[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 22nd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
137/21:35:06
575 0
4 0
7 0
7
N/A 0
4 -0
1 222
4
000/00:00:13
149 -0
3 0
0 214
3
138/01:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
5
138/04:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
3
138/08:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
3
140/17:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
7
150/04:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 215
8
Coasting Arc #1 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2017/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915820
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2558528
52 A = 6780488
09 meter
Y = -4211164
09 meter E =
0011938
Z = 4654634
71 I = 51
55661
XDOT = 7026
482221 Wp = 135
76845
YDOT = -1068
237223 meter/sec RA = 190
13978 deg
ZDOT = 2882
963776 TA = 285
48494
MA = 285
61674
Ha = 222
222 n
mi
Hp = 214
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8394122
44 X = -2533858
14
Y = -13816155
16 feet Y = -4239637
63 meter
Z = 15271111
25 Z = 4642265
73
XDOT = 23052
763193 XDOT = 7023
901168
YDOT = -3504
715300 feet/sec YDOT = -989
676950 meter/sec
ZDOT = 9458
542572 ZDOT = 2917
090198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16179404
41 X = -4931482
46
Y = -1103153
86 feet Y = -336241
30 meter
Z = 15217233
60 Z = 4638212
80
XDOT = 10412
075495 XDOT = 3173
600611
YDOT = -19574
683401 feet/sec YDOT = -5966
363500 meter/sec
ZDOT = 9609
087031 ZDOT = 2928
849727
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 17137
55345051
00016717 00000-0 10270-3 0 9004
2 25544 51
6389 191
0057 0005051 169
7469 190
3787 15
54030000 16987
Satellite: ISS
Catalog Number: 25544
Epoch time: 17137
55345051 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 191
0057 deg
Eccentricity:
0005051
Arg of perigee: 169
7469 deg
Mean anomaly: 190
3787 deg
Mean motion: 15
54030000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 305
Coasting Arc #2 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2017/137/21:35:13
149
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5358058
48 A = 6784494
11 meter
Y = -2102123
89 meter E =
0013889
Z = 3576283
24 I = 51
58261
XDOT = 4625
125439 Wp = 108
69312
YDOT = 4216
312550 meter/sec RA = 188
10212 deg
ZDOT = -4441
356927 TA = 28
96148
MA = 28
88449
Ha = 222
413 n
mi
Hp = 214
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17578932
01 X = 5363794
79
Y = -6896731
91 feet Y = -2042174
58 meter
Z = 11733212
72 Z = 3602325
05
XDOT = 15174
296061 XDOT = 4599
207882
YDOT = 13833
046424 feet/sec YDOT = 4267
889172 meter/sec
ZDOT = -14571
380993 ZDOT = -4418
952034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14364253
32 X = -4378224
41
Y = 12146533
44 feet Y = 3702263
39 meter
Z = 11848290
78 Z = 3611359
03
XDOT = -18013
920404 XDOT = -5490
642939
YDOT = -7154
056365 feet/sec YDOT = -2180
556380 meter/sec
ZDOT = -14473
272226 ZDOT = -4411
453374
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 17137
93929573
00016717 00000-0 10270-3 0 9014
2 25544 51
6398 189
0848 0005258 166
2909 193
8387 15
53887043 17040
Satellite: ISS
Catalog Number: 25544
Epoch time: 17137
93929573 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 189
0848 deg
Eccentricity:
0005258
Arg of perigee: 166
2909 deg
Mean anomaly: 193
8387 deg
Mean motion: 15
53887043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 358
Coasting Arc #3 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2017/138/01:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5288602
56 A = 6786406
94 meter
Y = 3053574
96 meter E =
0008580
Z = -2955324
75 I = 51
59293
XDOT = -4733
606317 Wp = 144
27717
