meter E =
0006781
Z = -4832588
27 I = 51
59371
XDOT = 7172
710369 Wp = 231
64897
YDOT = 1214
916015 meter/sec RA = 354
05327 deg
ZDOT = 2461
622795 TA = 62
52900
MA = 62
46007
Ha = 211
389 n
mi
Hp = 205
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7732528
15 X = 2425993
06
Y = -13442770
67 feet Y = -4070614
40 meter
Z = -15854948
40 Z = -4820970
19
XDOT = 23532
514334 XDOT = 7146
633539
YDOT = 3985
944930 feet/sec YDOT = 1294
980042 meter/sec
ZDOT = 8076
190272 ZDOT = 2496
404914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11749724
10 X = 3581315
91
Y = 10195588
83 feet Y = 3107615
48 meter
Z = -15807384
84 Z = -4818090
90
XDOT = -7548
239520 XDOT = -2300
703406
YDOT = 21472
724346 feet/sec YDOT = 6544
886381 meter/sec
ZDOT = 8217
755954 ZDOT = 2504
772015
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 11272
71150371
00016717 00000-0 10270-3 0 9016
2 25544 51
6407 354
5327 0016464 267
9892 91
9378 15
60104768 17236
Satellite: ISS
Catalog Number: 25544
Epoch time: 11272
71150371 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 354
5327 deg
Eccentricity:
0016464
Arg of perigee: 267
9892 deg
Mean anomaly: 91
9378 deg
Mean motion: 15
60104768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1723
Checksum: 316
Coasting Arc #3 (Orbit 1738)
---------------------------------------
Vector Time (GMT): 2011/273/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5642142
81 A = 6769574
52 meter
Y = 2949767
09 meter E =
0004801
Z = 2296525
64 I = 51
58824
XDOT = -4078
619247 Wp = 219
91848
YDOT = -3587
880727 meter/sec RA = 349
01851 deg
ZDOT = -5421
860724 TA = 294
42135
MA = 294
47143
Ha = 211
176 n
mi
Hp = 205
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18510967
21 X = -5685864
60
Y = 9677713
54 feet Y = 2886428
85 meter
Z = 7534532
95 Z = 2269009
37
XDOT = -13381
296741 XDOT = -4011
856933
YDOT = -11771
262229 feet/sec YDOT = -3633
117341 meter/sec
ZDOT = -17788
256969 ZDOT = -5441
512576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6395177
66 X = -1949250
15
Y = -19927227
96 feet Y = -6073819
08 meter
Z = 7422298
96 Z = 2262316
72
XDOT = 12397
242902 XDOT = 3778
679637
YDOT = -10621
661540 feet/sec YDOT = -3237
482437 meter/sec
ZDOT = -17868
057793 ZDOT = -5446
184015
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 11273
73636341
00016717 00000-0 10270-3 0 9026
2 25544 51
6393 349
3767 0016336 272
3997 87
5289 15
60191039 17390
Satellite: ISS
Catalog Number: 25544
Epoch time: 11273
73636341 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 349
3767 deg
Eccentricity:
0016336
Arg of perigee: 272
3997 deg
Mean anomaly: 87
5289 deg
Mean motion: 15
60191039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1739
Checksum: 340
Coasting Arc #4 (Orbit 1754)
---------------------------------------
Vector Time (GMT): 2011/274/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6582882
06 A = 6770722
06 meter
Y = -756066
56 meter E =
0009416
Z = 1368397
14 I = 51
56312
XDOT = -631
249629 Wp = 332
98448
YDOT = 4978
388748 meter/sec RA = 344
01488 deg
ZDOT = 5811
274340 TA = 41
97883
MA = 41
90669
Ha = 211
085 n
mi
Hp = 205
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21597382
09 X = 6584199
79
Y = -2480533
34 feet Y = -682445
33 meter
Z = 4489491
92 Z = 1400380
35
XDOT = -2071
028965 XDOT = -715
102461
YDOT = 16333
296417 feet/sec YDOT = 4970
861092 meter/sec
ZDOT = 19065
860694 ZDOT = 5808
003835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -835997
58 X = -254812
06
Y = 21695950
05 feet Y = 6612925
57 meter
Z = 4619778
77 Z = 1408108
57
XDOT = -14228
169416 XDOT = -4336
746038
YDOT = -4588
