[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 19th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
032/21:57:47
723 3
1 4
9 4
9
N/A 0
2 -0
0 219
3
000/00:01:35
445 -3
8 -0
1 205
4
Coasting Arc #1 (Orbit 3451)
---------------------------------------
Vector Time (GMT): 2012/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5272355
10 A = 6768912
01 meter
Y = 1232534
42 meter E =
0017445
Z = -4058815
51 I = 51
76851
XDOT = -4203
666456 Wp = 310
03867
YDOT = 5114
091457 meter/sec RA = 156
96121 deg
ZDOT = -3885
529535 TA = 279
74214
MA = 279
93911
Ha = 216
338 n
mi
Hp = 205
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17297752
95 X = 5277897
48
Y = 4043748
08 feet Y = 1291524
47 meter
Z = -13316323
86 Z = -4033189
24
XDOT = -13791
556613 XDOT = -4241
665917
YDOT = 16778
515278 feet/sec YDOT = 5066
871340 meter/sec
ZDOT = -12747
800313 ZDOT = -3906
042491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4140120
04 X = 1261908
59
Y = 17355269
47 feet Y = 5289886
13 meter
Z = -13211459
59 Z = -4026852
88
XDOT = -19869
781676 XDOT = -6056
309455
YDOT = -5083
694816 feet/sec YDOT = -1549
510180 meter/sec
ZDOT = -12832
129629 ZDOT = -3911
233111
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 12018
52321094
00016717 00000-0 10270-3 0 9005
2 25544 51
6393 157
8680 0022075 293
8988 65
9855 15
58785177 34523
Satellite: ISS
Catalog Number: 25544
Epoch time: 12018
52321094 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 157
8680 deg
Eccentricity:
0022075
Arg of perigee: 293
8988 deg
Mean anomaly: 65
9855 deg
Mean motion: 15
58785177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3452
Checksum: 342
Coasting Arc #2 (Orbit 3467)
---------------------------------------
Vector Time (GMT): 2012/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2436973
32 A = 6763813
24 meter
Y = -3435793
73 meter E =
0019363
Z = 5305976
73 I = 51
78007
XDOT = 6563
021787 Wp = 298
99325
YDOT = -3929
026356 meter/sec RA = 151
92885 deg
ZDOT = 480
624330 TA = 146
48991
MA = 146
36726
Ha = 216
483 n
mi
Hp = 205
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7995319
28 X = -2424147
42
Y = -11272289
15 feet Y = -3462974
27 meter
Z = 17408060
15 Z = 5294168
97
XDOT = 21532
223709 XDOT = 6604
134426
YDOT = -12890
506416 feet/sec YDOT = -3855
404785 meter/sec
ZDOT = 1576
851478 ZDOT = 512
606329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6257355
73 X = 1907242
03
Y = -12389867
57 feet Y = -3776431
64 meter
Z = 17359921
43 Z = 5291304
05
XDOT = 20468
233037 XDOT = 6238
717430
YDOT = 12682
215540 feet/sec YDOT = 3865
539297 meter/sec
ZDOT = 1708
094905 ZDOT = 520
627327
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 12019
54895879
00016717 00000-0 10270-3 0 9016
2 25544 51
6399 152
7171 0022125 297
9356 61
9559 15
58822429 34684
Satellite: ISS
Catalog Number: 25544
Epoch time: 12019
54895879 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 152
7171 deg
Eccentricity:
0022125
Arg of perigee: 297
9356 deg
Mean anomaly: 61
9559 deg
Mean motion: 15
58822429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3468
Checksum: 354
Coasting Arc #3 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2012/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -940825
15 A = 6766720
71 meter
Y = 4896712
28 meter E =
0012353
Z = -4562273
05 I = 51
81708
XDOT = -6856
972886 Wp = 311
15255
YDOT = 1564
504028 meter/sec RA = 146
89457 deg
ZDOT = 3095
744731 TA = 349
66670
MA = 349
69207
Ha = 216
684 n
mi
Hp = 205
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3086696
68 X = -973349
11
Y = 16065329
01 feet Y = 4886010
00 meter
Z = -14968087
42 Z = -4566921
97
XDOT = -22496
630202 XDOT = -6888
996041
YDOT = 5132
887231 feet/sec YDOT = 1487
645783 meter/sec
ZDOT = 10156
642819 ZDOT = 3062
356776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15548543
26 X = -4739195
99
Y = 5028442
