[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 7th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 36597 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 66 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 2930)
---------------------------------------
Vector Time (GMT): 2011/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6677335
43 A = 6735976
57 meter
Y = -362042
85 meter E =
0015182
Z = 750890
64 I = 51
67400
XDOT = 939
250067 Wp = 56
51221
YDOT = -4761
365233 meter/sec RA = 178
01107 deg
ZDOT = 5978
446115 TA = 311
66533
MA = 311
79520
Ha = 192
989 n
mi
Hp = 185
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21907268
47 X = -6676438
43
Y = -1187804
63 feet Y = -436707
78 meter
Z = 2463551
98 Z = 718454
17
XDOT = 3081
529092 XDOT = 963
380363
YDOT = -15621
277011 feet/sec YDOT = -4750
726498 meter/sec
ZDOT = 19614
324525 ZDOT = 5983
068071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21708599
33 X = -6616781
08
Y = 3271795
12 feet Y = 997243
15 meter
Z = 2332477
59 Z = 710939
17
XDOT = -18
763891 XDOT = -5
719234
YDOT = -14314
134032 feet/sec YDOT = -4362
948053 meter/sec
ZDOT = 19633
039374 ZDOT = 5984
150401
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 11094
56218286
00016717 00000-0 10270-3 0 9000
2 25544 51
6457 178
7413 0001990 81
0824 279
0564 15
72590562 29313
Satellite: ISS
Catalog Number: 25544
Epoch time: 11094
56218286 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 178
7413 deg
Eccentricity:
0001990
Arg of perigee: 81
0824 deg
Mean anomaly: 279
0564 deg
Mean motion: 15
72590562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2931
Checksum: 317
Coasting Arc #2 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2011/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 86912
25 A = 6723835
34 meter
Y = 4190566
29 meter E =
0016872
Z = -5272015
84 I = 51
66371
XDOT = -7649
424063 Wp = 91
69466
YDOT = 646
337067 meter/sec RA = 172
87832 deg
ZDOT = 388
226026 TA = 181
99388
MA = 182
00062
Ha = 192
787 n
mi
Hp = 185
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 285145
17 X = 65656
79
Y = 13748577
06 feet Y = 4191418
95 meter
Z = -17296639
88 Z = -5271645
56
XDOT = -25096
535640 XDOT = -7657
968948
YDOT = 2120
528436 feet/sec YDOT = 560
748819 meter/sec
ZDOT = 1273
707435 ZDOT = 351
044021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3391691
29 X = 1033787
50
Y = 13328600
73 feet Y = 4062557
50 meter
Z = -17295180
34 Z = -5271570
97
XDOT = -23056
999534 XDOT = -7027
773458
YDOT = 7322
560229 feet/sec YDOT = 2231
916358 meter/sec
ZDOT = 1123
435721 ZDOT = 342
423208
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 11095
51533383
00016717 00000-0 10270-3 0 9015
2 25544 51
6445 173
8571 0001926 80
3964 279
7416 15
72705340 29468
Satellite: ISS
Catalog Number: 25544
Epoch time: 11095
51533383 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 173
8571 deg
Eccentricity:
0001926
Arg of perigee: 80
3964 deg
Mean anomaly: 279
7416 deg
Mean motion: 15
72705340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 317
Coasting Arc #3 (Orbit 2961)
---------------------------------------
Vector Time (GMT): 2011/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6571002
58 A = 6735489
30 meter
Y = -1452816
23 meter E =
0013809
Z = 33736
49 I = 51
73384
XDOT = 1067
184221 Wp = 127
46810
YDOT = 4647
575813 meter/sec RA = 167
75931 deg
ZDOT = -6044
898706 TA = 52
16607
MA = 52
04118
Ha = 192
676 n
mi
Hp = 184
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21558407
41 X = 6586595
98
Y = -4766457
44 feet Y = -1379248
10 meter
Z = 110684
03 Z = 65696
66
XDOT = 3501
260566 XDOT = 1044
