[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 5th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24218 8 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
125/11:22:02
504 1
7 1
8 1
9
N/A 0
6 -0
3 188
8
000/00:04:01
009 0
5 -0
0 183
9
Coasting Arc #1 (Orbit 3386)
---------------------------------------
Vector Time (GMT): 2011/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -480752
14 A = 6720108
33 meter
Y = -4653664
60 meter E =
0011464
Z = -4834421
76 I = 51
80562
XDOT = 7063
921376 Wp = 82
27307
YDOT = 1811
841807 meter/sec RA = 29
71219 deg
ZDOT = -2449
978586 TA = 163
84080
MA = 163
80421
Ha = 189
188 n
mi
Hp = 182
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1577270
79 X = -405193
08
Y = -15267928
47 feet Y = -4658618
04 meter
Z = -15860963
76 Z = -4836573
89
XDOT = 23175
595065 XDOT = 7055
037763
YDOT = 5944
362885 feet/sec YDOT = 1890
785265 meter/sec
ZDOT = -8037
987488 ZDOT = -2415
682979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10997613
92 X = -3352072
72
Y = -10694879
28 feet Y = -3259799
20 meter
Z = -15869456
18 Z = -4837010
24
XDOT = 20784
608117 XDOT = 6335
148554
YDOT = -9668
323195 feet/sec YDOT = -2946
904910 meter/sec
ZDOT = -7899
292621 ZDOT = -2407
704391
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 11123
52003929
00016717 00000-0 10270-3 0 9005
2 25544 51
6477 30
1414 0002131 183
1748 176
9402 15
74669001 33873
Satellite: ISS
Catalog Number: 25544
Epoch time: 11123
52003929 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 30
1414 deg
Eccentricity:
0002131
Arg of perigee: 183
1748 deg
Mean anomaly: 176
9402 deg
Mean motion: 15
74669001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3387
Checksum: 282
Coasting Arc #2 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2011/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6324405
43 A = 6728622
24 meter
Y = -1240636
36 meter E =
0014861
Z = 1905267
17 I = 51
80692
XDOT = -688
710047 Wp = 121
54281
YDOT = -5198
249464 meter/sec RA = 24
54723 deg
ZDOT = -5646
568770 TA = 37
31334
MA = 37
21021
Ha = 189
101 n
mi
Hp = 182
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20749361
66 X = -6319317
95
Y = -4070329
26 feet Y = -1311331
35 meter
Z = 6250876
54 Z = 1874555
00
XDOT = -2259
547398 XDOT = -603
100578
YDOT = -17054
624226 feet/sec YDOT = -5205
472085 meter/sec
ZDOT = -18525
488089 ZDOT = -5649
706891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18313426
00 X = -5581932
25
Y = 10642346
03 feet Y = 3243787
07 meter
Z = 6126658
64 Z = 1867405
55
XDOT = -12082
831049 XDOT = -3682
846904
YDOT = -10073
047795 feet/sec YDOT = -3070
264968 meter/sec
ZDOT = -18537
936490 ZDOT = -5650
363042
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 11124
53542296
00016717 00000-0 10270-3 0 9013
2 25544 51
6474 24
9224 0002284 189
1392 170
9730 15
74717236 34031
Satellite: ISS
Catalog Number: 25544
Epoch time: 11124
53542296 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 24
9224 deg
Eccentricity:
0002284
Arg of perigee: 189
1392 deg
Mean anomaly: 170
9730 deg
Mean motion: 15
74717236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3403
Checksum: 298
Coasting Arc #3 (Orbit 3417)
---------------------------------------
Vector Time (GMT): 2011/125/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3493925
04 A = 6720218
53 meter
Y = -2908642
67 meter E =
0011408
Z = -4959437