YDOT = 3376
439147 meter/sec RA = 187
44104 deg
ZDOT = -4996
315823 TA = 69
49518
MA = 69
40311
Ha = 222
453 n
mi
Hp = 214
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17351058
27 X = 5268419
26
Y = 10018290
56 feet Y = 3112603
01 meter
Z = -9695947
33 Z = -2929683
01
XDOT = -15530
204452 XDOT = -4746
740892
YDOT = 11077
556257 feet/sec YDOT = 3323
431592 meter/sec
ZDOT = -16392
112280 ZDOT = -5019
342112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15358089
22 X = -4681145
59
Y = 12950843
02 feet Y = 3947416
95 meter
Z = -9583398
36 Z = -2921019
82
XDOT = -4204
539863 XDOT = -1281
543750
YDOT = -17156
675072 feet/sec YDOT = -5229
354562 meter/sec
ZDOT = -16494
092540 ZDOT = -5027
399406
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 17138
06791624
00016717 00000-0 10270-3 0 9024
2 25544 51
6394 188
4430 0005111 170
0057 190
1198 15
53888284 17061
Satellite: ISS
Catalog Number: 25544
Epoch time: 17138
06791624 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 188
4430 deg
Eccentricity:
0005111
Arg of perigee: 170
0057 deg
Mean anomaly: 190
1198 deg
Mean motion: 15
53888284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 309
Coasting Arc #4 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2017/138/04:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1637067
94 A = 6779213
62 meter
Y = 4228932
31 meter E =
0014010
Z = -5050535
24 I = 51
57173
XDOT = -7397
595094 Wp = 99
49333
YDOT = 626
155383 meter/sec RA = 186
75376 deg
ZDOT = -1880
259371 TA = 152
27974
MA = 152
20499
Ha = 222
565 n
mi
Hp = 214
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5370957
82 X = 1614190
46
Y = 13874449
84 feet Y = 4247111
47 meter
Z = -16569997
51 Z = -5042638
15
XDOT = -24270
325112 XDOT = -7394
913674
YDOT = 2054
315560 feet/sec YDOT = 543
445559 meter/sec
ZDOT = -6168
829956 ZDOT = -1916
188329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9490820
36 X = -2892802
05
Y = 11506660
03 feet Y = 3507229
98 meter
Z = -16535823
76 Z = -5040119
08
XDOT = -12680
210750 XDOT = -3864
928237
YDOT = -19519
743481 feet/sec YDOT = -5949
617813 meter/sec
ZDOT = -6327
265825 ZDOT = -1928
550624
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 17138
19654067
00016717 00000-0 10270-3 0 9038
2 25544 51
6376 187
7983 0005559 166
5879 193
5422 15
53911955 17085
Satellite: ISS
Catalog Number: 25544
Epoch time: 17138
19654067 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 187
7983 deg
Eccentricity:
0005559
Arg of perigee: 166
5879 deg
Mean anomaly: 193
5422 deg
Mean motion: 15
53911955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 357
Coasting Arc #5 (Orbit 1710)
---------------------------------------
Vector Time (GMT): 2017/138/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5679340
61 A = 6785708
22 meter
Y = -1930126
31 meter E =
0015338
Z = 3152953
10 I = 51
60183
XDOT = 4146
323277 Wp = 115
36209
YDOT = 4278
687474 meter/sec RA = 185
84893 deg
ZDOT = -4837
467264 TA = 28
21929
MA = 28
13627
Ha = 222
501 n
mi
Hp = 214
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18633007
27 X = 5685186
07
Y = -6332435
39 feet Y = -1866583
55 meter
Z = 10344334
33 Z = 3180555
89
XDOT = 13603
422826 XDOT = 4121
667934
YDOT = 14037
688563 feet/sec YDOT = 4324
916862 meter/sec
ZDOT = -15870
955591 ZDOT = -4817
385217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18380608
05 X = 5602409
33
Y = -6848674
00 feet Y = -2087475
84 meter
Z = 10466272
62 Z = 3190119
90
XDOT = 13594
804989 XDOT = 4143
696561
YDOT = 12306
798126 feet/sec YDOT = 3751
112069 meter/sec
ZDOT = -15783
086281 ZDOT = -4810
684699
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 17138
38947496
00016717 00000-0 10270-3 0 9041
