[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 30th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 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
028/23:50:31
818 1
9 3
2 3
3
N/A -2
3 -0
3 219
0
000/00:01:03
636 -1
2 0
1 204
9
Coasting Arc #1 (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 = -3318497
05 A = 6774349
32 meter
Y = 5764930
42 meter E =
0026493
Z = 1186411
61 I = 51
98198
XDOT = -3646
497340 Wp =
67454
YDOT = -3309
694151 meter/sec RA = 111
91084 deg
ZDOT = 5907
133788 TA = 12
20363
MA = 12
13958
Ha = 218
213 n
mi
Hp = 204
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10887457
52 X = -3388478
23
Y = 18913813
72 feet Y = 5727429
68 meter
Z = 3892426
54 Z = 1170120
72
XDOT = -11963
573950 XDOT = -3637
911639
YDOT = -10858
576612 feet/sec YDOT = -3350
423411 meter/sec
ZDOT = 19380
360197 ZDOT = 5889
440525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21738366
86 X = -6625854
22
Y = 2056909
60 feet Y = 626946
05 meter
Z = 3825257
43 Z = 1165938
46
XDOT = 2006
366240 XDOT = 611
540430
YDOT = -14551
317693 feet/sec YDOT = -4435
241633 meter/sec
ZDOT = 19308
061765 ZDOT = 5885
097226
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
56184475
00016717 00000-0 10270-3 0 9009
2 25544 51
6427 112
4890 0022286 329
5247 30
4612 15
59099512 35936
Satellite: ISS
Catalog Number: 25544
Epoch time: 12027
56184475 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 112
4890 deg
Eccentricity:
0022286
Arg of perigee: 329
5247 deg
Mean anomaly: 30
4612 deg
Mean motion: 15
59099512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 309
Coasting Arc #2 (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 = 4311880
96 A = 6767955
61 meter
Y = -3317047
09 meter E =
0022251
Z = -4039544
49 I = 51
97015
XDOT = 1254
626742 Wp = 351
20688
YDOT = 6455
821396 meter/sec RA = 106
92542 deg
ZDOT = -3937
661689 TA = 237
98029
MA = 238
19667
Ha = 218
343 n
mi
Hp = 203
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14146591
07 X = 4368275
26
Y = -10882700
43 feet Y = -3268513
74 meter
Z = -13253098
71 Z = -4018460
86
XDOT = 4116
229470 XDOT = 1201
471178
YDOT = 21180
516390 feet/sec YDOT = 6469
554124 meter/sec
ZDOT = -12918
837562 ZDOT = -3931
696094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17199806
82 X = 5242501
12
Y = 5001523
02 feet Y = 1524464
22 meter
Z = -13166443
94 Z = -4013132
11
XDOT = -14201
982760 XDOT = -4328
764345
YDOT = 14682
788531 feet/sec YDOT = 4475
313944 meter/sec
ZDOT = -12894
832155 ZDOT = -3930
344841
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
52327927
00016717 00000-0 10270-3 0 9018
2 25544 51
6415 107
6606 0022265 333
0133 26
9863 15
59138941 36080
Satellite: ISS
Catalog Number: 25544
Epoch time: 12028
52327927 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 107
6606 deg
Eccentricity:
0022265
Arg of perigee: 333
0133 deg
Mean anomaly: 26
9863 deg
Mean motion: 15
59138941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 302
Coasting Arc #3 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2012/028/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2469043
95 A = 6767956
38 meter
Y = -4449828
60 meter E =
0022666
Z = 4473226
71 I = 51
96943
XDOT = 4088
218772 Wp = 3
63860
YDOT = -5592
052772 meter/sec RA = 104
40946 deg
ZDOT = -3283
317025 TA = 119
41428
MA = 119
18784
Ha = 219
025 n
mi
Hp = 204
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8100537
91 X = -2440831
19
Y = -14599175
19 feet Y = -4477281
15 meter
Z = 14675940
64 Z = 4461300
97
XDOT = 13412
791247 XDOT = 4166
395762
YDOT = -18346
629829 feet/sec YDOT = -5545
898729 meter/sec
ZDOT = -10772
037485 ZDOT = -3263
266961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7360377
40 X = -2243443
03
Y = 15033391
07 feet Y = 4582177
60 meter
Z = 14627366
87 Z = 4458421
42
XDOT = -21659
607706 XDOT = -6601
848429
YDOT = -130
325716 feet/sec YDOT = -39
723278 meter/sec
ZDOT = -10689