47 feet Y = 1532669
26 meter
Z = -14987451
49 Z = -4568175
22
XDOT = -14903
858416 XDOT = -4542
696045
YDOT = -16244
821880 feet/sec YDOT = -4951
421709 meter/sec
ZDOT = 10019
772671 ZDOT = 3054
026710
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 12020
51057937
00016717 00000-0 10270-3 0 9021
2 25544 51
6404 147
8901 0022100 301
5345 58
3652 15
58844677 34830
Satellite: ISS
Catalog Number: 25544
Epoch time: 12020
51057937 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 147
8901 deg
Eccentricity:
0022100
Arg of perigee: 301
5345 deg
Mean anomaly: 58
3652 deg
Mean motion: 15
58844677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 295
Coasting Arc #4 (Orbit 3498)
---------------------------------------
Vector Time (GMT): 2012/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3857740
91 A = 6773609
01 meter
Y = -5152109
49 meter E =
0009449
Z = 2131069
33 I = 51
86583
XDOT = 5086
621429 Wp = 329
31923
YDOT = 1524
065486 meter/sec RA = 141
89091 deg
ZDOT = -5526
245616 TA = 187
12706
MA = 187
14050
Ha = 216
891 n
mi
Hp = 205
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12656630
30 X = 3904714
09
Y = -16903246
37 feet Y = -5108707
41 meter
Z = 6991697
27 Z = 2149923
29
XDOT = 16688
390514 XDOT = 5096
045654
YDOT = 5000
214848 feet/sec YDOT = 1581
000406 meter/sec
ZDOT = -18130
727087 ZDOT = -5501
512536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20921561
54 X = 6376891
96
Y = 2665971
67 feet Y = 812588
16 meter
Z = 7069279
81 Z = 2154716
49
XDOT = 4106
379711 XDOT = 1251
624536
YDOT = 15558
328423 feet/sec YDOT = 4742
178503 meter/sec
ZDOT = -18029
498276 ZDOT = -5495
391075
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 12021
53628867
00016717 00000-0 10270-3 0 9031
2 25544 51
6410 142
7399 0022069 305
4862 54
4234 15
58866175 34990
Satellite: ISS
Catalog Number: 25544
Epoch time: 12021
53628867 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 142
7399 deg
Eccentricity:
0022069
Arg of perigee: 305
4862 deg
Mean anomaly: 54
4234 deg
Mean motion: 15
58866175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3499
Checksum: 325
Coasting Arc #5 (Orbit 3514)
---------------------------------------
Vector Time (GMT): 2012/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5432479
12 A = 6774985
40 meter
Y = 3862305
67 meter E =
0022266
Z = 1135006
77 I = 51
89509
XDOT = -1973
899893 Wp = 345
89207
YDOT = -4499
748874 meter/sec RA = 136
91426 deg
ZDOT = 5909
767892 TA = 26
42537
MA = 26
31200
Ha = 217
198 n
mi
Hp = 205
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17823094
23 X = -5480777
91
Y = 12671606
53 feet Y = 3801286
21 meter
Z = 3723775
49 Z = 1108499
66
XDOT = -6476
049519 XDOT = -1952
143691
YDOT = -14762
955622 feet/sec YDOT = -4521
701023 meter/sec
ZDOT = 19389
002269 ZDOT = 5900
231531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19968794
61 X = -6086488
60
Y = -8959825
95 feet Y = -2730954
95 meter
Z = 3614908
65 Z = 1101824
16
XDOT = 8729
437652 XDOT = 2660
732596
YDOT = -11710
073393 feet/sec YDOT = -3569
230370 meter/sec
ZDOT = 19350
224942 ZDOT = 5897
948562
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 12022
56197767
00016717 00000-0 10270-3 0 9046
2 25544 51
6422 137
5894 0022106 309
8887 50
0324 15
58899645 35151
Satellite: ISS
Catalog Number: 25544
Epoch time: 12022
56197767 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 137
5894 deg
Eccentricity:
0022106
Arg of perigee: 309
8887 deg
Mean anomaly: 50
0324 deg
Mean motion: 15
58899645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3515
Checksum: 331
Coasting Arc #6 (Orbit 3529)
---------------------------------------
Vector Time (GMT): 2012/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5342054
14 A = 6768886
72 meter
Y = -1314009
70 meter E =
0019636
Z = -3948692
32 I = 51
89666
XDOT = -1444
861460 Wp = 330
28377
YDOT = 6355
535998 meter/sec RA = 131
