[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 29th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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
711 -0
6 1
1 1
1
N/A 0
3 -0
1 223
7
000/00:02:49
421 0
9 -0
0 219
9
Coasting Arc #1 (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 = 860021
84 A = 6795151
48 meter
Y = 6739702
22 meter E =
0003849
Z = 190492
02 I = 52
01559
XDOT = -4697
979510 Wp = 137
72335
YDOT = 426
946914 meter/sec RA = 81
47361 deg
ZDOT = 6031
084646 TA = 224
31438
MA = 224
34520
Ha = 226
235 n
mi
Hp = 217
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2821593
97 X = 783667
81
Y = 22111883
93 feet Y = 6748892
61 meter
Z = 624973
82 Z = 194484
25
XDOT = -15413
318603 XDOT = -4731
701258
YDOT = 1400
744470 feet/sec YDOT = 374
222723 meter/sec
ZDOT = 19787
023118 ZDOT = 6008
180899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15935322
17 X = -4857086
20
Y = 15586607
49 feet Y = 4750797
96 meter
Z = 640757
24 Z = 195302
81
XDOT = -9353
335886 XDOT = -2850
896778
YDOT = -10381
774314 feet/sec YDOT = -3164
364811 meter/sec
ZDOT = 19691
645673 ZDOT = 6002
013601
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
56401178
00016717 00000-0 10270-3 0 9003
2 25544 51
6461 81
9236 0013056 210
4911 149
5483 15
52119527 13025
Satellite: ISS
Catalog Number: 25544
Epoch time: 13028
56401178 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 81
9236 deg
Eccentricity:
0013056
Arg of perigee: 210
4911 deg
Mean anomaly: 149
5483 deg
Mean motion: 15
52119527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1302
Checksum: 282
Coasting Arc #2 (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 = -581774
39 A = 6794320
08 meter
Y = -6639611
00 meter E =
0018102
Z = -1254844
58 I = 52
00856
XDOT = 4884
230675 Wp = 185
33468
YDOT = 681
021089 meter/sec RA = 76
53647 deg
ZDOT = -5878
590625 TA = 8
24330
MA = 8
21360
Ha = 226
005 n
mi
Hp = 217
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1908708
64 X = -501390
05
Y = -21783500
66 feet Y = -6645667
36 meter
Z = -4116944
15 Z = -1257475
24
XDOT = 16024
378855 XDOT = 4904
808350
YDOT = 2234
321158 feet/sec YDOT = 735
754468 meter/sec
ZDOT = -19286
714649 ZDOT = -5854
814015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15983005
63 X = 4871620
11
Y = -14920594
37 feet Y = -4547797
16 meter
Z = -4127068
41 Z = -1257930
45
XDOT = 7112
983739 XDOT = 2168
037444
YDOT = 12917
130832 feet/sec YDOT = 3937
141478 meter/sec
ZDOT = -19187
840601 ZDOT = -5848
453815
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
52975809
00016717 00000-0 10270-3 0 9018
2 25544 51
6467 77
1234 0013094 213
6486 146
3835 15
52185032 13176
Satellite: ISS
Catalog Number: 25544
Epoch time: 13029
52975809 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 77
1234 deg
Eccentricity:
0013094
Arg of perigee: 213
6486 deg
Mean anomaly: 146
3835 deg
Mean motion: 15
52185032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1317
Checksum: 308
Coasting Arc #3 (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 = 265349
07 A = 6792852
32 meter
Y = 6401238
86 meter E =
0008061
Z = 2263920
49 I = 51
99451
XDOT = -5076
918155 Wp = 137
79869
YDOT = -1728
805636 meter/sec RA = 71
59668 deg
ZDOT = 5466
168141 TA = 247
21521
MA = 247
30039
Ha = 225
758 n
mi
Hp = 218
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 870567
83 X = 182752
03
Y = 21001439
83 feet Y = 6403744
44 meter
Z = 7427560
65 Z = 2265008
59
XDOT = -16656
555628 XDOT = -5083
761650
YDOT = -5671
934501 feet/sec YDOT = -1785
616933 meter/sec
ZDOT = 17933
622510 ZDOT = 5441
488830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15784263
71 X = -4811043
58
Y = 13878760
44 feet Y = 4230246
18 meter
Z = 7431288
45 Z = 2265056
72
XDOT = -5154
458490 XDOT = -1571
078948
YDOT = -15439
702921 feet/sec YDOT = -4706
