[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 26th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 ET - UTC (sec) : 68 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
217/02:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 212
7
220/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 1093)
---------------------------------------
Vector Time (GMT): 2016/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4250908
70 A = 6776141
49 meter
Y = 1459546
01 meter E =
0015096
Z = -5084605
44 I = 51
35579
XDOT = -4151
423623 Wp = 99
13239
YDOT = -6209
420731 meter/sec RA = 225
81041 deg
ZDOT = 1690
265431 TA = 187
27142
MA = 187
29334
Ha = 220
508 n
mi
Hp = 212
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13946550
86 X = -4242215
23
Y = 4788536
76 feet Y = 1412058
20 meter
Z = -16681776
38 Z = -5105233
92
XDOT = -13620
156244 XDOT = -4089
890264
YDOT = -20372
115260 feet/sec YDOT = -6255
500699 meter/sec
ZDOT = 5545
490260 ZDOT = 1670
248418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11516155
60 X = 3510124
23
Y = 9044211
21 feet Y = 2756675
58 meter
Z = -16771953
74 Z = -5112091
50
XDOT = -9076
897441 XDOT = -2766
638340
YDOT = 21669
844067 feet/sec YDOT = 6604
968471 meter/sec
ZDOT = 5459
276494 ZDOT = 1663
987475
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 16207
51321548
00016717 00000-0 10270-3 0 9002
2 25544 51
6423 226
8128 0001897 71
2906 288
8452 15
54860792 10940
Satellite: ISS
Catalog Number: 25544
Epoch time: 16207
51321548 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 226
8128 deg
Eccentricity:
0001897
Arg of perigee: 71
2906 deg
Mean anomaly: 288
8452 deg
Mean motion: 15
54860792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1094
Checksum: 316
Coasting Arc #2 (Orbit 1109)
---------------------------------------
Vector Time (GMT): 2016/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5327856
50 A = 6779513
27 meter
Y = 188184
83 meter E =
0012198
Z = 4180092
41 I = 51
38899
XDOT = 2673
898931 Wp = 74
60329
YDOT = 6183
090134 meter/sec RA = 220
79122 deg
ZDOT = -3674
308324 TA = 53
24449
MA = 53
13256
Ha = 220
387 n
mi
Hp = 212
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17479844
18 X = 5305051
27
Y = 617404
30 feet Y = 247636
86 meter
Z = 13714213
93 Z = 4205918
21
XDOT = 8772
634289 XDOT = 2622
407396
YDOT = 20285
728787 feet/sec YDOT = 6212
703649 meter/sec
ZDOT = -12054
817336 ZDOT = -3661
444194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9149999
73 X = -2788919
92
Y = -14802144
01 feet Y = -4511693
49 meter
Z = 13826779
89 Z = 4214402
51
XDOT = 10866
476354 XDOT = 3312
101993
YDOT = -17963
132078 feet/sec YDOT = -5475
162657 meter/sec
ZDOT = -11999
770067 ZDOT = -3657
529917
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 16208
54154936
00016717 00000-0 10270-3 0 9012
2 25544 51
6406 221
6810 0002072 73
9819 286
1562 15
54909039 11100
Satellite: ISS
Catalog Number: 25544
Epoch time: 16208
54154936 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 221
6810 deg
Eccentricity:
0002072
Arg of perigee: 73
9819 deg
Mean anomaly: 286
1562 deg
Mean motion: 15
54909039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1110
Checksum: 296
Coasting Arc #3 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2016/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5991189
31 A = 6783829
77 meter
Y = -1632451
66 meter E =
0006730
Z = -2732732
67 I = 51
42839
XDOT = -803
619146 Wp = 65
26334
YDOT = -5630
550389 meter/sec RA = 215
78745 deg
ZDOT = 5138
090376 TA = 263
