[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 27th 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
5
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
223/08:45:00
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
9
Coasting Arc #1 (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 = -5991176
54 A = 6783833
91 meter
Y = -1632265
77 meter E =
0006721
Z = -2732890
41 I = 51
42840
XDOT = -803
873407 Wp = 65
31309
YDOT = -5630
607273 meter/sec RA = 215
78727 deg
ZDOT = 5137
979063 TA = 263
67393
MA = 263
75049
Ha = 220
489 n
mi
Hp = 212
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19656091
00 X = -5959203
73
Y = -5355202
67 feet Y = -1699084
22 meter
Z = -8966175
88 Z = -2761916
27
XDOT = -2637
379943 XDOT = -765
808719
YDOT = -18473
120974 feet/sec YDOT = -5639
384108 meter/sec
ZDOT = 16856
886689 ZDOT = 5134
166286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6768375
15 X = 2063000
75
Y = 19155902
35 feet Y = 5838719
04 meter
Z = -9092465
12 Z = -2771383
37
XDOT = -12215
912057 XDOT = -3723
409995
YDOT = 12290
519965 feet/sec YDOT = 3746
150485 meter/sec
ZDOT = 16841
202764 ZDOT = 5133
198603
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
50561190
00016717 00000-0 10270-3 0 9002
2 25544 51
6406 216
8707 0002047 79
2092 280
9291 15
54896772 11251
Satellite: ISS
Catalog Number: 25544
Epoch time: 16209
50561190 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 216
8707 deg
Eccentricity:
0002047
Arg of perigee: 79
2092 deg
Mean anomaly: 280
9291 deg
Mean motion: 15
54896772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 307
Coasting Arc #2 (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 = 6100432
82 A = 6786749
27 meter
Y = 2828040
51 meter E =
0014997
Z = 871397
93 I = 51
46390
XDOT = -1322
908712 Wp = 119
81814
YDOT = 4698
407893 meter/sec RA = 210
79596 deg
ZDOT = -5917
672295 TA = 50
72521
MA = 50
59227
Ha = 220
538 n
mi
Hp = 212
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20014543
36 X = 6064122
71
Y = 9278348
12 feet Y = 2896056
54 meter
Z = 2858917
09 Z = 900944
07
XDOT = -4340
251681 XDOT = -1346
603879
YDOT = 15414
724060 feet/sec YDOT = 4683
482111 meter/sec
ZDOT = -19414
935350 ZDOT = -5924
155880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4145021
88 X = -1263402
67
Y = -21650357
39 feet Y = -6599028
93 meter
Z = 2987292
28 Z = 910526
69
XDOT = 13394
267132 XDOT = 4082
572622
YDOT = -5277
222112 feet/sec YDOT = -1608
497300 meter/sec
ZDOT = -19443
991060 ZDOT = -5926
528475
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
53394243
00016717 00000-0 10270-3 0 9011
2 25544 51
6398 211
7380 0002092 79
1826 280
9563 15
54896210 11413
Satellite: ISS
Catalog Number: 25544
Epoch time: 16210
53394243 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 211
7380 deg
Eccentricity:
0002092
Arg of perigee: 79
1826 deg
Mean anomaly: 280
9563 deg
Mean motion: 15
54896210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1141
Checksum: 298
Coasting Arc #3 (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 = -5606701
60 A = 6786525
79 meter
Y = -3658211
92 meter E =
0015301
Z = 1070660
22 I = 51
49071
XDOT = 3438
119448 Wp = 60
39491
YDOT = -3532
668158 meter/sec RA = 205
81226 deg
ZDOT = 5878
136923 TA = 311
24824
MA = 311
37997
Ha = 220
440 n
mi
Hp = 212
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18394690
28 X = -5570578
60
Y = -12002007
63 feet Y = -3720707
91 meter
Z = 3512664
75 Z = 1043512
01
XDOT = 11279
919450 XDOT = 3448
813937
YDOT = -11590
118627 feet/sec YDOT = -3494
161436 meter/sec
ZDOT = 19285
226124 ZDOT = 5894
