[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 24th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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
037/17:01:26
716 -0
6 1
1 1
1
N/A 0
3 -0
1 223
6
000/00:02:49
432 0
9 -0
0 219
9
Coasting Arc #1 (Orbit 1223)
---------------------------------------
Vector Time (GMT): 2013/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2143740
34 A = 6787410
87 meter
Y = -4757711
67 meter E =
0012124
Z = 4328298
50 I = 51
97983
XDOT = 4391
905201 Wp = 148
13628
YDOT = -5197
486875 meter/sec RA = 106
17277 deg
ZDOT = -3543
403990 TA = 337
73077
MA = 337
78337
Ha = 227
356 n
mi
Hp = 216
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7033268
84 X = -2111404
67
Y = -15609290
25 feet Y = -4781503
76 meter
Z = 14200454
41 Z = 4317962
83
XDOT = 14409
137800 XDOT = 4466
910824
YDOT = -17052
122292 feet/sec YDOT = -5147
954257 meter/sec
ZDOT = -11625
341173 ZDOT = -3521
886936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9419211
44 X = 2870975
65
Y = -14338712
58 feet Y = -4370439
59 meter
Z = 14158018
78 Z = 4315364
12
XDOT = 21099
452976 XDOT = 6431
113267
YDOT = 2488
483596 feet/sec YDOT = 758
489800 meter/sec
ZDOT = -11535
194402 ZDOT = -3515
927254
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 13023
54190042
00016717 00000-0 10270-3 0 9001
2 25544 51
6486 106
8772 0013559 192
2668 167
8155 15
52073319 12248
Satellite: ISS
Catalog Number: 25544
Epoch time: 13023
54190042 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 106
8772 deg
Eccentricity:
0013559
Arg of perigee: 192
2668 deg
Mean anomaly: 167
8155 deg
Mean motion: 15
52073319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1224
Checksum: 303
Coasting Arc #2 (Orbit 1238)
---------------------------------------
Vector Time (GMT): 2013/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1824773
45 A = 6789680
90 meter
Y = 5439173
29 meter E =
0013986
Z = -3645531
02 I = 51
99461
XDOT = -4398
793507 Wp = 172
94524
YDOT = 4442
445825 meter/sec RA = 101
22598 deg
ZDOT = 4414
660260 TA = 144
16085
MA = 144
06693
Ha = 227
104 n
mi
Hp = 216
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5986789
54 X = 1781524
53
Y = 17845056
73 feet Y = 5459337
42 meter
Z = -11960403
62 Z = -3636771
36
XDOT = -14431
737229 XDOT = -4469
587785
YDOT = 14574
953493 feet/sec YDOT = 4392
859695 meter/sec
ZDOT = 14483
793505 ZDOT = 4393
119981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11622892
91 X = -3542657
76
Y = 14834116
05 feet Y = 4521438
57 meter
Z = -11924609
62 Z = -3634621
01
XDOT = -19063
121245 XDOT = -5810
439356
YDOT = -3334
957426 feet/sec YDOT = -1016
495023 meter/sec
ZDOT = 14393
627517 ZDOT = 4387
177667
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 13024
50771420
00016717 00000-0 10270-3 0 9014
2 25544 51
6480 102
0783 0013568 195
5937 164
4798 15
52093000 12398
Satellite: ISS
Catalog Number: 25544
Epoch time: 13024
50771420 = yrday
fracday
Element set: 901
Inclination: 51
6480 deg
RA of node: 102
0783 deg
Eccentricity:
0013568
Arg of perigee: 195
5937 deg
Mean anomaly: 164
4798 deg
Mean motion: 15
52093000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1239
Checksum: 296
Coasting Arc #3 (Orbit 1254)
---------------------------------------
Vector Time (GMT): 2013/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1556708
37 A = 6791843
70 meter
Y = -5967427
