[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 2nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
182/12:31:21
741 2
0 4
2 4
3
N/A 2
9 -0
0 210
4
000/00:30:43
483 -2
4 -0
9 208
5
Coasting Arc #1 (Orbit 288)
---------------------------------------
Vector Time (GMT): 2011/180/20:18:28
120
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 336430
44 A = 6769639
90 meter
Y = -6739935
71 meter E =
0006311
Z = 482210
71 I = 51
99957
XDOT = 4754
803027 Wp = 158
75897
YDOT = -195
095225 meter/sec RA = 96
05801 deg
ZDOT = -6025
436572 TA = 16
05157
MA = 16
03158
Ha = 209
124 n
mi
Hp = 207
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1103774
39 X = 409430
22
Y = -22112649
96 feet Y = -6735765
47 meter
Z = 1582056
13 Z = 484021
10
XDOT = 15599
747463 XDOT = 4785
901521
YDOT = -640
076199 feet/sec YDOT = -141
749094 meter/sec
ZDOT = -19768
492690 ZDOT = -6002
262380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13800391
57 X = 4206359
35
Y = 17312203
07 feet Y = 5276759
50 meter
Z = 1589756
35 Z = 484557
73
XDOT = -10105
378552 XDOT = -3080
119383
YDOT = 9867
789623 feet/sec YDOT = 3007
702277 meter/sec
ZDOT = -19674
385419 ZDOT = -5996
752676
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 11180
87910994
00016717 00000-0 10270-3 0 9005
2 25544 51
6376 96
7154 0008059 287
7390 72
2886 15
60891510 2898
Satellite: ISS
Catalog Number: 25544
Epoch time: 11180
87910994 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 96
7154 deg
Eccentricity:
0008059
Arg of perigee: 287
7390 deg
Mean anomaly: 72
2886 deg
Mean motion: 15
60891510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 289
Checksum: 337
Coasting Arc #2 (Orbit 304)
---------------------------------------
Vector Time (GMT): 2011/181/20:18:28
120
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2643044
58 A = 6765243
32 meter
Y = 5304998
11 meter E =
0006264
Z = 3253601
88 I = 51
98831
XDOT = -3655
779071 Wp = 57
55213
YDOT = -4761
623652 meter/sec RA = 91
07489 deg
ZDOT = 4790
674544 TA = 340
09269
MA = 340
11712
Ha = 209
316 n
mi
Hp = 207
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8671406
11 X = -2717974
89
Y = 17404849
45 feet Y = 5275022
40 meter
Z = 10674546
87 Z = 3240581
12
XDOT = -11994
025825 XDOT = -3625
533942
YDOT = -15622
124841 feet/sec YDOT = -4802
336597 meter/sec
ZDOT = 15717
436168 ZDOT = 4772
987519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5278809
46 X = -1608981
12
Y = -18745352
95 feet Y = -5713583
58 meter
Z = 10621390
32 Z = 3237399
77
XDOT = 18091
944462 XDOT = 5514
424672
YDOT = 3776
726349 feet/sec YDOT = 1151
146191 meter/sec
ZDOT = 15645
865350 ZDOT = 4768
859759
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 11181
90349391
00016717 00000-0 10270-3 0 9018
2 25544 51
6389 91
5563 0007968 290
2496 69
7803 15
60896608 3055
Satellite: ISS
Catalog Number: 25544
Epoch time: 11181
90349391 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 91
5563 deg
Eccentricity:
0007968
Arg of perigee: 290
2496 deg
Mean anomaly: 69
7803 deg
Mean motion: 15
60896608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 305
Checksum: 337
Coasting Arc #3 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2011/182/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3851649
90 A = 6763605
15 meter
Y = 2862208
31 meter E =
0002458
Z = -4767329
47 I = 51
97367
XDOT = -1821
084158 Wp = 184