021450 meter/sec
ZDOT = 17831
123534 ZDOT = 5434
926453
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
55987760
00016717 00000-0 10270-3 0 9023
2 25544 51
6457 72
0028 0012876 217
2606 142
7653 15
52172576 13336
Satellite: ISS
Catalog Number: 25544
Epoch time: 13030
55987760 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 72
0028 deg
Eccentricity:
0012876
Arg of perigee: 217
2606 deg
Mean anomaly: 142
7653 deg
Mean motion: 15
52172576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 303
Coasting Arc #4 (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 = 141403
35 A = 6790540
03 meter
Y = -5980702
78 meter E =
0011335
Z = -3197246
41 I = 51
97796
XDOT = 5294
168292 Wp = 200
37891
YDOT = 2711
113843 meter/sec RA = 66
65328 deg
ZDOT = -4842
403322 TA = 16
37168
MA = 16
33510
Ha = 225
527 n
mi
Hp = 218
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 463921
76 X = 223801
47
Y = -19621728
28 feet Y = -5978660
96 meter
Z = -10489653
59 Z = -3196359
07
XDOT = 17369
318543 XDOT = 5286
981321
YDOT = 8894
730456 feet/sec YDOT = 2770
276136 meter/sec
ZDOT = -15887
150005 ZDOT = -4816
702683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15358387
12 X = 4681236
40
Y = -12224593
74 feet Y = -3726056
17 meter
Z = -10485205
27 Z = -3195890
57
XDOT = 3543
462219 XDOT = 1080
047284
YDOT = 17972
394128 feet/sec YDOT = 5477
985730 meter/sec
ZDOT = -15780
527779 ZDOT = -4809
904867
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
52560070
00016717 00000-0 10270-3 0 9033
2 25544 51
6469 67
2024 0012940 220
9606 139
0575 15
52225038 13484
Satellite: ISS
Catalog Number: 25544
Epoch time: 13031
52560070 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 67
2024 deg
Eccentricity:
0012940
Arg of perigee: 220
9606 deg
Mean anomaly: 139
0575 deg
Mean motion: 15
52225038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1348
Checksum: 281
Coasting Arc #5 (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 = -609044
85 A = 6788150
15 meter
Y = 5460669
26 meter E =
0011327
Z = 3993101
65 I = 51
95581
XDOT = -5474
351593 Wp = 170
59484
YDOT = -3551
102456 meter/sec RA = 61
70474 deg
ZDOT = 4008
774021 TA = 237
69273
MA = 237
80248
Ha = 225
256 n
mi
Hp = 218
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1998178
65 X = -689459
15
Y = 17915581
57 feet Y = 5453409
09 meter
Z = 13100727
18 Z = 3989947
44
XDOT = -17960
471105 XDOT = -5453
708878
YDOT = -11650
598608 feet/sec YDOT = -3612
204502 meter/sec
ZDOT = 13152
145737 ZDOT = 3982
230691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14877286
89 X = -4534597
05
Y = 10197507
18 feet Y = 3108200
19 meter
Z = 13086902
45 Z = 3988887
87
XDOT = -2317
612431 XDOT = -706
408269
YDOT = -20171
322351 feet/sec YDOT = -6148
219053 meter/sec
ZDOT = 13042
129218 ZDOT = 3975
240986
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
55569467
00016717 00000-0 10270-3 0 9047
2 25544 51
6458 62
0816 0012778 224
5206 135
4920 15
52225370 13640
Satellite: ISS
Catalog Number: 25544
Epoch time: 13032
55569467 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 62
0816 deg
Eccentricity:
0012778
Arg of perigee: 224
5206 deg
Mean anomaly: 135
4920 deg
Mean motion: 15
52225370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 301
Coasting Arc #6 (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 = 1186722
04 A = 6785705
49 meter
Y = -4809939
58 meter E =
0005042
Z = -4634647
19 I = 51
93387
XDOT = 5612
506502 Wp = 178
47801
YDOT = 4272
703993 meter/sec RA = 56
75155 deg
ZDOT = -3002
181066 TA = 61
71810
MA = 61
66723
Ha = 225
049 n
mi
Hp = 218
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3893445
01 X = 1262933
27
Y = -15780641
67 feet Y = -4796242
92 meter
Z = -15205535
40 Z = -4628697
00
XDOT = 18413
735243 XDOT = 5578
894746
YDOT = 14018
057719 feet/sec YDOT = 4335
