[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 6th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
200/03:26:03
716 2
4 4
4 4
4
N/A 1
5 -0
1 220
3
000/00:38:07
432 3
4 0
3 214
0
Coasting Arc #1 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2012/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2137619
42 A = 6776082
33 meter
Y = -4774070
01 meter E =
0014058
Z = -4318913
77 I = 51
78230
XDOT = 6797
743246 Wp = 94
12109
YDOT = 140
912875 meter/sec RA = 25
32615 deg
ZDOT = -3531
146003 TA = 140
01237
MA = 139
90877
Ha = 220
587 n
mi
Hp = 209
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7013187
06 X = -2063096
00
Y = -15662959
35 feet Y = -4797557
02 meter
Z = -14169664
58 Z = -4329117
57
XDOT = 22302
307239 XDOT = 6812
815499
YDOT = 462
312583 feet/sec YDOT = 217
014131 meter/sec
ZDOT = -11585
124682 ZDOT = -3498
086851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13510417
48 X = -4117975
25
Y = 10526302
16 feet Y = 3208416
90 meter
Z = -14211195
07 Z = -4331572
26
XDOT = -4222
897392 XDOT = -1287
139125
YDOT = -20828
607214 feet/sec YDOT = -6348
559479 meter/sec
ZDOT = -11448
790945 ZDOT = -3489
591480
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 12188
52243889
00016717 00000-0 10270-3 0 9008
2 25544 51
6365 25
7420 0007227 124
9031 235
2803 15
55949106 21029
Satellite: ISS
Catalog Number: 25544
Epoch time: 12188
52243889 = yrday
fracday
Element set: 900
Inclination: 51
6365 deg
RA of node: 25
7420 deg
Eccentricity:
0007227
Arg of perigee: 124
9031 deg
Mean anomaly: 235
2803 deg
Mean motion: 15
55949106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 291
Coasting Arc #2 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2012/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -227186
48 A = 6772506
29 meter
Y = 4303500
40 meter E =
0011033
Z = 5217857
59 I = 51
74233
XDOT = -7381
851629 Wp = 126
07241
YDOT = -1777
754064 meter/sec RA = 20
32075 deg
ZDOT = 1136
793069 TA = 313
01236
MA = 313
10475
Ha = 220
609 n
mi
Hp = 209
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -745362
48 X = -300638
98
Y = 14119095
79 feet Y = 4300548
67 meter
Z = 17118955
36 Z = 5216575
94
XDOT = -24218
673323 XDOT = -7366
945976
YDOT = -5832
526456 feet/sec YDOT = -1860
219271 meter/sec
ZDOT = 3729
636054 ZDOT = 1100
968987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13856369
99 X = 4223421
57
Y = -2846662
62 feet Y = -867662
77 meter
Z = 17113169
97 Z = 5216094
21
XDOT = 456
237390 XDOT = 139
061157
YDOT = 23913
474555 feet/sec YDOT = 7288
827044 meter/sec
ZDOT = 3582
092856 ZDOT = 1091
821903
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 12189
55006088
00016717 00000-0 10270-3 0 9011
2 25544 51
6368 20
6037 0007241 128
3842 231
7963 15
55928055 21189
Satellite: ISS
Catalog Number: 25544
Epoch time: 12189
55006088 = yrday
fracday
Element set: 901
Inclination: 51
6368 deg
RA of node: 20
6037 deg
Eccentricity:
0007241
Arg of perigee: 128
3842 deg
Mean anomaly: 231
7963 deg
Mean motion: 15
55928055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 304
Coasting Arc #3 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2012/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2705122
64 A = 6772734
20 meter
Y = -3481667
48 meter E =
0020258
Z = -5158944
05 I = 51
71400
XDOT = 6840
928566 Wp = 111
82625
YDOT = 3095
796282 meter/sec RA = 15
30561 deg
ZDOT = 1495
155737 TA = 172
59497
MA = 172
56501
Ha = 220
467 n
mi
Hp = 209
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8875074
28 X = 2768914
96
Y = -11422793
56 feet Y = -3451060
02 meter
Z = -16925669
45 Z = -5145648
19
XDOT = 22443
991357 XDOT = 6798
539271
YDOT = 10156
811949 feet/sec YDOT = 3172
058657 meter/sec
ZDOT = 4905
366590 ZDOT = 1528
285508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13459839
48 X = -4102559
07
Y = -5472359
24 feet Y = -1667975
10 meter
Z = -16870431
18 Z = -5142107
42
XDOT = 3169
