[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 27th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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
037/17:01:26
708 -0
6 1
1 1
1
N/A 0
3 -0
1 223
7
000/00:02:49
415 0
9 -0
0 220
0
Coasting Arc #1 (Orbit 1254)
---------------------------------------
Vector Time (GMT): 2013/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1560773
62 A = 6791867
46 meter
Y = -5964060
57 meter E =
0017331
Z = 2822012
12 I = 52
00677
XDOT = 4431
008331 Wp = 149
89477
YDOT = -3589
176707 meter/sec RA = 96
28458 deg
ZDOT = -5135
716520 TA = 358
22526
MA = 358
23140
Ha = 226
939 n
mi
Hp = 217
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5120648
36 X = -1507674
51
Y = -19567127
86 feet Y = -5981217
34 meter
Z = 9258569
95 Z = 2814558
91
XDOT = 14537
428909 XDOT = 4495
761338
YDOT = -11775
514129 feet/sec YDOT = -3539
264128 meter/sec
ZDOT = -16849
463647 ZDOT = -5114
034401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13286858
99 X = 4049834
62
Y = -15268035
35 feet Y = -4653697
18 meter
Z = 9228278
53 Z = 2812779
30
XDOT = 16851
280601 XDOT = 5136
270327
YDOT = 4537
304360 feet/sec YDOT = 1382
970369 meter/sec
ZDOT = -16758
800013 ZDOT = -5108
082244
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 13025
53791125
00016717 00000-0 10270-3 0 9001
2 25544 51
6477 96
9607 0013452 199
5333 160
5305 15
52104575 12555
Satellite: ISS
Catalog Number: 25544
Epoch time: 13025
53791125 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 96
9607 deg
Eccentricity:
0013452
Arg of perigee: 199
5333 deg
Mean anomaly: 160
5305 deg
Mean motion: 15
52104575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1255
Checksum: 300
Coasting Arc #2 (Orbit 1269)
---------------------------------------
Vector Time (GMT): 2013/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1324310
16 A = 6793783
29 meter
Y = 6394860
07 meter E =
0006819
Z = -1887674
97 I = 52
01463
XDOT = -4470
929255 Wp = 186
83710
YDOT = 2595
055865 meter/sec RA = 91
34490 deg
ZDOT = 5645
964569 TA = 152
53377
MA = 152
49772
Ha = 226
721 n
mi
Hp = 217
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4344849
59 X = 1261872
65
Y = 20980512
03 feet Y = 6409320
27 meter
Z = -6193159
35 Z = -1881393
24
XDOT = -14668
403068 XDOT = -4527
041364
YDOT = 8513
962812 feet/sec YDOT = 2544
745256 meter/sec
ZDOT = 18523
505805 ZDOT = 5624
109470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14635639
67 X = -4460942
97
Y = 15657941
78 feet Y = 4772540
65 meter
Z = -6167798
36 Z = -1879944
94
XDOT = -14328
947974 XDOT = -4367
463342
YDOT = -6121
541321 feet/sec YDOT = -1865
845795 meter/sec
ZDOT = 18432
235309 ZDOT = 5618
145322
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 13026
50370598
00016717 00000-0 10270-3 0 9017
2 25544 51
6470 92
1611 0013384 203
3067 156
7479 15
52082611 12705
Satellite: ISS
Catalog Number: 25544
Epoch time: 13026
50370598 = yrday
fracday
Element set: 901
Inclination: 51
6470 deg
RA of node: 92
1611 deg
Eccentricity:
0013384
Arg of perigee: 203
3067 deg
Mean anomaly: 156
7479 deg
Mean motion: 15
52082611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1270
Checksum: 286
Coasting Arc #3 (Orbit 1285)
---------------------------------------
Vector Time (GMT): 2013/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1097531
56 A = 6794821
20 meter
Y = -6634815
59 meter E =
