[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 11th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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
017/02:17:37
972 -1
0 1
3 1
3
N/A 0
1 -0
1 228
4
000/00:03:15
944 0
9 0
1 215
3
Coasting Arc #1 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2013/011/08:33:36
647
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 637057
72 A = 6783515
05 meter
Y = 4175679
43 meter E =
0026798
Z = -5328692
43 I = 51
70225
XDOT = -7479
552315 Wp = 119
50389
YDOT = 1560
394970 meter/sec RA = 166
33893 deg
ZDOT = 316
902395 TA = 153
59141
MA = 153
45458
Ha = 229
305 n
mi
Hp = 213
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2090084
39 X = 616201
98
Y = 13699735
67 feet Y = 4182687
34 meter
Z = -17482586
70 Z = -5325647
94
XDOT = -24539
213633 XDOT = -7497
984487
YDOT = 5119
406070 feet/sec YDOT = 1476
650841 meter/sec
ZDOT = 1039
706020 ZDOT = 280
523357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12838246
43 X = -3913097
51
Y = -5258978
61 feet Y = -1602936
68 meter
Z = -17470392
68 Z = -5324975
69
XDOT = 8030
823249 XDOT = 2447
794926
YDOT = -22683
144450 feet/sec YDOT = -6913
822428 meter/sec
ZDOT = 888
345893 ZDOT = 270
767828
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 13011
37235860
00016717 00000-0 10270-3 0 9007
2 25544 51
6437 167
3427 0015155 145
3998 214
8143 15
52027369 10356
Satellite: ISS
Catalog Number: 25544
Epoch time: 13011
37235860 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 167
3427 deg
Eccentricity:
0015155
Arg of perigee: 145
3998 deg
Mean anomaly: 214
8143 deg
Mean motion: 15
52027369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1035
Checksum: 297
Coasting Arc #2 (Orbit 1050)
---------------------------------------
Vector Time (GMT): 2013/012/08:33:36
647
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 238135
06 A = 6784071
44 meter
Y = -4378899
66 meter E =
0015432
Z = 5164103
75 I = 51
73456
XDOT = 7425
034314 Wp = 132
89242
YDOT = -1296
846367 meter/sec RA = 161
36756 deg
ZDOT = -1449
582715 TA = 330
98293
MA = 331
06863
Ha = 229
216 n
mi
Hp = 213
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 781283
01 X = 261997
82
Y = -14366468
69 feet Y = -4376103
67 meter
Z = 16942597
61 Z = 5165318
18
XDOT = 24360
348800 XDOT = 7446
025622
YDOT = -4254
745299 feet/sec YDOT = -1213
697499 meter/sec
ZDOT = -4755
848803 ZDOT = -1413
462391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12047047
24 X = 3671940
00
Y = 7854117
23 feet Y = 2393934
93 meter
Z = 16948124
82 Z = 5165788
45
XDOT = -8100
622219 XDOT = -2469
069652
YDOT = 22310
073059 feet/sec YDOT = 6800
110269 meter/sec
ZDOT = -4605
570968 ZDOT = -1403
778031
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 13012
40257981
00016717 00000-0 10270-3 0 9011
2 25544 51
6444 162
2237 0015104 149
3895 210
8141 15
52039370 10518
Satellite: ISS
Catalog Number: 25544
Epoch time: 13012
40257981 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 162
2237 deg
Eccentricity:
0015104
Arg of perigee: 149
3895 deg
Mean anomaly: 210
8141 deg
Mean motion: 15
52039370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1051
Checksum: 273
Coasting Arc #3 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2013/013/08:33:36
647
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1122936
98 A = 6785433
59 meter
Y = 4648600
48 meter E =
0024738
