[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 12th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 3039)
---------------------------------------
Vector Time (GMT): 2011/101/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2041262
41 A = 6722612
42 meter
Y = 3659477
40 meter E =
0017329
Z = -5271786
66 I = 51
83073
XDOT = -6325
394938 Wp = 94
30243
YDOT = 4331
893762 meter/sec RA = 142
31459 deg
ZDOT = 558
109936 TA = 180
99477
MA = 180
99822
Ha = 192
285 n
mi
Hp = 184
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6697055
14 X = 2025799
00
Y = 12006159
47 feet Y = 3682217
44 meter
Z = -17295888
00 Z = -5261907
91
XDOT = -20752
608063 XDOT = -6376
076066
YDOT = 14212
249874 feet/sec YDOT = 4260
876000 meter/sec
ZDOT = 1831
069344 ZDOT = 527
258084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8508607
74 X = 2593423
64
Y = 10861883
86 feet Y = 3310702
20 meter
Z = -17255991
07 Z = -5259626
08
XDOT = -17629
215751 XDOT = -5373
384961
YDOT = 16518
880492 feet/sec YDOT = 5034
954774 meter/sec
ZDOT = 1706
240580 ZDOT = 520
062129
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
48725400
00016717 00000-0 10270-3 0 9001
2 25544 51
6435 143
2426 0002422 93
5313 266
6127 15
73151851 30406
Satellite: ISS
Catalog Number: 25544
Epoch time: 11101
48725400 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 143
2426 deg
Eccentricity:
0002422
Arg of perigee: 93
5313 deg
Mean anomaly: 266
6127 deg
Mean motion: 15
73151851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 261
Coasting Arc #2 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2011/102/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5068213
77 A = 6734285
95 meter
Y = -4418461
46 meter E =
0013824
Z = -255875
94 I = 51
89520
XDOT = 2957
524863 Wp = 129
77177
YDOT = 3729
990408 meter/sec RA = 137
20793 deg
ZDOT = -6052
163007 TA = 52
99824
MA = 52
87180
Ha = 192
214 n
mi
Hp = 183
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16627997
94 X = 5118488
16
Y = -14496264
62 feet Y = -4361504
53 meter
Z = -839487
98 Z = -231132
41
XDOT = 9703
165561 XDOT = 2944
995729
YDOT = 12237
501338 feet/sec YDOT = 3762
992942 meter/sec
ZDOT = -19856
177844 ZDOT = -6037
826024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14003246
33 X = 4268189
48
Y = -17049903
22 feet Y = -5196810
50 meter
Z = -739348
20 Z = -225353
33
XDOT = 10468
864338 XDOT = 3190
909850
YDOT = 9420
622589 feet/sec YDOT = 2871
405765 meter/sec
ZDOT = -19798
248478 ZDOT = -6034
506136
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
50359875
00016717 00000-0 10270-3 0 9015
2 25544 51
6441 138
0296 0002587 94
8450 265
3008 15
73251334 30566
Satellite: ISS
Catalog Number: 25544
Epoch time: 11102
50359875 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 138
0296 deg
Eccentricity:
0002587
Arg of perigee: 94
8450 deg
Mean anomaly: 265
3008 deg
Mean motion: 15
73251334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 295
Coasting Arc #3 (Orbit 3071)
---------------------------------------
Vector Time (GMT): 2011/103/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3062842
35 A = 6722056
78 meter
Y = -2797279
94 meter E =
0004982
Z = 5285397
41 I = 51
87556
XDOT = 5176
503317 Wp = 95
19004
YDOT = -5706
110906 meter/sec RA = 132
09349 deg
ZDOT = -20
626915 TA = 355
00247
MA = 355
00744
Ha = 192
220 n
mi
Hp = 183
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10048695
38 X = -3057010
36
Y = -9177427
62 feet Y = -2831497
57 meter
Z = 17340542
69 Z = 5270532
54
XDOT = 16983
278598 XDOT = 5240
025609
YDOT = -18720
836307 feet/sec YDOT = -5647
868934 meter/sec
ZDOT = -67
673607 ZDOT = 4
