[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 10th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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
191/04:12:02
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
4
194/19:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
2
198/02:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
1
198/21:41:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 213
1
200/04:45:26
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
1
201/00:22:53
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
1
201/08:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 213
0
202/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
0
Coasting Arc #1 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2016/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1745043
74 A = 6776683
70 meter
Y = 4155321
33 meter E =
0006413
Z = 5057386
60 I = 51
35098
XDOT = -5875
109628 Wp = 52
79604
YDOT = 4611
142221 meter/sec RA = 311
03485 deg
ZDOT = -1756
125480 TA = 54
27633
MA = 54
21669
Ha = 220
276 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5725209
13 X = 1673881
99
Y = 13632944
00 feet Y = 4174437
32 meter
Z = 16592475
73 Z = 5065690
91
XDOT = -19275
294055 XDOT = -5917
705570
YDOT = 15128
419361 feet/sec YDOT = 4545
204787 meter/sec
ZDOT = -5761
566536 ZDOT = -1784
767956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11554782
02 X = 3521897
56
Y = -9162334
12 feet Y = -2792679
44 meter
Z = 16627810
39 Z = 5068156
61
XDOT = 19181
052168 XDOT = 5846
384701
YDOT = 13473
544110 feet/sec YDOT = 4106
736245 meter/sec
ZDOT = -5887
282209 ZDOT = -1794
443617
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 16190
54513405
00016717 00000-0 10270-3 0 9001
2 25544 51
6434 311
4803 0001037 41
5788 318
5444 15
54722764 8302
Satellite: ISS
Catalog Number: 25544
Epoch time: 16190
54513405 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 311
4803 deg
Eccentricity:
0001037
Arg of perigee: 41
5788 deg
Mean anomaly: 318
5444 deg
Mean motion: 15
54722764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 287
Coasting Arc #2 (Orbit 839)
---------------------------------------
Vector Time (GMT): 2016/191/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1938480
57 A = 6776635
26 meter
Y = -4098909
25 meter E =
0013368
Z = -5048253
67 I = 51
33835
XDOT = 5609
391100 Wp = 97
29890
YDOT = -4888
384472 meter/sec RA = 307
65838 deg
ZDOT = 1817
635145 TA = 190
38004
MA = 190
40767
Ha = 220
243 n
mi
Hp = 213
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6359844
39 X = -1867979
58
Y = -13447865
00 feet Y = -4120192
12 meter
Z = -16562512
05 Z = -5057499
21
XDOT = 18403
514109 XDOT = 5654
808188
YDOT = -16038
006799 feet/sec YDOT = -4825
402694 meter/sec
ZDOT = 5963
369898 ZDOT = 1844
993763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3745370
25 X = -1141588
85
Y = -14351185
09 feet Y = -4374241
22 meter
Z = -16601963
36 Z = -5060278
43
XDOT = 19891
353462 XDOT = 6062
884535
YDOT = -12219
497239 feet/sec YDOT = -3724
502758 meter/sec
ZDOT = 6083
539788 ZDOT = 1854
262927
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 16191
18789760
00016717 00000-0 10270-3 0 9012
2 25544 51
6445 308
2784 0001472 21
3441 338
7773 15
54766330 8408
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
18789760 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 308
2784 deg
Eccentricity:
0001472
Arg of perigee: 21
3441 deg
Mean anomaly: 338
7773 deg
Mean motion: 15
54766330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 840
Checksum: 314
Coasting Arc #3 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2016/192/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 499036
52 A = 6780107
03 meter
Y = 5348904