Z = -4836081
61 I = 51
76733
XDOT = -7148
821983 Wp = 133
78555
YDOT = 932
867301 meter/sec RA = 156
39703 deg
ZDOT = 2548
135576 TA = 161
36242
MA = 161
27167
Ha = 229
059 n
mi
Hp = 213
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3684176
43 X = -1151343
27
Y = 15251313
92 feet Y = 4635884
53 meter
Z = -15866409
47 Z = -4841605
37
XDOT = -23454
140363 XDOT = -7171
100081
YDOT = 3060
588259 feet/sec YDOT = 852
799995 meter/sec
ZDOT = 8360
024856 ZDOT = 2513
353906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11522102
30 X = -3511936
78
Y = -10614686
76 feet Y = -3235356
52 meter
Z = -15889879
33 Z = -4843235
22
XDOT = 8104
896323 XDOT = 2470
372399
YDOT = -21137
665637 feet/sec YDOT = -6442
760486 meter/sec
ZDOT = 8215
332940 ZDOT = 2504
033480
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 13013
36839534
00016717 00000-0 10270-3 0 9028
2 25544 51
6436 157
4224 0015131 152
6416 207
5536 15
52076725 10669
Satellite: ISS
Catalog Number: 25544
Epoch time: 13013
36839534 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 157
4224 deg
Eccentricity:
0015131
Arg of perigee: 152
6416 deg
Mean anomaly: 207
5536 deg
Mean motion: 15
52076725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1066
Checksum: 291
Coasting Arc #4 (Orbit 1081)
---------------------------------------
Vector Time (GMT): 2013/014/08:33:36
647
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1903225
21 A = 6787358
73 meter
Y = -4882730
88 meter E =
0018716
Z = 4293324
77 I = 51
80226
XDOT = 6780
180720 Wp = 125
73846
YDOT = -494
759633 meter/sec RA = 151
43349 deg
ZDOT = -3568
123706 TA =
51604
MA =
51412
Ha = 228
876 n
mi
Hp = 214
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6244177
21 X = 1936828
09
Y = -16019458
26 feet Y = -4861260
06 meter
Z = 14085711
20 Z = 4302651
76
XDOT = 22244
687401 XDOT = 6802
541948
YDOT = -1623
227142 feet/sec YDOT = -418
814270 meter/sec
ZDOT = -11706
442605 ZDOT = -3535
132547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11154501
34 X = 3399892
01
Y = 13041509
05 feet Y = 3975051
96 meter
Z = 14125020
12 Z = 4305306
13
XDOT = -8246
295332 XDOT = -2513
470817
YDOT = 19584
259755 feet/sec YDOT = 5969
282373 meter/sec
ZDOT = -11569
227319 ZDOT = -3526
300487
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 13014
39858016
00016717 00000-0 10270-3 0 9039
2 25544 51
6442 152
3031 0015019 156
7459 203
4376 15
52099685 10828
Satellite: ISS
Catalog Number: 25544
Epoch time: 13014
39858016 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 152
3031 deg
Eccentricity:
0015019
Arg of perigee: 156
7459 deg
Mean anomaly: 203
4376 deg
Mean motion: 15
52099685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1082
Checksum: 301
Coasting Arc #5 (Orbit 1096)
---------------------------------------
Vector Time (GMT): 2013/015/08:33:36
647
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2619104
59 A = 6789608
91 meter
Y = 5136909
40 meter E =
0018327
Z = -3608175
32 I = 51
83589
XDOT = -6228
927573 Wp = 145
03837
YDOT = -56
528634 meter/sec RA = 146
47353 deg
ZDOT = 4437
538387 TA = 172
53243
MA = 172
50510
Ha = 228
802 n
mi
Hp = 214
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8592862
82 X = -2658824
69
Y = 16853377
30 feet Y = 5107398
89 meter
Z = -11837845
54 Z = -3620994
90
XDOT = -20436
114086 XDOT = -6249
388508
YDOT = -185
461399 feet/sec YDOT = -126
298862 meter/sec
