[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 7th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
128/06:58:09
462 -0
5 4
6 4
6
N/A 3
7 -0
3 224
2
000/00:14:18
923 2
7 0
1 221
5
137/01:53:03
499 -3
0 4
6 4
6
N/A -0
1 -0
2 225
7
000/00:14:06
998 -3
4 -0
1 222
3
Coasting Arc #1 (Orbit 2840)
---------------------------------------
Vector Time (GMT): 2013/127/14:27:04
301
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2631548
20 A = 6794129
80 meter
Y = 5900950
16 meter E =
0009169
Z = 2081239
28 I = 51
38596
XDOT = -5314
129807 Wp = 143
70686
YDOT = -424
893469 meter/sec RA = 308
94287 deg
ZDOT = -5509
330787 TA = 13
18969
MA = 13
16573
Ha = 223
292 n
mi
Hp = 221
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8633688
33 X = -2707448
60
Y = 19360072
71 feet Y = 5871098
16 meter
Z = 6828212
86 Z = 2068270
80
XDOT = -17434
809077 XDOT = -5282
220242
YDOT = -1394
007444 feet/sec YDOT = -484
141046 meter/sec
ZDOT = -18075
232240 ZDOT = -5535
069335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17875226
97 X = 5448369
18
Y = 11426980
55 feet Y = 3482943
67 meter
Z = 6773319
47 Z = 2064507
77
XDOT = -3092
941149 XDOT = -942
728462
YDOT = 15626
155166 feet/sec YDOT = 4762
852094 meter/sec
ZDOT = -18182
466910 ZDOT = -5542
015914
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 13127
63841886
00016717 00000-0 10270-3 0 9005
2 25544 51
6450 309
4132 0007997 252
1399 107
8881 15
51859968 28413
Satellite: ISS
Catalog Number: 25544
Epoch time: 13127
63841886 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 309
4132 deg
Eccentricity:
0007997
Arg of perigee: 252
1399 deg
Mean anomaly: 107
8881 deg
Mean motion: 15
51859968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2841
Checksum: 342
Coasting Arc #2 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2013/128/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4485326
73 A = 6787686
00 meter
Y = 670470
37 meter E =
0001979
Z = 5051215
46 I = 51
34659
XDOT = -3060
672122 Wp = 194
78629
YDOT = 6785
899766 meter/sec RA = 305
52424 deg
ZDOT = 1815
342113 TA = 237
54373
MA = 237
56286
Ha = 224
203 n
mi
Hp = 221
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14715638
89 X = 4452958
09
Y = 2199705
94 feet Y = 720447
12 meter
Z = 16572229
19 Z = 5072926
60
XDOT = -10041
575205 XDOT = -3145
144655
YDOT = 22263
450675 feet/sec YDOT = 6751
201081 meter/sec
ZDOT = 5955
846828 ZDOT = 1800
268181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11837283
17 X = 3608003
91
Y = 8846620
41 feet Y = 2696449
90 meter
Z = 16662639
32 Z = 5078772
46
XDOT = -18759
562414 XDOT = -5717
914624
YDOT = 13993
094391 feet/sec YDOT = 4265
095170 meter/sec
ZDOT = 5892
053766 ZDOT = 1795
897988
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 13128
34680756
00016717 00000-0 10270-3 0 9012
2 25544 51
6489 305
8999 0005093 283
3126 76
7457 15
50949957 28527
Satellite: ISS
Catalog Number: 25544
Epoch time: 13128
34680756 = yrday
fracday
Element set: 901
Inclination: 51
6489 deg
RA of node: 305
8999 deg
Eccentricity:
0005093
Arg of perigee: 283
3126 deg
Mean anomaly: 76
7457 deg
Mean motion: 15
50949957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 353
Coasting Arc #3 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2013/129/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224288
46 A = 6786884
62 meter
Y = -1053872
39 meter E =
0009838
Z = -5214919
71 I = 51
32734
XDOT = 3074
508842 Wp = 67