73 meter E =
0011457
Z = 4129947
70 I = 51
33082
XDOT = -5752
343251 Wp = 69
20114
YDOT = 3433
303427 meter/sec RA = 302
63811 deg
ZDOT = -3739
152727 TA = 59
48144
MA = 59
36839
Ha = 220
213 n
mi
Hp = 213
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1637258
91 X = 419125
36
Y = 17548900
04 feet Y = 5354038
25 meter
Z = 13549697
19 Z = 4132178
08
XDOT = -18872
517227 XDOT = -5772
144816
YDOT = 11264
118855 feet/sec YDOT = 3368
866384 meter/sec
ZDOT = -12267
561441 ZDOT = -3767
143736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1313500
13 X = -400354
84
Y = 17569427
46 feet Y = 5355161
49 meter
Z = 13558345
76 Z = 4132583
79
XDOT = -19087
955343 XDOT = -5818
008789
YDOT = 8165
906918 feet/sec YDOT = 2488
968429 meter/sec
ZDOT = -12390
182995 ZDOT = -3776
527777
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 16192
21631405
00016717 00000-0 10270-3 0 9020
2 25544 51
6439 303
1472 0001630 21
9969 338
1254 15
54805988 8564
Satellite: ISS
Catalog Number: 25544
Epoch time: 16192
21631405 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 303
1472 deg
Eccentricity:
0001630
Arg of perigee: 21
9969 deg
Mean anomaly: 338
1254 deg
Mean motion: 15
54805988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 308
Coasting Arc #4 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2016/193/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 797410
09 A = 6784399
61 meter
Y = -6174111
06 meter E =
0006265
Z = -2694676
12 I = 51
32707
XDOT = 5461
875216 Wp = 48
16250
YDOT = -1538
969490 meter/sec RA = 297
62923 deg
ZDOT = 5154
263634 TA = 281
25334
MA = 281
32375
Ha = 220
284 n
mi
Hp = 213
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2616174
82 X = 879480
74
Y = -20256269
87 feet Y = -6164734
85 meter
Z = -8840800
92 Z = -2690603
55
XDOT = 17919
538111 XDOT = 5453
641466
YDOT = -5049
112500 feet/sec YDOT = -1477
937490 meter/sec
ZDOT = 16910
313761 ZDOT = 5180
775725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5581876
79 X = 1701356
04
Y = -19655493
16 feet Y = -5990994
31 meter
Z = -8821838
86 Z = -2688896
49
XDOT = 16920
328526 XDOT = 5157
316135
YDOT = -2819
085441 feet/sec YDOT = -859
257242 meter/sec
ZDOT = 17026
109142 ZDOT = 5189
558066
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 16193
18044947
00016717 00000-0 10270-3 0 9037
2 25544 51
6428 298
3367 0001527 24
6237 335
4989 15
54767837 8715
Satellite: ISS
Catalog Number: 25544
Epoch time: 16193
18044947 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 298
3367 deg
Eccentricity:
0001527
Arg of perigee: 24
6237 deg
Mean anomaly: 335
4989 deg
Mean motion: 15
54767837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 346
Coasting Arc #5 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2016/194/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1933833
38 A = 6787150
17 meter
Y = 6441871
74 meter E =
0013353
Z = 866733
50 I = 51
32290
XDOT = -4849
835870 Wp = 119
14174
YDOT = -652
866277 meter/sec RA = 292
63057 deg
ZDOT = -5905
891794 TA = 51
43570
MA = 51
31613
Ha = 220
314 n
mi
Hp = 213
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6344597
69 X = -2009934
47
Y = 21134749
79 feet Y = 6419820
76 meter
Z = 2843613
85 Z = 857155
05
XDOT = -15911
535005 XDOT = -4813
486830
YDOT = -2141
949727 feet/sec YDOT = -706
896771 meter/sec
ZDOT = -19376
285415 ZDOT = -5929
362674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9014581
84 X = -2747644
55
Y = 20147245
94 feet Y = 6140880
56 meter
Z = 2800625
56 Z = 853630
67
XDOT = -13912
946662 XDOT = -4240
666143
YDOT = -3488
499221 feet/sec YDOT = -1063
294562 meter/sec
ZDOT = -19478
398758 ZDOT = -5937
015941
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 16194
20885193
00016717 00000-0 10270-3 0 9048