868495 feet/sec YDOT = -1398
687117 meter/sec
ZDOT = 19052
229149 ZDOT = 5807
119445
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 11274
76118733
00016717 00000-0 10270-3 0 9031
2 25544 51
6391 344
2205 0016403 275
8637 84
0649 15
60258245 17556
Satellite: ISS
Catalog Number: 25544
Epoch time: 11274
76118733 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 344
2205 deg
Eccentricity:
0016403
Arg of perigee: 275
8637 deg
Mean anomaly: 84
0649 deg
Mean motion: 15
60258245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1755
Checksum: 311
Coasting Arc #5 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2011/275/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4821967
75 A = 6763310
89 meter
Y = -1860923
59 meter E =
0009722
Z = -4359080
35 I = 51
50873
XDOT = 4937
830509 Wp = 308
25109
YDOT = -4796
148002 meter/sec RA = 338
98618 deg
ZDOT = -3403
605162 TA = 287
20482
MA = 287
31122
Ha = 211
170 n
mi
Hp = 205
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15820104
15 X = -4779624
38
Y = -6105392
35 feet Y = -1914609
16 meter
Z = -14301444
72 Z = -4382402
72
XDOT = 16200
231330 XDOT = 5007
629198
YDOT = -15735
393707 feet/sec YDOT = -4740
539998 meter/sec
ZDOT = -11166
683603 ZDOT = -3379
447327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8179900
14 X = 2493233
56
Y = -14762067
50 feet Y = -4499478
17 meter
Z = -14396299
14 Z = -4387991
98
XDOT = 12312
321718 XDOT = 3752
795660
YDOT = 17651
374932 feet/sec YDOT = 5380
139079 meter/sec
ZDOT = -11068
006989 ZDOT = -3373
528530
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 11275
72193088
00016717 00000-0 10270-3 0 9045
2 25544 51
6382 339
3858 0016313 280
3059 79
6257 15
60266969 17708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11275
72193088 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 339
3858 deg
Eccentricity:
0016313
Arg of perigee: 280
3059 deg
Mean anomaly: 79
6257 deg
Mean motion: 15
60266969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 337
Coasting Arc #6 (Orbit 1785)
---------------------------------------
Vector Time (GMT): 2011/276/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1161292
62 A = 6759566
42 meter
Y = 4096728
27 meter E =
0014211
Z = 5261655
45 I = 51
46829
XDOT = -7078
935750 Wp = 292
17895
YDOT = 2871
816504 meter/sec RA = 333
91456 deg
ZDOT = -669
806431 TA = 164
25394
MA = 164
20971
Ha = 211
411 n
mi
Hp = 205
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3810015
16 X = 1089835
64
Y = 13440709
53 feet Y = 4109315
20 meter
Z = 17262649
11 Z = 5267123
31
XDOT = -23224
854823 XDOT = -7107
269031
YDOT = 9421
970158 feet/sec YDOT = 2792
497068 meter/sec
ZDOT = -2197
527662 ZDOT = -704
264931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13785602
77 X = -4201851
73
Y = 2089423
24 feet Y = 636856
20 meter
Z = 17284658
20 Z = 5268363
82
XDOT = -6457
020195 XDOT = -1968
099756
YDOT = -23157
647689 feet/sec YDOT = -7058
451016 meter/sec
ZDOT = -2338
028409 ZDOT = -712
631059
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 11276
74668877
00016717 00000-0 10270-3 0 9052
2 25544 51
6380 334
2288 0016367 284
4811 75
4529 15
60317498 17864
Satellite: ISS
Catalog Number: 25544
Epoch time: 11276
74668877 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 334
2288 deg
Eccentricity:
0016367
Arg of perigee: 284
4811 deg
Mean anomaly: 75
4529 deg
Mean motion: 15
60317498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1786
Checksum: 350
Coasting Arc #7 (Orbit 1800)
---------------------------------------
Vector Time (GMT): 2011/277/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2790054
59 A = 6765863
34 meter