864003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1390191
99 X = 423730
52
Y = 21938411
10 feet Y = 6686827
70 meter
Z = 3394866
15 Z = 1034755
20
XDOT = -14358
620696 XDOT = -4376
507588
YDOT = -2115
129331 feet/sec YDOT = -644
691420 meter/sec
ZDOT = 19358
765526 ZDOT = 5900
551732
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
56226791
00016717 00000-0 10270-3 0 9028
2 25544 51
6389 206
6068 0001952 87
2690 272
8686 15
54938425 11570
Satellite: ISS
Catalog Number: 25544
Epoch time: 16211
56226791 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 206
6068 deg
Eccentricity:
0001952
Arg of perigee: 87
2690 deg
Mean anomaly: 272
8686 deg
Mean motion: 15
54938425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1157
Checksum: 332
Coasting Arc #4 (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 = 4483579
15 A = 6783599
04 meter
Y = 4179824
70 meter E =
0006438
Z = -2908643
33 I = 51
50892
XDOT = -5339
175500 Wp = 107
10244
YDOT = 2240
907176 meter/sec RA = 200
82379 deg
ZDOT = -5020
962000 TA = 106
10797
MA = 106
03707
Ha = 220
570 n
mi
Hp = 212
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14709905
35 X = 4450634
81
Y = 13713335
64 feet Y = 4229779
10 meter
Z = -9542793
08 Z = -2886943
23
XDOT = -17516
979987 XDOT = -5339
447744
YDOT = 7352
057663 feet/sec YDOT = 2181
199806 meter/sec
ZDOT = -16472
972441 ZDOT = -5046
898512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1815792
11 X = 553453
44
Y = -20072976
66 feet Y = -6118243
29 meter
Z = -9448825
15 Z = -2880001
91
XDOT = 14999
340052 XDOT = 4571
798848
YDOT = 9147
230283 feet/sec YDOT = 2788
075790 meter/sec
ZDOT = -16586
479076 ZDOT = -5055
558822
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
52632563
00016717 00000-0 10270-3 0 9034
2 25544 51
6380 201
7948 0002040 84
3410 275
7975 15
54888552 11726
Satellite: ISS
Catalog Number: 25544
Epoch time: 16212
52632563 = yrday
fracday
Element set: 903
Inclination: 51
6380 deg
RA of node: 201
7948 deg
Eccentricity:
0002040
Arg of perigee: 84
3410 deg
Mean anomaly: 275
7975 deg
Mean motion: 15
54888552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 304
Coasting Arc #5 (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 = -2858893
90 A = 6779188
36 meter
Y = -4372570
88 meter E =
0011557
Z = 4312420
26 I = 51
52527
XDOT = 6763
979477 Wp = 104
79163
YDOT = -967
496760 meter/sec RA = 195
82611 deg
ZDOT = 3492
425162 TA = 309
61258
MA = 309
71454
Ha = 220
481 n
mi
Hp = 212
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9379573
17 X = -2830733
73
Y = -14345704
98 feet Y = -4404383
79 meter
Z = 14148360
42 Z = 4298600
81
XDOT = 22191
533717 XDOT = 6757
331170
YDOT = -3174
201967 feet/sec YDOT = -891
894842 meter/sec
ZDOT = 11458
087802 ZDOT = 3525
266075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5276713
49 X = -1608342
27
Y = 16358915
75 feet Y = 4986197
52 meter
Z = 14088786
92 Z = 4294262
25
XDOT = -15108
794272 XDOT = -4605
160494
YDOT = -14895
483387 feet/sec YDOT = -4540
143336 meter/sec
ZDOT = 11601
523040 ZDOT = 3536
144223
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
55464740
00016717 00000-0 10270-3 0 9049
2 25544 51
6383 196
6631 0001830 87
8638 272
2724 15
54921190 11883
Satellite: ISS
Catalog Number: 25544
Epoch time: 16213
55464740 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 196
6631 deg
Eccentricity:
0001830
Arg of perigee: 87
8638 deg
Mean anomaly: 272
2724 deg
Mean motion: 15
54921190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1188
Checksum: 316
Coasting Arc #6 (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 = 856763