25351
YDOT = 6951
136992 meter/sec RA = 87
59547 deg
ZDOT = 2699
543697 TA = 112
27579
MA = 112
24973
Ha = 210
373 n
mi
Hp = 208
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12636646
66 X = 3842516
37
Y = 9390447
21 feet Y = 2905229
61 meter
Z = -15640844
71 Z = -4748640
07
XDOT = -5974
685558 XDOT = -1911
791476
YDOT = 22805
567558 feet/sec YDOT = 6930
264853 meter/sec
ZDOT = 8856
770661 ZDOT = 2690
477945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4437811
42 X = 1352644
92
Y = -15183374
20 feet Y = -4627892
46 meter
Z = -15565100
02 Z = -4744242
49
XDOT = 22380
583162 XDOT = 6821
601748
YDOT = -2508
266797 feet/sec YDOT = -764
519720 meter/sec
ZDOT = 8819
580178 ZDOT = 2688
208038
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 11182
54374168
00016717 00000-0 10270-3 0 9020
2 25544 51
6416 88
3378 0010821 276
1134 83
8789 15
59686676 3159
Satellite: ISS
Catalog Number: 25544
Epoch time: 11182
54374168 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 88
3378 deg
Eccentricity:
0010821
Arg of perigee: 276
1134 deg
Mean anomaly: 83
8789 deg
Mean motion: 15
59686676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 333
Coasting Arc #4 (Orbit 330)
---------------------------------------
Vector Time (GMT): 2011/183/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2532197
99 A = 6771148
38 meter
Y = -5861519
85 meter E =
0003706
Z = 2246569
97 I = 51
99622
XDOT = 3833
170406 Wp = 135
11232
YDOT = -3759
258130 meter/sec RA = 82
59330 deg
ZDOT = -5484
825734 TA = 19
97664
MA = 19
96214
Ha = 210
586 n
mi
Hp = 208
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8307736
18 X = -2477378
38
Y = -19230708
15 feet Y = -5889530
29 meter
Z = 7370636
37 Z = 2234400
94
XDOT = 12576
018393 XDOT = 3901
566086
YDOT = -12333
524047 feet/sec YDOT = -3716
009949 meter/sec
ZDOT = -17994
835084 ZDOT = -5466
039015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14933167
13 X = -4551629
34
Y = 14715997
03 feet Y = 4485435
90 meter
Z = 7321533
17 Z = 2231603
31
XDOT = -15001
100715 XDOT = -4572
335498
YDOT = -6302
904426 feet/sec YDOT = -1921
125269 meter/sec
ZDOT = -17918
330177 ZDOT = -5461
507038
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 11183
56890731
00016717 00000-0 10270-3 0 9033
2 25544 51
6414 83
1846 0010729 279
6830 80
3114 15
59667753 3315
Satellite: ISS
Catalog Number: 25544
Epoch time: 11183
56890731 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 83
1846 deg
Eccentricity:
0010729
Arg of perigee: 279
6830 deg
Mean anomaly: 80
3114 deg
Mean motion: 15
59667753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 331
Checksum: 312
Coasting Arc #5 (Orbit 346)
---------------------------------------
Vector Time (GMT): 2011/184/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 444012
48 A = 6772506
42 meter
Y = 6631790
51 meter E =
0009867
Z = 1264589
76 I = 51
99622
XDOT = -4876
951680 Wp = 7
07180
YDOT = -793
532394 meter/sec RA = 77
61992 deg
ZDOT = 5878
506184 TA = 6
64959
MA = 6
63651
Ha = 211
053 n
mi
Hp = 208
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1456733
85 X = 363678
49
Y = 21757842
89 feet Y = 6636306
38 meter
Z = 4148916
54 Z = 1266552
57
XDOT = -16000
497637 XDOT = -4896
271941
YDOT = -2603
452735 feet/sec YDOT = -848
178313 meter/sec
ZDOT = 19286
437610 ZDOT = 5854
767367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19622396
