[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 26th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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
118/10:07:52
392 3
3 4
8 4
8
N/A 1
6 -0
5 225
3
000/00:11:44
784 3
2 -0
1 220
0
Coasting Arc #1 (Orbit 2559)
---------------------------------------
Vector Time (GMT): 2013/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5877241
71 A = 6789485
49 meter
Y = -307519
10 meter E =
0011491
Z = -3400860
40 I = 51
79855
XDOT = 2962
877439 Wp = 147
13490
YDOT = 5318
948183 meter/sec RA = 24
05388 deg
ZDOT = 4637
328731 TA = 173
32034
MA = 173
30501
Ha = 226
196 n
mi
Hp = 215
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19282289
07 X = 5896764
29
Y = -1008920
93 feet Y = -241687
21 meter
Z = -11157678
49 Z = -3372261
52
XDOT = 9720
726505 XDOT = 2880
652458
YDOT = 17450
617397 feet/sec YDOT = 5351
621598 meter/sec
ZDOT = 15214
333108 ZDOT = 4651
522110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16272613
29 X = 4959892
53
Y = -10520217
69 feet Y = -3206562
35 meter
Z = -11038363
05 Z = -3364493
06
XDOT = 16276
823737 XDOT = 4961
175875
YDOT = 9144
768199 feet/sec YDOT = 2787
325347 meter/sec
ZDOT = 15272
787927 ZDOT = 4655
145760
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 13112
50702018
00016717 00000-0 10270-3 0 9008
2 25544 51
6471 24
6012 0010000 171
9395 188
1920 15
52431958 25602
Satellite: ISS
Catalog Number: 25544
Epoch time: 13112
50702018 = yrday
fracday
Element set: 900
Inclination: 51
6471 deg
RA of node: 24
6012 deg
Eccentricity:
0010000
Arg of perigee: 171
9395 deg
Mean anomaly: 188
1920 deg
Mean motion: 15
52431958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2560
Checksum: 264
Coasting Arc #2 (Orbit 2575)
---------------------------------------
Vector Time (GMT): 2013/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6329386
70 A = 6791901
83 meter
Y = -172590
52 meter E =
0019696
Z = 2422171
48 I = 51
77823
XDOT = -1919
432698 Wp = 134
34500
YDOT = -5138
466984 meter/sec RA = 19
09575 deg
ZDOT = -5368
344486 TA = 18
60353
MA = 18
53163
Ha = 226
199 n
mi
Hp = 216
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20765704
39 X = -6338752
78
Y = -566241
86 feet Y = -243421
88 meter
Z = 7946756
81 Z = 2391400
66
XDOT = -6297
351371 XDOT = -1835
752217
YDOT = -16858
487479 feet/sec YDOT = -5159
463847 meter/sec
ZDOT = -17612
678759 ZDOT = -5377
465384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18153912
42 X = -5533312
50
Y = 10197706
84 feet Y = 3108261
04 meter
Z = 7818458
39 Z = 2383066
12
XDOT = -13221
001737 XDOT = -4029
761329
YDOT = -9969
486627 feet/sec YDOT = -3038
699524 meter/sec
ZDOT = -17649
996358 ZDOT = -5379
718890
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 13113
53697962
00016717 00000-0 10270-3 0 9014
2 25544 51
6473 19
4804 0010029 175
7390 184
3849 15
52418822 25763
Satellite: ISS
Catalog Number: 25544
Epoch time: 13113
53697962 = yrday
fracday
Element set: 901
Inclination: 51
6473 deg
RA of node: 19
4804 deg
Eccentricity:
0010029
Arg of perigee: 175
7390 deg
Mean anomaly: 184
3849 deg
Mean motion: 15
52418822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2576
Checksum: 321
Coasting Arc #3 (Orbit 2590)
---------------------------------------
Vector Time (GMT): 2013/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6635816
55 A = 6793427
80 meter
Y = 572968
