[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 4th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 32291 73 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
343/19:50:37
609 3
0 3
9 3
9
N/A 1
2 -0
3 223
2
000/00:01:15
217 2
3 -0
0 200
9
Coasting Arc #1 (Orbit 2718)
---------------------------------------
Vector Time (GMT): 2011/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3375350
53 A = 6772921
20 meter
Y = -5046749
91 meter E =
0032945
Z = -3007507
69 I = 51
84097
XDOT = 5753
123331 Wp = 117
47243
YDOT = -908
839032 meter/sec RA = 33
31815 deg
ZDOT = -4988
226204 TA = 96
89623
MA = 96
52133
Ha = 224
474 n
mi
Hp = 197
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11073984
69 X = -3304055
92
Y = -16557578
43 feet Y = -5084096
40 meter
Z = -9867151
21 Z = -3023732
23
XDOT = 18875
076546 XDOT = 5787
090562
YDOT = -2981
755354 feet/sec YDOT = -844
313964 meter/sec
ZDOT = -16365
571535 ZDOT = -4960
194943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19310937
86 X = 5885973
86
Y = -4750808
98 feet Y = -1448046
58 meter
Z = -9933010
94 Z = -3027581
74
XDOT = -3970
442448 XDOT = -1210
190858
YDOT = 17453
515919 feet/sec YDOT = 5319
831652 meter/sec
ZDOT = -16250
983416 ZDOT = -4953
299745
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 11336
52601672
00016717 00000-0 10270-3 0 9000
2 25544 51
6414 33
7296 0028483 119
3435 241
0570 15
58435255 27195
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
52601672 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 33
7296 deg
Eccentricity:
0028483
Arg of perigee: 119
3435 deg
Mean anomaly: 241
0570 deg
Mean motion: 15
58435255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2719
Checksum: 299
Coasting Arc #2 (Orbit 2734)
---------------------------------------
Vector Time (GMT): 2011/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 403515
43 A = 6766229
88 meter
Y = 4611943
60 meter E =
0034839
Z = 4915594
66 I = 51
79358
XDOT = -7123
507767 Wp = 122
34819
YDOT = -1816
813710 meter/sec RA = 28
30736 deg
ZDOT = 2259
452904 TA = 305
53527
MA = 305
85965
Ha = 224
293 n
mi
Hp = 198
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1323869
51 X = 328034
53
Y = 15131048
56 feet Y = 4616033
74 meter
Z = 16127279
06 Z = 4917371
77
XDOT = -23371
088475 XDOT = -7113
638448
YDOT = -5960
674902 feet/sec YDOT = -1896
418044 meter/sec
ZDOT = 7412
903229 ZDOT = 2224
870564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14718277
45 X = -4486130
97
Y = -3721811
49 feet Y = -1134408
14 meter
Z = 16134150
70 Z = 4917689
13
XDOT = 12925
439199 XDOT = 3939
673868
YDOT = -19166
616319 feet/sec YDOT = -5841
984654 meter/sec
ZDOT = 7271
786154 ZDOT = 2216
440420
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 11337
55197500
00016717 00000-0 10270-3 0 9015
2 25544 51
6416 28
5822 0028375 123
0469 237
3417 15
58519567 27358
Satellite: ISS
Catalog Number: 25544
Epoch time: 11337
55197500 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 28
5822 deg
Eccentricity:
0028375
Arg of perigee: 123
0469 deg
Mean anomaly: 237
3417 deg
Mean motion: 15
58519567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2735
Checksum: 317
Coasting Arc #3 (Orbit 2749)
---------------------------------------
Vector Time (GMT): 2011/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2995945
86 A = 6765189
32 meter
Y = -3174981
40 meter E =
0041292
Z = -5203650
25 I = 51
76311
XDOT = 6441
722237 Wp = 117
34706
YDOT = 3900
905663 meter/sec RA = 23
26990 deg
ZDOT = 1318
201050 TA = 165
39339
MA = 165
27371
Ha = 224
194 n
mi
Hp = 198
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9829218
71 X = 3056505
12
Y = -10416605
64 feet Y = -3141140
08 meter
Z = -17072343
33 Z = -5188948
82
XDOT = 21134
259307 XDOT = 6391
219121
YDOT = 12798
246927 feet/sec YDOT = 3972
658522 meter/sec
ZDOT = 4324
806594 ZDOT = 1349
372741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6874096
29 X = 2095224
55
Y = 12646031
37 feet Y = 3854510