92612 deg
ZDOT = -4044
410398 TA = 257
53529
MA = 257
75506
Ha = 217
401 n
mi
Hp = 205
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17526424
34 X = 5375531
96
Y = -4311055
44 feet Y = -1254084
18 meter
Z = -12955027
30 Z = -3922660
32
XDOT = -4740
359121 XDOT = -1496
176650
YDOT = 20851
496058 feet/sec YDOT = 6339
091958 meter/sec
ZDOT = -13269
062987 ZDOT = -4051
553594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12861903
75 X = 3920308
26
Y = 12770553
52 feet Y = 3892464
71 meter
Z = -12848263
55 Z = -3916150
73
XDOT = -19288
665983 XDOT = -5879
185392
YDOT = 5962
984802 feet/sec YDOT = 1817
517768 meter/sec
ZDOT = -13298
755921 ZDOT = -4053
460805
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 12023
52354278
00016717 00000-0 10270-3 0 9056
2 25544 51
6425 132
7624 0022142 313
2694 46
6613 15
58927178 35309
Satellite: ISS
Catalog Number: 25544
Epoch time: 12023
52354278 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 132
7624 deg
Eccentricity:
0022142
Arg of perigee: 313
2694 deg
Mean anomaly: 46
6613 deg
Mean motion: 15
58927178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3530
Checksum: 299
Coasting Arc #7 (Orbit 3545)
---------------------------------------
Vector Time (GMT): 2012/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3738542
63 A = 6763352
47 meter
Y = -1942526
07 meter E =
0019493
Z = 5300086
54 I = 51
89894
XDOT = 4187
286882 Wp = 320
69685
YDOT = -6394
046975 meter/sec RA = 126
90244 deg
ZDOT = 626
083323 TA = 123
44145
MA = 123
25490
Ha = 217
594 n
mi
Hp = 204
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12265559
80 X = -3742288
98
Y = -6373117
02 feet Y = -1984353
85 meter
Z = 17388735
36 Z = 5281916
20
XDOT = 13737
817853 XDOT = 4255
433897
YDOT = -20977
844406 feet/sec YDOT = -6346
841143 meter/sec
ZDOT = 2054
079144 ZDOT = 646
589770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1255118
20 X = -382560
03
Y = -13858752
62 feet Y = -4224147
80 meter
Z = 17314397
17 Z = 5277428
26
XDOT = 24055
927078 XDOT = 7332
246573
YDOT = 427
492250 feet/sec YDOT = 130
299638 meter/sec
ZDOT = 2138
544604 ZDOT = 651
828395
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 12024
54919154
00016717 00000-0 10270-3 0 9060
2 25544 51
6430 127
6116 0022219 317
4048 42
5383 15
58996307 35464
Satellite: ISS
Catalog Number: 25544
Epoch time: 12024
54919154 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 127
6116 deg
Eccentricity:
0022219
Arg of perigee: 317
4048 deg
Mean anomaly: 42
5383 deg
Mean motion: 15
58996307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3546
Checksum: 308
Coasting Arc #8 (Orbit 3560)
---------------------------------------
Vector Time (GMT): 2012/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1293554
42 A = 6766048
76 meter
Y = 4765921
50 meter E =
0014369
Z = -4614856
66 I = 51
92554
XDOT = -5523
219609 Wp = 343
50695
YDOT = 4408
419596 meter/sec RA = 121
87448 deg
ZDOT = 3015
707299 TA = 316
34316
MA = 316
45674
Ha = 217
810 n
mi
Hp = 204
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4243944
95 X = 1262582
16
Y = 15636225
39 feet Y = 4780213
67 meter
Z = -15140605
85 Z = -4608648
00
XDOT = -18120
799242 XDOT = -5586
754196
YDOT = 14463
318884 feet/sec YDOT = 4346
300297 meter/sec
ZDOT = 9894
052819 ZDOT = 2988
722131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10663610
41 X = -3250268
45
Y = 12229077
04 feet Y = 3727422
68 meter
Z = -15115477
05 Z = -4607197
40
XDOT = -21193
043478 XDOT = -6459
639652
YDOT = -6433
124074 feet/sec YDOT = -1960
816218 meter/sec
ZDOT = 9783
158236 ZDOT = 2981
906630
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 12025
51072103
00016717 00000-0 10270-3 0 9073
2 25544 51
6427 122
7846 0022155 321
3102 38
6466 15
59023579 35618
Satellite: ISS
Catalog Number: 25544
Epoch time: 12025
51072103 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 122
