[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 6th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 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 860)
---------------------------------------
Vector Time (GMT): 2011/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3950490
85 A = 6761706
61 meter
Y = 2659033
26 meter E =
0023272
Z = -4822287
46 I = 51
28036
XDOT = -1746
449435 Wp = 57
14184
YDOT = -7044
624794 meter/sec RA = 271
77783 deg
ZDOT = -2449
951723 TA = 188
63817
MA = 188
67829
Ha = 215
574 n
mi
Hp = 201
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12960927
98 X = -3956505
49
Y = 8723862
39 feet Y = 2614823
02 meter
Z = -15821153
09 Z = -4841493
27
XDOT = -5729
820981 XDOT = -1655
643961
YDOT = -23112
286069 feet/sec YDOT = -7063
646841 meter/sec
ZDOT = -8037
899353 ZDOT = -2458
215602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15147974
85 X = 4617102
73
Y = 3485897
69 feet Y = 1062501
62 meter
Z = -15899298
39 Z = -4846106
15
XDOT = -12808
612651 XDOT = -3904
065136
YDOT = 18791
032227 feet/sec YDOT = 5727
506623 meter/sec
ZDOT = -8071
120718 ZDOT = -2460
077595
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 11217
52035230
00016717 00000-0 10270-3 0 9009
2 25544 51
6385 272
4346 0012314 42
7573 317
4538 15
60216348 8619
Satellite: ISS
Catalog Number: 25544
Epoch time: 11217
52035230 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 272
4346 deg
Eccentricity:
0012314
Arg of perigee: 42
7573 deg
Mean anomaly: 317
4538 deg
Mean motion: 15
60216348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 282
Coasting Arc #2 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2011/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4153282
13 A = 6760469
19 meter
Y = 1695838
09 meter E =
0017537
Z = 5049089
50 I = 51
27713
XDOT = -941
206215 Wp = 48
59182
YDOT = 7434
314436 meter/sec RA = 266
68864 deg
ZDOT = -1707
463670 TA = 58
03756
MA = 57
86719
Ha = 215
437 n
mi
Hp = 201
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13626253
70 X = 4109482
91
Y = 5563773
27 feet Y = 1742037
43 meter
Z = 16565254
28 Z = 5069159
68
XDOT = -3087
946901 XDOT = -1015
973738
YDOT = 24390
795394 feet/sec YDOT = 7423
371349 meter/sec
ZDOT = -5601
914927 ZDOT = -1712
217171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5366734
32 X = -1635780
62
Y = -13606010
56 feet Y = -4147112
02 meter
Z = 16646700
92 Z = 5073914
44
XDOT = 18703
313198 XDOT = 5700
769863
YDOT = -14316
256358 feet/sec YDOT = -4363
594938 meter/sec
ZDOT = -5621
585955 ZDOT = -1713
459399
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 11218
54514842
00016717 00000-0 10270-3 0 9014
2 25544 51
6386 267
2782 0012366 46
0258 314
1915 15
60280629 8773
Satellite: ISS
Catalog Number: 25544
Epoch time: 11218
54514842 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 267
2782 deg
Eccentricity:
0012366
Arg of perigee: 46
0258 deg
Mean anomaly: 314
1915 deg
Mean motion: 15
60280629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 311
Coasting Arc #3 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2011/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3107516
85 A = 6767879
92 meter
Y = -5277823
27 meter E =
0017034
Z = -2878249
52 I = 51
30504
XDOT = 3376
974438 Wp = 54
21218
YDOT = -4713
706382 meter/sec RA = 261
62340 deg
ZDOT = 5028
218721 TA = 272
76731
MA = 272
96227
Ha = 215
605 n
mi
Hp = 201
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10195265
27 X = -3034286
39
Y = -17315693
15 feet Y = -5312163
74 meter
Z = -9443075
87 Z = -2893168
22
XDOT = 11079
312460 XDOT = 3405
007126