39 I = 51
74891
XDOT = 6256
313816 Wp = 116
85211
YDOT = 3962
648425 meter/sec RA = 19
54331 deg
ZDOT = 2082
148187 TA = 173
31641
MA = 173
30118
Ha = 188
764 n
mi
Hp = 183
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11463008
65 X = 3550282
75
Y = -9542790
90 feet Y = -2869256
03 meter
Z = -16271120
04 Z = -4942326
96
XDOT = 20525
963962 XDOT = 6201
422893
YDOT = 13000
815043 feet/sec YDOT = 4032
303271 meter/sec
ZDOT = 6831
194838 ZDOT = 2112
408722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4444062
11 X = 1354550
13
Y = -14316730
06 feet Y = -4363739
32 meter
Z = -16201738
34 Z = -4938289
85
XDOT = 23215
707412 XDOT = 7076
147619
YDOT = -667
748290 feet/sec YDOT = -203
529679 meter/sec
ZDOT = 6953
449279 ZDOT = 2119
411340
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 11125
48729033
00016717 00000-0 10270-3 0 9025
2 25544 51
6477 20
0281 0002765 229
4122 130
6801 15
74480191 34182
Satellite: ISS
Catalog Number: 25544
Epoch time: 11125
48729033 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 20
0281 deg
Eccentricity:
0002765
Arg of perigee: 229
4122 deg
Mean anomaly: 130
6801 deg
Mean motion: 15
74480191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3418
Checksum: 281
Coasting Arc #4 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2011/126/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5629764
55 A = 6728826
65 meter
Y = -3083524
13 meter E =
0007088
Z = -2006040
09 I = 51
74950
XDOT = 3930
115834 Wp = 164
26405
YDOT = -3542
613131 meter/sec RA = 14
44717 deg
ZDOT = -5595
357496 TA = 38
05973
MA = 38
00967
Ha = 188
518 n
mi
Hp = 183
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18470356
12 X = -5585120
49
Y = -10116549
00 feet Y = -3146229
80 meter
Z = -6581496
37 Z = -2033281
58
XDOT = 12894
080821 XDOT = 3996
619437
YDOT = -11622
746494 feet/sec YDOT = -3498
291918 meter/sec
ZDOT = -18357
472101 ZDOT = -5576
103524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20930116
49 X = -6379499
51
Y = 1991922
13 feet Y = 607137
86 meter
Z = -6691575
55 Z = -2039592
23
XDOT = 4367
181869 XDOT = 1331
117034
YDOT = -15396
573655 feet/sec YDOT = -4692
875650 meter/sec
ZDOT = -18279
380669 ZDOT = -5571
555228
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 11126
50278577
00016717 00000-0 10270-3 0 9032
2 25544 51
6479 14
8097 0002993 233
7215 126
3672 15
74540341 34344
Satellite: ISS
Catalog Number: 25544
Epoch time: 11126
50278577 = yrday
fracday
Element set: 903
Inclination: 51
6479 deg
RA of node: 14
8097 deg
Eccentricity:
0002993
Arg of perigee: 233
7215 deg
Mean anomaly: 126
3672 deg
Mean motion: 15
74540341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 310
Coasting Arc #5 (Orbit 3449)
---------------------------------------
Vector Time (GMT): 2011/127/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3379317
67 A = 6720298
64 meter
Y = 3282461
25 meter E =
0004370
Z = 4790175
98 I = 51
69161
XDOT = -6587
776199 Wp = 59
04877
YDOT = -3095
090740 meter/sec RA = 9
27478 deg
ZDOT = -2522
664469 TA = 55
63817
MA = 55
59684
Ha = 188
290 n
mi
Hp = 183
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11087000
23 X = -3439041
58
Y = 10769229
84 feet Y = 3244337
36 meter
Z = 15715800
45 Z = 4773614
33
XDOT = -21613
438973 XDOT = -6540
421951
YDOT = -10154
497177 feet/sec YDOT = -3168
494278 meter/sec
ZDOT = -8276
458233 ZDOT = -2554