7846 deg
Eccentricity:
0022155
Arg of perigee: 321
3102 deg
Mean anomaly: 38
6466 deg
Mean motion: 15
59023579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3561
Checksum: 285
Coasting Arc #9 (Orbit 3576)
---------------------------------------
Vector Time (GMT): 2012/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1299092
24 A = 6773145
42 meter
Y = -6296495
04 meter E =
0013602
Z = 2157339
27 I = 51
96377
XDOT = 5252
211644 Wp = 2
27826
YDOT = -812
309868 meter/sec RA = 116
87664 deg
ZDOT = -5519
151296 TA = 153
89913
MA = 153
83050
Ha = 218
016 n
mi
Hp = 204
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4262113
65 X = 1358924
72
Y = -20657792
11 feet Y = -6281633
22 meter
Z = 7077884
74 Z = 2163795
46
XDOT = 17231
665500 XDOT = 5287
714891
YDOT = -2665
058622 feet/sec YDOT = -753
377956 meter/sec
ZDOT = -18107
451760 ZDOT = -5493
550619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19428510
01 X = 5921809
85
Y = -8189118
85 feet Y = -2496043
43 meter
Z = 7104771
02 Z = 2165534
21
XDOT = 11399
590630 XDOT = 3474
595224
YDOT = 11385
667012 feet/sec YDOT = 3470
351305 meter/sec
ZDOT = -18002
465207 ZDOT = -5487
151395
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 12026
53633230
00016717 00000-0 10270-3 0 9081
2 25544 51
6421 117
6343 0022189 325
3813 34
5896 15
59020090 35771
Satellite: ISS
Catalog Number: 25544
Epoch time: 12026
53633230 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 117
6343 deg
Eccentricity:
0022189
Arg of perigee: 325
3813 deg
Mean anomaly: 34
5896 deg
Mean motion: 15
59020090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3577
Checksum: 296
Coasting Arc #10 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2012/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3294018
83 A = 6774556
90 meter
Y = 5786909
51 meter E =
0026601
Z = 1147695
70 I = 51
98170
XDOT = -3674
863700 Wp =
43557
YDOT = -3260
332203 meter/sec RA = 111
90517 deg
ZDOT = 5916
967521 TA = 12
01531
MA = 11
95198
Ha = 218
316 n
mi
Hp = 204
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10807148
39 X = -3364059
53
Y = 18985923
58 feet Y = 5749682
16 meter
Z = 3765405
85 Z = 1131523
58
XDOT = -12056
639435 XDOT = -3666
875635
YDOT = -10696
627962 feet/sec YDOT = -3301
382014 meter/sec
ZDOT = 19412
623100 ZDOT = 5899
135005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21750202
02 X = -6629461
58
Y = 2164763
07 feet Y = 659819
78 meter
Z = 3698722
05 Z = 1127370
48
XDOT = 1828
192487 XDOT = 557
233070
YDOT = -14532
708531 feet/sec YDOT = -4429
569560 meter/sec
ZDOT = 19339
750513 ZDOT = 5894
755956
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 12027
56192290
00016717 00000-0 10270-3 0 9092
2 25544 51
6424 112
4829 0022327 329
5109 30
4747 15
59040904 35938
Satellite: ISS
Catalog Number: 25544
Epoch time: 12027
56192290 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 112
4829 deg
Eccentricity:
0022327
Arg of perigee: 329
5109 deg
Mean anomaly: 30
4747 deg
Mean motion: 15
59040904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 304
Coasting Arc #11 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2012/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4298930
96 A = 6768275
79 meter
Y = -3381639
99 meter E =
0022185
Z = -4000150
84 I = 51
97019
XDOT = 1310
120886 Wp = 350
70554
YDOT = 6412
934056 meter/sec RA = 106
92059 deg
ZDOT = -3988
962764 TA = 237
83558
MA = 238
05098
Ha = 218
455 n
mi
Hp = 203
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14104104
20 X = 4355857
15
Y = -11094619
39 feet Y = -3333248
48 meter
Z = -13123854
46 Z = -3979128
83
XDOT = 4298
296871 XDOT = 1257
689977
YDOT = 21039
809894 feet/sec YDOT = 6427
291405 meter/sec
ZDOT = -13087
148177 ZDOT = -3982
725825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17344779
78 X = 5286688
88
Y = 4841018
56 feet Y = 1475542
46 meter
Z = -13037447
77 Z = -3973814
08