887570 XDOT = 966
181731
YDOT = -23365
993016 feet/sec YDOT = -7121
954671 meter/sec
ZDOT = 5041
638728 ZDOT = 1536
691484
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 12190
51344187
00016717 00000-0 10270-3 0 9025
2 25544 51
6362 15
7857 0007282 132
4540 227
7230 15
55989525 21332
Satellite: ISS
Catalog Number: 25544
Epoch time: 12190
51344187 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 15
7857 deg
Eccentricity:
0007282
Arg of perigee: 132
4540 deg
Mean anomaly: 227
7230 deg
Mean motion: 15
55989525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 301
Coasting Arc #4 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2012/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4836715
10 A = 6776893
92 meter
Y = 2397511
92 meter E =
0015621
Z = 4081603
84 I = 51
69866
XDOT = -5266
619136 Wp = 100
34071
YDOT = -4049
524169 meter/sec RA = 10
29894 deg
ZDOT = -3852
531047 TA = 29
43834
MA = 29
35045
Ha = 220
447 n
mi
Hp = 209
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15868487
86 X = -4882992
41
Y = 7865852
76 feet Y = 2343165
71 meter
Z = 13391088
72 Z = 4057995
31
XDOT = -17278
934172 XDOT = -5202
230559
YDOT = -13285
840448 feet/sec YDOT = -4108
058461 meter/sec
ZDOT = -12639
537555 ZDOT = -3877
959704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12191918
91 X = 3716096
88
Y = 12947707
04 feet Y = 3946461
11 meter
Z = 13293449
48 Z = 4051843
40
XDOT = -6723
883691 XDOT = -2049
439749
YDOT = 19448
755792 feet/sec YDOT = 5927
980765 meter/sec
ZDOT = -12743
932584 ZDOT = -3884
350652
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 12191
54103601
00016717 00000-0 10270-3 0 9034
2 25544 51
6366 10
6480 0007150 136
8774 223
2941 15
56001711 21493
Satellite: ISS
Catalog Number: 25544
Epoch time: 12191
54103601 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 10
6480 deg
Eccentricity:
0007150
Arg of perigee: 136
8774 deg
Mean anomaly: 223
2941 deg
Mean motion: 15
56001711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 271
Coasting Arc #5 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2012/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6286887
01 A = 6781726
42 meter
Y = -1201986
77 meter E =
0008930
Z = -2250602
54 I = 51
68493
XDOT = 2822
075213 Wp = 96
69132
YDOT = 4587
702079 meter/sec RA = 5
30754 deg
ZDOT = 5450
642536 TA = 238
29938
MA = 238
38647
Ha = 220
319 n
mi
Hp = 209
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20626269
72 X = 6310793
46
Y = -3943526
13 feet Y = -1131549
04 meter
Z = -7383866
60 Z = -2220003
37
XDOT = 9258
776947 XDOT = 2744
087040
YDOT = 15051
516006 feet/sec YDOT = 4618
823776 meter/sec
ZDOT = 17882
685487 ZDOT = 5464
162898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10142029
20 X = -3091290
50
Y = -18438633
40 feet Y = -5620095
46 meter
Z = -7257542
88 Z = -2212099
07
XDOT = 10141
602344 XDOT = 3091
160395
YDOT = -12615
694051 feet/sec YDOT = -3845
263547 meter/sec
ZDOT = 17937
904463 ZDOT = 5467
473280
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 12192
50439413
00016717 00000-0 10270-3 0 9045
2 25544 51
6366 5
8306 0007304 139
9049 220
2645 15
56028511 21648
Satellite: ISS
Catalog Number: 25544
Epoch time: 12192
50439413 = yrday
fracday
Element set: 904
Inclination: 51
6366 deg
RA of node: 5
8306 deg
Eccentricity:
0007304
Arg of perigee: 139
9049 deg
Mean anomaly: 220
2645 deg
Mean motion: 15
56028511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 287
Coasting Arc #6 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2012/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6773336
26 A = 6783633
71 meter
Y = -90608
17 meter E =
0018908
Z = -65373
42 I = 51
66156
XDOT = 111
885432 Wp = 137
60086
YDOT = -4760
645325 meter/sec RA =
32911 deg
ZDOT = -6020
428018 TA = 43
10409
MA = 42
95618
Ha = 220
044 n
mi
Hp = 209
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22222231
83 X = -6771502
08
Y = -297270
