[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 17th 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) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
322/07:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 216
8
322/20:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 217
0
324/22:01:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 217
2
326/13:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 217
3
328/20:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 217
7
332/03:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 217
7
Coasting Arc #1 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2016/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5300072
58 A = 6784153
40 meter
Y = -1558724
20 meter E =
0007335
Z = -3944950
35 I = 51
75861
XDOT = 4418
816507 Wp = 162
60346
YDOT = 4773
523295 meter/sec RA = 17
85860 deg
ZDOT = 4045
721306 TA = 149
67341
MA = 149
63095
Ha = 221
679 n
mi
Hp = 216
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17388689
57 X = 5336271
98
Y = -5113924
55 feet Y = -1499252
62 meter
Z = -12942750
50 Z = -3919115
55
XDOT = 14497
429485 XDOT = 4345
456551
YDOT = 15661
165665 feet/sec YDOT = 4822
527070 meter/sec
ZDOT = 13273
363866 ZDOT = 4067
009329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5791239
06 X = -1765169
67
Y = 17259896
93 feet Y = 5260816
58 meter
Z = -12829304
26 Z = -3910371
94
XDOT = -19830
470818 XDOT = -6044
327505
YDOT = 3292
952732 feet/sec YDOT = 1003
691993 meter/sec
ZDOT = 13365
617806 ZDOT = 4073
840307
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 16321
50846220
00016717 00000-0 10270-3 0 9007
2 25544 51
6422 18
4205 0006655 218
3134 141
7547 15
53683217 28679
Satellite: ISS
Catalog Number: 25544
Epoch time: 16321
50846220 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 18
4205 deg
Eccentricity:
0006655
Arg of perigee: 218
3134 deg
Mean anomaly: 141
7547 deg
Mean motion: 15
53683217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 290
Coasting Arc #2 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/322/07:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4112701
28 A = 6781753
01 meter
Y = 2750787
95 meter E =
0003756
Z = 4634279
20 I = 51
72589
XDOT = -5923
617726 Wp = 116
14433
YDOT = -3868
686580 meter/sec RA = 13
87100 deg
ZDOT = -2960
332539 TA = 3
30770
MA = 3
30522
Ha = 221
799 n
mi
Hp = 216
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13493114
45 X = -4165667
33
Y = 9024894
86 feet Y = 2704500
55 meter
Z = 15204328
08 Z = 4614171
90
XDOT = -19434
441358 XDOT = -5865
536568
YDOT = -12692
541272 feet/sec YDOT = -3934
603530 meter/sec
ZDOT = -9712
377095 ZDOT = -2988
967612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15504879
92 X = 4725887
40
Y = -5079189
84 feet Y = -1548137
06 meter
Z = 15115719
84 Z = 4607271
41
XDOT = 14918
965472 XDOT = 4547
300676
YDOT = 16264
711753 feet/sec YDOT = 4957
484142 meter/sec
ZDOT = -9836
983483 ZDOT = -2998
312565
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 16322
34464254
00016717 00000-0 10270-3 0 9014
2 25544 51
6427 14
2518 0006734 219
9861 140
0796 15
53636502 28805
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
34464254 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 14
2518 deg
Eccentricity:
0006734
Arg of perigee: 219
9861 deg
Mean anomaly: 140
0796 deg
Mean motion: 15
53636502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 303
Coasting Arc #3 (Orbit 2887)
---------------------------------------
Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3389340
35 A = 6780636
04 meter
Y = -3266360
97 meter E =
0010407
Z = -4889439
39 I = 51
70502
XDOT = 6535
283154 Wp = 138
96193
YDOT = 3207
400119 meter/sec RA = 11
16321 deg
ZDOT = 2382
764938 TA = 154
41405
MA = 154
36251
Ha = 221
339 n
mi
Hp = 217
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11119883
04 X = 3449364
85
Y = -10716407
38 feet Y = -3228123
21 meter
Z = -16041467
83 Z = -4872828
98
XDOT = 21441
217698 XDOT = 6487
356862
YDOT = 10522
966271 feet/sec YDOT = 3280
213941 meter/sec
ZDOT = 7817
470269 ZDOT = 2414
395913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10936111
83 X = 3333326
88
Y = -11011092
96 feet Y = -3356181
13 meter
Z = -15968067
07 Z = -4867066
84
XDOT = 20858
116429 XDOT = 6357
553888
YDOT = 9156
560197 feet/sec YDOT = 2790
919548 meter/sec
ZDOT = 7955
328328 ZDOT = 2424
784074
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 16322
85921119
00016717 00000-0 10270-3 0 9029
2 25544 51
6423 11
6924 0006272 225
8980 134
1657 15
53671837 28886
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
85921119 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 11
6924 deg
Eccentricity:
0006272
Arg of perigee: 225
8980 deg
Mean anomaly: 134
1657 deg
Mean motion: 15
53671837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2888
Checksum: 319
Coasting Arc #4 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4701773
54 A = 6783785
95 meter
Y = 2717311
70 meter E =
0006073
Z = 4059278
16 I = 51
68339
XDOT = -5488
950511 Wp = 107
57060
YDOT = -3684
836839 meter/sec RA = 6
18076 deg
ZDOT = -3888
074739 TA = 22
69237
MA = 22
66553
Ha = 221
274 n
mi
Hp = 217
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15425766
22 X = -4751528
19
Y = 8915064
64 feet Y = 2664454
95 meter
Z = 13317841
74 Z = 4036317
16
XDOT = -18008
367818 XDOT = -5428
450990
YDOT = -12089
359708 feet/sec YDOT = -3745
879530 meter/sec
ZDOT = -12756
150719 ZDOT = -3914
592165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15107786
05 X = -4604853
19
Y = 9584884
01 feet Y = 2921472
65 meter
Z = 13216745
01 Z = 4028463
88
XDOT = -17737
035106 XDOT = -5406
248300
YDOT = -10194
877830 feet/sec YDOT = -3107
398763 meter/sec
ZDOT = -12871
516982 ZDOT = -3923
238376
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 16323
88834744
00016717 00000-0 10270-3 0 9031
2 25544 51
6421 6
5669 0006279 229
7739 130
2865 15
53667259 29045
Satellite: ISS
Catalog Number: 25544
Epoch time: 16323
88834744 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 6
5669 deg
Eccentricity:
0006279
Arg of perigee: 229
7739 deg
Mean anomaly: 130
2865 deg
Mean motion: 15
53667259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 340
Coasting Arc #5 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2016/324/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5752158
36 A = 6787180
16 meter
Y = -2160467
05 meter E =
0001861
Z = -2884123
77 I = 51
66335
XDOT = 4067
317386 Wp = 211
99602
YDOT = 4081
162947 meter/sec RA = 1
20284 deg
ZDOT = 5051
751591 TA = 115
20413
MA = 115
18483
Ha = 220
975 n
mi
Hp = 217
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18871910
64 X = 5789899
68
Y = -7088146
49 feet Y = -2095931
45 meter
Z = -9462348
34 Z = -2856089
39
XDOT = 13344
217146 XDOT = 3996
839058
YDOT = 13389
642216 feet/sec YDOT = 4126
252217 meter/sec
ZDOT = 16573
988161 ZDOT = 5071
338684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18466576
75 X = 5628612
59
Y = -8227552
73 feet Y = -2507758