97064
YDOT = -6926
762511 meter/sec RA = 300
53687 deg
ZDOT = -1088
694776 TA = 191
52401
MA = 191
54655
Ha = 224
397 n
mi
Hp = 221
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13859214
11 X = -4186856
67
Y = -3457586
60 feet Y = -1100901
64 meter
Z = -17109316
63 Z = -5235350
46
XDOT = 10086
971266 XDOT = 3157
025578
YDOT = -22725
598791 feet/sec YDOT = -6891
920015 meter/sec
ZDOT = -3571
833254 ZDOT = -1073
558491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10647777
16 X = -3245442
48
Y = -9367023
14 feet Y = -2855068
65 meter
Z = -17194334
99 Z = -5240833
30
XDOT = 18701
791936 XDOT = 5700
306182
YDOT = -14808
197075 feet/sec YDOT = -4513
538469 meter/sec
ZDOT = -3507
762634 ZDOT = -1069
166051
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 13129
31331206
00016717 00000-0 10270-3 0 9024
2 25544 51
6490 301
1046 0005234 288
0205 72
0376 15
50990107 28676
Satellite: ISS
Catalog Number: 25544
Epoch time: 13129
31331206 = yrday
fracday
Element set: 902
Inclination: 51
6490 deg
RA of node: 301
1046 deg
Eccentricity:
0005234
Arg of perigee: 288
0205 deg
Mean anomaly: 72
0376 deg
Mean motion: 15
50990107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 274
Coasting Arc #4 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2013/130/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3987041
59 A = 6786510
14 meter
Y = 1482134
53 meter E =
0002750
Z = 5290104
47 I = 51
31168
XDOT = -3055
145486 Wp = 297
79121
YDOT = 7018
452749 meter/sec RA = 295
54781 deg
ZDOT = 337
625314 TA = 148
98067
MA = 148
96443
Ha = 224
416 n
mi
Hp = 221
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13080845
11 X = 3944473
29
Y = 4862646
10 feet Y = 1526481
92 meter
Z = 17355985
78 Z = 5309370
22
XDOT = -10023
443195 XDOT = -3135
040391
YDOT = 23026
419779 feet/sec YDOT = 6983
841455 meter/sec
ZDOT = 1107
694599 ZDOT = 322
589598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9486640
41 X = 2891528
00
Y = 10098046
34 feet Y = 3077884
52 meter
Z = 17436088
79 Z = 5314519
86
XDOT = -18439
809473 XDOT = -5620
453927
YDOT = 15528
484822 feet/sec YDOT = 4733
082174 meter/sec
ZDOT = 1044
032105 ZDOT = 318
220986
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 13130
34423783
00016717 00000-0 10270-3 0 9032
2 25544 51
6492 295
9898 0005268 291
6422 68
4168 15
50998046 28837
Satellite: ISS
Catalog Number: 25544
Epoch time: 13130
34423783 = yrday
fracday
Element set: 903
Inclination: 51
6492 deg
RA of node: 295
9898 deg
Eccentricity:
0005268
Arg of perigee: 291
6422 deg
Mean anomaly: 68
4168 deg
Mean motion: 15
50998046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 343
Coasting Arc #5 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2013/131/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3798934
09 A = 6786463
68 meter
Y = -1936019
91 meter E =
0009982
Z = -5288263
25 I = 51
29905
XDOT = 2998
639465 Wp = 81
27646
YDOT = -7032
076925 meter/sec RA = 290
55694 deg
ZDOT = 422
461889 TA = 192
76523
MA = 192
79052
Ha = 224
607 n
mi
Hp = 221
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12463694
52 X = -3751313
31
Y = -6351771
34 feet Y = -1978235
43 meter
Z = -17349945
06 Z = -5306602
92
XDOT = 9838
055987 XDOT = 3074
998548
YDOT = -23071
118521 feet/sec YDOT = -6998
117324 meter/sec
ZDOT = 1386
029819 ZDOT = 437
214380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8465564
27 X = -2580303
99
Y = -11016968
76 feet Y = -3357972
08 meter