2 25544 51
6434 293
2051 0001517 30
5762 329
5479 15
54772489 8878
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
20885193 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 293
2051 deg
Eccentricity:
0001517
Arg of perigee: 30
5762 deg
Mean anomaly: 329
5479 deg
Mean motion: 15
54772489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 330
Coasting Arc #6 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2016/194/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3706138
85 A = 6785259
78 meter
Y = -5244772
81 meter E =
0015179
Z = 2167033
07 I = 51
30697
XDOT = 3066
091388 Wp = 68
16791
YDOT = 4433
280233 meter/sec RA = 289
56609 deg
ZDOT = 5460
657329 TA = 316
01404
MA = 316
13473
Ha = 220
242 n
mi
Hp = 213
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12159248
19 X = 3753985
32
Y = -17207259
87 feet Y = -5203060
91 meter
Z = 7109688
56 Z = 2185152
33
XDOT = 10059
354946 XDOT = 2989
764091
YDOT = 14544
882654 feet/sec YDOT = 4467
140176 meter/sec
ZDOT = 17915
542418 ZDOT = 5475
366454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 38188
15 X = 11639
75
Y = 21042632
44 feet Y = 6413794
37 meter
Z = 7189641
29 Z = 2191402
67
XDOT = -14981
158672 XDOT = -4566
257163
YDOT = -6143
628908 feet/sec YDOT = -1872
578091 meter/sec
ZDOT = 17978
751284 ZDOT = 5479
923391
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 16194
85159707
00016717 00000-0 10270-3 0 9055
2 25544 51
6406 289
9976 0001448 42
6026 317
5239 15
54828961 8974
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
85159707 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 289
9976 deg
Eccentricity:
0001448
Arg of perigee: 42
6026 deg
Mean anomaly: 317
5239 deg
Mean motion: 15
54828961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 353
Coasting Arc #7 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2016/195/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4121925
35 A = 6781294
98 meter
Y = 3854936
74 meter E =
0007522
Z = -3768068
90 I = 51
28278
XDOT = -1889
384700 Wp = 69
42834
YDOT = -6122
260996 meter/sec RA = 284
55748 deg
ZDOT = -4200
820197 TA = 155
94259
MA = 155
90743
Ha = 220
414 n
mi
Hp = 213
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13523377
14 X = -4146422
31
Y = 12647430
26 feet Y = 3808705
94 meter
Z = -12362430
78 Z = -3788151
29
XDOT = -6198
768702 XDOT = -1800
377938
YDOT = -20086
158124 feet/sec YDOT = -6142
891368 meter/sec
ZDOT = -13782
218494 ZDOT = -4209
782595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3368352
79 X = 1026673
93
Y = -18146741
24 feet Y = -5531126
73 meter
Z = -12450658
55 Z = -3794960
73
XDOT = 15478
293799 XDOT = 4717
783950
YDOT = 12345
668606 feet/sec YDOT = 3762
959791 meter/sec
ZDOT = -13820
074165 ZDOT = -4212
358605
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 16195
81571427
00016717 00000-0 10270-3 0 9060
2 25544 51
6399 285
1861 0001692 43
9354 316
1933 15
54792691 9129
Satellite: ISS
Catalog Number: 25544
Epoch time: 16195
81571427 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 285
1861 deg
Eccentricity:
0001692
Arg of perigee: 43
9354 deg
Mean anomaly: 316
1933 deg
Mean motion: 15
54792691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 333
Coasting Arc #8 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2016/196/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4278880
17 A = 6777258
41 meter
Y = -2038635
14 meter E =
0007385
Z = 4839018
72 I = 51
26239
XDOT = 734
331305 Wp = 108
50899
YDOT = 7251
121670 meter/sec RA = 279
53631 deg
ZDOT = 2400
180431 TA = 317
82109
MA = 317
87789
Ha = 220
202 n
mi
Hp = 213
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14038320
75 X = 4277852
93
Y = -6688435
51 feet Y = -1990792
03 meter
Z = 15876045
