[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 28th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
118/10:08:56
224 2
9 4
8 4
8
N/A 1
7 -0
5 225
2
000/00:11:52
447 3
4 -0
0 219
9
128/06:37:00
569 3
1 4
1 4
1
N/A -0
9 -0
0 223
7
000/00:10:01
137 2
5 0
0 222
6
Coasting Arc #1 (Orbit 2669)
---------------------------------------
Vector Time (GMT): 2013/116/13:47:10
108
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2402269
94 A = 6783896
51 meter
Y = 4040392
80 meter E =
0013845
Z = 4892346
43 I = 51
66055
XDOT = -7160
247663 Wp = 161
17582
YDOT = 1384
833335 meter/sec RA = 3
86633 deg
ZDOT = 2357
515586 TA = 265
65628
MA = 265
81449
Ha = 225
467 n
mi
Hp = 216
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7881463
07 X = 2333144
61
Y = 13255881
89 feet Y = 4066870
06 meter
Z = 16051005
34 Z = 4903848
75
XDOT = -23491
626190 XDOT = -7186
653434
YDOT = 4543
416453 feet/sec YDOT = 1304
615324 meter/sec
ZDOT = 7734
631187 ZDOT = 2322
666780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15369540
04 X = 4684635
80
Y = -299816
19 feet Y = -91383
98 meter
Z = 16098384
60 Z = 4906787
63
XDOT = -7577
332403 XDOT = -2309
570916
YDOT = 21631
020253 feet/sec YDOT = 6593
134973 meter/sec
ZDOT = 7589
125305 ZDOT = 2313
165393
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 13116
62675434
00016717 00000-0 10270-3 0 9006
2 25544 51
6474 4
1199 0009746 188
1857 171
9137 15
52494142 26708
Satellite: ISS
Catalog Number: 25544
Epoch time: 13116
62675434 = yrday
fracday
Element set: 900
Inclination: 51
6474 deg
RA of node: 4
1199 deg
Eccentricity:
0009746
Arg of perigee: 188
1857 deg
Mean anomaly: 171
9137 deg
Mean motion: 15
52494142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2670
Checksum: 318
Coasting Arc #2 (Orbit 2684)
---------------------------------------
Vector Time (GMT): 2013/117/13:47:10
108
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1271688
98 A = 6782286
50 meter
Y = -4125727
66 meter E =
0014256
Z = -5240066
53 I = 51
62352
XDOT = 7520
271534 Wp = 121
71901
YDOT = -985
215116 meter/sec RA = 358
88347 deg
ZDOT = -1058
803021 TA = 138
17752
MA = 138
06850
Ha = 225
263 n
mi
Hp = 216
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4172207
94 X = -1200004
34
Y = -13535851
91 feet Y = -4139547
62 meter
Z = -17191819
31 Z = -5246070
33
XDOT = 24672
806870 XDOT = 7535
872978
YDOT = -3232
333058 feet/sec YDOT = -901
031457 meter/sec
ZDOT = -3473
763191 ZDOT = -1022
231571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13846226
68 X = -4220329
89
Y = -2840395
77 feet Y = -865752
63 meter
Z = -17216254
41 Z = -5247514
35
XDOT = 8658
097049 XDOT = 2638
987980
YDOT = -22263
484568 feet/sec YDOT = -6785
910096 meter/sec
ZDOT = -3321
133367 ZDOT = -1012
281450
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 13117
59227720
00016717 00000-0 10270-3 0 9015
2 25544 51
6459 359
3173 0009766 192
7364 167
3542 15
52550262 26855
Satellite: ISS
Catalog Number: 25544
Epoch time: 13117
59227720 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 359
3173 deg
Eccentricity:
0009766
Arg of perigee: 192
7364 deg
Mean anomaly: 167
3542 deg
Mean motion: 15
52550262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2685
Checksum: 324
Coasting Arc #3 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2013/118/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6537859
73 A = 6796132
29 meter
Y = -1490667
78 meter E =
