[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 23rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 31215 34 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
126/05:17:59
946 -1
2 6
3 6
3
N/A -5
0 -0
1 215
8
000/00:15:59
892 -3
7 0
2 215
4
Coasting Arc #1 (Orbit 1948)
---------------------------------------
Vector Time (GMT): 2015/113/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2165005
55 A = 6772965
30 meter
Y = -3941181
78 meter E =
0008130
Z = -5072198
77 I = 51
61817
XDOT = 7260
292180 Wp = 77
89484
YDOT = -1684
515153 meter/sec RA = 357
90885 deg
ZDOT = -1790
830080 TA = 174
76964
MA = 174
76114
Ha = 216
470 n
mi
Hp = 213
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7103036
57 X = -2096134
30
Y = -12930386
43 feet Y = -3965007
28 meter
Z = -16641072
08 Z = -5082548
72
XDOT = 23819
856234 XDOT = 7287
288502
YDOT = -5526
624517 feet/sec YDOT = -1603
174903 meter/sec
ZDOT = -5875
426773 ZDOT = -1755
495012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7109065
56 X = 2166843
18
Y = -12870766
33 feet Y = -3923009
58 meter
Z = -16684659
50 Z = -5085484
22
XDOT = 16591
710579 XDOT = 5057
153385
YDOT = 16580
720649 feet/sec YDOT = 5053
803654 meter/sec
ZDOT = -5723
611200 ZDOT = -1744
556694
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 15113
27610912
00016717 00000-0 10270-3 0 9006
2 25544 51
6439 358
3479 0005192 254
6556 105
4024 15
55982538 19499
Satellite: ISS
Catalog Number: 25544
Epoch time: 15113
27610912 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 358
3479 deg
Eccentricity:
0005192
Arg of perigee: 254
6556 deg
Mean anomaly: 105
4024 deg
Mean motion: 15
55982538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1949
Checksum: 319
Coasting Arc #2 (Orbit 1964)
---------------------------------------
Vector Time (GMT): 2015/114/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -427147
35 A = 6772021
80 meter
Y = 4252891
39 meter E =
0002413
Z = 5254766
70 I = 51
58402
XDOT = -7618
688363 Wp = 287
52970
YDOT = 276
971677 meter/sec RA = 352
88669 deg
ZDOT = -843
076687 TA = 170
53690
MA = 170
53235
Ha = 216
199 n
mi
Hp = 213
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1401402
08 X = -500198
34
Y = 13953055
73 feet Y = 4247706
39 meter
Z = 17240048
23 Z = 5252514
17
XDOT = -24995
696729 XDOT = -7617
123903
YDOT = 908
699728 feet/sec YDOT = 191
783258 meter/sec
ZDOT = -2765
999630 ZDOT = -880
083294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12452983
79 X = -3795669
46
Y = 6475866
63 feet Y = 1973844
15 meter
Z = 17229547
33 Z = 5251566
03
XDOT = -14126
216226 XDOT = -4305
670706
YDOT = -19379
667201 feet/sec YDOT = -5906
922563 meter/sec
ZDOT = -2924
697232 ZDOT = -891
447716
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 15114
30368397
00016717 00000-0 10270-3 0 9019
2 25544 51
6440 353
2111 0005308 259
4560 100
5995 15
56049916 19651
Satellite: ISS
Catalog Number: 25544
Epoch time: 15114
30368397 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 353
2111 deg
Eccentricity:
0005308
Arg of perigee: 259
4560 deg
Mean anomaly: 100
5995 deg
Mean motion: 15
56049916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1965
Checksum: 304
Coasting Arc #3 (Orbit 1979)
---------------------------------------
Vector Time (GMT): 2015/115/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2943809
27 A = 6775373
38 meter
Y = -4217186
57 meter E =
0004835