59 meter E =
0006178
Z = -1351625
74 I = 51
75523
XDOT = 756
712454 Wp = 117
92531
YDOT = 4919
623906 meter/sec RA = 14
13884 deg
ZDOT = 5818
084892 TA = 227
40614
MA = 227
45828
Ha = 225
883 n
mi
Hp = 216
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21771051
67 X = 6635482
26
Y = 1879818
22 feet Y = 647172
52 meter
Z = -4434467
65 Z = -1319389
75
XDOT = 2482
652409 XDOT = 673
380671
YDOT = 16140
498380 feet/sec YDOT = 4927
620401 meter/sec
ZDOT = 19088
205027 ZDOT = 5821
558261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19504834
14 X = 5945073
44
Y = -9911977
02 feet Y = -3021170
59 meter
Z = -4300124
13 Z = -1310677
83
XDOT = 9807
616402 XDOT = 2989
361479
YDOT = 11038
146355 feet/sec YDOT = 3364
427009 meter/sec
ZDOT = 19101
994878 ZDOT = 5822
288039
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 13114
50255432
00016717 00000-0 10270-3 0 9025
2 25544 51
6479 14
6792 0009931 179
9135 180
2020 15
52466854 25916
Satellite: ISS
Catalog Number: 25544
Epoch time: 13114
50255432 = yrday
fracday
Element set: 902
Inclination: 51
6479 deg
RA of node: 14
6792 deg
Eccentricity:
0009931
Arg of perigee: 179
9135 deg
Mean anomaly: 180
2020 deg
Mean motion: 15
52466854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2591
Checksum: 305
Coasting Arc #4 (Orbit 2606)
---------------------------------------
Vector Time (GMT): 2013/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6713587
76 A = 6794247
40 meter
Y = -940349
04 meter E =
0020276
Z = 181354
20 I = 51
72787
XDOT = 494
064786 Wp = 155
19047
YDOT = -4732
037282 meter/sec RA = 9
18274 deg
ZDOT = -6020
864085 TA = 22
85747
MA = 22
76735
Ha = 225
828 n
mi
Hp = 216
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22026206
56 X = -6703454
59
Y = -3085134
64 feet Y = -1015367
94 meter
Z = 594994
09 Z = 148764
10
XDOT = 1620
947460 XDOT = 576
191121
YDOT = -15525
056699 feet/sec YDOT = -4726
053409 meter/sec
ZDOT = -19753
491091 ZDOT = -6018
264213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20179890
72 X = -6150830
69
Y = 9358790
72 feet Y = 2852559
41 meter
Z = 459234
18 Z = 139974
58
XDOT = -6276
200391 XDOT = -1912
985879
YDOT = -12517
267983 feet/sec YDOT = -3815
263281 meter/sec
ZDOT = -19741
976226 ZDOT = -6017
354354
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 13115
53249083
00016717 00000-0 10270-3 0 9035
2 25544 51
6481 9
5582 0010042 183
8556 176
2520 15
52438108 26074
Satellite: ISS
Catalog Number: 25544
Epoch time: 13115
53249083 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 9
5582 deg
Eccentricity:
0010042
Arg of perigee: 183
8556 deg
Mean anomaly: 176
2520 deg
Mean motion: 15
52438108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2607
Checksum: 293
Coasting Arc #5 (Orbit 2622)
---------------------------------------
Vector Time (GMT): 2013/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6605824
03 A = 6793656
96 meter
Y = 1256133
65 meter E =
0010087
Z = 969976
47 I = 51
69596
XDOT = -1741
184009 Wp = 101
68666
YDOT = 4551
707223 meter/sec RA = 4
22410 deg
ZDOT = 5909
343707 TA = 268
79609
MA = 268
91165
Ha = 225
537 n
mi
Hp = 216
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21672651
01 X = 6586574
71
Y = 4121173
40 feet Y = 1329896
53 meter
Z = 3182337
50 Z = 1002020
94
XDOT = -5712
545960 XDOT = -1820
659428
YDOT = 14933
422649 feet/sec YDOT = 4531
791931 meter/sec
ZDOT = 19387
