[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 28th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
311/10:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 221
1
314/23:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 220
9
Coasting Arc #1 (Orbit 1540)
---------------------------------------
Vector Time (GMT): 2013/301/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6402276
91 A = 6800377
05 meter
Y = -255190
21 meter E =
0015042
Z = 2258309
79 I = 51
73889
XDOT = 2128
528561 Wp = 74
29531
YDOT = -4950
905009 meter/sec RA = 166
14381 deg
ZDOT = 5448
648621 TA = 310
75093
MA = 310
88142
Ha = 228
631 n
mi
Hp = 221
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21004845
50 X = -6409917
91
Y = -837238
21 feet Y = -326827
10 meter
Z = 7409152
85 Z = 2227189
09
XDOT = 6983
361419 XDOT = 2157
264008
YDOT = -16243
126670 feet/sec YDOT = -4926
941385 meter/sec
ZDOT = 17876
143770 ZDOT = 5459
059134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4414487
01 X = 1345535
64
Y = -20599428
44 feet Y = -6278705
79 meter
Z = 7278454
54 Z = 2218472
94
XDOT = 13329
630826 XDOT = 4062
871476
YDOT = 9219
433128 feet/sec YDOT = 2810
083218 meter/sec
ZDOT = 17920
506383 ZDOT = 5462
170345
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 13301
68198447
00016717 00000-0 10270-3 0 9002
2 25544 51
6458 166
9190 0001366 101
0984 259
0320 15
49626251 15415
Satellite: ISS
Catalog Number: 25544
Epoch time: 13301
68198447 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 166
9190 deg
Eccentricity:
0001366
Arg of perigee: 101
0984 deg
Mean anomaly: 259
0320 deg
Mean motion: 15
49626251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1541
Checksum: 301
Coasting Arc #2 (Orbit 1555)
---------------------------------------
Vector Time (GMT): 2013/302/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6332107
17 A = 6799841
86 meter
Y = -95992
08 meter E =
0006726
Z = -2474703
36 I = 51
76738
XDOT = -2000
720708 Wp = 125
78982
YDOT = 5118
474970 meter/sec RA = 161
20065 deg
ZDOT = -5331
858579 TA = 81
81423
MA = 81
73794
Ha = 228
601 n
mi
Hp = 221
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20774629
82 X = 6344731
60
Y = -314934
65 feet Y = -25112
05 meter
Z = -8119105
53 Z = -2443911
36
XDOT = -6564
044318 XDOT = -2031
906751
YDOT = 16792
896884 feet/sec YDOT = 5095
926820 meter/sec
ZDOT = -17492
974339 ZDOT = -5341
654245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2886259
86 X = -879732
01
Y = 20626148
25 feet Y = 6286849
99 meter
Z = -7989731
83 Z = -2435270
26
XDOT = -14096
918725 XDOT = -4296
740827
YDOT = -8746
786678 feet/sec YDOT = -2666
020579 meter/sec
ZDOT = -17534
780862 ZDOT = -5344
601207
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 13302
64931667
00016717 00000-0 10270-3 0 9019
2 25544 51
6461 162
1296 0001447 97
7001 262
4313 15
49661402 15568
Satellite: ISS
Catalog Number: 25544
Epoch time: 13302
64931667 = yrday
fracday
Element set: 901
Inclination: 51
6461 deg
RA of node: 162
1296 deg
Eccentricity:
0001447
Arg of perigee: 97
7001 deg
Mean anomaly: 262
4313 deg
Mean motion: 15
49661402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1556
Checksum: 291
Coasting Arc #3 (Orbit 1571)
---------------------------------------
Vector Time (GMT): 2013/303/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6235684
85 A = 6799431
18 meter
Y = 459586
23 meter E =
0014812
Z = 2655240
00 I = 51
79432
XDOT = 1842
065207 Wp = 80
44603
YDOT = -5299
343464 meter/sec RA = 156
25819 deg
ZDOT = 5220
808949 TA = 309
38398
MA = 309
51507
Ha = 228
586 n
mi
Hp = 221
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20458283
64 X = -6253259
29
Y = 1507828
83 feet Y = 389756
81 meter
Z = 8711417
34 Z = 2624904
27
XDOT = 6043
521019 XDOT = 1875
824936
YDOT = -17386
297454 feet/sec YDOT = -5278
555084 meter/sec
ZDOT = 17128
638284 ZDOT = 5229
840197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1306574