88 feet Y = -166341
55 meter
Z = -214479
71 Z = -98273
37
XDOT = 367
078188 XDOT = 194
357363
YDOT = -15618
915109 feet/sec YDOT = -4758
932471 meter/sec
ZDOT = -19752
060425 ZDOT = -6019
684604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6951768
35 X = 2118898
99
Y = 21107161
85 feet Y = 6433462
93 meter
Z = -350134
86 Z = -106721
10
XDOT = -13389
109495 XDOT = -4081
000574
YDOT = 4116
400885 feet/sec YDOT = 1254
678990 meter/sec
ZDOT = -19748
436966 ZDOT = -6019
323587
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 12193
53196101
00016717 00000-0 10270-3 0 9054
2 25544 51
6366
6924 0007026 142
6658 217
4985 15
56089724 21801
Satellite: ISS
Catalog Number: 25544
Epoch time: 12193
53196101 = yrday
fracday
Element set: 905
Inclination: 51
6366 deg
RA of node:
6924 deg
Eccentricity:
0007026
Arg of perigee: 142
6658 deg
Mean anomaly: 217
4985 deg
Mean motion: 15
56089724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 309
Coasting Arc #7 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2012/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6224753
36 A = 6781312
74 meter
Y = 1338740
78 meter E =
0017323
Z = 2322475
81 I = 51
62320
XDOT = -3006
234745 Wp = 96
75876
YDOT = 4538
783348 meter/sec RA = 355
34743 deg
ZDOT = 5404
486116 TA = 289
16147
MA = 289
34890
Ha = 220
080 n
mi
Hp = 209
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20422419
15 X = 6198038
63
Y = 4392194
15 feet Y = 1408200
21 meter
Z = 7619671
29 Z = 2352650
51
XDOT = -9862
974886 XDOT = -3083
018585
YDOT = 14891
021482 feet/sec YDOT = 4504
735872 meter/sec
ZDOT = 17731
253662 ZDOT = 5389
695996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2834471
24 X = -863946
83
Y = -20650016
03 feet Y = -6294124
89 meter
Z = 7743937
93 Z = 2360352
28
XDOT = 15897
178136 XDOT = 4845
459896
YDOT = 4488
541298 feet/sec YDOT = 1368
107388 meter/sec
ZDOT = 17669
733402 ZDOT = 5385
734741
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 12194
55951649
00016717 00000-0 10270-3 0 9064
2 25544 51
6366 355
5541 0007294 147
4487 212
7117 15
56075497 21962
Satellite: ISS
Catalog Number: 25544
Epoch time: 12194
55951649 = yrday
fracday
Element set: 906
Inclination: 51
6366 deg
RA of node: 355
5541 deg
Eccentricity:
0007294
Arg of perigee: 147
4487 deg
Mean anomaly: 212
7117 deg
Mean motion: 15
56075497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 340
Coasting Arc #8 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2012/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4686084
90 A = 6776095
85 meter
Y = -2563802
62 meter E =
0011678
Z = -4176591
84 I = 51
57650
XDOT = 5442
332672 Wp = 107
17784
YDOT = -3914
805468 meter/sec RA = 350
34910 deg
ZDOT = -3715
086983 TA = 124
65674
MA = 124
54660
Ha = 219
954 n
mi
Hp = 209
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15374294
29 X = -4636778
80
Y = -8411425
93 feet Y = -2615929
15 meter
Z = -13702729
13 Z = -4199237
07
XDOT = 17855
422152 XDOT = 5503
751314
YDOT = -12843
849962 feet/sec YDOT = -3853
602076 meter/sec
ZDOT = -12188
605586 ZDOT = -3688
499773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2383865
09 X = -726602
08
Y = 17288112
75 feet Y = 5269416
77 meter
Z = -13795801
58 Z = -4204960
32
XDOT = -17149
278983 XDOT = -5227
100234
YDOT = -11972
193074 feet/sec YDOT = -3649
124449 meter/sec
ZDOT = -12078
514892 ZDOT = -3681
531339
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 12195
52283637
00016717 00000-0 10270-3 0 9078
2 25544 51
6373 350
7373 0007229 149
7892 210
3680 15
56099486 22114
Satellite: ISS
Catalog Number: 25544
Epoch time: 12195
52283637 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 350
7373 deg
Eccentricity:
0007229
Arg of perigee: 149
7892 deg
Mean anomaly: 210
3680 deg
Mean motion: 15
56099486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 326
Coasting Arc #9 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2012/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2481535