610587 ZDOT = 5900
691874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20279959
12 X = 6181331
54
Y = -8633890
56 feet Y = -2631609
84 meter
Z = 3315770
79 Z = 1010646
94
XDOT = 2842
591103 XDOT = 866
421768
YDOT = 14173
863747 feet/sec YDOT = 4320
193670 meter/sec
ZDOT = 19350
881180 ZDOT = 5898
148584
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
56241382
00016717 00000-0 10270-3 0 9044
2 25544 51
6480 4
4366 0009798 188
2291 171
8702 15
52491409 26232
Satellite: ISS
Catalog Number: 25544
Epoch time: 13116
56241382 = yrday
fracday
Element set: 904
Inclination: 51
6480 deg
RA of node: 4
4366 deg
Eccentricity:
0009798
Arg of perigee: 188
2291 deg
Mean anomaly: 171
8702 deg
Mean motion: 15
52491409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2623
Checksum: 310
Coasting Arc #6 (Orbit 2637)
---------------------------------------
Vector Time (GMT): 2013/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6247290
48 A = 6792179
94 meter
Y = -1590313
52 meter E =
0014538
Z = -2112384
41 I = 51
66022
XDOT = 2983
115767 Wp = 171
44609
YDOT = -4407
157016 meter/sec RA = 359
26204 deg
ZDOT = -5523
427667 TA = 31
94479
MA = 31
85673
Ha = 225
378 n
mi
Hp = 216
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20496359
84 X = -6218781
33
Y = -5217564
04 feet Y = -1660015
23 meter
Z = -6930395
04 Z = -2142664
59
XDOT = 9787
125221 XDOT = 3059
007712
YDOT = -14459
176562 feet/sec YDOT = -4373
373548 meter/sec
ZDOT = -18121
481848 ZDOT = -5508
751353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19770088
10 X = -6025922
85
Y = 7396260
72 feet Y = 2254380
27 meter
Z = -7056419
81 Z = -2150796
76
XDOT = 407
696438 XDOT = 124
265874
YDOT = -16081
910784 feet/sec YDOT = -4901
766407 meter/sec
ZDOT = -18059
649269 ZDOT = -5504
581097
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
52795704
00016717 00000-0 10270-3 0 9054
2 25544 51
6480 359
6354 0009963 192
5942 167
4963 15
52475046 26384
Satellite: ISS
Catalog Number: 25544
Epoch time: 13117
52795704 = yrday
fracday
Element set: 905
Inclination: 51
6480 deg
RA of node: 359
6354 deg
Eccentricity:
0009963
Arg of perigee: 192
5942 deg
Mean anomaly: 167
4963 deg
Mean motion: 15
52475046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2638
Checksum: 342
Coasting Arc #7 (Orbit 2651)
---------------------------------------
Vector Time (GMT): 2013/118/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6368407
72 A = 6795784
39 meter
Y = -1814153
92 meter E =
0000179
Z = -1527539
40 I = 51
63521
XDOT = 2612
806892 Wp = 5
26965
YDOT = 4328
124314 meter/sec RA = 354
62114 deg
ZDOT = 5752
967603 TA = 338
07085
MA = 338
07162
Ha = 225
332 n
mi
Hp = 219
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20893726
11 X = 6395641
16
Y = -5951948
55 feet Y = -1742786
06 meter
Z = -5011612
21 Z = -1496535
61
XDOT = 8572
201090 XDOT = 2536
267844
YDOT = 14199
882919 feet/sec YDOT = 4356
914260 meter/sec
ZDOT = 18874
565627 ZDOT = 5765
474805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19707757
90 X = 6006924
61
Y = -9211913
59 feet Y = -2807791
26 meter
Z = -4882075
97 Z = -1488056
76
XDOT = 9939
577459 XDOT = 3029
583210
YDOT = 11234
577559 feet/sec YDOT = 3424
299240 meter/sec
ZDOT = 18926
084604 ZDOT = 5768
670587
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
42912085
00016717 00000-0 10270-3 0 9068
2 25544 51
6482 355