455909 ZDOT = -3258
146161
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
03605692
00016717 00000-0 10270-3 0 9024
2 25544 51
6419 105
0866 0020612 339
8773 20
1567 15
58585100 36160
Satellite: ISS
Catalog Number: 25544
Epoch time: 12029
03605692 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 105
0866 deg
Eccentricity:
0020612
Arg of perigee: 339
8773 deg
Mean anomaly: 20
1567 deg
Mean motion: 15
58585100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 298
Coasting Arc #4 (Orbit 3630)
---------------------------------------
Vector Time (GMT): 2012/029/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 560724
32 A = 6774546
78 meter
Y = 6415262
52 meter E =
0024817
Z = -2051669
86 I = 51
99895
XDOT = -4794
674719 Wp = 356
38506
YDOT = 2201
203866 meter/sec RA = 99
41862 deg
ZDOT = 5592
901788 TA = 340
95684
MA = 341
04946
Ha = 219
190 n
mi
Hp = 204
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1839646
72 X = 498912
32
Y = 21047449
23 feet Y = 6421187
27 meter
Z = -6731200
33 Z = -2049096
09
XDOT = -15730
560103 XDOT = -4846
101388
YDOT = 7221
797460 feet/sec YDOT = 2147
299345 meter/sec
ZDOT = 18349
415316 ZDOT = 5569
484841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16016924
59 X = 4881958
62
Y = -13783079
75 feet Y = -4201082
71 meter
Z = -6721109
74 Z = -2048594
25
XDOT = 14090
690744 XDOT = 4294
842539
YDOT = 7506
246656 feet/sec YDOT = 2287
903981 meter/sec
ZDOT = 18253
262923 ZDOT = 5563
594539
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
99783046
00016717 00000-0 10270-3 0 9030
2 25544 51
6425 100
2592 0020622 343
4311 16
6167 15
58608736 36314
Satellite: ISS
Catalog Number: 25544
Epoch time: 12029
99783046 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 100
2592 deg
Eccentricity:
0020622
Arg of perigee: 343
4311 deg
Mean anomaly: 16
6167 deg
Mean motion: 15
58608736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3631
Checksum: 298
Coasting Arc #5 (Orbit 3646)
---------------------------------------
Vector Time (GMT): 2012/030/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1392627
71 A = 6775786
18 meter
Y = -6543425
98 meter E =
0012636
Z = -1127275
67 I = 52
00713
XDOT = 4469
874182 Wp = 5
47399
YDOT = 1969
101569 meter/sec RA = 94
45201 deg
ZDOT = -5901
068679 TA = 186
69755
MA = 186
71445
Ha = 219
301 n
mi
Hp = 204
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4568988
53 X = 1471170
09
Y = -21467933
02 feet Y = -6527413
60 meter
Z = -3698411
00 Z = -1120319
70
XDOT = 14664
941542 XDOT = 4476
188816
YDOT = 6460
306985 feet/sec YDOT = 2019
121804 meter/sec
ZDOT = -19360
461546 ZDOT = -5879
339127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19973554
42 X = -6087939
39
Y = 9111452
74 feet Y = 2777170
79 meter
Z = -3669414
27 Z = -1118437
47
XDOT = -2961
591578 XDOT = -902
693113
YDOT = -14262
408818 feet/sec YDOT = -4347
182208 meter/sec
ZDOT = -19271
525136 ZDOT = -5873
960861
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
02369950
00016717 00000-0 10270-3 0 9042
2 25544 51
6425 95
1104 0020529 347
0966 12
9661 15
58610493 36475
Satellite: ISS
Catalog Number: 25544
Epoch time: 12031
02369950 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 95
1104 deg
Eccentricity:
0020529
Arg of perigee: 347
0966 deg
Mean anomaly: 12
9661 deg
Mean motion: 15
58610493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3647
Checksum: 301
Coasting Arc #6 (Orbit 3662)
---------------------------------------
Vector Time (GMT): 2012/031/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3008360
26 A = 6769743
89 meter
Y = 4623047
11 meter E =
0020327
Z = 3903438
90 I = 51
98872
XDOT = -3274
101396 Wp = 22
92121
YDOT = -5602
067037 meter/sec RA = 89
47071 deg
ZDOT = 4122
570611 TA = 24
23318
MA = 24
13771
Ha = 219
597 n
mi
Hp = 203
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9869948
37 X = -3078794
32
Y = 15167477
41 feet Y = 4589011
88 meter