85 X = 398244
01
Y = -20525914
57 feet Y = -6256298
76 meter
Z = 8583903
69 Z = 2616373
85
XDOT = 14914
634101 XDOT = 4545
980474
YDOT = 8159
935008 feet/sec YDOT = 2487
148190 meter/sec
ZDOT = 17167
262940 ZDOT = 5232
581744
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 13303
68112175
00016717 00000-0 10270-3 0 9020
2 25544 51
6455 157
0199 0001443 109
5386 250
5920 15
49672059 15720
Satellite: ISS
Catalog Number: 25544
Epoch time: 13303
68112175 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 157
0199 deg
Eccentricity:
0001443
Arg of perigee: 109
5386 deg
Mean anomaly: 250
5920 deg
Mean motion: 15
49672059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1572
Checksum: 304
Coasting Arc #4 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2013/304/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6113372
22 A = 6798805
16 meter
Y = -767056
04 meter E =
0006143
Z = -2875536
81 I = 51
82083
XDOT = -1694
918113 Wp = 115
78358
YDOT = 5476
218305 meter/sec RA = 151
31832 deg
ZDOT = -5075
222985 TA = 96
76445
MA = 96
69454
Ha = 228
530 n
mi
Hp = 221
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20056995
46 X = 6135464
15
Y = -2516588
06 feet Y = -698569
15 meter
Z = -9434175
88 Z = -2845784
16
XDOT = -5560
754965 XDOT = -1731
373775
YDOT = 17966
595489 feet/sec YDOT = 5457
060369 meter/sec
ZDOT = -16650
994044 ZDOT = -5083
545973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 95693
41 X = 29167
35
Y = 20271954
83 feet Y = 6178891
83 meter
Z = -9309062
63 Z = -2837402
29
XDOT = -15706
232059 XDOT = -4787
259532
YDOT = -7571
665445 feet/sec YDOT = -2307
843628 meter/sec
ZDOT = -16686
673900 ZDOT = -5086
098205
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 13304
64842394
00016717 00000-0 10270-3 0 9031
2 25544 51
6459 152
2304 0001497 105
8929 254
2387 15
49710676 15872
Satellite: ISS
Catalog Number: 25544
Epoch time: 13304
64842394 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 152
2304 deg
Eccentricity:
0001497
Arg of perigee: 105
8929 deg
Mean anomaly: 254
2387 deg
Mean motion: 15
49710676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 327
Coasting Arc #5 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2013/305/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5967072
57 A = 6798311
04 meter
Y = 1081071
65 meter E =
0014352
Z = 3059543
32 I = 51
84526
XDOT = 1514
531174 Wp = 87
05747
YDOT = -5663
871814 meter/sec RA = 146
37908 deg
ZDOT = 4935
854313 TA = 307
89035
MA = 308
02005
Ha = 228
512 n
mi
Hp = 221
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19577009
75 X = -5993580
70
Y = 3546823
01 feet Y = 1014196
06 meter
Z = 10037871
79 Z = 3030490
56
XDOT = 4968
934299 XDOT = 1553
775571
YDOT = -18582
256609 feet/sec YDOT = -5646
715563 meter/sec
ZDOT = 16193
747746 ZDOT = 4943
307721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1518016
06 X = -462691
29
Y = -19899087
48 feet Y = -6065241
86 meter
Z = 9915648
20 Z = 3022289
57
XDOT = 16533
767814 XDOT = 5039
492430
YDOT = 6855
840572 feet/sec YDOT = 2089
660206 meter/sec
ZDOT = 16225
808569 ZDOT = 4945
626452
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 13305
68019694
00016717 00000-0 10270-3 0 9046
2 25544 51
6453 147
1206 0001492 117
2831 242
8472 15
49724590 16031
Satellite: ISS
Catalog Number: 25544
Epoch time: 13305
68019694 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 147
1206 deg
Eccentricity:
0001492
Arg of perigee: 117
2831 deg
Mean anomaly: 242
8472 deg
Mean motion: 15
49724590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 301
Coasting Arc #6 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2013/306/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5804608
61 A = 6797646
25 meter
Y = -1334270
98 meter E =
0006051
Z = -3279939
10 I = 51
86883
XDOT = -1340
358601 Wp = 102
64913
YDOT = 5845
256706 meter/sec RA = 141
44197 deg
ZDOT = -4758
603090 TA = 115
17620
MA = 115