0001738
Z = -1101101
12 I = 51
63696
XDOT = 2010
541977 Wp = 42
71358
YDOT = 4482
479184 meter/sec RA = 354
62396 deg
ZDOT = 5876
053182 TA = 305
36016
MA = 305
37640
Ha = 225
227 n
mi
Hp = 219
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21449671
04 X = 6559391
73
Y = -4890642
31 feet Y = -1417436
89 meter
Z = -3612536
48 Z = -1069287
97
XDOT = 6596
266329 XDOT = 1931
723735
YDOT = 14706
296537 feet/sec YDOT = 4504
521478 meter/sec
ZDOT = 19278
389704 ZDOT = 5885
629053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20376302
78 X = 6210697
09
Y = -8351966
99 feet Y = -2545679
54 meter
Z = -3479672
68 Z = -1060604
23
XDOT = 8196
372961 XDOT = 2498
254478
YDOT = 11957
902758 feet/sec YDOT = 3644
768761 meter/sec
ZDOT = 19317
663847 ZDOT = 5888
023940
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 13118
42905554
00016717 00000-0 10270-3 0 9027
2 25544 51
6484 355
1559 0007833 217
4127 142
6480 15
51625833 26987
Satellite: ISS
Catalog Number: 25544
Epoch time: 13118
42905554 = yrday
fracday
Element set: 902
Inclination: 51
6484 deg
RA of node: 355
1559 deg
Eccentricity:
0007833
Arg of perigee: 217
4127 deg
Mean anomaly: 142
6480 deg
Mean motion: 15
51625833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2698
Checksum: 318
Coasting Arc #4 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2013/119/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6641065
40 A = 6796651
24 meter
Y = 1382452
47 meter E =
0014961
Z = 212495
70 I = 51
60833
XDOT = -1157
935540 Wp = 164
34097
YDOT = -4626
315903 meter/sec RA = 349
66312 deg
ZDOT = -6006
163272 TA = 13
36959
MA = 13
32999
Ha = 225
124 n
mi
Hp = 220
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21788272
31 X = -6657062
96
Y = 4535605
22 feet Y = 1308098
44 meter
Z = 697164
36 Z = 180194
79
XDOT = -3799
001114 XDOT = -1076
940344
YDOT = -15178
201780 feet/sec YDOT = -4638
811592 meter/sec
ZDOT = -19705
260079 ZDOT = -6011
591911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20609292
07 X = -6281712
22
Y = 8409963
30 feet Y = 2563356
81 meter
Z = 562281
44 Z = 171383
38
XDOT = -5754
129896 XDOT = -1753
858792
YDOT = -12759
004484 feet/sec YDOT = -3888
944567 meter/sec
ZDOT = -19727
219727 ZDOT = -6012
856573
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 13119
45954604
00016717 00000-0 10270-3 0 9032
2 25544 51
6486 350
0383 0007923 220
8675 139
1884 15
51610413 27140
Satellite: ISS
Catalog Number: 25544
Epoch time: 13119
45954604 = yrday
fracday
Element set: 903
Inclination: 51
6486 deg
RA of node: 350
0383 deg
Eccentricity:
0007923
Arg of perigee: 220
8675 deg
Mean anomaly: 139
1884 deg
Mean motion: 15
51610413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 306
Coasting Arc #5 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2013/120/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6641627
35 A = 6796290
88 meter
Y = -1262476
81 meter E =
0005542
Z = 674280
39 I = 51
57785
XDOT = 306
735844 Wp = 61
62817
YDOT = 4811
785404 meter/sec RA = 344
69968 deg
ZDOT = 5953
174995 TA = 305
64941
MA = 305
70101
Ha = 224
805 n
mi
Hp = 220
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21790115
98 X = 6651975
51
Y = -4141984
27 feet Y = -1188148
10 meter
Z = 2212206
00 Z = 706570
18
XDOT = 1006
351194 XDOT = 223
987484
YDOT = 15786
697520 feet/sec YDOT = 4814
752666 meter/sec
ZDOT = 19531
414026 ZDOT = 5954
464254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20523805