Z = 12806558
08 Z = 3888653
60
XDOT = -10741
802479 XDOT = -3231
240906
YDOT = -18379
485029 feet/sec YDOT = -5638
440487 meter/sec
ZDOT = 13525
494132 ZDOT = 4106
769357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18087501
66 X = 5513070
51
Y = -1366847
75 feet Y = -416615
20 meter
Z = 12745595
03 Z = 3884857
37
XDOT = -8064
277064 XDOT = -2457
991649
YDOT = 18467
238618 feet/sec YDOT = 5628
814331 meter/sec
ZDOT = 13461
134308 ZDOT = 4102
953737
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
04954446
00016717 00000-0 10270-3 0 9056
2 25544 51
6426 89
9606 0020740 351
4518 8
6281 15
58653686 36630
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
04954446 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 89
9606 deg
Eccentricity:
0020740
Arg of perigee: 351
4518 deg
Mean anomaly: 8
6281 deg
Mean motion: 15
58653686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3663
Checksum: 320
Coasting Arc #7 (Orbit 3677)
---------------------------------------
Vector Time (GMT): 2012/032/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4018330
51 A = 6764236
54 meter
Y = -1361486
32 meter E =
0025598
Z = -5281683
11 I = 51
96937
XDOT = 1394
337716 Wp = 29
16234
YDOT = 7488
621243 meter/sec RA = 84
45689 deg
ZDOT = -849
529038 TA = 232
63168
MA = 232
86508
Ha = 219
589 n
mi
Hp = 203
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13183499
04 X = 4058913
15
Y = -4466818
63 feet Y = -1316323
81 meter
Z = -17328356
66 Z = -5262063
96
XDOT = 4574
598806 XDOT = 1314
621590
YDOT = 24568
967334 feet/sec YDOT = 7503
767894 meter/sec
ZDOT = -2787
168759 ZDOT = -842
948899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11777293
82 X = -3589719
16
Y = -7605083
36 feet Y = -2318029
41 meter
Z = -17247814
85 Z = -5257133
97
XDOT = 15793
715931 XDOT = 4813
924616
YDOT = -18047
298767 feet/sec YDOT = -5500
816664 meter/sec
ZDOT = -2760
765580 ZDOT = -841
481349
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 12033
01125078
00016717 00000-0 10270-3 0 9066
2 25544 51
6424 85
1334 0020776 354
6686 5
4244 15
58729479 36788
Satellite: ISS
Catalog Number: 25544
Epoch time: 12033
01125078 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 85
1334 deg
Eccentricity:
0020776
Arg of perigee: 354
6686 deg
Mean anomaly: 5
4244 deg
Mean motion: 15
58729479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3678
Checksum: 318
Coasting Arc #8 (Orbit 3693)
---------------------------------------
Vector Time (GMT): 2012/033/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4211352
92 A = 6766379
13 meter
Y = -2383360
28 meter E =
0025187
Z = 4734886
66 I = 51
97350
XDOT = 876
797255 Wp = 14
44203
YDOT = -7100
454465 meter/sec RA = 79
43238 deg
ZDOT = -2767
308685 TA = 102
95469
MA = 102
67330
Ha = 219
671 n
mi
Hp = 203
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13816774
66 X = -4207389
35
Y = -7819423
50 feet Y = -2430432
24 meter
Z = 15534405
07 Z = 4714437
96
XDOT = 2876
631415 XDOT = 969
573540
YDOT = -23295
454283 feet/sec YDOT = -7090
130735 meter/sec
ZDOT = -9079
096736 ZDOT = -2762
824229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2829054
42 X = 862295
79
Y = 15704623
84 feet Y = 4786769
35 meter
Z = 15450748
45 Z = 4709388
13
XDOT = -18684
339628 XDOT = -5694
986719
YDOT = 12366
935177 feet/sec YDOT = 3769
441842 meter/sec
ZDOT = -9060
154176 ZDOT = -2761
534993
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 12034
03704792
00016717 00000-0 10270-3 0 9076
2 25544 51
6428 79
9837 0020816 358
2471 1
8608 15
58786555 36948
Satellite: ISS
Catalog Number: 25544
Epoch time: 12034
03704792 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 79
9837 deg
Eccentricity:
0020816
Arg of perigee: 358
2471 deg
Mean anomaly: 1
8608 deg
Mean motion: 15
58786555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3694
Checksum: 338
Coasting Arc #9 (Orbit 3708)
---------------------------------------