72563
MA = 263
80230
Ha = 220
489 n
mi
Hp = 212
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19656132
92 X = -5959215
20
Y = -5355812
54 feet Y = -1699270
25 meter
Z = -8965658
36 Z = -2761758
59
XDOT = -2636
545753 XDOT = -765
555654
YDOT = -18472
934346 feet/sec YDOT = -5639
324388 meter/sec
ZDOT = 16857
251889 ZDOT = 5134
278831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6767899
87 X = 2062855
88
Y = 19156287
10 feet Y = 5838836
31 meter
Z = -9091947
82 Z = -2771225
70
XDOT = -12216
204700 XDOT = -3723
499192
YDOT = 12289
764744 feet/sec YDOT = 3745
920294 meter/sec
ZDOT = 16841
573328 ZDOT = 5133
311550
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 16209
50561153
00016717 00000-0 10270-3 0 9023
2 25544 51
6406 216
8707 0002055 79
0026 281
1358 15
54898326 11259
Satellite: ISS
Catalog Number: 25544
Epoch time: 16209
50561153 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 216
8707 deg
Eccentricity:
0002055
Arg of perigee: 79
0026 deg
Mean anomaly: 281
1358 deg
Mean motion: 15
54898326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 296
Coasting Arc #4 (Orbit 1140)
---------------------------------------
Vector Time (GMT): 2016/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6100248
15 A = 6786744
03 meter
Y = 2828679
57 meter E =
0014998
Z = 870614
86 I = 51
46389
XDOT = -1323
950743 Wp = 119
78660
YDOT = 4697
927329 meter/sec RA = 210
79613 deg
ZDOT = -5917
817194 TA = 50
76532
MA = 50
63230
Ha = 220
537 n
mi
Hp = 212
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20013937
49 X = 6063934
72
Y = 9280444
78 feet Y = 2896693
52 meter
Z = 2856347
97 Z = 900160
10
XDOT = -4343
670416 XDOT = -1347
639754
YDOT = 15413
147405 feet/sec YDOT = 4682
989929 meter/sec
ZDOT = -19415
410743 ZDOT = -5924
305827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4142975
96 X = -1262779
07
Y = -21651103
32 feet Y = -6599256
29 meter
Z = 2984719
10 Z = 909742
38
XDOT = 13394
927469 XDOT = 4082
773892
YDOT = -5273
677874 feet/sec YDOT = -1607
417016 meter/sec
ZDOT = -19444
488383 ZDOT = -5926
680059
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 16210
53394087
00016717 00000-0 10270-3 0 9039
2 25544 51
6398 211
7381 0002100 79
0055 281
1335 15
54898221 11411
Satellite: ISS
Catalog Number: 25544
Epoch time: 16210
53394087 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 211
7381 deg
Eccentricity:
0002100
Arg of perigee: 79
0055 deg
Mean anomaly: 281
1335 deg
Mean motion: 15
54898221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1141
Checksum: 284
Coasting Arc #5 (Orbit 1156)
---------------------------------------
Vector Time (GMT): 2016/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5605804
45 A = 6786517
36 meter
Y = -3659120
77 meter E =
0015312
Z = 1072155
46 I = 51
49070
XDOT = 3439
967383 Wp = 60
40000
YDOT = -3531
468296 meter/sec RA = 205
81242 deg
ZDOT = 5877
792826 TA = 311
25967
MA = 311
39147
Ha = 220
439 n
mi
Hp = 212
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18391746
89 X = -5569678
62
Y = -12004989
41 feet Y = -3721606
71 meter
Z = 3517570
41 Z = 1045011
61
XDOT = 11285
982227 XDOT = 3450
649989
YDOT = -11586
182074 feet/sec YDOT = -3492
940977 meter/sec
ZDOT = 19284
097197 ZDOT = 5894
528854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1386061
40 X = 422471
51
Y = 21937859
53 feet Y = 6686659
59 meter
Z = 3399790
99 Z = 1036256
29
XDOT = -14359
134421 XDOT = -4376
664172
YDOT = -2122
047241 feet/sec YDOT = -646
799999 meter/sec
ZDOT = 19357
675426 ZDOT = 5900
219470