2 25544 51
6404 186
8374 0005722 168
9796 191
1483 15
53888570 17118
Satellite: ISS
Catalog Number: 25544
Epoch time: 17138
38947496 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 186
8374 deg
Eccentricity:
0005722
Arg of perigee: 168
9796 deg
Mean anomaly: 191
1483 deg
Mean motion: 15
53888570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1711
Checksum: 353
Coasting Arc #6 (Orbit 1725)
---------------------------------------
Vector Time (GMT): 2017/139/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6447970
53 A = 6788745
07 meter
Y = 1258443
98 meter E =
0005307
Z = -1714278
85 I = 51
64465
XDOT = -2394
223686 Wp = 85
08150
YDOT = -4538
921966 meter/sec RA = 180
87306 deg
ZDOT = 5689
103877 TA = 256
13608
MA = 256
19512
Ha = 222
419 n
mi
Hp = 214
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21154758
96 X = -6453236
36
Y = 4128753
20 feet Y = 1186309
03 meter
Z = -5624274
43 Z = -1745614
09
XDOT = -7855
064586 XDOT = -2370
925437
YDOT = -14891
476265 feet/sec YDOT = -4565
565758 meter/sec
ZDOT = 18665
038968 ZDOT = 5677
529786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20909520
74 X = -6373221
92
Y = 5078140
95 feet Y = 1547817
36 meter
Z = -5762579
21 Z = -1756434
14
XDOT = -8270
995274 XDOT = -2520
999359
YDOT = -12989
482080 feet/sec YDOT = -3959
194138 meter/sec
ZDOT = 18614
696001 ZDOT = 5673
759341
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 17139
35414388
00016717 00000-0 10270-3 0 9059
2 25544 51
6408 182
0307 0005422 173
2815 186
8411 15
53877565 17264
Satellite: ISS
Catalog Number: 25544
Epoch time: 17139
35414388 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 182
0307 deg
Eccentricity:
0005422
Arg of perigee: 173
2815 deg
Mean anomaly: 186
8411 deg
Mean motion: 15
53877565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1726
Checksum: 317
Coasting Arc #7 (Orbit 1741)
---------------------------------------
Vector Time (GMT): 2017/140/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6757878
88 A = 6790002
04 meter
Y = -545079
22 meter E =
0016906
Z = 77408
38 I = 51
68059
XDOT = 457
869413 Wp = 147
10974
YDOT = 4736
339559 meter/sec RA = 175
90560 deg
ZDOT = -6019
140888 TA = 32
05649
MA = 31
95378
Ha = 222
397 n
mi
Hp = 214
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22171518
65 X = 6763095
83
Y = -1788317
65 feet Y = -469478
87 meter
Z = 253964
50 Z = 110249
06
XDOT = 1502
196236 XDOT = 434
110735
YDOT = 15539
171782 feet/sec YDOT = 4741
327113 meter/sec
ZDOT = -19747
837560 ZDOT = -6016
974234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22014730
16 X = 6710089
75
Y = -3167241
58 feet Y = -965375
23 meter
Z = 398815
78 Z = 121559
05
XDOT = 2365
795203 XDOT = 721
094378
YDOT = 13800
139712 feet/sec YDOT = 4206
282584 meter/sec
ZDOT = -19738
987328 ZDOT = -6016
443338
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 17140
38312369
00016717 00000-0 10270-3 0 9061
2 25544 51
6399 176
9035 0005664 176
8505 183
2684 15
53896646 17428
Satellite: ISS
Catalog Number: 25544
Epoch time: 17140
38312369 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 176
9035 deg
Eccentricity:
0005664
Arg of perigee: 176
8505 deg
Mean anomaly: 183
2684 deg
Mean motion: 15
53896646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1742
Checksum: 343
Coasting Arc #8 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2017/140/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1680190
26 A = 6778371
33 meter
Y = -3979279
26 meter E =
0008076
Z = 5222125
66 I = 51
65232
XDOT = 7406
055793 Wp = 155
26643
YDOT = -1653
938733 meter/sec RA = 174
08476 deg
ZDOT = 1114
752553 TA = 284
00879
MA = 284
09856
Ha = 222
199 n
mi
Hp = 214
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5512435