Vector Time (GMT): 2012/034/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3475801
63 A = 6773278
50 meter
Y = 5238277
95 meter E =
0024845
Z = -2485624
59 I = 51
98898
XDOT = -3076
352588 Wp = 10
77675
YDOT = 4569
509756 meter/sec RA = 74
43515 deg
ZDOT = 5360
402029 TA = 321
40454
MA = 321
58189
Ha = 219
861 n
mi
Hp = 203
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11403548
64 X = 3429042
19
Y = 17185951
28 feet Y = 5276885
15 meter
Z = -8154936
32 Z = -2468853
01
XDOT = -10093
020302 XDOT = -3153
260233
YDOT = 14991
829907 feet/sec YDOT = 4534
677865 meter/sec
ZDOT = 17586
620831 ZDOT = 5345
270913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5617591
52 X = 1712241
89
Y = -19873366
17 feet Y = -6057402
01 meter
Z = -8086582
23 Z = -2464790
26
XDOT = 16574
272978 XDOT = 5051
838404
YDOT = -2402
126609 feet/sec YDOT = -732
168190 meter/sec
ZDOT = 17524
214237 ZDOT = 5341
380499
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 12034
99871275
00016717 00000-0 10270-3 0 9083
2 25544 51
6419 75
1558 0020831 1
8081 358
3146 15
58767497 37099
Satellite: ISS
Catalog Number: 25544
Epoch time: 12034
99871275 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 75
1558 deg
Eccentricity:
0020831
Arg of perigee: 1
8081 deg
Mean anomaly: 358
3146 deg
Mean motion: 15
58767497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3709
Checksum: 336
Coasting Arc #10 (Orbit 3724)
---------------------------------------
Vector Time (GMT): 2012/035/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1824067
13 A = 6775548
46 meter
Y = -6494201
96 meter E =
0015309
Z = -728962
66 I = 51
98735
XDOT = 4741
012027 Wp = 34
90368
YDOT = -666
088942 meter/sec RA = 69
46571 deg
ZDOT = -5978
987150 TA = 152
93405
MA = 152
85414
Ha = 219
843 n
mi
Hp = 202
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5984472
20 X = -1747771
04
Y = -21306436
89 feet Y = -6514173
19 meter
Z = -2391609
78 Z = -737638
57
XDOT = 15554
501400 XDOT = 4777
151891
YDOT = -2185
331176 feet/sec YDOT = -612
869773 meter/sec
ZDOT = -19616
099572 ZDOT = -5955
868308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11995049
04 X = -3656090
95
Y = 18593763
85 feet Y = 5667379
22 meter
Z = -2426664
76 Z = -739647
42
XDOT = -10670
873139 XDOT = -3252
482133
YDOT = -9410
626568 feet/sec YDOT = -2868
358978 meter/sec
ZDOT = -19521
244715 ZDOT = -5950
075389
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 12036
02446424
00016717 00000-0 10270-3 0 9094
2 25544 51
6415 70
0062 0020666 5
8872 354
2522 15
58795090 37258
Satellite: ISS
Catalog Number: 25544
Epoch time: 12036
02446424 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 70
0062 deg
Eccentricity:
0020666
Arg of perigee: 5
8872 deg
Mean anomaly: 354
2522 deg
Mean motion: 15
58795090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3725
Checksum: 296
Coasting Arc #11 (Orbit 3740)
---------------------------------------
Vector Time (GMT): 2012/036/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -459554
99 A = 6769969
55 meter
Y = 5664428
42 meter E =
0024819
Z = 3648206
47 I = 51
95662
XDOT = -5385
895575 Wp = 37
68527
YDOT = -3274
406129 meter/sec RA = 64
48420 deg
ZDOT = 4409
051471 TA = 5
62500
MA = 5
59718
Ha = 219
993 n
mi
Hp = 202
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1507726
34 X = -540583
29
Y = 18584082
74 feet Y = 5658836
29 meter
Z = 11969181
34 Z = 3645777
30
XDOT = -17670
261073 XDOT = -5370
297821
YDOT = -10742
802259 feet/sec YDOT = -3334
547377 meter/sec
ZDOT = 14465
391964 ZDOT = 4382
925577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14768410
94 X = 4501411
65
Y = -11392310
00 feet Y = -3472376
09 meter
Z = 11958761
77 Z = 3645030
59
XDOT = 3248
793937 XDOT = 990
232392
YDOT = 19272
119213 feet/sec YDOT = 5874
141936 meter/sec
ZDOT = 14358
520346 ZDOT = 4376
477001
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 12037
05019024
00016717 00000-0 10270-3 0 9102