36 meter
Z = -17012019
61 Z = -5185263
58
XDOT = -17727
082214 XDOT = -5403
214659
YDOT = 15671
025736 feet/sec YDOT = 4776
528644 meter/sec
ZDOT = 4451
807127 ZDOT = 1356
910812
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 11338
51377556
00016717 00000-0 10270-3 0 9024
2 25544 51
6419 23
7547 0028299 126
2393 234
1384 15
58536712 27504
Satellite: ISS
Catalog Number: 25544
Epoch time: 11338
51377556 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 23
7547 deg
Eccentricity:
0028299
Arg of perigee: 126
2393 deg
Mean anomaly: 234
1384 deg
Mean motion: 15
58536712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2750
Checksum: 322
Coasting Arc #4 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2011/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5602843
27 A = 6770820
50 meter
Y = 1128268
92 meter E =
0038112
Z = 3585031
30 I = 51
75458
XDOT = -3857
591939 Wp = 116
83965
YDOT = -4962
898176 meter/sec RA = 18
24565 deg
ZDOT = -4447
560517 TA = 20
58178
MA = 20
42865
Ha = 224
075 n
mi
Hp = 198
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18382031
73 X = -5632459
03
Y = 3701669
67 feet Y = 1065448
71 meter
Z = 11761913
70 Z = 3557740
46
XDOT = -12656
141533 XDOT = -3780
203403
YDOT = -16282
474332 feet/sec YDOT = -5005
603203 meter/sec
ZDOT = -14591
733980 ZDOT = -4466
113214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1806465
41 X = 550610
66
Y = -18733667
80 feet Y = -5710021
95 meter
Z = 11650340
60 Z = 3551023
81
XDOT = 17861
452291 XDOT = 5444
170658
YDOT = -7438
854195 feet/sec YDOT = -2267
362759 meter/sec
ZDOT = -14667
088891 ZDOT = -4470
528694
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 11339
53965486
00016717 00000-0 10270-3 0 9033
2 25544 51
6417 18
6060 0028305 129
7723 230
5931 15
58646765 27663
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
53965486 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 18
6060 deg
Eccentricity:
0028305
Arg of perigee: 129
7723 deg
Mean anomaly: 230
5931 deg
Mean motion: 15
58646765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 330
Coasting Arc #5 (Orbit 2780)
---------------------------------------
Vector Time (GMT): 2011/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6675070
90 A = 6775902
32 meter
Y = 961252
36 meter E =
0029705
Z = -753945
46 I = 51
74315
XDOT = -40
760093 Wp = 111
93402
YDOT = 4814
908939 meter/sec RA = 13
25207 deg
ZDOT = 5955
428672 TA = 239
93190
MA = 240
22682
Ha = 223
891 n
mi
Hp = 198
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21899838
92 X = 6667488
46
Y = 3153715
10 feet Y = 1035854
75 meter
Z = -2473574
33 Z = -721535
85
XDOT = -133
727340 XDOT = -123
529134
YDOT = 15796
945338 feet/sec YDOT = 4813
989949 meter/sec
ZDOT = 19538
807980 ZDOT = 5955
029930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9025062
42 X = -2750839
03
Y = 20217173
44 feet Y = 6162194
46 meter
Z = -2341277
45 Z = -713621
37
XDOT = -13652
964812 XDOT = -4161
423675
YDOT = -3903
519154 feet/sec YDOT = -1189
792638 meter/sec
ZDOT = 19536
758480 ZDOT = 5954
803985
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 11340
50138149
00016717 00000-0 10270-3 0 9041
2 25544 51
6420 13
7793 0028332 133
1189 227
2343 15
58676844 27819
Satellite: ISS
Catalog Number: 25544
Epoch time: 11340
50138149 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 13
7793 deg
Eccentricity:
0028332
Arg of perigee: 133
1189 deg
Mean anomaly: 227
2343 deg
Mean motion: 15
58676844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2781
Checksum: 304
Coasting Arc #6 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2011/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5651719
57 A = 6773280
75 meter
Y = -2787073
45 meter E =
0033649
Z = -2464285
65 I = 51
70584
XDOT = 4111
876678 Wp = 135
37884
YDOT = -3669
544179 meter/sec RA = 8
26418 deg
ZDOT = -5347
694310 TA = 72
26965
MA = 71
90266
Ha = 223
653 n
mi
Hp = 198
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18542387
