[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 31st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 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
There are no maneuvers
Coasting Arc #1 (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 = 265449
93 A = 6792851
58 meter
Y = 6401257
75 meter E =
0007999
Z = 2263740
75 I = 51
99530
XDOT = -5076
833950 Wp = 137
55375
YDOT = -1728
606012 meter/sec RA = 71
59762 deg
ZDOT = 5466
369142 TA = 247
45788
MA = 247
54256
Ha = 225
732 n
mi
Hp = 218
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 870898
71 X = 182853
53
Y = 21001501
80 feet Y = 6403764
46 meter
Z = 7426970
97 Z = 2264829
35
XDOT = -16656
279365 XDOT = -5083
680660
YDOT = -5671
279567 feet/sec YDOT = -1785
416385 meter/sec
ZDOT = 17934
281963 ZDOT = 5441
690232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15784100
94 X = -4810993
97
Y = 13879059
16 feet Y = 4230337
23 meter
Z = 7430700
81 Z = 2264877
61
XDOT = -5154
773602 XDOT = -1571
174994
YDOT = -15439
090616 feet/sec YDOT = -4705
834820 meter/sec
ZDOT = 17831
784629 ZDOT = 5435
127955
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
55987805
00016717 00000-0 10270-3 0 9001
2 25544 51
6465 72
0038 0012831 217
5008 142
5250 15
52172943 13335
Satellite: ISS
Catalog Number: 25544
Epoch time: 13030
55987805 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 72
0038 deg
Eccentricity:
0012831
Arg of perigee: 217
5008 deg
Mean anomaly: 142
5250 deg
Mean motion: 15
52172943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 280
Coasting Arc #2 (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 = 141174
75 A = 6790541
77 meter
Y = -5980864
15 meter E =
0011275
Z = -3197025
93 I = 51
97874
XDOT = 5294
042493 Wp = 200
55972
YDOT = 2710
829109 meter/sec RA = 66
65430 deg
ZDOT = -4842
641711 TA = 16
18725
MA = 16
15126
Ha = 225
502 n
mi
Hp = 218
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 463171
75 X = 223573
62
Y = -19622257
70 feet Y = -5978824
88 meter
Z = -10488930
21 Z = -3196139
69
XDOT = 17368
905817 XDOT = 5286
859874
YDOT = 8893
796288 feet/sec YDOT = 2769
990019 meter/sec
ZDOT = -15887
932122 ZDOT = -4816
941673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15358306
71 X = 4681211
89
Y = -12225511
86 feet Y = -3726336
02 meter
Z = -10484486
48 Z = -3195671
48
XDOT = 3543
847758 XDOT = 1080
164797
YDOT = 17971
486531 feet/sec YDOT = 5477
709095 meter/sec
ZDOT = -15781
312357 ZDOT = -4810
144006
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
52560122
00016717 00000-0 10270-3 0 9019
2 25544 51
6477 67
2035 0012896 221
2022 138
8157 15
52224663 13487
Satellite: ISS
Catalog Number: 25544
Epoch time: 13031
52560122 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 67
2035 deg
Eccentricity:
0012896
Arg of perigee: 221
2022 deg
Mean anomaly: 138
8157 deg
Mean motion: 15
52224663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1348
Checksum: 280
Coasting Arc #3 (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 = -608638
24 A = 6788154
59 meter
Y = 5460912
56 meter E =
0011256
Z = 3992792
01 I = 51
95660
XDOT = -5474
324214 Wp = 170
57460
YDOT = -3550
626028 meter/sec RA = 61
70585 deg
ZDOT = 4009
287453 TA = 237
70751
MA = 237
81660
Ha = 225
232 n
mi
Hp = 218
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1996844
61 X = -689053
78
Y = 17916379
79 feet Y = 5453656
93 meter
Z = 13099711
32 Z = 3989639
78
XDOT = -17960
381279 XDOT = -5453
689322
YDOT = -11649
035526 feet/sec YDOT = -3611
727812 meter/sec
ZDOT = 13153
830225 ZDOT = 3982