Z = -4415605
32 I = 51
56454
XDOT = 6789
978698 Wp = 140
28355
YDOT = 1246
809908 meter/sec RA = 347
86652 deg
ZDOT = 3334
358675 TA = 163
45136
MA = 163
43558
Ha = 215
979 n
mi
Hp = 213
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9658166
89 X = 3012197
54
Y = -13835913
95 feet Y = -4183884
72 meter
Z = -14486894
10 Z = -4401138
56
XDOT = 22276
832998 XDOT = 6759
334764
YDOT = 4090
583689 feet/sec YDOT = 1322
568641 meter/sec
ZDOT = 10939
496965 ZDOT = 3367
268800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16926469
75 X = 5159187
98
Y = 156243
85 feet Y = 47623
13 meter
Z = -14424042
87 Z = -4396448
27
XDOT = 9268
028220 XDOT = 2824
895001
YDOT = 19361
911514 feet/sec YDOT = 5901
510629 meter/sec
ZDOT = 11080
326620 ZDOT = 3377
283554
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 15115
26699335
00016717 00000-0 10270-3 0 9025
2 25544 51
6442 348
3946 0005405 263
8794 96
1739 15
56107193 19805
Satellite: ISS
Catalog Number: 25544
Epoch time: 15115
26699335 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 348
3946 deg
Eccentricity:
0005405
Arg of perigee: 263
8794 deg
Mean anomaly: 96
1739 deg
Mean motion: 15
56107193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1980
Checksum: 334
Coasting Arc #4 (Orbit 1995)
---------------------------------------
Vector Time (GMT): 2015/116/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4963565
20 A = 6780353
25 meter
Y = 3755580
89 meter E =
0008389
Z = 2677952
45 I = 51
55177
XDOT = -4916
448751 Wp = 111
22332
YDOT = -2792
707929 meter/sec RA = 342
86201 deg
ZDOT = -5185
962751 TA = 38
46937
MA = 38
40960
Ha = 215
805 n
mi
Hp = 213
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16284662
73 X = -5018200
65
Y = 12321459
61 feet Y = 3699769
68 meter
Z = 8785933
24 Z = 2653707
44
XDOT = -16130
081203 XDOT = -4859
663030
YDOT = -9162
427588 feet/sec YDOT = -2847
369574 meter/sec
ZDOT = -17014
313487 ZDOT = -5209
707985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19533942
86 X = -5953945
78
Y = -6104258
77 feet Y = -1860578
07 meter
Z = 8681263
23 Z = 2646049
03
XDOT = -2328
831282 XDOT = -709
827775
YDOT = -16936
558824 feet/sec YDOT = -5162
263130 meter/sec
ZDOT = -17115
546744 ZDOT = -5216
818648
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 15116
29448053
00016717 00000-0 10270-3 0 9039
2 25544 51
6448 343
2570 0005475 268
3320 91
7207 15
56194876 19962
Satellite: ISS
Catalog Number: 25544
Epoch time: 15116
29448053 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 343
2570 deg
Eccentricity:
0005475
Arg of perigee: 268
3320 deg
Mean anomaly: 91
7207 deg
Mean motion: 15
56194876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1996
Checksum: 325
Coasting Arc #5 (Orbit 2010)
---------------------------------------
Vector Time (GMT): 2015/117/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6144151
09 A = 6783080
38 meter
Y = -2833649
98 meter E =
0008820
Z = -390879
26 I = 51
53155
XDOT = 2314
554982 Wp = 13
62096
YDOT = 4197
185352 meter/sec RA = 337
87193 deg
ZDOT = 5990
758409 TA = 342
15467
MA = 342
18562
Ha = 215
635 n
mi
Hp = 213
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20157976
02 X = 6177279
75
Y = -9296751
91 feet Y = -2764756
86 meter
Z = -1282412
26 Z = -360951
38
XDOT = 7593
684324 XDOT = 2238
348007
YDOT = 13770
293149 feet/sec YDOT = 4222
642428 meter/sec
ZDOT = 19654
719189 ZDOT = 6001