0020280
Z = 870528
03 I = 52
01852
XDOT = 4572
275760 Wp = 165
83028
YDOT = -1540
748279 meter/sec RA = 86
40784 deg
ZDOT = -5968
282215 TA = 4
79619
MA = 4
77679
Ha = 226
477 n
mi
Hp = 217
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3600825
33 X = -1027486
77
Y = -21767767
67 feet Y = -6646697
23 meter
Z = 2856063
11 Z = 865366
57
XDOT = 15000
904723 XDOT = 4618
156521
YDOT = -5054
948421 feet/sec YDOT = -1489
361674 meter/sec
ZDOT = -19580
978396 ZDOT = -5945
959606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15450947
85 X = 4709448
91
Y = -15753967
25 feet Y = -4801809
22 meter
Z = 2835396
83 Z = 864228
96
XDOT = 11849
017259 XDOT = 3611
580461
YDOT = 8107
663362 feet/sec YDOT = 2471
215793 meter/sec
ZDOT = -19487
885744 ZDOT = -5939
907575
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 13027
53387531
00016717 00000-0 10270-3 0 9027
2 25544 51
6472 87
0414 0013247 206
6837 153
3634 15
52135549 12862
Satellite: ISS
Catalog Number: 25544
Epoch time: 13027
53387531 = yrday
fracday
Element set: 902
Inclination: 51
6472 deg
RA of node: 87
0414 deg
Eccentricity:
0013247
Arg of perigee: 206
6837 deg
Mean anomaly: 153
3634 deg
Mean motion: 15
52135549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1286
Checksum: 303
Coasting Arc #4 (Orbit 1301)
---------------------------------------
Vector Time (GMT): 2013/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 869069
61 A = 6795214
64 meter
Y = 6738903
46 meter E =
0003793
Z = 179223
46 I = 52
01587
XDOT = -4695
865261 Wp = 138
11989
YDOT = 443
154474 meter/sec RA = 81
47137 deg
ZDOT = 6031
532312 TA = 223
79723
MA = 223
82732
Ha = 226
260 n
mi
Hp = 217
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2851278
26 X = 792778
58
Y = 22109263
32 feet Y = 6748195
38 meter
Z = 588003
49 Z = 183259
80
XDOT = -15406
382090 XDOT = -4729
770577
YDOT = 1453
918877 feet/sec YDOT = 390
452899 meter/sec
ZDOT = 19788
491838 ZDOT = 6008
638389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15915185
52 X = -4850948
55
Y = 15608880
48 feet Y = 4757586
77 meter
Z = 603970
56 Z = 184090
23
XDOT = -9389
941468 XDOT = -2862
054160
YDOT = -10345
639473 feet/sec YDOT = -3153
350911 meter/sec
ZDOT = 19693
153280 ZDOT = 6002
473120
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 13028
56403428
00016717 00000-0 10270-3 0 9036
2 25544 51
6464 81
9213 0013052 210
6369 149
4022 15
52098464 13022
Satellite: ISS
Catalog Number: 25544
Epoch time: 13028
56403428 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 81
9213 deg
Eccentricity:
0013052
Arg of perigee: 210
6369 deg
Mean anomaly: 149
4022 deg
Mean motion: 15
52098464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1302
Checksum: 282
Coasting Arc #5 (Orbit 1316)
---------------------------------------
Vector Time (GMT): 2013/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -597156
64 A = 6794405
17 meter
Y = -6641730
27 meter E =
0018117
Z = -1236647
59 I = 52
00890
XDOT = 4881
863288 Wp = 185
29497
YDOT = 654
554393 meter/sec RA = 76
53437 deg
ZDOT = -5883
521483 TA = 8
08222
MA = 8
05307
Ha = 226
033 n
mi
Hp = 217
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1959175
34 X = -516835
86
Y = -21790453
65 feet Y = -6647959
00 meter
Z = -4057242
76 Z = -1239353
14
XDOT = 16016
611836 XDOT = 4902
761047
YDOT = 2147
488165 feet/sec YDOT = 709
263087 meter/sec
ZDOT = -19302