11343
Ha = 228
442 n
mi
Hp = 221
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19043991
52 X = 5835030
85
Y = -4377529
47 feet Y = -1269190
23 meter
Z = -10760955
04 Z = -3251666
02
XDOT = -4397
501973 XDOT = -1382
505229
YDOT = 19177
351396 feet/sec YDOT = 5830
032052 meter/sec
ZDOT = -15612
214862 ZDOT = -4765
217315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2732888
94 X = 832984
55
Y = 19414285
33 feet Y = 5917474
17 meter
Z = -10641962
87 Z = -3243670
28
XDOT = -17323
870663 XDOT = -5280
315778
YDOT = -6119
077552 feet/sec YDOT = -1865
094838 meter/sec
ZDOT = -15640
785918 ZDOT = -4767
311548
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 13306
64746918
00016717 00000-0 10270-3 0 9050
2 25544 51
6457 142
3307 0001499 114
4374 245
6932 15
49751525 16188
Satellite: ISS
Catalog Number: 25544
Epoch time: 13306
64746918 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 142
3307 deg
Eccentricity:
0001499
Arg of perigee: 114
4374 deg
Mean anomaly: 245
6932 deg
Mean motion: 15
49751525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 322
Coasting Arc #7 (Orbit 1633)
---------------------------------------
Vector Time (GMT): 2013/307/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5621701
21 A = 6797037
69 meter
Y = 1588651
74 meter E =
0013617
Z = 3463768
36 I = 51
89052
XDOT = 1131
650503 Wp = 94
03425
YDOT = -6034
092532 meter/sec RA = 136
50542 deg
ZDOT = 4587
734365 TA = 306
37054
MA = 306
49611
Ha = 228
405 n
mi
Hp = 221
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18443901
60 X = -5655874
61
Y = 5212112
02 feet Y = 1525595
33 meter
Z = 11364069
44 Z = 3436374
75
XDOT = 3712
764117 XDOT = 1176
754285
YDOT = -19796
891508 feet/sec YDOT = -6021
185377 meter/sec
ZDOT = 15051
621934 ZDOT = 4593
341720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3939752
14 X = -1200836
45
Y = -18826317
01 feet Y = -5738261
42 meter
Z = 11248725
83 Z = 3428611
63
XDOT = 18130
347723 XDOT = 5526
129986
YDOT = 5246
407242 feet/sec YDOT = 1599
104927 meter/sec
ZDOT = 15076
001431 ZDOT = 4595
165236
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 13307
67920950
00016717 00000-0 10270-3 0 9065
2 25544 51
6456 137
2207 0001480 124
3527 235
7763 15
49781317 16341
Satellite: ISS
Catalog Number: 25544
Epoch time: 13307
67920950 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 137
2207 deg
Eccentricity:
0001480
Arg of perigee: 124
3527 deg
Mean anomaly: 235
7763 deg
Mean motion: 15
49781317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1634
Checksum: 310
Coasting Arc #8 (Orbit 1648)
---------------------------------------
Vector Time (GMT): 2013/308/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5433692
52 A = 6796370
85 meter
Y = -1779855
95 meter E =
0006623
Z = -3679677
84 I = 51
91054
XDOT = -924
379705 Wp = 89
72529
YDOT = 6211
882384 meter/sec RA = 131
57063 deg
ZDOT = -4376
464603 TA = 133
71473
MA = 133
65985
Ha = 228
330 n
mi
Hp = 221
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17827075
21 X = 5471066
83
Y = -5839422
40 feet Y = -1718883
98 meter
Z = -12072433
87 Z = -3653189
88
XDOT = -3032
741815 XDOT = -972
513329
YDOT = 20380
191550 feet/sec YDOT = 6201
276233 meter/sec
ZDOT = -14358
479667 ZDOT = -4381
072235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4920762
98 X = 1499848
56
Y = 18176114
84 feet Y = 5540079
80 meter
Z = -11960855
53 Z = -3645668
76
XDOT = -18877
197400 XDOT = -5753
769768
YDOT = -4336
623717 feet/sec YDOT = -1321
802909 meter/sec
ZDOT = -14378
697009 ZDOT = -4382
626848
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 13308
64645177
00016717 00000-0 10270-3 0 9079
2 25544 51
6461 132
4306 0001442 122
6716 237
4573 15
49789421 16491
Satellite: ISS
Catalog Number: 25544
Epoch time: 13308
64645177 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 132
4306 deg
Eccentricity:
0001442
Arg of perigee: 122
6716 deg
Mean anomaly: 237
4573 deg