82 meter E =
0017270
Z = 2817173
10 I = 52
00731
XDOT = 4432
724402 Wp = 149
67517
YDOT = -3582
101561 meter/sec RA = 96
28308 deg
ZDOT = -5139
127474 TA = 358
50629
MA = 358
51144
Ha = 226
884 n
mi
Hp = 217
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5107310
92 X = -1503548
41
Y = -19578175
28 feet Y = -5984538
79 meter
Z = 9242693
91 Z = 2809739
79
XDOT = 14543
059063 XDOT = 4497
414735
YDOT = -11752
301710 feet/sec YDOT = -3532
170143 meter/sec
ZDOT = -16860
654442 ZDOT = -5117
437171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13303544
07 X = 4054920
23
Y = -15263118
46 feet Y = -4652198
51 meter
Z = 9212485
69 Z = 2807965
64
XDOT = 16835
628241 XDOT = 5131
499488
YDOT = 4553
833311 feet/sec YDOT = 1388
008393 meter/sec
ZDOT = -16769
957606 ZDOT = -5111
483078
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 13025
53790019
00016717 00000-0 10270-3 0 9024
2 25544 51
6483 96
9591 0013346 199
5849 160
4792 15
52116675 12551
Satellite: ISS
Catalog Number: 25544
Epoch time: 13025
53790019 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 96
9591 deg
Eccentricity:
0013346
Arg of perigee: 199
5849 deg
Mean anomaly: 160
4792 deg
Mean motion: 15
52116675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1255
Checksum: 329
Coasting Arc #4 (Orbit 1269)
---------------------------------------
Vector Time (GMT): 2013/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1316705
31 A = 6793749
99 meter
Y = 6399197
92 meter E =
0006678
Z = -1877893
77 I = 52
01519
XDOT = -4473
778100 Wp = 186
56898
YDOT = 2581
107800 meter/sec RA = 91
34340 deg
ZDOT = 5650
233837 TA = 152
91345
MA = 152
87859
Ha = 226
657 n
mi
Hp = 217
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4319899
31 X = 1254172
35
Y = 20994743
84 feet Y = 6413572
55 meter
Z = -6161068
79 Z = -1871649
21
XDOT = -14677
749671 XDOT = -4529
754765
YDOT = 8468
201442 feet/sec YDOT = 2530
766090 meter/sec
ZDOT = 18537
512590 ZDOT = 5628
365228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14661752
30 X = -4468902
10
Y = 15645567
17 feet Y = 4768768
87 meter
Z = -6135863
04 Z = -1870211
05
XDOT = -14297
854933 XDOT = -4357
986184
YDOT = -6153
685360 feet/sec YDOT = -1875
643298 meter/sec
ZDOT = 18446
187569 ZDOT = 5622
397971
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 13026
50368586
00016717 00000-0 10270-3 0 9033
2 25544 51
6475 92
1595 0013271 203
3494 156
7057 15
52099308 12703
Satellite: ISS
Catalog Number: 25544
Epoch time: 13026
50368586 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 92
1595 deg
Eccentricity:
0013271
Arg of perigee: 203
3494 deg
Mean anomaly: 156
7057 deg
Mean motion: 15
52099308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1270
Checksum: 310
Coasting Arc #5 (Orbit 1285)
---------------------------------------
Vector Time (GMT): 2013/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1084769
68 A = 6794770
50 meter
Y = -6639111
51 meter E =
0020203
Z = 853661
35 I = 52
01906
XDOT = 4576
100157 Wp = 165
75397
YDOT = -1516
893835 meter/sec RA = 86
40634 deg
ZDOT = -5971
414267 TA = 5
05578
MA = 5
03541
Ha = 226
406 n
mi
Hp = 217
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3558955
65 X = -1014595
86
Y = -21781861
92 feet Y = -6650849
73 meter
Z = 2800726
21 Z = 848562
19
XDOT = 15013
451959 XDOT = 4621
729103
YDOT = -4976
685809 feet/sec YDOT = -1465
465871 meter/sec