24 X = -1660934
86
Y = -13055378
14 feet Y = -3997960
77 meter
Z = 17132958
20 Z = 5214010
37
XDOT = 24298
083312 XDOT = 7418
585151
YDOT = -5426
308180 feet/sec YDOT = -1571
049179 meter/sec
ZDOT = 3657
324648 ZDOT = 1150
759677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4920534
61 X = -1499778
95
Y = 13335015
88 feet Y = 4064512
84 meter
Z = 17097771
43 Z = 5211400
73
XDOT = -20356
255075 XDOT = -6204
586547
YDOT = -12437
351822 feet/sec YDOT = -3790
904835 meter/sec
ZDOT = 3816
305032 ZDOT = 1163
209774
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 17140
76898977
00016717 00000-0 10270-3 0 9078
2 25544 51
6383 174
9827 0005109 178
4821 181
6348 15
53931967 17482
Satellite: ISS
Catalog Number: 25544
Epoch time: 17140
76898977 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 174
9827 deg
Eccentricity:
0005109
Arg of perigee: 178
4821 deg
Mean anomaly: 181
6348 deg
Mean motion: 15
53931967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 364
Coasting Arc #9 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2017/141/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -45188
40 A = 6778158
50 meter
Y = 4261185
81 meter E =
0015820
Z = -5284184
25 I = 51
68403
XDOT = -7571
899506 Wp = 114
44289
YDOT = 855
896893 meter/sec RA = 169
08824 deg
ZDOT = 750
331198 TA = 162
75872
MA = 162
70493
Ha = 222
081 n
mi
Hp = 214
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -148255
92 X = -67166
38
Y = 13980268
42 feet Y = 4260557
75 meter
Z = -17336562
49 Z = -5284457
02
XDOT = -24842
189981 XDOT = -7584
552404
YDOT = 2808
060673 feet/sec YDOT = 771
152016 meter/sec
ZDOT = 2461
716528 ZDOT = 713
517998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9483491
71 X = 2890568
27
Y = -10269841
83 feet Y = -3130247
79 meter
Z = -17338397
20 Z = -5284743
47
XDOT = 19455
721241 XDOT = 5930
103834
YDOT = 14058
594925 feet/sec YDOT = 4285
059733 meter/sec
ZDOT = 2299
283093 ZDOT = 700
821487
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 17141
73365426
00016717 00000-0 10270-3 0 9085
2 25544 51
6386 170
1745 0005044 181
1242 178
9900 15
53910253 17633
Satellite: ISS
Catalog Number: 25544
Epoch time: 17141
73365426 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 170
1745 deg
Eccentricity:
0005044
Arg of perigee: 181
1242 deg
Mean anomaly: 178
9900 deg
Mean motion: 15
53910253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 302
Coasting Arc #10 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2017/142/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1706660
84 A = 6780025
05 meter
Y = -4443397
87 meter E =
0005990
Z = 4822677
75 I = 51
72174
XDOT = 7239
196831 Wp = 103
96886
YDOT = 22
019475 meter/sec RA = 164
09813 deg
ZDOT = -2540
307059 TA = 10
98565
MA = 10
97257
Ha = 221
964 n
mi
Hp = 214
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5599280
99 X = 1732794
60
Y = -14578076
99 feet Y = -4424166
88 meter
Z = 15822433
57 Z = 4831031
65
XDOT = 23750
645770 XDOT = 7250
752364
YDOT = 72
242373 feet/sec YDOT = 103
037781 meter/sec
ZDOT = -8334
340746 ZDOT = -2505
112561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13786495
54 X = -4202123
84
Y = 7253742
93 feet Y = 2210940
84 meter
Z = 15859931
74 Z = 4834107
19
XDOT = -17227
085803 XDOT = -5250
815753
YDOT = -14849
771523 feet/sec YDOT = -4526
210360 meter/sec
ZDOT = -8179
157823 ZDOT = -2493
007304
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 17142
76262677
00016717 00000-0 10270-3 0 9094
2 25544 51
6382 165
0474 0004968 184
3463 175
7648 15
53914438 17795
Satellite: ISS
Catalog Number: 25544
Epoch time: 17142
76262677 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 165
0474 deg