744237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14877008
72 X = -4534512
26
Y = 10199042
10 feet Y = 3108668
03 meter
Z = 13085894
77 Z = 3988580
73
XDOT = -2318
627256 XDOT = -706
717588
YDOT = -20170
256203 feet/sec YDOT = -6147
894091 meter/sec
ZDOT = 13043
814117 ZDOT = 3975
754543
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
55569579
00016717 00000-0 10270-3 0 9029
2 25544 51
6465 62
0828 0012734 224
7675 135
2449 15
52224179 13645
Satellite: ISS
Catalog Number: 25544
Epoch time: 13032
55569579 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 62
0828 deg
Eccentricity:
0012734
Arg of perigee: 224
7675 deg
Mean anomaly: 135
2449 deg
Mean motion: 15
52224179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 318
Coasting Arc #4 (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 = 1185664
79 A = 6785713
32 meter
Y = -4810743
75 meter E =
0004972
Z = -4634121
04 I = 51
93466
XDOT = 5612
653374 Wp = 178
55196
YDOT = 4271
651552 meter/sec RA = 56
75276 deg
ZDOT = -3003
340422 TA = 61
63134
MA = 61
58122
Ha = 225
026 n
mi
Hp = 218
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3889976
35 X = 1261882
54
Y = -15783280
03 feet Y = -4797058
88 meter
Z = -15203809
20 Z = -4628175
98
XDOT = 18414
217105 XDOT = 5579
059007
YDOT = 14014
604831 feet/sec YDOT = 4334
227843 meter/sec
ZDOT = -9853
479074 ZDOT = -2976
156610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14391280
81 X = 4386462
39
Y = -7609566
94 feet Y = -2319396
00 meter
Z = -15178444
80 Z = -4626389
97
XDOT = 1405
629009 XDOT = 428
435722
YDOT = 22055
870251 feet/sec YDOT = 6722
629253 meter/sec
ZDOT = -9740
897270 ZDOT = -2969
025488
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
52139705
00016717 00000-0 10270-3 0 9032
2 25544 51
6478 57
2828 0012806 228
6344 131
3707 15
52255775 13797
Satellite: ISS
Catalog Number: 25544
Epoch time: 13033
52139705 = yrday
fracday
Element set: 903
Inclination: 51
6478 deg
RA of node: 57
2828 deg
Eccentricity:
0012806
Arg of perigee: 228
6344 deg
Mean anomaly: 131
3707 deg
Mean motion: 15
52255775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1379
Checksum: 313
Coasting Arc #5 (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 = -1818705
20 A = 6783909
31 meter
Y = 4124301
47 meter E =
0012178
Z = 5077646
20 I = 51
90998
XDOT = -5656
185765 Wp = 206
40304
YDOT = -4811
838612 meter/sec RA = 51
79431 deg
ZDOT = 1873
580601 TA = 225
43824
MA = 225
53773
Ha = 224
711 n
mi
Hp = 218
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5966880
59 X = -1889354
48
Y = 13531172
81 feet Y = 4103568
60 meter
Z = 16658944
22 Z = 5068639
52
XDOT = -18557
039912 XDOT = -5611
059659
YDOT = -15786
872085 feet/sec YDOT = -4874
837297 meter/sec
ZDOT = 6146
917983 ZDOT = 1846
213243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14034733
84 X = -4277786
87
Y = 4794579
38 feet Y = 1461387
79 meter
Z = 16620919
91 Z = 5066056
39
XDOT = -793
949026 XDOT = -241
995663
YDOT = -23341
729722 feet/sec YDOT = -7114
559219 meter/sec
ZDOT = 6033
650601 ZDOT = 1839
056703
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
55146733
00016717 00000-0 10270-3 0 9046
2 25544 51
6467 52
1620 0012678 232
4352 127
5648 15
52265976 13951
Satellite: ISS
Catalog Number: 25544
Epoch time: 13034
55146733 = yrday
fracday
Element set: 904
Inclination: 51
6467 deg
RA of node: 52
1620 deg
Eccentricity:
0012678
Arg of perigee: 232
4352 deg
Mean anomaly: 127
5648 deg
Mean motion: 15
52265976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 311