500111
YDOT = 15247
952143 feet/sec YDOT = 4659
382544 meter/sec
ZDOT = -19832
344835 ZDOT = -6039
769639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19824789
74 X = 6042595
91
Y = -9716813
80 feet Y = -2961684
85 meter
Z = 239872
90 Z = 73113
26
XDOT = 6405
597431 XDOT = 1952
426097
YDOT = 12517
434342 feet/sec YDOT = 3815
313987 meter/sec
ZDOT = -19811
660495 ZDOT = -6038
594119
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 11096
53195511
00016717 00000-0 10270-3 0 9026
2 25544 51
6439 168
6462 0002123 82
2518 277
8885 15
72836069 29628
Satellite: ISS
Catalog Number: 25544
Epoch time: 11096
53195511 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 168
6462 deg
Eccentricity:
0002123
Arg of perigee: 82
2518 deg
Mean anomaly: 277
8885 deg
Mean motion: 15
72836069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2962
Checksum: 328
Coasting Arc #4 (Orbit 2977)
---------------------------------------
Vector Time (GMT): 2011/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1715440
87 A = 6723092
03 meter
Y = -3813190
31 meter E =
0004594
Z = 5260849
14 I = 51
72319
XDOT = 7226
541318 Wp = 99
80977
YDOT = -2629
942650 meter/sec RA = 162
64316 deg
ZDOT = 449
062801 TA = 345
92523
MA = 345
93803
Ha = 192
466 n
mi
Hp = 184
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5628086
85 X = -1698230
01
Y = -12510466
90 feet Y = -3832276
98 meter
Z = 17260003
74 Z = 5252557
41
XDOT = 23709
125058 XDOT = 7253
231258
YDOT = -8628
420767 feet/sec YDOT = -2548
981834 meter/sec
ZDOT = 1473
303152 ZDOT = 484
234542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8704897
74 X = -2653252
83
Y = -10656749
37 feet Y = -3248177
21 meter
Z = 17226529
56 Z = 5250646
21
XDOT = 19975
329879 XDOT = 6088
480547
YDOT = -13699
439137 feet/sec YDOT = -4175
589049 meter/sec
ZDOT = 1615
501822 ZDOT = 492
404955
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 11097
54849771
00016717 00000-0 10270-3 0 9033
2 25544 51
6440 163
4345 0002016 83
1950 276
9442 15
72975404 29787
Satellite: ISS
Catalog Number: 25544
Epoch time: 11097
54849771 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 163
4345 deg
Eccentricity:
0002016
Arg of perigee: 83
1950 deg
Mean anomaly: 276
9442 deg
Mean motion: 15
72975404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2978
Checksum: 324
Coasting Arc #5 (Orbit 2992)
---------------------------------------
Vector Time (GMT): 2011/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5947528
22 A = 6734705
29 meter
Y = 3067873
07 meter E =
0012352
Z = -711142
74 I = 51
79092
XDOT = -2754
622766 Wp = 46
48259
YDOT = -3967
432893 meter/sec RA = 157
51265 deg
ZDOT = 5995
270867 TA = 305
78876
MA = 305
90352
Ha = 192
376 n
mi
Hp = 184
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19512887
87 X = -5977937
11
Y = 10065200
38 feet Y = 3001194
17 meter
Z = -2333145
46 Z = -740109
92
XDOT = -9037
476267 XDOT = -2739
177549
YDOT = -13016
512115 feet/sec YDOT = -3998
150250 meter/sec
ZDOT = 19669
523842 ZDOT = 5981
926449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16069818
60 X = -4898080
71
Y = 14941942
58 feet Y = 4554304
10 meter
Z = -2450286
00 Z = -746847
17
XDOT = -11230
915363 XDOT = -3423
183003
YDOT = -8899
330215 feet/sec YDOT = -2712
515850 meter/sec
ZDOT = 19615
625797 ZDOT = 5978
842743
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 11098
50143893
00016717 00000-0 10270-3 0 9043
2 25544 51
6431 158
5483 0002231 78
2300 281
9112 15
73025410 29939
Satellite: ISS
Catalog Number: 25544
Epoch time: 11098
50143893 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 158
5483 deg
Eccentricity:
0002231
Arg of perigee: 78