04 X = -5608162
68
Y = -9143941
77 feet Y = -2850030
70 meter
Z = -8084926
68 Z = -2491636
54
XDOT = 13490
409049 XDOT = 4178
583147
YDOT = -12039
186939 feet/sec YDOT = -3623
189223 meter/sec
ZDOT = -17544
928837 ZDOT = -5327
556800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13587180
07 X = 4141372
49
Y = -15524350
54 feet Y = -4731822
05 meter
Z = -8196395
87 Z = -2498261
46
XDOT = 7012
407580 XDOT = 2137
381831
YDOT = 15241
635248 feet/sec YDOT = 4645
650423 meter/sec
ZDOT = -17462
351472 ZDOT = -5322
524729
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 11341
52718304
00016717 00000-0 10270-3 0 9052
2 25544 51
6424 8
6289 0028354 136
8999 223
4383 15
58740847 27973
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
52718304 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 8
6289 deg
Eccentricity:
0028354
Arg of perigee: 136
8999 deg
Mean anomaly: 223
4383 deg
Mean motion: 15
58740847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2797
Checksum: 339
Coasting Arc #7 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2011/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2936942
55 A = 6766313
94 meter
Y = 3882221
54 meter E =
0035732
Z = 4689031
98 I = 51
65139
XDOT = -6923
177060 Wp = 134
82847
YDOT = 1819
634307 meter/sec RA = 3
24702 deg
ZDOT = 2792
012525 TA = 287
37339
MA = 287
76386
Ha = 223
520 n
mi
Hp = 198
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9635638
30 X = 2870533
73
Y = 12736947
30 feet Y = 3914692
44 meter
Z = 15383963
19 Z = 4703138
93
XDOT = -22713
835499 XDOT = -6956
573291
YDOT = 5969
928828 feet/sec YDOT = 1742
028078 meter/sec
ZDOT = 9160
146081 ZDOT = 2758
298347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14656748
88 X = -4467377
06
Y = 6204000
87 feet Y = 1890979
47 meter
Z = 15441235
73 Z = 4706488
65
XDOT = 124
915613 XDOT = 38
074279
YDOT = -22467
523590 feet/sec YDOT = -6848
101190 meter/sec
ZDOT = 9022
277161 ZDOT = 2749
990079
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 11342
55294495
00016717 00000-0 10270-3 0 9067
2 25544 51
6410 3
4798 0028388 140
3924 219
9312 15
58800935 28137
Satellite: ISS
Catalog Number: 25544
Epoch time: 11342
55294495 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 3
4798 deg
Eccentricity:
0028388
Arg of perigee: 140
3924 deg
Mean anomaly: 219
9312 deg
Mean motion: 15
58800935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 318
Coasting Arc #8 (Orbit 2827)
---------------------------------------
Vector Time (GMT): 2011/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 850525
28 A = 6763974
84 meter
Y = -4198958
64 meter E =
0039518
Z = -5264098
07 I = 51
61429
XDOT = 7589
553222 Wp = 128
10361
YDOT = 439
716872 meter/sec RA = 358
19790 deg
ZDOT = 856
078257 TA = 150
21673
MA = 149
99122
Ha = 223
375 n
mi
Hp = 198
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2790437
28 X = 922987
97
Y = -13776111
02 feet Y = -4189041
76 meter
Z = -17270662
95 Z = -5259790
66
XDOT = 24900
108995 XDOT = 7579
913425
YDOT = 1442
640657 feet/sec YDOT = 524
533910 meter/sec
ZDOT = 2808
655700 ZDOT = 892
925343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12782015
78 X = 3895958
41
Y = 5899858
53 feet Y = 1798276
88 meter
Z = -17252690
11 Z = -5258619
95
XDOT = -6535
616991 XDOT = -1992
056059
YDOT = 22999
194245 feet/sec YDOT = 7010
154406 meter/sec
ZDOT = 2959
119061 ZDOT = 901
939490
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 11343
51455989
00016717 00000-0 10270-3 0 9072
2 25544 51
6419 358
6514 0028212 144
1564 216
1491 15
58837209 28282
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
51455989 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 358
6514 deg
Eccentricity:
0028212
Arg of perigee: 144
1564 deg
Mean anomaly: 216
1491 deg
Mean motion: 15
58837209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2828
Checksum: 328
Coasting Arc #9 (Orbit 2832)
---------------------------------------
Vector Time (GMT): 2011/343/19:51:15
217
