[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 6th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26909 78 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
258/03:19:36
859 -3
7 4
2 4
2
N/A -1
3 0
0 234
5
000/00:09:13
718 1
5 -0
0 214
7
Coasting Arc #1 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2012/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2471164
17 A = 6793309
95 meter
Y = 4822904
74 meter E =
0021853
Z = 4072513
81 I = 51
98681
XDOT = -3920
710163 Wp = 62
31242
YDOT = -5316
172970 meter/sec RA = 81
15565 deg
ZDOT = 3910
576291 TA = 347
37491
MA = 347
42956
Ha = 232
092 n
mi
Hp = 216
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8107493
99 X = -2544694
61
Y = 15823178
30 feet Y = 4794859
81 meter
Z = 13361265
79 Z = 4060330
04
XDOT = -12863
222321 XDOT = -3879
968946
YDOT = -17441
512368 feet/sec YDOT = -5359
788713 meter/sec
ZDOT = 12829
974709 ZDOT = 3891
628976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12190441
91 X = 3715646
69
Y = -12994386
08 feet Y = -3960688
88 meter
Z = 13310406
09 Z = 4057011
77
XDOT = 6752
814032 XDOT = 2058
257717
YDOT = 19417
821896 feet/sec YDOT = 5918
552114 meter/sec
ZDOT = 12752
122372 ZDOT = 3886
846899
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 12249
55558332
00016717 00000-0 10270-3 0 9001
2 25544 51
6430 81
6183 0015290 35
9954 324
2223 15
50366938 30513
Satellite: ISS
Catalog Number: 25544
Epoch time: 12249
55558332 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 81
6183 deg
Eccentricity:
0015290
Arg of perigee: 35
9954 deg
Mean anomaly: 324
2223 deg
Mean motion: 15
50366938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 298
Coasting Arc #2 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2012/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2391864
58 A = 6792140
31 meter
Y = -4629540
31 meter E =
0023334
Z = -4381145
91 I = 51
97727
XDOT = 4123
804294 Wp = 50
46734
YDOT = 5417
987338 meter/sec RA = 76
22036 deg
ZDOT = -3471
709351 TA = 184
30933
MA = 184
32946
Ha = 232
029 n
mi
Hp = 216
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7847324
73 X = 2464737
94
Y = -15188780
55 feet Y = -4602385
79 meter
Z = -14373838
28 Z = -4369349
04
XDOT = 13529
541646 XDOT = 4079
777553
YDOT = 17775
549009 feet/sec YDOT = 5463
855912 meter/sec
ZDOT = -11390
122544 ZDOT = -3451
783330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11557310
88 X = -3522668
36
Y = 12653913
49 feet Y = 3856912
83 meter
Z = -14324588
14 Z = -4366134
47
XDOT = -7675
933817 XDOT = -2339
624627
YDOT = -19819
755604 feet/sec YDOT = -6041
061508 meter/sec
ZDOT = -11308
240847 ZDOT = -3446
751810
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 12250
52244331
00016717 00000-0 10270-3 0 9012
2 25544 51
6426 76
8251 0015364 40
0475 320
1806 15
50415767 30660
Satellite: ISS
Catalog Number: 25544
Epoch time: 12250
52244331 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 76
8251 deg
Eccentricity:
0015364
Arg of perigee: 40
0475 deg
Mean anomaly: 320
1806 deg
Mean motion: 15
50415767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 276
Coasting Arc #3 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2012/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2335339
22 A = 6791076
76 meter
Y = 4373341
57 meter E =
0019661
Z = 4621572
95 I = 51
96583
XDOT = -4374
018939 Wp = 66
88112
YDOT = -5535
396789 meter/sec RA = 71
28308 deg
ZDOT = 3025
174801 TA = 353
08222
MA = 353
10931
Ha = 232
122 n
mi
Hp = 215
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7661874
09 X = -2406519
84
Y = 14348233
50 feet Y = 4346828
59 meter
Z = 15162640
92 Z = 4610054
86
XDOT = -14350
455836 XDOT = -4326
491522
YDOT = -18160
750619 feet/sec YDOT = -5584
043902 meter/sec
ZDOT = 9925
114178 ZDOT = 3004
041723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10961530
02 X = 3341074
35
Y = -12077943
44 feet Y = -3681357
16 meter
Z = 15114560
56 Z = 4606918
06
XDOT = 8768