Eccentricity:
0004968
Arg of perigee: 184
3463 deg
Mean anomaly: 175
7648 deg
Mean motion: 15
53914438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 353
Coasting Arc #11 (Orbit 1793)
---------------------------------------
Vector Time (GMT): 2017/143/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3207089
34 A = 6783399
00 meter
Y = 4525531
27 meter E =
0008804
Z = -3915208
80 I = 51
76357
XDOT = -6401
338451 Wp = 141
04786
YDOT = -1001
828253 meter/sec RA = 159
11638 deg
ZDOT = 4083
883267 TA = 171
71406
MA = 171
69951
Ha = 221
874 n
mi
Hp = 215
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10521946
65 X = -3238438
09
Y = 14847543
55 feet Y = 4489492
36 meter
Z = -12845173
24 Z = -3930864
09
XDOT = -21001
766570 XDOT = -6409
497909
YDOT = -3286
838099 feet/sec YDOT = -1073
458197 meter/sec
ZDOT = 13398
567150 ZDOT = 4052
767005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17587248
02 X = 5360593
20
Y = -4478131
87 feet Y = -1364934
60 meter
Z = -12914891
74 Z = -3936459
00
XDOT = 13545
842115 XDOT = 4128
772677
YDOT = 14937
520036 feet/sec YDOT = 4552
956107 meter/sec
ZDOT = 13261
498761 ZDOT = 4042
104822
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 17143
72728640
00016717 00000-0 10270-3 0 9100
2 25544 51
6378 160
2401 0004985 188
8546 171
2520 15
53913008 17946
Satellite: ISS
Catalog Number: 25544
Epoch time: 17143
72728640 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 160
2401 deg
Eccentricity:
0004985
Arg of perigee: 188
8546 deg
Mean anomaly: 171
2520 deg
Mean motion: 15
53913008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1794
Checksum: 310
Coasting Arc #12 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2017/144/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4421323
25 A = 6786957
98 meter
Y = -4425006
57 meter E =
0014421
Z = 2610842
64 I = 51
80643
XDOT = 5191
109099 Wp = 122
88287
YDOT = 2078
466009 meter/sec RA = 154
14605 deg
ZDOT = -5254
794967 TA = 27
77044
MA = 27
69352
Ha = 221
690 n
mi
Hp = 215
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14505653
72 X = 4457793
76
Y = -14517738
11 feet Y = -4375360
63 meter
Z = 8565756
70 Z = 2632408
78
XDOT = 17031
197832 XDOT = 5193
007118
YDOT = 6819
114202 feet/sec YDOT = 2136
527531 meter/sec
ZDOT = -17240
140969 ZDOT = -5229
572828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20387619
81 X = -6214146
52
Y = 1968118
01 feet Y = 599882
37 meter
Z = 8661545
32 Z = 2640039
01
XDOT = -8714
433927 XDOT = -2656
159461
YDOT = -14696
979643 feet/sec YDOT = -4479
639395 meter/sec
ZDOT = -17129
216415 ZDOT = -5220
985163
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 17144
75625356
00016717 00000-0 10270-3 0 9115
2 25544 51
6386 155
1119 0004912 192
8739 167
2289 15
53927840 18108
Satellite: ISS
Catalog Number: 25544
Epoch time: 17144
75625356 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 155
1119 deg
Eccentricity:
0004912
Arg of perigee: 192
8739 deg
Mean anomaly: 167
2289 deg
Mean motion: 15
53927840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 327
Coasting Arc #13 (Orbit 1824)
---------------------------------------
Vector Time (GMT): 2017/145/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5277231
43 A = 6789398
29 meter
Y = 4131935
11 meter E =
0005265
Z = -1075896
00 I = 51
84266
XDOT = -3699
303959 Wp = 58
75513
YDOT = -3193
896352 meter/sec RA = 149
18580 deg
ZDOT = 5902
900801 TA = 289
61630
MA = 289
67313
Ha = 221
626 n
mi
Hp = 215
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17313751
41 X = -5317817
31
Y = 13556217
54 feet Y = 4072694
71 meter
Z = -3529842
53 Z = -1101629
83
XDOT = -12136
824013 XDOT = -3691
988012
YDOT = -10478
662571 feet/sec YDOT = -3235