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 16211
56226486
00016717 00000-0 10270-3 0 9041
2 25544 51
6389 206
6069 0001960 87
0700 273
0677 15
54940876 11576
Satellite: ISS
Catalog Number: 25544
Epoch time: 16211
56226486 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 206
6069 deg
Eccentricity:
0001960
Arg of perigee: 87
0700 deg
Mean anomaly: 273
0677 deg
Mean motion: 15
54940876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1157
Checksum: 321
Coasting Arc #6 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2016/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4481390
52 A = 6783585
46 meter
Y = 4180748
08 meter E =
0006443
Z = -2910687
49 I = 51
50889
XDOT = -5341
509858 Wp = 106
96081
YDOT = 2238
720914 meter/sec RA = 200
82393 deg
ZDOT = -5019
443164 TA = 106
27598
MA = 106
20510
Ha = 220
568 n
mi
Hp = 212
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14702724
82 X = 4448445
95
Y = 13716365
10 feet Y = 4230678
00 meter
Z = -9549499
64 Z = -2888998
02
XDOT = -17524
638643 XDOT = -5341
764860
YDOT = 7344
884890 feet/sec YDOT = 2178
987537 meter/sec
ZDOT = -16467
989382 ZDOT = -5045
390973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1822553
25 X = 555514
23
Y = -20069182
14 feet Y = -6117086
71 meter
Z = -9455578
25 Z = -2882060
25
XDOT = 14998
645336 XDOT = 4571
587098
YDOT = 9157
208413 feet/sec YDOT = 2791
117124 meter/sec
ZDOT = -16581
544938 ZDOT = -5054
054897
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 16212
52632088
00016717 00000-0 10270-3 0 9058
2 25544 51
6380 201
7948 0002048 84
1947 275
9439 15
54891492 11721
Satellite: ISS
Catalog Number: 25544
Epoch time: 16212
52632088 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 201
7948 deg
Eccentricity:
0002048
Arg of perigee: 84
1947 deg
Mean anomaly: 275
9439 deg
Mean motion: 15
54891492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 323
Coasting Arc #7 (Orbit 1187)
---------------------------------------
Vector Time (GMT): 2016/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2854922
00 A = 6779170
96 meter
Y = -4373132
38 meter E =
0011555
Z = 4314449
76 I = 51
52523
XDOT = 6766
131694 Wp = 104
79246
YDOT = -964
210257 meter/sec RA = 195
82620 deg
ZDOT = 3489
192599 TA = 309
64971
MA = 309
75160
Ha = 220
478 n
mi
Hp = 212
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9366541
98 X = -2826765
70
Y = -14347547
19 feet Y = -4404900
90 meter
Z = 14155018
88 Z = 4300649
59
XDOT = 22198
594796 XDOT = 6759
462179
YDOT = -3163
419477 feet/sec YDOT = -888
584390 meter/sec
ZDOT = 11447
482280 ZDOT = 3522
043916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5286269
41 X = -1611254
92
Y = 16349929
04 feet Y = 4983458
37 meter
Z = 14095529
61 Z = 4296317
42
XDOT = -15105
490419 XDOT = -4604
153480
YDOT = -14907
090830 feet/sec YDOT = -4543
681285 meter/sec
ZDOT = 11590
962367 ZDOT = 3532
925329
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 16213
55464052
00016717 00000-0 10270-3 0 9067
2 25544 51
6383 196
6631 0001838 87
7076 272
4287 15
54924568 11884
Satellite: ISS
Catalog Number: 25544
Epoch time: 16213
55464052 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 196
6631 deg
Eccentricity:
0001838
Arg of perigee: 87
7076 deg
Mean anomaly: 272
4287 deg
Mean motion: 15
54924568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1188
Checksum: 335
Coasting Arc #8 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2016/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 850824
53 A = 6775866
24 meter
Y = 4330678