YDOT = -15464
915950 feet/sec YDOT = -4675
786651 meter/sec
ZDOT = 16496
780580 ZDOT = 5044
691604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5118380
61 X = -1560082
41
Y = 19401941
92 feet Y = 5913711
90 meter
Z = -9503429
62 Z = -2896645
35
XDOT = -17290
813936 XDOT = -5270
240088
YDOT = 3502
845589 feet/sec YDOT = 1067
667335 meter/sec
ZDOT = 16563
926993 ZDOT = 5048
684948
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 11219
50588740
00016717 00000-0 10270-3 0 9020
2 25544 51
6387 262
4441 0012539 50
3279 309
8981 15
60291675 8920
Satellite: ISS
Catalog Number: 25544
Epoch time: 11219
50588740 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 262
4441 deg
Eccentricity:
0012539
Arg of perigee: 50
3279 deg
Mean anomaly: 309
8981 deg
Mean motion: 15
60291675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 324
Coasting Arc #4 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2011/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 968015
35 A = 6771209
47 meter
Y = 6660565
28 meter E =
0016891
Z = -752196
75 I = 51
32202
XDOT = -4867
112345 Wp = 91
89178
YDOT = 50
871433 meter/sec RA = 256
59796 deg
ZDOT = -5929
094753 TA = 96
28754
MA = 96
09512
Ha = 215
730 n
mi
Hp = 200
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3175903
40 X = 897117
66
Y = 21852248
29 feet Y = 6670993
87 meter
Z = -2467837
10 Z = -747665
81
XDOT = -15968
216356 XDOT = -4838
517421
YDOT = 166
901028 feet/sec YDOT = -3
395174 meter/sec
ZDOT = -19452
410606 ZDOT = -5952
669377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12928608
04 X = 3940639
73
Y = -17903831
89 feet Y = -5457087
96 meter
Z = -2449741
91 Z = -746681
33
XDOT = 10185
034354 XDOT = 3104
398471
YDOT = 9977
043630 feet/sec YDOT = 3041
002898 meter/sec
ZDOT = -19548
192169 ZDOT = -5958
288973
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 11220
53066284
00016717 00000-0 10270-3 0 9030
2 25544 51
6390 257
2870 0012647 53
7289 306
5033 15
60297376 9084
Satellite: ISS
Catalog Number: 25544
Epoch time: 11220
53066284 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 257
2870 deg
Eccentricity:
0012647
Arg of perigee: 53
7289 deg
Mean anomaly: 306
5033 deg
Mean motion: 15
60297376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 908
Checksum: 308
Coasting Arc #5 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2011/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1600770
40 A = 6764705
66 meter
Y = -5228338
26 meter E =
0022071
Z = 3960612
88 I = 51
30693
XDOT = 4835
094291 Wp = 77
61271
YDOT = 4486
905363 meter/sec RA = 251
56128 deg
ZDOT = 3954
925415 TA = 331
11512
MA = 331
23711
Ha = 215
772 n
mi
Hp = 200
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5251871
38 X = 1639876
15
Y = -17153340
75 feet Y = -5210219
17 meter
Z = 12994136
74 Z = 3968483
80
XDOT = 15863
170246 XDOT = 4765
349548
YDOT = 14720
818119 feet/sec YDOT = 4540
584022 meter/sec
ZDOT = 12975
477082 ZDOT = 3978
244838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15506177
09 X = -4726282
78
Y = 8974370
77 feet Y = 2735388
21 meter
Z = 13026357
24 Z = 3970433
69
XDOT = -791
483921 XDOT = -241
244299
YDOT = -20405
044631 feet/sec YDOT = -6219
457604 meter/sec
ZDOT = 13070
023116 ZDOT = 3983
743046
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 11221
55542755
00016717 00000-0 10270-3 0 9046
2 25544 51
6377 252
1306 0012784 57
7916 302
4477 15
60294309 9248
Satellite: ISS
Catalog Number: 25544
Epoch time: 11221
55542755 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 252
1306 deg
Eccentricity:
0012784
Arg of perigee: 57
7916 deg
Mean anomaly: 302