48 X = 6255655
91
Y = -8374002
89 feet Y = -2552396
08 meter
Z = 2347025
28 Z = 715373
30
XDOT = 3385
489675 XDOT = 1031
897253
YDOT = 13803
082901 feet/sec YDOT = 4207
179668 meter/sec
ZDOT = 19536
087964 ZDOT = 5954
599611
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 13120
49002117
00016717 00000-0 10270-3 0 9042
2 25544 51
6487 344
9200 0007803 226
2693 133
7813 15
51661656 27303
Satellite: ISS
Catalog Number: 25544
Epoch time: 13120
49002117 = yrday
fracday
Element set: 904
Inclination: 51
6487 deg
RA of node: 344
9200 deg
Eccentricity:
0007803
Arg of perigee: 226
2693 deg
Mean anomaly: 133
7813 deg
Mean motion: 15
51661656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 289
Coasting Arc #6 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2013/121/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6516116
50 A = 6795463
97 meter
Y = 1083671
67 meter E =
0011537
Z = -1562004
93 I = 51
54600
XDOT = 533
255538 Wp = 185
57364
YDOT = -5055
753760 meter/sec RA = 339
73427 deg
ZDOT = -5739
741978 TA = 11
51525
MA = 11
48888
Ha = 224
634 n
mi
Hp = 220
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21378334
96 X = -6520162
21
Y = 3555353
24 feet Y = 1010781
75 meter
Z = -5124688
10 Z = -1593669
61
XDOT = 1749
526042 XDOT = 617
632686
YDOT = -16587
118634 feet/sec YDOT = -5049
318686 meter/sec
ZDOT = -18831
174468 ZDOT = -5736
946591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20083154
74 X = -6121345
56
Y = 8060294
49 feet Y = 2456777
76 meter
Z = -5256873
49 Z = -1602295
04
XDOT = -1155
800414 XDOT = -352
287966
YDOT = -15137
314431 feet/sec YDOT = -4613
853438 meter/sec
ZDOT = -18818
784526 ZDOT = -5735
965524
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 13121
45608020
00016717 00000-0 10270-3 0 9055
2 25544 51
6490 340
1224 0007998 229
6999 130
3454 15
51648195 27455
Satellite: ISS
Catalog Number: 25544
Epoch time: 13121
45608020 = yrday
fracday
Element set: 905
Inclination: 51
6490 deg
RA of node: 340
1224 deg
Eccentricity:
0007998
Arg of perigee: 229
6999 deg
Mean anomaly: 130
3454 deg
Mean motion: 15
51648195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 314
Coasting Arc #7 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2013/122/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6296709
50 A = 6793914
05 meter
Y = -861106
93 meter E =
0006909
Z = 2396813
25 I = 51
51270
XDOT = -1314
333413 Wp = 96
17574
YDOT = 5323
064007 meter/sec RA = 334
76420 deg
ZDOT = 5351
296706 TA = 290
62029
MA = 290
69438
Ha = 224
359 n
mi
Hp = 220
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20658495
72 X = 6294227
47
Y = -2825153
97 feet Y = -790707
03 meter
Z = 7863560
52 Z = 2427396
20
XDOT = -4312
117496 XDOT = -1399
754635
YDOT = 17464
120757 feet/sec YDOT = 5307
888693 meter/sec
ZDOT = 17556
747722 ZDOT = 5344
704272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19394094
49 X = 5911320
00
Y = -7523320
05 feet Y = -2293107
95 meter
Z = 7991200
08 Z = 2435717
78
XDOT = -801
677302 XDOT = -244
351242
YDOT = 16600
120985 feet/sec YDOT = 5059
716876 meter/sec
ZDOT = 17528
491870 ZDOT = 5342
684322
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 13122
48652940
00016717 00000-0 10270-3 0 9060
2 25544 51
6488 335
0040 0007787 235
0124 125
0297 15
51692408 27618
Satellite: ISS
Catalog Number: 25544
Epoch time: 13122
48652940 = yrday
fracday
Element set: 906
Inclination: 51
