[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 15th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 325)
---------------------------------------
Vector Time (GMT): 2012/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2486771
48 A = 6763484
38 meter
Y = -3640334
74 meter E =
0020845
Z = 5123741
77 I = 51
32866
XDOT = 5129
433930 Wp = 149
20091
YDOT = 5537
646141 meter/sec RA = 235
87967 deg
ZDOT = 1424
678618 TA = 286
94278
MA = 287
17118
Ha = 218
411 n
mi
Hp = 202
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8158699
09 X = 2502403
82
Y = -11943355
44 feet Y = -3612438
47 meter
Z = 16810176
41 Z = 5135860
45
XDOT = 16828
851476 XDOT = 5060
208905
YDOT = 18168
130384 feet/sec YDOT = 5594
619649 meter/sec
ZDOT = 4674
142447 ZDOT = 1449
428577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9694466
97 X = 2954873
53
Y = -10655730
69 feet Y = -3247866
71 meter
Z = 16860096
53 Z = 5138957
42
XDOT = 13227
373579 XDOT = 4031
703467
YDOT = 19694
349806 feet/sec YDOT = 6002
837821 meter/sec
ZDOT = 4775
275551 ZDOT = 1455
503988
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 12074
55057788
00016717 00000-0 10270-3 0 9006
2 25544 51
6366 236
5634 0016724 155
5462 204
6490 15
59147435 3266
Satellite: ISS
Catalog Number: 25544
Epoch time: 12074
55057788 = yrday
fracday
Element set: 900
Inclination: 51
6366 deg
RA of node: 236
5634 deg
Eccentricity:
0016724
Arg of perigee: 155
5462 deg
Mean anomaly: 204
6490 deg
Mean motion: 15
59147435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 326
Checksum: 316
Coasting Arc #2 (Orbit 340)
---------------------------------------
Vector Time (GMT): 2012/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4710018
90 A = 6764446
77 meter
Y = 377291
63 meter E =
0025976
Z = -4862869
98 I = 51
35146
XDOT = -2982
670161 Wp = 137
86440
YDOT = -6646
366862 meter/sec RA = 230
80566 deg
ZDOT = 2361
702049 TA = 155
45529
MA = 155
33142
Ha = 218
274 n
mi
Hp = 202
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15452817
90 X = -4690265
33
Y = 1237833
42 feet Y = 324731
49 meter
Z = -15954297
84 Z = -4885702
81
XDOT = -9785
663259 XDOT = -2919
599952
YDOT = -21805
665558 feet/sec YDOT = -6679
368157 meter/sec
ZDOT = 7748
366302 ZDOT = 2347
366071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15388233
46 X = -4690333
56
Y = -725886
35 feet Y = -221250
16 meter
Z = -16047952
89 Z = -4891416
04
XDOT = -7032
673807 XDOT = -2143
558976
YDOT = -21756
479937 feet/sec YDOT = -6631
375085 meter/sec
ZDOT = 7689
990863 ZDOT = 2343
909215
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 12075
51197285
00016717 00000-0 10270-3 0 9011
2 25544 51
6376 231
7337 0016775 159
0268 201
1579 15
59208741 3418
Satellite: ISS
Catalog Number: 25544
Epoch time: 12075
51197285 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 231
7337 deg
Eccentricity:
0016775
Arg of perigee: 159
0268 deg
Mean anomaly: 201
1579 deg
Mean motion: 15
59208741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 341
Checksum: 313
Coasting Arc #3 (Orbit 356)
---------------------------------------
Vector Time (GMT): 2012/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5589171
12 A = 6771502
02 meter
Y = 2746070
43 meter E =
0026202
Z = 2615457
86 I = 51
39472
XDOT = -323
318778 Wp = 136
28519
YDOT = 5640
953617 meter/sec RA = 225
75913 deg
ZDOT = -5219
161936 TA = 14
01086
MA = 13
93830
Ha = 217
988 n
mi
Hp = 202
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18337175
59 X = 5545343
49
Y = 9009417
44 feet Y = 2808327
11 meter
Z = 8580898
49 Z = 2642502
76
XDOT = -1060
757146 XDOT = -361
019901
YDOT = 18507
065672 feet/sec YDOT = 5637