2300 deg
Mean anomaly: 281
9112 deg
Mean motion: 15
73025410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2993
Checksum: 286
Coasting Arc #6 (Orbit 3008)
---------------------------------------
Vector Time (GMT): 2011/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2987255
21 A = 6722912
81 meter
Y = 3060672
77 meter E =
0016633
Z = -5201582
80 I = 51
78029
XDOT = -6295
854936 Wp = 82
10654
YDOT = 4270
526459 meter/sec RA = 152
41040 deg
ZDOT = -1103
625799 TA = 177
36860
MA = 177
35984
Ha = 192
207 n
mi
Hp = 184
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9800706
08 X = 2978076
57
Y = 10041577
34 feet Y = 3094026
66 meter
Z = -17065560
38 Z = -5187093
04
XDOT = -20655
692048 XDOT = -6337
779626
YDOT = 14010
913580 feet/sec YDOT = 4199
887959 meter/sec
ZDOT = -3620
819550 ZDOT = -1134
313039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12358514
26 X = 3766875
15
Y = 6793302
67 feet Y = 2070598
65 meter
Z = -17007017
10 Z = -5183738
81
XDOT = -15275
578313 XDOT = -4655
996270
YDOT = 18420
449698 feet/sec YDOT = 5614
553068 meter/sec
ZDOT = -3744
947295 ZDOT = -1141
459936
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 11099
51783473
00016717 00000-0 10270-3 0 9050
2 25544 51
6431 153
3352 0002270 84
9068 275
2353 15
73166307 30098
Satellite: ISS
Catalog Number: 25544
Epoch time: 11099
51783473 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 153
3352 deg
Eccentricity:
0002270
Arg of perigee: 84
9068 deg
Mean anomaly: 275
2353 deg
Mean motion: 15
73166307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3009
Checksum: 302
Coasting Arc #7 (Orbit 3024)
---------------------------------------
Vector Time (GMT): 2011/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5012762
10 A = 6733450
28 meter
Y = -4326617
22 meter E =
0015878
Z = 1183206
13 I = 51
84457
XDOT = 3963
641538 Wp = 116
73185
YDOT = 2963
827254 meter/sec RA = 147
27206 deg
ZDOT = -5901
070312 TA = 50
34205
MA = 50
20208
Ha = 192
006 n
mi
Hp = 183
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16446069
87 X = 5055022
80
Y = -14194938
40 feet Y = -4270325
16 meter
Z = 3881909
86 Z = 1207660
82
XDOT = 13004
073289 XDOT = 3958
871162
YDOT = 9723
842698 feet/sec YDOT = 3008
124316 meter/sec
ZDOT = -19360
466904 ZDOT = -5881
826612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11366356
52 X = 3464465
47
Y = -18493173
03 feet Y = -5636719
14 meter
Z = 3980854
83 Z = 1213364
55
XDOT = 14095
675018 XDOT = 4296
361745
YDOT = 4475
916459 feet/sec YDOT = 1364
259337 meter/sec
ZDOT = -19282
694548 ZDOT = -5877
365298
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 11100
53415245
00016717 00000-0 10270-3 0 9065
2 25544 51
6435 148
1219 0002418 84
0127 276
1312 15
73329260 30259
Satellite: ISS
Catalog Number: 25544
Epoch time: 11100
53415245 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 148
1219 deg
Eccentricity:
0002418
Arg of perigee: 84
0127 deg
Mean anomaly: 276
1312 deg
Mean motion: 15
73329260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3025
Checksum: 268
Coasting Arc #8 (Orbit 3040)
---------------------------------------
Vector Time (GMT): 2011/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3847484
54 A = 6722575
50 meter
Y = -2085799
07 meter E =
0007170
Z = 5097937
77 I = 51
83353
XDOT = 5110
646411 Wp = 113
83216
YDOT = -5543
455257 meter/sec RA = 142
18053 deg
ZDOT = 1584
413744 TA = 320
97895
MA = 321
03067
Ha = 192
017 n
mi
Hp = 183
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12622980
78 X = -3848639
54
Y = -6843172
80 feet Y = -2128830
30 meter
Z = 16725517
63 Z = 5079244
03
XDOT = 16767
212634 XDOT = 5164
557787