67 Z = 4859801
68
XDOT = 2409
223440 XDOT = 641
533873
YDOT = 23789
769259 feet/sec YDOT = 7258
814378 meter/sec
ZDOT = 7874
607712 ZDOT = 2403
522863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7052348
60 X = -2149555
85
Y = 13754221
72 feet Y = 4192286
78 meter
Z = 15966972
46 Z = 4866733
21
XDOT = -15265
342020 XDOT = -4652
876248
YDOT = -17004
063153 feet/sec YDOT = -5182
838449 meter/sec
ZDOT = 7887
775041 ZDOT = 2404
193832
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 16196
84409818
00016717 00000-0 10270-3 0 9079
2 25544 51
6400 280
0551 0001578 41
9867 318
1406 15
54816876 9288
Satellite: ISS
Catalog Number: 25544
Epoch time: 16196
84409818 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 280
0551 deg
Eccentricity:
0001578
Arg of perigee: 41
9867 deg
Mean anomaly: 318
1406 deg
Mean motion: 15
54816876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 331
Coasting Arc #9 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2016/197/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4253835
04 A = 6775397
25 meter
Y = -33401
38 meter E =
0016175
Z = -5287544
02 I = 51
25251
XDOT = 389
485610 Wp = 83
91620
YDOT = -7643
265741 meter/sec RA = 274
50393 deg
ZDOT = -264
074893 TA = 183
54384
MA = 183
55531
Ha = 220
422 n
mi
Hp = 212
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13956151
71 X = -4227460
93
Y = -109584
59 feet Y = -80822
60 meter
Z = -17347585
38 Z = -5308143
91
XDOT = 1277
839928 XDOT = 476
208340
YDOT = -25076
331170 feet/sec YDOT = -7638
425330 meter/sec
ZDOT = -866
387443 ZDOT = -261
973018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10947238
35 X = 3336718
25
Y = -8474829
29 feet Y = -2583127
97 meter
Z = -17437320
29 Z = -5314895
23
XDOT = 13882
899181 XDOT = 4231
507670
YDOT = 19700
437286 feet/sec YDOT = 6004
693285 meter/sec
ZDOT = -855
774742 ZDOT = -260
840141
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 16197
80820221
00016717 00000-0 10270-3 0 9082
2 25544 51
6408 275
2440 0001714 46
7783 313
3513 15
54810063 9436
Satellite: ISS
Catalog Number: 25544
Epoch time: 16197
80820221 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 275
2440 deg
Eccentricity:
0001714
Arg of perigee: 46
7783 deg
Mean anomaly: 313
3513 deg
Mean motion: 15
54810063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 292
Coasting Arc #10 (Orbit 947)
---------------------------------------
Vector Time (GMT): 2016/198/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2443284
32 A = 6782280
23 meter
Y = 5336061
08 meter E =
0013514
Z = 3389223
31 I = 51
27842
XDOT = -3931
129300 Wp = 83
96454
YDOT = 4726
278011 meter/sec RA = 272
97987 deg
ZDOT = -4589
995043 TA = 56
17005
MA = 56
04149
Ha = 220
234 n
mi
Hp = 213
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8016024
67 X = 2366970
27
Y = 17506762
08 feet Y = 5362956
46 meter
Z = 11119499
03 Z = 3400907
29
XDOT = -12897
405840 XDOT = -3961
391494
YDOT = 15506
161455 feet/sec YDOT = 4682
148777 meter/sec
ZDOT = -15059
038856 ZDOT = -4609
164369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3204340
72 X = -976683
05
Y = 18956889
13 feet Y = 5778059
81 meter
Z = 11169386
01 Z = 3404428
86
XDOT = -17899
398305 XDOT = -5455
736603
YDOT = 5930
035443 feet/sec YDOT = 1807
474803 meter/sec
ZDOT = -15143
447206 ZDOT = -4615
722708
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 16198
12956707
00016717 00000-0 10270-3 0 9098
2 25544 51
6440 273
6416 0001749 35
2663 324
8605 15
54861329 9480
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
12956707 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 273
6416 deg
Eccentricity:
0001749
Arg of perigee: 35
2663 deg
Mean anomaly: 324
8605 deg
Mean motion: 15
54861329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 332
