[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 2nd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 67 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
093/19:42:18
671 -0
8 1
9 1
9
N/A 1
8 -0
2 228
2
000/00:04:37
342 0
1 -0
1 214
4
Coasting Arc #1 (Orbit 2280)
---------------------------------------
Vector Time (GMT): 2013/091/13:20:20
923
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5216867
40 A = 6792241
43 meter
Y = -3596031
47 meter E =
0016779
Z = -2452956
24 I = 51
93214
XDOT = 1175
617812 Wp = 106
18087
YDOT = 5339
488276 meter/sec RA = 127
77114 deg
ZDOT = -5362
355267 TA = 101
11414
MA = 100
92542
Ha = 228
388 n
mi
Hp = 213
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17115706
69 X = 5268607
12
Y = -11798003
52 feet Y = -3537404
01 meter
Z = -8047756
68 Z = -2427487
18
XDOT = 3857
013818 XDOT = 1141
872137
YDOT = 17518
006155 feet/sec YDOT = 5352
445813 meter/sec
ZDOT = -17593
029092 ZDOT = -5356
726439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9182048
56 X = 2798688
40
Y = -18695839
10 feet Y = -5698491
76 meter
Z = -7941175
91 Z = -2420470
42
XDOT = 10676
535399 XDOT = 3254
207990
YDOT = 12657
235456 feet/sec YDOT = 3857
925367 meter/sec
ZDOT = -17570
144387 ZDOT = -5355
380009
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 13091
58323844
00016717 00000-0 10270-3 0 9008
2 25544 51
6438 128
5977 0012110 94
0887 266
1649 15
52273731 22812
Satellite: ISS
Catalog Number: 25544
Epoch time: 13091
58323844 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 128
5977 deg
Eccentricity:
0012110
Arg of perigee: 94
0887 deg
Mean anomaly: 266
1649 deg
Mean motion: 15
52273731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2281
Checksum: 314
Coasting Arc #2 (Orbit 2296)
---------------------------------------
Vector Time (GMT): 2013/092/13:20:20
923
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5065115
49 A = 6790009
94 meter
Y = 3020523
11 meter E =
0024645
Z = 3345378
43 I = 51
94230
XDOT = -479
924370 Wp = 92
83898
YDOT = -6045
420524 meter/sec RA = 122
82385 deg
ZDOT = 4700
764593 TA = 305
96340
MA = 306
19173
Ha = 228
393 n
mi
Hp = 213
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16617832
98 X = -5114766
13
Y = 9909852
71 feet Y = 2963604
36 meter
Z = 10975651
01 Z = 3320651
79
XDOT = -1574
555020 XDOT = -435
122572
YDOT = -19834
056836 feet/sec YDOT = -6050
536596 meter/sec
ZDOT = 15422
456015 ZDOT = 4698
542297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9398195
64 X = -2864570
03
Y = 16979144
99 feet Y = 5175243
39 meter
Z = 10872213
35 Z = 3313850
63
XDOT = -10216
989772 XDOT = -3114
138482
YDOT = -15590
857067 feet/sec YDOT = -4752
093234 meter/sec
ZDOT = 15413
858605 ZDOT = 4698
144103
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 13092
61328950
00016717 00000-0 10270-3 0 9017
2 25544 51
6432 123
4773 0012115 97
2476 263
0053 15
52297564 22970
Satellite: ISS
Catalog Number: 25544
Epoch time: 13092
61328950 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 123
4773 deg
Eccentricity:
0012115
Arg of perigee: 97
2476 deg
Mean anomaly: 263
0053 deg
Mean motion: 15
52297564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2297
Checksum: 301
Coasting Arc #3 (Orbit 2311)
---------------------------------------
Vector Time (GMT): 2013/093/13:20:20
923
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4877787
34 A = 6787397
34 meter
Y = -2244050
57 meter E =
0019013
Z = -4168638
41 I = 51
94953
XDOT = -164
089738 Wp = 89
49802
YDOT = 6647
953645 meter/sec RA = 117
87243 deg
ZDOT = -3785
454106 TA = 141
65045
MA = 141
51512
Ha = 228
297 n
mi
Hp = 213
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16003239
30 X = 4922768
32
Y = -7362370
65 feet Y = -2189252
84 meter
Z = -13676635
21 Z = -4144833
24
XDOT = -538
352159 XDOT = -220
027724
YDOT = 21810
871540 feet/sec YDOT = 6645
805686 meter/sec
ZDOT = -12419
468853 ZDOT = -3786