278543 meter/sec
ZDOT = -9849
675412 ZDOT = -2974
998010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14391650
72 X = 4386575
14
Y = -7605216
25 feet Y = -2318069
91 meter
Z = -15180149
79 Z = -4626909
66
XDOT = 1403
043065 XDOT = 427
647526
YDOT = 22057
780033 feet/sec YDOT = 6723
211354 meter/sec
ZDOT = -9737
096893 ZDOT = -2967
867133
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
52139488
00016717 00000-0 10270-3 0 9052
2 25544 51
6470 57
2815 0012849 228
3852 131
6200 15
52257727 13793
Satellite: ISS
Catalog Number: 25544
Epoch time: 13033
52139488 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 57
2815 deg
Eccentricity:
0012849
Arg of perigee: 228
3852 deg
Mean anomaly: 131
6200 deg
Mean motion: 15
52257727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1379
Checksum: 309
Coasting Arc #7 (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 = -1820423
91 A = 6783899
02 meter
Y = 4122894
76 meter E =
0012241
Z = 5078177
84 I = 51
90919
XDOT = -5655
574878 Wp = 206
27202
YDOT = -4813
345705 meter/sec RA = 51
79298 deg
ZDOT = 1871
510757 TA = 225
58935
MA = 225
68962
Ha = 224
733 n
mi
Hp = 218
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5972519
38 X = -1891059
90
Y = 13526557
63 feet Y = 4102142
75 meter
Z = 16660688
45 Z = 5069162
84
XDOT = -18555
035689 XDOT = -5610
421910
YDOT = -15791
816617 feet/sec YDOT = -4876
337409 meter/sec
ZDOT = 6140
127157 ZDOT = 1844
146432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14035213
76 X = -4277933
15
Y = 4787300
34 feet Y = 1459169
14 meter
Z = 16622629
71 Z = 5066577
54
XDOT = -789
468482 XDOT = -240
629993
YDOT = -23343
572429 feet/sec YDOT = -7115
120876 meter/sec
ZDOT = 6026
872598 ZDOT = 1836
990768
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
55146351
00016717 00000-0 10270-3 0 9064
2 25544 51
6459 52
1606 0012721 232
1800 127
8201 15
52268751 13952
Satellite: ISS
Catalog Number: 25544
Epoch time: 13034
55146351 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 52
1606 deg
Eccentricity:
0012721
Arg of perigee: 232
1800 deg
Mean anomaly: 127
8201 deg
Mean motion: 15
52268751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 280
Coasting Arc #8 (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 = 2545450
83 A = 6782852
00 meter
Y = -3373307
33 meter E =
0007171
Z = -5308456
59 I = 51
88670
XDOT = 5580
633868 Wp = 145
71728
YDOT = 5212
468674 meter/sec RA = 46
83106 deg
ZDOT = -642
541450 TA = 118
20145
MA = 118
12901
Ha = 224
530 n
mi
Hp = 219
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8351216
63 X = 2608769
47
Y = -11067281
28 feet Y = -3344488
43 meter
Z = -17416196
15 Z = -5295937
37
XDOT = 18309
166232 XDOT = 5525
053434
YDOT = 17101
275177 feet/sec YDOT = 5274
564061 meter/sec
ZDOT = -2108
075624 ZDOT = -615
566467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13837568
26 X = 4217690
81
Y = -1605280
79 feet Y = -489289
58 meter
Z = -17363645
95 Z = -5292439
29
XDOT = 310
333836 XDOT = 94
589753
YDOT = 24049
968579 feet/sec YDOT = 7330
430423 meter/sec
ZDOT = -1996
500995 ZDOT = -608
533503
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
51714036
00016717 00000-0 10270-3 0 9073
2 25544 51
6465 47
3606 0012802 236
1260 123
8675 15
52281062 14108
Satellite: ISS
Catalog Number: 25544
Epoch time: 13035
51714036 = yrday
fracday
Element set: 907
Inclination: 51
6465 deg
RA of node: 47
3606 deg
Eccentricity:
0012802
Arg of perigee: 236
1260 deg
Mean anomaly: 123
8675 deg
Mean motion: 15
52281062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 275
Coasting Arc #9 (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 = -3288649
35 A = 6782781
52 meter
Y = 2653416
91 meter E =
0009775
Z = 5312392
06 I = 51
86403
XDOT = -5358
274838 Wp = 238
09943
YDOT = -5440
393183 meter/sec RA = 41
86611 deg
ZDOT = -605
549261 TA = 217