ZDOT = -19591
254156 ZDOT = -5949
073691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15487217
16 X = 4720503
79
Y = -15728180
69 feet Y = -4793949
48 meter
Z = 2780319
79 Z = 847441
47
XDOT = 11795
111028 XDOT = 3595
149841
YDOT = 8161
337248 feet/sec YDOT = 2487
575593 meter/sec
ZDOT = -19498
089657 ZDOT = -5943
017728
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 13027
53384235
00016717 00000-0 10270-3 0 9047
2 25544 51
6477 87
0399 0013131 206
7057 153
3420 15
52157121 12869
Satellite: ISS
Catalog Number: 25544
Epoch time: 13027
53384235 = yrday
fracday
Element set: 904
Inclination: 51
6477 deg
RA of node: 87
0399 deg
Eccentricity:
0013131
Arg of perigee: 206
7057 deg
Mean anomaly: 153
3420 deg
Mean motion: 15
52157121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1286
Checksum: 290
Coasting Arc #6 (Orbit 1301)
---------------------------------------
Vector Time (GMT): 2013/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 849763
75 A = 6795133
63 meter
Y = 6740494
38 meter E =
0003809
Z = 204214
62 I = 52
01636
XDOT = -4700
411828 Wp = 135
71916
YDOT = 407
732028 meter/sec RA = 81
46982 deg
ZDOT = 6030
658299 TA = 226
46545
MA = 226
49710
Ha = 226
182 n
mi
Hp = 217
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2787938
81 X = 773334
96
Y = 22114482
89 feet Y = 6749569
64 meter
Z = 669995
46 Z = 208156
83
XDOT = -15421
298649 XDOT = -4733
916460
YDOT = 1337
703505 feet/sec YDOT = 354
981851 meter/sec
ZDOT = 19785
624341 ZDOT = 6007
743264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15957867
37 X = -4863957
97
Y = 15561115
39 feet Y = 4743027
97 meter
Z = 685570
61 Z = 208961
92
XDOT = -9309
725852 XDOT = -2837
604440
YDOT = -10424
518270 feet/sec YDOT = -3177
393169 meter/sec
ZDOT = 19690
202286 ZDOT = 6001
573657
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 13028
56398523
00016717 00000-0 10270-3 0 9057
2 25544 51
6470 81
9197 0012930 210
6410 149
3988 15
52124895 13029
Satellite: ISS
Catalog Number: 25544
Epoch time: 13028
56398523 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 81
9197 deg
Eccentricity:
0012930
Arg of perigee: 210
6410 deg
Mean anomaly: 149
3988 deg
Mean motion: 15
52124895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1302
Checksum: 310
Coasting Arc #7 (Orbit 1316)
---------------------------------------
Vector Time (GMT): 2013/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -569198
91 A = 6794278
25 meter
Y = -6637786
04 meter E =
0017944
Z = -1270543
02 I = 52
00928
XDOT = 4886
105828 Wp = 185
34199
YDOT = 703
353940 meter/sec RA = 76
53273 deg
ZDOT = -5874
268278 TA = 8
40889
MA = 8
37886
Ha = 225
948 n
mi
Hp = 217
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1867450
48 X = -488759
65
Y = -21777513
25 feet Y = -6643701
46 meter
Z = -4168448
23 Z = -1273112
46
XDOT = 16030
530932 XDOT = 4906
412637
YDOT = 2307
591667 feet/sec YDOT = 758
106774 meter/sec
ZDOT = -19272
533719 ZDOT = -5850
483218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16003943
28 X = 4878001
91
Y = -14884182
03 feet Y = -4536698
68 meter
Z = -4178317
90 Z = -1273551
30
XDOT = 7061
712261 XDOT = 2152
409897
YDOT = 12965
578085 feet/sec YDOT = 3951
908200 meter/sec
ZDOT = -19173
627274 ZDOT = -5844
121593
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 13029
52972717
00016717 00000-0 10270-3 0 9068
2 25544 51
6476 77
1194 0012966 213