ZDOT = 14558
852977 ZDOT = 4407
229630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11028435
03 X = -3361467
00
Y = -15328701
96 feet Y = -4672188
36 meter
Z = -11891708
13 Z = -3624592
64
XDOT = 8506
671362 XDOT = 2592
833431
YDOT = -17325
667843 feet/sec YDOT = -5280
863558 meter/sec
ZDOT = 14432
838659 ZDOT = 4399
129223
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 13015
36436237
00016717 00000-0 10270-3 0 9045
2 25544 51
6437 147
5021 0015129 159
7059 200
4697 15
52129812 10973
Satellite: ISS
Catalog Number: 25544
Epoch time: 13015
36436237 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 147
5021 deg
Eccentricity:
0015129
Arg of perigee: 159
7059 deg
Mean anomaly: 200
4697 deg
Mean motion: 15
52129812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1097
Checksum: 302
Coasting Arc #6 (Orbit 1112)
---------------------------------------
Vector Time (GMT): 2013/016/08:33:36
647
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3206618
60 A = 6791802
03 meter
Y = -5300801
92 meter E =
0024189
Z = 2744433
11 I = 51
86854
XDOT = 5626
551465 Wp = 134
43150
YDOT = 717
919623 meter/sec RA = 141
52033 deg
ZDOT = -5175
951748 TA = 14
57686
MA = 14
50722
Ha = 228
543 n
mi
Hp = 214
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10520402
21 X = 3252323
43
Y = -17391082
41 feet Y = -5264687
96 meter
Z = 9004045
65 Z = 2760121
36
XDOT = 18459
814518 XDOT = 5643
248391
YDOT = 2355
379339 feet/sec YDOT = 780
932622 meter/sec
ZDOT = -16981
468991 ZDOT = -5148
578281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10905366
27 X = 3323955
64
Y = 17117594
52 feet Y = 5217442
81 meter
Z = 9069861
76 Z = 2764493
87
XDOT = -9131
388448 XDOT = -2783
247199
YDOT = 14774
809931 feet/sec YDOT = 4503
362067 meter/sec
ZDOT = -16867
722865 ZDOT = -5141
281929
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 13016
39451012
00016717 00000-0 10270-3 0 9058
2 25544 51
6437 142
3822 0014948 163
9054 196
2575 15
52166447 11136
Satellite: ISS
Catalog Number: 25544
Epoch time: 13016
39451012 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 142
3822 deg
Eccentricity:
0014948
Arg of perigee: 163
9054 deg
Mean anomaly: 196
2575 deg
Mean motion: 15
52166447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1113
Checksum: 298
Coasting Arc #7 (Orbit 1123)
---------------------------------------
Vector Time (GMT): 2013/017/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2681019
60 A = 6792024
73 meter
Y = 5522914
95 meter E =
0013727
Z = -2927085
97 I = 51
88823
XDOT = -5755
045035 Wp = 148
44974
YDOT = -122
797853 meter/sec RA = 137
85629 deg
ZDOT = 5038
860235 TA = 178
39016
MA = 178
38574
Ha = 228
425 n
mi
Hp = 215
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8795996
06 X = -2728359
91
Y = 18119799
70 feet Y = 5492669
42 meter
Z = -9603300
44 Z = -2940224
95
XDOT = -18881
381348 XDOT = -5777
721300
YDOT = -402
880095 feet/sec YDOT = -187
281180 meter/sec
ZDOT = 16531
693686 ZDOT = 5010
847980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16489947
62 X = 5026136
03
Y = -11520163
31 feet Y = -3511345
78 meter
Z = -9658547
10 Z = -2943925
16
XDOT = 15514
499698 XDOT = 4728
819508
YDOT = 8442
978047 feet/sec YDOT = 2573
419709 meter/sec
ZDOT = 16415
219768 ZDOT = 5003
358985
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 13017
10272791
00016717 00000-0 10270-3 0 9064
2 25544 51