553322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2932271
43 X = -893756
33
Y = 15244898
52 feet Y = 4646645
07 meter
Z = 15648614
07 Z = 4769697
57
XDOT = -22363
466959 XDOT = -6816
384729
YDOT = 4339
624004 feet/sec YDOT = 1322
717396 meter/sec
ZDOT = -8405
342431 ZDOT = -2561
948373
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 11127
51822262
00016717 00000-0 10270-3 0 9041
2 25544 51
6476 9
5908 0002978 241
8336 118
2527 15
74690526 34508
Satellite: ISS
Catalog Number: 25544
Epoch time: 11127
51822262 = yrday
fracday
Element set: 904
Inclination: 51
6476 deg
RA of node: 9
5908 deg
Eccentricity:
0002978
Arg of perigee: 241
8336 deg
Mean anomaly: 118
2527 deg
Mean motion: 15
74690526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3450
Checksum: 313
Coasting Arc #6 (Orbit 3465)
---------------------------------------
Vector Time (GMT): 2011/128/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5818090
88 A = 6727493
15 meter
Y = 2342470
87 meter E =
0010951
Z = 2420227
31 I = 51
68597
XDOT = -3839
593494 Wp = 76
88951
YDOT = 3972
167563 meter/sec RA = 4
17824 deg
ZDOT = 5367
792312 TA = 310
42199
MA = 310
51747
Ha = 188
048 n
mi
Hp = 183
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19088224
67 X = 5779707
44
Y = 7685271
89 feet Y = 2407317
50 meter
Z = 7940378
31 Z = 2448398
62
XDOT = -12597
091516 XDOT = -3909
801505
YDOT = 13032
045812 feet/sec YDOT = 3928
837957 meter/sec
ZDOT = 17610
867164 ZDOT = 5348
969261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19906520
03 X = 6067507
30
Y = -5033162
08 feet Y = -1534107
80 meter
Z = 8054258
05 Z = 2454937
85
XDOT = -2929
266009 XDOT = -892
840280
YDOT = 16566
163979 feet/sec YDOT = 5049
366781 meter/sec
ZDOT = 17534
492940 ZDOT = 5344
513448
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 11128
53360525
00016717 00000-0 10270-3 0 9054
2 25544 51
6477 4
3709 0002983 246
3799 113
7052 15
74725632 34667
Satellite: ISS
Catalog Number: 25544
Epoch time: 11128
53360525 = yrday
fracday
Element set: 905
Inclination: 51
6477 deg
RA of node: 4
3709 deg
Eccentricity:
0002983
Arg of perigee: 246
3799 deg
Mean anomaly: 113
7052 deg
Mean motion: 15
74725632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3466
Checksum: 315
Coasting Arc #7 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2011/129/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3341601
71 A = 6720891
50 meter
Y = -3659456
23 meter E =
0007833
Z = -4547860
19 I = 51
63376
XDOT = 6677
701510 Wp = 124
93902
YDOT = 2301
010330 meter/sec RA = 358
99408 deg
ZDOT = 3054
309560 TA = 175
47754
MA = 175
47046
Ha = 187
782 n
mi
Hp = 183
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10963260
19 X = 3404366
79
Y = -12006090
01 feet Y = -3621737
21 meter
Z = -14920801
16 Z = -4531474
44
XDOT = 21908
469522 XDOT = 6636
637576
YDOT = 7549
246488 feet/sec YDOT = 2375
454661 meter/sec
ZDOT = 10020
700657 ZDOT = 3086
650244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1556711
30 X = 474485
60
Y = -16244870
13 feet Y = -4951436
41 meter
Z = -14854306
55 Z = -4527592
64
XDOT = 20788
030523 XDOT = 6336
191703
YDOT = -7292
535833 feet/sec YDOT = -2222
764922 meter/sec
ZDOT = 10151
454864 ZDOT = 3094
163442
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 11129
48547231
00016717 00000-0 10270-3 0 9061
2 25544 51
6477 359
4774 0003224 251
3467 108
7347 15
74833810 34816
Satellite: ISS
