[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 17th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 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
322/05:00:33
881 -0
2 9
8 9
8
N/A 9
7 -0
8 219
2
000/00:03:07
762 -1
5 0
1 203
0
Coasting Arc #1 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2011/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2116613
67 A = 6761164
32 meter
Y = 3993329
93 meter E =
0031934
Z = -5052406
34 I = 51
90792
XDOT = -5251
866593 Wp = 74
08975
YDOT = 5222
587740 meter/sec RA = 123
27246 deg
ZDOT = 1946
367701 TA = 214
64670
MA = 214
85515
Ha = 219
348 n
mi
Hp = 197
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6944270
56 X = 2096346
22
Y = 13101476
14 feet Y = 4016886
19 meter
Z = -16576136
28 Z = -5042172
65
XDOT = -17230
533443 XDOT = -5319
331519
YDOT = 17134
474214 feet/sec YDOT = 5163
480812 meter/sec
ZDOT = 6385
720805 ZDOT = 1920
690173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14679553
14 X = -4474327
80
Y = -2399556
35 feet Y = -731384
77 meter
Z = -16534591
42 Z = -5039743
46
XDOT = -3234
960544 XDOT = -986
015974
YDOT = -23063
539804 feet/sec YDOT = -7029
766932 meter/sec
ZDOT = 6280
602599 ZDOT = 1914
327672
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
51274148
00016717 00000-0 10270-3 0 9003
2 25544 51
6365 124
1685 0021724 56
2169 304
1052 15
60123650 24381
Satellite: ISS
Catalog Number: 25544
Epoch time: 11318
51274148 = yrday
fracday
Element set: 900
Inclination: 51
6365 deg
RA of node: 124
1685 deg
Eccentricity:
0021724
Arg of perigee: 56
2169 deg
Mean anomaly: 304
1052 deg
Mean motion: 15
60123650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 278
Coasting Arc #2 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2011/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 901208
90 A = 6768692
72 meter
Y = -6135673
33 meter E =
0032981
Z = 2696612
57 I = 51
94922
XDOT = 5440
469954 Wp = 75
70209
YDOT = -1515
703894 meter/sec RA = 118
25401 deg
ZDOT = -5205
954898 TA = 73
87425
MA = 73
51143
Ha = 219
258 n
mi
Hp = 197
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2956722
11 X = 956652
41
Y = -20130161
84 feet Y = -6125285
61 meter
Z = 8847154
11 Z = 2701125
03
XDOT = 17849
310872 XDOT = 5482
304404
YDOT = -4972
781806 feet/sec YDOT = -1454
631022 meter/sec
ZDOT = -17079
904520 ZDOT = -5179
423233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14438190
20 X = 4400760
37
Y = 14323811
72 feet Y = 4365897
81 meter
Z = 8865936
99 Z = 2702337
60
XDOT = -5655
493378 XDOT = -1723
794382
YDOT = 16328
973496 feet/sec YDOT = 4977
071121 meter/sec
ZDOT = -16971
499553 ZDOT = -5172
913064
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 11319
53759686
00016717 00000-0 10270-3 0 9012
2 25544 51
6362 119
0114 0021628 59
6633 300
6659 15
60177152 24542
Satellite: ISS
Catalog Number: 25544
Epoch time: 11319
53759686 = yrday
fracday
Element set: 901
Inclination: 51
6362 deg
RA of node: 119
0114 deg
Eccentricity:
0021628
Arg of perigee: 59
6633 deg
Mean anomaly: 300
6659 deg
Mean motion: 15
60177152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 308
Coasting Arc #3 (Orbit 2469)
---------------------------------------
Vector Time (GMT): 2011/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3257209
81 A = 6771329
21 meter
Y = 5855346
72 meter E =
0035049
Z = 867479
77 I = 51
97325
XDOT = -3787
947817 Wp = 60
11388
YDOT = -3016
165850 meter/sec RA = 113
27520 deg
ZDOT = 5973
504585 TA = 309
26701
MA = 309
57744
Ha = 219
239 n
mi
Hp = 197
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10686383
88 X = -3326657
47
Y = 19210455
13 feet Y = 5818534
27 meter
Z = 2846062
25 Z = 851487
66
XDOT = -12427
650317 XDOT = -3782
957410
YDOT = -9895
557251 feet/sec YDOT = -3058
497368 meter/sec
ZDOT = 19598
112155 ZDOT = 5955
114542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9396554
85 X = -2864069
92
Y = -19882517
