[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 14th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 ET - UTC (sec) : 67 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
351/13:37:55
266 -0
8 1
4 1
4
N/A 1
1 0
1 230
6
000/00:07:50
532 -0
5 0
3 212
7
Coasting Arc #1 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2012/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5350579
20 A = 6788706
25 meter
Y = 1453723
72 meter E =
0022368
Z = -3943443
69 I = 51
37714
XDOT = 1214
240675 Wp = 45
49822
YDOT = -6398
361431 meter/sec RA = 310
17297 deg
ZDOT = -4004
995720 TA = 182
39118
MA = 182
40190
Ha = 229
813 n
mi
Hp = 213
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17554393
70 X = -5347280
93
Y = 4769434
77 feet Y = 1393909
18 meter
Z = -12937807
39 Z = -3969428
47
XDOT = 3983
729250 XDOT = 1305
153698
YDOT = -20991
999446 feet/sec YDOT = -6384
274158 meter/sec
ZDOT = -13139
749739 ZDOT = -3998
877023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2216701
52 X = -675650
62
Y = -17977382
33 feet Y = -5479506
13 meter
Z = -13045729
77 Z = -3976338
43
XDOT = 18883
529626 XDOT = 5755
699830
YDOT = 7190
625509 feet/sec YDOT = 2191
702655 meter/sec
ZDOT = -13113
517100 ZDOT = -3997
000012
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 12348
52361845
00016717 00000-0 10270-3 0 9009
2 25544 51
6461 310
6540 0016645 35
1871 325
0376 15
52055805 5873
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
52361845 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 310
6540 deg
Eccentricity:
0016645
Arg of perigee: 35
1871 deg
Mean anomaly: 325
0376 deg
Mean motion: 15
52055805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 587
Checksum: 296
Coasting Arc #2 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2012/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4972056
20 A = 6786354
83 meter
Y = -758075
64 meter E =
0020408
Z = 4535535
38 I = 51
35135
XDOT = -1778
061941 Wp = 62
16053
YDOT = 6804
096723 meter/sec RA = 305
18242 deg
ZDOT = 3085
164181 TA = 356
87608
MA = 356
88880
Ha = 229
593 n
mi
Hp = 212
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16312520
33 X = 4958131
07
Y = -2487124
81 feet Y = -702553
46 meter
Z = 14880365
42 Z = 4559655
43
XDOT = -5833
536553 XDOT = -1869
001627
YDOT = 22323
151979 feet/sec YDOT = 6783
704442 meter/sec
ZDOT = 10121
929727 ZDOT = 3076
306466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 419589
64 X = 127890
92
Y = 16404844
09 feet Y = 5000196
48 meter
Z = 14980467
92 Z = 4566046
62
XDOT = -20205
370265 XDOT = -6158
596857
YDOT = -8695
698999 feet/sec YDOT = -2650
449055 meter/sec
ZDOT = 10084
292134 ZDOT = 3073
692243
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 12349
55382306
00016717 00000-0 10270-3 0 9019
2 25544 51
6466 305
5353 0016444 38
5725 321
6598 15
52104643 6037
Satellite: ISS
Catalog Number: 25544
Epoch time: 12349
55382306 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 305
5353 deg
Eccentricity:
0016444
Arg of perigee: 38
5725 deg
Mean anomaly: 321
6598 deg
Mean motion: 15
52104643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 300
Coasting Arc #3 (Orbit 617)
---------------------------------------
Vector Time (GMT): 2012/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4616613
47 A = 6784672
10 meter
Y = -17177
52 meter E =
0028165
Z = -4997018
55 I = 51
32887
XDOT = 2219
687076 Wp = 56
12966
YDOT = -7030
295539 meter/sec RA = 300
18582 deg
ZDOT = -2019
406428 TA = 194
05325
MA = 194
13178
Ha = 229
884 n
mi
Hp = 212
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15146369
65 X = -4591804
05
Y = -56356
70 feet Y = -68664
09 meter
Z = -16394417
81 Z = -5019385
44
XDOT = 7282
437915 XDOT = 2307
946098
YDOT = -23065
274078 feet/sec YDOT = -7004
979894 meter/sec
ZDOT = -6625
349174 ZDOT = -2008
409795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1698470
51 X = 517693
81
Y = -14949301