4477 deg
Mean motion: 15
60294309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 308
Coasting Arc #6 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2011/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3869330
48 A = 6759452
97 meter
Y = 1727149
87 meter E =
0026681
Z = -5288971
44 I = 51
30095
XDOT = -3079
359466 Wp = 76
60004
YDOT = -7012
861913 meter/sec RA = 246
48153 deg
ZDOT = -31
351183 TA = 193
06481
MA = 193
13406
Ha = 215
785 n
mi
Hp = 200
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12694653
80 X = -3862663
97
Y = 5666502
20 feet Y = 1683918
34 meter
Z = -17352268
49 Z = -5307751
88
XDOT = -10102
885387 XDOT = -3000
559120
YDOT = -23008
077144 feet/sec YDOT = -7046
856589 meter/sec
ZDOT = -102
858213 ZDOT = -46
119498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13134687
15 X = 4003452
64
Y = 4252818
78 feet Y = 1296259
16 meter
Z = -17428661
17 Z = -5312255
92
XDOT = -7648
567951 XDOT = -2331
283511
YDOT = 22876
702433 feet/sec YDOT = 6972
818902 meter/sec
ZDOT = -162
560594 ZDOT = -49
548469
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 11222
51613293
00016717 00000-0 10270-3 0 9050
2 25544 51
6387 247
2964 0012615 60
8557 299
3860 15
60301167 9390
Satellite: ISS
Catalog Number: 25544
Epoch time: 11222
51613293 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 247
2964 deg
Eccentricity:
0012615
Arg of perigee: 60
8557 deg
Mean anomaly: 299
3860 deg
Mean motion: 15
60301167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 314
Coasting Arc #7 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2011/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4919180
67 A = 6764359
40 meter
Y = 2357844
79 meter E =
0023409
Z = 3986415
87 I = 51
32946
XDOT = 30
163224 Wp = 70
86720
YDOT = 6610
115278 meter/sec RA = 241
40106 deg
ZDOT = -3920
517042 TA = 60
04574
MA = 59
81353
Ha = 215
694 n
mi
Hp = 200
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16139044
19 X = 4873084
41
Y = 7735711
24 feet Y = 2412596
09 meter
Z = 13078792
23 Z = 4010200
79
XDOT = 98
960709 XDOT = -24
709956
YDOT = 21686
729915 feet/sec YDOT = 6610
145998 meter/sec
ZDOT = -12862
588719 ZDOT = -3920
503409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6992516
32 X = -2131318
97
Y = -16397547
01 feet Y = -4997972
33 meter
Z = 13175353
87 Z = 4015847
86
XDOT = 12951
356088 XDOT = 3947
573336
YDOT = -15927
198038 feet/sec YDOT = -4854
609962 meter/sec
ZDOT = -12862
813800 ZDOT = -3920
585646
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 11223
54087349
00016717 00000-0 10270-3 0 9062
2 25544 51
6369 242
1390 0012771 64
3807 295
8667 15
60364955 9555
Satellite: ISS
Catalog Number: 25544
Epoch time: 11223
54087349 = yrday
fracday
Element set: 906
Inclination: 51
6369 deg
RA of node: 242
1390 deg
Eccentricity:
0012771
Arg of perigee: 64
3807 deg
Mean anomaly: 295
8667 deg
Mean motion: 15
60364955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 331
Coasting Arc #8 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2011/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4225435
07 A = 6770904
26 meter
Y = -5224111
43 meter E =
0022301
Z = -781449
36 I = 51
36755
XDOT = 3328
816691 Wp = 55
84554
YDOT = -3560
308835 meter/sec RA = 236
36636 deg
ZDOT = 5935
238574 TA = 295
64993
MA = 295
88013
Ha = 215
720 n
mi
Hp = 200
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13862975
95 X = -4162907
96
Y = -17139473
19 feet Y = -5271013
19 meter
Z = -2563810
24 Z = -801824
27
XDOT = 10921
314602 XDOT = 3339
549834
YDOT = -11680
803265 feet/sec YDOT = -3523
024181 meter/sec