1525 0008163 218
3552 141
7020 15
51587538 26526
Satellite: ISS
Catalog Number: 25544
Epoch time: 13118
42912085 = yrday
fracday
Element set: 906
Inclination: 51
6482 deg
RA of node: 355
1525 deg
Eccentricity:
0008163
Arg of perigee: 218
3552 deg
Mean anomaly: 141
7020 deg
Mean motion: 15
51587538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2652
Checksum: 298
Coasting Arc #8 (Orbit 2667)
---------------------------------------
Vector Time (GMT): 2013/119/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6528892
36 A = 6796630
07 meter
Y = 1728319
86 meter E =
0015052
Z = 666843
57 I = 51
60750
XDOT = -1796
325737 Wp = 160
87438
YDOT = -4475
548279 meter/sec RA = 349
66004 deg
ZDOT = -5963
430111 TA = 11
92373
MA = 11
88814
Ha = 225
249 n
mi
Hp = 220
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21420250
52 X = -6550972
94
Y = 5670340
74 feet Y = 1655186
19 meter
Z = 2187806
99 Z = 635072
83
XDOT = -5893
457144 XDOT = -1717
176599
YDOT = -14683
557345 feet/sec YDOT = -4495
193173 meter/sec
ZDOT = -19565
059418 ZDOT = -5971
964509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20097190
32 X = -6125623
61
Y = 9361942
45 feet Y = 2853520
06 meter
Z = 2055084
17 Z = 626389
65
XDOT = -7589
452287 XDOT = -2313
265057
YDOT = -11971
132642 feet/sec YDOT = -3648
801229 meter/sec
ZDOT = -19599
990777 ZDOT = -5974
077189
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
45964077
00016717 00000-0 10270-3 0 9071
2 25544 51
6483 350
0351 0008223 221
8043 138
2481 15
51565071 26686
Satellite: ISS
Catalog Number: 25544
Epoch time: 13119
45964077 = yrday
fracday
Element set: 907
Inclination: 51
6483 deg
RA of node: 350
0351 deg
Eccentricity:
0008223
Arg of perigee: 221
8043 deg
Mean anomaly: 138
2481 deg
Mean motion: 15
51565071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2668
Checksum: 301
Coasting Arc #9 (Orbit 2683)
---------------------------------------
Vector Time (GMT): 2013/120/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6591743
75 A = 6796614
39 meter
Y = -1634967
41 meter E =
0004396
Z = 205172
47 I = 51
57827
XDOT = 968
324595 Wp = 49
28244
YDOT = 4666
841732 meter/sec RA = 344
69679 deg
ZDOT = 5997
084117 TA = 312
92644
MA = 312
96332
Ha = 224
919 n
mi
Hp = 220
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21626455
88 X = 6608539
71
Y = -5364066
30 feet Y = -1561160
47 meter
Z = 673138
02 Z = 237235
57
XDOT = 3176
917962 XDOT = 886
934554
YDOT = 15311
160537 feet/sec YDOT = 4677
214889 meter/sec
ZDOT = 19675
472826 ZDOT = 6001
590635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20177398
01 X = 6150070
91
Y = -9441989
70 feet Y = -2877918
46 meter
Z = 807066
44 Z = 245993
85
XDOT = 5268
885436 XDOT = 1605
956281
YDOT = 12961
963228 feet/sec YDOT = 3950
806392 meter/sec
ZDOT = 19693
582552 ZDOT = 6002
603962
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
49014801
00016717 00000-0 10270-3 0 9089
2 25544 51
6485 344
9170 0008140 227
1361 132
9108 15
51615795 26843
Satellite: ISS
Catalog Number: 25544
Epoch time: 13120
49014801 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 344
9170 deg
Eccentricity:
0008140
Arg of perigee: 227
1361 deg
Mean anomaly: 132
9108 deg
Mean motion: 15
51615795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2684
Checksum: 296
Coasting Arc #10 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2013/121/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6531890