Coasting Arc #11 (Orbit 960)
---------------------------------------
Vector Time (GMT): 2016/198/21:41:46
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1169430
65 A = 6786204
27 meter
Y = -6480206
10 meter E =
0015633
Z = 1608612
66 I = 51
28822
XDOT = 4612
242854 Wp = 61
31856
YDOT = 2256
278224 meter/sec RA = 268
93846 deg
ZDOT = 5701
453944 TA = 316
38706
MA = 316
51052
Ha = 220
390 n
mi
Hp = 213
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3836714
73 X = 1233993
15
Y = -21260518
70 feet Y = -6466767
93 meter
Z = 5277600
59 Z = 1614449
50
XDOT = 15132
030362 XDOT = 4558
974831
YDOT = 7402
487613 feet/sec YDOT = 2307
556924 meter/sec
ZDOT = 18705
557559 ZDOT = 5723
729744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20243246
73 X = 6170141
60
Y = 7527215
88 feet Y = 2294295
40 meter
Z = 5304251
70 Z = 1616735
92
XDOT = -9409
787217 XDOT = -2868
103144
YDOT = 11976
561793 feet/sec YDOT = 3650
456034 meter/sec
ZDOT = 18802
180350 ZDOT = 5730
904571
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 16198
96512062
00016717 00000-0 10270-3 0 9104
2 25544 51
6419 269
4720 0001776 45
9758 314
1541 15
54823893 9610
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
96512062 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 269
4720 deg
Eccentricity:
0001776
Arg of perigee: 45
9758 deg
Mean anomaly: 314
1541 deg
Mean motion: 15
54823893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 961
Checksum: 328
Coasting Arc #12 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2016/199/21:41:46
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2101519
24 A = 6782485
33 meter
Y = 5523464
12 meter E =
0006122
Z = -3334493
06 I = 51
27842
XDOT = -4213
172964 Wp = 81
15349
YDOT = -4403
290166 meter/sec RA = 263
93338 deg
ZDOT = -4644
996005 TA = 137
88596
MA = 137
83890
Ha = 220
378 n
mi
Hp = 212
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6894748
17 X = -2146930
49
Y = 18121601
44 feet Y = 5499710
00 meter
Z = -10939937
84 Z = -3344811
26
XDOT = -13822
745946 XDOT = -4141
058019
YDOT = -14446
490045 feet/sec YDOT = -4450
000928 meter/sec
ZDOT = -15239
488205 ZDOT = -4665
287645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16784539
05 X = -5115927
50
Y = -9654063
30 feet Y = -2942558
49 meter
Z = -10985924
71 Z = -3348509
85
XDOT = 15766
171576 XDOT = 4805
529096
YDOT = -9993
272170 feet/sec YDOT = -3045
949357 meter/sec
ZDOT = -15327
076800 ZDOT = -4671
693009
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 16199
92921414
00016717 00000-0 10270-3 0 9117
2 25544 51
6427 264
6616 0001767 47
7699 312
3603 15
54847060 9761
Satellite: ISS
Catalog Number: 25544
Epoch time: 16199
92921414 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 264
6616 deg
Eccentricity:
0001767
Arg of perigee: 47
7699 deg
Mean anomaly: 312
3603 deg
Mean motion: 15
54847060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 976
Checksum: 332
Coasting Arc #13 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2016/200/04:45:26
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3514697
69 A = 6777173
55 meter
Y = -3149941
33 meter E =
0007548
Z = 4858439
56 I = 51
25780
XDOT = 2795
351348 Wp = 110
23652
YDOT = 6749
246540 meter/sec RA = 262
44741 deg
ZDOT = 2348
077626 TA = 316
63424
MA = 316
69360
Ha = 220
262 n
mi
Hp = 213
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11531160
41 X = 3526060
02
Y = -10334453
19 feet Y = -3110574
66 meter
Z = 15939762
35 Z = 4875540
11
XDOT = 9171
100223 XDOT = 2708
266019
YDOT = 22143
197309 feet/sec YDOT = 6780
018835 meter/sec
ZDOT = 7703
666751 ZDOT = 2361
445812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10096571
42 X = 3077434
97
Y = -11637363
10 feet Y = -3547068