298422 XDOT = 2672
577359
YDOT = 20280
546748 feet/sec YDOT = 6181
510649 meter/sec
ZDOT = 9838
259422 ZDOT = 2998
701472
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 12251
55373504
00016717 00000-0 10270-3 0 9022
2 25544 51
6426 71
7116 0015284 43
3160 316
9190 15
50437745 30829
Satellite: ISS
Catalog Number: 25544
Epoch time: 12251
55373504 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 71
7116 deg
Eccentricity:
0015284
Arg of perigee: 43
3160 deg
Mean anomaly: 316
9190 deg
Mean motion: 15
50437745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 285
Coasting Arc #4 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2012/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2349102
82 A = 6790023
23 meter
Y = -4136480
22 meter E =
0026372
Z = -4870021
79 I = 51
95235
XDOT = 4588
114269 Wp = 57
88033
YDOT = 5570
027806 meter/sec RA = 66
34490 deg
ZDOT = -2514
286571 TA = 187
40444
MA = 187
44346
Ha = 232
034 n
mi
Hp = 215
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7707030
25 X = 2418840
65
Y = -13571129
32 feet Y = -4109821
38 meter
Z = -15977761
77 Z = -4858440
39
XDOT = 15052
868336 XDOT = 4537
701886
YDOT = 18274
369442 feet/sec YDOT = 5621
052976 meter/sec
ZDOT = -8248
971691 ZDOT = -2492
120443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10628190
95 X = -3239472
60
Y = 11495971
68 feet Y = 3503972
17 meter
Z = -15929435
96 Z = -4855292
08
XDOT = -9821
415742 XDOT = -2993
567518
YDOT = -20400
599210 feet/sec YDOT = -6218
102639 meter/sec
ZDOT = -8157
854075 ZDOT = -2486
513922
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 12252
52054659
00016717 00000-0 10270-3 0 9038
2 25544 51
6428 66
9184 0015374 47
4830 312
7617 15
50494602 30970
Satellite: ISS
Catalog Number: 25544
Epoch time: 12252
52054659 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 66
9184 deg
Eccentricity:
0015374
Arg of perigee: 47
4830 deg
Mean anomaly: 312
7617 deg
Mean motion: 15
50494602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 312
Coasting Arc #5 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2012/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2398593
01 A = 6789156
95 meter
Y = 3844587
44 meter E =
0017863
Z = 5039263
59 I = 51
93622
XDOT = -4835
863393 Wp = 68
38813
YDOT = -5620
319369 meter/sec RA = 61
40386 deg
ZDOT = 1986
889849 TA = 2
42244
MA = 2
41380
Ha = 232
149 n
mi
Hp = 215
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7869399
64 X = -2465885
24
Y = 12613475
85 feet Y = 3817388
84 meter
Z = 16533017
02 Z = 5027447
76
XDOT = -15865
693546 XDOT = -4782
308232
YDOT = -18439
368008 feet/sec YDOT = -5674
097477 meter/sec
ZDOT = 6518
667484 ZDOT = 1963
527851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10394171
58 X = 3168143
50
Y = -10705849
43 feet Y = -3263142
91 meter
Z = 16483745
34 Z = 5024245
58
XDOT = 10992
827523 XDOT = 3350
613829
YDOT = 20557
720864 feet/sec YDOT = 6265
993319 meter/sec
ZDOT = 6422
613737 ZDOT = 1957
612667
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 12253
55178608
00016717 00000-0 10270-3 0 9044
2 25544 51
6425 61
8045 0015329 50
7292 309
5216 15
50509673 31139
Satellite: ISS
Catalog Number: 25544
Epoch time: 12253
55178608 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 61
8045 deg
Eccentricity:
0015329
Arg of perigee: 50
7292 deg
Mean anomaly: 309
5216 deg
Mean motion: 15
50509673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 297
Coasting Arc #6 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2012/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2514541
78 A = 6788372
17 meter
Y = -3591742
10 meter E =
0028556
Z = -5207476
33 I = 51
91958
XDOT = 5027
222577 Wp = 66
14810
YDOT = 5578
044008 meter/sec RA = 56
46242 deg
ZDOT = -1414
756018 TA = 190
21864
MA = 190
27682
Ha = 232
016 n
mi
Hp = 215
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8249808
98 X = 2579815
09
Y = -11783930
77 feet Y = -3563258
21 meter