ZDOT = 19472
567500 ZDOT = 5951
435458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -485758
60 X = -148059
22
Y = 22029010
96 feet Y = 6714442
54 meter
Z = -2646409
11 Z = -806625
50
XDOT = -14184
366470 XDOT = -4323
394900
YDOT = 1983
462664 feet/sec YDOT = 604
559420 meter/sec
ZDOT = 19538
541392 ZDOT = 5955
347416
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 11224
50155833
00016717 00000-0 10270-3 0 9074
2 25544 51
6374 237
3052 0012727 68
5953 291
6560 15
60391472 9708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11224
50155833 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 237
3052 deg
Eccentricity:
0012727
Arg of perigee: 68
5953 deg
Mean anomaly: 291
6560 deg
Mean motion: 15
60391472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 306
Coasting Arc #9 (Orbit 985)
---------------------------------------
Vector Time (GMT): 2011/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1751266
39 A = 6767747
26 meter
Y = 5875850
67 meter E =
0016342
Z = -2881805
65 I = 51
37302
XDOT = -5739
674580 Wp = 83
57329
YDOT = -743
981843 meter/sec RA = 231
34390 deg
ZDOT = -5027
703843 TA = 129
41686
MA = 129
27208
Ha = 215
834 n
mi
Hp = 200
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5745624
62 X = 1699430
23
Y = 19277725
31 feet Y = 5895144
61 meter
Z = -9454742
95 Z = -2873424
05
XDOT = -18830
953347 XDOT = -5706
505630
YDOT = -2440
885311 feet/sec YDOT = -807
980856 meter/sec
ZDOT = -16495
091348 ZDOT = -5055
505873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7691364
40 X = 2344327
87
Y = -18604423
74 feet Y = -5670628
36 meter
Z = -9420901
78 Z = -2871490
86
XDOT = 11612
774952 XDOT = 3539
573805
YDOT = 13172
916404 feet/sec YDOT = 4015
104920 meter/sec
ZDOT = -16608
068026 ZDOT = -5062
139134
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 11225
52627645
00016717 00000-0 10270-3 0 9083
2 25544 51
6361 232
1467 0012735 71
8778 288
3764 15
60361343 9868
Satellite: ISS
Catalog Number: 25544
Epoch time: 11225
52627645 = yrday
fracday
Element set: 908
Inclination: 51
6361 deg
RA of node: 232
1467 deg
Eccentricity:
0012735
Arg of perigee: 71
8778 deg
Mean anomaly: 288
3764 deg
Mean motion: 15
60361343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 986
Checksum: 325
Coasting Arc #10 (Orbit 1001)
---------------------------------------
Vector Time (GMT): 2011/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1636517
75 A = 6760134
93 meter
Y = -4147891
94 meter E =
0016543
Z = 5066601
67 I = 51
36684
XDOT = 6067
050038 Wp = 89
19194
YDOT = 4425
999028 meter/sec RA = 226
28270 deg
ZDOT = 1659
333124 TA = 344
75017
MA = 344
79997
Ha = 215
762 n
mi
Hp = 200
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5369152
72 X = 1658166
63
Y = -13608569
34 feet Y = -4129470
32 meter
Z = 16622708
89 Z = 5074604
28
XDOT = 19905
019809 XDOT = 6009
046199
YDOT = 14520
994185 feet/sec YDOT = 4493
520176 meter/sec
ZDOT = 5444
006311 ZDOT = 1688
665205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12559327
13 X = -3828082
91
Y = 7429443
46 feet Y = 2264494
37 meter
Z = 16655392
02 Z = 5076563
49
XDOT = -6083
387419 XDOT = -1854
216485
YDOT = -22787
869193 feet/sec YDOT = -6945
742530 meter/sec
ZDOT = 5563
075320 ZDOT = 1695
625358
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 11226
55098236
00016717 00000-0 10270-3 0 9096
2 25544 51
6354 226
9891 0012749 75
2469 285
0099 15
60384502 10029
Satellite: ISS
Catalog Number: 25544
Epoch time: 11226
55098236 = yrday
fracday
Element set: 909
Inclination: 51
6354 deg
RA of node: 226
9891 deg
Eccentricity:
0012749
Arg of perigee: 75