27 meter
Z = 16014856
62 Z = 4881328
30
XDOT = 10879
864753 XDOT = 3316
182777
YDOT = 20144
163514 feet/sec YDOT = 6139
941039 meter/sec
ZDOT = 7760
657850 ZDOT = 2365
448513
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 16200
25057721
00016717 00000-0 10270-3 0 9128
2 25544 51
6391 263
0542 0001540 53
8937 306
2358 15
54825174 9811
Satellite: ISS
Catalog Number: 25544
Epoch time: 16200
25057721 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 263
0542 deg
Eccentricity:
0001540
Arg of perigee: 53
8937 deg
Mean anomaly: 306
2358 deg
Mean motion: 15
54825174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 293
Coasting Arc #14 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2016/201/00:22:53
000
Vector Time (MET): N/A
Weight (LBS) : 909228
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3426481
17 A = 6783633
25 meter
Y = -5085902
26 meter E =
0006180
Z = -2900602
61 I = 51
28796
XDOT = 3078
172489 Wp = 59
82159
YDOT = -4922
138362 meter/sec RA = 258
30898 deg
ZDOT = 5005
272917 TA = 266
95108
MA = 267
02180
Ha = 220
316 n
mi
Hp = 213
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11241736
12 X = -3355265
02
Y = -16686031
03 feet Y = -5123820
95 meter
Z = -9516412
78 Z = -2917074
91
XDOT = 10098
991105 XDOT = 3108
671236
YDOT = -16148
747908 feet/sec YDOT = -4887
546189 meter/sec
ZDOT = 16421
499073 ZDOT = 5020
299224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8193432
44 X = 2497358
21
Y = -18338883
11 feet Y = -5589691
57 meter
Z = -9587252
26 Z = -2922194
49
XDOT = 17651
478716 XDOT = 5380
170713
YDOT = -714
428626 feet/sec YDOT = -217
757845 meter/sec
ZDOT = 16487
880477 ZDOT = 5025
505969
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 16201
02184603
00016717 00000-0 10270-3 0 9135
2 25544 51
6434 259
2103 0001693 43
5327 316
5959 15
54840613 9936
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
02184603 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 259
2103 deg
Eccentricity:
0001693
Arg of perigee: 43
5327 deg
Mean anomaly: 316
5959 deg
Mean motion: 15
54840613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 295
Coasting Arc #15 (Orbit 998)
---------------------------------------
Vector Time (GMT): 2016/201/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 909228
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4193132
04 A = 6775170
34 meter
Y = -665500
27 meter E =
0003929
Z = 5276730
69 I = 51
26198
XDOT = 1553
059112 Wp = 72
30967
YDOT = 7508
811451 meter/sec RA = 256
60086 deg
ZDOT = -285
771460 TA = 20
43494
MA = 20
41922
Ha = 220
144 n
mi
Hp = 213
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13756994
88 X = 4174630
55
Y = -2183399
83 feet Y = -618713
86 meter
Z = 17312108
57 Z = 5297054
53
XDOT = 5095
338293 XDOT = 1470
366395
YDOT = 24635
208171 feet/sec YDOT = 7525
716460 meter/sec
ZDOT = -937
570406 ZDOT = -278
427291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3504894
50 X = 1068291
84
Y = -13366353
66 feet Y = -4074064
60 meter
Z = 17400791
67 Z = 5303761
30
XDOT = 23626
107734 XDOT = 7201
237637
YDOT = 5008
751828 feet/sec YDOT = 1526
667557 meter/sec
ZDOT = -906
944593 ZDOT = -276
436712
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 16201
40747937
00016717 00000-0 10270-3 0 9143
2 25544 51
6431 257
2810 0001441 63
5847 296
5454 15
54883770 9990
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
40747937 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 257
2810 deg
Eccentricity:
0001441
Arg of perigee: 63
5847 deg
Mean anomaly: 296
5454 deg
Mean motion: 15
54883770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 999
Checksum: 327
Coasting Arc #16 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2016/202/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 909228