Mean motion: 15
49789421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1649
Checksum: 314
Coasting Arc #9 (Orbit 1664)
---------------------------------------
Vector Time (GMT): 2013/309/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5229914
82 A = 6795652
96 meter
Y = 1967543
97 meter E =
0012603
Z = 3858875
12 I = 51
92912
XDOT = 682
774085 Wp = 101
26258
YDOT = -6393
332374 meter/sec RA = 126
63646 deg
ZDOT = 4171
237559 TA = 304
94275
MA = 305
06107
Ha = 228
278 n
mi
Hp = 221
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17158513
20 X = -5270273
50
Y = 6455196
75 feet Y = 1908834
03 meter
Z = 12660351
45 Z = 3833369
99
XDOT = 2240
072457 XDOT = 733
951714
YDOT = -20975
499914 feet/sec YDOT = -6385
411064 meter/sec
ZDOT = 13685
162594 ZDOT = 4174
678728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5870608
85 X = -1789361
58
Y = -17445063
50 feet Y = -5317255
36 meter
Z = 12552862
23 Z = 3826112
41
XDOT = 19617
579294 XDOT = 5979
438169
YDOT = 3289
864203 feet/sec YDOT = 1002
750609 meter/sec
ZDOT = 13700
516886 ZDOT = 4175
917547
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 13309
67815916
00016717 00000-0 10270-3 0 9084
2 25544 51
6469 127
3207 0001406 130
2212 229
9062 15
49837973 16651
Satellite: ISS
Catalog Number: 25544
Epoch time: 13309
67815916 = yrday
fracday
Element set: 908
Inclination: 51
6469 deg
RA of node: 127
3207 deg
Eccentricity:
0001406
Arg of perigee: 130
2212 deg
Mean anomaly: 229
9062 deg
Mean motion: 15
49837973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1665
Checksum: 319
Coasting Arc #10 (Orbit 1679)
---------------------------------------
Vector Time (GMT): 2013/310/14:55:32
144
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5032961
61 A = 6795000
99 meter
Y = -2092616
36 meter E =
0007836
Z = -4064991
93 I = 51
94502
XDOT = -439
182577 Wp = 80
65096
YDOT = 6556
645767 meter/sec RA = 121
70366 deg
ZDOT = -3924
265374 TA = 148
74538
MA = 148
69877
Ha = 228
199 n
mi
Hp = 221
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16512341
24 X = 5075734
70
Y = -6865539
23 feet Y = -2036095
33 meter
Z = -13336587
70 Z = -4040437
87
XDOT = -1440
887719 XDOT = -493
404359
YDOT = 21511
305010 feet/sec YDOT = 6551
431462 meter/sec
ZDOT = -12874
886399 ZDOT = -3926
530493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6590794
59 X = 2008874
19
Y = 16706438
33 feet Y = 5092122
40 meter
Z = -13233063
09 Z = -4033437
63
XDOT = -20266
524643 XDOT = -6177
236711
YDOT = -2197
476713 feet/sec YDOT = -669
790902 meter/sec
ZDOT = -12885
332943 ZDOT = -3927
449481
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 13310
64537126
00016717 00000-0 10270-3 0 9098
2 25544 51
6474 122
5308 0001344 129
7234 230
4035 15
49829919 16809
Satellite: ISS
Catalog Number: 25544
Epoch time: 13310
64537126 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 122
5308 deg
Eccentricity:
0001344
Arg of perigee: 129
7234 deg
Mean anomaly: 230
4035 deg
Mean motion: 15
49829919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1680
Checksum: 301
Coasting Arc #11 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2013/311/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2353862
29 A = 6791305
42 meter
Y = -3942376
48 meter E =
0006681
Z = 4999640
62 I = 51
94449
XDOT = 4804
461058 Wp = 64
20149
YDOT = -5578
477444 meter/sec RA = 117
63495 deg
ZDOT = -2131
795735 TA = 46
51091
MA = 46
45539
Ha = 228
142 n
mi
Hp = 221
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7722645
29 X = -2333890
15
Y = -12934306
04 feet Y = -3968587
30 meter
Z = 16403020
41 Z = 4988253
99
XDOT = 15762
667512 XDOT = 4876
839615
YDOT = -18302
091351 feet/sec YDOT = -5524
346167 meter/sec
ZDOT = -6994
080497 ZDOT = -2108
279986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12404205
82 X = 3780801
94
Y = 8638356
02 feet Y = 2632970
92 meter
Z = 16355704
96 Z = 4985218
87
XDOT = -6376
317701 XDOT = -1943
501635