47 A = 6772129
32 meter
Y = 3596287
92 meter E =
0011000
Z = 5169963
89 I = 51
53291
XDOT = -6979
810183 Wp = 142
79834
YDOT = 2908
796230 meter/sec RA = 345
32900 deg
ZDOT = 1316
796405 TA = 294
48730
MA = 294
60198
Ha = 219
806 n
mi
Hp = 210
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8141520
57 X = 2416022
24
Y = 11798844
89 feet Y = 3623671
01 meter
Z = 16961823
80 Z = 5181860
35
XDOT = -22899
639708 XDOT = -7018
214843
YDOT = 9543
294718 feet/sec YDOT = 2830
528760 meter/sec
ZDOT = 4320
198180 ZDOT = 1282
796096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7939461
27 X = 2419947
80
Y = -11866340
12 feet Y = -3616860
47 meter
Z = 17010452
42 Z = 5184785
90
XDOT = 16556
893864 XDOT = 5046
541250
YDOT = 17116
509110 feet/sec YDOT = 5217
111977 meter/sec
ZDOT = 4179
660007 ZDOT = 1273
960370
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 12196
55036415
00016717 00000-0 10270-3 0 9083
2 25544 51
6369 345
5983 0007152 154
2612 205
8899 15
56108387 22273
Satellite: ISS
Catalog Number: 25544
Epoch time: 12196
55036415 = yrday
fracday
Element set: 908
Inclination: 51
6369 deg
RA of node: 345
5983 deg
Eccentricity:
0007152
Arg of perigee: 154
2612 deg
Mean anomaly: 205
8899 deg
Mean motion: 15
56108387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 330
Coasting Arc #10 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2012/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73406
46 A = 6772186
17 meter
Y = -4393145
89 meter E =
0018827
Z = -5169491
36 I = 51
50496
XDOT = 7386
287093 Wp = 119
05142
YDOT = -1490
483111 meter/sec RA = 340
29986 deg
ZDOT = 1366
354138 TA = 164
15547
MA = 164
09648
Ha = 219
801 n
mi
Hp = 210
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 240834
86 X = 147638
07
Y = -14413208
31 feet Y = -4391909
25 meter
Z = -16960273
49 Z = -5168955
06
XDOT = 24233
225371 XDOT = 7395
767632
YDOT = -4890
036453 feet/sec YDOT = -1407
832247 meter/sec
ZDOT = 4482
789168 ZDOT = 1402
258910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13408707
63 X = -4086974
08
Y = 5300726
86 feet Y = 1615661
55 meter
Z = -16957544
23 Z = -5168659
48
XDOT = -13550
446549 XDOT = -4130
176108
YDOT = -19407
788338 feet/sec YDOT = -5915
493885 meter/sec
ZDOT = 4631
012661 ZDOT = 1411
532659
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 12197
51365859
00016717 00000-0 10270-3 0 9098
2 25544 51
6380 340
7820 0007234 157
3922 202
7551 15
56135826 22428
Satellite: ISS
Catalog Number: 25544
Epoch time: 12197
51365859 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 340
7820 deg
Eccentricity:
0007234
Arg of perigee: 157
3922 deg
Mean anomaly: 202
7551 deg
Mean motion: 15
56135826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 310
Coasting Arc #11 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2012/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2502372
38 A = 6776373
49 meter
Y = 4755981
77 meter E =
0013336
Z = 4113770
89 I = 51
49030
XDOT = -6678
982729 Wp = 108
83831
YDOT = -237
749812 meter/sec RA = 335
27566 deg
ZDOT = -3782
094763 TA = 20
19453
MA = 20
14182
Ha = 219
764 n
mi
Hp = 210
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8209883
15 X = -2575352
30
Y = 15603614
73 feet Y = 4727590
06 meter
Z = 13496623
66 Z = 4101438
02
XDOT = -21912
672997 XDOT = -6657
455421
YDOT = -780
019068 feet/sec YDOT = -312
317444 meter/sec
ZDOT = -12408
447386 ZDOT = -3814
488327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17626497
94 X = 5372556
57
Y = 1251665
05 feet Y = 381507
51 meter
Z = 13445212
13 Z = 4098100
66
XDOT = 8232
817940 XDOT = 2509
362908
YDOT = 18991
660940 feet/sec YDOT = 5788
658254 meter/sec
ZDOT = -12541
990559 ZDOT = -3822
798722
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 12198
54115987
00016717 00000-0 10270-3 0 9109
2 25544 51
6378 335
6426 0007209 161
2227 198
9194 15
56125337 22586