2 25544 51
6406 64
8549 0020808 9
6192 350
5357 15
58841786 37411
Satellite: ISS
Catalog Number: 25544
Epoch time: 12037
05019024 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 64
8549 deg
Eccentricity:
0020808
Arg of perigee: 9
6192 deg
Mean anomaly: 350
5357 deg
Mean motion: 15
58841786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3741
Checksum: 307
Coasting Arc #12 (Orbit 3755)
---------------------------------------
Vector Time (GMT): 2012/037/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2856908
39 A = 6763975
72 meter
Y = -3226853
30 meter E =
0029208
Z = -5233079
21 I = 51
92147
XDOT = 4606
755622 Wp = 39
91800
YDOT = 6005
910972 meter/sec RA = 59
46785 deg
ZDOT = -1170
228789 TA = 218
78483
MA = 218
99484
Ha = 219
980 n
mi
Hp = 202
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9373059
03 X = 2918199
77
Y = -10586789
05 feet Y = -3194562
95 meter
Z = -17168895
05 Z = -5219051
97
XDOT = 15114
027630 XDOT = 4544
938483
YDOT = 19704
432322 feet/sec YDOT = 6057
080900 meter/sec
ZDOT = -3839
333296 ZDOT = -1148
000232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14203718
80 X = -4329293
49
Y = 411838
62 feet Y = 125528
41 meter
Z = -17111109
15 Z = -5215466
07
XDOT = 3906
547110 XDOT = 1190
715559
YDOT = -23507
253746 feet/sec YDOT = -7165
010942 meter/sec
ZDOT = -3748
664452 ZDOT = -1142
592925
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 12038
01178509
00016717 00000-0 10270-3 0 9114
2 25544 51
6392 60
0259 0020703 13
4110 346
7591 15
58890914 37568
Satellite: ISS
Catalog Number: 25544
Epoch time: 12038
01178509 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 60
0259 deg
Eccentricity:
0020703
Arg of perigee: 13
4110 deg
Mean anomaly: 346
7591 deg
Mean motion: 15
58890914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3756
Checksum: 296
Coasting Arc #13 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2012/038/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4738268
57 A = 6765584
24 meter
Y = -123049
53 meter E =
0026403
Z = 4826424
47 I = 51
91118
XDOT = -2435
221685 Wp = 27
76828
YDOT = -6824
114521 meter/sec RA = 54
43650 deg
ZDOT = -2536
351196 TA = 87
20393
MA = 86
90176
Ha = 220
077 n
mi
Hp = 202
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15545500
54 X = -4759985
46
Y = -403705
82 feet Y = -176157
02 meter
Z = 15834725
95 Z = 4803354
08
XDOT = -7989
572457 XDOT = -2346
411405
YDOT = -22388
827169 feet/sec YDOT = -6850
850197 meter/sec
ZDOT = -8321
362192 ZDOT = -2547
965096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10671438
17 X = 3252654
36
Y = 11442592
48 feet Y = 3487702
19 meter
Z = 15740126
94 Z = 4797590
69
XDOT = -9578
473070 XDOT = -2919
518592
YDOT = 20573
153318 feet/sec YDOT = 6270
697131 meter/sec
ZDOT = -8368
433999 ZDOT = -2550
698683
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 12039
03746161
00016717 00000-0 10270-3 0 9123
2 25544 51
6396 54
8747 0020626 17
1095 343
0751 15
58931045 37729
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039
03746161 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 54
8747 deg
Eccentricity:
0020626
Arg of perigee: 17
1095 deg
Mean anomaly: 343
0751 deg
Mean motion: 15
58931045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3772
Checksum: 306
Coasting Arc #14 (Orbit 3786)
---------------------------------------
Vector Time (GMT): 2012/039/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5390207
04 A = 6772414
39 meter
Y = 3122360
10 meter E =
0025033
Z = -2633456
30 I = 51
91486
XDOT = -669
217966 Wp = 26
85277
YDOT = 5558
013479 meter/sec RA = 49
43034 deg
ZDOT = 5261
226135 TA = 303
49607
MA = 303
73504
Ha = 220
112 n
mi
Hp = 201
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17684406
29 X = 5367683
98
Y = 10243963
59 feet Y = 3182510
63 meter
Z = -8639948
49 Z = -2607326
48
XDOT = -2195
597001 XDOT = -756
876240
YDOT = 18234
952360 feet/sec YDOT = 5550
