[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 3rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19913 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 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
There are no maneuvers
Coasting Arc #1 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2011/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2728998
77 A = 6762809
35 meter
Y = -3507848
07 meter E =
0025389
Z = 5098107
70 I = 51
53915
XDOT = 6889
193512 Wp = 13
70318
YDOT = 2977
898715 meter/sec RA = 193
54799 deg
ZDOT = -1612
919102 TA = 92
00689
MA = 91
71611
Ha = 219
217 n
mi
Hp = 201
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8953408
04 X = 2743255
42
Y = -11508687
89 feet Y = -3477251
13 meter
Z = 16726075
14 Z = 5111399
89
XDOT = 22602
340918 XDOT = 6863
217395
YDOT = 9770
008907 feet/sec YDOT = 3054
792691 meter/sec
ZDOT = -5291
729337 ZDOT = -1579
514050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 274088
13 X = 83542
06
Y = 14516106
54 feet Y = 4424509
27 meter
Z = 16780421
00 Z = 5114672
32
XDOT = -22719
710692 XDOT = -6924
967819
YDOT = 6486
580522 feet/sec YDOT = 1977
109743 meter/sec
ZDOT = -5155
684449 ZDOT = -1571
452620
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 11304
54541648
00016717 00000-0 10270-3 0 9003
2 25544 51
6412 194
3910 0021967 4
9357 355
2011 15
59424006 22200
Satellite: ISS
Catalog Number: 25544
Epoch time: 11304
54541648 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 194
3910 deg
Eccentricity:
0021967
Arg of perigee: 4
9357 deg
Mean anomaly: 355
2011 deg
Mean motion: 15
59424006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 277
Coasting Arc #2 (Orbit 2234)
---------------------------------------
Vector Time (GMT): 2011/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5701023
96 A = 6769481
18 meter
Y = 1715413
06 meter E =
0023680
Z = -3203549
95 I = 51
59161
XDOT = -4019
871836 Wp = 19
68467
YDOT = -4451
107865 meter/sec RA = 188
50671 deg
ZDOT = 4802
421855 TA = 303
10765
MA = 303
33473
Ha = 219
313 n
mi
Hp = 201
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18704146
86 X = -5704219
93
Y = 5627995
61 feet Y = 1651642
87 meter
Z = -10510334
49 Z = -3231253
52
XDOT = -13188
555893 XDOT = -3993
129405
YDOT = -14603
372262 feet/sec YDOT = -4495
911043 meter/sec
ZDOT = 15755
977214 ZDOT = 4782
958074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10765312
02 X = 3281267
10
Y = -16224635
43 feet Y = -4945268
88 meter
Z = -10623362
82 Z = -3238000
99
XDOT = 18361
728065 XDOT = 5596
654714
YDOT = 1986
904496 feet/sec YDOT = 605
608490 meter/sec
ZDOT = 15676
820333 ZDOT = 4778
294837
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 11305
50668380
00016717 00000-0 10270-3 0 9014
2 25544 51
6415 189
5607 0021968 8
4831 351
6692 15
59426058 22359
Satellite: ISS
Catalog Number: 25544
Epoch time: 11305
50668380 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 189
5607 deg
Eccentricity:
0021968
Arg of perigee: 8
4831 deg
Mean anomaly: 351
6692 deg
Mean motion: 15
59426058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2235
Checksum: 317
Coasting Arc #3 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2011/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6764668
83 A = 6773904
50 meter
Y = 484891
76 meter E =
0018321
Z = -89147
74 I = 51
63656
XDOT = -408
755643 Wp = 46
33393
YDOT = 4738
152433 meter/sec RA = 183
50379 deg
ZDOT = -6006
273323 TA = 134
62656
MA = 134
47700
Ha = 219
441 n
mi
Hp = 201
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22193795
37 X = 6759176
97
Y = 1590852
24 feet Y = 560507
73 meter
Z = -292479
45 Z = -56298
06
XDOT = -1341
061822 XDOT = -432
530600