387524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9917699
62 X = 3022914
85
Y = -14651270
83 feet Y = -4465707
35 meter
Z = -13577113
75 Z = -4138304
27
XDOT = 9871
482523 XDOT = 3008
827873
YDOT = 18150
263870 feet/sec YDOT = 5532
200428 meter/sec
ZDOT = -12424
104442 ZDOT = -3786
867034
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 13093
57895130
00016717 00000-0 10270-3 0 9023
2 25544 51
6432 118
6759 0012091 100
7999 259
4515 15
52308949 23123
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
57895130 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 118
6759 deg
Eccentricity:
0012091
Arg of perigee: 100
7999 deg
Mean anomaly: 259
4515 deg
Mean motion: 15
52308949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2312
Checksum: 320
Coasting Arc #4 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/093/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2956967
49 A = 6784273
37 meter
Y = 3214686
78 meter E =
0024289
Z = -5212697
77 I = 51
94204
XDOT = -4288
728947 Wp = 101
20008
YDOT = 6178
659051 meter/sec RA = 116
51568 deg
ZDOT = 1378
423769 TA = 182
02995
MA = 182
03982
Ha = 228
183 n
mi
Hp = 214
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9701336
90 X = 2946122
19
Y = 10546872
63 feet Y = 3247692
46 meter
Z = -17102026
81 Z = -5198359
70
XDOT = -14070
633028 XDOT = -4364
197271
YDOT = 20271
191112 feet/sec YDOT = 6130
277908 meter/sec
ZDOT = 4522
387692 ZDOT = 1357
405865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2361163
00 X = 719682
48
Y = -14205867
65 feet Y = -4329948
46 meter
Z = -17042594
12 Z = -5194582
69
XDOT = 23626
088220 XDOT = 7201
231689
YDOT = -1389
167143 feet/sec YDOT = -423
418145 meter/sec
ZDOT = 4434
045983 ZDOT = 1351
497216
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 13093
83646073
00016717 00000-0 10270-3 0 9033
2 25544 51
6456 117
3960 0010386 101
9447 258
2870 15
51965781 23162
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
83646073 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 117
3960 deg
Eccentricity:
0010386
Arg of perigee: 101
9447 deg
Mean anomaly: 258
2870 deg
Mean motion: 15
51965781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 319
Coasting Arc #5 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/094/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2529247
99 A = 6785474
69 meter
Y = -3972168
92 meter E =
0015980
Z = 4871987
76 I = 51
95911
XDOT = 4367
924694 Wp = 87
17544
YDOT = -5811
042810 meter/sec RA = 111
56118 deg
ZDOT = -2462
511095 TA = 26
90574
MA = 26
82296
Ha = 228
160 n
mi
Hp = 214
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8298057
71 X = -2508309
05
Y = -13032050
27 feet Y = -4000335
07 meter
Z = 15984211
81 Z = 4859752
17
XDOT = 14330
461596 XDOT = 4444
542539
YDOT = -19065
101083 feet/sec YDOT = -5761
769743 meter/sec
ZDOT = -8079
104643 ZDOT = -2441
105615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4938273
44 X = -1505185
74
Y = 14694214
99 feet Y = 4478796
73 meter
Z = 15933631
87 Z = 4856570
99
XDOT = -22799
777369 XDOT = -6949
372142
YDOT = 1028
247600 feet/sec YDOT = 313
409868 meter/sec
ZDOT = -7989
175903 ZDOT = -2435
100815
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 13094
86672300
00016717 00000-0 10270-3 0 9040
2 25544 51
6453 112
2768 0010294 105
3592 254
8698 15
52011815 23325
Satellite: ISS
Catalog Number: 25544
Epoch time: 13094
86672300 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 112
2768 deg
Eccentricity:
0010294
Arg of perigee: 105
3592 deg
Mean anomaly: 254
8698 deg
Mean motion: 15
52011815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 299
Coasting Arc #6 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2013/095/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2188962
58 A = 6787414
25 meter
Y = 4699368
64 meter E =
0019153
Z = -4400453
02 I = 51
97632
XDOT = -4372
103832 Wp = 109
79416