892006 ZDOT = -5859
755596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15957115
72 X = 4863728
87
Y = -14964889
15 feet Y = -4561298
21 meter
Z = -4067678
40 Z = -1239828
38
XDOT = 7173
366165 XDOT = 2186
442007
YDOT = 12859
416640 feet/sec YDOT = 3919
550192 meter/sec
ZDOT = -19204
059296 ZDOT = -5853
397273
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 13029
52979425
00016717 00000-0 10270-3 0 9049
2 25544 51
6471 77
1211 0013091 213
7956 146
2363 15
52162424 13171
Satellite: ISS
Catalog Number: 25544
Epoch time: 13029
52979425 = yrday
fracday
Element set: 904
Inclination: 51
6471 deg
RA of node: 77
1211 deg
Eccentricity:
0013091
Arg of perigee: 213
7956 deg
Mean anomaly: 146
2363 deg
Mean motion: 15
52162424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1317
Checksum: 294
Coasting Arc #6 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2013/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 287884
12 A = 6792969
11 meter
Y = 6408802
37 meter E =
0007955
Z = 2239909
49 I = 51
99494
XDOT = -5075
384031 Wp = 137
51758
YDOT = -1692
834556 meter/sec RA = 71
59479 deg
ZDOT = 5478
787728 TA = 247
21260
MA = 247
29666
Ha = 225
788 n
mi
Hp = 218
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 944501
70 X = 205317
46
Y = 21026254
48 feet Y = 6411560
11 meter
Z = 7348784
43 Z = 2241107
14
XDOT = -16651
522412 XDOT = -5082
691178
YDOT = -5553
919147 feet/sec YDOT = -1749
631289 meter/sec
ZDOT = 17975
025355 ZDOT = 5454
114742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15756614
86 X = -4802616
21
Y = 13952170
26 feet Y = 4252621
50 meter
Z = 7352967
20 Z = 2241184
40
XDOT = -5237
713056 XDOT = -1596
454940
YDOT = -15363
617725 feet/sec YDOT = -4682
830682 meter/sec
ZDOT = 17872
548202 ZDOT = 5447
552692
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 13030
55992940
00016717 00000-0 10270-3 0 9052
2 25544 51
6461 72
0007 0012873 217
4206 142
6050 15
52148064 13338
Satellite: ISS
Catalog Number: 25544
Epoch time: 13030
55992940 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 72
0007 deg
Eccentricity:
0012873
Arg of perigee: 217
4206 deg
Mean anomaly: 142
6050 deg
Mean motion: 15
52148064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 274
Coasting Arc #7 (Orbit 1347)
---------------------------------------
Vector Time (GMT): 2013/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 110483
88 A = 6790690
97 meter
Y = -5996366
57 meter E =
0011437
Z = -3169136
75 I = 51
97849
XDOT = 5295
133742 Wp = 200
55025
YDOT = 2666
602273 meter/sec RA = 66
65167 deg
ZDOT = -4866
027329 TA = 15
82439
MA = 15
78868
Ha = 225
558 n
mi
Hp = 218
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 362479
93 X = 192922
90
Y = -19673118
66 feet Y = -5994670
28 meter
Z = -10397430
29 Z = -3168399
51
XDOT = 17372
486030 XDOT = 5288
559195
YDOT = 8748
695123 feet/sec YDOT = 2725
778786 meter/sec
ZDOT = -15964
656592 ZDOT = -4840
320511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15332061
71 X = 4673212
41
Y = -12335737
17 feet Y = -3759932
69 meter
Z = -10393604
71 Z = -3167970
71
XDOT = 3649
476938 XDOT = 1112
360571
YDOT = 17883
110929 feet/sec YDOT = 5450
772211 meter/sec
ZDOT = -15858
003027 ZDOT = -4833
519323
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 13031
52566814
00016717 00000-0 10270-3 0 9068
2 25544 51
6473 67
2004 0012940 221
1219 138
8958 15
52199134 13489