816815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19489120
85 X = 5940284
04
Y = 10642443
91 feet Y = 3243816
90 meter
Z = -1153572
92 Z = -351609
03
XDOT = -5824
480960 XDOT = -1775
301797
YDOT = 12787
452487 feet/sec YDOT = 3897
615518 meter/sec
ZDOT = 19701
292897 ZDOT = 6004
954075
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 15117
25770835
00016717 00000-0 10270-3 0 9043
2 25544 51
6447 338
4402 0005570 271
7676 88
2840 15
56262121 20111
Satellite: ISS
Catalog Number: 25544
Epoch time: 15117
25770835 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 338
4402 deg
Eccentricity:
0005570
Arg of perigee: 271
7676 deg
Mean anomaly: 88
2840 deg
Mean motion: 15
56262121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2011
Checksum: 298
Coasting Arc #6 (Orbit 2026)
---------------------------------------
Vector Time (GMT): 2015/118/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6312250
43 A = 6781153
41 meter
Y = 1439176
46 meter E =
0004565
Z = -2006618
86 I = 51
49776
XDOT = 567
520786 Wp = 196
87452
YDOT = -5256
914019 meter/sec RA = 332
88243 deg
ZDOT = -5556
697184 TA = 5
35345
MA = 5
34857
Ha = 215
540 n
mi
Hp = 213
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20709483
02 X = -6318127
02
Y = 4721707
54 feet Y = 1368555
77 meter
Z = -6583395
22 Z = -2037297
13
XDOT = 1861
944835 XDOT = 653
255224
YDOT = -17247
093239 feet/sec YDOT = -5250
088589 meter/sec
ZDOT = -18230
633806 ZDOT = -5553
731706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16349844
43 X = -4983432
58
Y = -13494717
74 feet Y = -4113189
97 meter
Z = -6715168
05 Z = -2046783
22
XDOT = 13889
041172 XDOT = 4233
379749
YDOT = -7764
370562 feet/sec YDOT = -2366
580147 meter/sec
ZDOT = -18216
892669 ZDOT = -5552
508885
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 15118
28510817
00016717 00000-0 10270-3 0 9050
2 25544 51
6456 333
3021 0005685 276
7032 83
3475 15
56330422 20277
Satellite: ISS
Catalog Number: 25544
Epoch time: 15118
28510817 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 333
3021 deg
Eccentricity:
0005685
Arg of perigee: 276
7032 deg
Mean anomaly: 83
3475 deg
Mean motion: 15
56330422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2027
Checksum: 291
Coasting Arc #7 (Orbit 2042)
---------------------------------------
Vector Time (GMT): 2015/119/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5466488
96 A = 6775838
40 meter
Y = 319302
09 meter E =
0005047
Z = 3987569
61 I = 51
45289
XDOT = -3219
346274 Wp = 103
47755
YDOT = 5736
296857 meter/sec RA = 327
87636 deg
ZDOT = 3948
651593 TA = 305
34576
MA = 305
39292
Ha = 215
369 n
mi
Hp = 213
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17934675
07 X = 5443141
85
Y = 1047579
04 feet Y = 380301
66 meter
Z = 13082577
46 Z = 4014068
29
XDOT = -10562
159692 XDOT = -3302
432903
YDOT = 18819
871578 feet/sec YDOT = 5699
831706 meter/sec
ZDOT = 12954
893677 ZDOT = 3932
810306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10313005
85 X = 3143404
18
Y = 14608527
57 feet Y = 4452679
20 meter
Z = 13196084
92 Z = 4022166
68
XDOT = -20285
476615 XDOT = -6183
013272
YDOT = 2664
941474 feet/sec YDOT = 812
274161 meter/sec
ZDOT = 12885
880181 ZDOT = 3927
616279
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 15119
31246260
00016717 00000-0 10270-3 0 9064
2 25544 51
6456 328
1639 0005768 279
9422 80
1081 15
56404995 20437
Satellite: ISS