6474 138
8658 0013828 167
1962 192
9544 15
51944929 11243
Satellite: ISS
Catalog Number: 25544
Epoch time: 13017
10272791 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 138
8658 deg
Eccentricity:
0013828
Arg of perigee: 167
1962 deg
Mean anomaly: 192
9544 deg
Mean motion: 15
51944929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1124
Checksum: 331
Coasting Arc #8 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2013/018/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3098855
94 A = 6793946
33 meter
Y = -5674886
22 meter E =
0024051
Z = 2034163
76 I = 51
91622
XDOT = 5201
709769 Wp = 141
04803
YDOT = 832
312668 meter/sec RA = 132
90997 deg
ZDOT = -5584
860402 TA = 16
53968
MA = 16
46135
Ha = 228
330 n
mi
Hp = 215
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10166850
18 X = 3152202
07
Y = -18618393
11 feet Y = -5639934
62 meter
Z = 6673765
60 Z = 2049347
10
XDOT = 17065
976932 XDOT = 5219
145572
YDOT = 2730
684605 feet/sec YDOT = 890
578993 meter/sec
ZDOT = -18323
032816 ZDOT = -5559
548827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17748550
74 X = -5409758
27
Y = 11582013
16 feet Y = 3530197
61 meter
Z = 6737541
82 Z = 2053602
75
XDOT = -12980
590811 XDOT = -3956
484079
YDOT = -9260
948730 feet/sec YDOT = -2822
737173 meter/sec
ZDOT = -18217
860861 ZDOT = -5552
803990
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 13018
13300960
00016717 00000-0 10270-3 0 9079
2 25544 51
6472 133
7470 0013829 170
8461 189
2945 15
51930869 11403
Satellite: ISS
Catalog Number: 25544
Epoch time: 13018
13300960 = yrday
fracday
Element set: 907
Inclination: 51
6472 deg
RA of node: 133
7470 deg
Eccentricity:
0013829
Arg of perigee: 170
8461 deg
Mean anomaly: 189
2945 deg
Mean motion: 15
51930869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 306
Coasting Arc #9 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2013/019/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3420547
76 A = 6794981
81 meter
Y = 5774613
19 meter E =
0009408
Z = -1093197
16 I = 51
94095
XDOT = -4600
349830 Wp = 131
46858
YDOT = -1613
170148 meter/sec RA = 127
96675 deg
ZDOT = 5899
759275 TA = 216
75025
MA = 216
81479
Ha = 228
040 n
mi
Hp = 215
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11222269
57 X = -3479556
07
Y = 18945581
34 feet Y = 5736032
57 meter
Z = -3586604
86 Z = -1109956
95
XDOT = -15093
011253 XDOT = -4610
628333
YDOT = -5292
552979 feet/sec YDOT = -1664
671745 meter/sec
ZDOT = 19356
165599 ZDOT = 5877
386353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18651424
88 X = 5684954
30
Y = -11682855
00 feet Y = -3560934
21 meter
Z = -3656961
86 Z = -1114641
97
XDOT = 10229
130423 XDOT = 3117
838953
YDOT = 10327
808203 feet/sec YDOT = 3147
915940 meter/sec
ZDOT = 19263
296807 ZDOT = 5871
452867
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 13019
09887972
00016717 00000-0 10270-3 0 9089
2 25544 51
6476 128
9475 0013646 174
7566 185
3731 15
52001498 11558
Satellite: ISS
Catalog Number: 25544
Epoch time: 13019
09887972 = yrday
fracday
Element set: 908
Inclination: 51
6476 deg
RA of node: 128
9475 deg
Eccentricity:
0013646
Arg of perigee: 174
7566 deg
Mean anomaly: 185
3731 deg
Mean motion: 15
52001498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 341
Coasting Arc #10 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2013/020/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3649675