95 A = 6796179
06 meter
Y = 1490946
45 meter E =
0012682
Z = -1088150
96 I = 51
54759
XDOT = -145
894499 Wp = 182
24919
YDOT = -4921
860595 meter/sec RA = 339
73212 deg
ZDOT = -5878
059655 TA = 9
56327
MA = 9
53915
Ha = 224
781 n
mi
Hp = 220
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21430088
42 X = -6542791
60
Y = 4891556
60 feet Y = 1417841
80 meter
Z = -3570049
07 Z = -1119908
91
XDOT = -478
656492 XDOT = -62
292183
YDOT = -16147
836597 feet/sec YDOT = -4923
024535 meter/sec
ZDOT = -19284
972621 ZDOT = -5878
565415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19901861
67 X = -6066087
44
Y = 9280480
06 feet Y = 2828690
32 meter
Z = -3702682
52 Z = -1128577
63
XDOT = -3068
241568 XDOT = -935
200030
YDOT = -14261
882743 feet/sec YDOT = -4347
021860 meter/sec
ZDOT = -19286
366473 ZDOT = -5878
484501
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
45624051
00016717 00000-0 10270-3 0 9091
2 25544 51
6488 340
1196 0008302 230
3930 129
6490 15
51591018 26994
Satellite: ISS
Catalog Number: 25544
Epoch time: 13121
45624051 = yrday
fracday
Element set: 909
Inclination: 51
6488 deg
RA of node: 340
1196 deg
Eccentricity:
0008302
Arg of perigee: 230
3930 deg
Mean anomaly: 129
6490 deg
Mean motion: 15
51591018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 299
Coasting Arc #11 (Orbit 2714)
---------------------------------------
Vector Time (GMT): 2013/122/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6379318
10 A = 6794931
46 meter
Y = -1307228
09 meter E =
0006227
Z = 1933863
93 I = 51
51536
XDOT = -630
815870 Wp = 83
66503
YDOT = 5206
067965 meter/sec RA = 334
76331 deg
ZDOT = 5585
190740 TA = 297
66187
MA = 297
72505
Ha = 224
486 n
mi
Hp = 220
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20929521
33 X = 6384067
45
Y = -4288806
07 feet Y = -1235863
98 meter
Z = 6344697
93 Z = 1964865
75
XDOT = -2069
605873 XDOT = -716
115817
YDOT = 17080
275475 feet/sec YDOT = 5198
536853 meter/sec
ZDOT = 18324
116602 ZDOT = 5581
919082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19371911
79 X = 5904558
71
Y = -8916745
41 feet Y = -2717824
00 meter
Z = 6474148
39 Z = 1973320
43
XDOT = 1100
100641 XDOT = 335
310675
YDOT = 15718
715568 feet/sec YDOT = 4791
064505 meter/sec
ZDOT = 18309
723569 ZDOT = 5580
803744
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
48672754
00016717 00000-0 10270-3 0 9100
2 25544 51
6486 335
0014 0008129 235
8335 124
2046 15
51638601 27157
Satellite: ISS
Catalog Number: 25544
Epoch time: 13122
48672754 = yrday
fracday
Element set: 910
Inclination: 51
6486 deg
RA of node: 335
0014 deg
Eccentricity:
0008129
Arg of perigee: 235
8335 deg
Mean anomaly: 124
2046 deg
Mean motion: 15
51638601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2715
Checksum: 291
Coasting Arc #12 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2013/123/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6122825
47 A = 6793327
80 meter
Y = 1040948
01 meter E =
0007376
Z = -2740280
78 I = 51
48252
XDOT = 1359
717605 Wp = 204
42383
YDOT = -5523
831381 meter/sec RA = 329
79168 deg
ZDOT = -5138
074601 TA = 6
63589
MA = 6
62613
Ha = 224
253 n
mi
Hp = 221
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20088010
07 X = -6120698
89
Y = 3415183
77 feet Y = 972490
56 meter
Z = -8990422
51 Z = -2770019
93
XDOT = 4461
015763 XDOT = 1446