Catalog Number: 25544
Epoch time: 15119
31246260 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 328
1639 deg
Eccentricity:
0005768
Arg of perigee: 279
9422 deg
Mean anomaly: 80
1081 deg
Mean motion: 15
56404995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2043
Checksum: 315
Coasting Arc #8 (Orbit 2057)
---------------------------------------
Vector Time (GMT): 2015/120/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3806621
17 A = 6771238
63 meter
Y = -2255083
12 meter E =
0008943
Z = -5133578
74 I = 51
41172
XDOT = 5209
428323 Wp = 62
06768
YDOT = -5426
292511 meter/sec RA = 322
84657 deg
ZDOT = -1477
060425 TA = 193
64930
MA = 193
67350
Ha = 215
590 n
mi
Hp = 213
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12488914
58 X = -3756184
04
Y = -7398566
66 feet Y = -2297369
56 meter
Z = -16842449
95 Z = -5151948
16
XDOT = 17091
300273 XDOT = 5276
894340
YDOT = -17802
796952 feet/sec YDOT = -5367
660145 meter/sec
ZDOT = -4845
998771 ZDOT = -1451
589495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2182674
59 X = -665279
22
Y = -14258489
74 feet Y = -4345987
67 meter
Z = -16920735
75 Z = -5157440
26
XDOT = 23590
649307 XDOT = 7190
429909
YDOT = 2017
070319 feet/sec YDOT = 614
803033 meter/sec
ZDOT = -4735
785201 ZDOT = -1443
467329
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 15120
27556738
00016717 00000-0 10270-3 0 9076
2 25544 51
6456 323
3460 0005832 285
0173 75
0335 15
56468115 20584
Satellite: ISS
Catalog Number: 25544
Epoch time: 15120
27556738 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 323
3460 deg
Eccentricity:
0005832
Arg of perigee: 285
0173 deg
Mean anomaly: 75
0335 deg
Mean motion: 15
56468115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2058
Checksum: 304
Coasting Arc #9 (Orbit 2073)
---------------------------------------
Vector Time (GMT): 2015/121/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1647885
24 A = 6770961
87 meter
Y = 4067469
48 meter E =
0004936
Z = 5158860
91 I = 51
38649
XDOT = -6255
985655 Wp = 335
05336
YDOT = 4232
532745 meter/sec RA = 317
80524 deg
ZDOT = -1334
847502 TA = 127
83787
MA = 127
79319
Ha = 215
660 n
mi
Hp = 213
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5406447
63 X = 1577219
13
Y = 13344716
14 feet Y = 4085502
39 meter
Z = 16925396
69 Z = 5166694
27
XDOT = -20524
887319 XDOT = -6296
365587
YDOT = 13886
262287 feet/sec YDOT = 4162
348369 meter/sec
ZDOT = -4379
420937 ZDOT = -1365
336681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6695251
40 X = -2040712
63
Y = 12703306
53 feet Y = 3871967
83 meter
Z = 16958177
67 Z = 5168852
55
XDOT = -22950
246923 XDOT = -6995
235262
YDOT = -6056
926354 feet/sec YDOT = -1846
151153 meter/sec
ZDOT = -4510
898452 ZDOT = -1374
921848
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 15121
30283463
00016717 00000-0 10270-3 0 9084
2 25544 51
6455 318
2074 0006003 289
1887 70
8617 15
56540565 20749
Satellite: ISS
Catalog Number: 25544
Epoch time: 15121
30283463 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 318
2074 deg
Eccentricity:
0006003
Arg of perigee: 289
1887 deg
Mean anomaly: 70
8617 deg
Mean motion: 15
56540565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2074
Checksum: 307
Coasting Arc #10 (Orbit 2088)
---------------------------------------
Vector Time (GMT): 2015/122/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 597930
11 A = 6775214
18 meter
Y = -5403869