6488 deg
RA of node: 335
0040 deg
Eccentricity:
0007787
Arg of perigee: 235
0124 deg
Mean anomaly: 125
0297 deg
Mean motion: 15
51692408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 302
Coasting Arc #8 (Orbit 2775)
---------------------------------------
Vector Time (GMT): 2013/123/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5972892
52 A = 6792020
50 meter
Y = 549495
76 meter E =
0005455
Z = -3178815
18 I = 51
47897
XDOT = 2039
616117 Wp = 205
11992
YDOT = -5613
064328 meter/sec RA = 329
79072 deg
ZDOT = -4804
459593 TA = 11
64428
MA = 11
63166
Ha = 224
095 n
mi
Hp = 220
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19596104
07 X = -5963151
27
Y = 1802807
61 feet Y = 482757
52 meter
Z = -10429183
65 Z = -3207807
46
XDOT = 6691
653926 XDOT = 2125
569911
YDOT = -18415
565379 feet/sec YDOT = -5589
775546 meter/sec
ZDOT = -15762
662708 ZDOT = -4794
342388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18471411
59 X = -5630086
25
Y = 6597480
55 feet Y = 2010912
07 meter
Z = -10550141
51 Z = -3215683
13
XDOT = 2482
103880 XDOT = 756
545263
YDOT = -18178
939073 feet/sec YDOT = -5540
940629 meter/sec
ZDOT = -15719
674972 ZDOT = -4791
356931
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 13123
45256266
00016717 00000-0 10270-3 0 9070
2 25544 51
6486 330
2064 0008027 238
8454 121
1911 15
51700959 27761
Satellite: ISS
Catalog Number: 25544
Epoch time: 13123
45256266 = yrday
fracday
Element set: 907
Inclination: 51
6486 deg
RA of node: 330
2064 deg
Eccentricity:
0008027
Arg of perigee: 238
8454 deg
Mean anomaly: 121
1911 deg
Mean motion: 15
51700959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2776
Checksum: 305
Coasting Arc #9 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2013/124/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5583745
35 A = 6789934
21 meter
Y = -172943
99 meter E =
0006653
Z = 3860082
13 I = 51
44585
XDOT = -2666
089932 Wp = 141
48175
YDOT = 5889
433181 meter/sec RA = 324
81133 deg
ZDOT = 4111
523396 TA = 265
14741
MA = 265
22338
Ha = 223
900 n
mi
Hp = 221
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18319374
51 X = 5566512
86
Y = -567401
55 feet Y = -110599
27 meter
Z = 12664311
44 Z = 3887165
83
XDOT = -8747
014213 XDOT = -2751
721524
YDOT = 19322
287340 feet/sec YDOT = 5859
140605 meter/sec
ZDOT = 13489
249988 ZDOT = 4098
363501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17438316
13 X = 5315198
76
Y = -5380813
35 feet Y = -1640071
91 meter
Z = 12777252
82 Z = 3894506
66
XDOT = -3785
218125 XDOT = -1153
734484
YDOT = 19700
965424 feet/sec YDOT = 6004
854261 meter/sec
ZDOT = 13433
543840 ZDOT = 4094
544162
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 13124
48298638
00016717 00000-0 10270-3 0 9084
2 25544 51
6483 325
0877 0007793 243
5348 116
5004 15
51719450 27921
Satellite: ISS
Catalog Number: 25544
Epoch time: 13124
48298638 = yrday
fracday
Element set: 908
Inclination: 51
6483 deg
RA of node: 325
0877 deg
Eccentricity:
0007793
Arg of perigee: 243
5348 deg
Mean anomaly: 116
5004 deg
Mean motion: 15
51719450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 329
Coasting Arc #10 (Orbit 2806)
---------------------------------------
Vector Time (GMT): 2013/125/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5128852
32 A = 6787789
58 meter
Y = -303431
06 meter E =
0001384
Z = -4437171
49 I = 51
41349
XDOT = 3204
484109 Wp = 81
30142
YDOT = -6135
783209 meter/sec RA = 319