86 feet Y = -4556547
21 meter
Z = -16487152
48 Z = -5025284
07
XDOT = 21039
123961 XDOT = 6412
724983
YDOT = 9671
638194 feet/sec YDOT = 2947
915322 meter/sec
ZDOT = -6578
821667 ZDOT = -2005
224844
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 12350
51963174
00016717 00000-0 10270-3 0 9026
2 25544 51
6469 300
7352 0016601 42
1553 318
0872 15
52081950 6187
Satellite: ISS
Catalog Number: 25544
Epoch time: 12350
51963174 = yrday
fracday
Element set: 902
Inclination: 51
6469 deg
RA of node: 300
7352 deg
Eccentricity:
0016601
Arg of perigee: 42
1553 deg
Mean anomaly: 318
0872 deg
Mean motion: 15
52081950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 618
Checksum: 287
Coasting Arc #4 (Orbit 633)
---------------------------------------
Vector Time (GMT): 2012/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4209985
57 A = 6783394
76 meter
Y = 889690
63 meter E =
0017695
Z = 5229971
49 I = 51
31100
XDOT = -2596
256724 Wp = 55
63610
YDOT = 7172
020497 meter/sec RA = 295
18673 deg
ZDOT = 877
552968 TA = 25
98804
MA = 25
89930
Ha = 229
718 n
mi
Hp = 212
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13812288
63 X = 4174318
18
Y = 2918932
51 feet Y = 936569
41 meter
Z = 17158699
11 Z = 5250336
67
XDOT = -8517
902639 XDOT = -2680
525720
YDOT = 23530
250976 feet/sec YDOT = 7142
516276 meter/sec
ZDOT = 2879
110789 ZDOT = 864
736560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4168436
43 X = -1270539
42
Y = 13379937
26 feet Y = 4078204
88 meter
Z = 17243023
40 Z = 5255673
53
XDOT = -21670
010443 XDOT = -6605
019183
YDOT = -10359
453703 feet/sec YDOT = -3157
561489 meter/sec
ZDOT = 2825
030103 ZDOT = 861
069175
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 12351
54981340
00016717 00000-0 10270-3 0 9036
2 25544 51
6472 295
6164 0016525 45
5769 314
6732 15
52131610 6349
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
54981340 = yrday
fracday
Element set: 903
Inclination: 51
6472 deg
RA of node: 295
6164 deg
Eccentricity:
0016525
Arg of perigee: 45
5769 deg
Mean anomaly: 314
6732 deg
Mean motion: 15
52131610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 634
Checksum: 299
Coasting Arc #5 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2012/351/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2120269
03 A = 6786523
93 meter
Y = 4394161
11 meter E =
0024871
Z = 4706552
10 I = 51
31843
XDOT = -4847
298448 Wp = 53
27440
YDOT = 5285
338744 meter/sec RA = 294
80558 deg
ZDOT = -2726
196685 TA = 63
93037
MA = 63
67458
Ha = 230
552 n
mi
Hp = 212
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6956263
23 X = 2048111
86
Y = 14416539
07 feet Y = 4417467
40 meter
Z = 15441443
89 Z = 4716677
31
XDOT = -15903
210131 XDOT = -4892
796828
YDOT = 17340
350209 feet/sec YDOT = 5230
879073 meter/sec
ZDOT = -8944
214847 ZDOT = -2749
854464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11151093
53 X = -3398853
31
Y = 11427983
72 feet Y = 3483249
44 meter
Z = 15482851
40 Z = 4719173
11
XDOT = -20920
346924 XDOT = -6376
521742
YDOT = -8052
513645 feet/sec YDOT = -2454
406159 meter/sec
ZDOT = -9042
999766 ZDOT = -2756
306329
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 12351
61421017
00016717 00000-0 10270-3 0 9045
2 25544 51
6480 295
2965 0017203 49
3373 310
9271 15
51849215 6354
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
61421017 = yrday
fracday
Element set: 904
Inclination: 51
6480 deg
RA of node: 295
2965 deg
Eccentricity:
0017203
Arg of perigee: 49
3373 deg
Mean anomaly: 310
9271 deg
Mean motion: 15
51849215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 293
Coasting Arc #6 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2012/352/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1795038
51 A = 6788322
42 meter
Y = -5008838
23 meter E =
0022624
Z = -4228936
34 I = 51
31304
XDOT = 4789
173666 Wp = 70
11285
YDOT = -4749
811759 meter/sec RA = 289
81167 deg
ZDOT = 3616