07 meter
Z = -9339153
42 Z = -2846573
96
XDOT = 13426
592509 XDOT = 4092
425397
YDOT = 11214
594524 feet/sec YDOT = 3418
208411 meter/sec
ZDOT = 16658
924795 ZDOT = 5077
640278
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 16324
85315836
00016717 00000-0 10270-3 0 9046
2 25544 51
6427 1
7602 0006343 233
7619 126
2947 15
53686646 29192
Satellite: ISS
Catalog Number: 25544
Epoch time: 16324
85315836 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 1
7602 deg
Eccentricity:
0006343
Arg of perigee: 233
7619 deg
Mean anomaly: 126
2947 deg
Mean motion: 15
53686646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 322
Coasting Arc #6 (Orbit 2920)
---------------------------------------
Vector Time (GMT): 2016/324/22:01:46
000
Vector Time (MET): N/A
Weight (LBS) : 909067
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6780764
47 A = 6790590
26 meter
Y = 240799
25 meter E =
0006210
Z = 173254
49 I = 51
67386
XDOT = -325
031657 Wp = 39
50837
YDOT = 4746
536676 meter/sec RA =
87724 deg
ZDOT = 6010
114861 TA = 322
35630
MA = 322
39974
Ha = 220
935 n
mi
Hp = 217
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22246602
60 X = 6776726
23
Y = 790023
79 feet Y = 316603
73 meter
Z = 568420
24 Z = 206184
20
XDOT = -1066
376827 XDOT = -407
279265
YDOT = 15572
626889 feet/sec YDOT = 4742
441924 meter/sec
ZDOT = 19718
224610 ZDOT = 6008
336278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19846505
01 X = 6049214
73
Y = -10073085
97 feet Y = -3070276
60 meter
Z = 712561
75 Z = 217188
82
XDOT = 5757
858840 XDOT = 1754
995375
YDOT = 12759
731027 feet/sec YDOT = 3889
166017 meter/sec
ZDOT = 19709
471123 ZDOT = 6007
446798
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 16324
98179855
00016717 00000-0 10270-3 0 9050
2 25544 51
6439 1
1199 0006400 235
2005 124
8546 15
53687433 29217
Satellite: ISS
Catalog Number: 25544
Epoch time: 16324
98179855 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 1
1199 deg
Eccentricity:
0006400
Arg of perigee: 235
2005 deg
Mean anomaly: 124
8546 deg
Mean motion: 15
53687433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2921
Checksum: 311
Coasting Arc #7 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2016/325/22:01:46
000
Vector Time (MET): N/A
Weight (LBS) : 909067
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6497559
98 A = 6789371
16 meter
Y = -904355
43 meter E =
0009314
Z = -1725147
06 I = 51
63788
XDOT = 2158
383956 Wp = 184
92841
YDOT = -4668
550794 meter/sec RA = 355
91001 deg
ZDOT = -5688
737859 TA = 13
99787
MA = 13
97207
Ha = 220
771 n
mi
Hp = 217
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21317454
00 X = -6478584
25
Y = -2967045
38 feet Y = -976909
39 meter
Z = -5659931
31 Z = -1756664
75
XDOT = 7081
312190 XDOT = 2238
062119
YDOT = -15316
767698 feet/sec YDOT = -4643
968725 meter/sec
ZDOT = -18663
838119 ZDOT = -5678
059411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19922914
82 X = -6072504
44
Y = 8045843
42 feet Y = 2452373
07 meter
Z = -5797749
10 Z = -1767153
93
XDOT = -814
670485 XDOT = -248
311564
YDOT = -15416
189600 feet/sec YDOT = -4698
854590 meter/sec
ZDOT = -18616
134431 ZDOT = -5674
197775
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 16325
94660461
00016717 00000-0 10270-3 0 9066
2 25544 51
6445 356
3143 0006484 238
2276 121
8246 15
53658725 29365
Satellite: ISS
Catalog Number: 25544
Epoch time: 16325
94660461 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 356
3143 deg
Eccentricity:
0006484
Arg of perigee: 238