Satellite: ISS
Catalog Number: 25544
Epoch time: 13031
52566814 = yrday
fracday
Element set: 906
Inclination: 51
6473 deg
RA of node: 67
2004 deg
Eccentricity:
0012940
Arg of perigee: 221
1219 deg
Mean anomaly: 138
8958 deg
Mean motion: 15
52199134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1348
Checksum: 301
Coasting Arc #8 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2013/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -569041
53 A = 6788328
23 meter
Y = 5486382
58 meter E =
0011222
Z = 3963878
99 I = 51
95643
XDOT = -5479
849806 Wp = 170
07916
YDOT = -3500
325711 meter/sec RA = 61
70350 deg
ZDOT = 4045
651653 TA = 237
73835
MA = 237
84714
Ha = 225
290 n
mi
Hp = 218
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1866934
14 X = -649604
37
Y = 17999942
85 feet Y = 5479568
92 meter
Z = 13004852
34 Z = 3960918
76
XDOT = -17978
509863 XDOT = -5459
953619
YDOT = -11484
008238 feet/sec YDOT = -3561
493414 meter/sec
ZDOT = 13273
135345 ZDOT = 4019
079799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14854334
17 X = -4527601
06
Y = 10352325
26 feet Y = 3155388
74 meter
Z = 12991831
59 Z = 3959910
27
XDOT = -2444
302286 XDOT = -745
023337
YDOT = -20077
761000 feet/sec YDOT = -6119
701553 meter/sec
ZDOT = 13162
993626 ZDOT = 4012
080457
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 13032
55577986
00016717 00000-0 10270-3 0 9075
2 25544 51
6461 62
0798 0012777 224
6913 135
3209 15
52197690 13640
Satellite: ISS
Catalog Number: 25544
Epoch time: 13032
55577986 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 62
0798 deg
Eccentricity:
0012777
Arg of perigee: 224
6913 deg
Mean anomaly: 135
3209 deg
Mean motion: 15
52197690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 329
Coasting Arc #9 (Orbit 1378)
---------------------------------------
Vector Time (GMT): 2013/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1136807
79 A = 6785892
46 meter
Y = -4847621
98 meter E =
0005040
Z = -4607892
36 I = 51
93451
XDOT = 5625
685740 Wp = 180
58592
YDOT = 4218
052512 meter/sec RA = 56
75076 deg
ZDOT = -3054
470236 TA = 59
03618
MA = 58
98667
Ha = 225
083 n
mi
Hp = 218
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3729684
34 X = 1213314
14
Y = -15904271
58 feet Y = -4834481
84 meter
Z = -15117757
08 Z = -4602183
93
XDOT = 18456
974211 XDOT = 5592
938133
YDOT = 13838
754961 feet/sec YDOT = 4280
779271 meter/sec
ZDOT = -10021
227807 ZDOT = -3027
221057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14373468
85 X = 4381033
31
Y = -7810023
75 feet Y = -2380495
24 meter
Z = -15093372
76 Z = -4600460
02
XDOT = 1550
955011 XDOT = 472
731087
YDOT = 21971
946307 feet/sec YDOT = 6697
049234 meter/sec
ZDOT = -9908
367027 ZDOT = -3020
070270
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 13033
52149767
00016717 00000-0 10270-3 0 9086
2 25544 51
6474 57
2799 0012848 228
5592 131
4457 15
52229062 13793
Satellite: ISS
Catalog Number: 25544
Epoch time: 13033
52149767 = yrday
fracday
Element set: 908
Inclination: 51
6474 deg
RA of node: 57
2799 deg
Eccentricity:
0012848
Arg of perigee: 228
5592 deg
Mean anomaly: 131
4457 deg
Mean motion: 15
52229062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1379
Checksum: 333
Coasting Arc #10 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2013/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1760772
66 A = 6784073
39 meter