04 meter E =
0001249
Z = -4043767
47 I = 51
37853
XDOT = 6246
140063 Wp = 83
38368
YDOT = -2202
161613 meter/sec RA = 312
76968 deg
ZDOT = 3867
601689 TA = 226
81035
MA = 226
82079
Ha = 215
767 n
mi
Hp = 212
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1961712
95 X = 677956
50
Y = -17729229
14 feet Y = -5396735
33 meter
Z = -13266953
65 Z = -4040668
16
XDOT = 20492
585508 XDOT = 6251
513206
YDOT = -7224
939674 feet/sec YDOT = -2132
282971 meter/sec
ZDOT = 12688
981918 ZDOT = 3897
957958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14627898
91 X = 4458583
59
Y = -10226355
13 feet Y = -3116993
04 meter
Z = -13252629
05 Z = -4039401
33
XDOT = 18196
969003 XDOT = 5546
436152
YDOT = 9420
995335 feet/sec YDOT = 2871
519378 meter/sec
ZDOT = 12819
489033 ZDOT = 3907
380257
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 15122
26585726
00016717 00000-0 10270-3 0 9098
2 25544 51
6456 313
3884 0006032 293
1982 66
8536 15
56599857 20897
Satellite: ISS
Catalog Number: 25544
Epoch time: 15122
26585726 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 313
3884 deg
Eccentricity:
0006032
Arg of perigee: 293
1982 deg
Mean anomaly: 66
8536 deg
Mean motion: 15
56599857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2089
Checksum: 349
Coasting Arc #11 (Orbit 2104)
---------------------------------------
Vector Time (GMT): 2015/123/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2585647
70 A = 6780347
85 meter
Y = 5938940
59 meter E =
0007896
Z = 1992456
30 I = 51
37537
XDOT = -5277
003959 Wp = 107
84848
YDOT = -429
789697 meter/sec RA = 307
75440 deg
ZDOT = -5551
201825 TA = 50
04514
MA = 49
97580
Ha = 215
900 n
mi
Hp = 212
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8483096
12 X = -2661544
99
Y = 19484713
22 feet Y = 5909601
88 meter
Z = 6536930
11 Z = 1979710
93
XDOT = -17313
005114 XDOT = -5244
839513
YDOT = -1410
071185 feet/sec YDOT = -488
620926 meter/sec
ZDOT = -18212
604413 ZDOT = -5576
758893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20122062
44 X = -6133204
63
Y = 6888064
58 feet Y = 2099482
09 meter
Z = 6481172
26 Z = 1975461
30
XDOT = -10081
013554 XDOT = -3072
692931
YDOT = -12160
744349 feet/sec YDOT = -3706
594877 meter/sec
ZDOT = -18322
034260 ZDOT = -5584
556042
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 15123
29303739
00016717 00000-0 10270-3 0 9106
2 25544 51
6457 308
2486 0006110 297
1870 62
8660 15
56650851 21051
Satellite: ISS
Catalog Number: 25544
Epoch time: 15123
29303739 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 308
2486 deg
Eccentricity:
0006110
Arg of perigee: 297
1870 deg
Mean anomaly: 62
8660 deg
Mean motion: 15
56650851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2105
Checksum: 301
Coasting Arc #12 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2015/124/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3997583
10 A = 6781697
41 meter
Y = -5443158
98 meter E =
0012514
Z = 521987
53 I = 51
36207
XDOT = 3599
797935 Wp = 22
19186
YDOT = 3219
311402 meter/sec RA = 302
75213 deg
ZDOT = 5966
124519 TA = 343
47004
MA = 343
51081
Ha = 215
990 n
mi
Hp = 212
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13115430
11 X = 4055617
01
Y = -17858133
14 feet Y = -5398130
90 meter
Z = 1712557
50 Z = 541548
46
XDOT = 11810
360679 XDOT = 3534
549442
YDOT = 10562
045283 feet/sec YDOT = 3259
201930 meter/sec
ZDOT = 19573
899342 ZDOT = 5983