040052 meter/sec
ZDOT = 17261
240601 ZDOT = 5257
761952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5458304
52 X = -1663691
22
Y = -19741319
55 feet Y = -6017154
20 meter
Z = -8533049
87 Z = -2600873
60
XDOT = 12990
073687 XDOT = 3959
374460
YDOT = -10987
302041 feet/sec YDOT = -3348
929662 meter/sec
ZDOT = 17246
580775 ZDOT = 5256
757820
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 12039
99901074
00016717 00000-0 10270-3 0 9135
2 25544 51
6386 50
0449 0020566 21
0516 339
1482 15
58963439 37875
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039
99901074 = yrday
fracday
Element set: 913
Inclination: 51
6386 deg
RA of node: 50
0449 deg
Eccentricity:
0020566
Arg of perigee: 21
0516 deg
Mean anomaly: 339
1482 deg
Mean motion: 15
58963439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3787
Checksum: 324
Coasting Arc #15 (Orbit 3802)
---------------------------------------
Vector Time (GMT): 2012/040/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4458606
76 A = 6774883
62 meter
Y = -5072580
43 meter E =
0018929
Z = -635702
71 I = 51
90371
XDOT = 3930
676072 Wp = 55
21111
YDOT = -2719
135631 meter/sec RA = 44
45367 deg
ZDOT = -5986
952635 TA = 131
62802
MA = 131
46574
Ha = 220
076 n
mi
Hp = 201
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14627974
94 X = -4398464
74
Y = -16642324
23 feet Y = -5122103
09 meter
Z = -2085638
80 Z = -657215
50
XDOT = 12895
918871 XDOT = 3989
872492
YDOT = -8921
048658 feet/sec YDOT = -2674
849828 meter/sec
ZDOT = -19642
233055 ZDOT = -5967
714027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -874109
27 X = -266428
50
Y = 22131574
51 feet Y = 6745703
91 meter
Z = -2173439
34 Z = -662464
31
XDOT = -13966
185140 XDOT = -4256
893231
YDOT = -2437
007517 feet/sec YDOT = -742
799891 meter/sec
ZDOT = -19563
118496 ZDOT = -5962
838518
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 12041
02463641
00016717 00000-0 10270-3 0 9146
2 25544 51
6389 44
8937 0020749 24
8845 335
3306 15
59040870 38038
Satellite: ISS
Catalog Number: 25544
Epoch time: 12041
02463641 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 44
8937 deg
Eccentricity:
0020749
Arg of perigee: 24
8845 deg
Mean anomaly: 335
3306 deg
Mean motion: 15
59040870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3803
Checksum: 308
Coasting Arc #16 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2012/041/23:51:03
636
Vector Time (MET): N/A
Weight (LBS) : 884810
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2018477
40 A = 6769397
53 meter
Y = 5334707
89 meter E =
0027607
Z = 3611319
16 I = 51
86269
XDOT = -6255
151163 Wp = 51
58636
YDOT = -639
574929 meter/sec RA = 39
46582 deg
ZDOT = 4434
975524 TA = 351
26667
MA = 351
31460
Ha = 220
013 n
mi
Hp = 201
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6622301
18 X = 1941130
93
Y = 17502322
47 feet Y = 5356847
54 meter
Z = 11848159
96 Z = 3620936
40
XDOT = -20522
149485 XDOT = -6269
078158
YDOT = -2098
342944 feet/sec YDOT = -709
601432 meter/sec
ZDOT = 14550
444631 ZDOT = 4404
555019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7015156
50 X = 2138219
70
Y = -17321900
02 feet Y = -5279715
13 meter
Z = 11887153
50 Z = 3623204
39
XDOT = 12497
540217 XDOT = 3809
250258
YDOT = 14974
520101 feet/sec YDOT = 4564
233727 meter/sec
ZDOT = 14425
758490 ZDOT = 4396
971188
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 12042
05023613
00016717 00000-0 10270-3 0 9152
2 25544 51
6385 39
7417 0020411 29
0259 331
2026 15
59062603 38191
Satellite: ISS
Catalog Number: 25544
Epoch time: 12042
05023613 = yrday
fracday
Element set: 915
Inclination: 51
6385 deg
RA of node: 39
7417 deg
Eccentricity:
0020411
Arg of perigee: 29
0259 deg
Mean anomaly: 331
2026 deg
Mean motion: 15
59062603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 277
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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