309878 TA = 237
03140
MA = 237
24911
Ha = 230
586 n
mi
Hp = 212
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5889233
94 X = -1718352
17
Y = -16433196
28 feet Y = -5028482
40 meter
Z = -13874463
07 Z = -4237470
56
XDOT = 15712
512029 XDOT = 4824
364055
YDOT = -15583
371913 feet/sec YDOT = -4696
059714 meter/sec
ZDOT = 11864
533719 ZDOT = 3639
660412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13215487
21 X = 4028080
50
Y = -11363041
00 feet Y = -3463454
90 meter
Z = -13909203
39 Z = -4239525
19
XDOT = 19360
947295 XDOT = 5901
216736
YDOT = 7968
552260 feet/sec YDOT = 2428
814729 meter/sec
ZDOT = 11961
968292 ZDOT = 3646
007935
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 12352
58015627
00016717 00000-0 10270-3 0 9059
2 25544 51
6483 290
4980 0017209 52
8439 307
4281 15
51867485 6507
Satellite: ISS
Catalog Number: 25544
Epoch time: 12352
58015627 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 290
4980 deg
Eccentricity:
0017209
Arg of perigee: 52
8439 deg
Mean anomaly: 307
4281 deg
Mean motion: 15
51867485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 320
Coasting Arc #7 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2012/353/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1443130
25 A = 6790593
07 meter
Y = 5608138
34 meter E =
0028294
Z = 3533221
44 I = 51
31071
XDOT = -4756
562788 Wp = 69
27279
YDOT = 4050
827791 meter/sec RA = 284
81965 deg
ZDOT = -4448
093135 TA = 68
86949
MA = 68
56730
Ha = 230
639 n
mi
Hp = 212
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4734679
31 X = 1363148
14
Y = 18399403
99 feet Y = 5623828
92 meter
Z = 11591933
87 Z = 3540038
09
XDOT = -15605
520957 XDOT = -4779
898792
YDOT = 13290
117426 feet/sec YDOT = 3997
506693 meter/sec
ZDOT = -14593
481413 ZDOT = -4471
256608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15269437
74 X = -4654124
62
Y = 11276525
42 feet Y = 3437084
95 meter
Z = 11619485
00 Z = 3541619
03
XDOT = -17348
036667 XDOT = -5287
681576
YDOT = -8223
063121 feet/sec YDOT = -2506
389639 meter/sec
ZDOT = -14690
044750 ZDOT = -4477
525640
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 12353
61048774
00016717 00000-0 10270-3 0 9064
2 25544 51
6478 285
3792 0017211 56
7593 303
5205 15
51872657 6669
Satellite: ISS
Catalog Number: 25544
Epoch time: 12353
61048774 = yrday
fracday
Element set: 906
Inclination: 51
6478 deg
RA of node: 285
3792 deg
Eccentricity:
0017211
Arg of perigee: 56
7593 deg
Mean anomaly: 303
5205 deg
Mean motion: 15
51872657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 327
Coasting Arc #8 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2012/354/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1223902
50 A = 6792452
32 meter
Y = -6067101
33 meter E =
0021893
Z = -2799307
09 I = 51
31102
XDOT = 4700
236323 Wp = 60
06453
YDOT = -3275
433566 meter/sec RA = 279
83042 deg
ZDOT = 5084
691907 TA = 268
06842
MA = 268
31916
Ha = 230
600 n
mi
Hp = 212
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4015428
13 X = -1142369
58
Y = -19905188
09 feet Y = -6080331
76 meter
Z = -9184078
37 Z = -2805054
97
XDOT = 15420
722845 XDOT = 4711
813395
YDOT = -10746
173116 feet/sec YDOT = -3222
808092 meter/sec
ZDOT = 16682
060063 ZDOT = 5107
553315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16734587
10 X = 5100702
15
Y = -11483443
72 feet Y = -3500153
65 meter
Z = -9207148
64 Z = -2806338
91
XDOT = 15074
781504 XDOT = 4594
793402
YDOT = 8623
283714 feet/sec YDOT = 2628
376876 meter/sec
ZDOT = 16777
268522 ZDOT = 5113
711445
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 12354
57641197
00016717 00000-0 10270-3 0 9079
2 25544 51
6484 280
5806 0017175 60
1221 300
1635 15
51908286 6810
Satellite: ISS
Catalog Number: 25544
Epoch time: 12354
57641197 = yrday
fracday
Element set: 907
Inclination: 51
6484 deg
RA of node: 280
5806 deg
Eccentricity:
0017175
Arg of perigee: 60
1221 deg
Mean anomaly: 300