7876 146
2451 15
52193591 13174
Satellite: ISS
Catalog Number: 25544
Epoch time: 13029
52972717 = yrday
fracday
Element set: 906
Inclination: 51
6476 deg
RA of node: 77
1194 deg
Eccentricity:
0012966
Arg of perigee: 213
7876 deg
Mean anomaly: 146
2451 deg
Mean motion: 15
52193591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1317
Checksum: 326
Coasting Arc #8 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2013/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 249414
03 A = 6792784
22 meter
Y = 6395479
60 meter E =
0008061
Z = 2281512
09 I = 51
99518
XDOT = -5078
094857 Wp = 137
16141
YDOT = -1754
757197 meter/sec RA = 71
59293 deg
ZDOT = 5456
969727 TA = 248
06072
MA = 248
14642
Ha = 225
696 n
mi
Hp = 218
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 818287
50 X = 166797
12
Y = 20982544
62 feet Y = 6397806
87 meter
Z = 7485275
89 Z = 2282522
74
XDOT = -16660
416198 XDOT = -5084
603386
YDOT = -5757
077419 feet/sec YDOT = -1811
579780 meter/sec
ZDOT = 17903
443987 ZDOT = 5432
285514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15802776
13 X = -4816686
16
Y = 13825991
34 feet Y = 4214162
16 meter
Z = 7488682
02 Z = 2282550
28
XDOT = -5094
523234 XDOT = -1552
810682
YDOT = -15494
876273 feet/sec YDOT = -4722
838288 meter/sec
ZDOT = 17800
927860 ZDOT = 5425
722812
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 13030
55983994
00016717 00000-0 10270-3 0 9073
2 25544 51
6466 71
9989 0012746 217
3839 142
6427 15
52184434 13339
Satellite: ISS
Catalog Number: 25544
Epoch time: 13030
55983994 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 71
9989 deg
Eccentricity:
0012746
Arg of perigee: 217
3839 deg
Mean anomaly: 142
6427 deg
Mean motion: 15
52184434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 336
Coasting Arc #9 (Orbit 1347)
---------------------------------------
Vector Time (GMT): 2013/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 161921
85 A = 6790444
86 meter
Y = -5969954
85 meter E =
0011123
Z = -3216423
96 I = 51
97857
XDOT = 5293
461085 Wp = 200
25970
YDOT = 2740
965052 meter/sec RA = 66
64947 deg
ZDOT = -4826
156951 TA = 16
74723
MA = 16
71053
Ha = 225
461 n
mi
Hp = 218
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 531239
67 X = 244291
41
Y = -19586466
05 feet Y = -5967683
74 meter
Z = -10552572
04 Z = -3215437
01
XDOT = 17366
998309 XDOT = 5285
861445
YDOT = 8992
667495 feet/sec YDOT = 2800
117131 meter/sec
ZDOT = -15833
848264 ZDOT = -4800
460752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15374976
80 X = 4686292
93
Y = -12150083
78 feet Y = -3703345
54 meter
Z = -10547710
52 Z = -3214942
17
XDOT = 3472
231142 XDOT = 1058
336052
YDOT = 18032
192453 feet/sec YDOT = 5496
212260 meter/sec
ZDOT = -15727
248288 ZDOT = -4793
665278
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 13031
52555478
00016717 00000-0 10270-3 0 9084
2 25544 51
6478 67
1986 0012808 221
0757 138
9431 15
52239933 13480
Satellite: ISS
Catalog Number: 25544
Epoch time: 13031
52555478 = yrday
fracday
Element set: 908
Inclination: 51
6478 deg
RA of node: 67
1986 deg
Eccentricity:
0012808
Arg of perigee: 221
0757 deg
Mean anomaly: 138
9431 deg
Mean motion: 15
52239933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1348
Checksum: 328
Coasting Arc #10 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2013/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -635311