57 A = 6775882
82 meter
Y = 4330880
46 meter E =
0015681
Z = -5154195
33 I = 51
54548
XDOT = -7512
647500 Wp = 80
12224
YDOT = -252
907544 meter/sec RA = 190
81629 deg
ZDOT = -1462
477889 TA = 175
76914
MA = 175
75587
Ha = 220
527 n
mi
Hp = 212
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2810904
09 X = 833307
21
Y = 14208925
39 feet Y = 4340330
51 meter
Z = -16910089
67 Z = -5150090
20
XDOT = -24647
793636 XDOT = -7502
157137
YDOT = -829
749160 feet/sec YDOT = -336
860246 meter/sec
ZDOT = -4798
155805 ZDOT = -1498
946207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9071098
67 X = 2764870
88
Y = -11317753
59 feet Y = -3449651
29 meter
Z = -16892883
05 Z = -5148950
76
XDOT = 14251
028414 XDOT = 4343
713461
YDOT = 18815
549730 feet/sec YDOT = 5734
979558 meter/sec
ZDOT = -4957
240707 ZDOT = -1510
966967
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
51869797
00016717 00000-0 10270-3 0 9058
2 25544 51
6385 191
8509 0002009 87
4705 272
6678 15
54895313 12033
Satellite: ISS
Catalog Number: 25544
Epoch time: 16214
51869797 = yrday
fracday
Element set: 905
Inclination: 51
6385 deg
RA of node: 191
8509 deg
Eccentricity:
0002009
Arg of perigee: 87
4705 deg
Mean anomaly: 272
6678 deg
Mean motion: 15
54895313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 335
Coasting Arc #7 (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 = 1274773
60 A = 6775272
33 meter
Y = -4066981
47 meter E =
0004841
Z = 5262905
53 I = 51
57521
XDOT = 7512
138555 Wp = 73
78497
YDOT = 1369
203790 meter/sec RA = 185
80342 deg
ZDOT = -759
604952 TA = 23
48509
MA = 23
46299
Ha = 220
443 n
mi
Hp = 212
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4182328
09 X = 1294592
54
Y = -13343115
07 feet Y = -4052615
50 meter
Z = 17266750
42 Z = 5269145
89
XDOT = 24646
123868 XDOT = 7499
959206
YDOT = 4492
138419 feet/sec YDOT = 1453
141473 meter/sec
ZDOT = -2492
142230 ZDOT = -723
143241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12773142
31 X = -3893253
78
Y = 5604771
46 feet Y = 1708334
34 meter
Z = 17294641
66 Z = 5271406
78
XDOT = -12252
255009 XDOT = -3734
487327
YDOT = -20703
667297 feet/sec YDOT = -6310
477792 meter/sec
ZDOT = -2333
243765 ZDOT = -711
172699
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
54701604
00016717 00000-0 10270-3 0 9065
2 25544 51
6383 186
7191 0001902 90
4883 269
6488 15
54898081 12190
Satellite: ISS
Catalog Number: 25544
Epoch time: 16215
54701604 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 186
7191 deg
Eccentricity:
0001902
Arg of perigee: 90
4883 deg
Mean anomaly: 269
6488 deg
Mean motion: 15
54898081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 329
Coasting Arc #8 (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 = -3300006
48 A = 6777784
08 meter
Y = 3653836
12 meter E =
0012526
Z = -4670196
78 I = 51
61682
XDOT = -6691
292825 Wp = 107
36843
YDOT = -2371
101027 meter/sec RA = 180
79586 deg
ZDOT = 2875
766815 TA = 191
23619
MA = 191
26418
Ha = 220
473 n
mi
Hp = 212
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10826792
91 X = -3317934
07
Y = 11987651
31 feet Y = 3616833
09 meter
Z = -15322167
90 Z = -4686270
47
XDOT = -21953
060449 XDOT = -6678
250171
YDOT = -7779
202843 feet/sec YDOT = -2445
854665 meter/sec
ZDOT = 9434
930495 ZDOT = 2843
294591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16085636
84 X = 4902902
11
Y = 51496
70 feet Y = 15696
19 meter
Z = -15392910
49 Z = -4691759
12
XDOT = 8819
400241 XDOT = 2688
153193
YDOT = 20446
093703 feet/sec YDOT = 6231
969361 meter/sec
ZDOT = 9293
583350 ZDOT = 2832
684205