1635 deg
Mean motion: 15
51908286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 303
Coasting Arc #9 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2012/355/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 958278
99 A = 6794347
52 meter
Y = 6454579
21 meter E =
0028304
Z = 1872962
31 I = 51
31260
XDOT = -4692
116368 Wp = 85
89580
YDOT = 2341
013965 meter/sec RA = 274
84354 deg
ZDOT = -5591
600009 TA = 73
40587
MA = 73
09523
Ha = 230
680 n
mi
Hp = 212
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3143959
94 X = 876932
89
Y = 21176440
99 feet Y = 6464840
37 meter
Z = 6144889
48 Z = 1877420
31
XDOT = -15394
082571 XDOT = -4690
782655
YDOT = 7680
492011 feet/sec YDOT = 2288
551512 meter/sec
ZDOT = -18345
144388 ZDOT = -5614
390716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18043470
73 X = -5499649
88
Y = 11512675
28 feet Y = 3509063
43 meter
Z = 6162570
56 Z = 1878351
51
XDOT = -12428
034429 XDOT = -3788
064894
YDOT = -9475
574936 feet/sec YDOT = -2888
155240 meter/sec
ZDOT = -18439
940754 ZDOT = -5620
493942
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 12355
60672105
00016717 00000-0 10270-3 0 9088
2 25544 51
6481 275
4612 0017170 64
1382 296
1537 15
51893988 6976
Satellite: ISS
Catalog Number: 25544
Epoch time: 12355
60672105 = yrday
fracday
Element set: 908
Inclination: 51
6481 deg
RA of node: 275
4612 deg
Eccentricity:
0017170
Arg of perigee: 64
1382 deg
Mean anomaly: 296
1537 deg
Mean motion: 15
51893988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 328
Coasting Arc #10 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2012/356/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -798148
06 A = 6795285
19 meter
Y = -6670310
38 meter E =
0026142
Z = -976242
44 I = 51
31514
XDOT = 4708
532477 Wp = 56
91268
YDOT = -1405
842511 meter/sec RA = 269
85869 deg
ZDOT = 5884
706252 TA = 292
47108
MA = 292
74769
Ha = 230
594 n
mi
Hp = 212
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2618595
99 X = -718757
55
Y = -21884220
41 feet Y = -6678791
82 meter
Z = -3202895
15 Z = -979927
35
XDOT = 15447
941197 XDOT = 4695
316351
YDOT = -4612
344196 feet/sec YDOT = -1353
262982 meter/sec
ZDOT = 19306
779041 ZDOT = 5907
547933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18698930
93 X = 5699434
15
Y = -11663332
36 feet Y = -3554983
70 meter
Z = -3217350
69 Z = -980648
49
XDOT = 9844
473849 XDOT = 3000
595629
YDOT = 10546
823255 feet/sec YDOT = 3214
671728 meter/sec
ZDOT = 19401
671233 ZDOT = 5913
629392
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 12356
57262391
00016717 00000-0 10270-3 0 9098
2 25544 51
6486 270
6624 0017109 67
1723 293
1234 15
51941025 7120
Satellite: ISS
Catalog Number: 25544
Epoch time: 12356
57262391 = yrday
fracday
Element set: 909
Inclination: 51
6486 deg
RA of node: 270
6624 deg
Eccentricity:
0017109
Arg of perigee: 67
1723 deg
Mean anomaly: 293
1234 deg
Mean motion: 15
51941025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 302
Coasting Arc #11 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2012/357/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 557180
71 A = 6795765
07 meter
Y = 6770711
71 meter E =
0024804
Z = -62247
70 I = 51
31757
XDOT = -4774
980708 Wp = 96
93781
YDOT = 356
917437 meter/sec RA = 264
87524 deg
ZDOT = -5979
875946 TA = 83
73470
MA = 83
45222
Ha = 230
662 n
mi
Hp = 212
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1828020
71 X = 481730
16
Y = 22213621
09 feet Y = 6776520
59 meter
Z = -204224
74 Z = -59723
74
XDOT = -15665
947204 XDOT = -4749
567991
YDOT = 1170
988967 feet/sec YDOT = 303
663118 meter/sec
ZDOT = -19619
015571 ZDOT = -6003
010891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19130354
27 X = -5830931
98
Y = 11437657
52 feet Y = 3486198
01 meter
Z = -194589
64 Z = -59310
92
XDOT = -7070
822204 XDOT = -2155
186608
YDOT = -12041
167542 feet/sec YDOT = -3670
147867 meter/sec
ZDOT = -19714