Satellite: ISS
Catalog Number: 25544
Epoch time: 12198
54115987 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 335
6426 deg
Eccentricity:
0007209
Arg of perigee: 161
2227 deg
Mean anomaly: 198
9194 deg
Mean motion: 15
56125337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 329
Coasting Arc #12 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2012/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4442714
42 A = 6781291
62 meter
Y = -4604735
80 meter E =
0006461
Z = -2255589
79 I = 51
48121
XDOT = 4967
853814 Wp = 111
32326
YDOT = 2138
921492 meter/sec RA = 330
26966 deg
ZDOT = 5428
617092 TA = 223
53076
MA = 223
58176
Ha = 219
535 n
mi
Hp = 210
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14575834
72 X = 4504832
31
Y = -15107400
93 feet Y = -4554706
99 meter
Z = -7400228
97 Z = -2233857
35
XDOT = 16298
732985 XDOT = 4917
196142
YDOT = 7017
458962 feet/sec YDOT = 2194
191136 meter/sec
ZDOT = 17810
423529 ZDOT = 5452
627582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19860555
45 X = -6053497
30
Y = -6897316
82 feet Y = -2102302
17 meter
Z = -7310079
86 Z = -2228112
34
XDOT = -956
196006 XDOT = -291
448543
YDOT = -16191
486458 feet/sec YDOT = -4935
165072 meter/sec
ZDOT = 17909
179972 ZDOT = 5458
718055
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 12199
50442836
00016717 00000-0 10270-3 0 9113
2 25544 51
6391 330
8256 0007062 164
7535 195
3833 15
56168213 22734
Satellite: ISS
Catalog Number: 25544
Epoch time: 12199
50442836 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 330
8256 deg
Eccentricity:
0007062
Arg of perigee: 164
7535 deg
Mean anomaly: 195
3833 deg
Mean motion: 15
56168213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 311
Coasting Arc #13 (Orbit 2283)
---------------------------------------
Vector Time (GMT): 2012/200/03:45:07
432
Vector Time (MET): N/A
Weight (LBS) : 907810
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5191488
13 A = 6780175
05 meter
Y = 714096
39 meter E =
0010121
Z = 4296919
54 I = 51
44664
XDOT = -3700
123343 Wp = 114
75016
YDOT = 5732
053920 meter/sec RA = 327
02768 deg
ZDOT = 3507
187297 TA = 299
42339
MA = 299
52437
Ha = 220
283 n
mi
Hp = 214
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17032441
38 X = 5162244
02
Y = 2342835
93 feet Y = 771986
77 meter
Z = 14097505
05 Z = 4322068
18
XDOT = -12139
512279 XDOT = -3780
982172
YDOT = 18805
951181 feet/sec YDOT = 5690
224289 meter/sec
ZDOT = 11506
520004 ZDOT = 3489
016908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16441586
87 X = 5011395
68
Y = 4725985
35 feet Y = 1440480
33 meter
Z = 14201122
21 Z = 4328502
05
XDOT = -14411
398718 XDOT = -4392
594329
YDOT = 15683
748813 feet/sec YDOT = 4780
406638 meter/sec
ZDOT = 11430
930968 ZDOT = 3484
147759
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 12200
21088617
00016717 00000-0 10270-3 0 9128
2 25544 51
6411 327
2978 0001285 182
1245 177
9903 15
54541018 22843
Satellite: ISS
Catalog Number: 25544
Epoch time: 12200
21088617 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 327
2978 deg
Eccentricity:
0001285
Arg of perigee: 182
1245 deg
Mean anomaly: 177
9903 deg
Mean motion: 15
54541018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2284
Checksum: 295
Coasting Arc #14 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2012/201/03:45:07
432
Vector Time (MET): N/A
Weight (LBS) : 907810
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3944870
14 A = 6776839
36 meter
Y = -2092389
88 meter E =
0013149
Z = -5109318
19 I = 51
41114
XDOT = 5025
190494 Wp = 82
43393
YDOT = -5552
190587 meter/sec RA = 322
01388 deg
ZDOT = -1608
023748 TA = 171
99601
MA = 171
97501
Ha = 220
223 n
mi
Hp = 213
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12942487
34 X = -3896360
00
Y = -6864796
21 feet Y = -2136232
06 meter
Z = -16762854
95 Z = -5128364
22
XDOT = 16486
845453 XDOT = 5094
714008
YDOT = -18215
848383 feet/sec YDOT = -5495