82739 deg
ZDOT = -3285
095368 TA = 155
43777
MA = 155
43118
Ha = 223
568 n
mi
Hp = 221
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16826943
32 X = -5103523
26
Y = -995508
71 feet Y = -360643
63 meter
Z = -14557649
26 Z = -4462025
77
XDOT = 10513
399309 XDOT = 3288
815888
YDOT = -20130
522339 feet/sec YDOT = -6099
477220 meter/sec
ZDOT = -10777
871943 ZDOT = -3269
323060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16340086
01 X = -4980458
22
Y = 3756638
66 feet Y = 1145023
46 meter
Z = -14661223
21 Z = -4468740
84
XDOT = 4756
796190 XDOT = 1449
871479
YDOT = -21104
318390 feet/sec YDOT = -6432
596245 meter/sec
ZDOT = -10711
246302 ZDOT = -3264
787873
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 13125
44899396
00016717 00000-0 10270-3 0 9090
2 25544 51
6472 320
2894 0008017 247
5006 112
5297 15
51756781 28075
Satellite: ISS
Catalog Number: 25544
Epoch time: 13125
44899396 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 320
2894 deg
Eccentricity:
0008017
Arg of perigee: 247
5006 deg
Mean anomaly: 112
5297 deg
Mean motion: 15
51756781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2807
Checksum: 329
Coasting Arc #11 (Orbit 2822)
---------------------------------------
Vector Time (GMT): 2013/126/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4648402
84 A = 6786090
15 meter
Y = 847060
07 meter E =
0006240
Z = 4874581
46 I = 51
38482
XDOT = -3629
859313 Wp = 195
17629
YDOT = 6321
187437 meter/sec RA = 314
83847 deg
ZDOT = 2357
777555 TA = 231
59957
MA = 231
65563
Ha = 223
437 n
mi
Hp = 221
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15250665
50 X = 4614905
58
Y = 2779068
47 feet Y = 898854
26 meter
Z = 15992721
33 Z = 4897081
96
XDOT = -11908
987248 XDOT = -3711
728036
YDOT = 20738
803926 feet/sec YDOT = 6280
138362 meter/sec
ZDOT = 7735
490665 ZDOT = 2339
944739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15291611
98 X = 4660883
33
Y = -1862106
73 feet Y = -567570
13 meter
Z = 16086401
61 Z = 4903135
21
XDOT = -5367
425013 XDOT = -1635
991144
YDOT = 22245
359820 feet/sec YDOT = 6780
385673 meter/sec
ZDOT = 7660
254883 ZDOT = 2334
845688
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 13126
47939157
00016717 00000-0 10270-3 0 9106
2 25544 51
6471 315
1707 0007848 251
4917 108
5382 15
51751337 28236
Satellite: ISS
Catalog Number: 25544
Epoch time: 13126
47939157 = yrday
fracday
Element set: 910
Inclination: 51
6471 deg
RA of node: 315
1707 deg
Eccentricity:
0007848
Arg of perigee: 251
4917 deg
Mean anomaly: 108
5382 deg
Mean motion: 15
51751337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2823
Checksum: 316
Coasting Arc #12 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2013/127/10:14:52
447
Vector Time (MET): N/A
Weight (LBS) : 904536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4148853
52 A = 6784689
45 meter
Y = -1475577
28 meter E =
0006030
Z = -5166873
23 I = 51
35821
XDOT = 3956
940330 Wp = 85
78067
YDOT = -6419
818608 meter/sec RA = 309
84483 deg
ZDOT = -1344
838193 TA = 171
23527
MA = 171
22473
Ha = 223
064 n
mi
Hp = 221
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13611724
13 X = -4106945
19
Y = -4841132
80 feet Y = -1521738
11 meter
Z = -16951683
82 Z = -5186926
55
XDOT = 12982
087696 XDOT = 4034
967013
YDOT = -21062
397009 feet/sec YDOT = -6375
133349 meter/sec
ZDOT = -4412
198797 ZDOT = -1325
425777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14344306