2276 deg
Mean anomaly: 121
8246 deg
Mean motion: 15
53658725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 325
Coasting Arc #8 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2016/326/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6466518
63 A = 6790104
31 meter
Y = 1716038
65 meter E =
0012321
Z = 1112240
35 I = 51
61722
XDOT = -2186
059497 Wp = 149
57136
YDOT = -4415
236844 meter/sec RA = 352
70469 deg
ZDOT = -5879
411067 TA = 18
35263
MA = 18
30821
Ha = 220
749 n
mi
Hp = 217
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21215612
30 X = -6490630
03
Y = 5630048
07 feet Y = 1643590
88 meter
Z = 3649082
52 Z = 1080768
81
XDOT = -7172
111211 XDOT = -2107
964832
YDOT = -14485
685184 feet/sec YDOT = -4439
246154 meter/sec
ZDOT = -19289
406388 ZDOT = -5889
840818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1901403
64 X = -579547
83
Y = -21890029
98 feet Y = -6672081
14 meter
Z = 3510940
26 Z = 1070134
59
XDOT = 13885
733780 XDOT = 4232
371656
YDOT = -4317
057410 feet/sec YDOT = -1315
839098 meter/sec
ZDOT = -19334
176948 ZDOT = -5893
057134
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 16326
58980534
00016717 00000-0 10270-3 0 9074
2 25544 51
6418 353
1088 0006111 238
6602 121
3953 15
53695993 29461
Satellite: ISS
Catalog Number: 25544
Epoch time: 16326
58980534 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 353
1088 deg
Eccentricity:
0006111
Arg of perigee: 238
6602 deg
Mean anomaly: 121
3953 deg
Mean motion: 15
53695993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 329
Coasting Arc #9 (Orbit 2961)
---------------------------------------
Vector Time (GMT): 2016/327/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6683707
35 A = 6790358
17 meter
Y = -1086825
03 meter E =
0006855
Z = 451277
22 I = 51
58591
XDOT = 369
580320 Wp = 39
23508
YDOT = 4776
361274 meter/sec RA = 347
73471 deg
ZDOT = 5984
750996 TA = 325
63326
MA = 325
67758
Ha = 220
534 n
mi
Hp = 217
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21928173
72 X = 6693171
62
Y = -3565698
92 feet Y = -1012030
41 meter
Z = 1480568
32 Z = 483768
33
XDOT = 1212
533859 XDOT = 287
070715
YDOT = 15670
476622 feet/sec YDOT = 4780
032852 meter/sec
ZDOT = 19635
009829 ZDOT = 5986
345918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 132624
60 X = 40423
98
Y = 22205838
27 feet Y = 6768339
51 meter
Z = 1623037
73 Z = 494701
90
XDOT = -14032
250327 XDOT = -4277
029900
YDOT = -1361
519467 feet/sec YDOT = -414
991133 meter/sec
ZDOT = 19641
026925 ZDOT = 5986
585007
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 16327
61892302
00016717 00000-0 10270-3 0 9085
2 25544 51
6410 347
9828 0006333 242
1014 117
9497 15
53738734 29622
Satellite: ISS
Catalog Number: 25544
Epoch time: 16327
61892302 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 347
9828 deg
Eccentricity:
0006333
Arg of perigee: 242
1014 deg
Mean anomaly: 117
9497 deg
Mean motion: 15
53738734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2962
Checksum: 321
Coasting Arc #10 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2016/328/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6475802
89 A = 6788823
24 meter
Y = 355637
83 meter E =
0007573
Z = -1989336
75 I = 51
54878
XDOT = 1430
734458 Wp = 189
60213
YDOT = -5073
818133 meter/sec RA = 342
75981 deg
ZDOT = -5568
711046 TA = 12
38836
MA = 12
36976
Ha = 220
231 n
mi
Hp = 217
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21246072
47 X = -6469634
96
Y = 1166790
77 feet Y = 283255
53 meter