46 meter E =
0015698
Z = -5155342
49 I = 51
54545
XDOT = -7513
503767 Wp = 80
14518
YDOT = -257
270453 meter/sec RA = 190
81632 deg
ZDOT = -1457
287680 TA = 175
79729
MA = 175
78409
Ha = 220
524 n
mi
Hp = 212
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2791419
05 X = 827376
45
Y = 14208262
67 feet Y = 4340062
14 meter
Z = -16913853
33 Z = -5151266
19
XDOT = -24650
602909 XDOT = -7502
989764
YDOT = -844
063167 feet/sec YDOT = -341
232598 meter/sec
ZDOT = -4781
127560 ZDOT = -1493
760100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9083012
01 X = 2768502
06
Y = -11302351
77 feet Y = -3444956
82 meter
Z = -16896772
47 Z = -5150136
25
XDOT = 14242
999008 XDOT = 4341
266098
YDOT = 18826
065160 feet/sec YDOT = 5738
184661 meter/sec
ZDOT = -4940
229651 ZDOT = -1505
781998
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 16214
51868879
00016717 00000-0 10270-3 0 9070
2 25544 51
6385 191
8509 0002017 87
3686 272
7698 15
54899235 12039
Satellite: ISS
Catalog Number: 25544
Epoch time: 16214
51868879 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 191
8509 deg
Eccentricity:
0002017
Arg of perigee: 87
3686 deg
Mean anomaly: 272
7698 deg
Mean motion: 15
54899235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 353
Coasting Arc #9 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2016/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1282462
16 A = 6775262
51 meter
Y = -4065565
87 meter E =
0004859
Z = 5262109
85 I = 51
57521
XDOT = 7510
475575 Wp = 73
65631
YDOT = 1374
540842 meter/sec RA = 185
80340 deg
ZDOT = -766
513368 TA = 23
68024
MA = 23
65789
Ha = 220
439 n
mi
Hp = 212
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4207553
03 X = 1302268
57
Y = -13338470
71 feet Y = -4051113
99 meter
Z = 17264139
91 Z = 5268387
52
XDOT = 24640
667896 XDOT = 7498
270226
YDOT = 4509
648431 feet/sec YDOT = 1458
459783 meter/sec
ZDOT = -2514
807637 ZDOT = -730
059798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12786065
43 X = -3897192
74
Y = 5582597
53 feet Y = 1701575
73 meter
Z = 17292193
78 Z = 5270660
66
XDOT = -12237
131082 XDOT = -3729
877554
YDOT = -20710
104649 feet/sec YDOT = -6312
439897 meter/sec
ZDOT = -2355
945563 ZDOT = -718
092208
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 16215
54700408
00016717 00000-0 10270-3 0 9088
2 25544 51
6383 186
7191 0001910 90
4058 269
7314 15
54902579 12190
Satellite: ISS
Catalog Number: 25544
Epoch time: 16215
54700408 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 186
7191 deg
Eccentricity:
0001910
Arg of perigee: 90
4058 deg
Mean anomaly: 269
7314 deg
Mean motion: 15
54902579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 312
Coasting Arc #10 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2016/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3308587
82 A = 6777784
05 meter
Y = 3650781
30 meter E =
0012511
Z = -4666494
65 I = 51
61686
XDOT = -6685
893798 Wp = 107
37128
YDOT = -2377
078595 meter/sec RA = 180
79582 deg
ZDOT = 2883
416663 TA = 191
31639
MA = 191
34454
Ha = 220
469 n
mi
Hp = 212
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10854946
92 X = -3326498
60
Y = 11977628
93 feet Y = 3613682
41 meter
Z = -15310021
82 Z = -4682609
99
XDOT = -21935
347107 XDOT = -6672
821862
YDOT = -7798
814289 feet/sec YDOT = -2451
771694 meter/sec
ZDOT = 9460
028421 ZDOT = 2850
970736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16096908
54 X = 4906337
72
Y = 79253
06 feet Y = 24156
33 meter
Z = -15380945
68 Z = -4688112
24
XDOT = 8795
108091 XDOT = 2680