Z = -17084896
11 Z = -5195102
16
XDOT = 16493
512392 XDOT = 4971
346622
YDOT = 18300
669319 feet/sec YDOT = 5633
949056 meter/sec
ZDOT = -4641
587987 ZDOT = -1390
470131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10428769
18 X = -3178688
85
Y = 9996012
38 feet Y = 3046784
57 meter
Z = -17033336
65 Z = -5191761
01
XDOT = -12040
905246 XDOT = -3670
067919
YDOT = -20329
784859 feet/sec YDOT = -6196
518425 meter/sec
ZDOT = -4541
712301 ZDOT = -1384
313909
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 12254
51854729
00016717 00000-0 10270-3 0 9057
2 25544 51
6433 57
0115 0015393 54
7732 305
4858 15
50575538 31283
Satellite: ISS
Catalog Number: 25544
Epoch time: 12254
51854729 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 57
0115 deg
Eccentricity:
0015393
Arg of perigee: 54
7732 deg
Mean anomaly: 305
4858 deg
Mean motion: 15
50575538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 314
Coasting Arc #7 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2012/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2674642
10 A = 6787876
07 meter
Y = 3293600
72 meter E =
0017182
Z = 5284047
04 I = 51
89988
XDOT = -5234
194283 Wp = 66
92029
YDOT = -5554
522348 meter/sec RA = 51
51699 deg
ZDOT = 817
246973 TA = 15
32981
MA = 15
27782
Ha = 232
159 n
mi
Hp = 215
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8775072
52 X = -2736941
55
Y = 10805776
63 feet Y = 3263343
18 meter
Z = 17336112
34 Z = 5270902
34
XDOT = -17172
553423 XDOT = -5175
663415
YDOT = -18223
498516 feet/sec YDOT = -5612
727057 meter/sec
ZDOT = 2681
256472 ZDOT = 791
962198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10606137
70 X = 3232750
77
Y = -9119800
48 feet Y = -2779715
19 meter
Z = 17281394
03 Z = 5267368
90
XDOT = 13136
038414 XDOT = 4003
864509
YDOT = 20132
807882 feet/sec YDOT = 6136
479842 meter/sec
ZDOT = 2577
249804 ZDOT = 785
545740
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 12255
54973285
00016717 00000-0 10270-3 0 9061
2 25544 51
6427 51
8967 0015395 58
0490 302
2155 15
50584007 31447
Satellite: ISS
Catalog Number: 25544
Epoch time: 12255
54973285 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 51
8967 deg
Eccentricity:
0015395
Arg of perigee: 58
0490 deg
Mean anomaly: 302
2155 deg
Mean motion: 15
50584007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 312
Coasting Arc #8 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2012/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2890107
09 A = 6787497
51 meter
Y = -3055599
26 meter E =
0029400
Z = -5352061
41 I = 51
88075
XDOT = 5364
648023 Wp = 74
63992
YDOT = 5437
917884 meter/sec RA = 46
57206 deg
ZDOT = -201
069982 TA = 193
40421
MA = 193
48248
Ha = 231
969 n
mi
Hp = 214
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9481978
66 X = 2950059
52
Y = -10024931
96 feet Y = -3022945
49 meter
Z = -17559256
58 Z = -5337875
66
XDOT = 17600
551258 XDOT = 5304
418128
YDOT = 17840
937939 feet/sec YDOT = 5497
571942 meter/sec
ZDOT = -659
678420 ZDOT = -175
155724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11026469
56 X = -3360867
92
Y = 8419779
12 feet Y = 2566348
67 meter
Z = -17500256
01 Z = -5334078
03
XDOT = -14014
492538 XDOT = -4271
617326
YDOT = -19548
223600 feet/sec YDOT = -5958
298553 meter/sec
ZDOT = -553
059026 ZDOT = -168
572391
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 12256
51644184
00016717 00000-0 10270-3 0 9073
2 25544 51
6439 47
1038 0015403 61
8071 298
4634 15
50659542 31595
Satellite: ISS
Catalog Number: 25544
Epoch time: 12256
51644184 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 47
1038 deg
Eccentricity:
0015403
Arg of perigee: 61
8071 deg
Mean anomaly: 298
4634 deg
Mean motion: 15
50659542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 312
Coasting Arc #9 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2012/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3152132
56 A = 6787522
30 meter
Y = 2782197
55 meter E =