YDOT = 15545
119532 feet/sec YDOT = 4733
448484 meter/sec
ZDOT = -19705
621138 ZDOT = -6008
316871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17882380
27 X = -5450549
51
Y = 13242969
63 feet Y = 4036457
14 meter
Z = -158552
98 Z = -48326
95
XDOT = -8226
933007 XDOT = -2507
569180
YDOT = -11289
964583 feet/sec YDOT = -3441
181205 meter/sec
ZDOT = -19714
164665 ZDOT = -6008
877390
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 11306
53200546
00016717 00000-0 10270-3 0 9025
2 25544 51
6414 184
4077 0021757 12
3712 347
7973 15
59443942 22518
Satellite: ISS
Catalog Number: 25544
Epoch time: 11306
53200546 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 184
4077 deg
Eccentricity:
0021757
Arg of perigee: 12
3712 deg
Mean anomaly: 347
7973 deg
Mean motion: 15
59443942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2251
Checksum: 297
Coasting Arc #4 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2011/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5330979
19 A = 6769155
22 meter
Y = -2482632
20 meter E =
0028564
Z = 3313232
86 I = 51
65119
XDOT = 4718
373078 Wp = 41
25741
YDOT = -3848
160923 meter/sec RA = 178
50120 deg
ZDOT = 4706
431480 TA = 357
49088
MA = 357
50518
Ha = 219
636 n
mi
Hp = 200
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17490089
22 X = -5318916
92
Y = -8145118
77 feet Y = -2542178
95 meter
Z = 10870186
54 Z = 3287364
11
XDOT = 15480
226633 XDOT = 4738
190101
YDOT = -12625
199877 feet/sec YDOT = -3795
286257 meter/sec
ZDOT = 15441
048164 ZDOT = 4729
401765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18534563
03 X = 5649334
81
Y = -5567415
97 feet Y = -1696948
39 meter
Z = 10764803
24 Z = 3281112
03
XDOT = -3527
912318 XDOT = -1075
307674
YDOT = 18304
983205 feet/sec YDOT = 5579
358881 meter/sec
ZDOT = 15534
891493 ZDOT = 4735
034927
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 11307
55729605
00016717 00000-0 10270-3 0 9031
2 25544 51
6413 179
2541 0022009 16
0275 344
1572 15
59496720 22676
Satellite: ISS
Catalog Number: 25544
Epoch time: 11307
55729605 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 179
2541 deg
Eccentricity:
0022009
Arg of perigee: 16
0275 deg
Mean anomaly: 344
1572 deg
Mean motion: 15
59496720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 301
Coasting Arc #5 (Orbit 2281)
---------------------------------------
Vector Time (GMT): 2011/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2022666
91 A = 6762228
05 meter
Y = 3886814
84 meter E =
0031219
Z = -5173437
21 I = 51
65860
XDOT = -7281
110746 Wp = 42
10704
YDOT = 1931
278044 meter/sec RA = 173
46327 deg
ZDOT = -1377
929898 TA = 214
52871
MA = 214
73188
Ha = 219
506 n
mi
Hp = 200
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6636046
31 X = 2004185
34
Y = 12752017
19 feet Y = 3909330
01 meter
Z = -16973219
19 Z = -5163656
03
XDOT = -23888
158615 XDOT = -7295
471718
YDOT = 6336
214055 feet/sec YDOT = 1849
775850 meter/sec
ZDOT = -4520
767382 ZDOT = -1413
336864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13590482
88 X = -4142379
18
Y = -4826653
18 feet Y = -1471163
89 meter
Z = -16933499
84 Z = -5161330
75
XDOT = 12925
478035 XDOT = 3939
685705
YDOT = -19821
798034 feet/sec YDOT = -6041
684041 meter/sec
ZDOT = -4665
255480 ZDOT = -1421
969870
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 11308
51847700
00016717 00000-0 10270-3 0 9046
2 25544 51
6408 174
4231 0021905 19
1396 341
0578 15
59577845 22822
Satellite: ISS
Catalog Number: 25544
Epoch time: 11308
51847700 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 174
4231 deg
Eccentricity:
0021905
Arg of perigee: 19
1396 deg
Mean anomaly: 341
0578 deg
Mean motion: 15