675033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11656531
32 X = -3552910
75
Y = -7169855
45 feet Y = -2185371
94 meter
Z = 17280460
87 Z = 5267084
47
XDOT = 12758
864762 XDOT = 3888
901980
YDOT = -20655
835955 feet/sec YDOT = -6295
898799 meter/sec
ZDOT = 34
754774 ZDOT = 10
593255
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
51990340
00016717 00000-0 10270-3 0 9026
2 25544 51
6434 132
8167 0002624 98
9939 261
1521 15
73309903 30724
Satellite: ISS
Catalog Number: 25544
Epoch time: 11103
51990340 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 132
8167 deg
Eccentricity:
0002624
Arg of perigee: 98
9939 deg
Mean anomaly: 261
1521 deg
Mean motion: 15
73309903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 294
Coasting Arc #4 (Orbit 3086)
---------------------------------------
Vector Time (GMT): 2011/104/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3919893
00 A = 6734026
14 meter
Y = 5465510
32 meter E =
0013471
Z = -199603
09 I = 51
93621
XDOT = -3959
040029 Wp = 52
98896
YDOT = -2628
674411 meter/sec RA = 126
97993 deg
ZDOT = 6058
006868 TA = 304
85181
MA = 304
97842
Ha = 192
063 n
mi
Hp = 183
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12860541
35 X = -3979748
41
Y = 17931464
32 feet Y = 5421341
02 meter
Z = -654865
78 Z = -218791
69
XDOT = -12988
976474 XDOT = -3958
780064
YDOT = -8624
259879 feet/sec YDOT = -2672
944872 meter/sec
ZDOT = 19875
350618 ZDOT = 6038
774747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9023069
56 X = -2750231
60
Y = 20134729
71 feet Y = 6137065
61 meter
Z = -732571
47 Z = -223287
78
XDOT = -13095
643452 XDOT = -3991
552124
YDOT = -5178
901013 feet/sec YDOT = -1578
529029 meter/sec
ZDOT = 19797
598640 ZDOT = 6034
308065
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
47265314
00016717 00000-0 10270-3 0 9039
2 25544 51
6437 127
9291 0002647 98
9840 261
1623 15
73341628 30875
Satellite: ISS
Catalog Number: 25544
Epoch time: 11104
47265314 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 127
9291 deg
Eccentricity:
0002647
Arg of perigee: 98
9840 deg
Mean anomaly: 261
1623 deg
Mean motion: 15
73341628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3087
Checksum: 308
Coasting Arc #5 (Orbit 3102)
---------------------------------------
Vector Time (GMT): 2011/105/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3767823
09 A = 6721865
27 meter
Y = 1787137
33 meter E =
0017448
Z = -5286834
96 I = 51
91364
XDOT = -3766
603893 Wp = 89
55413
YDOT = 6687
690598 meter/sec RA = 121
87468 deg
ZDOT = -424
774919 TA = 176
42632
MA = 176
41384
Ha = 191
946 n
mi
Hp = 183
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12361624
30 X = 3773241
48
Y = 5863311
46 feet Y = 1829301
25 meter
Z = -17345259
04 Z = -5268517
84
XDOT = -12357
624320 XDOT = -3839
043498
YDOT = 21941
242118 feet/sec YDOT = 6645
165077 meter/sec
ZDOT = -1393
618502 ZDOT = -443
249661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13437934
20 X = 4095882
35
Y = 3028858
15 feet Y = 923195
97 meter
Z = -17271193
66 Z = -5264259
83
XDOT = -7092
253943 XDOT = -2161
719002
YDOT = 23112
267817 feet/sec YDOT = 7044
619230 meter/sec
ZDOT = -1468
466097 ZDOT = -447
588466
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
48887941
00016717 00000-0 10270-3 0 9048
2 25544 51
6440 122
7150 0002622 105
5450 254
6002 15
73405528 31038
Satellite: ISS
Catalog Number: 25544
Epoch time: 11105
48887941 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 122
7150 deg
Eccentricity:
0002622
Arg of perigee: 105
5450 deg
Mean anomaly: 254
6002 deg
Mean motion: 15
73405528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3103