606882 meter/sec
ZDOT = -5275
668465 ZDOT = -1583
443830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11881502
66 X = -3621482
01
Y = -8416186
57 feet Y = -2565253
67 meter
Z = -16841152
27 Z = -5133183
21
XDOT = 18051
380559 XDOT = 5502
060794
YDOT = -15143
366635 feet/sec YDOT = -4615
698150 meter/sec
ZDOT = -5173
677507 ZDOT = -1576
936904
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 12201
17514952
00016717 00000-0 10270-3 0 9131
2 25544 51
6413 322
4873 0001187 192
1959 167
9166 15
54588495 22996
Satellite: ISS
Catalog Number: 25544
Epoch time: 12201
17514952 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 322
4873 deg
Eccentricity:
0001187
Arg of perigee: 192
1959 deg
Mean anomaly: 167
9166 deg
Mean motion: 15
54588495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 331
Coasting Arc #15 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2012/202/03:45:07
432
Vector Time (MET): N/A
Weight (LBS) : 907810
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2476685
37 A = 6776029
89 meter
Y = 3452757
87 meter E =
0002173
Z = 5276280
36 I = 51
38534
XDOT = -5853
912820 Wp = 92
49662
YDOT = 4934
644865 meter/sec RA = 316
99234 deg
ZDOT = -481
289450 TA = 2
10926
MA = 2
10835
Ha = 220
048 n
mi
Hp = 214
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8125608
18 X = 2412261
41
Y = 11327945
77 feet Y = 3480093
01 meter
Z = 17310631
12 Z = 5288155
57
XDOT = -19205
750723 XDOT = -5906
320012
YDOT = 16189
779740 feet/sec YDOT = 4868
889797 meter/sec
ZDOT = -1579
033627 ZDOT = -509
853750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6751153
72 X = 2057751
65
Y = 12127884
34 feet Y = 3696579
15 meter
Z = 17359209
61 Z = 5291087
09
XDOT = -19945
388735 XDOT = -6079
354486
YDOT = 13532
777608 feet/sec YDOT = 4124
790615 meter/sec
ZDOT = -1697
375847 ZDOT = -517
360158
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 12202
20368557
00016717 00000-0 10270-3 0 9145
2 25544 51
6414 317
3562 0001208 199
9705 160
1401 15
54610656 23154
Satellite: ISS
Catalog Number: 25544
Epoch time: 12202
20368557 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 317
3562 deg
Eccentricity:
0001208
Arg of perigee: 199
9705 deg
Mean anomaly: 160
1401 deg
Mean motion: 15
54610656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 283
Coasting Arc #16 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2012/203/03:45:07
432
Vector Time (MET): N/A
Weight (LBS) : 907810
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -949178
77 A = 6778101
92 meter
Y = -4692000
46 meter E =
0011353
Z = -4809490
76 I = 51
37017
XDOT = 6142
724966 Wp = 113
47764
YDOT = -3821
967763 meter/sec RA = 311
97046 deg
ZDOT = 2516
600001 TA = 181
39100
MA = 181
39416
Ha = 220
078 n
mi
Hp = 214
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3114103
58 X = -873278
37
Y = -15393702
28 feet Y = -4702190
05 meter
Z = -15779169
18 Z = -4813917
71
XDOT = 20153
297134 XDOT = 6172
781631
YDOT = -12539
264313 feet/sec YDOT = -3753
108116 meter/sec
ZDOT = 8256
561682 ZDOT = 2546
513217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1608471
59 X = -490262
14
Y = -15605017
45 feet Y = -4756409
32 meter
Z = -15796902
87 Z = -4814896
00
XDOT = 20019
252876 XDOT = 6101
868277
YDOT = -10545
856422 feet/sec YDOT = -3214
377037 meter/sec
ZDOT = 8380
333259 ZDOT = 2554
325577
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 12203
16792791
00016717 00000-0 10270-3 0 9153
2 25544 51
6410 312
5452 0001137 207
8485 152
2607 15
54614357 23309
Satellite: ISS
Catalog Number: 25544
Epoch time: 12203
16792791 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 312
5452 deg
Eccentricity:
0001137
Arg of perigee: 207
8485 deg
Mean anomaly: 152
2607 deg
Mean motion: 15
54614357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 286
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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