2469 deg
Mean anomaly: 285
0099 deg
Mean motion: 15
60384502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1002
Checksum: 319
Coasting Arc #11 (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 = -4683492
08 A = 6761310
63 meter
Y = 989488
30 meter E =
0023519
Z = -4795862
81 I = 51
39289
XDOT = -3881
645372 Wp = 92
82574
YDOT = -6096
344611 meter/sec RA = 221
19977 deg
ZDOT = 2542
552615 TA = 202
25366
MA = 202
35589
Ha = 215
802 n
mi
Hp = 200
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15365787
65 X = -4670911
71
Y = 3246352
69 feet Y = 937184
87 meter
Z = -15734458
03 Z = -4818584
18
XDOT = -12735
056995 XDOT = -3825
537360
YDOT = -20001
130614 feet/sec YDOT = -6139
437770 meter/sec
ZDOT = 8341
708055 ZDOT = 2523
832401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14121077
42 X = 4304104
40
Y = 6657710
56 feet Y = 2029270
18 meter
Z = -15826859
07 Z = -4824026
64
XDOT = -1440
408897 XDOT = -439
036632
YDOT = 22629
904450 feet/sec YDOT = 6897
594876 meter/sec
ZDOT = 8265
823663 ZDOT = 2519
423052
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
51163262
00016717 00000-0 10270-3 0 9107
2 25544 51
6358 222
1545 0012699 78
4163 281
8418 15
60381695 10172
Satellite: ISS
Catalog Number: 25544
Epoch time: 11227
51163262 = yrday
fracday
Element set: 910
Inclination: 51
6358 deg
RA of node: 222
1545 deg
Eccentricity:
0012699
Arg of perigee: 78
4163 deg
Mean anomaly: 281
8418 deg
Mean motion: 15
60381695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1017
Checksum: 303
Coasting Arc #12 (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 = 5996684
97 A = 6769094
11 meter
Y = 2318614
69 meter E =
0025860
Z = 2089361
63 I = 51
44283
XDOT = -127
863496 Wp = 96
75478
YDOT = 5349
586844 meter/sec RA = 216
15122 deg
ZDOT = -5513
997848 TA = 59
96498
MA = 59
70869
Ha = 215
686 n
mi
Hp = 200
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19674163
30 X = 5960162
52
Y = 7607003
59 feet Y = 2385469
14 meter
Z = 6854861
00 Z = 2118404
23
XDOT = -419
499659 XDOT = -160
888587
YDOT = 17551
137939 feet/sec YDOT = 5347
972181 meter/sec
ZDOT = -18090
544121 ZDOT = -5514
699372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11332419
84 X = -3454121
57
Y = -17744969
37 feet Y = -5408666
66 meter
Z = 6972850
72 Z = 2125324
90
XDOT = 9335
549696 XDOT = 2845
475547
YDOT = -13142
220386 feet/sec YDOT = -4005
748774 meter/sec
ZDOT = -18093
579728 ZDOT = -5514
923101
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
53631379
00016717 00000-0 10270-3 0 9110
2 25544 51
6355 216
9960 0012710 81
6453 278
6143 15
60449410 10330
Satellite: ISS
Catalog Number: 25544
Epoch time: 11228
53631379 = yrday
fracday
Element set: 911
Inclination: 51
6355 deg
RA of node: 216
9960 deg
Eccentricity:
0012710
Arg of perigee: 81
6453 deg
Mean anomaly: 278
6143 deg
Mean motion: 15
60449410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1033
Checksum: 294
Coasting Arc #13 (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 = -4857484
74 A = 6769850
66 meter
Y = -4421579
21 meter E =
0026020
Z = 1598223
98 I = 51
47073
XDOT = 4359
155791 Wp = 74
36177
YDOT = -2693
560499 meter/sec RA = 211
13896 deg
ZDOT = 5726
254570 TA = 303
22878
MA = 303
47792
Ha = 215
648 n
mi
Hp = 200
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15936629
72 X = -4815444
53
Y = -14506493
48 feet Y = -4475663
46 meter
Z = 5243516
99 Z = 1574728
90
XDOT = 14301
692227 XDOT = 4361
135003
YDOT = -8837
140745 feet/sec YDOT = -2644
802513 meter/sec
ZDOT = 18786
924441 ZDOT = 5747
435943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4660387