24 feet Y = -6060191
26 meter
Z = 2780417
63 Z = 847471
29
XDOT = 13897
002946 XDOT = 4235
806498
YDOT = -3761
455778 feet/sec YDOT = -1146
491721 meter/sec
ZDOT = 19523
207971 ZDOT = 5950
673790
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 11320
56241887
00016717 00000-0 10270-3 0 9027
2 25544 51
6375 113
8557 0021702 63
7844 296
5540 15
60240461 24706
Satellite: ISS
Catalog Number: 25544
Epoch time: 11320
56241887 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 113
8557 deg
Eccentricity:
0021702
Arg of perigee: 63
7844 deg
Mean anomaly: 296
5540 deg
Mean motion: 15
60240461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2470
Checksum: 297
Coasting Arc #4 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2011/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4415026
13 A = 6764360
18 meter
Y = -3090455
09 meter E =
0029154
Z = -4119186
84 I = 51
96193
XDOT = 1004
928525 Wp = 68
10820
YDOT = 6543
565405 meter/sec RA = 108
28259 deg
ZDOT = -3843
444223 TA = 162
33868
MA = 162
23711
Ha = 219
212 n
mi
Hp = 197
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14484993
86 X = 4469266
51
Y = -10139288
35 feet Y = -3040780
17 meter
Z = -13514392
52 Z = -4097606
79
XDOT = 3297
009596 XDOT = 950
353311
YDOT = 21468
390436 feet/sec YDOT = 6554
498095 meter/sec
ZDOT = -12609
725141 ZDOT = -3838
694615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 77049
13 X = 23484
57
Y = 17748048
63 feet Y = 5409605
22 meter
Z = -13426088
54 Z = -4092271
79
XDOT = -18293
048934 XDOT = -5575
721315
YDOT = -9417
319686 feet/sec YDOT = -2870
399040 meter/sec
ZDOT = -12590
729507 ZDOT = -3837
654354
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 11321
52315760
00016717 00000-0 10270-3 0 9037
2 25544 51
6380 109
0215 0021783 66
9918 293
3532 15
60290038 24853
Satellite: ISS
Catalog Number: 25544
Epoch time: 11321
52315760 = yrday
fracday
Element set: 903
Inclination: 51
6380 deg
RA of node: 109
0215 deg
Eccentricity:
0021783
Arg of perigee: 66
9918 deg
Mean anomaly: 293
3532 deg
Mean motion: 15
60290038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 294
Coasting Arc #5 (Orbit 2495)
---------------------------------------
Vector Time (GMT): 2011/322/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4281406
44 A = 6764975
48 meter
Y = -93813
16 meter E =
0028142
Z = -5261357
93 I = 51
95563
XDOT = -1123
766975 Wp = 73
42889
YDOT = 7499
190110 meter/sec RA = 104
71325 deg
ZDOT = -1044
988548 TA = 186
57003
MA = 186
60701
Ha = 219
165 n
mi
Hp = 203
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14046609
05 X = 4307696
22
Y = -307785
96 feet Y = -45788
76 meter
Z = -17261673
01 Z = -5240494
82
XDOT = -3686
899525 XDOT = -1202
464470
YDOT = 24603
642094 feet/sec YDOT = 7486
183454 meter/sec
ZDOT = -3428
440118 ZDOT = -1050
638889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9632707
96 X = -2936049
39
Y = -10370485
02 feet Y = -3160923
83 meter
Z = -17176474
93 Z = -5235389
56
XDOT = 20067
211505 XDOT = 6116
486067
YDOT = -12904
734939 feet/sec YDOT = -3933
363209 meter/sec
ZDOT = -3451
974194 ZDOT = -1052
161734
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 11322
22768563
00016717 00000-0 10270-3 0 9049
2 25544 51
6405 105
4791 0014134 64
6929 295
5688 15
58521347 24964
Satellite: ISS
Catalog Number: 25544
Epoch time: 11322
22768563 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 105
4791 deg
Eccentricity:
0014134
Arg of perigee: 64
6929 deg
Mean anomaly: 295
5688 deg
Mean motion: 15
58521347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2496
Checksum: 327
Coasting Arc #6 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2011/323/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3258220
33 A = 6766431
72 meter
Y = -3408911
62 meter E =
0021169
Z = 4839610
21 I = 51
96786
XDOT = 3112
702711 Wp = 65
11128
YDOT = -6563
551886 meter/sec RA = 99
68955 deg
ZDOT = -2510
375564 TA = 49