XDOT = -13991
812901 XDOT = -4264
704572
YDOT = 14736
193054 feet/sec YDOT = 4491
591643 meter/sec
ZDOT = -13062
027523 ZDOT = -3981
305989
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 12028
52339537
00016717 00000-0 10270-3 0 9108
2 25544 51
6412 107
6547 0022304 332
9857 27
0136 15
59074608 36080
Satellite: ISS
Catalog Number: 25544
Epoch time: 12028
52339537 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 107
6547 deg
Eccentricity:
0022304
Arg of perigee: 332
9857 deg
Mean anomaly: 27
0136 deg
Mean motion: 15
59074608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 302
Coasting Arc #12 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2012/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4177712
39 A = 6762882
63 meter
Y = -329927
37 meter E =
0020565
Z = 5311983
17 I = 51
96120
XDOT = 1199
396225 Wp = 342
19815
YDOT = -7563
249294 meter/sec RA = 101
89884 deg
ZDOT = 493
110709 TA = 103
23659
MA = 103
00711
Ha = 218
657 n
mi
Hp = 203
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13706405
48 X = -4199516
65
Y = -1082438
89 feet Y = -376766
99 meter
Z = 17427766
30 Z = 5291635
34
XDOT = 3935
026984 XDOT = 1281
485461
YDOT = -24813
810019 feet/sec YDOT = -7549
377916 meter/sec
ZDOT = 1617
817287 ZDOT = 499
136711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7520868
54 X = -2292360
73
Y = -11635004
92 feet Y = -3546349
50 meter
Z = 17344378
34 Z = 5286566
52
XDOT = 21257
210259 XDOT = 6479
197687
YDOT = -11387
549733 feet/sec YDOT = -3470
925159 meter/sec
ZDOT = 1643
056054 ZDOT = 500
803485
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 12029
54894542
00016717 00000-0 10270-3 0 9114
2 25544 51
6417 102
5027 0022391 336
8289 23
1855 15
59137168 36244
Satellite: ISS
Catalog Number: 25544
Epoch time: 12029
54894542 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 102
5027 deg
Eccentricity:
0022391
Arg of perigee: 336
8289 deg
Mean anomaly: 23
1855 deg
Mean motion: 15
59137168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 312
Coasting Arc #13 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2012/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3099165
94 A = 6765991
25 meter
Y = 3938645
97 meter E =
0017893
Z = -4537671
83 I = 51
97626
XDOT = -3248
225235 Wp = 6
19607
YDOT = 6193
861061 meter/sec RA = 96
87330 deg
ZDOT = 3176
194635 TA = 295
37302
MA = 295
55817
Ha = 218
871 n
mi
Hp = 203
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10167867
27 X = 3076935
61
Y = 12922066
85 feet Y = 3973178
47 meter
Z = -14887374
76 Z = -4522670
39
XDOT = -10656
906940 XDOT = -3332
673869
YDOT = 20321
066474 feet/sec YDOT = 6157
065224 meter/sec
ZDOT = 10420
586072 ZDOT = 3160
209976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3771012
11 X = -1149404
49
Y = 16061245
82 feet Y = 4895467
72 meter
Z = -14826163
16 Z = -4519014
53
XDOT = -21417
703133 XDOT = -6528
115915
YDOT = 4473
481592 feet/sec YDOT = 1363
517189 meter/sec
ZDOT = 10354
608240 ZDOT = 3156
084591
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 12030
51038245
00016717 00000-0 10270-3 0 9124
2 25544 51
6408 97
6743 0022418 341
0934 18
9387 15
59163552 36392
Satellite: ISS
Catalog Number: 25544
Epoch time: 12030
51038245 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 97
6743 deg
Eccentricity:
0022418
Arg of perigee: 341
0934 deg
Mean anomaly: 18
9387 deg
Mean motion: 15
59163552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 310
Coasting Arc #14 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2012/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1316639
99 A = 6772989
26 meter
Y = -6359948
57 meter E =
0017919
Z = 1951445
24 I = 52
00329
XDOT = 4478
459915 Wp = 23
05609
YDOT = -2661
214307 meter/sec RA = 91
87889 deg
ZDOT = -5618
070972 TA = 135
52716
MA = 135
38317
Ha = 218
979 n
mi
Hp = 202
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4319684