Z = -17426126
79 Z = -5311483
45
XDOT = 17928
338387 XDOT = 5464
557540
YDOT = -16056
308611 feet/sec YDOT = -4893
962865 meter/sec
ZDOT = 1448
511545 ZDOT = 441
506319
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 13131
31071849
00016717 00000-0 10270-3 0 9043
2 25544 51
6488 291
1940 0005403 296
0099 64
0496 15
51026126 28982
Satellite: ISS
Catalog Number: 25544
Epoch time: 13131
31071849 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 291
1940 deg
Eccentricity:
0005403
Arg of perigee: 296
0099 deg
Mean anomaly: 64
0496 deg
Mean motion: 15
51026126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 309
Coasting Arc #6 (Orbit 2913)
---------------------------------------
Vector Time (GMT): 2013/132/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3644201
86 A = 6786821
18 meter
Y = 2420248
15 meter E =
0005162
Z = 5190864
22 I = 51
29095
XDOT = -2933
219569 Wp = 344
00254
YDOT = 6977
470417 meter/sec RA = 285
56619 deg
ZDOT = -1189
425658 TA = 117
49877
MA = 117
44630
Ha = 224
691 n
mi
Hp = 221
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11956042
85 X = 3591651
05
Y = 7940446
68 feet Y = 2460705
75 meter
Z = 17030394
42 Z = 5208440
23
XDOT = -9623
423784 XDOT = -3005
247136
YDOT = 22891
963310 feet/sec YDOT = 6944
266655 meter/sec
ZDOT = -3902
315150 ZDOT = -1203
849715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7539949
36 X = 2298176
57
Y = 12110213
53 feet Y = 3691193
08 meter
Z = 17103329
51 Z = 5213094
83
XDOT = -17275
496089 XDOT = -5265
571208
YDOT = 16374
639264 feet/sec YDOT = 4990
990048 meter/sec
ZDOT = -3963
417262 ZDOT = -1208
049581
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 13132
34161804
00016717 00000-0 10270-3 0 9059
2 25544 51
6492 286
0795 0005476 299
6893 60
3713 15
51046561 29144
Satellite: ISS
Catalog Number: 25544
Epoch time: 13132
34161804 = yrday
fracday
Element set: 905
Inclination: 51
6492 deg
RA of node: 286
0795 deg
Eccentricity:
0005476
Arg of perigee: 299
6893 deg
Mean anomaly: 60
3713 deg
Mean motion: 15
51046561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2914
Checksum: 317
Coasting Arc #7 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2013/133/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3548385
07 A = 6787562
60 meter
Y = -2897954
15 meter E =
0007853
Z = -5015050
47 I = 51
28528
XDOT = 2853
767400 Wp = 91
02620
YDOT = -6837
512209 meter/sec RA = 280
57426 deg
ZDOT = 1934
389696 TA = 197
84995
MA = 197
87755
Ha = 224
846 n
mi
Hp = 221
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11641683
29 X = -3491353
71
Y = -9507723
58 feet Y = -2937315
20 meter
Z = -16453577
65 Z = -5032150
11
XDOT = 9362
753937 XDOT = 2920
616963
YDOT = -22432
782837 feet/sec YDOT = -6805
225939 meter/sec
ZDOT = 6346
422887 ZDOT = 1948
415138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6842257
16 X = -2085519
98
Y = -13295538
20 feet Y = -4052480
04 meter
Z = -16524466
59 Z = -5036657
42
XDOT = 16460
387494 XDOT = 5017
126108
YDOT = -16422
382230 feet/sec YDOT = -5005
542104 meter/sec
ZDOT = 6405
839785 ZDOT = 1952
499967
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 13133
30807513
00016717 00000-0 10270-3 0 9061
2 25544 51
6483 281
2834 0005546 303
6954 56
3677 15
51058951 29293
Satellite: ISS
Catalog Number: 25544
Epoch time: 13133
30807513 = yrday
fracday
Element set: 906
Inclination: 51
6483 deg
RA of node: 281
2834 deg
Eccentricity:
0005546
Arg of perigee: 303