Y = -5012507
78 meter E =
0011198
Z = -3573985
37 I = 51
46295
XDOT = 6271
250686 Wp = 293
83403
YDOT = 329
621590 meter/sec RA = 328
85124 deg
ZDOT = 4426
882111 TA = 23
63316
MA = 23
58176
Ha = 211
619 n
mi
Hp = 205
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9153722
41 X = 2863259
85
Y = -16445235
49 feet Y = -4980898
53 meter
Z = -11725673
80 Z = -3560253
23
XDOT = 20574
969442 XDOT = 6245
593696
YDOT = 1081
435662 feet/sec YDOT = 399
607307 meter/sec
ZDOT = 14523
891439 ZDOT = 4457
285515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15427663
14 X = 4702351
73
Y = 10841546
17 feet Y = 3304503
27 meter
Z = -11669443
72 Z = -3556846
45
XDOT = -2359
700504 XDOT = -719
236714
YDOT = 19147
232852 feet/sec YDOT = 5836
076573 meter/sec
ZDOT = 14647
678775 ZDOT = 4464
612491
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 11277
70736722
00016717 00000-0 10270-3 0 9065
2 25544 51
6380 329
3944 0016302 288
5936 71
3449 15
60358812 18019
Satellite: ISS
Catalog Number: 25544
Epoch time: 11277
70736722 = yrday
fracday
Element set: 906
Inclination: 51
6380 deg
RA of node: 329
3944 deg
Eccentricity:
0016302
Arg of perigee: 288
5936 deg
Mean anomaly: 71
3449 deg
Mean motion: 15
60358812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1801
Checksum: 318
Coasting Arc #8 (Orbit 1816)
---------------------------------------
Vector Time (GMT): 2011/278/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5402404
17 A = 6771027
62 meter
Y = 4077376
13 meter E =
0006531
Z = 129406
33 I = 51
45607
XDOT = -2968
993001 Wp = 250
03037
YDOT = -3751
272793 meter/sec RA = 323
82969 deg
ZDOT = -6000
510601 TA = 288
56915
MA = 288
64008
Ha = 211
766 n
mi
Hp = 205
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17724423
13 X = -5448225
30
Y = 13377218
26 feet Y = 4016706
94 meter
Z = 424561
45 Z = 103049
93
XDOT = -9740
790687 XDOT = -2897
675507
YDOT = -12307
325435 feet/sec YDOT = -3784
075513 meter/sec
ZDOT = -19686
714570 ZDOT = -6014
760481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11839187
57 X = -3608584
37
Y = -18788787
97 feet Y = -5726822
57 meter
Z = 316986
36 Z = 96617
44
XDOT = 11703
710676 XDOT = 3567
291014
YDOT = -7689
429719 feet/sec YDOT = -2343
738178 meter/sec
ZDOT = -19744
513551 ZDOT = -6018
127730
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 11278
73205706
00016717 00000-0 10270-3 0 9073
2 25544 51
6382 324
2372 0016350 292
8705 67
0724 15
60442918 18171
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
73205706 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 324
2372 deg
Eccentricity:
0016350
Arg of perigee: 292
8705 deg
Mean anomaly: 67
0724 deg
Mean motion: 15
60442918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1817
Checksum: 308
Coasting Arc #9 (Orbit 1832)
---------------------------------------
Vector Time (GMT): 2011/279/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5680383
16 A = 6765734
78 meter
Y = -1353844
43 meter E =
0007349
Z = 3411914
36 I = 51
41540
XDOT = -1315
904135 Wp = 340
87547
YDOT = 6015
314364 meter/sec RA = 318
80844 deg
ZDOT = 4587
292141 TA = 59
31839
MA = 59
24599
Ha = 211
760 n
mi
Hp = 204
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18636427
68 X = 5678525
48
Y = -4441746
82 feet Y = -1290333
02 meter
Z = 11193944
74 Z = 3439505
22
XDOT = -4317
270784 XDOT = -1405
354976
YDOT = 19735
283345 feet/sec YDOT = 6000
099343 meter/sec
ZDOT = 15050
171066 ZDOT = 4580
681722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3188277
92 X = 971787
11
Y = 18824204
38 feet Y = 5737617
49 meter
Z = 11306377
12 Z = 3446183
75
XDOT = -18024
000556 XDOT = -5493