997606 ZDOT = -6009
131270
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 12357
60291096
00016717 00000-0 10270-3 0 9109
2 25544 51
6486 265
5430 0017040 71
3760 288
9240 15
51914936 7287
Satellite: ISS
Catalog Number: 25544
Epoch time: 12357
60291096 = yrday
fracday
Element set: 910
Inclination: 51
6486 deg
RA of node: 265
5430 deg
Eccentricity:
0017040
Arg of perigee: 71
3760 deg
Mean anomaly: 288
9240 deg
Mean motion: 15
51914936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 310
Coasting Arc #12 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2012/358/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -380409
52 A = 6795204
71 meter
Y = -6698447
20 meter E =
0030191
Z = 1000708
98 I = 51
31984
XDOT = 4890
927205 Wp = 66
11046
YDOT = 619
690912 meter/sec RA = 259
89157 deg
ZDOT = 5878
524412 TA = 304
78245
MA = 305
06624
Ha = 230
575 n
mi
Hp = 211
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1248062
72 X = -310339
03
Y = -21976532
79 feet Y = -6702309
47 meter
Z = 3283165
95 Z = 999030
61
XDOT = 16046
349097 XDOT = 4855
077572
YDOT = 2033
106668 feet/sec YDOT = 674
183384 meter/sec
ZDOT = 19286
497414 ZDOT = 5902
197349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18975651
71 X = 5783778
64
Y = -11157535
32 feet Y = -3400816
77 meter
Z = 3277023
09 Z = 998836
64
XDOT = 4644
753770 XDOT = 1415
720949
YDOT = 13716
982214 feet/sec YDOT = 4180
936179 meter/sec
ZDOT = 19384
596385 ZDOT = 5908
424978
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 12358
63318516
00016717 00000-0 10270-3 0 9111
2 25544 51
6486 260
4241 0017036 74
3469 285
9561 15
51968273 7449
Satellite: ISS
Catalog Number: 25544
Epoch time: 12358
63318516 = yrday
fracday
Element set: 911
Inclination: 51
6486 deg
RA of node: 260
4241 deg
Eccentricity:
0017036
Arg of perigee: 74
3469 deg
Mean anomaly: 285
9561 deg
Mean motion: 15
51968273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 324
Coasting Arc #13 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2012/359/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 85226
45 A = 6793946
80 meter
Y = 6493895
39 meter E =
0020935
Z = -2009428
32 I = 51
32174
XDOT = -5029
430614 Wp = 94
66649
YDOT = -1630
850090 meter/sec RA = 254
90729 deg
ZDOT = -5535
470392 TA = 107
58216
MA = 107
35336
Ha = 230
584 n
mi
Hp = 211
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 279614
33 X = 22365
37
Y = 21305431
07 feet Y = 6494497
17 meter
Z = -6592612
61 Z = -2009166
35
XDOT = -16500
756607 XDOT = -4983
930206
YDOT = -5350
558039 feet/sec YDOT = -1686
837384 meter/sec
ZDOT = -18160
992101 ZDOT = -5559
792813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18636037
16 X = -5680264
13
Y = 10329648
41 feet Y = 3148476
84 meter
Z = -6592313
79 Z = -2009337
24
XDOT = -2256
314670 XDOT = -687
724711
YDOT = -15616
875025 feet/sec YDOT = -4760
023508 meter/sec
ZDOT = -18261
669607 ZDOT = -5566
156896
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 12359
59905855
00016717 00000-0 10270-3 0 9126
2 25544 51
6485 255
6248 0016887 78
2638 282
0407 15
51951943 7594
Satellite: ISS
Catalog Number: 25544
Epoch time: 12359
59905855 = yrday
fracday
Element set: 912
Inclination: 51
6485 deg
RA of node: 255
6248 deg
Eccentricity:
0016887
Arg of perigee: 78
2638 deg
Mean anomaly: 282
0407 deg
Mean motion: 15
51951943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 354
Coasting Arc #14 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2012/360/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 187383
10 A = 6792117
52 meter
Y = -6144801
96 meter E =
0030298
Z = 2855427
96 I = 51
32423
XDOT = 5214
699685 Wp = 81
10978
YDOT = 2519
340901 meter/sec RA = 249
92052 deg
ZDOT = 5038
107533 TA = 311
54567
MA = 311
80513
Ha = 230
556 n
mi
Hp = 211
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 614773
96 X = 242210
64
Y = -20160111
42 feet Y = -6142400
28 meter
Z = 9368201