Vector Time (MET): N/A
Weight (LBS) : 871652
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4688195
98 A = 6771899
30 meter
Y = -3224997
09 meter E =
0029093
Z = -3707539
49 I = 51
62572
XDOT = 5523
585678 Wp = 138
09159
YDOT = 3079
976599 meter/sec RA = 356
53615 deg
ZDOT = 4303
892659 TA = 177
77527
MA = 177
76230
Ha = 223
190 n
mi
Hp = 200
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15381220
42 X = 4741920
83
Y = -10580699
11 feet Y = -3172269
96 meter
Z = -12163843
47 Z = -3684633
91
XDOT = 18122
000257 XDOT = 5467
826509
YDOT = 10104
910101 feet/sec YDOT = 3141
432422 meter/sec
ZDOT = 14120
382740 ZDOT = 4330
591440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12133195
35 X = 3698197
94
Y = -14268604
27 feet Y = -4349070
58 meter
Z = -12069992
81 Z = -3678933
81
XDOT = 19016
649976 XDOT = 5796
274913
YDOT = 4129
596043 feet/sec YDOT = 1258
700874 meter/sec
ZDOT = 14229
156418 ZDOT = 4337
046876
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 11343
83509037
00016717 00000-0 10270-3 0 9082
2 25544 51
6433 357
0418 0024945 146
5792 213
6943 15
58160131 28335
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
83509037 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 357
0418 deg
Eccentricity:
0024945
Arg of perigee: 146
5792 deg
Mean anomaly: 213
6943 deg
Mean motion: 15
58160131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2833
Checksum: 311
Coasting Arc #10 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2011/344/19:51:15
217
Vector Time (MET): N/A
Weight (LBS) : 871652
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6448869
12 A = 6777247
41 meter
Y = 1750333
89 meter E =
0037762
Z = 986947
97 I = 51
61347
XDOT = -2122
876212 Wp = 141
03540
YDOT = -4428
480957 meter/sec RA = 351
53422 deg
ZDOT = -5923
643696 TA = 28
22142
MA = 28
01730
Ha = 223
126 n
mi
Hp = 200
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21157707
10 X = -6472756
85
Y = 5742565
26 feet Y = 1678084
99 meter
Z = 3238018
27 Z = 955561
39
XDOT = -6964
816968 XDOT = -2044
422132
YDOT = -14529
136997 feet/sec YDOT = -4451
780816 meter/sec
ZDOT = -19434
526563 ZDOT = -5933
766708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18731669
93 X = -5709412
99
Y = 11426502
57 feet Y = 3482797
98 meter
Z = 3109657
25 Z = 947823
53
XDOT = -9798
161663 XDOT = -2986
479675
YDOT = -10675
024653 feet/sec YDOT = -3253
747514 meter/sec
ZDOT = -19475
472887 ZDOT = -5936
124136
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 11344
86124387
00016717 00000-0 10270-3 0 9098
2 25544 51
6433 351
8944 0025094 150
5264 209
7312 15
58168694 28491
Satellite: ISS
Catalog Number: 25544
Epoch time: 11344
86124387 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 351
8944 deg
Eccentricity:
0025094
Arg of perigee: 150
5264 deg
Mean anomaly: 209
7312 deg
Mean motion: 15
58168694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 333
Coasting Arc #11 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2011/345/19:51:15
217
Vector Time (MET): N/A
Weight (LBS) : 871652
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6477269
89 A = 6775575
38 meter
Y = 82585
80 meter E =
0029509
Z = 2001951
93 I = 51
57921
XDOT = -1803
514523 Wp = 125
36257
YDOT = 4962
885816 meter/sec RA = 346
54089 deg
ZDOT = 5555
875722 TA = 256
77765
MA = 257
10700
Ha = 222
794 n
mi
Hp = 201
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21250885
46 X = 6466139
86
Y = 270950
79 feet Y = 154956
11 meter
Z = 6568083
76 Z = 2033391
53
XDOT = -5917
042397 XDOT = -1885
865928
YDOT = 16282
433780 feet/sec YDOT = 4942
256625 meter/sec
ZDOT = 18227
938721 ZDOT = 5546
914859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20342769
70 X = 6200476
21
Y = -6011814
42 feet Y = -1832401
04 meter
Z = 6696497
58 Z = 2041092
46
XDOT = -1381
894427 XDOT = -421
201421
YDOT = 15854
063242 feet/sec YDOT = 4832
318476 meter/sec
ZDOT = 18190
885755 ZDOT = 5544
581978
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 11345