YDOT = 5250
812446 meter/sec RA = 106
60964 deg
ZDOT = 3438
490833 TA = 194
97235
MA = 195
02913
Ha = 228
062 n
mi
Hp = 214
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7181635
75 X = 2157626
67
Y = 15417876
13 feet Y = 4723671
33 meter
Z = -14437181
84 Z = -4389895
89
XDOT = -14344
172676 XDOT = -4447
197790
YDOT = 17227
074955 feet/sec YDOT = 5201
501312 meter/sec
ZDOT = 11281
137904 ZDOT = 3417
068682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7240724
28 X = 2206972
76
Y = -15430901
37 feet Y = -4703338
74 meter
Z = -14393686
49 Z = -4387195
64
XDOT = 21336
606855 XDOT = 6503
397770
YDOT = -409
080833 feet/sec YDOT = -124
687838 meter/sec
ZDOT = 11191
193319 ZDOT = 3411
075724
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 13095
83258425
00016717 00000-0 10270-3 0 9057
2 25544 51
6459 107
4772 0010297 108
9474 251
2794 15
52000239 23475
Satellite: ISS
Catalog Number: 25544
Epoch time: 13095
83258425 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 107
4772 deg
Eccentricity:
0010297
Arg of perigee: 108
9474 deg
Mean anomaly: 251
2794 deg
Mean motion: 15
52000239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 316
Coasting Arc #7 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/096/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1863357
40 A = 6789621
82 meter
Y = -5351590
19 meter E =
0021405
Z = 3719180
86 I = 51
99138
XDOT = 4399
314352 Wp = 97
62348
YDOT = -4556
857870 meter/sec RA = 101
66191 deg
ZDOT = -4334
323917 TA = 38
23849
MA = 38
08686
Ha = 228
072 n
mi
Hp = 214
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6113377
28 X = -1821443
04
Y = -17557710
59 feet Y = -5372192
63 meter
Z = 12202036
94 Z = 3710231
28
XDOT = 14433
446037 XDOT = 4470
998101
YDOT = -14950
321097 feet/sec YDOT = -4507
261668 meter/sec
ZDOT = -14220
222826 ZDOT = -4312
777814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9303218
31 X = -2835620
94
Y = 16124244
76 feet Y = 4914669
80 meter
Z = 12165325
66 Z = 3707991
26
XDOT = -19626
136540 XDOT = -5982
046417
YDOT = -617
182006 feet/sec YDOT = -188
117075 meter/sec
ZDOT = -14129
832452 ZDOT = -4306
772931
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 13096
86282417
00016717 00000-0 10270-3 0 9060
2 25544 51
6455 102
3575 0010337 112
3849 247
8399 15
52025578 23639
Satellite: ISS
Catalog Number: 25544
Epoch time: 13096
86282417 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 102
3575 deg
Eccentricity:
0010337
Arg of perigee: 112
3849 deg
Mean anomaly: 247
8399 deg
Mean motion: 15
52025578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 323
Coasting Arc #8 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2013/097/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1626970
23 A = 6791752
62 meter
Y = 5903563
56 meter E =
0013598
Z = -2952473
31 I = 52
00404
XDOT = -4399
686156 Wp = 101
31538
YDOT = 3722
606879 meter/sec RA = 96
71775 deg
ZDOT = 5036
041198 TA = 225
24190
MA = 225
35263
Ha = 227
914 n
mi
Hp = 214
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5337828
82 X = 1575176
76
Y = 19368646
84 feet Y = 5921467
41 meter
Z = -9686592
22 Z = -2944696
14
XDOT = -14434
665867 XDOT = -4465
449954
YDOT = 12213
277163 feet/sec YDOT = 3673
039730 meter/sec
ZDOT = 16522
444875 ZDOT = 5014
507658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10904192
31 X = 3323597
81
Y = -16892293
36 feet Y = -5148771
02 meter
Z = -9654842
36 Z = -2942795
95
XDOT = 17552
468155 XDOT = 5349
992294
YDOT = 1970
515818 feet/sec YDOT = 600
613221 meter/sec
ZDOT = 16432
196432 ZDOT = 5008
533472
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 13097
82866218
00016717 00000-0 10270-3 0 9075
2 25544 51
6456 97
5575 0010190 116
1099 244
1102 15
52037268 23788
Satellite: ISS
Catalog Number: 25544
Epoch time: 13097
82866218 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 97
5575 deg
Eccentricity:
0010190
Arg of perigee: 116