52 A = 6788031
79 meter
Y = 5443178
63 meter E =
0011279
Z = 4012539
69 I = 51
95638
XDOT = -5470
771434 Wp = 170
53935
YDOT = -3584
590252 meter/sec RA = 61
70079 deg
ZDOT = 3984
036313 TA = 238
06329
MA = 238
17302
Ha = 225
187 n
mi
Hp = 218
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2084355
38 X = -715622
70
Y = 17858197
62 feet Y = 5435625
31 meter
Z = 13164500
29 Z = 4009258
14
XDOT = -17948
725176 XDOT = -5449
634349
YDOT = -11760
466706 feet/sec YDOT = -3645
649499 meter/sec
ZDOT = 13070
985279 ZDOT = 3957
511577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14890859
49 X = -4538733
97
Y = 10094540
34 feet Y = 3076815
90 meter
Z = 13150147
78 Z = 4008165
04
XDOT = -2234
215489 XDOT = -680
988881
YDOT = -20233
248625 feet/sec YDOT = -6167
094181 meter/sec
ZDOT = 12961
050429 ZDOT = 3950
528171
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 13032
55563783
00016717 00000-0 10270-3 0 9097
2 25544 51
6467 62
0778 0012644 224
6201 135
3933 15
52243534 13640
Satellite: ISS
Catalog Number: 25544
Epoch time: 13032
55563783 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 62
0778 deg
Eccentricity:
0012644
Arg of perigee: 224
6201 deg
Mean anomaly: 135
3933 deg
Mean motion: 15
52243534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 301
Coasting Arc #11 (Orbit 1378)
---------------------------------------
Vector Time (GMT): 2013/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1219714
92 A = 6785575
63 meter
Y = -4784485
75 meter E =
0004930
Z = -4652461
27 I = 51
93443
XDOT = 5603
574934 Wp = 176
18354
YDOT = 4308
707797 meter/sec RA = 56
74741 deg
ZDOT = -2966
881701 TA = 64
39786
MA = 64
34693
Ha = 224
977 n
mi
Hp = 218
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4001689
37 X = 1295725
61
Y = -15697131
72 feet Y = -4770421
27 meter
Z = -15263980
55 Z = -4646351
29
XDOT = 18384
432199 XDOT = 5569
389767
YDOT = 14136
180437 feet/sec YDOT = 4371
179264 meter/sec
ZDOT = -9733
863847 ZDOT = -2939
743427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14402339
76 X = 4389833
16
Y = -7468638
77 feet Y = -2276441
10 meter
Z = -15237933
22 Z = -4644522
05
XDOT = 1305
161642 XDOT = 397
813268
YDOT = 22113
800374 feet/sec YDOT = 6740
286354 meter/sec
ZDOT = -9621
476366 ZDOT = -2932
625996
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 13033
52132585
00016717 00000-0 10270-3 0 9109
2 25544 51
6479 57
2777 0012714 228
4761 131
5300 15
52278632 13798
Satellite: ISS
Catalog Number: 25544
Epoch time: 13033
52132585 = yrday
fracday
Element set: 910
Inclination: 51
6479 deg
RA of node: 57
2777 deg
Eccentricity:
0012714
Arg of perigee: 228
4761 deg
Mean anomaly: 131
5300 deg
Mean motion: 15
52278632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1379
Checksum: 301
Coasting Arc #12 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2013/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1860896
99 A = 6783770
52 meter
Y = 4087937
69 meter E =
0012113
Z = 5091480
00 I = 51
90980
XDOT = -5639
068372 Wp = 206
61008
YDOT = -4850
763412 meter/sec RA = 51
78860 deg
ZDOT = 1824
766529 TA = 225
71903
MA = 225
81847
Ha = 224
658 n
mi
Hp = 218
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6105305
08 X = -1931203
70
Y = 13411869
05 feet Y = 4066734
91 meter
Z = 16704330
72 Z = 5082269
20
XDOT = -18500
880486 XDOT = -5593
271149
YDOT = -15914
578124 feet/sec YDOT = -4913