Z = -6526695
37 Z = -2020780
01
XDOT = 4694
010688 XDOT = 1514
415608
YDOT = -16646
384951 feet/sec YDOT = -5057
350839 meter/sec
ZDOT = -18270
049364 ZDOT = -5561
557525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1763560
88 X = 537533
36
Y = -21161996
75 feet Y = -6450176
61 meter
Z = -6664420
11 Z = -2031315
25
XDOT = 14283
995376 XDOT = 4353
761791
YDOT = 6929
570286 feet/sec YDOT = 2112
133023 meter/sec
ZDOT = -18237
709121 ZDOT = -5558
853740
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 16328
58372049
00016717 00000-0 10270-3 0 9094
2 25544 51
6406 343
1760 0006121 247
0099 113
0408 15
53700669 29773
Satellite: ISS
Catalog Number: 25544
Epoch time: 16328
58372049 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 343
1760 deg
Eccentricity:
0006121
Arg of perigee: 247
0099 deg
Mean anomaly: 113
0408 deg
Mean motion: 15
53700669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 311
Coasting Arc #11 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2016/328/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4607513
43 A = 6786915
48 meter
Y = -4022654
68 meter E =
0001787
Z = -2940079
03 I = 51
53736
XDOT = 5289
604943 Wp = 262
43037
YDOT = 2403
368619 meter/sec RA = 341
32478 deg
ZDOT = 4998
386170 TA = 63
97676
MA = 63
95836
Ha = 220
146 n
mi
Hp = 217
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15116513
88 X = 4666435
18
Y = -13197685
95 feet Y = -3970800
93 meter
Z = -9645928
59 Z = -2917553
44
XDOT = 17354
346926 XDOT = 5238
056380
YDOT = 7885
067648 feet/sec YDOT = 2462
232333 meter/sec
ZDOT = 16398
904756 ZDOT = 5023
956884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14469960
24 X = 4410443
88
Y = -13971982
94 feet Y = -4258660
40 meter
Z = -9546506
58 Z = -2909775
21
XDOT = 16616
526455 XDOT = 5064
717263
YDOT = 5921
441562 feet/sec YDOT = 1804
855388 meter/sec
ZDOT = 16510
362183 ZDOT = 5032
358393
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 16328
84099881
00016717 00000-0 10270-3 0 9105
2 25544 51
6442 341
8953 0006315 250
0252 110
0220 15
53724425 29812
Satellite: ISS
Catalog Number: 25544
Epoch time: 16328
84099881 = yrday
fracday
Element set: 910
Inclination: 51
6442 deg
RA of node: 341
8953 deg
Eccentricity:
0006315
Arg of perigee: 250
0252 deg
Mean anomaly: 110
0220 deg
Mean motion: 15
53724425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 291
Coasting Arc #12 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2016/329/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5477762
02 A = 6789698
96 meter
Y = 3706242
47 meter E =
0010522
Z = 1505654
20 I = 51
51545
XDOT = -3830
808790 Wp = 143
13950
YDOT = -3318
159791 meter/sec RA = 336
34488 deg
ZDOT = -5756
503444 TA = 20
38689
MA = 20
34492
Ha = 220
087 n
mi
Hp = 217
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17971660
17 X = -5526112
99
Y = 12159588
16 feet Y = 3644716
11 meter
Z = 4939810
37 Z = 1478926
72
XDOT = -12568
270307 XDOT = -3765
456485
YDOT = -10886
351021 feet/sec YDOT = -3360
633058 meter/sec
ZDOT = -18886
166154 ZDOT = -5774
954129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17117241
45 X = -5217335
19
Y = 13378550
04 feet Y = 4077782
05 meter
Z = 4822066
34 Z = 1469765
82
XDOT = -12194
666262 XDOT = -3716
934277
YDOT = -8751
127494 feet/sec YDOT = -2667
343660 meter/sec
ZDOT = -18966
265634 ZDOT = -5780
917765
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 16329
87010880
00016717 00000-0 10270-3 0 9112
2 25544 51
6436 336
7694 0006206 252
9426 107
1047 15
53687038 29972