344729
YDOT = -18122
806368 feet/sec YDOT = -5508
141894 meter/sec
ZDOT = -16857
200134 ZDOT = -5131
258666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18596572
26 X = -5668235
22
Y = 8192162
93 feet Y = 2496971
26 meter
Z = -9114564
85 Z = -2778119
37
XDOT = 609
189518 XDOT = 185
680965
YDOT = -17334
037023 feet/sec YDOT = -5283
414485 meter/sec
ZDOT = -16827
989347 ZDOT = -5129
171153
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
45279977
00016717 00000-0 10270-3 0 9119
2 25544 51
6484 330
2040 0008344 239
4159 120
6169 15
51633144 27304
Satellite: ISS
Catalog Number: 25544
Epoch time: 13123
45279977 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 330
2040 deg
Eccentricity:
0008344
Arg of perigee: 239
4159 deg
Mean anomaly: 120
6169 deg
Mean motion: 15
51633144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 297
Coasting Arc #13 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2013/124/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5798340
41 A = 6791357
56 meter
Y = -711618
14 meter E =
0006240
Z = 3463014
10 I = 51
44975
XDOT = -2000
850097 Wp = 127
82397
YDOT = 5837
615600 meter/sec RA = 324
81433 deg
ZDOT = 4540
362716 TA = 272
87117
MA = 272
94258
Ha = 224
041 n
mi
Hp = 221
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19023426
55 X = 5789044
40
Y = -2334705
19 feet Y = -646829
32 meter
Z = 11361594
83 Z = 3491159
59
XDOT = -6564
468822 XDOT = -2088
034899
YDOT = 19152
282151 feet/sec YDOT = 5814
753482 meter/sec
ZDOT = 14896
203136 ZDOT = 4530
430751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17692169
33 X = 5392573
21
Y = -7186531
31 feet Y = -2190454
74 meter
Z = 11479039
83 Z = 3498811
34
XDOT = -1965
665541 XDOT = -599
134857
YDOT = 18935
607246 feet/sec YDOT = 5771
573089 meter/sec
ZDOT = 14853
962177 ZDOT = 4527
487672
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
48326724
00016717 00000-0 10270-3 0 9127
2 25544 51
6480 325
0856 0008130 244
3800 115
6512 15
51655345 27468
Satellite: ISS
Catalog Number: 25544
Epoch time: 13124
48326724 = yrday
fracday
Element set: 912
Inclination: 51
6480 deg
RA of node: 325
0856 deg
Eccentricity:
0008130
Arg of perigee: 244
3800 deg
Mean anomaly: 115
6512 deg
Mean motion: 15
51655345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 289
Coasting Arc #14 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2013/125/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5405219
55 A = 6789242
24 meter
Y = 284823
50 meter E =
0000892
Z = -4097333
29 I = 51
41747
XDOT = 2562
220145 Wp = 222
63055
YDOT = -6137
085753 meter/sec RA = 319
83294 deg
ZDOT = -3806
863256 TA = 7
91210
MA = 7
91069
Ha = 223
732 n
mi
Hp = 221
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17733659
95 X = -5388098
80
Y = 934460
29 feet Y = 224474
53 meter
Z = -13442694
53 Z = -4123550
10
XDOT = 8406
234073 XDOT = 2649
148863
YDOT = -20134
795779 feet/sec YDOT = -6107
947460 meter/sec
ZDOT = -12489
708845 ZDOT = -3794
204738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16701957
71 X = -5090756
71
Y = 5783508
79 feet Y = 1762813
48 meter
Z = -13552032
40 Z = -4130659
48
XDOT = 2998
730530 XDOT = 914
013065
YDOT = -20479
332444 feet/sec YDOT = -6242
100529 meter/sec
ZDOT = -12436
064343 ZDOT = -3790
512412
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
44931913
00016717 00000-0 10270-3 0 9137
2 25544 51
6470 320