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
51106128
00016717 00000-0 10270-3 0 9074
2 25544 51
6393 181
9079 0001878 92
5222 267
6146 15
54893953 12344
Satellite: ISS
Catalog Number: 25544
Epoch time: 16216
51106128 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 181
9079 deg
Eccentricity:
0001878
Arg of perigee: 92
5222 deg
Mean anomaly: 267
6146 deg
Mean motion: 15
54893953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 322
Coasting Arc #9 (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 = -3181303
04 A = 6777460
18 meter
Y = -3638576
87 meter E =
0009627
Z = 4745609
32 I = 51
63904
XDOT = 6773
364201 Wp = 116
34615
YDOT = -2392
592851 meter/sec RA = 177
83688 deg
ZDOT = 2697
764694 TA = 306
97068
MA = 307
05878
Ha = 220
451 n
mi
Hp = 212
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10437345
92 X = -3163430
70
Y = -11937588
17 feet Y = -3674052
44 meter
Z = 15569584
37 Z = 4730199
08
XDOT = 22222
323495 XDOT = 6786
511097
YDOT = -7849
714077 feet/sec YDOT = -2316
775078 meter/sec
ZDOT = 8850
934037 ZDOT = 2730
699153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7943329
85 X = -2421126
94
Y = -13799263
42 feet Y = -4206015
49 meter
Z = 15502902
91 Z = 4725284
81
XDOT = 22279
011821 XDOT = 6790
642803
YDOT = -2687
805224 feet/sec YDOT = -819
243032 meter/sec
ZDOT = 8995
073300 ZDOT = 2741
698342
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
15375514
00016717 00000-0 10270-3 0 9083
2 25544 51
6429 178
6972 0001861 109
8384 250
2970 15
54946207 12447
Satellite: ISS
Catalog Number: 25544
Epoch time: 16217
15375514 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 178
6972 deg
Eccentricity:
0001861
Arg of perigee: 109
8384 deg
Mean anomaly: 250
2970 deg
Mean motion: 15
54946207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 324
Coasting Arc #10 (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 = 1130410
87 A = 6775178
53 meter
Y = 4083089
89 meter E =
0016375
Z = -5301295
45 I = 51
66337
XDOT = -7513
313051 Wp = 88
53284
YDOT = 1377
087206 meter/sec RA = 172
83329 deg
ZDOT = -542
484964 TA = 176
29148
MA = 176
27933
Ha = 220
394 n
mi
Hp = 212
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3708697
09 X = 1110419
58
Y = 13395964
20 feet Y = 4095619
06 meter
Z = -17392701
61 Z = -5295852
91
XDOT = -24649
977203 XDOT = -7525
518485
YDOT = 4518
002644 feet/sec YDOT = 1293
000067 meter/sec
ZDOT = -1779
806311 ZDOT = -579
011642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1309430
61 X = 399114
45
Y = 13867045
65 feet Y = 4226675
51 meter
Z = -17369594
02 Z = -5294252
26
XDOT = -24037
477265 XDOT = -7326
623070
YDOT = -155
275788 feet/sec YDOT = -47
328060 meter/sec
ZDOT = -1939
479306 ZDOT = -591
153292
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
11779664
00016717 00000-0 10270-3 0 9095
2 25544 51
6430 173
8871 0001819 110
0245 250
1104 15
54916974 12599
Satellite: ISS
Catalog Number: 25544
Epoch time: 16218
11779664 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 173
8871 deg
Eccentricity:
0001819
Arg of perigee: 110
0245 deg
Mean anomaly: 250
1104 deg
Mean motion: 15
54916974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 308
Coasting Arc #11 (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 = 1004451
47 A = 6775830
38 meter
Y = -4338948
55 meter E =
0006166
Z = 5102053
87 I = 51
69816
XDOT = 7482
247238 Wp = 69
78007
YDOT = -252
920766 meter/sec RA = 167
82820 deg
ZDOT = -1684
403859 TA = 36
48383
MA = 36
44184
Ha = 220
302 n
mi
Hp = 212
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3295444
45 X = 1028112
91
Y = -14235395
50 feet Y = -4327583