Satellite: ISS
Catalog Number: 25544
Epoch time: 16329
87010880 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 336
7694 deg
Eccentricity:
0006206
Arg of perigee: 252
9426 deg
Mean anomaly: 107
1047 deg
Mean motion: 15
53687038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 328
Coasting Arc #13 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2016/330/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5975786
85 A = 6790486
23 meter
Y = -3214217
03 meter E =
0007669
Z = 53431
26 I = 51
48896
XDOT = 2218
195673 Wp = 20
11983
YDOT = 4227
885403 meter/sec RA = 331
36635 deg
ZDOT = 5999
114266 TA = 340
45675
MA = 340
48613
Ha = 219
711 n
mi
Hp = 217
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19605599
89 X = 6011025
36
Y = -10545331
48 feet Y = -3147194
74 meter
Z = 175299
41 Z = 82546
24
XDOT = 7277
544858 XDOT = 2141
611855
YDOT = 13871
015103 feet/sec YDOT = 4252
262486 meter/sec
ZDOT = 19682
133417 ZDOT = 6009
703937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18618929
63 X = 5675049
75
Y = -12200725
75 feet Y = -3718781
21 meter
Z = 303387
22 Z = 92472
42
XDOT = 7432
710557 XDOT = 2265
490178
YDOT = 11845
015110 feet/sec YDOT = 3610
360605 meter/sec
ZDOT = 19727
637403 ZDOT = 6012
983880
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 16330
89921300
00016717 00000-0 10270-3 0 9125
2 25544 51
6432 331
6423 0006336 258
5290 101
5151 15
53729435 30139
Satellite: ISS
Catalog Number: 25544
Epoch time: 16330
89921300 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 331
6423 deg
Eccentricity:
0006336
Arg of perigee: 258
5290 deg
Mean anomaly: 101
5151 deg
Mean motion: 15
53729435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 278
Coasting Arc #14 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2016/331/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6094594
28 A = 6789427
77 meter
Y = 2503152
50 meter E =
0007332
Z = -1618400
81 I = 51
45765
XDOT = -571
832018 Wp = 192
19195
YDOT = -5083
691733 meter/sec RA = 326
38652 deg
ZDOT = -5711
729821 TA = 5
56542
MA = 5
55727
Ha = 219
505 n
mi
Hp = 217
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19995388
05 X = -6114270
55
Y = 8212442
60 feet Y = 2434888
68 meter
Z = -5309713
95 Z = -1648055
15
XDOT = -1876
089299 XDOT = -487
196697
YDOT = -16678
778652 feet/sec YDOT = -5089
612975 meter/sec
ZDOT = -18739
271067 ZDOT = -5714
302248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19002567
45 X = -5791982
56
Y = 10235306
98 feet Y = 3119721
57 meter
Z = -5440012
90 Z = -1658115
93
XDOT = -2726
515685 XDOT = -831
041981
YDOT = -15023
349220 feet/sec YDOT = -4579
116842 meter/sec
ZDOT = -18749
511257 ZDOT = -5714
851031
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 16331
86399701
00016717 00000-0 10270-3 0 9138
2 25544 51
6435 326
8365 0006469 261
1653 98
8767 15
53693600 30284
Satellite: ISS
Catalog Number: 25544
Epoch time: 16331
86399701 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 326
8365 deg
Eccentricity:
0006469
Arg of perigee: 261
1653 deg
Mean anomaly: 98
8767 deg
Mean motion: 15
53693600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 336
Coasting Arc #15 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2016/332/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4920730
47 A = 6781482
65 meter
Y = 989147
46 meter E =
0004993
Z = 4561458
89 I = 51
42238
XDOT = -3997
629769 Wp = 162
46968
YDOT = 5784
962226 meter/sec RA = 324
90443 deg
ZDOT = 3052
487177 TA = 256
88158
MA = 256
93731