96 Z = 2856470
76
XDOT = 17108
594766 XDOT = 5161
666351
YDOT = 8265
554137 feet/sec YDOT = 2577
357860 meter/sec
ZDOT = 16529
224189 ZDOT = 5063
311745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17881883
39 X = 5450398
06
Y = -9324770
79 feet Y = -2842190
14 meter
Z = 9373267
48 Z = 2856971
93
XDOT = 375
500984 XDOT = 114
452700
YDOT = 17575
983705 feet/sec YDOT = 5357
159833 meter/sec
ZDOT = 16633
462311 ZDOT = 5069
879312
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 12360
62931271
00016717 00000-0 10270-3 0 9134
2 25544 51
6480 250
5057 0016975 81
2890 279
0184 15
51985180 7759
Satellite: ISS
Catalog Number: 25544
Epoch time: 12360
62931271 = yrday
fracday
Element set: 913
Inclination: 51
6480 deg
RA of node: 250
5057 deg
Eccentricity:
0016975
Arg of perigee: 81
2890 deg
Mean anomaly: 279
0184 deg
Mean motion: 15
51985180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 317
Coasting Arc #15 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2012/361/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -603544
87 A = 6789775
60 meter
Y = 5681129
06 meter E =
0022420
Z = -3690561
10 I = 51
32712
XDOT = -5366
174501 Wp = 83
86229
YDOT = -3349
983279 meter/sec RA = 244
93109 deg
ZDOT = -4299
563342 TA = 140
16585
MA = 140
00107
Ha = 230
501 n
mi
Hp = 211
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1980134
09 X = -649099
76
Y = 18638874
89 feet Y = 5674125
57 meter
Z = -12108140
08 Z = -3693603
07
XDOT = -17605
559388 XDOT = -5307
429235
YDOT = -10990
758789 feet/sec YDOT = -3409
662235 meter/sec
ZDOT = -14106
178942 ZDOT = -4325
489572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17079159
06 X = -5205727
68
Y = 7701215
52 feet Y = 2347330
49 meter
Z = -12121437
60 Z = -3694614
18
XDOT = 1282
081047 XDOT = 390
778303
YDOT = -19423
361768 feet/sec YDOT = -5920
240667 meter/sec
ZDOT = -14213
325836 ZDOT = -4332
221715
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 12361
59516554
00016717 00000-0 10270-3 0 9145
2 25544 51
6471 245
7062 0016803 85
1464 275
1606 15
51996495 7905
Satellite: ISS
Catalog Number: 25544
Epoch time: 12361
59516554 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 245
7062 deg
Eccentricity:
0016803
Arg of perigee: 85
1464 deg
Mean anomaly: 275
1606 deg
Mean motion: 15
51996495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 324
Coasting Arc #16 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2012/362/13:41:50
532
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1025649
43 A = 6787597
60 meter
Y = -5120509
56 meter E =
0026264
Z = 4314758
33 I = 51
33315
XDOT = 5537
194058 Wp = 95
65100
YDOT = 4041
361726 meter/sec RA = 239
93885 deg
ZDOT = 3459
101646 TA = 319
01265
MA = 319
20975
Ha = 230
521 n
mi
Hp = 211
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3364991
57 X = 1061871
86
Y = -16799572
05 feet Y = -5108838
09 meter
Z = 14156031
28 Z = 4319828
23
XDOT = 18166
647173 XDOT = 5474
787759
YDOT = 13259
060780 feet/sec YDOT = 4102
932751 meter/sec
ZDOT = 11348
758682 ZDOT = 3485
849778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16077713
99 X = 4900487
22
Y = -5868797
49 feet Y = -1788809
47 meter
Z = 14177670
46 Z = 4321353
96
XDOT = -2436
505357 XDOT = -742
646833
YDOT = 21172
066756 feet/sec YDOT = 6453
245947 meter/sec
ZDOT = 11459
249218 ZDOT = 3492
779162
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 12362
62540008
00016717 00000-0 10270-3 0 9152
2 25544 51
6466 240
5867 0016933 88
4872 271
8219 15
51999439 8060
Satellite: ISS
Catalog Number: 25544
Epoch time: 12362
62540008 = yrday
fracday
Element set: 915
Inclination: 51
6466 deg
RA of node: 240
5867 deg
Eccentricity:
0016933
Arg of perigee: 88
4872 deg
Mean anomaly: 271
8219 deg
Mean motion: 15
51999439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 336
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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