47974
MA = 49
29553
Ha = 219
145 n
mi
Hp = 202
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10689699
24 X = -3243369
25
Y = -11184093
23 feet Y = -3445264
01 meter
Z = 15877986
25 Z = 4823817
67
XDOT = 10212
279234 XDOT = 3198
061386
YDOT = -21533
962879 feet/sec YDOT = -6528
266462 meter/sec
ZDOT = -8236
140303 ZDOT = -2495
046565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -925168
56 X = -281991
38
Y = 15509181
28 feet Y = 4727198
45 meter
Z = 15813709
80 Z = 4820018
75
XDOT = -21663
575040 XDOT = -6603
057672
YDOT = 7099
240552 feet/sec YDOT = 2163
848520 meter/sec
ZDOT = -8173
131820 ZDOT = -2491
170579
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 11323
25361139
00016717 00000-0 10270-3 0 9052
2 25544 51
6403 100
3300 0014061 67
7137 292
5508 15
58595645 25125
Satellite: ISS
Catalog Number: 25544
Epoch time: 11323
25361139 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 100
3300 deg
Eccentricity:
0014061
Arg of perigee: 67
7137 deg
Mean anomaly: 292
5508 deg
Mean motion: 15
58595645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 281
Coasting Arc #7 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2011/324/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1682658
75 A = 6773120
50 meter
Y = 5950202
82 meter E =
0018767
Z = -2768715
41 I = 51
99428
XDOT = -4352
721179 Wp = 67
84426
YDOT = 3621
534050 meter/sec RA = 94
69062 deg
ZDOT = 5172
447559 TA = 260
91483
MA = 261
12723
Ha = 219
094 n
mi
Hp = 202
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5520533
94 X = 1629447
46
Y = 19521662
79 feet Y = 5968721
81 meter
Z = -9083711
96 Z = -2760670
21
XDOT = -14280
581295 XDOT = -4418
021566
YDOT = 11881
673391 feet/sec YDOT = 3572
494163 meter/sec
ZDOT = 16969
972305 ZDOT = 5151
143094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10289032
80 X = 3136097
20
Y = -17501323
13 feet Y = -5334403
29 meter
Z = -9051239
06 Z = -2758817
67
XDOT = 17247
867534 XDOT = 5257
150024
YDOT = 1467
941463 feet/sec YDOT = 447
428558 meter/sec
ZDOT = 16882
739349 ZDOT = 5145
858954
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 11324
21538970
00016717 00000-0 10270-3 0 9069
2 25544 51
6402 95
5028 0014069 70
9980 289
2698 15
58596382 25274
Satellite: ISS
Catalog Number: 25544
Epoch time: 11324
21538970 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 95
5028 deg
Eccentricity:
0014069
Arg of perigee: 70
9980 deg
Mean anomaly: 289
2698 deg
Mean motion: 15
58596382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2527
Checksum: 337
Coasting Arc #8 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2011/325/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 256282
25 A = 6776278
46 meter
Y = -6758993
87 meter E =
0021772
Z = -370278
75 I = 52
00628
XDOT = 4714
601306 Wp = 102
82252
YDOT = 492
714511 meter/sec RA = 89
72069 deg
ZDOT = -6032
632371 TA = 81
15477
MA = 80
90831
Ha = 219
068 n
mi
Hp = 202
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 840821
04 X = 333642
39
Y = -22175176
75 feet Y = -6755695
42 meter
Z = -1214825
31 Z = -368845
79
XDOT = 15467
852054 XDOT = 4738
047266
YDOT = 1616
517424 feet/sec YDOT = 545
567161 meter/sec
ZDOT = -19792
100956 ZDOT = -6009
671453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16386236
79 X = -4994524
97
Y = 14965024
14 feet Y = 4561339
36 meter
Z = -1208528
36 Z = -368359
44
XDOT = -8701
946199 XDOT = -2652
353202
YDOT = -11038
746264 feet/sec YDOT = -3364
609861 meter/sec
ZDOT = -19698
366297 ZDOT = -6004
062047
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 11325
24125528
00016717 00000-0 10270-3 0 9075
2 25544 51
6402 90
3531 0014012 75
4043 284
8665 15
58607392 25431
Satellite: ISS
Catalog Number: 25544
Epoch time: 11325
24125528 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 90
3531 deg
Eccentricity:
0014012
Arg of perigee: 75
4043 deg
Mean anomaly: 284
8665 deg
Mean motion: 15