Checksum: 270
Coasting Arc #6 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2011/106/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2646613
50 A = 6733520
79 meter
Y = -6161590
19 meter E =
0015791
Z = 524880
44 I = 51
96750
XDOT = 4563
454623 Wp = 125
86092
YDOT = 1436
050610 meter/sec RA = 116
75521 deg
ZDOT = -6036
008217 TA = 48
45356
MA = 48
31824
Ha = 191
883 n
mi
Hp = 183
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8683115
17 X = 2712767
08
Y = -20215190
93 feet Y = -6131624
23 meter
Z = 1722048
68 Z = 537899
00
XDOT = 14971
963987 XDOT = 4576
379328
YDOT = 4711
452131 feet/sec YDOT = 1487
153679 meter/sec
ZDOT = -19803
176565 ZDOT = -6013
807515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3724494
82 X = 1135226
02
Y = -21679345
28 feet Y = -6607864
44 meter
Z = 1774827
15 Z = 540967
32
XDOT = 14191
567074 XDOT = 4325
589644
YDOT = 793
852404 feet/sec YDOT = 241
966213 meter/sec
ZDOT = -19713
394842 ZDOT = -6008
642748
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
50506458
00016717 00000-0 10270-3 0 9054
2 25544 51
6426 117
5004 0002769 108
0325 252
1140 15
73484216 31197
Satellite: ISS
Catalog Number: 25544
Epoch time: 11106
50506458 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 117
5004 deg
Eccentricity:
0002769
Arg of perigee: 108
0325 deg
Mean anomaly: 252
1140 deg
Mean motion: 15
73484216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 275
Coasting Arc #7 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2011/107/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4136670
45 A = 6721580
53 meter
Y = -711384
51 meter E =
0005942
Z = 5245623
13 I = 51
93990
XDOT = 2252
523802 Wp = 115
70063
YDOT = -7326
606683 meter/sec RA = 111
65695 deg
ZDOT = 779
531112 TA = 326
89778
MA = 326
93495
Ha = 191
896 n
mi
Hp = 183
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13571753
43 X = -4153890
78
Y = -2333938
67 feet Y = -757739
20 meter
Z = 17210049
63 Z = 5225485
14
XDOT = 7390
169953 XDOT = 2330
497033
YDOT = -24037
423500 feet/sec YDOT = -7300
981570 meter/sec
ZDOT = 2557
516772 ZDOT = 790
663906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13824015
09 X = -4213559
80
Y = 1154692
24 feet Y = 351950
19 meter
Z = 17128597
77 Z = 5220796
60
XDOT = 1224
146203 XDOT = 373
119763
YDOT = -24109
255352 feet/sec YDOT = -7348
501031 meter/sec
ZDOT = 2602
704821 ZDOT = 793
304429
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
52120793
00016717 00000-0 10270-3 0 9062
2 25544 51
6418 112
2854 0002758 111
1599 248
9859 15
73550556 31358
Satellite: ISS
Catalog Number: 25544
Epoch time: 11107
52120793 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 112
2854 deg
Eccentricity:
0002758
Arg of perigee: 111
1599 deg
Mean anomaly: 248
9859 deg
Mean motion: 15
73550556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 314
Coasting Arc #8 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2011/108/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1283472
53 A = 6732852
29 meter
Y = 6555606
05 meter E =
0011249
Z = -812687
48 I = 51
98983
XDOT = -4825
270974 Wp = 53
43194
YDOT = -209
403071 meter/sec RA = 106
53360 deg
ZDOT = 5994
783186 TA = 297
75111
MA = 297
86514
Ha = 191
573 n
mi
Hp = 183
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4210867
88 X = -1352735
23
Y = 21507893
85 feet Y = 6540866
18 meter
Z = -2666297
51 Z = -819091
19
XDOT = -15830
941516 XDOT = -4851
692789
YDOT = -687
017951 feet/sec YDOT = -263
509677 meter/sec
ZDOT = 19667
923837 ZDOT = 5971
277484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1683788
15 X = 513218
63
Y = 21848252