Coasting Arc #6 (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 = 2542609
60 A = 6782863
51 meter
Y = -3375891
20 meter E =
0007107
Z = -5308194
60 I = 51
88748
XDOT = 5582
138874 Wp = 145
36281
YDOT = 5210
414628 meter/sec RA = 46
83252 deg
ZDOT = -645
996452 TA = 118
52252
MA = 118
45095
Ha = 224
509 n
mi
Hp = 219
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8341895
02 X = 2605956
07
Y = -11075758
51 feet Y = -3347103
91 meter
Z = -17415336
63 Z = -5295689
12
XDOT = 18314
103918 XDOT = 5526
598081
YDOT = 17094
536180 feet/sec YDOT = 5272
527066 meter/sec
ZDOT = -2119
410932 ZDOT = -619
014062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13837186
58 X = 4217574
47
Y = -1617878
59 feet Y = -493129
40 meter
Z = -17362843
25 Z = -5292194
62
XDOT = 317
741765 XDOT = 96
847690
YDOT = 24048
916065 feet/sec YDOT = 7330
109617 meter/sec
ZDOT = -2007
805199 ZDOT = -611
979025
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
51714623
00016717 00000-0 10270-3 0 9053
2 25544 51
6473 47
3621 0012760 236
3836 123
6099 15
52277516 14105
Satellite: ISS
Catalog Number: 25544
Epoch time: 13035
51714623 = yrday
fracday
Element set: 905
Inclination: 51
6473 deg
RA of node: 47
3621 deg
Eccentricity:
0012760
Arg of perigee: 236
3836 deg
Mean anomaly: 123
6099 deg
Mean motion: 15
52277516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 292
Coasting Arc #7 (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 = -3284840
58 A = 6782792
10 meter
Y = 2657176
12 meter E =
0009740
Z = 5312890
89 I = 51
86480
XDOT = -5361
148737 Wp = 238
40392
YDOT = -5438
084602 meter/sec RA = 41
86768 deg
ZDOT = -600
666148 TA = 217
28388
MA = 217
35154
Ha = 224
161 n
mi
Hp = 219
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10777036
02 X = -3340117
77
Y = 8717769
43 feet Y = 2620133
80 meter
Z = 17430744
38 Z = 5296799
44
XDOT = -17589
070659 XDOT = -5297
022638
YDOT = -17841
484914 feet/sec YDOT = -5497
677770 meter/sec
ZDOT = -1970
689463 ZDOT = -626
554112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13861259
88 X = -4224912
01
Y = -1533646
38 feet Y = -467455
42 meter
Z = 17363417
35 Z = 5292369
61
XDOT = 80
336056 XDOT = 24
486430
YDOT = -24033
657859 feet/sec YDOT = -7325
458915 meter/sec
ZDOT = -2077
705134 ZDOT = -633
284525
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
54719189
00016717 00000-0 10270-3 0 9060
2 25544 51
6462 42
2411 0012673 240
3519 119
6371 15
52306719 14263
Satellite: ISS
Catalog Number: 25544
Epoch time: 13036
54719189 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 42
2411 deg
Eccentricity:
0012673
Arg of perigee: 240
3519 deg
Mean anomaly: 119
6371 deg
Mean motion: 15
52306719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 297
Coasting Arc #8 (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 = 4060418
85 A = 6783828
46 meter
Y = -1941496
14 meter E =
0008752
Z = -5079324
46 I = 51
84470
XDOT = 4963
998404 Wp = 171
57823
YDOT = 5538
339679 meter/sec RA = 36
90219 deg
ZDOT = 1843
242109 TA = 116
28032
MA = 116
19037
Ha = 223
886 n
mi
Hp = 219
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13321584
17 X = 4106500
81
Y = -6369737
99 feet Y = -1895832
22 meter
Z = -16664450
31 Z = -5059487
79
XDOT = 16286
084002 XDOT = 4892
744781
YDOT = 18170
405772 feet/sec YDOT = 5593
451784 meter/sec
ZDOT = 6047
382248 ZDOT = 1867
183356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14079917
56 X = 4291558
87
Y = 4748431
23 feet Y = 1447321
84 meter
Z = -16581628
19 Z = -5054080
27
XDOT = -598
806104 XDOT = -182
516100
YDOT = 23331
049124 feet/sec YDOT = 7111