99 X = -1254903
48
Y = -20865972
99 feet Y = -6374326
89 meter
Z = 6402379
39 Z = 1945199
00
XDOT = 14693
109956 XDOT = 4535
176307
YDOT = -8731
018068 feet/sec YDOT = -2610
816217 meter/sec
ZDOT = -18431
991378 ZDOT = -5596
177337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13378295
71 X = 4077704
53
Y = -16594906
51 feet Y = -5058127
50 meter
Z = 6377244
79 Z = 1943784
21
XDOT = 14926
856573 XDOT = 4549
705883
YDOT = 4942
556123 feet/sec YDOT = 1506
491106 meter/sec
ZDOT = -18342
037859 ZDOT = -5590
653139
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 12031
53589400
00016717 00000-0 10270-3 0 9132
2 25544 51
6414 92
5225 0022626 344
9704 15
0776 15
59208141 36558
Satellite: ISS
Catalog Number: 25544
Epoch time: 12031
53589400 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 92
5225 deg
Eccentricity:
0022626
Arg of perigee: 344
9704 deg
Mean anomaly: 15
0776 deg
Mean motion: 15
59208141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 294
Coasting Arc #15 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -741319
53 A = 6773912
80 meter
Y = 6564922
49 meter E =
0030122
Z = 1400755
72 I = 52
00553
XDOT = -4671
923449 Wp = 15
03021
YDOT = -1775
620094 meter/sec RA = 86
90955 deg
ZDOT = 5849
731153 TA =
22917
MA =
22779
Ha = 219
294 n
mi
Hp = 202
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2432150
69 X = -821479
18
Y = 21538459
62 feet Y = 6556184
37 meter
Z = 4595655
24 Z = 1396959
92
XDOT = -15327
832839 XDOT = -4680
137208
YDOT = -5825
525242 feet/sec YDOT = -1827
910489 meter/sec
ZDOT = 19192
031341 ZDOT = 5827
015442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18015348
75 X = -5491078
30
Y = 12058821
37 feet Y = 3675528
75 meter
Z = 4579594
21 Z = 1395860
32
XDOT = -4670
944712 XDOT = -1423
703948
YDOT = -14230
894339 feet/sec YDOT = -4337
576595 meter/sec
ZDOT = 19099
035663 ZDOT = 5821
386070
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 12032
56138825
00016717 00000-0 10270-3 0 9148
2 25544 51
6411 87
3708 0022663 349
3853 10
6821 15
59164090 36712
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
56138825 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 87
3708 deg
Eccentricity:
0022663
Arg of perigee: 349
3853 deg
Mean anomaly: 10
6821 deg
Mean motion: 15
59164090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 304
Coasting Arc #16 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2012/032/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 128173
82 A = 6776879
50 meter
Y = -6717813
78 meter E =
0010950
Z = -938763
33 I = 52
00762
XDOT = 4744
802647 Wp = 10
54293
YDOT = 921
052448 meter/sec RA = 84
82795 deg
ZDOT = -5943
699890 TA = 179
56945
MA = 179
56851
Ha = 219
287 n
mi
Hp = 205
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 420517
77 X = 207844
47
Y = -22040071
47 feet Y = -6715934
97 meter
Z = -3079932
18 Z = -937947
35
XDOT = 15566
937819 XDOT = 4763
023387
YDOT = 3021
825616 feet/sec YDOT = 974
213803 meter/sec
ZDOT = -19500
327723 ZDOT = -5920
605867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21759297
41 X = -6632233
85
Y = 3535297
25 feet Y = 1077558
60 meter
Z = -3076071
73 Z = -937586
66
XDOT = 405
840421 XDOT = 123
700160
YDOT = -14385
766089 feet/sec YDOT = -4384
781504 meter/sec
ZDOT = -19405
714593 ZDOT = -5914
861808
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 12032
94595895
00016717 00000-0 10270-3 0 9155
2 25544 51
6424 85
4400 0018978 347
2609 12
8064 15
58287384 36774
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
94595895 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 85
4400 deg
Eccentricity:
0018978
Arg of perigee: 347
2609 deg
Mean anomaly: 12
8064 deg
Mean motion: 15
58287384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3677
Checksum: 343
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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