83 A = 6795615
30 meter
Y = -5713960
28 meter E =
0024027
Z = 69453
26 I = 51
96083
XDOT = 4023
302948 Wp = 157
59331
YDOT = 2488
267822 meter/sec RA = 123
02678 deg
ZDOT = -6044
812591 TA = 21
66149
MA = 21
56003
Ha = 228
013 n
mi
Hp = 215
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11974002
07 X = 3712961
91
Y = -18746588
83 feet Y = -5672793
46 meter
Z = 227865
01 Z = 87336
44
XDOT = 13199
812821 XDOT = 4024
543436
YDOT = 8163
608339 feet/sec YDOT = 2533
266065 meter/sec
ZDOT = -19832
062306 ZDOT = -6025
264790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19051517
86 X = -5806902
64
Y = 11480904
07 feet Y = 3499379
56 meter
Z = 302902
49 Z = 92324
68
XDOT = -7474
765203 XDOT = -2278
308434
YDOT = -11839
419509 feet/sec YDOT = -3608
655066 meter/sec
ZDOT = -19751
039264 ZDOT = -6020
116768
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 13020
12912532
00016717 00000-0 10270-3 0 9097
2 25544 51
6478 123
8283 0013722 178
5925 181
5268 15
51971105 11718
Satellite: ISS
Catalog Number: 25544
Epoch time: 13020
12912532 = yrday
fracday
Element set: 909
Inclination: 51
6478 deg
RA of node: 123
8283 deg
Eccentricity:
0013722
Arg of perigee: 178
5925 deg
Mean anomaly: 181
5268 deg
Mean motion: 15
51971105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 299
Coasting Arc #11 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2013/021/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3792806
71 A = 6795024
50 meter
Y = 5564079
98 meter E =
0011846
Z = 929038
34 I = 51
97556
XDOT = -3467
453716 Wp = 118
77945
YDOT = -3365
662400 meter/sec RA = 118
08722 deg
ZDOT = 5938
446483 TA = 251
21171
MA = 251
34026
Ha = 227
631 n
mi
Hp = 216
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12443591
55 X = -3859256
51
Y = 18254855
58 feet Y = 5521294
86 meter
Z = 3048026
06 Z = 910452
24
XDOT = -11376
160485 XDOT = -3458
407576
YDOT = -11042
199475 feet/sec YDOT = -3404
387335 meter/sec
ZDOT = 19483
092135 ZDOT = 5921
623865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19083065
74 X = 5816518
44
Y = -11152958
96 feet Y = -3399421
89 meter
Z = 2970066
38 Z = 905276
23
XDOT = 4841
746086 XDOT = 1475
764207
YDOT = 13510
606838 feet/sec YDOT = 4118
032964 meter/sec
ZDOT = 19413
503819 ZDOT = 5917
235964
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 13021
15934997
00016717 00000-0 10270-3 0 9102
2 25544 51
6478 118
7085 0013428 182
6770 177
4312 15
52050359 11879
Satellite: ISS
Catalog Number: 25544
Epoch time: 13021
15934997 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 118
7085 deg
Eccentricity:
0013428
Arg of perigee: 182
6770 deg
Mean anomaly: 177
4312 deg
Mean motion: 15
52050359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 315
Coasting Arc #12 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2013/022/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3878877
47 A = 6793881
44 meter
Y = -5214843
45 meter E =
0019057
Z = -1940110
08 I = 51
98525
XDOT = 2957
374298 Wp = 171
42046
YDOT = 4286
442864 meter/sec RA = 113
14818 deg
ZDOT = -5634
289930 TA = 29
86798
MA = 29
75936
Ha = 227
608 n
mi
Hp = 216
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12725975
94 X = 3946327
09
Y = -17109066
44 feet Y = -5171090
18 meter
Z = -6365190
54 Z = -1921103
49
XDOT = 9702
671582 XDOT = 2936
592150
YDOT = 14063
132757 feet/sec YDOT = 4319
398180 meter/sec
ZDOT = -18485