1099 deg
Mean anomaly: 244
1102 deg
Mean motion: 15
52037268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 317
Coasting Arc #9 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2013/098/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1376276
18 A = 6793735
76 meter
Y = -6328088
93 meter E =
0024201
Z = 2012884
37 I = 52
01301
XDOT = 4460
116438 Wp = 115
18395
YDOT = -2764
397112 meter/sec RA = 91
77751 deg
ZDOT = -5598
809907 TA = 42
69308
MA = 42
50529
Ha = 227
964 n
mi
Hp = 214
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4515341
81 X = -1315189
97
Y = -20761446
61 feet Y = -6343137
52 meter
Z = 6603951
35 Z = 2006347
64
XDOT = 14632
927946 XDOT = 4517
894740
YDOT = -9069
544330 feet/sec YDOT = -2714
198902 meter/sec
ZDOT = -18368
798906 ZDOT = -5577
002227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12207156
50 X = -3720741
30
Y = 17400023
61 feet Y = 5303527
20 meter
Z = 6577435
57 Z = 2004802
36
XDOT = -15386
982343 XDOT = -4689
952218
YDOT = -3833
017723 feet/sec YDOT = -1168
303802 meter/sec
ZDOT = -18277
513622 ZDOT = -5570
986152
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 13098
85887904
00016717 00000-0 10270-3 0 9085
2 25544 51
6455 92
4374 0010339 120
0674 240
1505 15
52032446 23940
Satellite: ISS
Catalog Number: 25544
Epoch time: 13098
85887904 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 92
4374 deg
Eccentricity:
0010339
Arg of perigee: 120
0674 deg
Mean anomaly: 240
1505 deg
Mean motion: 15
52032446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 309
Coasting Arc #10 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2013/099/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1191599
50 A = 6794810
82 meter
Y = 6606083
38 meter E =
0014534
Z = -1057279
43 I = 52
01700
XDOT = -4532
027682 Wp = 82
38634
YDOT = 1753
415458 meter/sec RA = 86
83915 deg
ZDOT = 5919
273580 TA = 266
22891
MA = 266
39511
Ha = 227
745 n
mi
Hp = 214
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3909447
17 X = 1122776
33
Y = 21673501
89 feet Y = 6619023
66 meter
Z = -3468764
53 Z = -1051658
60
XDOT = -14868
857223 XDOT = -4580
052471
YDOT = 5752
675387 feet/sec YDOT = 1702
467618 meter/sec
ZDOT = 19420
188910 ZDOT = 5897
140303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12997996
18 X = 3961789
23
Y = -17782946
18 feet Y = -5420242
00 meter
Z = -3446115
06 Z = -1050375
87
XDOT = 13201
206709 XDOT = 4023
727805
YDOT = 5949
314617 feet/sec YDOT = 1813
351095 meter/sec
ZDOT = 19327
661663 ZDOT = 5891
071275
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 13099
82469372
00016717 00000-0 10270-3 0 9099
2 25544 51
6454 87
6371 0010116 123
5572 236
6547 15
52081257 24097
Satellite: ISS
Catalog Number: 25544
Epoch time: 13099
82469372 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 87
6371 deg
Eccentricity:
0010116
Arg of perigee: 123
5572 deg
Mean anomaly: 236
6547 deg
Mean motion: 15
52081257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 320
Coasting Arc #11 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2013/100/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -946384
99 A = 6795381
55 meter
Y = -6719035
93 meter E =
0022246
Z = -12051
00 I = 52
01595
XDOT = 4674
087786 Wp = 131
51094
YDOT = -660
418680 meter/sec RA = 81
90310 deg
ZDOT = -6045
447937 TA = 48
61817
MA = 48
42710
Ha = 227
783 n
mi
Hp = 214
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3104937
62 X = -871122
41
Y = -22044081
14 feet Y = -6729198
19 meter
Z = -39537
40 Z = -16465
03
XDOT = 15334
933682 XDOT = 4710
492902
YDOT = -2166
727953 feet/sec YDOT = -607
947137 meter/sec
ZDOT = -19834
146774 ZDOT = -6022
652831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13533967
46 X = -4125153
28
Y = 17675185
31 feet Y = 5387396
48 meter
Z = -57124
97 Z = -17411
69
XDOT = -11098
449958 XDOT = -3382
807547
YDOT = -8509
101427 feet/sec YDOT = -2593
574115 meter/sec