YDOT = -18187
189162 feet/sec YDOT = -5486
003432 meter/sec
ZDOT = 5198
207820 ZDOT = 1609
372251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14239582
74 X = -4340224
82
Y = -2434144
93 feet Y = -741927
37 meter
Z = 16649949
54 Z = 5074904
62
XDOT = 9894
558445 XDOT = 3015
861414
YDOT = -21531
668881 feet/sec YDOT = -6562
852675 meter/sec
ZDOT = 5299
221637 ZDOT = 1615
202755
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 11101
55039393
00016717 00000-0 10270-3 0 9075
2 25544 51
6431 142
9085 0002528 89
2836 270
8616 15
73431992 30416
Satellite: ISS
Catalog Number: 25544
Epoch time: 11101
55039393 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 142
9085 deg
Eccentricity:
0002528
Arg of perigee: 89
2836 deg
Mean anomaly: 270
8616 deg
Mean motion: 15
73431992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3041
Checksum: 305
Coasting Arc #9 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2011/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3886501
20 A = 6732377
71 meter
Y = 5273017
04 meter E =
0009869
Z = -1542769
65 I = 51
89210
XDOT = -4734
261091 Wp = 49
95762
YDOT = -1802
636935 meter/sec RA = 137
03717 deg
ZDOT = 5795
667294 TA = 293
10382
MA = 293
20780
Ha = 191
712 n
mi
Hp = 183
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12750988
20 X = -3937681
78
Y = 17299924
68 feet Y = 5229269
60 meter
Z = -5061580
23 Z = -1561774
70
XDOT = -15532
352660 XDOT = -4741
905937
YDOT = -5914
163171 feet/sec YDOT = -1855
620817 meter/sec
ZDOT = 19014
656475 ZDOT = 5772
649898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6195648
80 X = -1888433
76
Y = 20559771
26 feet Y = 6266618
28 meter
Z = -5138524
11 Z = -1566222
15
XDOT = -15223
488682 XDOT = -4640
119350
YDOT = 116
913722 feet/sec YDOT = 35
635302 meter/sec
ZDOT = 18921
590667 ZDOT = 5767
300835
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 11102
50305009
00016717 00000-0 10270-3 0 9082
2 25544 51
6438 138
0203 0002586 91
7087 268
4372 15
73552620 30561
Satellite: ISS
Catalog Number: 25544
Epoch time: 11102
50305009 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 138
0203 deg
Eccentricity:
0002586
Arg of perigee: 91
7087 deg
Mean anomaly: 268
4372 deg
Mean motion: 15
73552620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 287
Coasting Arc #10 (Orbit 3071)
---------------------------------------
Vector Time (GMT): 2011/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4332149
48 A = 6722289
99 meter
Y = 1092252
28 meter E =
0015641
Z = -5036758
98 I = 51
88098
XDOT = -3793
980777 Wp = 79
36593
YDOT = 6419
382684 meter/sec RA = 131
95192 deg
ZDOT = -1873
217181 TA = 172
60514
MA = 172
58204
Ha = 191
586 n
mi
Hp = 183
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14213088
84 X = 4344081
26
Y = 3583504
84 feet Y = 1140763
41 meter
Z = -16524799
81 Z = -5015684
60
XDOT = -12447
443494 XDOT = -3856
381860
YDOT = 21060
966810 feet/sec YDOT = 6376
607072 meter/sec
ZDOT = -6145
725659 ZDOT = -1891
800197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14658914
82 X = 4468037
24
Y = -1667028
07 feet Y = -508110
16 meter
Z = -16439575
53 Z = -5010782
62
XDOT = -4352
578127 XDOT = -1326
665813
YDOT = 23007
410976 feet/sec YDOT = 7012
658865 meter/sec
ZDOT = -6220
988749 ZDOT = -1896
157371
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 11103
51914039
00016717 00000-0 10270-3 0 9094
2 25544 51
6442 132
8054 0002601 95
8323 264
3137 15
73650071 30729
Satellite: ISS
Catalog Number: 25544
Epoch time: 11103
51914039 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 132
8054 deg
Eccentricity:
0002601
Arg of perigee: 95
8323 deg
Mean anomaly: 264