29 feet Y = 6659347
30 meter
Z = -2692355
44 Z = -820629
94
XDOT = -13962
096314 XDOT = -4255
646957
YDOT = 3462
583437 feet/sec YDOT = 1055
395432 meter/sec
ZDOT = 19572
834195 ZDOT = 5965
799863
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
47380419
00016717 00000-0 10270-3 0 9071
2 25544 51
6424 107
3972 0002806 117
4272 242
7177 15
73657831 31508
Satellite: ISS
Catalog Number: 25544
Epoch time: 11108
47380419 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 107
3972 deg
Eccentricity:
0002806
Arg of perigee: 117
4272 deg
Mean anomaly: 242
7177 deg
Mean motion: 15
73657831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 303
Coasting Arc #9 (Orbit 3165)
---------------------------------------
Vector Time (GMT): 2011/109/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4233888
88 A = 6721416
62 meter
Y = -307296
34 meter E =
0016690
Z = -5225595
57 I = 51
95822
XDOT = -714
846081 Wp = 87
67752
YDOT = 7585
548831 meter/sec RA = 101
44012 deg
ZDOT = -1027
401887 TA = 172
56554
MA = 172
54076
Ha = 191
509 n
mi
Hp = 183
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13890711
55 X = 4262395
83
Y = -1008190
10 feet Y = -259791
08 meter
Z = -17144342
43 Z = -5204957
78
XDOT = -2345
295541 XDOT = -794
624999
YDOT = 24886
971229 feet/sec YDOT = 7577
108912 meter/sec
ZDOT = -3370
741100 ZDOT = -1031
068509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13136437
45 X = 4003986
13
Y = -4925303
97 feet Y = -1501232
65 meter
Z = -17060837
73 Z = -5200143
34
XDOT = 4449
293443 XDOT = 1356
144642
YDOT = 23570
406281 feet/sec YDOT = 7184
259834 meter/sec
ZDOT = -3385
769763 ZDOT = -1031
982624
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 11109
48986586
00016717 00000-0 10270-3 0 9081
2 25544 51
6417 102
1814 0002660 119
3879 240
7550 15
73663018 31664
Satellite: ISS
Catalog Number: 25544
Epoch time: 11109
48986586 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 102
1814 deg
Eccentricity:
0002660
Arg of perigee: 119
3879 deg
Mean anomaly: 240
7550 deg
Mean motion: 15
73663018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3166
Checksum: 319
Coasting Arc #10 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2011/110/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -24603
91 A = 6732477
90 meter
Y = -6654694
14 meter E =
0016345
Z = 967849
74 I = 52
00111
XDOT = 4789
157885 Wp = 124
00224
YDOT = -894
602738 meter/sec RA = 96
31242 deg
ZDOT = -5967
019780 TA = 45
47426
MA = 45
34084
Ha = 191
373 n
mi
Hp = 183
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -80721
49 X = 45110
28
Y = -21832986
02 feet Y = -6654579
50 meter
Z = 3175360
02 Z = 967899
43
XDOT = 15712
460253 XDOT = 4827
792609
YDOT = -2935
048353 feet/sec YDOT = -840
831348 meter/sec
ZDOT = -19576
836548 ZDOT = -5943
659944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6629325
88 X = -2020618
53
Y = -20802292
48 feet Y = -6340538
75 meter
Z = 3175747
43 Z = 967967
82
XDOT = 12708
258005 XDOT = 3873
477040
YDOT = -7055
331232 feet/sec YDOT = -2150
464960 meter/sec
ZDOT = -19482
294841 ZDOT = -5938
203467
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 11110
50588449
00016717 00000-0 10270-3 0 9093
2 25544 51
6415 96
9656 0002655 120
6350 239
5075 15
73752576 31823
Satellite: ISS
Catalog Number: 25544
Epoch time: 11110
50588449 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 96
9656 deg
Eccentricity:
0002655
Arg of perigee: 120
6350 deg
Mean anomaly: 239
5075 deg
Mean motion: 15
73752576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 320
Coasting Arc #11 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2011/111/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4086029