6954 deg
Mean anomaly: 56
3677 deg
Mean motion: 15
51058951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2929
Checksum: 318
Coasting Arc #8 (Orbit 2944)
---------------------------------------
Vector Time (GMT): 2013/134/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3486896
71 A = 6788593
42 meter
Y = 3386140
29 meter E =
0007347
Z = 4740366
52 I = 51
28463
XDOT = -2793
304511 Wp = 17
57827
YDOT = 6618
098882 meter/sec RA = 275
58400 deg
ZDOT = -2664
791789 TA = 98
93474
MA = 98
85157
Ha = 224
974 n
mi
Hp = 221
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11439949
83 X = 3425745
34
Y = 11109384
15 feet Y = 3424790
73 meter
Z = 15552383
59 Z = 4757157
43
XDOT = -9164
384879 XDOT = -2854
156932
YDOT = 21712
922841 feet/sec YDOT = 6586
522324 meter/sec
ZDOT = -8742
755212 ZDOT = -2678
508924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6280868
45 X = 1914408
70
Y = 14583333
96 feet Y = 4445000
19 meter
Z = 15621925
80 Z = 4761562
98
XDOT = -15602
441749 XDOT = -4755
624245
YDOT = 16175
282412 feet/sec YDOT = 4930
226079 meter/sec
ZDOT = -8800
851323 ZDOT = -2682
499483
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 13134
33894828
00016717 00000-0 10270-3 0 9071
2 25544 51
6485 276
1688 0005671 307
4105 52
6530 15
51092154 29452
Satellite: ISS
Catalog Number: 25544
Epoch time: 13134
33894828 = yrday
fracday
Element set: 907
Inclination: 51
6485 deg
RA of node: 276
1688 deg
Eccentricity:
0005671
Arg of perigee: 307
4105 deg
Mean anomaly: 52
6530 deg
Mean motion: 15
51092154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2945
Checksum: 317
Coasting Arc #9 (Orbit 2959)
---------------------------------------
Vector Time (GMT): 2013/135/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3482442
46 A = 6789938
50 meter
Y = -3833987
62 meter E =
0004264
Z = -4393858
41 I = 51
28561
XDOT = 2745
263809 Wp = 82
82490
YDOT = -6320
958841 meter/sec RA = 270
59331 deg
ZDOT = 3343
044176 TA = 221
17121
MA = 221
20338
Ha = 225
083 n
mi
Hp = 220
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11425336
16 X = -3417966
80
Y = -12578699
53 feet Y = -3872569
71 meter
Z = -14415545
96 Z = -4410619
58
XDOT = 9006
771028 XDOT = 2799
502350
YDOT = -20738
053940 feet/sec YDOT = -6289
956510 meter/sec
ZDOT = 10967
992703 ZDOT = 3356
511896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5989822
61 X = -1825697
93
Y = -15839169
76 feet Y = -4827778
94 meter
Z = -14484912
15 Z = -4415001
22
XDOT = 14708
323304 XDOT = 4483
096943
YDOT = -15634
607092 feet/sec YDOT = -4765
428242 meter/sec
ZDOT = 11025
002226 ZDOT = 3360
420679
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 13135
30538142
00016717 00000-0 10270-3 0 9084
2 25544 51
6470 271
3724 0005628 311
1875 48
8791 15
51092292 29608
Satellite: ISS
Catalog Number: 25544
Epoch time: 13135
30538142 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 271
3724 deg
Eccentricity:
0005628
Arg of perigee: 311
1875 deg
Mean anomaly: 48
8791 deg
Mean motion: 15
51092292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2960
Checksum: 306
Coasting Arc #10 (Orbit 2975)
---------------------------------------
Vector Time (GMT): 2013/136/07:05:18
923
Vector Time (MET): N/A
Weight (LBS) : 904509
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3503219
87 A = 6791385
39 meter
Y = 4270520
71 meter E =
0009012
Z = 3950250
44 I = 51
29169
XDOT = -2743
101408 Wp = 47
64712
YDOT = 5943
777293 meter/sec RA = 265