16 X = 1420486
01
Y = 21063864
86 feet Y = 6420266
01 meter
Z = 5148143
25 Z = 1569154
06
XDOT = -15150
200166 XDOT = -4617
781011
YDOT = -1318
422395 feet/sec YDOT = -401
855146 meter/sec
ZDOT = 18873
130276 ZDOT = 5752
530108
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
56098130
00016717 00000-0 10270-3 0 9127
2 25544 51
6355 211
8395 0012621 86
7391 273
5208 15
60492296 10497
Satellite: ISS
Catalog Number: 25544
Epoch time: 11229
56098130 = yrday
fracday
Element set: 912
Inclination: 51
6355 deg
RA of node: 211
8395 deg
Eccentricity:
0012621
Arg of perigee: 86
7391 deg
Mean anomaly: 273
5208 deg
Mean motion: 15
60492296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 308
Coasting Arc #14 (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 = 1504028
12 A = 6762187
42 meter
Y = 4780685
33 meter E =
0022316
Z = -4560690
04 I = 51
47125
XDOT = -6988
324944 Wp = 81
05088
YDOT = -710
998680 meter/sec RA = 206
10052 deg
ZDOT = -3059
321525 TA = 158
30457
MA = 158
20989
Ha = 215
733 n
mi
Hp = 200
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4934475
46 X = 1472612
56
Y = 15684663
16 feet Y = 4797328
52 meter
Z = -14962893
84 Z = -4553459
98
XDOT = -22927
575274 XDOT = -6964
993554
YDOT = -2332
672836 feet/sec YDOT = -789
016024 meter/sec
ZDOT = -10037
144112 ZDOT = -3093
213757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4683371
96 X = 1427491
77
Y = -15789168
99 feet Y = -4812538
71 meter
Z = -14933655
56 Z = -4551778
21
XDOT = 16427
949773 XDOT = 5007
239091
YDOT = 14467
196634 feet/sec YDOT = 4409
601534 meter/sec
ZDOT = -10174
922623 ZDOT = -3101
316416
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
52159856
00016717 00000-0 10270-3 0 9139
2 25544 51
6356 207
0030 0012704 89
2925 270
9687 15
60453264 10645
Satellite: ISS
Catalog Number: 25544
Epoch time: 11230
52159856 = yrday
fracday
Element set: 913
Inclination: 51
6356 deg
RA of node: 207
0030 deg
Eccentricity:
0012704
Arg of perigee: 89
2925 deg
Mean anomaly: 270
9687 deg
Mean motion: 15
60453264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1064
Checksum: 298
Coasting Arc #15 (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 = 2657807
96 A = 6759290
22 meter
Y = -3401236
52 meter E =
0015790
Z = 5188153
35 I = 51
48967
XDOT = 6732
923337 Wp = 84
92556
YDOT = 3544
051307 meter/sec RA = 201
02586 deg
ZDOT = -1121
463570 TA = 15
83883
MA = 15
78950
Ha = 215
569 n
mi
Hp = 200
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8719842
39 X = 2670440
81
Y = -11158912
48 feet Y = -3371444
57 meter
Z = 17021500
49 Z = 5201095
62
XDOT = 22089
643495 XDOT = 6698
240480
YDOT = 11627
464919 feet/sec YDOT = 3619
149026 meter/sec
ZDOT = -3679
342421 ZDOT = -1088
839597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13328275
95 X = -4062458
51
Y = 4595204
18 feet Y = 1400618
24 meter
Z = 17074238
39 Z = 5204227
86
XDOT = -11762
482317 XDOT = -3585
204610
YDOT = -20885
736176 feet/sec YDOT = -6365
972387 meter/sec
ZDOT = -3546
803613 ZDOT = -1081
065741
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
54624162
00016717 00000-0 10270-3 0 9140
2 25544 51
6356 201
8459 0012578 92
7145 267
5451 15
60481077 10806
Satellite: ISS
Catalog Number: 25544
Epoch time: 11231
54624162 = yrday
fracday
Element set: 914
Inclination: 51
6356 deg
RA of node: 201
8459 deg
Eccentricity:
0012578
Arg of perigee: 92
7145 deg
Mean anomaly: 267
5451 deg
Mean motion: 15
60481077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 300
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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