08 A = 6721126
97 meter
Y = 1231118
41 meter E =
0006550
Z = 5188599
86 I = 51
96530
XDOT = -767
719675 Wp = 125
26050
YDOT = -7573
578454 meter/sec RA = 91
22215 deg
ZDOT = 1187
687309 TA = 313
42555
MA = 313
48004
Ha = 191
355 n
mi
Hp = 183
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13405607
21 X = -4124697
46
Y = 4039102
41 feet Y = 1185209
59 meter
Z = 17022965
42 Z = 5168655
90
XDOT = -2518
765338 XDOT = -688
743027
YDOT = -24847
698340 feet/sec YDOT = -7581
722017 meter/sec
ZDOT = 3896
611907 ZDOT = 1184
149292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11541563
50 X = -3517868
55
Y = 8096868
38 feet Y = 2467925
48 meter
Z = 16942226
51 Z = 5163990
64
XDOT = -9664
781313 XDOT = -2945
825344
YDOT = -21933
196825 feet/sec YDOT = -6685
238392 meter/sec
ZDOT = 3882
523396 ZDOT = 1183
393131
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 11111
52185984
00016717 00000-0 10270-3 0 9105
2 25544 51
6412 91
7500 0002562 126
5637 233
5762 15
73799861 31983
Satellite: ISS
Catalog Number: 25544
Epoch time: 11111
52185984 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 91
7500 deg
Eccentricity:
0002562
Arg of perigee: 126
5637 deg
Mean anomaly: 233
5762 deg
Mean motion: 15
73799861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 312
Coasting Arc #12 (Orbit 3212)
---------------------------------------
Vector Time (GMT): 2011/112/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1291083
19 A = 6731949
11 meter
Y = 6515217
29 meter E =
0009889
Z = -1080512
70 I = 52
00240
XDOT = -4523
309505 Wp = 54
13517
YDOT = 1874
317528 meter/sec RA = 86
09267 deg
ZDOT = 5940
104626 TA = 294
10792
MA = 294
21133
Ha = 191
103 n
mi
Hp = 183
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4235837
25 X = 1223381
78
Y = 21375384
81 feet Y = 6529276
47 meter
Z = -3544989
19 Z = -1074404
82
XDOT = -14840
254281 XDOT = -4572
788331
YDOT = 6149
335722 feet/sec YDOT = 1823
458279 meter/sec
ZDOT = 19488
532236 ZDOT = 5918
010208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11110620
77 X = 3386517
21
Y = 18750377
95 feet Y = 5715115
20 meter
Z = -3520479
30 Z = -1073042
09
XDOT = -10700
023446 XDOT = -3261
367146
YDOT = 9955
787560 feet/sec YDOT = 3034
524048 meter/sec
ZDOT = 19399
062318 ZDOT = 5912
834194
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 11112
47429600
00016717 00000-0 10270-3 0 9117
2 25544 51
6414 86
8609 0002759 130
7955 229
3448 15
73901815 32134
Satellite: ISS
Catalog Number: 25544
Epoch time: 11112
47429600 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 86
8609 deg
Eccentricity:
0002759
Arg of perigee: 130
7955 deg
Mean anomaly: 229
3448 deg
Mean motion: 15
73901815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3213
Checksum: 305
Coasting Arc #13 (Orbit 3228)
---------------------------------------
Vector Time (GMT): 2011/113/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3796872
59 A = 6720789
21 meter
Y = -1987616
25 meter E =
0015932
Z = -5190767
75 I = 51
96203
XDOT = 2130
580882 Wp = 88
08300
YDOT = 7284
345946 meter/sec RA = 81
00181 deg
ZDOT = -1233
541345 TA = 170
17978
MA = 170
14860
Ha = 190
967 n
mi
Hp = 183
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12456931
08 X = 3844032
09
Y = -6521050
69 feet Y = -1944893
49 meter
Z = -17030077
93 Z = -5172208
07
XDOT = 6990
094758 XDOT = 2054
959898
YDOT = 23898
772790 feet/sec YDOT = 7307
748608 meter/sec
ZDOT = -4047
051656 ZDOT = -1223
374477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9502974
19 X = 2896506
53
Y = -10485589
90 feet Y = -3196007
80 meter