58607392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 290
Coasting Arc #9 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2011/326/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2092154
99 A = 6771499
06 meter
Y = 5508005
94 meter E =
0026634
Z = 3310953
93 I = 51
98940
XDOT = -4125
172349 Wp = 82
54884
YDOT = -4431
557934 meter/sec RA = 84
74548 deg
ZDOT = 4736
529357 TA = 315
89689
MA = 316
10899
Ha = 219
047 n
mi
Hp = 202
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6864025
56 X = -2169675
49
Y = 18070885
62 feet Y = 5484176
68 meter
Z = 10862709
76 Z = 3300601
80
XDOT = -13534
030018 XDOT = -4098
320926
YDOT = -14539
232067 feet/sec YDOT = -4477
538081 meter/sec
ZDOT = 15539
794479 ZDOT = 4716
553965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17597666
45 X = 5363768
73
Y = -8057213
24 feet Y = -2455838
60 meter
Z = 10820058
58 Z = 3297953
85
XDOT = -1029
729827 XDOT = -313
861651
YDOT = 18638
682716 feet/sec YDOT = 5681
070492 meter/sec
ZDOT = 15458
519688 ZDOT = 4711
756801
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 11326
26708762
00016717 00000-0 10270-3 0 9086
2 25544 51
6398 85
2030 0014094 77
7418 282
5315 15
58676015 25595
Satellite: ISS
Catalog Number: 25544
Epoch time: 11326
26708762 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 85
2030 deg
Eccentricity:
0014094
Arg of perigee: 77
7418 deg
Mean anomaly: 282
5315 deg
Mean motion: 15
58676015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 325
Coasting Arc #10 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2011/327/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3610576
92 A = 6764880
68 meter
Y = -2581885
17 meter E =
0027404
Z = -5129449
18 I = 51
96360
XDOT = 2608
695828 Wp = 79
17271
YDOT = 6996
222299 meter/sec RA = 79
73699 deg
ZDOT = -1687
902688 TA = 174
58507
MA = 174
55538
Ha = 218
850 n
mi
Hp = 202
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11845724
79 X = 3664098
28
Y = -8470751
87 feet Y = -2541210
01 meter
Z = -16828901
50 Z = -5111778
66
XDOT = 8558
713345 XDOT = 2538
468530
YDOT = 22953
485233 feet/sec YDOT = 7025
001746 meter/sec
ZDOT = -5537
738479 ZDOT = -1675
399611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14500086
50 X = -4419626
36
Y = -2062073
75 feet Y = -628520
08 meter
Z = -16756554
01 Z = -5107397
66
XDOT = 9391
124299 XDOT = 2862
414686
YDOT = -21517
655939 feet/sec YDOT = -6558
581530 meter/sec
ZDOT = -5487
170060 ZDOT = -1672
489434
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 11327
22877526
00016717 00000-0 10270-3 0 9099
2 25544 51
6394 80
3745 0013966 81
1342 279
1393 15
58746101 25741
Satellite: ISS
Catalog Number: 25544
Epoch time: 11327
22877526 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 80
3745 deg
Eccentricity:
0013966
Arg of perigee: 81
1342 deg
Mean anomaly: 279
1393 deg
Mean motion: 15
58746101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 324
Coasting Arc #11 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2011/328/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4376310
50 A = 6765043
05 meter
Y = -1091472
07 meter E =
0019249
Z = 5027377
10 I = 51
95910
XDOT = -428
077483 Wp = 76
15388
YDOT = -7418
725101 meter/sec RA = 74
71058 deg
ZDOT = -1972
499759 TA = 32
91728
MA = 32
79756
Ha = 218
890 n
mi
Hp = 202
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14357974
07 X = -4388202
86
Y = -3580945
10 feet Y = -1140477
52 meter
Z = 16494019
37 Z = 5006087
50
XDOT = -1404
453683 XDOT = -335
505733
YDOT = -24339
649281 feet/sec YDOT = -7422
994383 meter/sec
ZDOT = -6471
455902 ZDOT = -1974
355097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8251635
50 X = 2515098
50
Y = 12399322
62 feet Y = 3779313
53 meter
Z = 16407150
04 Z = 5000899
33
XDOT = -14516
065317 XDOT = -4424
496709
YDOT = 18279
917019 feet/sec YDOT = 5571
718707 meter/sec
ZDOT = -6478
490786 ZDOT = -1974
643991
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 11328