3137 deg
Mean motion: 15
73650071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 277
Coasting Arc #11 (Orbit 3087)
---------------------------------------
Vector Time (GMT): 2011/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2747719
71 A = 6731499
41 meter
Y = -5896397
88 meter E =
0016748
Z = 1701438
82 I = 51
93172
XDOT = 5088
776003 Wp = 112
78174
YDOT = 703
870650 meter/sec RA = 126
80614 deg
ZDOT = -5740
644975 TA = 48
47000
MA = 48
32645
Ha = 191
416 n
mi
Hp = 183
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9014828
44 X = 2805184
88
Y = -19345137
39 feet Y = -5865349
77 meter
Z = 5582148
37 Z = 1714927
25
XDOT = 16695
459329 XDOT = 5108
413917
YDOT = 2309
286911 feet/sec YDOT = 760
885782 meter/sec
ZDOT = -18834
137057 ZDOT = -5715
876128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1255922
01 X = 382805
03
Y = -21291100
33 feet Y = -6489527
38 meter
Z = 5636803
99 Z = 1718097
86
XDOT = 14929
893538 XDOT = 4550
631550
YDOT = -4111
912835 feet/sec YDOT = -1253
311032 meter/sec
ZDOT = -18733
957984 ZDOT = -5710
110393
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 11104
53515147
00016717 00000-0 10270-3 0 9106
2 25544 51
6428 127
5899 0002742 97
8109 262
3365 15
73788659 30883
Satellite: ISS
Catalog Number: 25544
Epoch time: 11104
53515147 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 127
5899 deg
Eccentricity:
0002742
Arg of perigee: 97
8109 deg
Mean anomaly: 262
3365 deg
Mean motion: 15
73788659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 333
Coasting Arc #12 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2011/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4494286
80 A = 6721721
67 meter
Y = -166695
05 meter E =
0008602
Z = 4990147
24 I = 51
91643
XDOT = 2490
080705 Wp = 117
14520
YDOT = -7011
590486 meter/sec RA = 121
72369 deg
ZDOT = 2001
961669 TA = 313
54483
MA = 313
61625
Ha = 191
392 n
mi
Hp = 182
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14745035
42 X = -4516330
04
Y = -546899
77 feet Y = -217075
70 meter
Z = 16371874
13 Z = 4968260
42
XDOT = 8169
556120 XDOT = 2558
575391
YDOT = -23003
905794 feet/sec YDOT = -6983
361740 meter/sec
ZDOT = 6568
115713 ZDOT = 2014
225500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13920722
59 X = -4243036
24
Y = 5178775
97 feet Y = 1578490
92 meter
Z = 16283340
99 Z = 4963162
33
XDOT = -920
093924 XDOT = -280
444628
YDOT = -23348
412579 feet/sec YDOT = -7116
596154 meter/sec
ZDOT = 6617
844946 ZDOT = 2017
119139
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 11105
55108284
00016717 00000-0 10270-3 0 9110
2 25544 51
6420 122
3737 0002783 101
7053 258
4422 15
73901784 31042
Satellite: ISS
Catalog Number: 25544
Epoch time: 11105
55108284 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 122
3737 deg
Eccentricity:
0002783
Arg of perigee: 101
7053 deg
Mean anomaly: 258
4422 deg
Mean motion: 15
73901784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 276
Coasting Arc #13 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2011/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1616074
61 A = 6730626
18 meter
Y = 6292899
26 meter E =
0008919
Z = -1751533
58 I = 51
96379
XDOT = -5139
854336 Wp = 55
55459
YDOT = 266
058776 meter/sec RA = 116
57788 deg
ZDOT = 5723
699350 TA = 285
14742
MA = 285
24605
Ha = 190
995 n
mi
Hp = 182
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5302082
04 X = -1677814
20
Y = 20645994
96 feet Y = 6274481
98 meter
Z = -5746501
23 Z = -1759535
03
XDOT = -16863
039160 XDOT = -5170
252366
YDOT = 872
896248 feet/sec YDOT = 208
412328 meter/sec
ZDOT = 18778
541176 ZDOT = 5698