59577845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2282
Checksum: 312
Coasting Arc #6 (Orbit 2297)
---------------------------------------
Vector Time (GMT): 2011/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2077190
50 A = 6763470
12 meter
Y = -4291657
28 meter E =
0027927
Z = 4793829
11 I = 51
69393
XDOT = 7213
559316 Wp = 32
11277
YDOT = 590
418571 meter/sec RA = 168
40868 deg
ZDOT = -2567
072860 TA = 83
25938
MA = 82
94165
Ha = 219
423 n
mi
Hp = 200
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6814929
47 X = 2101738
40
Y = -14080240
42 feet Y = -4268291
39 meter
Z = 15727785
80 Z = 4803980
06
XDOT = 23666
533190 XDOT = 7218
891555
YDOT = 1937
068804 feet/sec YDOT = 671
114715 meter/sec
ZDOT = -8422
155051 ZDOT = -2532
015979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4837609
22 X = 1474503
29
Y = 14831853
84 feet Y = 4520749
05 meter
Z = 15769379
46 Z = 4806506
86
XDOT = -17434
706898 XDOT = -5314
098662
YDOT = 14593
562072 feet/sec YDOT = 4448
117720 meter/sec
ZDOT = -8279
195243 ZDOT = -2523
498710
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 11309
54370828
00016717 00000-0 10270-3 0 9053
2 25544 51
6411 169
2693 0021850 22
6336 337
5778 15
59644998 22985
Satellite: ISS
Catalog Number: 25544
Epoch time: 11309
54370828 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 169
2693 deg
Eccentricity:
0021850
Arg of perigee: 22
6336 deg
Mean anomaly: 337
5778 deg
Mean motion: 15
59644998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2298
Checksum: 342
Coasting Arc #7 (Orbit 2312)
---------------------------------------
Vector Time (GMT): 2011/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5242547
14 A = 6770835
67 meter
Y = 3534448
28 meter E =
0027030
Z = -2394609
63 I = 51
74687
XDOT = -4521
360555 Wp = 30
71949
YDOT = -3087
023410 meter/sec RA = 163
38636 deg
ZDOT = 5391
617320 TA = 302
47114
MA = 302
73217
Ha = 219
499 n
mi
Hp = 199
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17199957
80 X = -5270047
61
Y = 11595958
92 feet Y = 3475669
03 meter
Z = -7856330
82 Z = -2420145
33
XDOT = -14833
860090 XDOT = -4512
696772
YDOT = -10128
029559 feet/sec YDOT = -3137
535358 meter/sec
ZDOT = 17689
033201 ZDOT = 5369
673346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4083621
50 X = 1244687
83
Y = -20297261
60 feet Y = -6186605
34 meter
Z = -7960650
25 Z = -2426406
20
XDOT = 16270
682859 XDOT = 4959
304136
YDOT = -3566
397914 feet/sec YDOT = -1087
038084 meter/sec
ZDOT = 17599
663491 ZDOT = 5364
377432
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 11310
50483750
00016717 00000-0 10270-3 0 9061
2 25544 51
6399 164
4378 0021835 26
0467 334
1782 15
59638602 23134
Satellite: ISS
Catalog Number: 25544
Epoch time: 11310
50483750 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 164
4378 deg
Eccentricity:
0021835
Arg of perigee: 26
0467 deg
Mean anomaly: 334
1782 deg
Mean motion: 15
59638602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2313
Checksum: 309
Coasting Arc #8 (Orbit 2328)
---------------------------------------
Vector Time (GMT): 2011/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6490185
65 A = 6772724
04 meter
Y = -1616642
52 meter E =
0020222
Z = -1125558
61 I = 51
78152
XDOT = 211
328476 Wp = 56
29456
YDOT = 4900
105294 meter/sec RA = 158
39797 deg
ZDOT = -5884
528352 TA = 135
89950
MA = 135
73806
Ha = 219
568 n
mi
Hp = 199
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21293259
99 X = 6513248
77
Y = -5303945
26 feet Y = -1543936
37 meter
Z = -3692777
58 Z = -1093972
54
XDOT = 693
334896 XDOT = 185
105404
YDOT = 16076
460939 feet/sec YDOT = 4902
321661 meter/sec
ZDOT = -19306
195380 ZDOT = -5883