224184 meter/sec
ZDOT = 19366
472443 ZDOT = 5884
947795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21969882
41 X = 6696420
16
Y = 205923
76 feet Y = 62765
56 meter
Z = -3643991
26 Z = -1110688
54
XDOT = 3053
033850 XDOT = 930
564717
YDOT = 14238
303820 feet/sec YDOT = 4339
835004 meter/sec
ZDOT = 19287
772164 ZDOT = 5878
912956
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 17145
72090714
00016717 00000-0 10270-3 0 9128
2 25544 51
6379 150
3043 0004842 196
2552 163
8446 15
53922812 18253
Satellite: ISS
Catalog Number: 25544
Epoch time: 17145
72090714 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 150
3043 deg
Eccentricity:
0004842
Arg of perigee: 196
2552 deg
Mean anomaly: 163
8446 deg
Mean motion: 15
53922812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1825
Checksum: 305
Coasting Arc #14 (Orbit 1840)
---------------------------------------
Vector Time (GMT): 2017/146/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5739892
54 A = 6789804
67 meter
Y = -3562696
94 meter E =
0013955
Z = -591529
94 I = 51
87232
XDOT = 2065
592756 Wp = 157
23347
YDOT = 4313
823700 meter/sec RA = 144
23179 deg
ZDOT = -5997
779409 TA = 29
13289
MA = 29
05511
Ha = 221
593 n
mi
Hp = 215
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18831668
45 X = 5782178
36
Y = -11688638
26 feet Y = -3498273
07 meter
Z = -1940715
02 Z = -563544
61
XDOT = 6776
879122 XDOT = 2046
335660
YDOT = 14152
964896 feet/sec YDOT = 4336
815631 meter/sec
ZDOT = -19677
753967 ZDOT = -5987
791475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22059823
56 X = -6723834
22
Y = -2255254
18 feet Y = -687401
47 meter
Z = -1816697
29 Z = -553729
33
XDOT = 3011
953947 XDOT = 918
043563
YDOT = -13813
719397 feet/sec YDOT = -4210
421672 meter/sec
ZDOT = -19634
361148 ZDOT = -5984
553278
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 17146
74986968
00016717 00000-0 10270-3 0 9137
2 25544 51
6389 145
1763 0004919 200
1619 159
9340 15
53921074 18415
Satellite: ISS
Catalog Number: 25544
Epoch time: 17146
74986968 = yrday
fracday
Element set: 913
Inclination: 51
6389 deg
RA of node: 145
1763 deg
Eccentricity:
0004919
Arg of perigee: 200
1619 deg
Mean anomaly: 159
9340 deg
Mean motion: 15
53921074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1841
Checksum: 336
Coasting Arc #15 (Orbit 1856)
---------------------------------------
Vector Time (GMT): 2017/147/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5808830
88 A = 6787972
06 meter
Y = 2749403
99 meter E =
0011074
Z = 2175133
51 I = 51
89237
XDOT = -445
037063 Wp = 88
78911
YDOT = -5315
653553 meter/sec RA = 139
27708 deg
ZDOT = 5506
633188 TA = 295
25468
MA = 295
36941
Ha = 221
410 n
mi
Hp = 215
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19057844
08 X = -5849709
54
Y = 9020354
31 feet Y = 2684216
86 meter
Z = 7136264
80 Z = 2146816
80
XDOT = -1460
095352 XDOT = -412
311749
YDOT = -17439
808245 feet/sec YDOT = -5320
448013 meter/sec
ZDOT = 18066
381849 ZDOT = 5504
550092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20711022
31 X = 6312719
60
Y = 4170790
66 feet Y = 1271256
99 meter
Z = 7010887
83 Z = 2136918
61
XDOT = -8842
457470 XDOT = -2695
181037
YDOT = 13420
248467 feet/sec YDOT = 4090
491733 meter/sec
ZDOT = 18058
025625 ZDOT = 5504
086211
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 17147
77882929
00016717 00000-0 10270-3 0 9144
2 25544 51
6393 140
0482 0004850 204
7165 155
3756 15
53930495 18577
Satellite: ISS
Catalog Number: 25544
Epoch time: 17147
77882929 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 140
0482 deg
Eccentricity:
0004850
Arg of perigee: 204
7165 deg
Mean anomaly: 155
3756 deg
Mean motion: 15
53930495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1857