63470
MA = 217
70313
Ha = 224
181 n
mi
Hp = 219
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10789531
99 X = -3343881
80
Y = 8705436
06 feet Y = 2616332
24 meter
Z = 17429107
82 Z = 5296282
22
XDOT = -17579
641857 XDOT = -5294
099417
YDOT = -17849
058999 feet/sec YDOT = -5499
953937 meter/sec
ZDOT = -1986
710174 ZDOT = -631
423144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13861364
14 X = -4224943
79
Y = -1551196
19 feet Y = -472804
60 meter
Z = 17361704
75 Z = 5291847
61
XDOT = 91
149347 XDOT = 27
782321
YDOT = -24032
267636 feet/sec YDOT = -7325
035175 meter/sec
ZDOT = -2093
666929 ZDOT = -638
149680
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
54718332
00016717 00000-0 10270-3 0 9081
2 25544 51
6455 42
2396 0012715 240
0878 119
9011 15
52311115 14269
Satellite: ISS
Catalog Number: 25544
Epoch time: 13036
54718332 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 42
2396 deg
Eccentricity:
0012715
Arg of perigee: 240
0878 deg
Mean anomaly: 119
9011 deg
Mean motion: 15
52311115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 284
Coasting Arc #10 (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 = 4065423
11 A = 6783821
69 meter
Y = -1936056
36 meter E =
0008825
Z = -5077396
45 I = 51
84395
XDOT = 4958
939875 Wp = 171
81463
YDOT = 5540
701059 meter/sec RA = 36
90048 deg
ZDOT = 1849
738108 TA = 116
10946
MA = 116
01862
Ha = 223
906 n
mi
Hp = 219
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13338002
32 X = 4111434
50
Y = -6351890
96 feet Y = -1890336
88 meter
Z = -16658124
84 Z = -5057535
65
XDOT = 16269
487779 XDOT = 4887
628667
YDOT = 18178
153080 feet/sec YDOT = 5595
756273 meter/sec
ZDOT = 6068
694579 ZDOT = 1873
654642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14079290
94 X = 4291367
88
Y = 4772647
09 feet Y = 1454702
83 meter
Z = -16575202
99 Z = -5052121
87
XDOT = -614
452894 XDOT = -187
285242
YDOT = 23325
041495 feet/sec YDOT = 7109
472648 meter/sec
ZDOT = 6167
489027 ZDOT = 1879
850655
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
51283632
00016717 00000-0 10270-3 0 9090
2 25544 51
6454 37
4390 0012722 244
0111 115
9731 15
52311298 14414
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
51283632 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 37
4390 deg
Eccentricity:
0012722
Arg of perigee: 244
0111 deg
Mean anomaly: 115
9731 deg
Mean motion: 15
52311298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 278
Coasting Arc #11 (Orbit 1444)
---------------------------------------
Vector Time (GMT): 2013/037/17:02:51
421
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030983
00 A = 6793151
90 meter
Y = 5018558
93 meter E =
0001828
Z = 2168847
23 I = 51
86989
XDOT = -5054
265172 Wp = 84
65115
YDOT = 1678
132185 meter/sec RA = 35
89215 deg
ZDOT = 5506
869252 TA = 299
29742
MA = 299
31569
Ha = 223
662 n
mi
Hp = 219
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13225009
83 X = 3964029
36
Y = 16465088
37 feet Y = 5063261
51 meter
Z = 7115640
53 Z = 2188266
47
XDOT = -16582
234817 XDOT = -5099
405100
YDOT = 5505
683022 feet/sec YDOT = 1621
359719 meter/sec
ZDOT = 18067
156338 ZDOT = 5482
206974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19890834
78 X = 6062726
44
Y = 7014819
84 feet Y = 2138117
09 meter
Z = 7195787
29 Z = 2193275
97
XDOT = -10751
316916 XDOT = -3277
001396
YDOT = 12045
387948 feet/sec YDOT = 3671
434246 meter/sec
ZDOT = 17964
284611 ZDOT = 5475
513950
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
77035229
00016717 00000-0 10270-3 0 9107
2 25544 51
6471 36
1591 0012103 249
0427 110
9429 15
52115664 14452
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
77035229 = yrday
fracday
Element set: 910
Inclination: 51
6471 deg
RA of node: 36
1591 deg
Eccentricity:
0012103
Arg of perigee: 249
0427 deg
Mean anomaly: 110
9429 deg