126940 meter/sec
ZDOT = -17123
234698 ZDOT = -5220
824508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17181660
92 X = 5236970
25
Y = 10968100
41 feet Y = 3343077
00 meter
Z = 8691647
22 Z = 2649214
07
XDOT = -2188
419464 XDOT = -667
030253
YDOT = 17035
392429 feet/sec YDOT = 5192
387612 meter/sec
ZDOT = -17130
396374 ZDOT = -5221
344815
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 12076
53742837
00016717 00000-0 10270-3 0 9024
2 25544 51
6367 226
5811 0016691 162
9901 197
1817 15
59244030 3578
Satellite: ISS
Catalog Number: 25544
Epoch time: 12076
53742837 = yrday
fracday
Element set: 902
Inclination: 51
6367 deg
RA of node: 226
5811 deg
Eccentricity:
0016691
Arg of perigee: 162
9901 deg
Mean anomaly: 197
1817 deg
Mean motion: 15
59244030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 357
Checksum: 316
Coasting Arc #4 (Orbit 372)
---------------------------------------
Vector Time (GMT): 2012/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4744039
87 A = 6774054
51 meter
Y = -4794548
89 meter E =
0016403
Z = 671918
78 I = 51
42746
XDOT = 3839
219262 Wp = 119
72592
YDOT = -2949
332660 meter/sec RA = 220
74664 deg
ZDOT = 5943
964432 TA = 247
55832
MA = 247
73213
Ha = 217
846 n
mi
Hp = 202
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15564435
27 X = -4693337
64
Y = -15730147
27 feet Y = -4847316
13 meter
Z = 2204457
93 Z = 648996
39
XDOT = 12595
863722 XDOT = 3843
040011
YDOT = -9676
288254 feet/sec YDOT = -2906
378292 meter/sec
ZDOT = 19501
195642 ZDOT = 5962
624384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14047533
78 X = -4281688
30
Y = -17110243
93 feet Y = -5215202
35 meter
Z = 2110725
09 Z = 643349
01
XDOT = 12074
967648 XDOT = 3680
450139
YDOT = -7448
838136 feet/sec YDOT = -2270
405864 meter/sec
ZDOT = 19577
906020 ZDOT = 5967
345755
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 12077
56284834
00016717 00000-0 10270-3 0 9037
2 25544 51
6381 221
4290 0016665 166
6631 193
4968 15
59334441 3731
Satellite: ISS
Catalog Number: 25544
Epoch time: 12077
56284834 = yrday
fracday
Element set: 903
Inclination: 51
6381 deg
RA of node: 221
4290 deg
Eccentricity:
0016665
Arg of perigee: 166
6631 deg
Mean anomaly: 193
4968 deg
Mean motion: 15
59334441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 373
Checksum: 322
Coasting Arc #5 (Orbit 387)
---------------------------------------
Vector Time (GMT): 2012/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2136234
95 A = 6768204
49 meter
Y = 5213886
45 meter E =
0017210
Z = -3744007
94 I = 51
43197
XDOT = -6382
203687 Wp = 150
75073
YDOT = -418
585768 meter/sec RA = 215
72574 deg
ZDOT = -4247
416781 TA = 74
30844
MA = 74
11864
Ha = 217
604 n
mi
Hp = 203
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7008644
84 X = 2095960
68
Y = 17105926
68 feet Y = 5237549
59 meter
Z = -12283490
61 Z = -3733728
74
XDOT = -20938
988474 XDOT = -6356
415996
YDOT = -1373
312887 feet/sec YDOT = -489
811758 meter/sec
ZDOT = -13935
094425 ZDOT = -4278
358025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5765553
79 X = 1757340
79
Y = 17593148
92 feet Y = 5362391
79 meter
Z = -12241628
66 Z = -3731248
42
XDOT = -19406
757982 XDOT = -5915
179833
YDOT = -3372
054636 feet/sec YDOT = -1027
802253 meter/sec
ZDOT = -14061
988768 ZDOT = -4286
094176
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 12078
52414945
00016717 00000-0 10270-3 0 9043
2 25544 51
6382 216
5984 0016429 170
3471 189
8003 15
59361976 3887
Satellite: ISS
Catalog Number: 25544
Epoch time: 12078
52414945 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 216
5984 deg
Eccentricity:
0016429
Arg of perigee: 170
3471 deg