565574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11140344
97 X = -3395577
15
Y = 18930478
55 feet Y = 5770009
86 meter
Z = -3563854
47 Z = -1086262
84
XDOT = -10662
366627 XDOT = -3249
889348
YDOT = -9866
921523 feet/sec YDOT = -3007
437680 meter/sec
ZDOT = -19302
494271 ZDOT = -5883
400254
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 11311
53001251
00016717 00000-0 10270-3 0 9078
2 25544 51
6392 159
2839 0021730 30
0457 330
1940 15
59678507 23296
Satellite: ISS
Catalog Number: 25544
Epoch time: 11311
53001251 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 159
2839 deg
Eccentricity:
0021730
Arg of perigee: 30
0457 deg
Mean anomaly: 330
1940 deg
Mean motion: 15
59678507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2329
Checksum: 288
Coasting Arc #9 (Orbit 2344)
---------------------------------------
Vector Time (GMT): 2011/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5265912
27 A = 6765999
43 meter
Y = -976457
31 meter E =
0027366
Z = 4104381
04 I = 51
78612
XDOT = 3979
029502 Wp = 55
05701
YDOT = -5362
715406 meter/sec RA = 153
39362 deg
ZDOT = 3826
658866 TA = 355
67371
MA = 355
69732
Ha = 219
730 n
mi
Hp = 199
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17276615
05 X = -5274540
77
Y = -3203600
10 feet Y = -1035392
12 meter
Z = 13465817
07 Z = 4078777
70
XDOT = 13054
558735 XDOT = 4020
111048
YDOT = -17594
210650 feet/sec YDOT = -5317
989667 meter/sec
ZDOT = 12554
655071 ZDOT = 3846
089371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14265056
25 X = 4347989
15
Y = -10394880
52 feet Y = -3168359
58 meter
Z = 13361412
34 Z = 4072558
48
XDOT = 3083
427368 XDOT = 939
828662
YDOT = 20482
276337 feet/sec YDOT = 6242
997827 meter/sec
ZDOT = 12634
178482 ZDOT = 3850
897601
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 11312
55515783
00016717 00000-0 10270-3 0 9082
2 25544 51
6382 154
1287 0021817 33
5743 326
6790 15
59720214 23452
Satellite: ISS
Catalog Number: 25544
Epoch time: 11312
55515783 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 154
1287 deg
Eccentricity:
0021817
Arg of perigee: 33
5743 deg
Mean anomaly: 326
6790 deg
Mean motion: 15
59720214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2345
Checksum: 308
Coasting Arc #10 (Orbit 2359)
---------------------------------------
Vector Time (GMT): 2011/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2260379
90 A = 6760958
36 meter
Y = 3532398
33 meter E =
0033075
Z = -5327552
35 I = 51
79511
XDOT = -6495
987251 Wp = 58
44753
YDOT = 4052
463228 meter/sec RA = 148
35186 deg
ZDOT = -52
541728 TA = 210
95436
MA = 211
14972
Ha = 219
573 n
mi
Hp = 199
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7415944
54 X = 2246592
88
Y = 11589233
37 feet Y = 3557598
16 meter
Z = -17478846
30 Z = -5316604
66
XDOT = -21312
294131 XDOT = -6540
564647
YDOT = 13295
483032 feet/sec YDOT = 3979
571870 meter/sec
ZDOT = -172
380996 ZDOT = -84
208357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13626001
07 X = -4153205
13
Y = -2278601
38 feet Y = -694517
70 meter
Z = -17434354
08 Z = -5313991
12
XDOT = 4419
702761 XDOT = 1347
125401
YDOT = -23702
373448 feet/sec YDOT = -7224
483427 meter/sec
ZDOT = -301
777679 ZDOT = -91
981837
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 11313
51620362
00016717 00000-0 10270-3 0 9090
2 25544 51
6368 149
2958 0021729 37
3281 322
9379 15
59782706 23600
Satellite: ISS
Catalog Number: 25544
Epoch time: 11313
51620362 = yrday
fracday
Element set: 909
Inclination: 51
6368 deg
RA of node: 149
2958 deg
Eccentricity:
0021729
Arg of perigee: 37
3281 deg
Mean anomaly: 322
9379 deg
Mean motion: 15
59782706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2360
Checksum: 324
Coasting Arc #11 (Orbit 2375)