Y = 4173271
03 meter E =
0012218
Z = 5058250
51 I = 51
90978
XDOT = -5679
543620 Wp = 205
65909
YDOT = -4757
791890 meter/sec RA = 51
79267 deg
ZDOT = 1939
365718 TA = 225
52249
MA = 225
62245
Ha = 224
770 n
mi
Hp = 219
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5776813
21 X = -1831879
61
Y = 13691834
08 feet Y = 4153183
43 meter
Z = 16595310
08 Z = 5049524
15
XDOT = -18633
673295 XDOT = -5635
339703
YDOT = -15609
553444 feet/sec YDOT = -4821
056933 meter/sec
ZDOT = 6362
748418 ZDOT = 1911
882649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14022262
72 X = -4273985
68
Y = 5043433
63 feet Y = 1537238
57 meter
Z = 16558445
98 Z = 5047014
33
XDOT = -958
645493 XDOT = -292
195146
YDOT = -23278
657684 feet/sec YDOT = -7095
334862 meter/sec
ZDOT = 6248
992398 ZDOT = 1904
692883
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 13034
55158619
00016717 00000-0 10270-3 0 9097
2 25544 51
6463 52
1591 0012721 232
3629 127
6369 15
52237799 13952
Satellite: ISS
Catalog Number: 25544
Epoch time: 13034
55158619 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 52
1591 deg
Eccentricity:
0012721
Arg of perigee: 232
3629 deg
Mean anomaly: 127
6369 deg
Mean motion: 15
52237799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 323
Coasting Arc #11 (Orbit 1409)
---------------------------------------
Vector Time (GMT): 2013/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2476646
32 A = 6782980
05 meter
Y = -3437034
79 meter E =
0006962
Z = -5300143
74 I = 51
88712
XDOT = 5619
918080 Wp = 145
48417
YDOT = 5159
162332 meter/sec RA = 46
83123 deg
ZDOT = -725
593996 TA = 117
63941
MA = 117
56871
Ha = 224
569 n
mi
Hp = 219
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8125480
07 X = 2540642
31
Y = -11276360
87 feet Y = -3408981
51 meter
Z = -17388923
02 Z = -5287957
12
XDOT = 18438
051443 XDOT = 5565
334252
YDOT = 16926
385604 feet/sec YDOT = 5221
702593 meter/sec
ZDOT = -2380
557731 ZDOT = -698
425756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13831023
97 X = 4215696
11
Y = -1913017
03 feet Y = -583087
59 meter
Z = -17337748
59 Z = -5284545
77
XDOT = 504
405819 XDOT = 153
742894
YDOT = 24022
848235 feet/sec YDOT = 7322
164142 meter/sec
ZDOT = -2268
171727 ZDOT = -691
338742
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 13035
51728266
00016717 00000-0 10270-3 0 9107
2 25544 51
6469 47
3593 0012804 236
3054 123
6877 15
52249234 14109
Satellite: ISS
Catalog Number: 25544
Epoch time: 13035
51728266 = yrday
fracday
Element set: 910
Inclination: 51
6469 deg
RA of node: 47
3593 deg
Eccentricity:
0012804
Arg of perigee: 236
3054 deg
Mean anomaly: 123
6877 deg
Mean motion: 15
52249234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 300
Coasting Arc #12 (Orbit 1425)
---------------------------------------
Vector Time (GMT): 2013/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3212637
85 A = 6782844
64 meter
Y = 2729907
42 meter E =
0009934
Z = 5320375
85 I = 51
86423
XDOT = -5416
598207 Wp = 237
67042
YDOT = -5391
980587 meter/sec RA = 41
86666 deg
ZDOT = -509
960362 TA = 217
15067
MA = 217
21946
Ha = 224
220 n
mi
Hp = 219
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10540150
44 X = -3268770
07
Y = 8956389
16 feet Y = 2693667
73 meter
Z = 17455301
35 Z = 5304633
08
XDOT = -17770
991492 XDOT = -5353
424149
YDOT = -17690
225023 feet/sec YDOT = -5452
199151 meter/sec
ZDOT = -1673