Checksum: 335
Coasting Arc #16 (Orbit 1871)
---------------------------------------
Vector Time (GMT): 2017/148/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5524289
94 A = 6784525
08 meter
Y = -1641667
58 meter E =
0004696
Z = -3578969
72 I = 51
90670
XDOT = -1076
240377 Wp = 142
60316
YDOT = 6127
444021 meter/sec RA = 134
31746 deg
ZDOT = -4478
579030 TA = 79
49040
MA = 79
43749
Ha = 221
328 n
mi
Hp = 215
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18124310
83 X = 5559621
88
Y = -5386048
51 feet Y = -1579693
22 meter
Z = -11742026
63 Z = -3552048
69
XDOT = -3530
972364 XDOT = -1122
924226
YDOT = 20103
162800 feet/sec YDOT = 6115
148323 meter/sec
ZDOT = -14693
500756 ZDOT = -4483
919701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17926472
77 X = -5463988
90
Y = -6238884
21 feet Y = -1901611
91 meter
Z = -11622962
13 Z = -3542678
86
XDOT = 14059
079703 XDOT = 4285
207494
YDOT = -13018
499702 feet/sec YDOT = -3968
038709 meter/sec
ZDOT = -14718
040202 ZDOT = -4486
058653
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 17148
74347487
00016717 00000-0 10270-3 0 9158
2 25544 51
6409 135
2411 0004793 208
6678 151
4212 15
53950220 18720
Satellite: ISS
Catalog Number: 25544
Epoch time: 17148
74347487 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 135
2411 deg
Eccentricity:
0004793
Arg of perigee: 208
6678 deg
Mean anomaly: 151
4212 deg
Mean motion: 15
53950220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1872
Checksum: 312
Coasting Arc #17 (Orbit 1887)
---------------------------------------
Vector Time (GMT): 2017/149/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4957146
35 A = 6780979
23 meter
Y = 344039
61 meter E =
0009249
Z = 4613309
08 I = 51
91640
XDOT = 2368
800201 Wp = 144
87951
YDOT = -6633
370385 meter/sec RA = 129
34989 deg
ZDOT = 3029
654005 TA = 274
93565
MA = 275
04124
Ha = 221
256 n
mi
Hp = 215
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16263603
50 X = -4983034
29
Y = 1128738
89 feet Y = 288460
17 meter
Z = 15135528
48 Z = 4589165
92
XDOT = 7771
654204 XDOT = 2428
083639
YDOT = -21763
026197 feet/sec YDOT = -6606
549729 meter/sec
ZDOT = 9939
809727 ZDOT = 3041
304155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14096556
73 X = 4296630
49
Y = 8383430
68 feet Y = 2555269
67 meter
Z = 15028913
83 Z = 4580812
94
XDOT = -18111
342486 XDOT = -5520
337190
YDOT = 12479
226876 feet/sec YDOT = 3803
668352 meter/sec
ZDOT = 9992
287650 ZDOT = 3045
649276
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 17149
77242961
00016717 00000-0 10270-3 0 9164
2 25544 51
6406 130
1134 0004771 211
4599 148
6269 15
53940393 18880
Satellite: ISS
Catalog Number: 25544
Epoch time: 17149
77242961 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 130
1134 deg
Eccentricity:
0004771
Arg of perigee: 211
4599 deg
Mean anomaly: 148
6269 deg
Mean motion: 15
53940393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1888
Checksum: 328
Coasting Arc #18 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2017/150/04:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1785607
08 A = 6779087
83 meter
Y = -4176980
54 meter E =
0002338
Z = 5029842
68 I = 51
92041
XDOT = 5613
727612 Wp = 119
54346
YDOT = -4822
940969 meter/sec RA = 127
03016 deg
ZDOT = -2012
695901 TA = 349
92803
MA = 349
93272
Ha = 221
225 n
mi
Hp = 215
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5858290
94 X = -1763198
80
Y = -13704004
39 feet Y = -4196823
65 meter
Z = 16502108
54 Z = 5021222
73
XDOT = 18417
741509 XDOT = 5677
018473
YDOT = -15823
297144 feet/sec YDOT = -4759
810373 meter/sec
ZDOT = -6603
333009 ZDOT = -1985
272918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6424880