Catalog Number: 25544
Epoch time: 11129
48547231 = yrday
fracday
Element set: 906
Inclination: 51
6477 deg
RA of node: 359
4774 deg
Eccentricity:
0003224
Arg of perigee: 251
3467 deg
Mean anomaly: 108
7347 deg
Mean motion: 15
74833810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 321
Coasting Arc #8 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2011/130/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5801485
60 A = 6725804
72 meter
Y = -1717687
15 meter E =
0002673
Z = -2935055
35 I = 51
62027
XDOT = 3839
040803 Wp = 159
81634
YDOT = -4404
536664 meter/sec RA = 353
89841 deg
ZDOT = -5014
461970 TA = 54
01607
MA = 53
99128
Ha = 187
532 n
mi
Hp = 183
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19033745
42 X = -5767588
95
Y = -5635456
53 feet Y = -1782373
24 meter
Z = -9629446
69 Z = -2963156
71
XDOT = 12595
278226 XDOT = 3912
367201
YDOT = -14450
579605 feet/sec YDOT = -4361
195985 meter/sec
ZDOT = -16451
646883 ZDOT = -4995
633977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18404855
02 X = -5609799
81
Y = 7287104
06 feet Y = 2221109
32 meter
Z = -9743074
69 Z = -2969689
17
XDOT = 1589
391042 XDOT = 484
446390
YDOT = -17863
346599 feet/sec YDOT = -5444
748043 meter/sec
ZDOT = -16375
233984 ZDOT = -4991
171318
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 11130
50074343
00016717 00000-0 10270-3 0 9076
2 25544 51
6476 354
2575 0003447 255
2130 104
8652 15
74889749 34979
Satellite: ISS
Catalog Number: 25544
Epoch time: 11130
50074343 = yrday
fracday
Element set: 907
Inclination: 51
6476 deg
RA of node: 354
2575 deg
Eccentricity:
0003447
Arg of perigee: 255
2130 deg
Mean anomaly: 104
8652 deg
Mean motion: 15
74889749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 319
Coasting Arc #9 (Orbit 3512)
---------------------------------------
Vector Time (GMT): 2011/131/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3362601
60 A = 6721677
35 meter
Y = 4049765
83 meter E =
0006900
Z = 4176073
50 I = 51
57731
XDOT = -6566
105261 Wp = 70
15516
YDOT = -1658
381366 meter/sec RA = 348
70332 deg
ZDOT = -3671
649704 TA = 57
34900
MA = 57
28244
Ha = 187
321 n
mi
Hp = 183
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11032157
48 X = -3427923
59
Y = 13286633
30 feet Y = 4011797
84 meter
Z = 13701028
53 Z = 4159579
38
XDOT = -21542
340094 XDOT = -6529
236667
YDOT = -5440
883748 feet/sec YDOT = -1731
601312 meter/sec
ZDOT = -12046
094828 ZDOT = -3703
458389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -236736
28 X = -72157
22
Y = 17321001
01 feet Y = 5279441
11 meter
Z = 13634081
78 Z = 4155668
13
XDOT = -18825
752378 XDOT = -5738
089325
YDOT = 9344
611640 feet/sec YDOT = 2848
237628 meter/sec
ZDOT = -12174
724826 ZDOT = -3710
856127
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 11131
51595620
00016717 00000-0 10270-3 0 9085
2 25544 51
6478 349
0368 0003476 263
1720 96
9048 15
75045767 35132
Satellite: ISS
Catalog Number: 25544
Epoch time: 11131
51595620 = yrday
fracday
Element set: 908
Inclination: 51
6478 deg
RA of node: 349
0368 deg
Eccentricity:
0003476
Arg of perigee: 263
1720 deg
Mean anomaly: 96
9048 deg
Mean motion: 15
75045767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3513
Checksum: 321
Coasting Arc #10 (Orbit 3528)
---------------------------------------
Vector Time (GMT): 2011/132/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5616214