Z = -16954901
20 Z = -5167853
88
XDOT = 14130
046998 XDOT = 4306
838325
YDOT = 19269
272267 feet/sec YDOT = 5873
274187 meter/sec
ZDOT = -4006
147781 ZDOT = -1221
073844
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 11113
49018513
00016717 00000-0 10270-3 0 9128
2 25544 51
6416 81
6439 0002578 134
5901 225
5473 15
73932140 32290
Satellite: ISS
Catalog Number: 25544
Epoch time: 11113
49018513 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 81
6439 deg
Eccentricity:
0002578
Arg of perigee: 134
5901 deg
Mean anomaly: 225
5473 deg
Mean motion: 15
73932140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3229
Checksum: 292
Coasting Arc #14 (Orbit 3244)
---------------------------------------
Vector Time (GMT): 2011/114/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2411594
02 A = 6731634
79 meter
Y = -6186078
12 meter E =
0016139
Z = 1060165
73 I = 51
99375
XDOT = 4127
852708 Wp = 125
79766
YDOT = -2637
433279 meter/sec RA = 75
87010 deg
ZDOT = -5946
317445 TA = 42
65880
MA = 42
53359
Ha = 190
761 n
mi
Hp = 183
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7912053
86 X = -2347390
95
Y = -20295531
89 feet Y = -6212687
06 meter
Z = 3478234
03 Z = 1048606
12
XDOT = 13542
823844 XDOT = 4185
924239
YDOT = -8652
996322 feet/sec YDOT = -2590
948356 meter/sec
ZDOT = -19508
915503 ZDOT = -5926
123380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14779097
51 X = -4504668
92
Y = -16012785
38 feet Y = -4880696
99 meter
Z = 3431662
00 Z = 1045970
58
XDOT = 8402
225269 XDOT = 2560
998262
YDOT = -11956
294105 feet/sec YDOT = -3644
278443 meter/sec
ZDOT = -19427
096165 ZDOT = -5921
378911
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 11114
50602832
00016717 00000-0 10270-3 0 9135
2 25544 51
6419 76
4274 0002435 138
4997 221
6351 15
74024832 32453
Satellite: ISS
Catalog Number: 25544
Epoch time: 11114
50602832 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 76
4274 deg
Eccentricity:
0002435
Arg of perigee: 138
4997 deg
Mean anomaly: 221
6351 deg
Mean motion: 15
74024832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 292
Coasting Arc #15 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2011/115/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3398670
54 A = 6720281
92 meter
Y = 2583858
18 meter E =
0006279
Z = 5186639
82 I = 51
94775
XDOT = -3366
667388 Wp = 132
26246
YDOT = -6826
936381 meter/sec RA = 70
77829 deg
ZDOT = 1189
882675 TA = 306
39783
MA = 306
45573
Ha = 190
680 n
mi
Hp = 183
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11150493
89 X = -3452506
80
Y = 8477224
99 feet Y = 2545551
19 meter
Z = 17016534
84 Z = 5169998
36
XDOT = -11045
496681 XDOT = -3295
857274
YDOT = -22398
085240 feet/sec YDOT = -6864
188572 meter/sec
ZDOT = 3903
814549 ZDOT = 1173
699501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7184643
14 X = -2189879
23
Y = 12118932
54 feet Y = 3693850
64 meter
Z = 16949091
20 Z = 5166083
00
XDOT = -17868
403881 XDOT = -5446
289503
YDOT = -15984
875315 feet/sec YDOT = -4872
189996 meter/sec
ZDOT = 3838
556956 ZDOT = 1169
992160
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 11115
52182604
00016717 00000-0 10270-3 0 9149
2 25544 51
6420 71
2113 0002420 145
7002 214
4318 15
74092796 32617
Satellite: ISS
Catalog Number: 25544
Epoch time: 11115
52182604 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 71
2113 deg
Eccentricity:
0002420
Arg of perigee: 145
7002 deg
Mean anomaly: 214
4318 deg
Mean motion: 15
74092796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 260
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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