Mean motion: 15
52115664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1445
Checksum: 283
Coasting Arc #12 (Orbit 1459)
---------------------------------------
Vector Time (GMT): 2013/038/17:02:51
421
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3505010
05 A = 6791016
68 meter
Y = -4925176
87 meter E =
0008645
Z = -3082340
45 I = 51
83854
XDOT = 5788
780403 Wp = 235
87304
YDOT = -1037
431068 meter/sec RA = 30
94084 deg
ZDOT = -4919
769217 TA = 339
41794
MA = 339
45274
Ha = 223
271 n
mi
Hp = 219
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11499376
80 X = -3434702
38
Y = -16158716
78 feet Y = -4963978
96 meter
Z = -10112665
52 Z = -3099196
32
XDOT = 18992
061688 XDOT = 5823
849254
YDOT = -3403
645236 feet/sec YDOT = -972
501173 meter/sec
ZDOT = -16140
975121 ZDOT = -4891
563375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18377688
37 X = -5601519
41
Y = -7361390
66 feet Y = -2243751
87 meter
Z = -10182155
78 Z = -3103521
08
XDOT = 13647
279598 XDOT = 4159
690821
YDOT = -11883
929481 feet/sec YDOT = -3622
221706 meter/sec
ZDOT = -16023
439030 ZDOT = -4883
944216
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 13038
73612378
00016717 00000-0 10270-3 0 9111
2 25544 51
6479 31
3593 0012098 252
7168 107
2660 15
52147654 14602
Satellite: ISS
Catalog Number: 25544
Epoch time: 13038
73612378 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 31
3593 deg
Eccentricity:
0012098
Arg of perigee: 252
7168 deg
Mean anomaly: 107
2660 deg
Mean motion: 15
52147654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1460
Checksum: 307
Coasting Arc #13 (Orbit 1475)
---------------------------------------
Vector Time (GMT): 2013/039/17:02:51
421
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2845458
88 A = 6788636
43 meter
Y = 4787893
39 meter E =
0004665
Z = 3885668
30 I = 51
80364
XDOT = -6436
550431 Wp = 187
68141
YDOT = 473
997469 meter/sec RA = 25
98330 deg
ZDOT = 4125
467910 TA = 219
04169
MA = 219
07537
Ha = 222
968 n
mi
Hp = 219
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9335495
01 X = 2772833
17
Y = 15708311
64 feet Y = 4819307
07 meter
Z = 12748255
59 Z = 3899314
44
XDOT = -21117
291440 XDOT = -6461
412236
YDOT = 1555
109806 feet/sec YDOT = 401
880963 meter/sec
ZDOT = 13534
999705 ZDOT = 4094
140219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16440515
33 X = 5011069
07
Y = 7885251
41 feet Y = 2403424
63 meter
Z = 12804405
81 Z = 3902782
89
XDOT = -16161
036839 XDOT = -4925
884028
YDOT = 11907
539584 feet/sec YDOT = 3629
418065 meter/sec
ZDOT = 13404
546016 ZDOT = 4085
705626
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 13039
76626774
00016717 00000-0 10270-3 0 9121
2 25544 51
6475 26
2388 0012048 256
4901 103
4909 15
52155181 14769
Satellite: ISS
Catalog Number: 25544
Epoch time: 13039
76626774 = yrday
fracday
Element set: 912
Inclination: 51
6475 deg
RA of node: 26
2388 deg
Eccentricity:
0012048
Arg of perigee: 256
4901 deg
Mean anomaly: 103
4909 deg
Mean motion: 15
52155181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1476
Checksum: 314
Coasting Arc #14 (Orbit 1490)
---------------------------------------
Vector Time (GMT): 2013/040/17:02:51
421
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2054147
53 A = 6786197
25 meter
Y = -4613624
37 meter E =
0003017
Z = -4531322
27 I = 51
76890
XDOT = 6979
542337 Wp = 296
69285
YDOT = 7
656508 meter/sec RA = 21
02029 deg
ZDOT = -3168
823975 TA = 301
53804
MA = 301
56751
Ha = 222
549 n
mi
Hp = 219
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6739329
15 X = -1980393
03
Y = -15136562
90 feet Y = -4636182
92 meter
Z = -14866542
88 Z = -4541121
53
XDOT = 22898
760949 XDOT = 6994
330830
YDOT = 25
119777 feet/sec YDOT = 85
788704 meter/sec
ZDOT = -10396
404119 ZDOT = -3134
883057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14105926