0018167
Z = 5314837
76 I = 51
85903
XDOT = -5488
468634 Wp = 65
32670
YDOT = -5346
865266 meter/sec RA = 41
62245 deg
ZDOT = -447
547283 TA = 28
97533
MA = 28
87460
Ha = 232
131 n
mi
Hp = 214
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10341642
26 X = -3208827
47
Y = 9127944
71 feet Y = 2746631
98 meter
Z = 17437131
76 Z = 5299386
98
XDOT = -18006
786857 XDOT = -5426
096895
YDOT = -17542
208879 feet/sec YDOT = -5407
892050 meter/sec
ZDOT = -1468
330981 ZDOT = -474
057750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11607036
95 X = 3537824
86
Y = -7601353
35 feet Y = -2316892
50 meter
Z = 17372927
91 Z = 5295268
43
XDOT = 14852
710008 XDOT = 4527
106011
YDOT = 19009
715459 feet/sec YDOT = 5794
161272 meter/sec
ZDOT = -1577
421792 ZDOT = -480
798162
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 12257
54757174
00016717 00000-0 10270-3 0 9082
2 25544 51
6435 41
9884 0015441 65
1699 295
1056 15
50662847 31759
Satellite: ISS
Catalog Number: 25544
Epoch time: 12257
54757174 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 41
9884 deg
Eccentricity:
0015441
Arg of perigee: 65
1699 deg
Mean anomaly: 295
1056 deg
Mean motion: 15
50662847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 335
Coasting Arc #10 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2012/258/03:24:13
718
Vector Time (MET): N/A
Weight (LBS) : 953928
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1603667
77 A = 6789907
32 meter
Y = 3984127
25 meter E =
0021008
Z = 5240762
20 I = 51
84765
XDOT = -6445
739955 Wp = 73
02609
YDOT = -4026
483240 meter/sec RA = 38
46705 deg
ZDOT = 1091
003201 TA = 6
57720
MA = 6
54967
Ha = 234
462 n
mi
Hp = 214
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5261377
20 X = -1673558
18
Y = 13071283
64 feet Y = 3965803
86 meter
Z = 17194101
72 Z = 5232801
50
XDOT = -21147
440797 XDOT = -6405
535731
YDOT = -13210
246851 feet/sec YDOT = -4098
338604 meter/sec
ZDOT = 3579
406827 ZDOT = 1059
788429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5166582
00 X = 1574774
19
Y = 13152668
63 feet Y = 4008933
40 meter
Z = 17160752
26 Z = 5230597
29
XDOT = -23466
149614 XDOT = -7152
482402
YDOT = 4725
829606 feet/sec YDOT = 1440
432864 meter/sec
ZDOT = 3450
721685 ZDOT = 1051
779970
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 12258
19204402
00016717 00000-0 10270-3 0 9096
2 25544 51
6459 38
7974 0018807 64
9739 295
3362 15
49943266 31858
Satellite: ISS
Catalog Number: 25544
Epoch time: 12258
19204402 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 38
7974 deg
Eccentricity:
0018807
Arg of perigee: 64
9739 deg
Mean anomaly: 295
3362 deg
Mean motion: 15
49943266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 348
Coasting Arc #11 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2012/259/03:24:13
718
Vector Time (MET): N/A
Weight (LBS) : 953928
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1609740
21 A = 6789687
30 meter
Y = -3945793
11 meter E =
0033186
Z = -5314391
05 I = 51
82368
XDOT = 6637
813309 Wp = 74
90656
YDOT = 3704
223233 meter/sec RA = 33
52448 deg
ZDOT = -735
124291 TA = 188
03326
MA = 188
08653
Ha = 234
421 n
mi
Hp = 214
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5281299
90 X = 1679559
27
Y = -12945515
46 feet Y = -3927402
31 meter
Z = -17435666
17 Z = -5306400
93
XDOT = 21777
602720 XDOT = 6599
469633
YDOT = 12152
963364 feet/sec YDOT = 3778
236915 meter/sec
ZDOT = -2411
825103 ZDOT = -702
971832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5288327
45 X = -1611882
21
Y = -12987609
67 feet Y = -3958623
43 meter
Z = -17402199
33 Z = -5304190
36
XDOT = 23084
943383 XDOT = 7036
290743
YDOT = -6325
758449 feet/sec YDOT = -1928
091175 meter/sec
ZDOT = -2279
235552 ZDOT = -694
710996
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 12259
15919037
00016717 00000-0 10270-3 0 9102
2 25544 51
6469 34
0062 0018944 68
1803 292
1361 15
49963336 32008
Satellite: ISS
Catalog Number: 25544