---------------------------------------
Vector Time (GMT): 2011/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1465712
75 A = 6765447
28 meter
Y = -5144233
12 meter E =
0030708
Z = 4134597
01 I = 51
83642
XDOT = 6578
167979 Wp = 52
12740
YDOT = -1195
226831 meter/sec RA = 143
31051 deg
ZDOT = -3781
524827 TA = 76
81033
MA = 76
46791
Ha = 219
484 n
mi
Hp = 199
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4808768
86 X = 1503041
99
Y = -16877405
24 feet Y = -5127633
95 meter
Z = 13564950
81 Z = 4141808
24
XDOT = 21581
915940 XDOT = 6609
414775
YDOT = -3921
347871 feet/sec YDOT = -1121
490969 meter/sec
ZDOT = -12406
577518 ZDOT = -3749
491364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9509573
41 X = 2898517
97
Y = 14721848
57 feet Y = 4487219
44 meter
Z = 13594636
60 Z = 4143645
24
XDOT = -10336
846752 XDOT = -3150
670890
YDOT = 18126
405270 feet/sec YDOT = 5524
928326 meter/sec
ZDOT = -12275
810433 ZDOT = -3741
667020
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 11314
54129017
00016717 00000-0 10270-3 0 9107
2 25544 51
6371 144
1406 0021629 40
7173 319
5595 15
59838817 23767
Satellite: ISS
Catalog Number: 25544
Epoch time: 11314
54129017 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 144
1406 deg
Eccentricity:
0021629
Arg of perigee: 40
7173 deg
Mean anomaly: 319
5595 deg
Mean motion: 15
59838817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2376
Checksum: 308
Coasting Arc #12 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2011/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4327100
62 A = 6772128
33 meter
Y = 5064512
55 meter E =
0030875
Z = -1152167
38 I = 51
88167
XDOT = -4311
185411 Wp = 42
91658
YDOT = -2365
853870 meter/sec RA = 138
31016 deg
ZDOT = 5906
163515 TA = 304
57206
MA = 304
86300
Ha = 219
520 n
mi
Hp = 198
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14196524
34 X = -4377814
23
Y = 16615854
82 feet Y = 5015840
74 meter
Z = -3780076
71 Z = -1173311
99
XDOT = -14144
309092 XDOT = -4313
101341
YDOT = -7761
987763 feet/sec YDOT = -2414
075086 meter/sec
ZDOT = 19377
176885 ZDOT = 5885
214520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3426846
98 X = -1044502
96
Y = -21569024
48 feet Y = -6574238
66 meter
Z = -3866628
71 Z = -1178548
43
XDOT = 13591
246327 XDOT = 4142
611880
YDOT = -5551
950548 feet/sec YDOT = -1692
234527 meter/sec
ZDOT = 19291
814632 ZDOT = 5880
145100
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 11315
50228361
00016717 00000-0 10270-3 0 9117
2 25544 51
6361 139
3074 0021651 44
5886 315
7007 15
59859462 23913
Satellite: ISS
Catalog Number: 25544
Epoch time: 11315
50228361 = yrday
fracday
Element set: 911
Inclination: 51
6361 deg
RA of node: 139
3074 deg
Eccentricity:
0021651
Arg of perigee: 44
5886 deg
Mean anomaly: 315
7007 deg
Mean motion: 15
59859462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 304
Coasting Arc #13 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2011/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5532119
13 A = 6770012
07 meter
Y = -3067886
34 meter E =
0022983
Z = -2447247
90 I = 51
89723
XDOT = 653
813507 Wp = 62
45677
YDOT = 5431
818093 meter/sec RA = 133
32885 deg
ZDOT = -5359
537957 TA = 144
83442
MA = 144
68252
Ha = 219
559 n
mi
Hp = 198
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18149997
15 X = 5577902
24
Y = -10065243
90 feet Y = -3005766
69 meter
Z = -8029028
55 Z = -2420261
19
XDOT = 2145
057439 XDOT = 619
061511
YDOT = 17820
925501 feet/sec YDOT = 5438
935385 meter/sec
ZDOT = -17583
785947 ZDOT = -5356
445811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3816400
83 X = -1163238
97
Y = 20443231
60 feet Y = 6231096
99 meter
Z = -7918724