21 X = -4299486
31
Y = -8623290
56 feet Y = -2628378
96 meter
Z = -14906706
43 Z = -4543564
12
XDOT = 18228
502454 XDOT = 5556
047548
YDOT = -12073
767063 feet/sec YDOT = -3680
084201 meter/sec
ZDOT = -10255
141406 ZDOT = -3125
767101
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 13040
73201409
00016717 00000-0 10270-3 0 9135
2 25544 51
6484 21
4388 0012065 260
4018 99
5770 15
52201904 14912
Satellite: ISS
Catalog Number: 25544
Epoch time: 13040
73201409 = yrday
fracday
Element set: 913
Inclination: 51
6484 deg
RA of node: 21
4388 deg
Eccentricity:
0012065
Arg of perigee: 260
4018 deg
Mean anomaly: 99
5770 deg
Mean motion: 15
52201904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1491
Checksum: 281
Coasting Arc #15 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2013/041/17:02:51
421
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1160278
94 A = 6784319
45 meter
Y = 4440731
79 meter E =
0008397
Z = 5003580
56 I = 51
73380
XDOT = -7360
973993 Wp = 236
26176
YDOT = -415
674411 meter/sec RA = 16
05115 deg
ZDOT = 2073
802956 TA = 193
55297
MA = 193
57553
Ha = 222
313 n
mi
Hp = 219
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3806689
43 X = 1086230
13
Y = 14569330
04 feet Y = 4453293
03 meter
Z = 16415946
70 Z = 5009036
81
XDOT = -24150
177142 XDOT = -7365
852449
YDOT = -1363
761191 feet/sec YDOT = -498
016598 meter/sec
ZDOT = 6803
815472 ZDOT = 2038
033171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11535020
68 X = 3515874
30
Y = 9642255
50 feet Y = 2938959
48 meter
Z = 16438058
73 Z = 5010320
30
XDOT = -19706
485556 XDOT = -6006
536798
YDOT = 12218
010099 feet/sec YDOT = 3724
049478 meter/sec
ZDOT = 6655
001439 ZDOT = 2028
444439
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 13041
76213103
00016717 00000-0 10270-3 0 9144
2 25544 51
6485 16
3182 0012075 263
9468 96
0308 15
52206196 15071
Satellite: ISS
Catalog Number: 25544
Epoch time: 13041
76213103 = yrday
fracday
Element set: 914
Inclination: 51
6485 deg
RA of node: 16
3182 deg
Eccentricity:
0012075
Arg of perigee: 263
9468 deg
Mean anomaly: 96
0308 deg
Mean motion: 15
52206196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 289
Coasting Arc #16 (Orbit 1521)
---------------------------------------
Vector Time (GMT): 2013/042/17:02:51
421
Vector Time (MET): N/A
Weight (LBS) : 903039
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -187438
01 A = 6783061
57 meter
Y = -4274193
10 meter E =
0002598
Z = -5265797
63 I = 51
70090
XDOT = 7573
329471 Wp = 62
16795
YDOT = 766
095397 meter/sec RA = 11
07755 deg
ZDOT = -890
558625 TA = 199
31214
MA = 199
32199
Ha = 222
091 n
mi
Hp = 219
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -614954
11 X = -114049
95
Y = -14022943
25 feet Y = -4275879
24 meter
Z = -17276238
94 Z = -5266529
57
XDOT = 24846
881467 XDOT = 7568
525954
YDOT = 2513
436341 feet/sec YDOT = 850
758196 meter/sec
ZDOT = -2921
780266 ZDOT = -853
780695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8812616
71 X = -2686085
57
Y = -10921236
98 feet Y = -3328793
03 meter
Z = -17278712
55 Z = -5266551
59
XDOT = 20613
345425 XDOT = 6282
947685
YDOT = -12248
399777 feet/sec YDOT = -3733
312252 meter/sec
ZDOT = -2768
825650 ZDOT = -843
938058
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 13042
72785237
00016717 00000-0 10270-3 0 9154
2 25544 51
6491 11
5181 0012108 267
9382 92
0383 15
52248318 15228
Satellite: ISS
Catalog Number: 25544
Epoch time: 13042
72785237 = yrday
fracday
Element set: 915
Inclination: 51
6491 deg
RA of node: 11
5181 deg
Eccentricity:
0012108
Arg of perigee: 267
9382 deg
Mean anomaly: 92
0383 deg
Mean motion: 15
52248318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1522
Checksum: 296
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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