098299 ZDOT = -536
120002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13862661
49 X = -4225339
22
Y = -1197522
42 feet Y = -365004
83 meter
Z = 17389415
75 Z = 5300293
92
XDOT = -132
051899 XDOT = -40
249419
YDOT = -24056
559853 feet/sec YDOT = -7332
439443 meter/sec
ZDOT = -1781
250834 ZDOT = -542
925254
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 13036
54734766
00016717 00000-0 10270-3 0 9114
2 25544 51
6459 42
2385 0012718 240
2820 119
7067 15
52276822 14267
Satellite: ISS
Catalog Number: 25544
Epoch time: 13036
54734766 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 42
2385 deg
Eccentricity:
0012718
Arg of perigee: 240
2820 deg
Mean anomaly: 119
7067 deg
Mean motion: 15
52276822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 305
Coasting Arc #13 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2013/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3985148
09 A = 6783798
97 meter
Y = -2024748
25 meter E =
0008711
Z = -5106338
93 I = 51
84385
XDOT = 5041
199523 Wp = 170
34105
YDOT = 5500
156444 meter/sec RA = 36
90129 deg
ZDOT = 1745
468953 TA = 116
54342
MA = 116
45409
Ha = 223
950 n
mi
Hp = 219
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13074632
85 X = 4032297
81
Y = -6642874
83 feet Y = -1979920
08 meter
Z = -16753080
48 Z = -5086865
33
XDOT = 16539
368514 XDOT = 4970
842082
YDOT = 18045
132691 feet/sec YDOT = 5556
136873 meter/sec
ZDOT = 5726
604176 ZDOT = 1769
787405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14092575
22 X = 4295416
93
Y = 4380789
61 feet Y = 1335264
67 meter
Z = -16671758
20 Z = -5081551
90
XDOT = -355
000215 XDOT = -108
204066
YDOT = 23417
430586 feet/sec YDOT = 7137
632843 meter/sec
ZDOT = 5827
076879 ZDOT = 1776
093033
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 13037
51302233
00016717 00000-0 10270-3 0 9123
2 25544 51
6458 37
4381 0012728 244
2084 115
7755 15
52275812 14410
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
51302233 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 37
4381 deg
Eccentricity:
0012728
Arg of perigee: 244
2084 deg
Mean anomaly: 115
7755 deg
Mean motion: 15
52275812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 287
Coasting Arc #14 (Orbit 1444)
---------------------------------------
Vector Time (GMT): 2013/037/17:02:51
415
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4113639
62 A = 6793421
52 meter
Y = 4990057
50 meter E =
0001779
Z = 2077835
74 I = 51
87076
XDOT = -4968
821497 Wp = 73
26765
YDOT = 1783
083581 meter/sec RA = 35
89162 deg
ZDOT = 5551
508208 TA = 309
61670
MA = 309
63240
Ha = 223
702 n
mi
Hp = 219
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13496192
97 X = 4047440
64
Y = 16371579
74 feet Y = 5035688
62 meter
Z = 6817046
39 Z = 2097658
34
XDOT = -16301
907798 XDOT = -5015
358203
YDOT = 5850
011748 feet/sec YDOT = 1727
258789 meter/sec
ZDOT = 18213
609607 ZDOT = 5527
257609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20073205
49 X = 6118313
03
Y = 6791163
62 feet Y = 2069946
67 meter
Z = 6898875
81 Z = 2102777
35
XDOT = -10348
460141 XDOT = -3154
210651
YDOT = 12176
790172 feet/sec YDOT = 3711
485644 meter/sec
ZDOT = 18112
437147 ZDOT = 5520
670842
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 13037
77054424
00016717 00000-0 10270-3 0 9138
2 25544 51
6474 36
1582 0012125 249
3169 110
6683 15
52079483 14452