748946
YDOT = 20445
186893 feet/sec YDOT = 6231
692965 meter/sec
ZDOT = 9318
797015 ZDOT = 2840
369330
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 16216
51104640
00016717 00000-0 10270-3 0 9093
2 25544 51
6393 181
9079 0001886 92
4584 267
6785 15
54898918 12348
Satellite: ISS
Catalog Number: 25544
Epoch time: 16216
51104640 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 181
9079 deg
Eccentricity:
0001886
Arg of perigee: 92
4584 deg
Mean anomaly: 267
6785 deg
Mean motion: 15
54898918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 345
Coasting Arc #11 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3171434
87 A = 6777429
00 meter
Y = -3642044
80 meter E =
0009611
Z = 4749510
98 I = 51
63898
XDOT = 6779
293099 Wp = 116
39108
YDOT = -2385
813395 meter/sec RA = 177
83681 deg
ZDOT = 2688
905432 TA = 307
02022
MA = 307
10812
Ha = 220
445 n
mi
Hp = 212
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10404970
03 X = -3153543
44
Y = -11948965
87 feet Y = -3677409
90 meter
Z = 15582385
11 Z = 4734148
73
XDOT = 22241
775258 XDOT = 6792
406778
YDOT = -7827
471769 feet/sec YDOT = -2309
929507 meter/sec
ZDOT = 8821
868216 ZDOT = 2721
868611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7909416
45 X = -2410790
13
Y = -13803965
65 feet Y = -4207448
73 meter
Z = 15515913
65 Z = 4729250
48
XDOT = 22293
474063 XDOT = 6795
050895
YDOT = -2664
566205 feet/sec YDOT = -812
159779 meter/sec
ZDOT = 8966
131753 ZDOT = 2732
876958
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 16217
15373813
00016717 00000-0 10270-3 0 9106
2 25544 51
6430 178
6971 0001868 109
7163 250
4192 15
54951407 12445
Satellite: ISS
Catalog Number: 25544
Epoch time: 16217
15373813 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 178
6971 deg
Eccentricity:
0001868
Arg of perigee: 109
7163 deg
Mean anomaly: 250
4192 deg
Mean motion: 15
54951407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 305
Coasting Arc #12 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2016/218/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1117157
20 A = 6775156
61 meter
Y = 4085504
65 meter E =
0016392
Z = -5302231
45 I = 51
66335
XDOT = -7515
836553 Wp = 88
61449
YDOT = 1367
925772 meter/sec RA = 172
83313 deg
ZDOT = -530
564230 TA = 176
32395
MA = 176
31189
Ha = 220
388 n
mi
Hp = 212
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3665213
90 X = 1097144
43
Y = 13403886
64 feet Y = 4097885
49 meter
Z = -17395772
47 Z = -5296853
35
XDOT = -24658
256407 XDOT = -7527
997257
YDOT = 4487
945447 feet/sec YDOT = 1283
810664 meter/sec
ZDOT = -1740
696293 ZDOT = -567
103058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1265252
33 X = 385648
91
Y = 13866893
47 feet Y = 4226629
13 meter
Z = -17372946
55 Z = -5295274
11
XDOT = -24040
385464 XDOT = -7327
509490
YDOT = -183
160829 feet/sec YDOT = -55
827421 meter/sec
ZDOT = -1900
420864 ZDOT = -579
248279
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 16218
11777618
00016717 00000-0 10270-3 0 9115
2 25544 51
6430 173
8871 0001827 109
9320 250
2030 15
54922923 12599
Satellite: ISS
Catalog Number: 25544
Epoch time: 16218
11777618 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 173
8871 deg
Eccentricity:
0001827
Arg of perigee: 109
9320 deg
Mean anomaly: 250
2030 deg
Mean motion: 15
54922923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 298
Coasting Arc #13 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2016/219/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1020172
79 A = 6775827
37 meter
Y = -4339453