Epoch time: 12259
15919037 = yrday
fracday
Element set: 910
Inclination: 51
6469 deg
RA of node: 34
0062 deg
Eccentricity:
0018944
Arg of perigee: 68
1803 deg
Mean anomaly: 292
1361 deg
Mean motion: 15
49963336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 304
Coasting Arc #12 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2012/260/03:24:13
718
Vector Time (MET): N/A
Weight (LBS) : 953928
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1649505
88 A = 6789323
66 meter
Y = 3864675
83 meter E =
0020982
Z = 5314989
43 I = 51
79746
XDOT = -6865
664195 Wp = 74
88209
YDOT = -3418
394556 meter/sec RA = 28
57982 deg
ZDOT = 359
018604 TA = 11
73101
MA = 11
68220
Ha = 234
373 n
mi
Hp = 214
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5411764
71 X = -1718417
95
Y = 12679382
64 feet Y = 3845845
44 meter
Z = 17437629
35 Z = 5306808
28
XDOT = -22525
144998 XDOT = -6828
672757
YDOT = -11215
205235 feet/sec YDOT = -3494
963816 meter/sec
ZDOT = 1177
882560 ZDOT = 325
755800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5229295
59 X = 1593889
30
Y = 12802408
30 feet Y = 3902174
05 meter
Z = 17403380
94 Z = 5304550
51
XDOT = -22824
416549 XDOT = -6956
882164
YDOT = 7926
839885 feet/sec YDOT = 2416
100797 meter/sec
ZDOT = 1040
680881 ZDOT = 317
199532
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 12260
19078263
00016717 00000-0 10270-3 0 9116
2 25544 51
6470 28
8956 0018797 71
6793 288
6400 15
50029298 32169
Satellite: ISS
Catalog Number: 25544
Epoch time: 12260
19078263 = yrday
fracday
Element set: 911
Inclination: 51
6470 deg
RA of node: 28
8956 deg
Eccentricity:
0018797
Arg of perigee: 71
6793 deg
Mean anomaly: 288
6400 deg
Mean motion: 15
50029298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 329
Coasting Arc #13 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2012/261/03:24:13
718
Vector Time (MET): N/A
Weight (LBS) : 953928
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1714979
99 A = 6789274
57 meter
Y = -3850490
42 meter E =
0033393
Z = -5350831
27 I = 51
77115
XDOT = 6987
797170 Wp = 81
28931
YDOT = 3081
274475 meter/sec RA = 23
63319 deg
ZDOT = 27
398820 TA = 188
94253
MA = 189
00215
Ha = 234
303 n
mi
Hp = 214
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5626574
78 X = 1783902
81
Y = -12632842
58 feet Y = -3830927
77 meter
Z = -17555220
70 Z = -5342332
01
XDOT = 22925
843734 XDOT = 6952
689269
YDOT = 10109
168226 feet/sec YDOT = 3159
220087 meter/sec
ZDOT = 89
891142 ZDOT = 61
259747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5267112
12 X = -1605415
77
Y = -12835574
39 feet Y = -3912283
07 meter
Z = -17519657
22 Z = -5339991
52
XDOT = 22139
765705 XDOT = 6748
200587
YDOT = -9375
767420 feet/sec YDOT = -2857
733910 meter/sec
ZDOT = 229
590535 ZDOT = 69
979195
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 12261
15787591
00016717 00000-0 10270-3 0 9125
2 25544 51
6479 24
1044 0018872 74
8252 285
4985 15
50049517 32310
Satellite: ISS
Catalog Number: 25544
Epoch time: 12261
15787591 = yrday
fracday
Element set: 912
Inclination: 51
6479 deg
RA of node: 24
1044 deg
Eccentricity:
0018872
Arg of perigee: 74
8252 deg
Mean anomaly: 285
4985 deg
Mean motion: 15
50049517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 319
Coasting Arc #14 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2012/262/03:24:13
718
Vector Time (MET): N/A
Weight (LBS) : 953928
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1815770
34 A = 6789112
38 meter
Y = 3802291
44 meter E =
0021461
Z = 5305586
26 I = 51
74332
XDOT = -7141
902504 Wp = 76
59292
YDOT = -2783
801404 meter/sec RA = 18
68414 deg
ZDOT = -442
823590 TA = 17
65630
MA = 17
58183
Ha = 234
252 n
mi
Hp = 214
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5957251
77 X = -1883927
00
Y = 12474709
45 feet Y = 3781605
89 meter
Z = 17406779
08 Z = 5296599
26
XDOT = -23431
438661 XDOT = -7108
091493
YDOT = -9133
206705 feet/sec YDOT = -2863