ZDOT = -19738
989012 ZDOT = -6016
443851
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 13100
85488632
00016717 00000-0 10270-3 0 9107
2 25544 51
6454 82
5170 0010218 128
1697 232
0376 15
52050377 24257
Satellite: ISS
Catalog Number: 25544
Epoch time: 13100
85488632 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 82
5170 deg
Eccentricity:
0010218
Arg of perigee: 128
1697 deg
Mean anomaly: 232
0376 deg
Mean motion: 15
52050377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 288
Coasting Arc #12 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2013/101/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 729992
30 A = 6794699
26 meter
Y = 6675258
90 meter E =
0018793
Z = 1017020
70 I = 52
00885
XDOT = -4841
303382 Wp = 87
17107
YDOT = -387
787200 meter/sec RA = 76
96557 deg
ZDOT = 5926
872276 TA = 283
78216
MA = 283
99123
Ha = 227
541 n
mi
Hp = 214
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2394987
87 X = 650353
39
Y = 21900455
72 feet Y = 6682976
93 meter
Z = 3336682
08 Z = 1020372
99
XDOT = -15883
541278 XDOT = -4865
398832
YDOT = -1272
267716 feet/sec YDOT = -442
059940 meter/sec
ZDOT = 19445
119015 ZDOT = 5903
294803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13648593
70 X = 4160091
36
Y = -17291439
96 feet Y = -5270430
90 meter
Z = 3349831
21 Z = 1021028
55
XDOT = 9268
442329 XDOT = 2825
021222
YDOT = 11122
946370 feet/sec YDOT = 3390
274054 meter/sec
ZDOT = 19346
826855 ZDOT = 5896
912825
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 13101
88506316
00016717 00000-0 10270-3 0 9112
2 25544 51
6450 77
3964 0010051 131
7839 228
4173 15
52132028 24415
Satellite: ISS
Catalog Number: 25544
Epoch time: 13101
88506316 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 77
3964 deg
Eccentricity:
0010051
Arg of perigee: 131
7839 deg
Mean anomaly: 228
4173 deg
Mean motion: 15
52132028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 281
Coasting Arc #13 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2013/102/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -403960
71 A = 6793420
12 meter
Y = -6456724
23 meter E =
0016578
Z = -2057951
10 I = 51
99622
XDOT = 5052
957412 Wp = 136
82905
YDOT = 1449
744593 meter/sec RA = 72
02726 deg
ZDOT = -5578
571288 TA = 65
79667
MA = 65
62349
Ha = 227
524 n
mi
Hp = 214
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1325330
41 X = -321733
09
Y = -21183478
46 feet Y = -6460781
95 meter
Z = -6751808
09 Z = -2059713
39
XDOT = 16577
944266 XDOT = 5063
470120
YDOT = 4756
379898 feet/sec YDOT = 1506
308368 meter/sec
ZDOT = -18302
399238 ZDOT = -5553
998654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13647238
38 X = -4159678
26
Y = 16253028
21 feet Y = 4953923
00 meter
Z = -6758337
92 Z = -2059941
40
XDOT = -7651
965120 XDOT = -2332
318969
YDOT = -13941
044875 feet/sec YDOT = -4249
230478 meter/sec
ZDOT = -18200
091119 ZDOT = -5547
387773
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 13102
85084562
00016717 00000-0 10270-3 0 9125
2 25544 51
6448 72
5964 0010029 135
6185 224
5772 15
52104160 24565
Satellite: ISS
Catalog Number: 25544
Epoch time: 13102
85084562 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 72
5964 deg
Eccentricity:
0010029
Arg of perigee: 135
6185 deg
Mean anomaly: 224
5772 deg
Mean motion: 15
52104160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 294
Coasting Arc #14 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2013/103/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 71639
40 A = 6791364
18 meter
Y = 6108484
23 meter E =
0020407
Z = 2957654
00 I = 51
97927
XDOT = -5274
337587 Wp = 106
31982
YDOT = -2387
506540 meter/sec RA = 67
08447 deg
ZDOT = 5024
443634 TA = 287
26382
MA = 287
48702
Ha = 227
344 n
mi
Hp = 214
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 235037
41 X = -11039
99
Y = 20040958
75 feet Y = 6108823
20 meter
Z = 9703589
25 Z = 2957800
90