68 meter
Z = 16739021
87 Z = 5106990
72
XDOT = 24548
055243 XDOT = 7492
701327
YDOT = -829
792538 feet/sec YDOT = -169
190864 meter/sec
ZDOT = -5526
259381 ZDOT = -1648
032247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5502648
96 X = 1677207
40
Y = -13508594
01 feet Y = -4117419
45 meter
Z = 16761265
91 Z = 5108833
85
XDOT = 23395
707147 XDOT = 7131
011538
YDOT = 2855
108280 feet/sec YDOT = 870
237004 meter/sec
ZDOT = -5367
426579 ZDOT = -1635
991621
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
14610404
00016717 00000-0 10270-3 0 9107
2 25544 51
6432 168
7550 0001806 113
2194 246
9150 15
54953307 12755
Satellite: ISS
Catalog Number: 25544
Epoch time: 16219
14610404 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 168
7550 deg
Eccentricity:
0001806
Arg of perigee: 113
2194 deg
Mean anomaly: 246
9150 deg
Mean motion: 15
54953307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 286
Coasting Arc #12 (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 = -2975848
07 A = 6779321
59 meter
Y = 4402431
22 meter E =
0009955
Z = -4220209
58 I = 51
74120
XDOT = -6650
860711 Wp = 111
73570
YDOT = -977
441614 meter/sec RA = 162
83362 deg
ZDOT = 3673
517098 TA = 195
88897
MA = 195
92023
Ha = 220
319 n
mi
Hp = 212
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9763281
07 X = -3004356
35
Y = 14443671
98 feet Y = 4368993
77 meter
Z = -13845831
96 Z = -4234734
66
XDOT = -21820
409156 XDOT = -6657
280500
YDOT = -3206
829443 feet/sec YDOT = -1051
851771 meter/sec
ZDOT = 12052
221451 ZDOT = 3641
193811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11714699
87 X = -3570640
52
Y = 12842406
18 feet Y = 3914365
40 meter
Z = -13909952
94 Z = -4239753
66
XDOT = -20240
679453 XDOT = -6169
359097
YDOT = -5573
820112 feet/sec YDOT = -1698
900370 meter/sec
ZDOT = 11911
245254 ZDOT = 3630
547553
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
11014008
00016717 00000-0 10270-3 0 9115
2 25544 51
6432 163
9449 0001845 116
6830 243
4512 15
54951494 12902
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
11014008 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 163
9449 deg
Eccentricity:
0001845
Arg of perigee: 116
6830 deg
Mean anomaly: 243
4512 deg
Mean motion: 15
54951494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1290
Checksum: 281
Coasting Arc #13 (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 = -3988247
23 A = 6777370
29 meter
Y = -2673432
03 meter E =
0009594
Z = 4777569
43 I = 51
73771
XDOT = 5923
883263 Wp = 116
00202
YDOT = -4099
402403 meter/sec RA = 162
13549 deg
ZDOT = 2643
002881 TA = 307
93602
MA = 308
02269
Ha = 220
548 n
mi
Hp = 212
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13084800
62 X = -3981262
86
Y = -8771102
47 feet Y = -2717992
08 meter
Z = 15674440
38 Z = 4758212
85
XDOT = 19435
312544 XDOT = 5956
445164
YDOT = -13449
482951 feet/sec YDOT = -4032
975437 meter/sec
ZDOT = 8671
269294 ZDOT = 2671
858407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15506040
26 X = -4726241
07
Y = 3214973
82 feet Y = 979924
02 meter
Z = 15590349
13 Z = 4751938
41
XDOT = 4289
565152 XDOT = 1307
459458
YDOT = -22106
397203 feet/sec YDOT = -6738
029867 meter/sec
ZDOT = 8797
914289 ZDOT = 2681
604275
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
30294688
00016717 00000-0 10270-3 0 9121
2 25544 51
6420 162
9836 0002002 106
3819 253
7554 15
54939966 12930
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
30294688 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 162
9836 deg
Eccentricity:
0002002
Arg of perigee: 106
3819 deg
Mean anomaly: 253