303773 meter/sec
ZDOT = 6146
279874 ZDOT = 1873
386106
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
51284795
00016717 00000-0 10270-3 0 9079
2 25544 51
6461 37
4407 0012682 244
2795 115
7048 15
52306105 14416
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
51284795 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 37
4407 deg
Eccentricity:
0012682
Arg of perigee: 244
2795 deg
Mean anomaly: 115
7048 deg
Mean motion: 15
52306105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 299
Coasting Arc #9 (Orbit 1456)
---------------------------------------
Vector Time (GMT): 2013/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4789624
15 A = 6785554
17 meter
Y = 1303299
80 meter E =
0004217
Z = 4629370
62 I = 51
82507
XDOT = -4394
032424 Wp = 252
69107
YDOT = -5515
448858 meter/sec RA = 31
93719 deg
ZDOT = -2996
856343 TA = 227
12808
MA = 227
16351
Ha = 223
546 n
mi
Hp = 219
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15713990
01 X = -4826329
64
Y = 4275917
97 feet Y = 1249533
93 meter
Z = 15188223
82 Z = 4606014
48
XDOT = -14416
116876 XDOT = -4317
473366
YDOT = -18095
304653 feet/sec YDOT = -5564
157587 meter/sec
ZDOT = -9832
205849 ZDOT = -3018
015751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14472288
93 X = -4411153
66
Y = -7662544
37 feet Y = -2335543
52 meter
Z = 15090837
17 Z = 4599687
17
XDOT = 1299
845344 XDOT = 396
192861
YDOT = -21968
245264 feet/sec YDOT = -6695
921156 meter/sec
ZDOT = -9919
527990 ZDOT = -3023
472131
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
54286842
00016717 00000-0 10270-3 0 9089
2 25544 51
6454 32
3195 0012687 248
4077 111
5724 15
52350289 14574
Satellite: ISS
Catalog Number: 25544
Epoch time: 13038
54286842 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 32
3195 deg
Eccentricity:
0012687
Arg of perigee: 248
4077 deg
Mean anomaly: 111
5724 deg
Mean motion: 15
52350289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1457
Checksum: 317
Coasting Arc #10 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2013/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5468701
34 A = 6788010
57 meter
Y = -710346
42 meter E =
0008042
Z = -3957614
93 I = 51
80659
XDOT = 3630
376740 Wp = 224
44978
YDOT = 5409
664250 meter/sec RA = 26
97403 deg
ZDOT = 4034
985143 TA = 87
65999
MA = 87
56792
Ha = 223
163 n
mi
Hp = 219
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17941933
52 X = 5495462
63
Y = -2330532
86 feet Y = -649042
36 meter
Z = -12984300
96 Z = -3930984
21
XDOT = 11910
684844 XDOT = 3550
014589
YDOT = 17748
242290 feet/sec YDOT = 5449
812103 meter/sec
ZDOT = 13238
140232 ZDOT = 4052
425464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14942935
46 X = 4554606
73
Y = 10340289
96 feet Y = 3151720
38 meter
Z = -12873364
62 Z = -3923801
54
XDOT = -2351
819075 XDOT = -716
834454
YDOT = 20012
726581 feet/sec YDOT = 6099
879062 meter/sec
ZDOT = 13309
998077 ZDOT = 4056
887414
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
50850113
00016717 00000-0 10270-3 0 9095
2 25544 51
6453 27
5184 0012589 252
1496 107
8282 15
52343847 14721
Satellite: ISS
Catalog Number: 25544
Epoch time: 13039
50850113 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 27
5184 deg
Eccentricity:
0012589
Arg of perigee: 252
1496 deg
Mean anomaly: 107
8282 deg
Mean motion: 15
52343847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 310
Coasting Arc #11 (Orbit 1487)
---------------------------------------
Vector Time (GMT): 2013/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6025949
81 A = 6790354
84 meter