56 meter E =
0006206
Z = 5098480
26 I = 51
69820
XDOT = 7479
540250 Wp = 69
76017
YDOT = -241
247373 meter/sec RA = 167
82798 deg
ZDOT = -1698
166246 TA = 36
64033
MA = 36
59791
Ha = 220
295 n
mi
Hp = 212
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3347023
57 X = 1043856
07
Y = -14237052
37 feet Y = -4327912
76 meter
Z = 16727297
43 Z = 5103493
54
XDOT = 24539
174048 XDOT = 7489
930855
YDOT = -791
494007 feet/sec YDOT = -157
548098 meter/sec
ZDOT = -5571
411567 ZDOT = -1661
807938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5553862
94 X = 1692817
42
Y = -13501666
33 feet Y = -4115307
90 meter
Z = 16749875
19 Z = 5105361
96
XDOT = 23381
393887 XDOT = 7126
648857
YDOT = 2887
714454 feet/sec YDOT = 880
175366 meter/sec
ZDOT = -5412
638705 ZDOT = -1649
772277
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 16219
14607955
00016717 00000-0 10270-3 0 9126
2 25544 51
6432 168
7549 0001814 113
1521 246
9824 15
54959501 12755
Satellite: ISS
Catalog Number: 25544
Epoch time: 16219
14607955 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 168
7549 deg
Eccentricity:
0001814
Arg of perigee: 113
1521 deg
Mean anomaly: 246
9824 deg
Mean motion: 15
54959501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 315
Coasting Arc #14 (Orbit 1289)
---------------------------------------
Vector Time (GMT): 2016/220/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2992263
47 A = 6779334
20 meter
Y = 4399990
59 meter E =
0009914
Z = -4211105
08 I = 51
74129
XDOT = -6641
471729 Wp = 111
69872
YDOT = -991
297031 meter/sec RA = 162
83342 deg
ZDOT = 3686
829932 TA = 196
08591
MA = 196
11741
Ha = 220
310 n
mi
Hp = 212
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9817137
38 X = -3020787
47
Y = 14435664
65 feet Y = 4366369
48 meter
Z = -13815961
55 Z = -4225709
94
XDOT = -21789
605409 XDOT = -6647
801948
YDOT = -3252
286847 feet/sec YDOT = -1065
601692 meter/sec
ZDOT = 12095
898727 ZDOT = 3654
552472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11766955
59 X = -3586568
07
Y = 12826449
23 feet Y = 3909501
73 meter
Z = -13880430
47 Z = -4230755
21
XDOT = -20204
899265 XDOT = -6158
453296
YDOT = -5610
416131 feet/sec YDOT = -1710
054837 meter/sec
ZDOT = 11955
124825 ZDOT = 3643
922047
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 16220
11011144
00016717 00000-0 10270-3 0 9135
2 25544 51
6432 163
9448 0001851 116
6687 243
4656 15
54958219 12909
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
11011144 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 163
9448 deg
Eccentricity:
0001851
Arg of perigee: 116
6687 deg
Mean anomaly: 243
4656 deg
Mean motion: 15
54958219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1290
Checksum: 298
Coasting Arc #15 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2016/220/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3973239
88 A = 6777322
34 meter
Y = -2683776
20 meter E =
0009561
Z = 4784215
12 I = 51
73760
XDOT = 5936
778859 Wp = 116
11625
YDOT = -4090
742607 meter/sec RA = 162
13523 deg
ZDOT = 2627
487443 TA = 307
98606
MA = 308
07238
Ha = 220
539 n
mi
Hp = 212
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13035563
92 X = -3966173
23
Y = -8805040
02 feet Y = -2728167
97 meter
Z = 15696243
83 Z = 4764931
64
XDOT = 19477
620927 XDOT = 5969
318331
YDOT = -13421
071544 feet/sec YDOT = -4024
171559 meter/sec
ZDOT = 8620
365627 ZDOT = 2656
405558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15495670
49 X = -4723080
37
Y = 3156199
81 feet Y = 962009
70 meter
Z = 15612473