88735704
00016717 00000-0 10270-3 0 9104
2 25544 51
6433 346
7471 0024819 154
1715 206
0691 15
58260395 28653
Satellite: ISS
Catalog Number: 25544
Epoch time: 11345
88735704 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 346
7471 deg
Eccentricity:
0024819
Arg of perigee: 154
1715 deg
Mean anomaly: 206
0691 deg
Mean motion: 15
58260395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 321
Coasting Arc #12 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2011/346/19:51:15
217
Vector Time (MET): N/A
Weight (LBS) : 871652
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4668054
18 A = 6768745
15 meter
Y = -2138870
83 meter E =
0026648
Z = -4414648
74 I = 51
52797
XDOT = 5206
721848 Wp = 137
10718
YDOT = -4536
903948 meter/sec RA = 341
52269 deg
ZDOT = -3338
448080 TA = 99
27053
MA = 98
96906
Ha = 222
493 n
mi
Hp = 201
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15315138
40 X = -4622344
45
Y = -7017292
76 feet Y = -2190815
76 meter
Z = -14483755
72 Z = -4437215
33
XDOT = 17082
420762 XDOT = 5273
284965
YDOT = -14884
855473 feet/sec YDOT = -4478
306606 meter/sec
ZDOT = -10952
913649 ZDOT = -3312
992763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16656862
40 X = -5077011
66
Y = -1916172
72 feet Y = -584049
45 meter
Z = -14575742
13 Z = -4442686
20
XDOT = 11507
517375 XDOT = 3507
491296
YDOT = -18278
579069 feet/sec YDOT = -5571
310900 meter/sec
ZDOT = -10848
524467 ZDOT = -3306
630257
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 11346
84930292
00016717 00000-0 10270-3 0 9111
2 25544 51
6435 341
9206 0024738 158
0544 202
1676 15
58323142 28808
Satellite: ISS
Catalog Number: 25544
Epoch time: 11346
84930292 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 341
9206 deg
Eccentricity:
0024738
Arg of perigee: 158
0544 deg
Mean anomaly: 202
1676 deg
Mean motion: 15
58323142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 303
Coasting Arc #13 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2011/347/19:51:15
217
Vector Time (MET): N/A
Weight (LBS) : 871652
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1723538
87 A = 6764944
85 meter
Y = 3839112
76 meter E =
0025654
Z = 5287806
00 I = 51
48761
XDOT = -7036
150512 Wp = 156
06001
YDOT = 3087
839742 meter/sec RA = 336
47446 deg
ZDOT = 28
462852 TA = 293
53413
MA = 293
80344
Ha = 222
314 n
mi
Hp = 201
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5654655
07 X = 1654793
98
Y = 12595514
29 feet Y = 3858001
49 meter
Z = 17348444
88 Z = 5296012
34
XDOT = -23084
483306 XDOT = -7070
294670
YDOT = 10130
707814 feet/sec YDOT = 3008
966276 meter/sec
ZDOT = 93
382059 ZDOT = -5
801188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9377828
86 X = 2858362
24
Y = 10076019
02 feet Y = 3071170
60 meter
Z = 17381622
79 Z = 5297918
62
XDOT = -17743
781169 XDOT = -5408
304500
YDOT = 16464
768342 feet/sec YDOT = 5018
461391 meter/sec
ZDOT = -46
857412 ZDOT = -14
282139
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 11347
87534225
00016717 00000-0 10270-3 0 9122
2 25544 51
6437 336
7734 0024804 161
7320 198
4731 15
58394175 28965
Satellite: ISS
Catalog Number: 25544
Epoch time: 11347
87534225 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 336
7734 deg
Eccentricity:
0024804
Arg of perigee: 161
7320 deg
Mean anomaly: 198
4731 deg
Mean motion: 15
58394175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 331
Coasting Arc #14 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2011/348/19:51:15
217
Vector Time (MET): N/A
Weight (LBS) : 871652
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1658739
40 A = 6768646
12 meter
Y = -4893643
44 meter E =
0030750
Z = -4400694
48 I = 51
47241
XDOT = 6848
641367 Wp = 151
24920
YDOT = -699
715196 meter/sec RA = 331
42143 deg
ZDOT = 3342
880119 TA = 152
77382
MA = 152
61228
Ha = 222
144 n
mi
Hp = 201
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5442058
40 X = 1734715
44
Y = -16055260
62 feet Y = -4874669
20 meter
Z = -14437974
00 Z = -4392452