44 X = 5980906
43
Y = -9509162
99 feet Y = -2898392
88 meter
Z = 4156523
38 Z = 1266908
33
XDOT = 2955
860534 XDOT = 900
946291
YDOT = 14480
893575 feet/sec YDOT = 4413
776362 meter/sec
ZDOT = 19190
063569 ZDOT = 5849
131376
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 11184
59406492
00016717 00000-0 10270-3 0 9045
2 25544 51
6415 78
0300 0010929 284
3427 75
6515 15
59697486 3476
Satellite: ISS
Catalog Number: 25544
Epoch time: 11184
59406492 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 78
0300 deg
Eccentricity:
0010929
Arg of perigee: 284
3427 deg
Mean anomaly: 75
6515 deg
Mean motion: 15
59697486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 347
Checksum: 325
Coasting Arc #6 (Orbit 361)
---------------------------------------
Vector Time (GMT): 2011/185/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1911503
21 A = 6765625
72 meter
Y = -4935442
79 meter E =
0006808
Z = -4215825
45 I = 51
96539
XDOT = 4572
038881 Wp = 333
35657
YDOT = 4933
977470 meter/sec RA = 72
62859 deg
ZDOT = -3694
933366 TA = 258
92496
MA = 259
00154
Ha = 211
321 n
mi
Hp = 208
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6271335
99 X = 1987029
54
Y = -16192397
62 feet Y = -4913644
40 meter
Z = -13831448
34 Z = -4206356
70
XDOT = 15000
127561 XDOT = 4534
475358
YDOT = 16187
590125 feet/sec YDOT = 4984
895211 meter/sec
ZDOT = -12122
484796 ZDOT = -3672
813464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17387996
40 X = -5299861
30
Y = 500968
94 feet Y = 152695
33 meter
Z = -13792714
39 Z = -4204019
35
XDOT = 9020
596580 XDOT = 2749
477838
YDOT = -18943
234793 feet/sec YDOT = -5773
897965 meter/sec
ZDOT = -12032
913516 ZDOT = -3667
632040
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 11185
55514525
00016717 00000-0 10270-3 0 9050
2 25544 51
6411 73
1985 0011090 287
7162 72
2782 15
59704226 3627
Satellite: ISS
Catalog Number: 25544
Epoch time: 11185
55514525 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 73
1985 deg
Eccentricity:
0011090
Arg of perigee: 287
7162 deg
Mean anomaly: 72
2782 deg
Mean motion: 15
59704226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 301
Coasting Arc #7 (Orbit 377)
---------------------------------------
Vector Time (GMT): 2011/186/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3903296
15 A = 6761112
44 meter
Y = 1474562
94 meter E =
0008919
Z = 5326811
90 I = 51
94046
XDOT = -2844
941869 Wp = 298
55721
YDOT = -7124
341219 meter/sec RA = 67
59734 deg
ZDOT = -108
500360 TA = 152
49556
MA = 152
44833
Ha = 211
662 n
mi
Hp = 208
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12806089
72 X = -3945371
14
Y = 4837804
91 feet Y = 1430678
11 meter
Z = 17476417
01 Z = 5307747
96
XDOT = -9333
798784 XDOT = -2764
537599
YDOT = -23373
822897 feet/sec YDOT = -7155
705514 meter/sec
ZDOT = -355
972309 ZDOT = -122
126281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9682211
08 X = 2951137
94
Y = 9816236
56 feet Y = 2991988
90 meter
Z = 17398900
26 Z = 5303184
80
XDOT = -16822
425850 XDOT = -5127
475399
YDOT = 17344
543674 feet/sec YDOT = 5286
616912 meter/sec
ZDOT = -410
917749 ZDOT = -125
247730
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 11186
58029250
00016717 00000-0 10270-3 0 9061
2 25544 51
6412 68
0441 0010997 291
6760 68
3224 15
59724491 3781
Satellite: ISS
Catalog Number: 25544
Epoch time: 11186