203184 ZDOT = -5619
973674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18691110
56 X = -5697050
50
Y = 10311210
17 feet Y = 3142856
86 meter
Z = -6285507
09 Z = -1915822
56
XDOT = -2381
401015 XDOT = -725
851030
YDOT = -15497
500504 feet/sec YDOT = -4723
638154 meter/sec
ZDOT = -18426
148675 ZDOT = -5616
290116
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 13022
12517121
00016717 00000-0 10270-3 0 9117
2 25544 51
6480 113
9093 0013518 186
6313 173
4662 15
52030609 12023
Satellite: ISS
Catalog Number: 25544
Epoch time: 13022
12517121 = yrday
fracday
Element set: 911
Inclination: 51
6480 deg
RA of node: 113
9093 deg
Eccentricity:
0013518
Arg of perigee: 186
6313 deg
Mean anomaly: 173
4662 deg
Mean motion: 15
52030609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1202
Checksum: 264
Coasting Arc #13 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2013/023/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3912567
95 A = 6791907
09 meter
Y = 4767932
21 meter E =
0015271
Z = 2849422
67 I = 51
99012
XDOT = -2512
254777 Wp = 134
77597
YDOT = -5127
693885 meter/sec RA = 108
20632 deg
ZDOT = 5103
336385 TA = 257
38429
MA = 257
55510
Ha = 227
229 n
mi
Hp = 216
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12836509
01 X = -3979434
72
Y = 15642822
20 feet Y = 4723805
38 meter
Z = 9348499
56 Z = 2830253
88
XDOT = -8242
305700 XDOT = -2479
519393
YDOT = -16823
142666 feet/sec YDOT = -5155
604748 meter/sec
ZDOT = 16743
229610 ZDOT = 5091
211463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18046924
19 X = 5500702
49
Y = -9234590
54 feet Y = -2814703
20 meter
Z = 9268179
89 Z = 2824941
23
XDOT = 303
053541 XDOT = 92
370719
YDOT = 17436
774713 feet/sec YDOT = 5314
728932 meter/sec
ZDOT = 16693
392755 ZDOT = 5088
146112
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 13023
15536201
00016717 00000-0 10270-3 0 9122
2 25544 51
6478 108
7893 0013202 190
2953 169
7931 15
52085467 12187
Satellite: ISS
Catalog Number: 25544
Epoch time: 13023
15536201 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 108
7893 deg
Eccentricity:
0013202
Arg of perigee: 190
2953 deg
Mean anomaly: 169
7931 deg
Mean motion: 15
52085467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 303
Coasting Arc #14 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2013/024/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3934335
79 A = 6789525
18 meter
Y = -4113325
62 meter E =
0012125
Z = -3692377
86 I = 51
99059
XDOT = 2112
664979 Wp = 169
54907
YDOT = 5933
578459 meter/sec RA = 103
26223 deg
ZDOT = -4372
761510 TA = 54
13772
MA = 54
02518
Ha = 227
144 n
mi
Hp = 216
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12907925
82 X = 3997975
73
Y = -13495162
81 feet Y = -4068973
38 meter
Z = -12114100
60 Z = -3673111
18
XDOT = 6931
315549 XDOT = 2067
398767
YDOT = 19467
120927 feet/sec YDOT = 5956
950744 meter/sec
ZDOT = -14346
330412 ZDOT = -4362
608169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17148163
38 X = -5226760
20
Y = 7524774
42 feet Y = 2293551
24 meter
Z = -12033439
42 Z = -3667792
33
XDOT = 1483
780310 XDOT = 452
256238
YDOT = -19421
439910 feet/sec YDOT = -5919
654885 meter/sec
ZDOT = -14304
795636 ZDOT = -4360
101710
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 13024
12114927
00016717 00000-0 10270-3 0 9138
2 25544 51
6474 103
9898 0013284 194
3637 165
7139 15
52102173 12336