453508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21973586
09 X = 6697549
04
Y = -2791249
54 feet Y = -850772
86 meter
Z = 1797420
29 Z = 547853
70
XDOT = 180
704087 XDOT = 55
078606
YDOT = 14145
857137 feet/sec YDOT = 4311
657255 meter/sec
ZDOT = 19647
534785 ZDOT = 5988
568603
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 15124
32017182
00016717 00000-0 10270-3 0 9116
2 25544 51
6459 303
1079 0006295 302
2084 57
8459 15
56715225 21219
Satellite: ISS
Catalog Number: 25544
Epoch time: 15124
32017182 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 303
1079 deg
Eccentricity:
0006295
Arg of perigee: 302
2084 deg
Mean anomaly: 57
8459 deg
Mean motion: 15
56715225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 289
Coasting Arc #13 (Orbit 2135)
---------------------------------------
Vector Time (GMT): 2015/125/06:10:07
284
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4707373
86 A = 6777843
62 meter
Y = 3888494
55 meter E =
0002278
Z = -2944373
51 I = 51
33440
XDOT = -1536
444215 Wp = 332
13331
YDOT = -5629
398968 meter/sec RA = 297
74432 deg
ZDOT = -4974
520676 TA = 241
66720
MA = 241
69018
Ha = 216
087 n
mi
Hp = 212
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15444139
97 X = -4736203
10
Y = 12757528
06 feet Y = 3835692
45 meter
Z = -9660018
09 Z = -2967311
51
XDOT = -5040
827478 XDOT = -1449
215864
YDOT = -18469
156718 feet/sec YDOT = -5646
092725 meter/sec
ZDOT = -16320
605893 ZDOT = -4981
772761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19880282
71 X = -6059510
17
Y = -2031557
45 feet Y = -619218
71 meter
Z = -9759050
41 Z = -2974558
56
XDOT = 9566
620897 XDOT = 2915
906050
YDOT = -15017
334711 feet/sec YDOT = -4577
283620 meter/sec
ZDOT = -16350
602914 ZDOT = -4983
663768
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 15125
28306764
00016717 00000-0 10270-3 0 9120
2 25544 51
6467 298
2889 0006441 305
1259 54
9291 15
56789057 21362
Satellite: ISS
Catalog Number: 25544
Epoch time: 15125
28306764 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 298
2889 deg
Eccentricity:
0006441
Arg of perigee: 305
1259 deg
Mean anomaly: 54
9291 deg
Mean motion: 15
56789057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2136
Checksum: 336
Coasting Arc #14 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2015/126/05:25:59
892
Vector Time (MET): N/A
Weight (LBS) : 923014
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4564794
61 A = 6774492
93 meter
Y = 558436
43 meter E =
0005250
Z = -4978918
84 I = 51
29752
XDOT = 1313
619311 Wp = 49
54353
YDOT = -7278
705219 meter/sec RA = 292
86249 deg
ZDOT = -2018
798954 TA = 200
72673
MA = 200
74803
Ha = 215
805 n
mi
Hp = 215
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14976360
28 X = -4546513
72
Y = 1832140
51 feet Y = 507492
25 meter
Z = -16335035
57 Z = -5001049
75
XDOT = 4309
774641 XDOT = 1404
720656
YDOT = -23880
266465 feet/sec YDOT = -7263
506043 meter/sec
ZDOT = -6623
356148 ZDOT = -2012
196415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9916990
63 X = -3022698
75
Y = -11233466
56 feet Y = -3423960
61 meter
Z = -16429973
19 Z = -5007855
83
XDOT = 21340
223317 XDOT = 6504
500067
YDOT = -9186
201559 feet/sec YDOT = -2799
954235 meter/sec
ZDOT = -6593
676225 ZDOT = -2009
752513
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 15126
24593798
00016717 00000-0 10270-3 0 9133
2 25544 51
6464 293
4693 0008358 270