58029250 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 68
0441 deg
Eccentricity:
0010997
Arg of perigee: 291
6760 deg
Mean anomaly: 68
3224 deg
Mean motion: 15
59724491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 378
Checksum: 316
Coasting Arc #8 (Orbit 392)
---------------------------------------
Vector Time (GMT): 2011/187/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4837436
04 A = 6766009
00 meter
Y = 2355460
46 meter E =
0003949
Z = -4098022
08 I = 51
94362
XDOT = 39
453351 Wp = 307
20615
YDOT = 6636
930643 meter/sec RA = 62
56625 deg
ZDOT = 3861
129144 TA = 2
48381
MA = 2
48185
Ha = 211
972 n
mi
Hp = 208
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15870853
13 X = 4830644
48
Y = 7727888
66 feet Y = 2409518
01 meter
Z = -13444954
32 Z = -4074538
40
XDOT = 129
440129 XDOT = -53
521446
YDOT = 21774
706835 feet/sec YDOT = 6636
851636 meter/sec
ZDOT = 12667
746537 ZDOT = 3861
095572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 247333
58 X = 75387
27
Y = -17722733
73 feet Y = -5401889
24 meter
Z = -13349703
16 Z = -4068989
52
XDOT = 18412
641774 XDOT = 5612
173213
YDOT = -9285
208345 feet/sec YDOT = -2830
131504 meter/sec
ZDOT = 12667
231311 ZDOT = 3860
972104
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 11187
54136264
00016717 00000-0 10270-3 0 9073
2 25544 51
6404 63
2113 0011147 295
2681 64
7319 15
59732828 3930
Satellite: ISS
Catalog Number: 25544
Epoch time: 11187
54136264 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 63
2113 deg
Eccentricity:
0011147
Arg of perigee: 295
2681 deg
Mean anomaly: 64
7319 deg
Mean motion: 15
59732828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 393
Checksum: 307
Coasting Arc #9 (Orbit 408)
---------------------------------------
Vector Time (GMT): 2011/188/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4262351
79 A = 6772650
09 meter
Y = -5151560
51 meter E =
0002767
Z = 1067619
15 I = 51
95116
XDOT = 3086
845364 Wp = 142
18827
YDOT = -3782
196491 meter/sec RA = 57
57498 deg
ZDOT = -5920
307962 TA = 26
26150
MA = 26
24747
Ha = 212
107 n
mi
Hp = 208
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13984093
81 X = -4209615
52
Y = -16901445
23 feet Y = -5198929
95 meter
Z = 3502687
51 Z = 1047040
45
XDOT = 10127
445419 XDOT = 3157
668734
YDOT = -12408
781137 feet/sec YDOT = -3747
280973 meter/sec
ZDOT = -19423
582554 ZDOT = -5905
140510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9039996
79 X = -2755391
02
Y = 20001717
28 feet Y = 6096523
43 meter
Z = 3419402
63 Z = 1042233
92
XDOT = -14188
067872 XDOT = -4324
523087
YDOT = -3099
033976 feet/sec YDOT = -944
585556 meter/sec
ZDOT = -19361
755808 ZDOT = -5901
463170
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 11188
56649953
00016717 00000-0 10270-3 0 9081
2 25544 51
6406 58
0578 0011050 299
2440 60
7610 15
59722513 4097
Satellite: ISS
Catalog Number: 25544
Epoch time: 11188
56649953 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 58
0578 deg
Eccentricity:
0011050
Arg of perigee: 299
2440 deg
Mean anomaly: 60
7610 deg
Mean motion: 15
59722513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 409
Checksum: 312
Coasting Arc #10 (Orbit 424)
---------------------------------------
Vector Time (GMT): 2011/189/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2135791
52 A = 6770452
23 meter
Y = 5936467
79 meter E =
0010411
Z = 2437397
94 I = 51
92645