66 X = -4372144
67
Y = -349865
69 feet Y = -106639
06 meter
Z = -17035071
05 Z = -5192289
66
XDOT = 5701
020943 XDOT = 1737
671184
YDOT = -23038
875392 feet/sec YDOT = -7022
249219 meter/sec
ZDOT = -4330
369038 ZDOT = -1319
896483
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 13127
44537400
00016717 00000-0 10270-3 0 9110
2 25544 51
6456 310
3712 0007989 255
3617 104
6649 15
51808462 28389
Satellite: ISS
Catalog Number: 25544
Epoch time: 13127
44537400 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 310
3712 deg
Eccentricity:
0007989
Arg of perigee: 255
3617 deg
Mean anomaly: 104
6649 deg
Mean motion: 15
51808462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 313
Coasting Arc #13 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2013/128/06:42:01
137
Vector Time (MET): N/A
Weight (LBS) : 904127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2605869
05 A = 6797069
45 meter
Y = -6026875
79 meter E =
0008611
Z = -1735016
06 I = 51
37825
XDOT = 5135
796609 Wp = 323
96998
YDOT = 589
527913 meter/sec RA = 305
56942 deg
ZDOT = 5658
247338 TA = 16
94399
MA = 16
91525
Ha = 223
717 n
mi
Hp = 222
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8549439
13 X = 2681497
60
Y = -19773214
53 feet Y = -5997312
45 meter
Z = -5692309
91 Z = -1722173
04
XDOT = 16849
726406 XDOT = 5101
335877
YDOT = 1934
146696 feet/sec YDOT = 646
766928 meter/sec
ZDOT = 18563
803603 ZDOT = 5683
113382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18183694
03 X = 5542389
94
Y = -11577668
32 feet Y = -3528873
30 meter
Z = -5637923
55 Z = -1718439
10
XDOT = 11938
050582 XDOT = 3638
717817
YDOT = 9647
203981 feet/sec YDOT = 2940
467774 meter/sec
ZDOT = 18667
376518 ZDOT = 5689
816363
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 13128
28255132
00016717 00000-0 10270-3 0 9123
2 25544 51
6481 306
2135 0009787 275
9391 84
0645 15
51041537 28519
Satellite: ISS
Catalog Number: 25544
Epoch time: 13128
28255132 = yrday
fracday
Element set: 912
Inclination: 51
6481 deg
RA of node: 306
2135 deg
Eccentricity:
0009787
Arg of perigee: 275
9391 deg
Mean anomaly: 84
0645 deg
Mean motion: 15
51041537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 306
Coasting Arc #14 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2013/129/06:42:01
137
Vector Time (MET): N/A
Weight (LBS) : 904127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2650051
00 A = 6797912
18 meter
Y = 6163311
68 meter E =
0006154
Z = 1070389
24 I = 51
36378
XDOT = -4820
135668 Wp = 163
98174
YDOT = -1054
066933 meter/sec RA = 300
59327 deg
ZDOT = -5861
994894 TA = 4
38171
MA = 4
37633
Ha = 224
178 n
mi
Hp = 222
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8694393
04 X = -2723973
29
Y = 20220838
83 feet Y = 6133263
79 meter
Z = 3511775
73 Z = 1057335
84
XDOT = -15814
093399 XDOT = -4779
514032
YDOT = -3458
224845 feet/sec YDOT = -1107
741473 meter/sec
ZDOT = -19232
266713 ZDOT = -5885
312527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18336157
43 X = -5588860
78
Y = 12192019
31 feet Y = 3716127
49 meter
Z = 3456495
08 Z = 1053539
70
XDOT = -10377
239391 XDOT = -3162
982566
YDOT = -10124
710845 feet/sec YDOT = -3086
011866 meter/sec
ZDOT = -19329
319039 ZDOT = -5891
576443
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 13129
31343642
00016717 00000-0 10270-3 0 9133
2 25544 51
6481 301
0986 0009761 279
4228 80
5819 15
51019266 28671
Satellite: ISS