Mean anomaly: 189
8003 deg
Mean motion: 15
59361976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 388
Checksum: 334
Coasting Arc #6 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2012/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1342606
59 A = 6762170
75 meter
Y = -4058400
30 meter E =
0018414
Z = 5237910
11 I = 51
43865
XDOT = 6871
991450 Wp = 166
17264
YDOT = 3331
889901 meter/sec RA = 210
66849 deg
ZDOT = 801
982217 TA = 276
04706
MA = 276
25686
Ha = 217
278 n
mi
Hp = 203
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4404877
27 X = 1362444
45
Y = -13314961
61 feet Y = -4043274
89 meter
Z = 17184744
44 Z = 5244481
00
XDOT = 22545
903707 XDOT = 6830
327053
YDOT = 10931
397312 feet/sec YDOT = 3408
503893 meter/sec
ZDOT = 2631
175252 ZDOT = 835
263930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5074146
38 X = 1546599
82
Y = -13038753
32 feet Y = -3974212
01 meter
Z = 17211930
12 Z = 5246196
30
XDOT = 20898
494894 XDOT = 6369
861244
YDOT = 11864
587338 feet/sec YDOT = 3616
326221 meter/sec
ZDOT = 2767
515471 ZDOT = 843
538715
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 12079
54950240
00016717 00000-0 10270-3 0 9050
2 25544 51
6389 211
4457 0016273 174
3804 185
7537 15
59438802 4043
Satellite: ISS
Catalog Number: 25544
Epoch time: 12079
54950240 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 211
4457 deg
Eccentricity:
0016273
Arg of perigee: 174
3804 deg
Mean anomaly: 185
7537 deg
Mean motion: 15
59438802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 404
Checksum: 317
Coasting Arc #7 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2012/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4658990
26 A = 6764829
35 meter
Y = 1808883
27 meter E =
0022207
Z = -4577777
11 I = 51
47535
XDOT = -4931
087005 Wp = 152
84508
YDOT = -5027
541880 meter/sec RA = 205
60254 deg
ZDOT = 3018
387314 TA = 147
45929
MA = 147
32222
Ha = 217
077 n
mi
Hp = 203
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15285401
11 X = -4656633
74
Y = 5934656
40 feet Y = 1756796
13 meter
Z = -15018953
77 Z = -4600404
52
XDOT = -16178
106971 XDOT = -4889
163999
YDOT = -16494
559973 feet/sec YDOT = -5082
449537 meter/sec
ZDOT = 9902
845518 ZDOT = 2994
535101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15426986
12 X = -4702145
37
Y = 5298271
50 feet Y = 1614913
15 meter
Z = -15111883
55 Z = -4606102
11
XDOT = -15153
254542 XDOT = -4618
711984
YDOT = -16028
621747 feet/sec YDOT = -4885
523909 meter/sec
ZDOT = 9805
271986 ZDOT = 2988
646901
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 12080
51073992
00016717 00000-0 10270-3 0 9060
2 25544 51
6394 206
6155 0016198 177
7776 182
3454 15
59470053 4192
Satellite: ISS
Catalog Number: 25544
Epoch time: 12080
51073992 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 206
6155 deg
Eccentricity:
0016198
Arg of perigee: 177
7776 deg
Mean anomaly: 182
3454 deg
Mean motion: 15
59470053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 419
Checksum: 326
Coasting Arc #8 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2012/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6420092
74 A = 6772030
23 meter
Y = 739444
90 meter E =
0024765
Z = 1967636
57 I = 51
52827
XDOT = 1120
885616 Wp = 149
73548
YDOT = 5163
710543 meter/sec RA = 200
57124 deg
ZDOT = -5588
260953 TA = 8
42373
MA = 8
38223
Ha = 216
809 n
mi
Hp = 203
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21063296
40 X = 6401788
70
Y = 2426000
34 feet Y = 811136
28 meter
Z = 6455500
57 Z = 1998780
28
XDOT = 3677
446246 XDOT = 1090
206956
YDOT = 16941
307555 feet/sec YDOT = 5176
072666 meter/sec
ZDOT = -18334
189477 ZDOT = -5582