XDOT = -5480
763920 Wp = 21
15430
YDOT = -234
491652 meter/sec RA = 52
59633 deg
ZDOT = 5376
041775 TA = 6
09004
MA = 6
07739
Ha = 212
308 n
mi
Hp = 207
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7007190
03 X = 2057409
67
Y = 19476600
37 feet Y = 5959913
00 meter
Z = 7996712
42 Z = 2447583
81
XDOT = -17981
508923 XDOT = -5503
850155
YDOT = -769
329568 feet/sec YDOT = -295
910538 meter/sec
ZDOT = 17637
932332 ZDOT = 5349
360248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14189988
99 X = 4325108
64
Y = -15047431
94 feet Y = -4586457
25 meter
Z = 8037729
04 Z = 2449899
81
XDOT = 6434
702884 XDOT = 1961
297439
YDOT = 15427
525018 feet/sec YDOT = 4702
309625 meter/sec
ZDOT = 17529
574193 ZDOT = 5343
014214
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 11189
59162862
00016717 00000-0 10270-3 0 9095
2 25544 51
6400 52
9023 0011256 302
7668 57
2402 15
59757602 4254
Satellite: ISS
Catalog Number: 25544
Epoch time: 11189
59162862 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 52
9023 deg
Eccentricity:
0011256
Arg of perigee: 302
7668 deg
Mean anomaly: 57
2402 deg
Mean motion: 15
59757602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 425
Checksum: 303
Coasting Arc #11 (Orbit 439)
---------------------------------------
Vector Time (GMT): 2011/190/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 954598
34 A = 6762983
34 meter
Y = -4610058
80 meter E =
0010491
Z = -4861174
95 I = 51
88113
XDOT = 6150
117260 Wp = 12
38946
YDOT = 3873
663213 meter/sec RA = 47
58481 deg
ZDOT = -2456
830713 TA = 233
54419
MA = 233
64093
Ha = 212
552 n
mi
Hp = 207
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3131884
33 X = 1029692
60
Y = -15124864
81 feet Y = -4598963
40 meter
Z = -15948736
72 Z = -4856355
72
XDOT = 20177
550066 XDOT = 6118
278917
YDOT = 12708
868810 feet/sec YDOT = 3942
259864 meter/sec
ZDOT = -8060
468218 ZDOT = -2427
030369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14870170
25 X = -4532427
89
Y = 4252210
69 feet Y = 1296073
82 meter
Z = -15928878
77 Z = -4855122
25
XDOT = 2033
984521 XDOT = 619
958482
YDOT = -22740
214043 feet/sec YDOT = -6931
217240 meter/sec
ZDOT = -7939
666987 ZDOT = -2420
010498
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 11190
55268403
00016717 00000-0 10270-3 0 9103
2 25544 51
6389 48
0702 0011225 306
6180 53
3943 15
59749284 4409
Satellite: ISS
Catalog Number: 25544
Epoch time: 11190
55268403 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 48
0702 deg
Eccentricity:
0011225
Arg of perigee: 306
6180 deg
Mean anomaly: 53
3943 deg
Mean motion: 15
59749284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 440
Checksum: 296
Coasting Arc #12 (Orbit 455)
---------------------------------------
Vector Time (GMT): 2011/191/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4015035
21 A = 6761861
45 meter
Y = 1796256
31 meter E =
0011045
Z = 5142020
17 I = 51
85669
XDOT = -4640
169780 Wp = 335
10459
YDOT = -5910
288947 meter/sec RA = 42
54206 deg
ZDOT = -1549
971606 TA = 129
82847
MA = 129
73122
Ha = 212
801 n
mi
Hp = 207
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13172687
69 X = -4059801
79
Y = 5893229
36 feet Y = 1751106
65 meter
Z = 16870144
93 Z = 5122406
74
XDOT = -15223
654133 XDOT = -4566
205465
YDOT = -19390
711768 feet/sec YDOT = -5961
764354 meter/sec
ZDOT = -5085
208680 ZDOT = -1572