7554 deg
Mean motion: 15
54939966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 315
Coasting Arc #14 (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 = 2119343
99 A = 6775135
61 meter
Y = 3650621
74 meter E =
0016498
Z = -5313669
78 I = 51
76146
XDOT = -6888
855031 Wp = 89
10508
YDOT = 3310
302143 meter/sec RA = 157
13769 deg
ZDOT = -474
364948 TA = 176
37737
MA = 176
36541
Ha = 220
414 n
mi
Hp = 212
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6953228
32 X = 2104175
52
Y = 11977105
46 feet Y = 3674236
70 meter
Z = -17433299
79 Z = -5303411
60
XDOT = -22601
230418 XDOT = -6923
055441
YDOT = 10860
571336 feet/sec YDOT = 3233
075121 meter/sec
ZDOT = -1556
315445 ZDOT = -507
912043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13540970
87 X = 4127287
92
Y = 3159130
15 feet Y = 962902
87 meter
Z = -17389088
12 Z = -5300194
06
XDOT = -7514
432304 XDOT = -2290
398966
YDOT = 22851
756139 feet/sec YDOT = 6965
215271 meter/sec
ZDOT = -1703
335063 ZDOT = -519
176527
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
26697902
00016717 00000-0 10270-3 0 9134
2 25544 51
6430 158
1728 0001901 110
1125 250
0233 15
54922664 13086
Satellite: ISS
Catalog Number: 25544
Epoch time: 16221
26697902 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 158
1728 deg
Eccentricity:
0001901
Arg of perigee: 110
1125 deg
Mean anomaly: 250
0233 deg
Mean motion: 15
54922664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 274
Coasting Arc #15 (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 = -124617
66 A = 6775906
51 meter
Y = -4465821
24 meter E =
0006512
Z = 5089782
87 I = 51
79199
XDOT = 7136
278887 Wp = 70
24600
YDOT = -2207
085701 meter/sec RA = 152
13954 deg
ZDOT = -1757
818930 TA = 36
72520
MA = 36
68059
Ha = 220
406 n
mi
Hp = 212
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -408850
59 X = -99394
19
Y = -14651644
47 feet Y = -4467073
65 meter
Z = 16698762
70 Z = 5089238
88
XDOT = 23412
988476 XDOT = 7168
967341
YDOT = -7241
094821 feet/sec YDOT = -2127
100328 meter/sec
ZDOT = -5767
122474 ZDOT = -1723
073564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11119046
53 X = -3389085
38
Y = -9553012
70 feet Y = -2911758
27 meter
Z = 16697103
73 Z = 5089277
22
XDOT = 9879
458695 XDOT = 3011
259010
YDOT = -21335
952480 feet/sec YDOT = -6503
198316 meter/sec
ZDOT = -5615
030150 ZDOT = -1711
461190
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
29527644
00016717 00000-0 10270-3 0 9144
2 25544 51
6411 153
0410 0001988 111
7317 248
4048 15
54956151 13243
Satellite: ISS
Catalog Number: 25544
Epoch time: 16222
29527644 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 153
0410 deg
Eccentricity:
0001988
Arg of perigee: 111
7317 deg
Mean anomaly: 248
4048 deg
Mean motion: 15
54956151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 291
Coasting Arc #16 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2016/223/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1755914
38 A = 6779522
62 meter
Y = 5046820
39 meter E =
0009732
Z = -4182533
79 I = 51
83341
XDOT = -6638
909989 Wp = 110
74372
YDOT = 787
038108 meter/sec RA = 147
15084 deg
ZDOT = 3740
492438 TA = 197
63149
MA = 197
66529
Ha = 220
359 n
mi
Hp = 212
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5760873
95 X = -1791901
92
Y = 16557809
68 feet Y = 5026983
30 meter
Z = -13722223
73 Z = -4191150
99
XDOT = -21781
200751 XDOT = -6665
386983
YDOT = 2582
146023 feet/sec YDOT = 712
649390 meter/sec
ZDOT = 12271
956817 ZDOT = 3708
178221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8587901
27 X = 2617592
31
Y = 15249259