Y = 210816
81 meter E =
0004321
Z = 3117187
62 I = 51
78714
XDOT = -2709
936428 Wp = 171
09164
YDOT = -5245
778615 meter/sec RA = 22
01343 deg
ZDOT = -4887
160011 TA = 333
14195
MA = 333
16431
Ha = 222
831 n
mi
Hp = 219
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19770176
55 X = -6043001
36
Y = 691656
21 feet Y = 143335
62 meter
Z = 10226993
51 Z = 3087873
53
XDOT = -8890
867547 XDOT = -2627
335802
YDOT = -17210
559760 feet/sec YDOT = -5275
621134 meter/sec
ZDOT = -16033
989537 ZDOT = -4900
123461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15407312
80 X = -4696148
94
Y = -12507366
03 feet Y = -3812245
17 meter
Z = 10104957
83 Z = 3079991
15
XDOT = 3766
897654 XDOT = 1148
150405
YDOT = -17628
759476 feet/sec YDOT = -5373
245888 meter/sec
ZDOT = -16087
237186 ZDOT = -4903
389894
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 13040
53849598
00016717 00000-0 10270-3 0 9107
2 25544 51
6452 22
3970 0012669 256
4906 103
4834 15
52395912 14880
Satellite: ISS
Catalog Number: 25544
Epoch time: 13040
53849598 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 22
3970 deg
Eccentricity:
0012669
Arg of perigee: 256
4906 deg
Mean anomaly: 103
4834 deg
Mean motion: 15
52395912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1488
Checksum: 321
Coasting Arc #12 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2013/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6446970
86 A = 6792536
15 meter
Y = 235872
27 meter E =
0008489
Z = -2113709
27 I = 51
76588
XDOT = 1631
922844 Wp = 287
93629
YDOT = 5054
676861 meter/sec RA = 17
05532 deg
ZDOT = 5525
852629 TA = 48
71135
MA = 48
63829
Ha = 222
430 n
mi
Hp = 219
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21151479
21 X = 6454121
68
Y = 773859
15 feet Y = 308006
21 meter
Z = -6934741
69 Z = -2082373
99
XDOT = 5354
077572 XDOT = 1548
436742
YDOT = 16583
585502 feet/sec YDOT = 5072
459557 meter/sec
ZDOT = 18129
437758 ZDOT = 5533
577081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15717705
33 X = 4790756
58
Y = 14238294
18 feet Y = 4339832
07 meter
Z = -6804358
24 Z = -2073968
39
XDOT = -5629
683363 XDOT = -1715
927489
YDOT = 14918
646271 feet/sec YDOT = 4547
203383 meter/sec
ZDOT = 18160
907124 ZDOT = 5535
444491
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 13041
50410471
00016717 00000-0 10270-3 0 9110
2 25544 51
6453 17
5958 0012526 259
6923 100
2817 15
52400700 15035
Satellite: ISS
Catalog Number: 25544
Epoch time: 13041
50410471 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 17
5958 deg
Eccentricity:
0012526
Arg of perigee: 259
6923 deg
Mean anomaly: 100
2817 deg
Mean motion: 15
52400700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 269
Coasting Arc #13 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2013/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6682974
22 A = 6793860
42 meter
Y = -607366
76 meter E =
0009047
Z = 1023159
18 I = 51
74195
XDOT = -460
170027 Wp = 188
54309
YDOT = -4863
422529 meter/sec RA = 12
09849 deg
ZDOT = -5908
144831 TA = 340
38999
MA = 340
42477
Ha = 222
177 n
mi
Hp = 219
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21925768
42 X = -6680655
93
Y = -1992673
09 feet Y = -682086
93 meter
Z = 3356821
47 Z = 990700
39
XDOT = -1509
744183 XDOT = -377
052550
YDOT = -15956
110659 feet/sec YDOT = -4868
104151 meter/sec
ZDOT = -19383
677268 ZDOT = -5910
177987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15775297
28 X = -4808310
61
Y = -15386299
01 feet Y = -4689743
94 meter
Z = 3221818
73 Z = 982010
35
XDOT = 7862
430294 XDOT = 2396