334711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11588763
26 X = 3532255
04
Y = 8754187
23 feet Y = 2668276
27 meter
Z = 16790366
74 Z = 5117703
78
XDOT = -8959
860914 XDOT = -2730
965607
YDOT = 21842
049516 feet/sec YDOT = 6657
456693 meter/sec
ZDOT = -5175
667882 ZDOT = -1577
543571
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 11191
57780383
00016717 00000-0 10270-3 0 9113
2 25544 51
6396 42
9159 0011226 310
2041 49
8131 15
59750922 4561
Satellite: ISS
Catalog Number: 25544
Epoch time: 11191
57780383 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 42
9159 deg
Eccentricity:
0011226
Arg of perigee: 310
2041 deg
Mean anomaly: 49
8131 deg
Mean motion: 15
59750922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 456
Checksum: 298
Coasting Arc #13 (Orbit 470)
---------------------------------------
Vector Time (GMT): 2011/192/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5828065
96 A = 6768829
64 meter
Y = 1354667
58 meter E =
0009579
Z = -3151222
27 I = 51
85610
XDOT = 1280
924867 Wp = 336
98826
YDOT = 5802
461230 meter/sec RA = 37
51687 deg
ZDOT = 4867
056142 TA = 346
67670
MA = 346
70198
Ha = 213
012 n
mi
Hp = 207
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19120951
30 X = 5827792
60
Y = 4444447
43 feet Y = 1419839
57 meter
Z = -10338655
75 Z = -3122910
16
XDOT = 4202
509405 XDOT = 1192
302315
YDOT = 19036
946294 feet/sec YDOT = 5816
288962 meter/sec
ZDOT = 15968
031961 ZDOT = 4873
064562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5734658
99 X = -1747924
06
Y = -18837208
86 feet Y = -5741581
26 meter
Z = -10223744
08 Z = -3116197
19
XDOT = 13065
974177 XDOT = 3982
508929
YDOT = -12650
725046 feet/sec YDOT = -3855
940994 meter/sec
ZDOT = 15992
061546 ZDOT = 4874
380359
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 11192
53884851
00016717 00000-0 10270-3 0 9126
2 25544 51
6384 38
0826 0011183 313
7640 46
2590 15
59768753 4718
Satellite: ISS
Catalog Number: 25544
Epoch time: 11192
53884851 = yrday
fracday
Element set: 912
Inclination: 51
6384 deg
RA of node: 38
0826 deg
Eccentricity:
0011183
Arg of perigee: 313
7640 deg
Mean anomaly: 46
2590 deg
Mean motion: 15
59768753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 471
Checksum: 318
Coasting Arc #14 (Orbit 486)
---------------------------------------
Vector Time (GMT): 2011/193/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5601558
37 A = 6772837
35 meter
Y = -3799339
85 meter E =
0000379
Z = -243179
32 I = 51
84554
XDOT = 2840
988477 Wp = 88
49091
YDOT = -3803
416811 meter/sec RA = 32
53019 deg
ZDOT = -6026
218861 TA = 94
12615
MA = 94
12182
Ha = 213
117 n
mi
Hp = 206
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18377816
16 X = -5557475
78
Y = -12465025
75 feet Y = -3861733
36 meter
Z = -797832
43 Z = -270284
98
XDOT = 9320
828337 XDOT = 2912
581800
YDOT = -12478
401610 feet/sec YDOT = -3771
245772 meter/sec
ZDOT = -19771
059255 ZDOT = -6012
244283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1237181
39 X = -377092
89
Y = 22167611
97 feet Y = 6756688
13 meter
Z = -907685
08 Z = -276662
41
XDOT = -13941
003041 XDOT = -4249
217727
YDOT = -1584
319201 feet/sec YDOT = -482
900493 meter/sec
ZDOT = -19714
044239 ZDOT = -6008
840684
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 11193
56395676
00016717 00000-0 10270-3 0 9133
2 25544 51
6386 32
9289 0011329 318
4124 41
6169 15
59805830 4873