YDOT = 22241
207298 feet/sec YDOT = 6779
119985 meter/sec
ZDOT = -6894
413578 ZDOT = -2101
417259
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 13311
48360741
00016717 00000-0 10270-3 0 9100
2 25544 51
6462 118
3814 0000942 116
4447 243
6800 15
49846562 16936
Satellite: ISS
Catalog Number: 25544
Epoch time: 13311
48360741 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 118
3814 deg
Eccentricity:
0000942
Arg of perigee: 116
4447 deg
Mean anomaly: 243
6800 deg
Mean motion: 15
49846562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 300
Coasting Arc #12 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2013/312/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2476564
22 A = 6791658
06 meter
Y = 4013370
44 meter E =
0012899
Z = -4899452
34 I = 51
95891
XDOT = -4458
268460 Wp = 108
35154
YDOT = 5721
545954 meter/sec RA = 112
70050 deg
ZDOT = 2434
537889 TA = 185
47122
MA = 185
48533
Ha = 228
041 n
mi
Hp = 221
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8125210
68 X = 2455302
31
Y = 13167225
86 feet Y = 4040946
14 meter
Z = -16074318
69 Z = -4887472
83
XDOT = -14626
865025 XDOT = -4533
743192
YDOT = 18771
476226 feet/sec YDOT = 5671
268726 meter/sec
ZDOT = 7987
329032 ZDOT = 2412
696458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13012372
12 X = -3966171
02
Y = -8465902
75 feet Y = -2580407
16 meter
Z = -16024520
86 Z = -4884273
96
XDOT = 4767
512621 XDOT = 1453
137847
YDOT = -22262
941492 feet/sec YDOT = -6785
744567 meter/sec
ZDOT = 7894
664405 ZDOT = 2406
293711
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 13312
45079118
00016717 00000-0 10270-3 0 9114
2 25544 51
6456 113
5898 0001079 117
7075 242
4185 15
49884532 17080
Satellite: ISS
Catalog Number: 25544
Epoch time: 13312
45079118 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 113
5898 deg
Eccentricity:
0001079
Arg of perigee: 117
7075 deg
Mean anomaly: 242
4185 deg
Mean motion: 15
49884532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 318
Coasting Arc #13 (Orbit 1723)
---------------------------------------
Vector Time (GMT): 2013/313/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2596506
84 A = 6792182
93 meter
Y = -4088203
03 meter E =
0008288
Z = 4756877
44 I = 51
97188
XDOT = 4132
943314 Wp = 68
59878
YDOT = -5837
892953 meter/sec RA = 107
76832 deg
ZDOT = -2754
528454 TA = 48
58060
MA = 48
50941
Ha = 228
079 n
mi
Hp = 221
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8518723
23 X = -2573706
57
Y = -13412739
60 feet Y = -4117111
32 meter
Z = 15606553
28 Z = 4744319
09
XDOT = 13559
525309 XDOT = 4211
297664
YDOT = -19153
192102 feet/sec YDOT = -5791
237655 meter/sec
ZDOT = -9037
166845 ZDOT = -2734
260409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13614734
80 X = 4149771
17
Y = 8290745
78 feet Y = 2527019
31 meter
Z = 15554332
67 Z = 4740960
60
XDOT = -3259
297247 XDOT = -993
433801
YDOT = 22187
457477 feet/sec YDOT = 6762
737039 meter/sec
ZDOT = -8951
087491 ZDOT = -2728
291467
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 13313
48243723
00016717 00000-0 10270-3 0 9124
2 25544 51
6457 108
4801 0000991 121
7177 238
4070 15
49890058 17244
Satellite: ISS
Catalog Number: 25544
Epoch time: 13313
48243723 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 108
4801 deg
Eccentricity:
0000991
Arg of perigee: 121
7177 deg
Mean anomaly: 238
4070 deg
Mean motion: 15
49890058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1724
Checksum: 302
Coasting Arc #14 (Orbit 1738)
---------------------------------------
Vector Time (GMT): 2013/314/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2755060
93 A = 6792641
01 meter
Y = 4161724
74 meter E =
0011212
Z = -4618646
05 I = 51
98239
XDOT = -3794
416127 Wp = 111
40011
YDOT = 5900
660023 meter/sec RA = 102
83572 deg
ZDOT = 3055
496462 TA = 189
04446
MA = 189
06468
Ha = 227
977 n
mi
Hp = 220
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9038913