Ha = 219
598 n
mi
Hp = 217
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16144128
83 X = 4887145
80
Y = 3245234
44 feet Y = 1043986
45 meter
Z = 14965416
31 Z = 4585281
51
XDOT = -13115
583230 XDOT = -4076
849551
YDOT = 18979
534861 feet/sec YDOT = 5739
815009 meter/sec
ZDOT = 10014
721709 ZDOT = 3032
875052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3313071
74 X = -1009824
27
Y = -16033159
31 feet Y = -4886906
96 meter
Z = 15069488
57 Z = 4593180
12
XDOT = 21461
629701 XDOT = 6541
504733
YDOT = 4913
186846 feet/sec YDOT = 1497
539351 meter/sec
ZDOT = 9927
721169 ZDOT = 3025
969412
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 16332
18558964
00016717 00000-0 10270-3 0 9143
2 25544 51
6422 325
2281 0006432 258
5489 101
4941 15
53752341 30336
Satellite: ISS
Catalog Number: 25544
Epoch time: 16332
18558964 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 325
2281 deg
Eccentricity:
0006432
Arg of perigee: 258
5489 deg
Mean anomaly: 101
4941 deg
Mean motion: 15
53752341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 303
Coasting Arc #16 (Orbit 3047)
---------------------------------------
Vector Time (GMT): 2016/333/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3858093
79 A = 6779094
73 meter
Y = -2134400
41 meter E =
0007650
Z = -5156152
99 I = 51
38836
XDOT = 4984
788114 Wp = 76
65334
YDOT = -5650
292860 meter/sec RA = 319
89707 deg
ZDOT = -1390
931002 TA = 179
91309
MA = 179
91295
Ha = 219
444 n
mi
Hp = 217
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12657788
03 X = -3808892
76
Y = -7002626
01 feet Y = -2177268
87 meter
Z = -16916512
45 Z = -5174775
62
XDOT = 16354
291713 XDOT = 5054
357333
YDOT = -18537
706235 feet/sec YDOT = -5594
160563 meter/sec
ZDOT = -4563
421921 ZDOT = -1366
546940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1270344
79 X = -387201
09
Y = 14314076
86 feet Y = 4362930
63 meter
Z = -16997593
65 Z = -5180866
55
XDOT = -22568
150886 XDOT = -6878
772390
YDOT = -7293
701839 feet/sec YDOT = -2223
120321 meter/sec
ZDOT = -4455
567492 ZDOT = -1358
056971
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 16333
15036811
00016717 00000-0 10270-3 0 9154
2 25544 51
6422 320
4225 0006285 262
9051 97
1387 15
53739682 30485
Satellite: ISS
Catalog Number: 25544
Epoch time: 16333
15036811 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 320
4225 deg
Eccentricity:
0006285
Arg of perigee: 262
9051 deg
Mean anomaly: 97
1387 deg
Mean motion: 15
53739682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3048
Checksum: 303
Coasting Arc #17 (Orbit 3063)
---------------------------------------
Vector Time (GMT): 2016/334/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2680979
10 A = 6778492
10 meter
Y = 3295356
56 meter E =
0003801
Z = 5285433
94 I = 51
36227
XDOT = -5619
144008 Wp = 277
06838
YDOT = 5199
170602 meter/sec RA = 314
88261 deg
ZDOT = -391
106572 TA = 176
67811
MA = 176
67558
Ha = 219
200 n
mi
Hp = 217
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8795863
17 X = 2618255
47
Y = 10811537
28 feet Y = 3324986
04 meter
Z = 17340662
53 Z = 5298305
56
XDOT = -18435
511836 XDOT = -5674
964973
YDOT = 17057
646331 feet/sec YDOT = 5136
021470 meter/sec
ZDOT = -1283
158045 ZDOT = -418
538751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6112046
18 X = 1862951
68
Y = -12448506
47 feet Y = -3794304
77 meter
Z = 17396341
64 Z = 5302404
93
XDOT = 22353
036891 XDOT = 6813
205644
YDOT = 9011
643754 feet/sec YDOT = 2746
749016 meter/sec
ZDOT = -1404