02 A = 6723759
08 meter
Y = 1227651
88 meter E =
0008758
Z = 3480196
07 I = 51
55391
XDOT = -3877
005712 Wp = 93
94410
YDOT = 4884
000200 meter/sec RA = 343
60527 deg
ZDOT = 4523
384855 TA = 307
44982
MA = 307
52946
Ha = 187
098 n
mi
Hp = 183
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18425899
01 X = 5585162
51
Y = 4027729
26 feet Y = 1290282
13 meter
Z = 11417966
11 Z = 3507404
38
XDOT = -12719
835014 XDOT = -3953
305299
YDOT = 16023
622705 feet/sec YDOT = 4840
218495 meter/sec
ZDOT = 14840
501494 ZDOT = 4504
364987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16634441
58 X = 5070177
79
Y = -8746823
32 feet Y = -2666031
75 meter
Z = 11527998
19 Z = 3513733
85
XDOT = -109
000002 XDOT = -33
223201
YDOT = 19294
473220 feet/sec YDOT = 5880
955437 meter/sec
ZDOT = 14763
297280 ZDOT = 4499
853011
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 11132
53111516
00016717 00000-0 10270-3 0 9097
2 25544 51
6469 343
8153 0003523 267
8424 92
2336 15
75069403 35290
Satellite: ISS
Catalog Number: 25544
Epoch time: 11132
53111516 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 343
8153 deg
Eccentricity:
0003523
Arg of perigee: 267
8424 deg
Mean anomaly: 92
2336 deg
Mean motion: 15
75069403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3529
Checksum: 301
Coasting Arc #11 (Orbit 3543)
---------------------------------------
Vector Time (GMT): 2011/133/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3402039
52 A = 6723003
92 meter
Y = -4487903
40 meter E =
0002120
Z = -3674493
88 I = 51
52213
XDOT = 6258
675407 Wp = 118
20895
YDOT = 1211
498143 meter/sec RA = 338
40161 deg
ZDOT = 4315
826701 TA = 197
52258
MA = 197
52989
Ha = 186
953 n
mi
Hp = 183
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11161546
99 X = 3469821
49
Y = -14724092
53 feet Y = -4449480
69 meter
Z = -12055426
12 Z = -3657802
02
XDOT = 20533
711966 XDOT = 6223
697313
YDOT = 3974
731441 feet/sec YDOT = 1281
290819 meter/sec
ZDOT = 14159
536422 ZDOT = 4346
146720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1214010
70 X = -370030
46
Y = -18480649
12 feet Y = -5632901
85 meter
Z = -11987665
22 Z = -3653840
36
XDOT = 16675
125051 XDOT = 5082
578116
YDOT = -10357
747454 feet/sec YDOT = -3157
041424 meter/sec
ZDOT = 14282
154259 ZDOT = 4353
200618
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 11133
48277196
00016717 00000-0 10270-3 0 9101
2 25544 51
6460 338
9199 0003711 270
4351 89
6388 15
75180917 35442
Satellite: ISS
Catalog Number: 25544
Epoch time: 11133
48277196 = yrday
fracday
Element set: 910
Inclination: 51
6460 deg
RA of node: 338
9199 deg
Eccentricity:
0003711
Arg of perigee: 270
4351 deg
Mean anomaly: 89
6388 deg
Mean motion: 15
75180917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3544
Checksum: 327
Coasting Arc #12 (Orbit 3559)
---------------------------------------
Vector Time (GMT): 2011/134/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5278100
18 A = 6721330
65 meter
Y = -957182
69 meter E =
0004404
Z = -4054816
10 I = 51
48811
XDOT = 3927
049292 Wp = 49
28219
YDOT = -5394
181533 meter/sec RA = 333
29933 deg
ZDOT = -3838
322769 TA = 181
12929
MA = 181
13029
Ha = 186
785 n
mi
Hp = 183
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17316601
64 X = -5247306
63
Y = -3140363
16 feet Y = -1016033
32 meter
Z = -13303202
43 Z = -4080382
73
XDOT = 12884
019986 XDOT = 4005
722357
YDOT = -17697