60536 deg
ZDOT = -3981
189645 TA = 84
15449
MA = 84
05177
Ha = 225
237 n
mi
Hp = 220
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11493503
51 X = 3436016
23
Y = 14010894
71 feet Y = 4309319
96 meter
Z = 12960139
23 Z = 3967105
87
XDOT = -8999
676537 XDOT = -2790
022446
YDOT = 19500
581670 feet/sec YDOT = 5912
840059 meter/sec
ZDOT = -13061
645816 ZDOT = -3994
629147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5836373
81 X = 1778926
74
Y = 17103530
54 feet Y = 5213156
11 meter
Z = 13029849
81 Z = 3971498
22
XDOT = -13888
706676 XDOT = -4233
277795
YDOT = 14762
656421 feet/sec YDOT = 4499
657677 meter/sec
ZDOT = -13118
480201 ZDOT = -3998
512765
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 13136
33622856
00016717 00000-0 10270-3 0 9095
2 25544 51
6472 266
2575 0005816 314
8547 45
2132 15
51134905 29767
Satellite: ISS
Catalog Number: 25544
Epoch time: 13136
33622856 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 266
2575 deg
Eccentricity:
0005816
Arg of perigee: 314
8547 deg
Mean anomaly: 45
2132 deg
Mean motion: 15
51134905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2976
Checksum: 316
Coasting Arc #11 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2013/137/02:00:06
998
Vector Time (MET): N/A
Weight (LBS) : 904003
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1622675
11 A = 6796774
39 meter
Y = 5849952
82 meter E =
0000831
Z = -3055520
40 I = 51
30367
XDOT = -4508
048447 Wp = 164
96758
YDOT = -3801
984233 meter/sec RA = 261
72624 deg
ZDOT = -4886
124713 TA = 50
20457
MA = 50
19725
Ha = 225
687 n
mi
Hp = 222
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5323737
23 X = -1673126
94
Y = 19192758
60 feet Y = 5831525
08 meter
Z = -10024673
21 Z = -3063525
56
XDOT = -14790
185192 XDOT = -4441
463151
YDOT = -12473
701553 feet/sec YDOT = -3852
023564 meter/sec
ZDOT = -16030
592892 ZDOT = -4907
862994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18556319
42 X = -5655966
16
Y = -7188963
48 feet Y = -2191196
07 meter
Z = -10058829
33 Z = -3065931
18
XDOT = 13382
032326 XDOT = 4078
843453
YDOT = -11990
785711 feet/sec YDOT = -3654
791485 meter/sec
ZDOT = -16120
734569 ZDOT = -4913
599897
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 13137
10937636
00016717 00000-0 10270-3 0 9108
2 25544 51
6479 262
4223 0004126 277
7115 82
3567 15
50211135 29880
Satellite: ISS
Catalog Number: 25544
Epoch time: 13137
10937636 = yrday
fracday
Element set: 910
Inclination: 51
6479 deg
RA of node: 262
4223 deg
Eccentricity:
0004126
Arg of perigee: 277
7115 deg
Mean anomaly: 82
3567 deg
Mean motion: 15
50211135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 302
Coasting Arc #12 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2013/138/02:00:06
998
Vector Time (MET): N/A
Weight (LBS) : 904003
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1434717
28 A = 6795884
48 meter
Y = -5714213
49 meter E =
0008486
Z = 3378887
35 I = 51
30559
XDOT = 4711
915581 Wp = 83
47273
YDOT = 3912
169895 meter/sec RA = 256
74744 deg
ZDOT = 4606
284753 TA = 316
12695
MA = 316
19431
Ha = 225
703 n
mi
Hp = 222
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4707077
68 X = 1482094
36
Y = -18747419
60 feet Y = -5697904
79 meter
Z = 11085588
43 Z = 3385972
03
XDOT = 15459
040619 XDOT = 4645
442390
YDOT = 12835
203066 feet/sec YDOT = 3964
489687 meter/sec
ZDOT = 15112
482784 ZDOT = 4629
013660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18286213