566928 meter/sec
ZDOT = 5986
766827 ZDOT = 1797
483955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14042134
04 X = -4280042
46
Y = 4611779
12 feet Y = 1405670
28 meter
Z = 16665461
62 Z = 5079632
70
XDOT = -674
914052 XDOT = -205
713803
YDOT = -23386
541560 feet/sec YDOT = -7128
217868 meter/sec
ZDOT = 5873
857413 ZDOT = 1790
351740
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 13034
55137934
00016717 00000-0 10270-3 0 9117
2 25544 51
6468 52
1568 0012584 232
2560 127
7452 15
52293363 13954
Satellite: ISS
Catalog Number: 25544
Epoch time: 13034
55137934 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 52
1568 deg
Eccentricity:
0012584
Arg of perigee: 232
2560 deg
Mean anomaly: 127
7452 deg
Mean motion: 15
52293363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 305
Coasting Arc #13 (Orbit 1409)
---------------------------------------
Vector Time (GMT): 2013/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2593323
80 A = 6782750
04 meter
Y = -3328181
81 meter E =
0007274
Z = -5313816
87 I = 51
88743
XDOT = 5552
636860 Wp = 144
83545
YDOT = 5248
989242 meter/sec RA = 46
82643 deg
ZDOT = -583
891126 TA = 119
64352
MA = 119
57105
Ha = 224
451 n
mi
Hp = 219
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8508280
18 X = 2656160
31
Y = -10919231
66 feet Y = -3298830
25 meter
Z = -17433782
37 Z = -5301066
26
XDOT = 18217
312532 XDOT = 5496
365222
YDOT = 17221
093315 feet/sec YDOT = 5310
767684 meter/sec
ZDOT = -1915
653300 ZDOT = -557
053827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13840262
94 X = 4218512
15
Y = -1389380
04 feet Y = -423483
04 meter
Z = -17380275
15 Z = -5297507
86
XDOT = 175
249846 XDOT = 53
416153
YDOT = 24066
098248 feet/sec YDOT = 7335
346746 meter/sec
ZDOT = -1804
656542 ZDOT = -550
059314
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 13035
51704002
00016717 00000-0 10270-3 0 9121
2 25544 51
6474 47
3568 0012665 236
1980 123
7967 15
52308339 14101
Satellite: ISS
Catalog Number: 25544
Epoch time: 13035
51704002 = yrday
fracday
Element set: 912
Inclination: 51
6474 deg
RA of node: 47
3568 deg
Eccentricity:
0012665
Arg of perigee: 236
1980 deg
Mean anomaly: 123
7967 deg
Mean motion: 15
52308339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 296
Coasting Arc #14 (Orbit 1425)
---------------------------------------
Vector Time (GMT): 2013/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3343336
64 A = 6782720
84 meter
Y = 2597283
01 meter E =
0009516
Z = 5305726
47 I = 51
86494
XDOT = -5315
343964 Wp = 238
63247
YDOT = -5474
482479 meter/sec RA = 41
86126 deg
ZDOT = -675
219995 TA = 217
76855
MA = 217
83537
Ha = 224
101 n
mi
Hp = 219
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10968952
22 X = -3397904
94
Y = 8521269
71 feet Y = 2559590
50 meter
Z = 17407239
09 Z = 5289352
58
XDOT = -17438
792532 XDOT = -5250
452103
YDOT = -17960
900523 feet/sec YDOT = -5533
559146 meter/sec
ZDOT = -2215
288699 ZDOT = -700
883588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13857860
43 X = -4223875
86
Y = -1808193
58 feet Y = -551137
40 meter
Z = 17338744
57 Z = 5284849
35
XDOT = 252
089178 XDOT = 76
836782
YDOT = -24010
995283 feet/sec YDOT = -7318
551362 meter/sec
ZDOT = -2321
365666 ZDOT = -707
552255
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 13036
54706355
00016717 00000-0 10270-3 0 9139
2 25544 51
6464 42