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
77054424 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 36
1582 deg
Eccentricity:
0012125
Arg of perigee: 249
3169 deg
Mean anomaly: 110
6683 deg
Mean motion: 15
52079483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1445
Checksum: 304
Coasting Arc #15 (Orbit 1459)
---------------------------------------
Vector Time (GMT): 2013/038/17:02:51
415
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3611769
83 A = 6791366
87 meter
Y = -4904882
65 meter E =
0008937
Z = -2990452
12 I = 51
83966
XDOT = 5704
486227 Wp = 234
76075
YDOT = -1153
775158 meter/sec RA = 30
94090 deg
ZDOT = -4991
806947 TA = 339
32852
MA = 339
36465
Ha = 223
315 n
mi
Hp = 219
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11849638
55 X = -3542127
51
Y = -16092134
66 feet Y = -4944882
31 meter
Z = -9811194
62 Z = -3007828
22
XDOT = 18715
505994 XDOT = 5741
212259
YDOT = -3785
351567 feet/sec YDOT = -1089
778627 meter/sec
ZDOT = -16377
319381 ZDOT = -4964
006564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18637226
48 X = -5680626
63
Y = -7114301
05 feet Y = -2168438
96 meter
Z = -9882852
90 Z = -3012293
56
XDOT = 13227
040423 XDOT = 4031
601921
YDOT = -12036
214435 feet/sec YDOT = -3668
638160 meter/sec
ZDOT = -16261
455127 ZDOT = -4956
491523
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 13038
73633892
00016717 00000-0 10270-3 0 9148
2 25544 51
6482 31
3586 0012123 252
9857 106
9966 15
52108647 14608
Satellite: ISS
Catalog Number: 25544
Epoch time: 13038
73633892 = yrday
fracday
Element set: 914
Inclination: 51
6482 deg
RA of node: 31
3586 deg
Eccentricity:
0012123
Arg of perigee: 252
9857 deg
Mean anomaly: 106
9966 deg
Mean motion: 15
52108647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1460
Checksum: 320
Coasting Arc #16 (Orbit 1475)
---------------------------------------
Vector Time (GMT): 2013/039/17:02:51
415
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2977966
41 A = 6789031
65 meter
Y = 4776814
78 meter E =
0004290
Z = 3799317
65 I = 51
80490
XDOT = -6359
844472 Wp = 184
96892
YDOT = 599
903761 meter/sec RA = 25
98410 deg
ZDOT = 4226
890673 TA = 220
41601
MA = 220
44789
Ha = 223
011 n
mi
Hp = 219
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9770231
00 X = 2905874
19
Y = 15671964
49 feet Y = 4809713
22 meter
Z = 12464952
91 Z = 3813608
77
XDOT = -20865
631471 XDOT = -6386
612560
YDOT = 1968
188193 feet/sec YDOT = 528
634373 meter/sec
ZDOT = 13867
751553 ZDOT = 4195
930970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16782661
58 X = 5115355
25
Y = 7611827
10 feet Y = 2320084
90 meter
Z = 12523789
14 Z = 3817250
93
XDOT = -15743
515498 XDOT = -4798
623524
YDOT = 12086
494741 feet/sec YDOT = 3683
963597 meter/sec
ZDOT = 13738
812468 ZDOT = 4187
590040
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 13039
76650870
00016717 00000-0 10270-3 0 9158
2 25544 51
6479 26
2382 0012070 256
7933 103
1872 15
52115280 14762
Satellite: ISS
Catalog Number: 25544
Epoch time: 13039
76650870 = yrday
fracday
Element set: 915
Inclination: 51
6479 deg
RA of node: 26
2382 deg
Eccentricity:
0012070
Arg of perigee: 256
7933 deg
Mean anomaly: 103
1872 deg
Mean motion: 15
52115280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1476
Checksum: 304
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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