83 X = 2730755
24
Y = 13653952
56 feet Y = 4192397
59 meter
Z = -15153038
22 Z = -4605321
18
XDOT = -12448
871807 XDOT = -3874
959548
YDOT = 19359
120811 feet/sec YDOT = 5857
778164 meter/sec
ZDOT = 10024
594691 ZDOT = 3036
867558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14325855
63 X = -4366520
80
Y = -8036111
79 feet Y = -2449406
87 meter
Z = -15097606
39 Z = -4601750
43
XDOT = 1800
539635 XDOT = 548
804481
YDOT = -21882
098320 feet/sec YDOT = -6669
663568 meter/sec
ZDOT = 9945
387515 ZDOT = 3031
354115
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 13314
44958996
00016717 00000-0 10270-3 0 9137
2 25544 51
6458 103
6886 0001148 122
3087 237
8175 15
49932771 17391
Satellite: ISS
Catalog Number: 25544
Epoch time: 13314
44958996 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 103
6886 deg
Eccentricity:
0001148
Arg of perigee: 122
3087 deg
Mean anomaly: 237
8175 deg
Mean motion: 15
49932771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1739
Checksum: 342
Coasting Arc #15 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2013/314/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4191450
45 A = 6792241
46 meter
Y = 2533763
05 meter E =
0009007
Z = 4700811
54 I = 51
98501
XDOT = -1015
536446 Wp = 115
66765
YDOT = -7031
469234 meter/sec RA = 100
23290 deg
ZDOT = 2876
425739 TA = 305
84383
MA = 305
92746
Ha = 227
994 n
mi
Hp = 220
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13751477
87 X = -4242307
59
Y = 8312870
89 feet Y = 2486607
35 meter
Z = 15422610
05 Z = 4680326
00
XDOT = -3331
812488 XDOT = -950
806599
YDOT = -23069
124782 feet/sec YDOT = -7042
463604 meter/sec
ZDOT = 9437
092318 ZDOT = 2871
649715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5007076
83 X = -1526157
02
Y = 15355703
54 feet Y = 4680418
44 meter
Z = 15336082
19 Z = 4674437
85
XDOT = -16562
359851 XDOT = -5048
207283
YDOT = -14833
153725 feet/sec YDOT = -4521
145255 meter/sec
ZDOT = 9418
036880 ZDOT = 2870
617641
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 13315
02987363
00016717 00000-0 10270-3 0 9143
2 25544 51
6460 100
8177 0000908 113
4163 246
7083 15
49961018 17488
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
02987363 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 100
8177 deg
Eccentricity:
0000908
Arg of perigee: 113
4163 deg
Mean anomaly: 246
7083 deg
Mean motion: 15
49961018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 305
Coasting Arc #16 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2013/315/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4046932
71 A = 6791635
95 meter
Y = -2497867
06 meter E =
0012337
Z = -4860201
12 I = 51
98770
XDOT = 1333
852581 Wp = 74
83560
YDOT = 7094
269824 meter/sec RA = 95
30031 deg
ZDOT = -2537
627189 TA = 170
28273
MA = 170
25884
Ha = 227
920 n
mi
Hp = 220
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13277338
29 X = 4098173
53
Y = -8195101
90 feet Y = -2452325
36 meter
Z = -15945541
72 Z = -4840416
63
XDOT = 4376
156762 XDOT = 1266
751046
YDOT = 23275
163463 feet/sec YDOT = 7108
810532 meter/sec
ZDOT = -8325
548521 ZDOT = -2531
310608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4470653
84 X = 1362655
29
Y = -15037258
58 feet Y = -4583356
42 meter
Z = -15861961
31 Z = -4834725
81
XDOT = 17753
791971 XDOT = 5411
355793
YDOT = 14025
768053 feet/sec YDOT = 4275
054103 meter/sec
ZDOT = -8300
032950 ZDOT = -2529
850043
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 13315
99700233
00016717 00000-0 10270-3 0 9159
2 25544 51
6461 96
0260 0000998 108
7690 251
3569 15
49960654 17632
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
99700233 = yrday
fracday
Element set: 915
Inclination: 51
6461 deg
RA of node: 96
0260 deg
Eccentricity:
0000998
Arg of perigee: 108
7690 deg
Mean anomaly: 251
3569 deg
Mean motion: 15
49960654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 325
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