891021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20958512
17 X = 6388154
51
Y = 2936530
41 feet Y = 895054
47 meter
Z = 6583234
55 Z = 2006569
89
XDOT = 3590
144178 XDOT = 1094
275945
YDOT = 15499
042597 feet/sec YDOT = 4724
108183 meter/sec
ZDOT = -18312
442275 ZDOT = -5581
632405
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 12081
53602588
00016717 00000-0 10270-3 0 9073
2 25544 51
6400 201
4623 0016167 181
4390 178
6721 15
59505442 4357
Satellite: ISS
Catalog Number: 25544
Epoch time: 12081
53602588 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 201
4623 deg
Eccentricity:
0016167
Arg of perigee: 181
4390 deg
Mean anomaly: 178
6721 deg
Mean motion: 15
59505442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 294
Coasting Arc #9 (Orbit 450)
---------------------------------------
Vector Time (GMT): 2012/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5956824
08 A = 6772630
46 meter
Y = -2874714
75 meter E =
0014149
Z = 1474653
61 I = 51
56073
XDOT = 3289
603455 Wp = 130
69274
YDOT = -3835
003225 meter/sec RA = 195
56891 deg
ZDOT = 5766
878929 TA = 245
43756
MA = 245
58509
Ha = 216
569 n
mi
Hp = 203
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19543386
08 X = -5931399
22
Y = -9431478
83 feet Y = -2941185
27 meter
Z = 4838102
39 Z = 1445777
89
XDOT = 10792
662253 XDOT = 3304
228646
YDOT = -12582
031577 feet/sec YDOT = -3798
134269 meter/sec
ZDOT = 18920
206459 ZDOT = 5782
895670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19504963
43 X = -5945112
85
Y = -9569953
79 feet Y = -2916921
92 meter
Z = 4719783
15 Z = 1438589
90
XDOT = 10068
707825 XDOT = 3068
942145
YDOT = -11082
524068 feet/sec YDOT = -3377
953336 meter/sec
ZDOT = 18986
132913 ZDOT = 5786
973312
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 12082
56127529
00016717 00000-0 10270-3 0 9085
2 25544 51
6408 196
3092 0015940 185
1623 174
9370 15
59584184 4512
Satellite: ISS
Catalog Number: 25544
Epoch time: 12082
56127529 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 196
3092 deg
Eccentricity:
0015940
Arg of perigee: 185
1623 deg
Mean anomaly: 174
9370 deg
Mean motion: 15
59584184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 451
Checksum: 321
Coasting Arc #10 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2012/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3208235
58 A = 6765496
00 meter
Y = 4090079
66 meter E =
0013821
Z = -4327084
48 I = 51
56691
XDOT = -6664
019170 Wp = 156
88797
YDOT = 1565
763096 meter/sec RA = 190
54789 deg
ZDOT = -3477
121164 TA = 77
87022
MA = 77
71541
Ha = 216
363 n
mi
Hp = 204
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10525707
27 X = 3183281
04
Y = 13418896
51 feet Y = 4125816
03 meter
Z = -14196471
38 Z = -4311560
17
XDOT = -21863
579953 XDOT = -6664
141485
YDOT = 5137
018033 feet/sec YDOT = 1491
240770 meter/sec
ZDOT = -11407
877836 ZDOT = -3509
495176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10746776
36 X = 3275617
43
Y = 13310233
99 feet Y = 4056959
32 meter
Z = -14132995
64 Z = -4307737
07
XDOT = -20770
263948 XDOT = -6330
776451
YDOT = 4572
598531 feet/sec YDOT = 1393
728032 meter/sec
ZDOT = -11540
802194 ZDOT = -3517
636509
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 12083
52241582
00016717 00000-0 10270-3 0 9099
2 25544 51
6410 191
4785 0015874 189
2175 170
8692 15
59613437 4665
Satellite: ISS
Catalog Number: 25544
Epoch time: 12083
52241582 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 191
4785 deg
Eccentricity:
0015874
Arg of perigee: 189
2175 deg
Mean anomaly: 170
8692 deg
Mean motion: 15
59613437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 328