468754
YDOT = -12110
651194 feet/sec YDOT = -3691
326484 meter/sec
ZDOT = -19391
486884 ZDOT = -5910
525202
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 13042
53407388
00016717 00000-0 10270-3 0 9128
2 25544 51
6462 12
4745 0012633 264
1980 95
7731 15
52430769 15194
Satellite: ISS
Catalog Number: 25544
Epoch time: 13042
53407388 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 12
4745 deg
Eccentricity:
0012633
Arg of perigee: 264
1980 deg
Mean anomaly: 95
7731 deg
Mean motion: 15
52430769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 306
Coasting Arc #14 (Orbit 1534)
---------------------------------------
Vector Time (GMT): 2013/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6720477
38 A = 6794162
31 meter
Y = 951824
38 meter E =
0008530
Z = 137985
30 I = 51
71326
XDOT = -784
397254 Wp = 335
56590
YDOT = 4686
750396 meter/sec RA = 7
14173 deg
ZDOT = 6014
757326 TA = 25
91790
MA = 25
87520
Ha = 221
931 n
mi
Hp = 219
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22048810
31 X = 6708664
12
Y = 3122783
41 feet Y = 1026910
95 meter
Z = 452707
69 Z = 170603
31
XDOT = -2573
481805 XDOT = -865
964647
YDOT = 15376
477676 feet/sec YDOT = 4677
523240 meter/sec
ZDOT = 19733
455794 ZDOT = 6010
748338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15418306
26 X = 4699499
75
Y = 16063513
63 feet Y = 4896158
95 meter
Z = 588318
54 Z = 179319
49
XDOT = -10440
235167 XDOT = -3182
183679
YDOT = 9311
789272 feet/sec YDOT = 2838
233370 meter/sec
ZDOT = 19716
145394 ZDOT = 6009
481116
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 13043
56402886
00016717 00000-0 10270-3 0 9131
2 25544 51
6462 7
3534 0012604 267
3111 92
6598 15
52462794 15350
Satellite: ISS
Catalog Number: 25544
Epoch time: 13043
56402886 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 7
3534 deg
Eccentricity:
0012604
Arg of perigee: 267
3111 deg
Mean anomaly: 92
6598 deg
Mean motion: 15
52462794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1535
Checksum: 305
Coasting Arc #15 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2013/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6544966
50 A = 6793425
45 meter
Y = -1263095
33 meter E =
0009836
Z = -1281726
70 I = 51
68153
XDOT = 2023
420230 Wp = 227
30313
YDOT = -4539
198906 meter/sec RA = 2
18260 deg
ZDOT = -5837
158143 TA = 326
62316
MA = 326
68513
Ha = 221
926 n
mi
Hp = 218
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21472987
21 X = -6524129
69
Y = -4144013
54 feet Y = -1336168
87 meter
Z = -4205140
11 Z = -1313470
29
XDOT = 6638
517816 XDOT = 2102
382987
YDOT = -14892
384862 feet/sec YDOT = -4516
130787 meter/sec
ZDOT = -19150
781309 ZDOT = -5827
136502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14598262
78 X = -4449550
50
Y = -16248872
28 feet Y = -4952656
27 meter
Z = -4337061
78 Z = -1321936
43
XDOT = 13191
447164 XDOT = 4020
753096
YDOT = -6732
451410 feet/sec YDOT = -2052
051190 meter/sec
ZDOT = -19108
472075 ZDOT = -5824
262289
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 13044
52960047
00016717 00000-0 10270-3 0 9147
2 25544 51
6473 2
5526 0012676 271
7228 88
2472 15
52466726 15505
Satellite: ISS
Catalog Number: 25544
Epoch time: 13044
52960047 = yrday
fracday
Element set: 914
Inclination: 51
6473 deg
RA of node: 2
5526 deg
Eccentricity:
0012676
Arg of perigee: 271
7228 deg
Mean anomaly: 88
2472 deg
Mean motion: 15
52466726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 306
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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