XDOT = -17304
257176 XDOT = -5271
655713
YDOT = -7833
026707 feet/sec YDOT = -2446
472268 meter/sec
ZDOT = 16484
395126 ZDOT = 4998
827641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13411143
61 X = 4087716
57
Y = -14894291
88 feet Y = -4539780
16 meter
Z = 9703412
35 Z = 2957600
08
XDOT = 6455
177038 XDOT = 1967
537961
YDOT = 16555
545646 feet/sec YDOT = 5046
130313 meter/sec
ZDOT = 16377
857964 ZDOT = 4991
971107
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 13103
88099898
00016717 00000-0 10270-3 0 9138
2 25544 51
6445 67
4756 0009952 139
5330 220
6564 15
52159795 24720
Satellite: ISS
Catalog Number: 25544
Epoch time: 13103
88099898 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 67
4756 deg
Eccentricity:
0009952
Arg of perigee: 139
5330 deg
Mean anomaly: 220
6564 deg
Mean motion: 15
52159795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 342
Coasting Arc #15 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2013/104/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 404052
70 A = 6788928
80 meter
Y = -5609760
35 meter E =
0013649
Z = -3807045
63 I = 51
95760
XDOT = 5479
552047 Wp = 118
34123
YDOT = 3261
907523 meter/sec RA = 62
13762 deg
ZDOT = -4242
765923 TA = 107
03700
MA = 106
88742
Ha = 227
318 n
mi
Hp = 215
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1325632
23 X = 485246
04
Y = -18404725
55 feet Y = -5604788
14 meter
Z = -12490307
20 Z = -3804885
33
XDOT = 17977
532963 XDOT = 5463
279908
YDOT = 10701
796336 feet/sec YDOT = 3323
092183 meter/sec
ZDOT = -13919
835707 ZDOT = -4216
186073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13250002
87 X = -4038600
87
Y = 12851927
44 feet Y = 3917267
48 meter
Z = -12480560
19 Z = -3804074
75
XDOT = -5495
254838 XDOT = -1674
953675
YDOT = -19018
948146 feet/sec YDOT = -5796
975395 meter/sec
ZDOT = -13809
395846 ZDOT = -4209
103854
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 13104
84675755
00016717 00000-0 10270-3 0 9148
2 25544 51
6437 62
6752 0010017 142
6098 217
5752 15
52162744 24872
Satellite: ISS
Catalog Number: 25544
Epoch time: 13104
84675755 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 62
6752 deg
Eccentricity:
0010017
Arg of perigee: 142
6098 deg
Mean anomaly: 217
5752 deg
Mean motion: 15
52162744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2487
Checksum: 314
Coasting Arc #16 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2013/105/19:44:37
342
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -903487
29 A = 6786671
35 meter
Y = 5035241
04 meter E =
0018230
Z = 4454005
20 I = 51
93487
XDOT = -5656
102066 Wp = 129
00098
YDOT = -3971
287622 meter/sec RA = 57
18564 deg
ZDOT = 3321
909808 TA = 287
51516
MA = 287
71430
Ha = 227
231 n
mi
Hp = 215
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2964197
13 X = -981361
85
Y = 16519819
67 feet Y = 5024702
40 meter
Z = 14612877
94 Z = 4449426
77
XDOT = -18556
765310 XDOT = -5627
411003
YDOT = -13029
158866 feet/sec YDOT = -4034
377187 meter/sec
ZDOT = 10898
654225 ZDOT = 3294
502520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13057524
72 X = 3979933
53
Y = -10572098
19 feet Y = -3222375
53 meter
Z = 14593111
26 Z = 4447980
31
XDOT = 4917
829299 XDOT = 1498
954370
YDOT = 21052
783709 feet/sec YDOT = 6416
888475 meter/sec
ZDOT = 10784
861137 ZDOT = 3287
225674
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 13105
87688742
00016717 00000-0 10270-3 0 9153
2 25544 51
6438 57
5545 0009960 146
5124 213
6659 15
52163993 25033
Satellite: ISS
Catalog Number: 25544
Epoch time: 13105
87688742 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 57
5545 deg
Eccentricity:
0009960
Arg of perigee: 146
5124 deg
Mean anomaly: 213
6659 deg
Mean motion: 15
52163993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2503
Checksum: 330
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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