445975 feet/sec YDOT = -5349
826891 meter/sec
ZDOT = -12592
922469 ZDOT = -3819
053923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14897406
96 X = -4540729
64
Y = 9221292
49 feet Y = 2810649
95 meter
Z = -13406595
36 Z = -4086330
26
XDOT = -1571
414685 XDOT = -478
967196
YDOT = -20733
996801 feet/sec YDOT = -6319
722225 meter/sec
ZDOT = -12514
691689 ZDOT = -3814
478027
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 11134
49781815
00016717 00000-0 10270-3 0 9112
2 25544 51
6449 333
6984 0003812 275
1806 84
8923 15
75258144 35600
Satellite: ISS
Catalog Number: 25544
Epoch time: 11134
49781815 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 333
6984 deg
Eccentricity:
0003812
Arg of perigee: 275
1806 deg
Mean anomaly: 84
8923 deg
Mean motion: 15
75258144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3560
Checksum: 326
Coasting Arc #13 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2011/135/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3439828
69 A = 6724380
45 meter
Y = 4941657
65 meter E =
0009290
Z = 2985202
42 I = 51
47295
XDOT = -5803
837151 Wp = 94
89315
YDOT = -1037
080804 meter/sec RA = 328
09223 deg
ZDOT = -4958
529063 TA = 50
50973
MA = 50
42761
Ha = 186
601 n
mi
Hp = 183
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11285527
18 X = -3509333
43
Y = 16212787
57 feet Y = 4902802
62 meter
Z = 9793971
19 Z = 2968322
85
XDOT = -19041
460469 XDOT = -5767
720871
YDOT = -3402
496075 feet/sec YDOT = -1101
780634 meter/sec
ZDOT = -16268
139971 ZDOT = -4986
636955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2784864
20 X = 848826
61
Y = 19590814
90 feet Y = 5971280
38 meter
Z = 9725429
52 Z = 2964310
92
XDOT = -14734
140782 XDOT = -4490
966110
YDOT = 10247
249384 feet/sec YDOT = 3123
361612 meter/sec
ZDOT = -16381
806573 ZDOT = -4993
174643
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 11135
51280512
00016717 00000-0 10270-3 0 9125
2 25544 51
6454 328
4757 0004043 281
4866 78
5844 15
75395766 35760
Satellite: ISS
Catalog Number: 25544
Epoch time: 11135
51280512 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 328
4757 deg
Eccentricity:
0004043
Arg of perigee: 281
4866 deg
Mean anomaly: 78
5844 deg
Mean motion: 15
75395766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3576
Checksum: 329
Coasting Arc #14 (Orbit 3591)
---------------------------------------
Vector Time (GMT): 2011/136/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4830765
26 A = 6718931
03 meter
Y = 926711
12 meter E =
0004462
Z = 4575071
10 I = 51
42790
XDOT = -3939
912545 Wp = 124
59059
YDOT = 5923
607495 meter/sec RA = 322
97823 deg
ZDOT = 2955
706704 TA = 295
99743
MA = 296
04339
Ha = 186
500 n
mi
Hp = 182
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15848967
39 X = 4797818
27
Y = 3040390
81 feet Y = 980547
07 meter
Z = 15010075
77 Z = 4598459
45
XDOT = -12926
222261 XDOT = -4020
217197
YDOT = 19434
407792 feet/sec YDOT = 5879
099748 meter/sec
ZDOT = 9697
200474 ZDOT = 2936
371669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13439871
35 X = 4096472
79
Y = -8772425
72 feet Y = -2673835
36 meter
Z = 15104652
38 Z = 4603898
04
XDOT = 3543
247327 XDOT = 1079
981785
YDOT = 22015
671970 feet/sec YDOT = 6710
376816 meter/sec
ZDOT = 9618
671708 ZDOT = 2931
771136
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 11136
52773798
00016717 00000-0 10270-3 0 9131
2 25544 51