715370
YDOT = -5951
690373 feet/sec YDOT = -1814
075226 meter/sec
ZDOT = 15022
894040 ZDOT = 4578
978103
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 11279
75671026
00016717 00000-0 10270-3 0 9089
2 25544 51
6383 319
0801 0016367 296
0371 63
9099 15
60519509 18333
Satellite: ISS
Catalog Number: 25544
Epoch time: 11279
75671026 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 319
0801 deg
Eccentricity:
0016367
Arg of perigee: 296
0371 deg
Mean anomaly: 63
9099 deg
Mean motion: 15
60519509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1833
Checksum: 326
Coasting Arc #10 (Orbit 1847)
---------------------------------------
Vector Time (GMT): 2011/280/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3697859
18 A = 6759003
13 meter
Y = -2174648
08 meter E =
0009913
Z = -5224665
31 I = 51
37070
XDOT = 4751
029849 Wp = 2
01536
YDOT = -5968
713705 meter/sec RA = 313
73986 deg
ZDOT = -868
604977 TA = 259
60228
MA = 259
71403
Ha = 212
070 n
mi
Hp = 204
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12132083
92 X = -3647886
50
Y = -7134672
17 feet Y = -2215720
90 meter
Z = -17141290
40 Z = -5242507
93
XDOT = 15587
368272 XDOT = 4821
639600
YDOT = -19582
394046 feet/sec YDOT = -5915
190063 meter/sec
ZDOT = -2849
753861 ZDOT = -845
352365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7725276
91 X = 2354664
40
Y = -11658449
00 feet Y = -3553495
26 meter
Z = -17213817
34 Z = -5246771
53
XDOT = 17931
550791 XDOT = 5465
536681
YDOT = 15996
151203 feet/sec YDOT = 4875
626887 meter/sec
ZDOT = -2754
721816 ZDOT = -839
639210
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 11280
71729268
00016717 00000-0 10270-3 0 9090
2 25544 51
6382 314
2447 0016312 300
4638 59
4906 15
60531945 18482
Satellite: ISS
Catalog Number: 25544
Epoch time: 11280
71729268 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 314
2447 deg
Eccentricity:
0016312
Arg of perigee: 300
4638 deg
Mean anomaly: 59
4906 deg
Mean motion: 15
60531945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1848
Checksum: 316
Coasting Arc #11 (Orbit 1863)
---------------------------------------
Vector Time (GMT): 2011/281/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 408121
32 A = 6762313
91 meter
Y = 5125265
13 meter E =
0013287
Z = 4403767
58 I = 51
36218
XDOT = -6059
324024 Wp = 338
90697
YDOT = 3336
242026 meter/sec RA = 308
65716 deg
ZDOT = -3312
228120 TA = 144
70429
MA = 144
61624
Ha = 212
352 n
mi
Hp = 204
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1338980
71 X = 329386
47
Y = 16815174
31 feet Y = 5129389
24 meter
Z = 14448056
36 Z = 4405558
43
XDOT = -19879
671995 XDOT = -6080
089918
YDOT = 10945
675937 feet/sec YDOT = 3268
366483 meter/sec
ZDOT = -10866
890159 ZDOT = -3341
715238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16847731
63 X = -5135188
60
Y = 703294
15 feet Y = 214364
06 meter
Z = 14455054
65 Z = 4405900
66
XDOT = -10242
539753 XDOT = -3121
926117
YDOT = -18931
262022 feet/sec YDOT = -5770
248664 meter/sec
ZDOT = -10987
146642 ZDOT = -3348
882297
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 11281
74187708
00016717 00000-0 10270-3 0 9103
2 25544 51
6383 309
0873 0016370 304
4173 55
5435 15
60597171 18645
Satellite: ISS
Catalog Number: 25544
Epoch time: 11281
74187708 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 309
0873 deg
Eccentricity:
0016370
Arg of perigee: 304
4173 deg
Mean anomaly: 55
5435 deg
Mean motion: 15
60597171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1864
Checksum: 312
Coasting Arc #12 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2011/282/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2748806