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4551156
83 A = 6777112
69 meter
Y = -1382697
62 meter E =
0013081
Z = -4839691
43 I = 51
27611
XDOT = -369
754869 Wp = 103
45318
YDOT = -7256
373884 meter/sec RA = 251
57088 deg
ZDOT = 2423
406903 TA = 190
45908
MA = 190
48632
Ha = 220
340 n
mi
Hp = 212
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14931616
89 X = -4511848
23
Y = -4536409
51 feet Y = -1433371
48 meter
Z = -15878252
71 Z = -4861704
02
XDOT = -1213
106527 XDOT = -300
356421
YDOT = -23807
000933 feet/sec YDOT = -7260
120912 meter/sec
ZDOT = 7950
810049 ZDOT = 2421
778683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9928046
05 X = -3026068
43
Y = 11912956
91 feet Y = 3631069
27 meter
Z = -15973930
72 Z = -4868854
08
XDOT = -21568
510450 XDOT = -6574
081985
YDOT = -7332
594967 feet/sec YDOT = -2234
974946 meter/sec
ZDOT = 7945
026370 ZDOT = 2421
644037
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 16202
37156213
00016717 00000-0 10270-3 0 9152
2 25544 51
6424 252
4718 0001530 69
8385 290
2933 15
54878595 10142
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
37156213 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 252
4718 deg
Eccentricity:
0001530
Arg of perigee: 69
8385 deg
Mean anomaly: 290
2933 deg
Mean motion: 15
54878595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 308
Coasting Arc #17 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2016/202/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930194
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4530544
08 A = 6779317
44 meter
Y = 2695303
01 meter E =
0011296
Z = 4255517
62 I = 51
28406
XDOT = -684
646230 Wp = 71
12683
YDOT = 6769
159045 meter/sec RA = 251
07193 deg
ZDOT = -3547
134464 TA = 55
26055
MA = 55
15423
Ha = 220
171 n
mi
Hp = 212
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14863989
76 X = 4479396
74
Y = 8842857
63 feet Y = 2745680
22 meter
Z = 13961671
98 Z = 4277401
44
XDOT = -2246
214665 XDOT = -743
059681
YDOT = 22208
527052 feet/sec YDOT = 6761
176570 meter/sec
ZDOT = -11637
580261 ZDOT = -3550
601532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5349869
17 X = 1630640
12
Y = -16366270
99 feet Y = -4988439
40 meter
Z = 14056552
95 Z = 4284437
34
XDOT = 20942
858688 XDOT = 6383
383328
YDOT = -3195
066387 feet/sec YDOT = -973
856235 meter/sec
ZDOT = -11653
911471 ZDOT = -3552
112216
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 16202
50010462
00016717 00000-0 10270-3 0 9163
2 25544 51
6419 251
8313 0001477 58
7357 301
3940 15
54889663 10168
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
50010462 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 251
8313 deg
Eccentricity:
0001477
Arg of perigee: 58
7357 deg
Mean anomaly: 301
3940 deg
Mean motion: 15
54889663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 295
Coasting Arc #18 (Orbit 1030)
---------------------------------------
Vector Time (GMT): 2016/203/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930194
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4405721
58 A = 6783655
21 meter
Y = -4301364
62 meter E =
0006163
Z = -2848282
66 I = 51
30865
XDOT = 2021
741766 Wp = 64
43714
YDOT = -5404
348312 meter/sec RA = 246
05904 deg
ZDOT = 5045
374393 TA = 263
02217
MA = 263
09227
Ha = 220
323 n
mi
Hp = 212
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14454467
14 X = -4343459
76
Y = -14112088
65 feet Y = -4350284
02 meter
Z = -9344759
38 Z = -2869533
17
XDOT = 6633
011044 XDOT = 2057
516554
YDOT = -17730
801547 feet/sec YDOT = -5381
540159 meter/sec
ZDOT = 16553
065593 ZDOT = 5055
281827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10274981
63 X = -3131814
40
Y = 17343077
93 feet Y = 5286170