Coasting Arc #11 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2012/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 743481
83 A = 6761156
45 meter
Y = -4143778
00 meter E =
0014767
Z = 5290857
74 I = 51
58387
XDOT = 7608
325265 Wp = 184
52511
YDOT = 982
000961 meter/sec RA = 185
49121 deg
ZDOT = -314
521726 TA = 268
38727
MA = 268
55642
Ha = 215
941 n
mi
Hp = 204
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2439244
84 X = 764061
25
Y = -13595072
17 feet Y = -4135348
22 meter
Z = 17358457
15 Z = 5294520
04
XDOT = 24961
697065 XDOT = 7598
306742
YDOT = 3221
787931 feet/sec YDOT = 1067
025903 meter/sec
ZDOT = -1031
895428 ZDOT = -277
585160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1961728
87 X = 597934
96
Y = -13652750
81 feet Y = -4161358
45 meter
Z = 17373714
42 Z = 5295508
15
XDOT = 24050
580883 XDOT = 7330
617053
YDOT = 2395
863340 feet/sec YDOT = 730
259146 meter/sec
ZDOT = -880
379089 ZDOT = -268
339546
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 12084
54759695
00016717 00000-0 10270-3 0 9103
2 25544 51
6412 186
3253 0015653 193
0721 167
0031 15
59712860 4828
Satellite: ISS
Catalog Number: 25544
Epoch time: 12084
54759695 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 186
3253 deg
Eccentricity:
0015653
Arg of perigee: 193
0721 deg
Mean anomaly: 167
0031 deg
Mean motion: 15
59712860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 305
Coasting Arc #12 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2012/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4546419
13 A = 6766308
35 meter
Y = 3096402
44 meter E =
0017123
Z = -3955111
75 I = 51
63165
XDOT = -5688
807666 Wp = 173
24834
YDOT = -3215
894503 meter/sec RA = 180
44003 deg
ZDOT = 4006
751975 TA = 138
62830
MA = 138
49849
Ha = 215
690 n
mi
Hp = 204
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14916073
27 X = -4561492
68
Y = 10158800
65 feet Y = 3045476
88 meter
Z = -12976088
43 Z = -3977235
11
XDOT = -18664
067146 XDOT = -5671
888079
YDOT = -10550
834982 feet/sec YDOT = -3279
415243 meter/sec
ZDOT = 13145
511730 ZDOT = 3979
157296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14370311
43 X = -4380070
92
Y = 10808127
70 feet Y = 3294317
32 meter
Z = -13067052
79 Z = -3982837
69
XDOT = -18406
287215 XDOT = -5610
236343
YDOT = -8657
833921 feet/sec YDOT = -2638
907779 meter/sec
ZDOT = 13032
446303 ZDOT = 3972
289633
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 12085
50867441
00016717 00000-0 10270-3 0 9110
2 25544 51
6408 181
4943 0015566 196
5391 163
5259 15
59741993 4977
Satellite: ISS
Catalog Number: 25544
Epoch time: 12085
50867441 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 181
4943 deg
Eccentricity:
0015566
Arg of perigee: 196
5391 deg
Mean anomaly: 163
5259 deg
Mean motion: 15
59741993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 341
Coasting Arc #13 (Orbit 512)
---------------------------------------
Vector Time (GMT): 2012/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6591878
32 A = 6772660
39 meter
Y = -1209649
43 meter E =
0023092
Z = 861336
00 I = 51
68268
XDOT = 1621
457153 Wp = 166
04220
YDOT = 4589
442033 meter/sec RA = 175
43071 deg
ZDOT = -5952
632223 TA = 4
60754
MA = 4
58632
Ha = 215
447 n
mi
Hp = 204
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21626897
39 X = 6600730
74
Y = -3968666
10 feet Y = -1135885
40 meter
Z = 2825905
51 Z = 893380
84
XDOT = 5319
741315 XDOT = 1598
933293
YDOT = 15057
224517 feet/sec YDOT = 4607
447702 meter/sec
ZDOT = -19529
633278 ZDOT = -5944
810329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21323462
64 X = 6499391
41
Y = -5293572
78 feet Y = -1613480