40 Z = 4758681
89
XDOT = 4335
453722 XDOT = 1321
446295
YDOT = -22117
513907 feet/sec YDOT = -6741
418239 meter/sec
ZDOT = 8747
282522 ZDOT = 2666
171713
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 16220
30291737
00016717 00000-0 10270-3 0 9145
2 25544 51
6421 162
9835 0002009 106
3969 253
7406 15
54947024 12933
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
30291737 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 162
9835 deg
Eccentricity:
0002009
Arg of perigee: 106
3969 deg
Mean anomaly: 253
7406 deg
Mean motion: 15
54947024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 302
Coasting Arc #16 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2016/221/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2099089
72 A = 6775106
96 meter
Y = 3660317
35 meter E =
0016516
Z = -5315019
09 I = 51
76143
XDOT = -6896
738503 Wp = 89
25335
YDOT = 3296
656136 meter/sec RA = 157
13730 deg
ZDOT = -454
454544 TA = 176
41927
MA = 176
40743
Ha = 220
405 n
mi
Hp = 212
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6886777
29 X = 2083820
88
Y = 12008915
20 feet Y = 3683705
25 meter
Z = -17437726
66 Z = -5304859
54
XDOT = -22627
094827 XDOT = -6930
882449
YDOT = 10815
800970 feet/sec YDOT = 3219
341272 meter/sec
ZDOT = -1490
992598 ZDOT = -488
039797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13518111
10 X = 4120320
26
Y = 3229137
42 feet Y = 984241
08 meter
Z = -17393947
24 Z = -5301675
12
XDOT = -7559
856564 XDOT = -2304
244281
YDOT = 22841
523373 feet/sec YDOT = 6962
096324 meter/sec
ZDOT = -1638
176663 ZDOT = -499
316247
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 16221
26694495
00016717 00000-0 10270-3 0 9150
2 25544 51
6430 158
1727 0001908 110
1563 249
9796 15
54930215 13080
Satellite: ISS
Catalog Number: 25544
Epoch time: 16221
26694495 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 158
1727 deg
Eccentricity:
0001908
Arg of perigee: 110
1563 deg
Mean anomaly: 249
9796 deg
Mean motion: 15
54930215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 314
Coasting Arc #17 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2016/222/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -100490
93 A = 6775906
77 meter
Y = -4473234
07 meter E =
0006568
Z = 5083778
62 I = 51
79206
XDOT = 7136
779586 Wp = 70
22472
YDOT = -2187
754864 meter/sec RA = 152
13910 deg
ZDOT = -1779
905216 TA = 36
96625
MA = 36
92101
Ha = 220
394 n
mi
Hp = 212
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -329694
64 X = -75157
19
Y = -14675964
78 feet Y = -4474216
06 meter
Z = 16679063
71 Z = 5083352
10
XDOT = 23414
631188 XDOT = 7169
359124
YDOT = -7177
673437 feet/sec YDOT = -2107
764500 meter/sec
ZDOT = -5839
584043 ZDOT = -1745
157683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11083171
28 X = -3378150
61
Y = -9627779
68 feet Y = -2934547
25 meter
Z = 16677918
93 Z = 5083429
69
XDOT = 9922
051350 XDOT = 3024
241252
YDOT = -21297
124671 feet/sec YDOT = -6491
363600 meter/sec
ZDOT = -5687
485356 ZDOT = -1733
545536
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 16222
29523705
00016717 00000-0 10270-3 0 9160
2 25544 51
6412 153
0408 0001994 111
8047 248
3319 15
54964736 13247
Satellite: ISS
Catalog Number: 25544
Epoch time: 16222
29523705 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 153
0408 deg
Eccentricity:
0001994
Arg of perigee: 111
8047 deg
Mean anomaly: 248
3319 deg
Mean motion: 15
54964736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 301
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