15 meter
Z = -9436609
28 Z = -2876278
51
XDOT = -17509
135159 XDOT = -5336
784396
YDOT = -1362
336232 feet/sec YDOT = -415
240084 meter/sec
ZDOT = 16597
206246 ZDOT = 5058
828464
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 16203
46418329
00016717 00000-0 10270-3 0 9174
2 25544 51
6408 247
0206 0001541 66
5828 293
5486 15
54871945 10314
Satellite: ISS
Catalog Number: 25544
Epoch time: 16203
46418329 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 247
0206 deg
Eccentricity:
0001541
Arg of perigee: 66
5828 deg
Mean anomaly: 293
5486 deg
Mean motion: 15
54871945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1031
Checksum: 312
Coasting Arc #19 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2016/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930194
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3931069
40 A = 6786641
61 meter
Y = 5430520
97 meter E =
0014552
Z = 1015028
76 I = 51
33332
XDOT = -3399
554731 Wp = 117
90042
YDOT = 3570
172039 meter/sec RA = 241
05855 deg
ZDOT = -5876
881636 TA = 51
04595
MA = 50
91636
Ha = 220
374 n
mi
Hp = 212
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12897209
33 X = 3865121
31
Y = 17816669
84 feet Y = 5474112
02 meter
Z = 3330146
84 Z = 1033964
60
XDOT = -11153
394787 XDOT = -3410
677864
YDOT = 11713
162859 feet/sec YDOT = 3532
094043 meter/sec
ZDOT = -19281
107729 ZDOT = -5893
422325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13943919
60 X = 4250106
69
Y = -16993787
93 feet Y = -5179706
56 meter
Z = 3411728
12 Z = 1039894
73
XDOT = 12897
669676 XDOT = 3931
209717
YDOT = 6660
145626 feet/sec YDOT = 2030
012387 meter/sec
ZDOT = -19353
827728 ZDOT = -5899
046692
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 16204
49252700
00016717 00000-0 10270-3 0 9188
2 25544 51
6414 241
8882 0001764 63
6397 296
4938 15
54896376 10475
Satellite: ISS
Catalog Number: 25544
Epoch time: 16204
49252700 = yrday
fracday
Element set: 918
Inclination: 51
6414 deg
RA of node: 241
8882 deg
Eccentricity:
0001764
Arg of perigee: 63
6397 deg
Mean anomaly: 296
4938 deg
Mean motion: 15
54896376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 337
Coasting Arc #20 (Orbit 1061)
---------------------------------------
Vector Time (GMT): 2016/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930194
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3117050
55 A = 6786934
80 meter
Y = -5950046
46 meter E =
0015328
Z = 919694
11 I = 51
34915
XDOT = 4662
785520 Wp = 56
32044
YDOT = -1521
191131 meter/sec RA = 236
06481 deg
ZDOT = 5899
120186 TA = 313
68253
MA = 313
80946
Ha = 220
526 n
mi
Hp = 212
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10226543
80 X = -3054751
36
Y = -19521149
80 feet Y = -5984555
09 meter
Z = 3017369
12 Z = 904703
66
XDOT = 15297
852755 XDOT = 4650
794461
YDOT = -4990
784549 feet/sec YDOT = -1469
115983 meter/sec
ZDOT = 19354
068851 ZDOT = 5921
741242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16003674
67 X = -4877920
04
Y = 15163240
35 feet Y = 4621755
66 meter
Z = 2953056
59 Z = 900091
65
XDOT = -7817
159567 XDOT = -2382
670236
YDOT = -12079
794959 feet/sec YDOT = -3681
921504 meter/sec
ZDOT = 19452
934687 ZDOT = 5929
254492
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 16205
52086906
00016717 00000-0 10270-3 0 9197
2 25544 51
6405 236
7567 0001899 66
0123 294
1229 15
54835725 10627
Satellite: ISS
Catalog Number: 25544
Epoch time: 16205
52086906 = yrday
fracday
Element set: 919
Inclination: 51
6405 deg
RA of node: 236
7567 deg
Eccentricity:
0001899
Arg of perigee: 66
0123 deg
Mean anomaly: 294
1229 deg
Mean motion: 15
54835725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1062
Checksum: 318
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