7909 89
2287 15
55570119 21516
Satellite: ISS
Catalog Number: 25544
Epoch time: 15126
24593798 = yrday
fracday
Element set: 913
Inclination: 51
6464 deg
RA of node: 293
4693 deg
Eccentricity:
0008358
Arg of perigee: 270
7909 deg
Mean anomaly: 89
2287 deg
Mean motion: 15
55570119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 343
Coasting Arc #15 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2015/127/05:25:59
892
Vector Time (MET): N/A
Weight (LBS) : 923014
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3875482
51 A = 6773000
17 meter
Y = 1759438
81 meter E =
0006227
Z = 5273962
83 I = 51
28169
XDOT = -2669
278196 Wp = 284
90798
YDOT = 7174
180560 meter/sec RA = 287
82297 deg
ZDOT = -430
746248 TA = 169
22807
MA = 169
21472
Ha = 216
704 n
mi
Hp = 216
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12714837
65 X = 3829900
65
Y = 5772437
05 feet Y = 1802521
94 meter
Z = 17303027
67 Z = 5292678
84
XDOT = -8757
474395 XDOT = -2747
210764
YDOT = 23537
337795 feet/sec YDOT = 7143
895215 meter/sec
ZDOT = -1413
209475 ZDOT = -443
902343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2596680
06 X = 791468
08
Y = 13618924
93 feet Y = 4151048
32 meter
Z = 17382894
72 Z = 5298306
31
XDOT = -23259
703728 XDOT = -7089
557696
YDOT = 6317
124299 feet/sec YDOT = 1925
459486 meter/sec
ZDOT = -1470
946012 ZDOT = -448
344344
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 15127
27380752
00016717 00000-0 10270-3 0 9142
2 25544 51
6463 288
3341 0008580 274
9939 85
0235 15
55646488 21671
Satellite: ISS
Catalog Number: 25544
Epoch time: 15127
27380752 = yrday
fracday
Element set: 914
Inclination: 51
6463 deg
RA of node: 288
3341 deg
Eccentricity:
0008580
Arg of perigee: 274
9939 deg
Mean anomaly: 85
0235 deg
Mean motion: 15
55646488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 337
Coasting Arc #16 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2015/128/05:25:59
892
Vector Time (MET): N/A
Weight (LBS) : 923014
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2934366
52 A = 6775516
82 meter
Y = -3950166
38 meter E =
0002655
Z = -4659977
13 I = 51
28212
XDOT = 3705
605465 Wp = 143
26573
YDOT = -6089
158364 meter/sec RA = 282
78453 deg
ZDOT = 2826
996443 TA = 154
93773
MA = 154
92484
Ha = 216
860 n
mi
Hp = 215
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9627186
73 X = -2867340
01
Y = -12959863
44 feet Y = -3982605
43 meter
Z = -15288638
88 Z = -4674069
25
XDOT = 12157
498245 XDOT = 3759
687805
YDOT = -19977
553689 feet/sec YDOT = -6047
417582 meter/sec
ZDOT = 9274
922714 ZDOT = 2845
128913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4779294
10 X = 1456728
84
Y = -15361373
13 feet Y = -4682146
53 meter
Z = -15348284
17 Z = -4678157
02
XDOT = 22138
625858 XDOT = 6747
853162
YDOT = -2462
037939 feet/sec YDOT = -750
429164 meter/sec
ZDOT = 9353
773240 ZDOT = 2851
030083
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 15128
23739728
00016717 00000-0 10270-3 0 9151
2 25544 51
6468 283
5196 0008605 279
5891 80
4290 15
55682841 21827
Satellite: ISS
Catalog Number: 25544
Epoch time: 15128
23739728 = yrday
fracday
Element set: 915
Inclination: 51
6468 deg
RA of node: 283
5196 deg
Eccentricity:
0008605
Arg of perigee: 279
5891 deg
Mean anomaly: 80
4290 deg
Mean motion: 15
55682841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 342
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