26
XDOT = 22469
295825 XDOT = 6839
717720
YDOT = -2295
653529 feet/sec YDOT = -623
179674 meter/sec
ZDOT = 10967
454459 ZDOT = 3376
128853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -341134
50 X = -103977
80
Y = -16978061
24 feet Y = -5174913
07 meter
Z = -14403872
75 Z = -4390300
42
XDOT = 19002
105820 XDOT = 5791
841854
YDOT = -9848
119560 feet/sec YDOT = -3001
706842 meter/sec
ZDOT = 11103
332571 ZDOT = 3384
295768
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 11348
83721908
00016717 00000-0 10270-3 0 9136
2 25544 51
6432 331
9461 0024715 165
4277 194
7596 15
58445472 29110
Satellite: ISS
Catalog Number: 25544
Epoch time: 11348
83721908 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 331
9461 deg
Eccentricity:
0024715
Arg of perigee: 165
4277 deg
Mean anomaly: 194
7596 deg
Mean motion: 15
58445472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 330
Coasting Arc #15 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2011/349/19:51:15
217
Vector Time (MET): N/A
Weight (LBS) : 871652
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4353945
58 A = 6775093
31 meter
Y = 4771870
43 meter E =
0034533
Z = 1965208
72 I = 51
46849
XDOT = -4850
745825 Wp = 148
74296
YDOT = -2118
809293 meter/sec RA = 326
39824 deg
ZDOT = -5587
165665 TA = 9
41388
MA = 9
34932
Ha = 221
969 n
mi
Hp = 201
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14284598
36 X = -4416528
55
Y = 15655742
88 feet Y = 4722831
88 meter
Z = 6447535
17 Z = 1943905
71
XDOT = -15914
520422 XDOT = -4799
551097
YDOT = -6951
474059 feet/sec YDOT = -2172
766679 meter/sec
ZDOT = -18330
596014 ZDOT = -5610
606230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7713377
11 X = -2351037
34
Y = 19768047
36 feet Y = 6025300
83 meter
Z = 6360099
26 Z = 1938558
25
XDOT = -15805
674650 XDOT = -4817
569633
YDOT = -222
987849 feet/sec YDOT = -67
966696 meter/sec
ZDOT = -18426
161416 ZDOT = -5616
294000
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 11349
86318431
00016717 00000-0 10270-3 0 9144
2 25544 51
6435 326
7985 0024764 168
9471 191
2234 15
58487772 29271
Satellite: ISS
Catalog Number: 25544
Epoch time: 11349
86318431 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 326
7985 deg
Eccentricity:
0024764
Arg of perigee: 168
9471 deg
Mean anomaly: 191
2234 deg
Mean motion: 15
58487772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 349
Coasting Arc #16 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2011/350/19:51:15
217
Vector Time (MET): N/A
Weight (LBS) : 871652
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5743813
22 A = 6775820
53 meter
Y = -3428978
13 meter E =
0022662
Z = 1134746
89 I = 51
44631
XDOT = 1617
937051 Wp = 139
40849
YDOT = 4673
206077 meter/sec RA = 321
39374 deg
ZDOT = 5848
954292 TA = 232
94004
MA = 233
14748
Ha = 221
691 n
mi
Hp = 201
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18844531
55 X = 5776217
47
Y = -11249928
24 feet Y = -3364566
16 meter
Z = 3722922
86 Z = 1162728
73
XDOT = 5308
192423 XDOT = 1537
147043
YDOT = 15332
040936 feet/sec YDOT = 4690
846801 meter/sec
ZDOT = 19189
482586 ZDOT = 5856
618214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13198834
96 X = 4023004
90
Y = -17510043
49 feet Y = -5337061
26 meter
Z = 3837517
67 Z = 1169675
39
XDOT = 9307
648783 XDOT = 2836
971349
YDOT = 11286
190260 feet/sec YDOT = 3440
030791 meter/sec
ZDOT = 19220
384432 ZDOT = 5858
373175
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 11350
88910766
00016717 00000-0 10270-3 0 9158
2 25544 51
6424 321
6493 0024804 173
2372 186
9122 15
58582747 29434
Satellite: ISS
Catalog Number: 25544
Epoch time: 11350
88910766 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 321
6493 deg
Eccentricity:
0024804
Arg of perigee: 173
2372 deg
Mean anomaly: 186
9122 deg
Mean motion: 15
58582747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 326
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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