66 feet Y = 4647974
34 meter
Z = -13760675
34 Z = -4194253
84
XDOT = -11501
968902 XDOT = -3505
800121
YDOT = 17413
253323 feet/sec YDOT = 5307
559613 meter/sec
ZDOT = 12130
694636 ZDOT = 3697
435725
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 16223
25930194
00016717 00000-0 10270-3 0 9150
2 25544 51
6425 148
2300 0001853 112
8484 247
2865 15
54938103 13397
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
25930194 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 148
2300 deg
Eccentricity:
0001853
Arg of perigee: 112
8484 deg
Mean anomaly: 247
2865 deg
Mean motion: 15
54938103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 301
Coasting Arc #17 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2016/223/08:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5392162
09 A = 6779934
71 meter
Y = 313181
36 meter E =
0008760
Z = -4106612
84 I = 51
83519
XDOT = -3260
718129 Wp = 79
62636
YDOT = 5767
988256 meter/sec RA = 146
62960 deg
ZDOT = -3847
012631 TA = 150
70886
MA = 150
65972
Ha = 220
386 n
mi
Hp = 212
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17690820
50 X = 5408207
25
Y = 1027497
90 feet Y = 373569
78 meter
Z = -13473139
24 Z = -4080380
31
XDOT = -10697
894125 XDOT = -3306
287912
YDOT = 18923
845983 feet/sec YDOT = 5731
269879 meter/sec
ZDOT = -12621
432517 ZDOT = -3862
963013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1131577
12 X = 344904
71
Y = -17771136
10 feet Y = -5416642
28 meter
Z = -13358615
86 Z = -4071706
12
XDOT = 17563
579194 XDOT = 5353
378938
YDOT = 10645
492588 feet/sec YDOT = 3244
746141 meter/sec
ZDOT = -12692
030387 ZDOT = -3868
530862
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 16223
38783933
00016717 00000-0 10270-3 0 9162
2 25544 51
6400 147
5877 0001845 111
6438 248
4911 15
54943134 13416
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
38783933 = yrday
fracday
Element set: 916
Inclination: 51
6400 deg
RA of node: 147
5877 deg
Eccentricity:
0001845
Arg of perigee: 111
6438 deg
Mean anomaly: 248
4911 deg
Mean motion: 15
54943134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 312
Coasting Arc #18 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2016/224/08:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4130893
78 A = 6776128
37 meter
Y = -1797398
13 meter E =
0007346
Z = 5057494
83 I = 51
84894
XDOT = 4793
889288 Wp = 122
43291
YDOT = -5685
882318 meter/sec RA = 141
64424 deg
ZDOT = 1889
022252 TA = 309
29105
MA = 309
35618
Ha = 220
375 n
mi
Hp = 212
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13552801
11 X = -4135054
74
Y = -5896975
48 feet Y = -1843615
79 meter
Z = 16592830
80 Z = 5037418
04
XDOT = 15727
983228 XDOT = 4847
937986
YDOT = -18654
469546 feet/sec YDOT = -5631
971633 meter/sec
ZDOT = 6197
579568 ZDOT = 1912
440876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5741043
73 X = -1749870
13
Y = 13725381
13 feet Y = 4183496
17 meter
Z = 16505426
42 Z = 5030853
97
XDOT = -17828
764140 XDOT = -5434
207310
YDOT = -15057
578586 feet/sec YDOT = -4589
549953 meter/sec
ZDOT = 6300
800584 ZDOT = 1920
484018
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 16224
41612778
00016717 00000-0 10270-3 0 9176
2 25544 51
6398 142
4562 0001652 115
1182 245
0142 15
54967399 13573
Satellite: ISS
Catalog Number: 25544
Epoch time: 16224
41612778 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 142
4562 deg
Eccentricity:
0001652
Arg of perigee: 115
1182 deg
Mean anomaly: 245
0142 deg
Mean motion: 15
54967399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 313
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