96 X = 5573638
01
Y = 6210005
75 feet Y = 1892809
75 meter
Z = 11115880
55 Z = 3388120
39
XDOT = -13639
104850 XDOT = -4157
199158
YDOT = 12889
181409 feet/sec YDOT = 3928
622493 meter/sec
ZDOT = 15206
751277 ZDOT = 4635
017789
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 13138
14080960
00016717 00000-0 10270-3 0 9113
2 25544 51
6474 257
3107 0004114 282
4798 77
5893 15
50215188 30046
Satellite: ISS
Catalog Number: 25544
Epoch time: 13138
14080960 = yrday
fracday
Element set: 911
Inclination: 51
6474 deg
RA of node: 257
3107 deg
Eccentricity:
0004114
Arg of perigee: 282
4798 deg
Mean anomaly: 77
5893 deg
Mean motion: 15
50215188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 303
Coasting Arc #13 (Orbit 3018)
---------------------------------------
Vector Time (GMT): 2013/139/02:00:06
998
Vector Time (MET): N/A
Weight (LBS) : 904003
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1291090
12 A = 6794829
35 meter
Y = 5552830
30 meter E =
0002754
Z = -3700526
67 I = 51
31104
XDOT = -4928
419211 Wp = 34
05482
YDOT = -4000
263079 meter/sec RA = 251
76861 deg
ZDOT = -4282
421916 TA = 190
17476
MA = 190
18033
Ha = 225
749 n
mi
Hp = 222
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4235859
98 X = -1335110
77
Y = 18217947
17 feet Y = 5538146
46 meter
Z = -12140835
52 Z = -3706905
53
XDOT = -16169
354367 XDOT = -4862
518058
YDOT = -13124
222699 feet/sec YDOT = -4055
007200 meter/sec
ZDOT = -14049
940669 ZDOT = -4306
203993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17894266
01 X = -5454172
28
Y = -5382119
70 feet Y = -1640470
09 meter
Z = -12168156
29 Z = -3708854
04
XDOT = 13789
457892 XDOT = 4203
026765
YDOT = -13853
761310 feet/sec YDOT = -4222
626447 meter/sec
ZDOT = -14148
599506 ZDOT = -4312
493129
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 13139
10776555
00016717 00000-0 10270-3 0 9123
2 25544 51
6481 252
5188 0004230 286
6805 73
3881 15
50249165 30193
Satellite: ISS
Catalog Number: 25544
Epoch time: 13139
10776555 = yrday
fracday
Element set: 912
Inclination: 51
6481 deg
RA of node: 252
5188 deg
Eccentricity:
0004230
Arg of perigee: 286
6805 deg
Mean anomaly: 73
3881 deg
Mean motion: 15
50249165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3019
Checksum: 310
Coasting Arc #14 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2013/140/02:00:06
998
Vector Time (MET): N/A
Weight (LBS) : 904003
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1172913
66 A = 6793876
02 meter
Y = -5368744
01 meter E =
0006810
Z = 3989216
25 I = 51
31819
XDOT = 5171
023338 Wp = 94
70109
YDOT = 4060
069612 meter/sec RA = 246
78916 deg
ZDOT = 3937
334517 TA = 314
11006
MA = 314
16606
Ha = 225
803 n
mi
Hp = 222
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3848141
93 X = 1213482
15
Y = -17613989
55 feet Y = -5355400
99 meter
Z = 13087979
83 Z = 3995012
68
XDOT = 16965
299665 XDOT = 5106
111681
YDOT = 13320
438358 feet/sec YDOT = 4117
532243 meter/sec
ZDOT = 12917
764164 ZDOT = 3962
297621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17400769
66 X = 5303754
59
Y = 4650012
87 feet Y = 1417323
92 meter
Z = 13112842
41 Z = 3996794
37
XDOT = -13816
342573 XDOT = -4211
221216
YDOT = 14923
473375 feet/sec YDOT = 4548
674685 meter/sec
ZDOT = 13021
349756 ZDOT = 3968
907406
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 13140
13917449
00016717 00000-0 10270-3 0 9138
2 25544 51
6479 247
4068 0004189 291