2358 0012576 240
1407 119
8495 15
52342300 14266
Satellite: ISS
Catalog Number: 25544
Epoch time: 13036
54706355 = yrday
fracday
Element set: 913
Inclination: 51
6464 deg
RA of node: 42
2358 deg
Eccentricity:
0012576
Arg of perigee: 240
1407 deg
Mean anomaly: 119
8495 deg
Mean motion: 15
52342300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 289
Coasting Arc #15 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2013/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4124739
81 A = 6783821
00 meter
Y = -1869171
89 meter E =
0008822
Z = -5054618
29 I = 51
84509
XDOT = 4896
353772 Wp = 172
17480
YDOT = 5569
596171 meter/sec RA = 36
89551 deg
ZDOT = 1927
859090 TA = 116
53123
MA = 116
44076
Ha = 223
818 n
mi
Hp = 219
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13532610
91 X = 4169888
22
Y = -6132453
70 feet Y = -1822793
91 meter
Z = -16583393
35 Z = -5034471
44
XDOT = 16064
152795 XDOT = 4824
344621
YDOT = 18272
953316 feet/sec YDOT = 5623
947604 meter/sec
ZDOT = 6324
997013 ZDOT = 1951
469897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14066380
00 X = 4287432
63
Y = 5065359
45 feet Y = 1543921
56 meter
Z = -16499289
95 Z = -5028983
58
XDOT = -807
779446 XDOT = -246
211175
YDOT = 23250
363339 feet/sec YDOT = 7086
710746 meter/sec
ZDOT = 6422
515117 ZDOT = 1957
582608
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 13037
51269632
00016717 00000-0 10270-3 0 9140
2 25544 51
6463 37
4351 0012580 244
0549 115
9307 15
52345396 14413
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
51269632 = yrday
fracday
Element set: 914
Inclination: 51
6463 deg
RA of node: 37
4351 deg
Eccentricity:
0012580
Arg of perigee: 244
0549 deg
Mean anomaly: 115
9307 deg
Mean motion: 15
52345396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 297
Coasting Arc #16 (Orbit 1444)
---------------------------------------
Vector Time (GMT): 2013/037/17:02:51
432
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3967680
79 A = 6792921
59 meter
Y = 5038607
75 meter E =
0002004
Z = 2237395
95 I = 51
87028
XDOT = -5117
848507 Wp = 89
87433
YDOT = 1598
413219 meter/sec RA = 35
88817 deg
ZDOT = 5471
875773 TA = 294
88172
MA = 294
90255
Ha = 223
578 n
mi
Hp = 219
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13017325
41 X = 3900174
67
Y = 16530865
31 feet Y = 5082599
35 meter
Z = 7340537
89 Z = 2256506
33
XDOT = -16790
841559 XDOT = -5161
922289
YDOT = 5244
137856 feet/sec YDOT = 1540
935685 meter/sec
ZDOT = 17952
348335 ZDOT = 5446
907207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19748106
29 X = 6019222
80
Y = 7181129
35 feet Y = 2188808
23 meter
Z = 7419396
48 Z = 2261432
05
XDOT = -11053
883774 XDOT = -3369
223774
YDOT = 11943
593141 feet/sec YDOT = 3640
407189 meter/sec
ZDOT = 17848
212580 ZDOT = 5440
135195
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 13037
77020654
00016717 00000-0 10270-3 0 9158
2 25544 51
6480 36
1552 0011953 249
0799 110
9073 15
52150702 14450
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
77020654 = yrday
fracday
Element set: 915
Inclination: 51
6480 deg
RA of node: 36
1552 deg
Eccentricity:
0011953
Arg of perigee: 249
0799 deg
Mean anomaly: 110
9073 deg
Mean motion: 15
52150702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1445
Checksum: 292
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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