40 X = 1958303
55
Y = -13493424
31 feet Y = -4112795
73 meter
Z = 16464729
20 Z = 5018449
46
XDOT = 23070
303177 XDOT = 7031
828408
YDOT = 3077
821991 feet/sec YDOT = 938
120143 meter/sec
ZDOT = -6481
518879 ZDOT = -1975
566954
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 17150
22259465
00016717 00000-0 10270-3 0 9174
2 25544 51
6410 127
8667 0005215 212
7705 147
3125 15
53973568 18951
Satellite: ISS
Catalog Number: 25544
Epoch time: 17150
22259465 = yrday
fracday
Element set: 917
Inclination: 51
6410 deg
RA of node: 127
8667 deg
Eccentricity:
0005215
Arg of perigee: 212
7705 deg
Mean anomaly: 147
3125 deg
Mean motion: 15
53973568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 319
Coasting Arc #19 (Orbit 1909)
---------------------------------------
Vector Time (GMT): 2017/151/04:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 628060
24 A = 6782152
61 meter
Y = 5258125
93 meter E =
0008372
Z = -4245903
30 I = 51
94949
XDOT = -5660
342607 Wp = 147
29172
YDOT = 3636
549860 meter/sec RA = 122
05957 deg
ZDOT = 3662
726008 TA = 160
11159
MA = 160
07893
Ha = 221
022 n
mi
Hp = 215
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2060565
11 X = 589840
34
Y = 17251069
32 feet Y = 5264935
99 meter
Z = -13930128
95 Z = -4242944
75
XDOT = -18570
677846 XDOT = -5718
378500
YDOT = 11930
937860 feet/sec YDOT = 3572
927257 meter/sec
ZDOT = 12016
817611 ZDOT = 3635
089170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11380304
78 X = -3468716
90
Y = 13140551
69 feet Y = 4005240
16 meter
Z = -13917915
72 Z = -4242180
71
XDOT = -20387
067542 XDOT = -6213
978187
YDOT = -5046
103618 feet/sec YDOT = -1538
052383 meter/sec
ZDOT = 11894
232853 ZDOT = 3625
362174
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 17151
18723588
00016717 00000-0 10270-3 0 9183
2 25544 51
6410 123
0602 0005236 215
9876 144
0925 15
53977213 19106
Satellite: ISS
Catalog Number: 25544
Epoch time: 17151
18723588 = yrday
fracday
Element set: 918
Inclination: 51
6410 deg
RA of node: 123
0602 deg
Eccentricity:
0005236
Arg of perigee: 215
9876 deg
Mean anomaly: 144
0925 deg
Mean motion: 15
53977213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1910
Checksum: 303
Coasting Arc #20 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2017/152/04:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 426448
77 A = 6785892
55 meter
Y = -6045916
99 meter E =
0011085
Z = 3036795
31 I = 51
97834
XDOT = 5447
881102 Wp = 118
71477
YDOT = -2116
244957 meter/sec RA = 117
09895 deg
ZDOT = -4969
734764 TA = 26
62997
MA = 26
57308
Ha = 220
915 n
mi
Hp = 216
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1399110
15 X = 479272
83
Y = -19835685
68 feet Y = -6040853
02 meter
Z = 9963239
21 Z = 3038994
73
XDOT = 17873
625664 XDOT = 5495
281174
YDOT = -6943
060884 feet/sec YDOT = -2055
057673 meter/sec
ZDOT = -16304
904081 ZDOT = -4943
155635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15419973
94 X = 4700008
06
Y = -12546839
81 feet Y = -3824276
77 meter
Z = 9973930
30 Z = 3040053
96
XDOT = 16423
465099 XDOT = 5005
872162
YDOT = 7294
371028 feet/sec YDOT = 2223
324289 meter/sec
ZDOT = -16187
221009 ZDOT = -4933
864964
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 17152
21618315
00016717 00000-0 10270-3 0 9190
2 25544 51
6410 117
9325 0005053 220
3078 139
7701 15
53962204 19265
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
21618315 = yrday
fracday
Element set: 919
Inclination: 51
6410 deg
RA of node: 117
9325 deg
Eccentricity:
0005053
Arg of perigee: 220
3078 deg
Mean anomaly: 139
7701 deg
Mean motion: 15
53962204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 289
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