47 Z = -2413627
22
XDOT = -13687
853255 XDOT = -4172
057672
YDOT = -9325
353335 feet/sec YDOT = -2842
367696 meter/sec
ZDOT = -17571
462203 ZDOT = -5355
781680
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 11316
52731311
00016717 00000-0 10270-3 0 9125
2 25544 51
6362 134
1519 0021810 48
3471 311
9548 15
59934281 24079
Satellite: ISS
Catalog Number: 25544
Epoch time: 11316
52731311 = yrday
fracday
Element set: 912
Inclination: 51
6362 deg
RA of node: 134
1519 deg
Eccentricity:
0021810
Arg of perigee: 48
3471 deg
Mean anomaly: 311
9548 deg
Mean motion: 15
59934281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 288
Coasting Arc #14 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2011/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4657561
39 A = 6762373
48 meter
Y = -269095
79 meter E =
0025041
Z = 4871927
98 I = 51
89151
XDOT = 2901
459141 Wp = 67
21819
YDOT = -6711
773968 meter/sec RA = 128
31452 deg
ZDOT = 2402
799673 TA = 359
40485
MA = 359
40783
Ha = 219
689 n
mi
Hp = 198
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15280713
24 X = -4677873
56
Y = -882860
20 feet Y = -321293
36 meter
Z = 15984015
67 Z = 4849251
74
XDOT = 9519
222904 XDOT = 2964
623283
YDOT = -22020
255800 feet/sec YDOT = -6678
975045 meter/sec
ZDOT = 7883
201028 ZDOT = 2417
048272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10269961
14 X = 3130284
16
Y = -11478558
87 feet Y = -3498664
74 meter
Z = 15891475
09 Z = 4843721
61
XDOT = 10486
331718 XDOT = 3196
233908
YDOT = 20378
394465 feet/sec YDOT = 6211
334633 meter/sec
ZDOT = 7941
734885 ZDOT = 2420
640793
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 11317
55231344
00016717 00000-0 10270-3 0 9131
2 25544 51
6359 128
9959 0021677 52
1572 308
1541 15
59947866 24232
Satellite: ISS
Catalog Number: 25544
Epoch time: 11317
55231344 = yrday
fracday
Element set: 913
Inclination: 51
6359 deg
RA of node: 128
9959 deg
Eccentricity:
0021677
Arg of perigee: 52
1572 deg
Mean anomaly: 308
1541 deg
Mean motion: 15
59947866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 327
Coasting Arc #15 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2011/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 855750
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2332810
15 A = 6761214
04 meter
Y = 3772037
79 meter E =
0032556
Z = -5127921
99 I = 51
90699
XDOT = -5133
335971 Wp = 73
81001
YDOT = 5428
764721 meter/sec RA = 123
27185 deg
ZDOT = 1675
689279 TA = 212
23516
MA = 212
43456
Ha = 219
539 n
mi
Hp = 198
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7653576
60 X = 2315368
01
Y = 12375452
07 feet Y = 3798027
50 meter
Z = -16823891
04 Z = -5116631
15
XDOT = -16841
653449 XDOT = -5201
800291
YDOT = 17810
907878 feet/sec YDOT = 5370
977704 meter/sec
ZDOT = 5497
668238 ZDOT = 1650
585167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14537142
67 X = -4430921
09
Y = -1393538
88 feet Y = -424750
65 meter
Z = -16778018
09 Z = -5113939
91
XDOT = -3938
122003 XDOT = -1200
339586
YDOT = -23173
601661 feet/sec YDOT = -7063
313786 meter/sec
ZDOT = 5394
878893 ZDOT = 1644
359086
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 11318
51322321
00016717 00000-0 10270-3 0 9145
2 25544 51
6367 124
1628 0021710 56
1280 304
1937 15
59997695 24386
Satellite: ISS
Catalog Number: 25544
Epoch time: 11318
51322321 = yrday
fracday
Element set: 914
Inclination: 51
6367 deg
RA of node: 124
1628 deg
Eccentricity:
0021710
Arg of perigee: 56
1280 deg
Mean anomaly: 304
1937 deg
Mean motion: 15
59997695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 305
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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