29 A = 6769744
68 meter
Y = -6031486
32 meter E =
0018667
Z = -1313729
41 I = 51
36915
XDOT = 4931
085125 Wp = 336
49056
YDOT = 977
988823 meter/sec RA = 303
61454 deg
ZDOT = 5815
936213 TA = 9
09849
MA = 9
06471
Ha = 212
506 n
mi
Hp = 204
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9018393
35 X = 2822429
17
Y = -19788340
94 feet Y = -6000335
98 meter
Z = -4310135
86 Z = -1300196
08
XDOT = 16178
100805 XDOT = 4891
529567
YDOT = 3208
624748 feet/sec YDOT = 1032
910735 meter/sec
ZDOT = 19081
155554 ZDOT = 5839
795424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19647090
34 X = 5988433
13
Y = 9347542
59 feet Y = 2849130
98 meter
Z = -4254693
39 Z = -1296830
55
XDOT = -2774
615278 XDOT = -845
702737
YDOT = 14578
742711 feet/sec YDOT = 4443
600778 meter/sec
ZDOT = 19178
246316 ZDOT = 5845
529477
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 11282
70239161
00016717 00000-0 10270-3 0 9112
2 25544 51
6380 304
2514 0016303 308
2208 51
7480 15
60643052 18792
Satellite: ISS
Catalog Number: 25544
Epoch time: 11282
70239161 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 304
2514 deg
Eccentricity:
0016303
Arg of perigee: 308
2208 deg
Mean anomaly: 51
7480 deg
Mean motion: 15
60643052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 278
Coasting Arc #13 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2011/283/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4593734
31 A = 6767621
81 meter
Y = 4323261
78 meter E =
0010982
Z = -2456241
69 I = 51
34765
XDOT = -2014
444885 Wp = 312
37296
YDOT = -5166
010276 meter/sec RA = 298
59274 deg
ZDOT = -5302
817857 TA = 255
31222
MA = 255
43397
Ha = 212
691 n
mi
Hp = 204
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15071306
80 X = -4629804
33
Y = 14183929
73 feet Y = 4271689
87 meter
Z = -8058535
74 Z = -2478646
43
XDOT = -6609
071146 XDOT = -1930
767368
YDOT = -16948
852610 feet/sec YDOT = -5188
069764 meter/sec
ZDOT = -17397
696381 ZDOT = -5312
400313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14210847
78 X = -4331466
40
Y = -14996583
36 feet Y = -4570958
61 meter
Z = -8149996
46 Z = -2484118
92
XDOT = 15844
268717 XDOT = 4829
333105
YDOT = -5498
562981 feet/sec YDOT = -1675
961997 meter/sec
ZDOT = -17436
424188 ZDOT = -5314
622092
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 11283
72690424
00016717 00000-0 10270-3 0 9129
2 25544 51
6387 299
0932 0016331 312
2233 47
7536 15
60712747 18951
Satellite: ISS
Catalog Number: 25544
Epoch time: 11283
72690424 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 299
0932 deg
Eccentricity:
0016331
Arg of perigee: 312
2233 deg
Mean anomaly: 47
7536 deg
Mean motion: 15
60712747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 314
Coasting Arc #14 (Orbit 1910)
---------------------------------------
Vector Time (GMT): 2011/284/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4557639
37 A = 6759338
23 meter
Y = -495675
18 meter E =
0010557
Z = 4970089
42 I = 51
30729
XDOT = -1401
349399 Wp = 321
60693
YDOT = 7272
087180 meter/sec RA = 293
53087 deg
ZDOT = 2020
757855 TA = 108
74030
MA = 108
62571
Ha = 212
667 n
mi
Hp = 203
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14952885
06 X = 4538699
17
Y = -1626230
91 feet Y = -444814
24 meter
Z = 16306067
66 Z = 4992184
84
XDOT = -4597
603015 XDOT = -1492
379793
YDOT = 23858
553741 feet/sec YDOT = 7255
907667 meter/sec
ZDOT = 6629
782990 ZDOT = 2013
728107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1907676
84 X = 581459
90
Y = 14820642
29 feet Y = 4517331
77 meter
Z = 16396053
56 Z = 4997517
13
XDOT = -22862
030780 XDOT = -6968
346982
YDOT = -4321