2877 0008341 248
0565 111
9700 15
51679746 27616
Satellite: ISS
Catalog Number: 25544
Epoch time: 13125
44931913 = yrday
fracday
Element set: 913
Inclination: 51
6470 deg
RA of node: 320
2877 deg
Eccentricity:
0008341
Arg of perigee: 248
0565 deg
Mean anomaly: 111
9700 deg
Mean motion: 15
51679746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 307
Coasting Arc #15 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2013/126/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4981022
19 A = 6787382
26 meter
Y = 211664
82 meter E =
0006014
Z = 4608936
41 I = 51
38816
XDOT = -3017
586669 Wp = 182
04004
YDOT = 6388
275771 meter/sec RA = 314
84617 deg
ZDOT = 2962
044908 TA = 238
27313
MA = 238
33177
Ha = 223
599 n
mi
Hp = 221
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16341936
32 X = 4955895
78
Y = 694438
37 feet Y = 267225
37 meter
Z = 15121182
44 Z = 4633073
11
XDOT = -9900
218729 XDOT = -3103
186507
YDOT = 20958
910011 feet/sec YDOT = 6354
052668 meter/sec
ZDOT = 9717
995105 ZDOT = 2947
177440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15737477
01 X = 4796782
99
Y = -4101305
93 feet Y = -1250078
05 meter
Z = 15221773
65 Z = 4639596
61
XDOT = -3672
642059 XDOT = -1119
421300
YDOT = 21811
662668 feet/sec YDOT = 6648
194781 meter/sec
ZDOT = 9655
111766 ZDOT = 2942
878066
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
47976666
00016717 00000-0 10270-3 0 9146
2 25544 51
6468 315
1690 0008156 252
3510 107
6751 15
51673251 27771
Satellite: ISS
Catalog Number: 25544
Epoch time: 13126
47976666 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 315
1690 deg
Eccentricity:
0008156
Arg of perigee: 252
3510 deg
Mean anomaly: 107
6751 deg
Mean motion: 15
51673251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 321
Coasting Arc #16 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2013/127/10:13:44
784
Vector Time (MET): N/A
Weight (LBS) : 889111
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4532141
12 A = 6785687
77 meter
Y = -797053
20 meter E =
0004475
Z = -4991103
57 I = 51
36055
XDOT = 3380
804116 Wp = 73
57887
YDOT = -6570
781079 meter/sec RA = 309
85493 deg
ZDOT = -2020
868896 TA = 176
68450
MA = 176
68153
Ha = 223
244 n
mi
Hp = 221
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14869229
39 X = -4498645
57
Y = -2615003
93 feet Y = -847547
22 meter
Z = -16375011
70 Z = -5013039
35
XDOT = 11091
877020 XDOT = 3463
845750
YDOT = -21557
680704 feet/sec YDOT = -6532
510505 meter/sec
ZDOT = -6630
147297 ZDOT = -2004
243167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14851892
37 X = -4526856
79
Y = 2086650
65 feet Y = 636011
12 meter
Z = -16466342
00 Z = -5018941
04
XDOT = 4059
807212 XDOT = 1237
429238
YDOT = -22863
173190 feet/sec YDOT = -6968
695188 meter/sec
ZDOT = -6559
912964 ZDOT = -1999
461471
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
44579862
00016717 00000-0 10270-3 0 9152
2 25544 51
6453 310
3701 0008312 255
9594 104
0633 15
51722182 27925
Satellite: ISS
Catalog Number: 25544
Epoch time: 13127
44579862 = yrday
fracday
Element set: 915
Inclination: 51
6453 deg
RA of node: 310
3701 deg
Eccentricity:
0008312
Arg of perigee: 255
9594 deg
Mean anomaly: 104
0633 deg
Mean motion: 15
51722182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 301
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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