477615 meter/sec
ZDOT = -1452
833299 ZDOT = -477
436524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5148240
24 X = 1569183
62
Y = 12880591
31 feet Y = 3926004
23 meter
Z = 17369201
84 Z = 5294132
72
XDOT = -21577
914514 XDOT = -6576
948344
YDOT = 10804
426934 feet/sec YDOT = 3293
189330 meter/sec
ZDOT = -1595
662781 ZDOT = -486
358016
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 12262
18941133
00016717 00000-0 10270-3 0 9134
2 25544 51
6480 18
9937 0018754 78
3213 282
0041 15
50117619 32471
Satellite: ISS
Catalog Number: 25544
Epoch time: 12262
18941133 = yrday
fracday
Element set: 913
Inclination: 51
6480 deg
RA of node: 18
9937 deg
Eccentricity:
0018754
Arg of perigee: 78
3213 deg
Mean anomaly: 282
0041 deg
Mean motion: 15
50117619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 299
Coasting Arc #15 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2012/263/03:24:13
718
Vector Time (MET): N/A
Weight (LBS) : 953928
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1929641
68 A = 6789285
13 meter
Y = -3828813
45 meter E =
0032894
Z = -5292423
08 I = 51
71504
XDOT = 7183
724171 Wp = 87
71688
YDOT = 2448
986204 meter/sec RA = 13
73293 deg
ZDOT = 853
368698 TA = 190
43257
MA = 190
50099
Ha = 234
158 n
mi
Hp = 214
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6330845
40 X = 1998022
55
Y = -12561723
90 feet Y = -3806853
14 meter
Z = -17363592
80 Z = -5282882
41
XDOT = 23568
648854 XDOT = 7151
659661
YDOT = 8034
731642 feet/sec YDOT = 2529
139885 meter/sec
ZDOT = 2799
766069 ZDOT = 888
189202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5187978
25 X = -1581295
77
Y = -13128002
89 feet Y = -4001415
28 meter
Z = -17323720
37 Z = -5280269
97
XDOT = 20624
266447 XDOT = 6286
276413
YDOT = -12009
113023 feet/sec YDOT = -3660
377649 meter/sec
ZDOT = 2943
480383 ZDOT = 897
172821
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 12263
15645066
00016717 00000-0 10270-3 0 9149
2 25544 51
6481 14
2022 0018769 81
4780 278
8496 15
50135557 32621
Satellite: ISS
Catalog Number: 25544
Epoch time: 12263
15645066 = yrday
fracday
Element set: 914
Inclination: 51
6481 deg
RA of node: 14
2022 deg
Eccentricity:
0018769
Arg of perigee: 81
4780 deg
Mean anomaly: 278
8496 deg
Mean motion: 15
50135557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 314
Coasting Arc #16 (Orbit 3277)
---------------------------------------
Vector Time (GMT): 2012/264/03:24:13
718
Vector Time (MET): N/A
Weight (LBS) : 953928
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2077686
05 A = 6789379
30 meter
Y = 3828290
68 meter E =
0022556
Z = 5189668
35 I = 51
68643
XDOT = -7252
190412 Wp = 78
91725
YDOT = -2160
103536 meter/sec RA = 8
77923 deg
ZDOT = -1300
927272 TA = 23
60517
MA = 23
50183
Ha = 234
104 n
mi
Hp = 214
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6816555
30 X = -2145550
91
Y = 12560008
81 feet Y = 3804677
62 meter
Z = 17026470
97 Z = 5179409
81
XDOT = -23793
275631 XDOT = -7221
176998
YDOT = -7086
953858 feet/sec YDOT = -2241
028738 meter/sec
ZDOT = -4268
134096 ZDOT = -1336
083001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5098758
07 X = 1554101
46
Y = 13404440
82 feet Y = 4085673
56 meter
Z = 16983627
21 Z = 5176609
57
XDOT = -19804
824201 XDOT = -6036
510417
YDOT = 13162
643284 feet/sec YDOT = 4011
973673 meter/sec
ZDOT = -4413
259302 ZDOT = -1345
161435
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 12264
18792832
00016717 00000-0 10270-3 0 9158
2 25544 51
6481 9
0911 0018678 84
9779 275
3503 15
50205668 32784
Satellite: ISS
Catalog Number: 25544
Epoch time: 12264
18792832 = yrday
fracday
Element set: 915
Inclination: 51
6481 deg
RA of node: 9
0911 deg
Eccentricity:
0018678
Arg of perigee: 84
9779 deg
Mean anomaly: 275
3503 deg
Mean motion: 15
50205668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3278
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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