968393 feet/sec YDOT = -1317
335966 meter/sec
ZDOT = 6600
762602 ZDOT = 2011
912441
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 11284
75137765
00016717 00000-0 10270-3 0 9138
2 25544 51
6389 293
9347 0016299 315
5385 44
4462 15
60794938 19116
Satellite: ISS
Catalog Number: 25544
Epoch time: 11284
75137765 = yrday
fracday
Element set: 913
Inclination: 51
6389 deg
RA of node: 293
9347 deg
Eccentricity:
0016299
Arg of perigee: 315
5385 deg
Mean anomaly: 44
4462 deg
Mean motion: 15
60794938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1911
Checksum: 348
Coasting Arc #15 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2011/285/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2870708
61 A = 6759740
81 meter
Y = -3711140
20 meter E =
0008923
Z = -4863919
55 I = 51
29763
XDOT = 4004
580182 Wp = 6
51673
YDOT = -6129
210817 meter/sec RA = 288
43726 deg
ZDOT = 2322
168602 TA = 286
22711
MA = 286
32527
Ha = 212
890 n
mi
Hp = 203
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9418335
32 X = -2805368
04
Y = -12175656
83 feet Y = -3742877
34 meter
Z = -15957741
31 Z = -4877706
66
XDOT = 13138
386425 XDOT = 4061
539696
YDOT = -20108
959372 feet/sec YDOT = -6084
110453 meter/sec
ZDOT = 7618
663393 ZDOT = 2341
762154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11830849
79 X = 3606043
02
Y = -9756767
66 feet Y = -2973862
78 meter
Z = -16013670
57 Z = -4880966
79
XDOT = 19858
065453 XDOT = 6052
738350
YDOT = 11492
621794 feet/sec YDOT = 3502
951123 meter/sec
ZDOT = 7698
768894 ZDOT = 2346
584759
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 11285
71178863
00016717 00000-0 10270-3 0 9140
2 25544 51
6388 289
0977 0016258 319
6801 40
3149 15
60820346 19269
Satellite: ISS
Catalog Number: 25544
Epoch time: 11285
71178863 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 289
0977 deg
Eccentricity:
0016258
Arg of perigee: 319
6801 deg
Mean anomaly: 40
3149 deg
Mean motion: 15
60820346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 333
Coasting Arc #16 (Orbit 1941)
---------------------------------------
Vector Time (GMT): 2011/286/16:47:49
084
Vector Time (MET): N/A
Weight (LBS) : 870615
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 261221
79 A = 6767748
51 meter
Y = 6409705
46 meter E =
0009111
Z = 2169537
80 I = 51
31704
XDOT = -4980
760417 Wp = 22
64295
YDOT = 2055
780668 meter/sec RA = 283
37701 deg
ZDOT = -5457
985040 TA = 133
12662
MA = 133
05038
Ha = 213
098 n
mi
Hp = 203
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 857026
86 X = 178988
34
Y = 21029217
39 feet Y = 6412166
98 meter
Z = 7117906
18 Z = 2170606
60
XDOT = -16341
077483 XDOT = -4976
863907
YDOT = 6744
687231 feet/sec YDOT = 2000
104119 meter/sec
ZDOT = -17906
775066 ZDOT = -5482
172776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20956090
24 X = -6387416
30
Y = 1935908
47 feet Y = 590064
90 meter
Z = 7121910
40 Z = 2170758
29
XDOT = -7459
853203 XDOT = -2273
763256
YDOT = -14321
325121 feet/sec YDOT = -4365
139897 meter/sec
ZDOT = -18005
362076 ZDOT = -5488
034361
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 11286
73618749
00016717 00000-0 10270-3 0 9156
2 25544 51
6393 283
9386 0016201 323
6296 36
3758 15
60883742 19421
Satellite: ISS
Catalog Number: 25544
Epoch time: 11286
73618749 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 283
9386 deg
Eccentricity:
0016201
Arg of perigee: 323
6296 deg
Mean anomaly: 36
3758 deg
Mean motion: 15
60883742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1942
Checksum: 341
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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