25454520
00016717 00000-0 10270-3 0 9100
2 25544 51
6401 75
2248 0013912 84
7667 275
5075 15
58807652 25905
Satellite: ISS
Catalog Number: 25544
Epoch time: 11328
25454520 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 75
2248 deg
Eccentricity:
0013912
Arg of perigee: 84
7667 deg
Mean anomaly: 275
5075 deg
Mean motion: 15
58807652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 309
Coasting Arc #12 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2011/329/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4198293
57 A = 6771579
33 meter
Y = 4307218
28 meter E =
0018352
Z = -3124386
41 I = 51
97141
XDOT = -2042
899948 Wp = 84
71131
YDOT = 5527
689324 meter/sec RA = 69
70359 deg
ZDOT = 4901
593880 TA = 239
47118
MA = 239
65245
Ha = 218
733 n
mi
Hp = 202
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13773929
04 X = 4164995
39
Y = 14131293
58 feet Y = 4353980
31 meter
Z = -10250611
57 Z = -3104071
12
XDOT = -6702
427652 XDOT = -2128
371380
YDOT = 18135
463663 feet/sec YDOT = 5504
365977 meter/sec
ZDOT = 16081
344752 ZDOT = 4891
462205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1011803
95 X = -308397
84
Y = -19750402
81 feet Y = -6019922
78 meter
Z = -10167962
37 Z = -3099194
93
XDOT = 15663
898438 XDOT = 4774
356244
YDOT = -9015
181772 feet/sec YDOT = -2747
827404 meter/sec
ZDOT = 16039
545725 ZDOT = 4888
853537
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 11329
21617667
00016717 00000-0 10270-3 0 9111
2 25544 51
6393 70
3962 0013928 88
1854 272
0897 15
58836753 26052
Satellite: ISS
Catalog Number: 25544
Epoch time: 11329
21617667 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 70
3962 deg
Eccentricity:
0013928
Arg of perigee: 88
1854 deg
Mean anomaly: 272
0897 deg
Mean motion: 15
58836753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 337
Coasting Arc #13 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2011/330/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2874477
76 A = 6775549
36 meter
Y = -6128989
90 meter E =
0024226
Z = -21801
72 I = 51
97386
XDOT = 4282
463552 Wp = 111
31885
YDOT = -2006
101565 meter/sec RA = 64
72926 deg
ZDOT = -6047
195171 TA = 68
91540
MA = 68
65654
Ha = 218
658 n
mi
Hp = 202
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9430701
31 X = -2805622
63
Y = -20108234
58 feet Y = -6160749
08 meter
Z = -71527
96 Z = -35599
60
XDOT = 14050
077269 XDOT = 4333
954514
YDOT = -6581
698047 feet/sec YDOT = -1957
923832 meter/sec
ZDOT = -19839
879169 ZDOT = -6026
265803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5880012
05 X = -1792227
67
Y = 21417132
54 feet Y = 6527942
00 meter
Z = -127411
27 Z = -38834
96
XDOT = -13489
840832 XDOT = -4111
703486
YDOT = -3762
127657 feet/sec YDOT = -1146
696510 meter/sec
ZDOT = -19754
234866 ZDOT = -6021
090787
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 11330
24188562
00016717 00000-0 10270-3 0 9124
2 25544 51
6395 65
2462 0013979 91
6322 268
6434 15
58881069 26213
Satellite: ISS
Catalog Number: 25544
Epoch time: 11330
24188562 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 65
2462 deg
Eccentricity:
0013979
Arg of perigee: 91
6322 deg
Mean anomaly: 268
6434 deg
Mean motion: 15
58881069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2621
Checksum: 321
Coasting Arc #14 (Orbit 2636)
---------------------------------------
Vector Time (GMT): 2011/331/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 681492
21 A = 6771272
88 meter
Y = 5973546
92 meter E =
0026769
Z = 3091883
46 I = 51
94539
XDOT = -5580
882111 Wp = 90
05499
YDOT = -1927
810661 meter/sec RA = 59
75236 deg
ZDOT = 4918
065237 TA = 305
45133
MA = 305
70092
Ha = 218
515 n
mi
Hp = 202
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2235866
82 X = 599624
22
Y = 19598251
05 feet Y = 5980709
67 meter
Z = 10143974
60 Z = 3094996
02
XDOT = -18309
980679 XDOT = -5582
801452
YDOT = -6324