Catalog Number: 25544
Epoch time: 13129
31343642 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 301
0986 deg
Eccentricity:
0009761
Arg of perigee: 279
4228 deg
Mean anomaly: 80
5819 deg
Mean motion: 15
51019266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 318
Coasting Arc #15 (Orbit 2881)
---------------------------------------
Vector Time (GMT): 2013/130/06:42:01
137
Vector Time (MET): N/A
Weight (LBS) : 904127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2656286
43 A = 6798147
80 meter
Y = -6238287
04 meter E =
0010927
Z = -377389
11 I = 51
35082
XDOT = 4542
246451 Wp = 349
47395
YDOT = 1571
835244 meter/sec RA = 295
61562 deg
ZDOT = 5971
475006 TA = 6
44550
MA = 6
43146
Ha = 224
464 n
mi
Hp = 222
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8714850
48 X = 2727680
16
Y = -20466821
01 feet Y = -6208183
57 meter
Z = -1238153
25 Z = -364311
67
XDOT = 14902
383371 XDOT = 4495
323853
YDOT = 5156
939777 feet/sec YDOT = 1622
366913 meter/sec
ZDOT = 19591
453432 ZDOT = 5993
427372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18259698
54 X = 5565556
11
Y = -12710502
91 feet Y = -3874161
29 meter
Z = -1182763
47 Z = -360506
31
XDOT = 8858
407593 XDOT = 2700
042634
YDOT = 10888
881884 feet/sec YDOT = 3318
931198 meter/sec
ZDOT = 19682
743108 ZDOT = 5999
300099
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 13130
27987717
00016717 00000-0 10270-3 0 9148
2 25544 51
6484 296
3024 0009926 284
0452 75
9595 15
51081113 28823
Satellite: ISS
Catalog Number: 25544
Epoch time: 13130
27987717 = yrday
fracday
Element set: 914
Inclination: 51
6484 deg
RA of node: 296
3024 deg
Eccentricity:
0009926
Arg of perigee: 284
0452 deg
Mean anomaly: 75
9595 deg
Mean motion: 15
51081113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2882
Checksum: 325
Coasting Arc #16 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2013/131/06:42:01
137
Vector Time (MET): N/A
Weight (LBS) : 904127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2633291
16 A = 6798236
16 meter
Y = 6255023
56 meter E =
0005719
Z = -324473
15 I = 51
33857
XDOT = -4305
120354 Wp = 197
90316
YDOT = -2123
338125 meter/sec RA = 290
63841 deg
ZDOT = -5971
207675 TA = 345
60313
MA = 345
61942
Ha = 224
778 n
mi
Hp = 222
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8639406
71 X = -2701464
24
Y = 20521730
84 feet Y = 6225195
28 meter
Z = -1064544
46 Z = -337430
94
XDOT = -14124
410610 XDOT = -4252
049703
YDOT = -6966
332432 feet/sec YDOT = -2171
183637 meter/sec
ZDOT = -19590
576360 ZDOT = -5991
993165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17989839
35 X = -5483303
03
Y = 13115890
48 feet Y = 3997723
42 meter
Z = -1119436
02 Z = -341204
10
XDOT = -7437
038920 XDOT = -2266
809463
YDOT = -11886
179511 feet/sec YDOT = -3622
907515 meter/sec
ZDOT = -19676
927616 ZDOT = -5997
527537
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 13131
31073656
00016717 00000-0 10270-3 0 9153
2 25544 51
6485 291
1877 0009932 287
1849 72
8214 15
51051733 28980
Satellite: ISS
Catalog Number: 25544
Epoch time: 13131
31073656 = yrday
fracday
Element set: 915
Inclination: 51
6485 deg
RA of node: 291
1877 deg
Eccentricity:
0009932
Arg of perigee: 287
1849 deg
Mean anomaly: 72
8214 deg
Mean motion: 15
51051733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 327
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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