98 meter
Z = 2957494
12 Z = 901444
21
XDOT = 5970
449666 XDOT = 1819
793058
YDOT = 13137
168210 feet/sec YDOT = 4004
208870 meter/sec
ZDOT = -19497
790090 ZDOT = -5942
926420
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 12086
53378986
00016717 00000-0 10270-3 0 9126
2 25544 51
6400 176
3409 0015485 200
0424 160
0125 15
59764234 5133
Satellite: ISS
Catalog Number: 25544
Epoch time: 12086
53378986 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 176
3409 deg
Eccentricity:
0015485
Arg of perigee: 200
0424 deg
Mean anomaly: 160
0125 deg
Mean motion: 15
59764234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 513
Checksum: 293
Coasting Arc #14 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2012/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6153788
69 A = 6769907
99 meter
Y = -1064210
60 meter E =
0012951
Z = 2623964
12 I = 51
70462
XDOT = 3053
514302 Wp = 147
33605
YDOT = -4703
241570 meter/sec RA = 170
43530 deg
ZDOT = 5230
967767 TA = 242
23880
MA = 242
37019
Ha = 215
127 n
mi
Hp = 204
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20189595
43 X = -6154177
80
Y = -3491504
60 feet Y = -1133028
05 meter
Z = 8608806
17 Z = 2594068
27
XDOT = 10018
091541 XDOT = 3080
468954
YDOT = -15430
582580 feet/sec YDOT = -4668
944184 meter/sec
ZDOT = 17161
967738 ZDOT = 5245
867504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20453741
62 X = -6234300
44
Y = -1884554
65 feet Y = -574412
26 meter
Z = 8486154
57 Z = 2586579
91
XDOT = 8529
049902 XDOT = 2599
654410
YDOT = -14671
565380 feet/sec YDOT = -4471
893128 meter/sec
ZDOT = 17223
396503 ZDOT = 5249
691254
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 12087
55886876
00016717 00000-0 10270-3 0 9132
2 25544 51
6401 171
1861 0015325 204
2256 155
8181 15
59846242 5292
Satellite: ISS
Catalog Number: 25544
Epoch time: 12087
55886876 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 171
1861 deg
Eccentricity:
0015325
Arg of perigee: 204
2256 deg
Mean anomaly: 155
8181 deg
Mean motion: 15
59846242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 318
Coasting Arc #15 (Orbit 543)
---------------------------------------
Vector Time (GMT): 2012/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3325314
66 A = 6762279
63 meter
Y = 3178599
39 meter E =
0011073
Z = -4957271
76 I = 51
70823
XDOT = -6505
952777 Wp = 154
84457
YDOT = 3455
858457 meter/sec RA = 165
40733 deg
ZDOT = -2159
835326 TA = 94
21321
MA = 94
08665
Ha = 214
898 n
mi
Hp = 205
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10909825
01 X = 3313605
18
Y = 10428475
68 feet Y = 3215719
32 meter
Z = -16264014
98 Z = -4941146
12
XDOT = -21344
989426 XDOT = -6533
621312
YDOT = 11338
118296 feet/sec YDOT = 3382
950030 meter/sec
ZDOT = -7086
073905 ZDOT = -2191
508496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11958331
88 X = 3644899
56
Y = 9323014
04 feet Y = 2841654
68 meter
Z = -16198002
28 Z = -4937151
09
XDOT = -19435
356394 XDOT = -5923
896629
YDOT = 12457
563269 feet/sec YDOT = 3797
065284 meter/sec
ZDOT = -7216
297802 ZDOT = -2199
527570
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 12088
51985099
00016717 00000-0 10270-3 0 9147
2 25544 51
6392 166
3542 0015219 208
1436 151
8898 15
59866515 5441
Satellite: ISS
Catalog Number: 25544
Epoch time: 12088
51985099 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 166
3542 deg
Eccentricity:
0015219
Arg of perigee: 208
1436 deg
Mean anomaly: 151
8898 deg
Mean motion: 15
59866515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 544
Checksum: 342
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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