838125 feet/sec YDOT = -1990
230814 meter/sec
ZDOT = 16135
384635 ZDOT = 4890
948171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10786032
27 X = 3287582
64
Y = -16507681
62 feet Y = -5031541
36 meter
Z = 10156215
87 Z = 3095614
60
XDOT = 8979
596913 XDOT = 2736
981139
YDOT = 15800
082310 feet/sec YDOT = 4815
865088 meter/sec
ZDOT = 16024
767143 ZDOT = 4884
349025
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 11331
26756186
00016717 00000-0 10270-3 0 9131
2 25544 51
6386 60
0952 0013863 95
6508 264
6228 15
58946717 26378
Satellite: ISS
Catalog Number: 25544
Epoch time: 11331
26756186 = yrday
fracday
Element set: 913
Inclination: 51
6386 deg
RA of node: 60
0952 deg
Eccentricity:
0013863
Arg of perigee: 95
6508 deg
Mean anomaly: 264
6228 deg
Mean motion: 15
58946717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2637
Checksum: 333
Coasting Arc #15 (Orbit 2651)
---------------------------------------
Vector Time (GMT): 2011/332/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2019478
55 A = 6764442
98 meter
Y = -4027264
29 meter E =
0026645
Z = -5069056
84 I = 51
90560
XDOT = 5406
899386 Wp = 87
63147
YDOT = 5081
061569 meter/sec RA = 54
74077 deg
ZDOT = -1890
212598 TA = 164
12874
MA = 164
04508
Ha = 218
537 n
mi
Hp = 202
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6625585
78 X = 2088986
79
Y = -13212809
34 feet Y = -4004292
05 meter
Z = -16630763
90 Z = -5059077
76
XDOT = 17739
171214 XDOT = 5358
862444
YDOT = 16670
149505 feet/sec YDOT = 5141
256447 meter/sec
ZDOT = -6201
484903 ZDOT = -1864
061899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13490196
36 X = -4111811
85
Y = 6152748
96 feet Y = 1875357
88 meter
Z = -16589674
74 Z = -5056532
86
XDOT = -3083
548182 XDOT = -939
865486
YDOT = -23128
602895 feet/sec YDOT = -7049
598162 meter/sec
ZDOT = -6095
064747 ZDOT = -1857
775735
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 11332
22910674
00016717 00000-0 10270-3 0 9143
2 25544 51
6376 55
2657 0014061 98
9420 261
3327 15
58970181 26528
Satellite: ISS
Catalog Number: 25544
Epoch time: 11332
22910674 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 55
2657 deg
Eccentricity:
0014061
Arg of perigee: 98
9420 deg
Mean anomaly: 261
3327 deg
Mean motion: 15
58970181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2652
Checksum: 305
Coasting Arc #16 (Orbit 2667)
---------------------------------------
Vector Time (GMT): 2011/333/05:02:07
762
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4362586
89 A = 6764340
29 meter
Y = 990227
76 meter E =
0018279
Z = 5058165
75 I = 51
88718
XDOT = -3629
708171 Wp = 89
33687
YDOT = -6522
465360 meter/sec RA = 49
70721 deg
ZDOT = -1847
737059 TA = 18
47846
MA = 18
41216
Ha = 218
601 n
mi
Hp = 201
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14312949
11 X = -4397907
26
Y = 3248778
73 feet Y = 941244
69 meter
Z = 16595032
00 Z = 5036886
57
XDOT = -11908
491374 XDOT = -3547
526916
YDOT = -21399
164568 feet/sec YDOT = -6562
595315 meter/sec
ZDOT = -6062
129458 ZDOT = -1865
171179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13410703
02 X = 4087582
28
Y = 6200681
78 feet Y = 1889967
81 meter
Z = 16508020
86 Z = 5031644
76
XDOT = -3165
215334 XDOT = -964
757634
YDOT = 23225
152298 feet/sec YDOT = 7079
026421 meter/sec
ZDOT = -6132
822868 ZDOT = -1869
284410
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 11333
25472321
00016717 00000-0 10270-3 0 9150
2 25544 51
6377 50
1145 0014012 102
6809 257
5914 15
59002214 26685
Satellite: ISS
Catalog Number: 25544
Epoch time: 11333
25472321 = yrday
fracday
Element set: 915
Inclination: 51
6377 deg
RA of node: 50
1145 deg
Eccentricity:
0014012
Arg of perigee: 102
6809 deg
Mean anomaly: 257
5914 deg
Mean motion: 15
59002214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2668
Checksum: 279
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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