258421 ZDOT = -428
017967
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 16334
17946021
00016717 00000-0 10270-3 0 9161
2 25544 51
6421 315
2951 0006308 266
8593 93
1837 15
53757019 30640
Satellite: ISS
Catalog Number: 25544
Epoch time: 16334
17946021 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 315
2951 deg
Eccentricity:
0006308
Arg of perigee: 266
8593 deg
Mean anomaly: 93
1837 deg
Mean motion: 15
53757019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3064
Checksum: 315
Coasting Arc #18 (Orbit 3078)
---------------------------------------
Vector Time (GMT): 2016/335/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1481123
79 A = 6779968
46 meter
Y = -4399664
49 meter E =
0006620
Z = -4947444
30 I = 51
34605
XDOT = 5900
904142 Wp = 120
67629
YDOT = -4394
617271 meter/sec RA = 309
86920 deg
ZDOT = 2140
309595 TA = 170
28773
MA = 170
27492
Ha = 219
267 n
mi
Hp = 217
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4859330
02 X = -1407782
58
Y = -14434594
80 feet Y = -4415816
97 meter
Z = -16231772
62 Z = -4954461
53
XDOT = 19359
921727 XDOT = 5939
210435
YDOT = -14418
035666 feet/sec YDOT = -4328
415374 meter/sec
ZDOT = 7022
013107 ZDOT = 2169
067906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10878144
44 X = -3315658
42
Y = 10614471
63 feet Y = 3235290
95 meter
Z = -16261611
96 Z = -4956539
32
XDOT = -20664
366039 XDOT = -6298
498769
YDOT = -10219
742730 feet/sec YDOT = -3114
977584 meter/sec
ZDOT = 7148
753512 ZDOT = 2178
940071
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 16335
14423051
00016717 00000-0 10270-3 0 9173
2 25544 51
6430 310
4897 0006254 270
0872 89
9564 15
53769869 30795
Satellite: ISS
Catalog Number: 25544
Epoch time: 16335
14423051 = yrday
fracday
Element set: 917
Inclination: 51
6430 deg
RA of node: 310
4897 deg
Eccentricity:
0006254
Arg of perigee: 270
0872 deg
Mean anomaly: 89
9564 deg
Mean motion: 15
53769869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3079
Checksum: 332
Coasting Arc #19 (Orbit 3094)
---------------------------------------
Vector Time (GMT): 2016/336/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 330625
20 A = 6783132
40 meter
Y = 5347312
52 meter E =
0004945
Z = 4158972
43 I = 51
33659
XDOT = -5874
203941 Wp = 51
91201
YDOT = 3248
550885 meter/sec RA = 304
85907 deg
ZDOT = -3703
769366 TA = 76
33708
MA = 76
28202
Ha = 219
420 n
mi
Hp = 217
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1084728
36 X = 250602
84
Y = 17543676
26 feet Y = 5350562
02 meter
Z = 13644922
66 Z = 4160384
62
XDOT = -19272
322640 XDOT = -5892
101925
YDOT = 10657
975345 feet/sec YDOT = 3182
761824 meter/sec
ZDOT = -12151
474297 ZDOT = -3732
348374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15171806
83 X = 4624366
72
Y = -8867558
58 feet Y = -2702831
86 meter
Z = 13650047
96 Z = 4160534
62
XDOT = 17574
034696 XDOT = 5356
565775
YDOT = 11139
095338 feet/sec YDOT = 3395
196259 meter/sec
ZDOT = -12277
200234 ZDOT = -3742
090631
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 16336
17331427
00016717 00000-0 10270-3 0 9183
2 25544 51
6433 305
3626 0006122 274
4462 85
5991 15
53736500 30958
Satellite: ISS
Catalog Number: 25544
Epoch time: 16336
17331427 = yrday
fracday
Element set: 918
Inclination: 51
6433 deg
RA of node: 305
3626 deg
Eccentricity:
0006122
Arg of perigee: 274
4462 deg
Mean anomaly: 85
5991 deg
Mean motion: 15
53736500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3095
Checksum: 305
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