Satellite: ISS
Catalog Number: 25544
Epoch time: 13024
12114927 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 103
9898 deg
Eccentricity:
0013284
Arg of perigee: 194
3637 deg
Mean anomaly: 165
7139 deg
Mean motion: 15
52102173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 298
Coasting Arc #15 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2013/025/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3945000
50 A = 6787220
40 meter
Y = 3386507
69 meter E =
0016341
Z = 4367798
47 I = 51
98902
XDOT = -1784
176058 Wp = 161
31374
YDOT = -6587
658129 meter/sec RA = 98
31417 deg
ZDOT = 3477
514258 TA = 253
41211
MA = 253
59164
Ha = 226
858 n
mi
Hp = 217
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12942915
02 X = -4003793
10
Y = 11110589
54 feet Y = 3342063
29 meter
Z = 14330047
49 Z = 4348491
75
XDOT = -5853
595992 XDOT = -1727
271354
YDOT = -21613
051605 feet/sec YDOT = -6607
291893 meter/sec
ZDOT = 11409
167512 ZDOT = 3468
984975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16190138
79 X = 4934754
30
Y = -5581348
36 feet Y = -1701194
98 meter
Z = 14249297
07 Z = 4343185
75
XDOT = -2790
585918 XDOT = -850
570588
YDOT = 21101
621926 feet/sec YDOT = 6431
774363 meter/sec
ZDOT = 11374
472586 ZDOT = 3466
939244
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
15130689
00016717 00000-0 10270-3 0 9146
2 25544 51
6474 98
8697 0013054 197
6548 162
4152 15
52116310 12491
Satellite: ISS
Catalog Number: 25544
Epoch time: 13025
15130689 = yrday
fracday
Element set: 914
Inclination: 51
6474 deg
RA of node: 98
8697 deg
Eccentricity:
0013054
Arg of perigee: 197
6548 deg
Mean anomaly: 162
4152 deg
Mean motion: 15
52116310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1249
Checksum: 311
Coasting Arc #16 (Orbit 1263)
---------------------------------------
Vector Time (GMT): 2013/026/02:19:15
944
Vector Time (MET): N/A
Weight (LBS) : 903179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3984008
57 A = 6784970
35 meter
Y = -2482417
72 meter E =
0010850
Z = -4901418
28 I = 51
98427
XDOT = 1475
302958 Wp = 143
19668
YDOT = 7120
021698 meter/sec RA = 93
36195 deg
ZDOT = -2418
113787 TA = 103
25166
MA = 103
13061
Ha = 226
680 n
mi
Hp = 217
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13070894
25 X = 4035280
62
Y = -8144415
09 feet Y = -2437579
21 meter
Z = -16080768
62 Z = -4881940
30
XDOT = 4840
232801 XDOT = 1407
322000
YDOT = 23359
651239 feet/sec YDOT = 7136
139433 meter/sec
ZDOT = -7933
444182 ZDOT = -2411
111954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15185538
99 X = -4628552
28
Y = 3031379
63 feet Y = 923964
51 meter
Z = -15999407
37 Z = -4876619
37
XDOT = 3800
818084 XDOT = 1158
489352
YDOT = -22487
868601 feet/sec YDOT = -6854
302349 meter/sec
ZDOT = -7905
173626 ZDOT = -2409
496921
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
11706108
00016717 00000-0 10270-3 0 9159
2 25544 51
6461 94
0692 0013134 201
6389 158
4210 15
52168331 12645
Satellite: ISS
Catalog Number: 25544
Epoch time: 13026
11706108 = yrday
fracday
Element set: 915
Inclination: 51
6461 deg
RA of node: 94
0692 deg
Eccentricity:
0013134
Arg of perigee: 201
6389 deg
Mean anomaly: 158
4210 deg
Mean motion: 15
52168331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1264
Checksum: 278
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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