655885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3401552
67 X = 1036793
25
Y = 21033882
39 feet Y = 6411127
35 meter
Z = -5778986
86 Z = -1761435
20
XDOT = -13685
120534 XDOT = -4171
224739
YDOT = 7321
816707 feet/sec YDOT = 2231
689732 meter/sec
ZDOT = 18677
227885 ZDOT = 5692
819059
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 11106
50344432
00016717 00000-0 10270-3 0 9124
2 25544 51
6425 117
4840 0002844 107
5194 252
6280 15
74068335 31196
Satellite: ISS
Catalog Number: 25544
Epoch time: 11106
50344432 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 117
4840 deg
Eccentricity:
0002844
Arg of perigee: 107
5194 deg
Mean anomaly: 252
6280 deg
Mean motion: 15
74068335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 284
Coasting Arc #14 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2011/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4446225
66 A = 6720936
25 meter
Y = -559207
99 meter E =
0015388
Z = -5022579
40 I = 51
94323
XDOT = -1260
244856 Wp = 81
48104
YDOT = 7334
530123 meter/sec RA = 111
49483 deg
ZDOT = -1935
032476 TA = 169
89617
MA = 169
86520
Ha = 190
832 n
mi
Hp = 182
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14587354
54 X = 4476547
48
Y = -1834671
87 feet Y = -509318
39 meter
Z = -16478278
87 Z = -5000905
67
XDOT = -4134
661602 XDOT = -1332
767147
YDOT = 24063
419039 feet/sec YDOT = 7320
031677 meter/sec
ZDOT = -6348
531745 ZDOT = -1941
331473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12604371
82 X = 3841812
53
Y = -7756870
97 feet Y = -2364294
27 meter
Z = -16390587
90 Z = -4995851
19
XDOT = 5679
272477 XDOT = 1731
042251
YDOT = 22677
876564 feet/sec YDOT = 6912
216777 meter/sec
ZDOT = -6374
165753 ZDOT = -1942
845722
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 11107
51921723
00016717 00000-0 10270-3 0 9131
2 25544 51
6413 112
2660 0002719 110
5317 249
6138 15
74145683 31356
Satellite: ISS
Catalog Number: 25544
Epoch time: 11107
51921723 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 112
2660 deg
Eccentricity:
0002719
Arg of perigee: 110
5317 deg
Mean anomaly: 249
6138 deg
Mean motion: 15
74145683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 281
Coasting Arc #15 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2011/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 604966
27 A = 6730216
79 meter
Y = -6501443
88 meter E =
0016811
Z = 1598595
41 I = 51
98559
XDOT = 4996
303409 Wp = 116
27029
YDOT = -967
152946 meter/sec RA = 106
34933 deg
ZDOT = -5784
924502 TA = 46
16187
MA = 46
02304
Ha = 190
596 n
mi
Hp = 182
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1984797
49 X = 669855
89
Y = -21330196
46 feet Y = -6494315
90 meter
Z = 5244735
58 Z = 1601692
25
XDOT = 16392
071551 XDOT = 5034
849515
YDOT = -3173
073971 feet/sec YDOT = -911
065948 meter/sec
ZDOT = -18979
411095 ZDOT = -5760
558416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7409401
82 X = -2258385
68
Y = -20096873
14 feet Y = -6125526
93 meter
Z = 5257414
58 Z = 1602459
96
XDOT = 12070
766337 XDOT = 3679
169580
YDOT = -9423
190413 feet/sec YDOT = -2872
188438 meter/sec
ZDOT = -18880
813341 ZDOT = -5754
871906
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 11108
53490646
00016717 00000-0 10270-3 0 9140
2 25544 51
6407 107
0477 0002721 112
4999 247
6452 15
74297868 31515
Satellite: ISS
Catalog Number: 25544
Epoch time: 11108
53490646 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 107
0477 deg
Eccentricity:
0002721
Arg of perigee: 112
4999 deg
Mean anomaly: 247
6452 deg
Mean motion: 15
74297868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 319
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