Satellite: ISS
Catalog Number: 25544
Epoch time: 11193
56395676 = yrday
fracday
Element set: 913
Inclination: 51
6386 deg
RA of node: 32
9289 deg
Eccentricity:
0011329
Arg of perigee: 318
4124 deg
Mean anomaly: 41
6169 deg
Mean motion: 15
59805830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 487
Checksum: 330
Coasting Arc #15 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2011/194/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3201471
80 A = 6767515
09 meter
Y = 4798654
01 meter E =
0009576
Z = 3526529
74 I = 51
80079
XDOT = -6163
042837 Wp = 31
58514
YDOT = 794
600564 meter/sec RA = 27
53576 deg
ZDOT = 4516
174014 TA = 9
99848
MA = 9
97944
Ha = 213
181 n
mi
Hp = 206
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10503516
41 X = 3130443
43
Y = 15743615
53 feet Y = 4834057
06 meter
Z = 11569979
45 Z = 3541910
54
XDOT = -20219
956813 XDOT = -6193
408544
YDOT = 2606
957231 feet/sec YDOT = 725
511094 meter/sec
ZDOT = 14816
843878 ZDOT = 4486
160837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7838855
90 X = 2389283
28
Y = -17184160
84 feet Y = -5237732
23 meter
Z = 11632139
34 Z = 3545476
07
XDOT = 11705
496856 XDOT = 3567
835442
YDOT = 15281
377926 feet/sec YDOT = 4657
763992 meter/sec
ZDOT = 14694
873510 ZDOT = 4478
997446
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 11194
58905982
00016717 00000-0 10270-3 0 9144
2 25544 51
6376 27
7731 0011179 321
1078 38
9273 15
59800540 5035
Satellite: ISS
Catalog Number: 25544
Epoch time: 11194
58905982 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 27
7731 deg
Eccentricity:
0011179
Arg of perigee: 321
1078 deg
Mean anomaly: 38
9273 deg
Mean motion: 15
59800540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 313
Coasting Arc #16 (Orbit 517)
---------------------------------------
Vector Time (GMT): 2011/195/12:46:43
483
Vector Time (MET): N/A
Weight (LBS) : 898465
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 538752
18 A = 6761204
05 meter
Y = -4248320
86 meter E =
0013637
Z = -5240666
37 I = 51
75210
XDOT = 7289
929972 Wp = 36
10210
YDOT = 2167
783040 meter/sec RA = 22
50061 deg
ZDOT = -998
437473 TA = 224
30299
MA = 224
41222
Ha = 213
399 n
mi
Hp = 206
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1767559
65 X = 611675
35
Y = -13938060
57 feet Y = -4241887
61 meter
Z = -17193787
30 Z = -5237872
73
XDOT = 23917
093085 XDOT = 7269
997724
YDOT = 7112
149082 feet/sec YDOT = 2249
192188 meter/sec
ZDOT = -3275
713495 ZDOT = -963
071801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12716265
34 X = -3875917
68
Y = 6007515
47 feet Y = 1831090
72 meter
Z = -17182155
70 Z = -5237121
06
XDOT = -6605
566313 XDOT = -2013
376612
YDOT = -23029
275666 feet/sec YDOT = -7019
323223 meter/sec
ZDOT = -3132
193767 ZDOT = -954
692660
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 11195
55009007
00016717 00000-0 10270-3 0 9156
2 25544 51
6375 22
9408 0011022 325
7525 34
2919 15
59797346 5187
Satellite: ISS
Catalog Number: 25544
Epoch time: 11195
55009007 = yrday
fracday
Element set: 915
Inclination: 51
6375 deg
RA of node: 22
9408 deg
Eccentricity:
0011022
Arg of perigee: 325
7525 deg
Mean anomaly: 34
2919 deg
Mean motion: 15
59797346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 518
Checksum: 307
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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