5700 68
5004 15
50252357 30350
Satellite: ISS
Catalog Number: 25544
Epoch time: 13140
13917449 = yrday
fracday
Element set: 913
Inclination: 51
6479 deg
RA of node: 247
4068 deg
Eccentricity:
0004189
Arg of perigee: 291
5700 deg
Mean anomaly: 68
5004 deg
Mean motion: 15
50252357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 302
Coasting Arc #15 (Orbit 3049)
---------------------------------------
Vector Time (GMT): 2013/141/02:00:06
998
Vector Time (MET): N/A
Weight (LBS) : 904003
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1103041
04 A = 6792814
21 meter
Y = 5173215
31 meter E =
0006056
Z = -4268205
61 I = 51
32844
XDOT = -5413
982032 Wp = 38
98952
YDOT = -4085
532342 meter/sec RA = 241
81023 deg
ZDOT = -3550
805768 TA = 194
55608
MA = 194
57353
Ha = 225
882 n
mi
Hp = 222
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3618901
05 X = -1140072
93
Y = 16972491
18 feet Y = 5160673
45 meter
Z = -14003299
25 Z = -4273654
01
XDOT = -17762
408240 XDOT = -5350
645201
YDOT = -13403
977499 feet/sec YDOT = -4145
720690 meter/sec
ZDOT = -11649
625223 ZDOT = -3576
953096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16844766
50 X = -5134284
83
Y = -4093938
09 feet Y = -1247832
33 meter
Z = -14026681
86 Z = -4275332
63
XDOT = 13686
397146 XDOT = 4171
613850
YDOT = -16006
827835 feet/sec YDOT = -4878
881124 meter/sec
ZDOT = -11758
154897 ZDOT = -3583
885613
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 13141
10610770
00016717 00000-0 10270-3 0 9144
2 25544 51
6484 242
6147 0004377 295
4209 64
6488 15
50287564 30505
Satellite: ISS
Catalog Number: 25544
Epoch time: 13141
10610770 = yrday
fracday
Element set: 914
Inclination: 51
6484 deg
RA of node: 242
6147 deg
Eccentricity:
0004377
Arg of perigee: 295
4209 deg
Mean anomaly: 64
6488 deg
Mean motion: 15
50287564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 303
Coasting Arc #16 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2013/142/02:00:06
998
Vector Time (MET): N/A
Weight (LBS) : 904003
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1067012
56 A = 6791902
46 meter
Y = -4962029
02 meter E =
0004665
Z = 4510008
39 I = 51
34083
XDOT = 5672
750701 Wp = 104
99389
YDOT = 4081
383096 meter/sec RA = 236
83112 deg
ZDOT = 3144
424786 TA = 313
28684
MA = 313
32574
Ha = 225
963 n
mi
Hp = 222
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3500697
36 X = 1100510
88
Y = -16279622
77 feet Y = -4949909
87 meter
Z = 14796615
46 Z = 4515273
14
XDOT = 18611
386813 XDOT = 5611
415105
YDOT = 13390
364488 feet/sec YDOT = 4144
476312 meter/sec
ZDOT = 10316
354284 ZDOT = 3171
834223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16221823
72 X = 4944411
87
Y = 3669394
75 feet Y = 1118431
52 meter
Z = 14819203
95 Z = 4516893
36
XDOT = -13418
833825 XDOT = -4090
060550
YDOT = 17147
572783 feet/sec YDOT = 5226
580184 meter/sec
ZDOT = 10430
156785 ZDOT = 3179
111788
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 13142
13749314
00016717 00000-0 10270-3 0 9156
2 25544 51
6486 237
5027 0004305 300
3992 59
6733 15
50287070 30669
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142
13749314 = yrday
fracday
Element set: 915
Inclination: 51
6486 deg
RA of node: 237
5027 deg
Eccentricity:
0004305
Arg of perigee: 300
3992 deg
Mean anomaly: 59
6733 deg
Mean motion: 15
50287070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 299
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list