6439 323
2520 0003973 285
3441 74
7284 15
75408379 35926
Satellite: ISS
Catalog Number: 25544
Epoch time: 11136
52773798 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 323
2520 deg
Eccentricity:
0003973
Arg of perigee: 285
3441 deg
Mean anomaly: 74
7284 deg
Mean motion: 15
75408379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3592
Checksum: 331
Coasting Arc #15 (Orbit 3606)
---------------------------------------
Vector Time (GMT): 2011/137/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3415119
45 A = 6725900
37 meter
Y = -5386639
59 meter E =
0006054
Z = -2123674
98 I = 51
42778
XDOT = 5255
951551 Wp = 3
12549
YDOT = 1162
949803 meter/sec RA = 317
77373 deg
ZDOT = 5509
088575 TA = 333
04124
MA = 333
07268
Ha = 186
484 n
mi
Hp = 182
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11204460
15 X = 3485416
67
Y = -17672702
06 feet Y = -5348056
36 meter
Z = -6967437
58 Z = -2106913
89
XDOT = 17243
935536 XDOT = 5215
793982
YDOT = 3815
452109 feet/sec YDOT = 1221
499899 meter/sec
ZDOT = 18074
437583 ZDOT = 5534
525004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4559311
42 X = -1389678
12
Y = -20445567
02 feet Y = -6231808
83 meter
Z = -6899346
36 Z = -2102920
77
XDOT = 13317
301800 XDOT = 4059
113588
YDOT = -9096
165663 feet/sec YDOT = -2772
511294 meter/sec
ZDOT = 18177
289204 ZDOT = 5540
437749
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 11137
47918076
00016717 00000-0 10270-3 0 9147
2 25544 51
6432 318
3543 0004037 287
1422 72
9299 15
75528146 36078
Satellite: ISS
Catalog Number: 25544
Epoch time: 11137
47918076 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 318
3543 deg
Eccentricity:
0004037
Arg of perigee: 287
1422 deg
Mean anomaly: 72
9299 deg
Mean motion: 15
75528146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3607
Checksum: 319
Coasting Arc #16 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2011/138/11:24:03
009
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4335610
34 A = 6716570
86 meter
Y = -1188828
43 meter E =
0010378
Z = -4999397
87 I = 51
37494
XDOT = 3878
768954 Wp = 62
95717
YDOT = -6386
002781 meter/sec RA = 312
64370 deg
ZDOT = -1843
501111 TA = 189
17752
MA = 189
19650
Ha = 186
436 n
mi
Hp = 182
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14224443
37 X = -4297707
93
Y = -3900355
75 feet Y = -1237099
28 meter
Z = -16402223
99 Z = -5020368
62
XDOT = 12725
619929 XDOT = 3958
845684
YDOT = -20951
452692 feet/sec YDOT = -6342
180059 meter/sec
ZDOT = -6048
231990 ZDOT = -1824
464144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12615385
48 X = -3845169
49
Y = 7457283
02 feet Y = 2272979
86 meter
Z = -16487009
89 Z = -5025240
62
XDOT = -5673
779464 XDOT = -1729
367981
YDOT = -22811
407122 feet/sec YDOT = -6952
916891 meter/sec
ZDOT = -5970
877635 ZDOT = -1819
923503
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 11138
49399763
00016717 00000-0 10270-3 0 9157
2 25544 51
6428 313
1308 0003990 292
4698 67
6044 15
75624286 36235
Satellite: ISS
Catalog Number: 25544
Epoch time: 11138
49399763 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 313
1308 deg
Eccentricity:
0003990
Arg of perigee: 292
4698 deg
Mean anomaly: 67
6044 deg
Mean motion: 15
75624286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 336
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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