[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 11th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
194/19:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
2
198/02:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
1
198/21:41:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 213
1
200/04:45:26
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
1
201/00:22:53
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
0
201/08:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 213
0
202/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 213
0
Coasting Arc #1 (Orbit 874)
---------------------------------------
Vector Time (GMT): 2016/193/09:36:08
422
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -749402
00 A = 6784551
77 meter
Y = 6206190
82 meter E =
0014278
Z = 2620968
59 I = 51
32232
XDOT = -5423
703239 Wp = 99
00809
YDOT = 1550
303793 meter/sec RA = 296
49604 deg
ZDOT = -5199
648660 TA = 51
30305
MA = 51
17544
Ha = 220
301 n
mi
Hp = 213
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2458667
99 X = -831476
92
Y = 20361518
43 feet Y = 6197351
44 meter
Z = 8598978
31 Z = 2617129
22
XDOT = -17794
301966 XDOT = -5415
378596
YDOT = 5086
298535 feet/sec YDOT = 1489
699173 meter/sec
ZDOT = -17059
214764 ZDOT = -5225
975115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18724709
83 X = 5707291
56
Y = 8386304
63 feet Y = 2556145
65 meter
Z = 8581028
23 Z = 2615497
40
XDOT = 275
656553 XDOT = 84
020117
YDOT = 17031
810713 feet/sec YDOT = 5191
295905 meter/sec
ZDOT = -17174
202640 ZDOT = -5234
696965
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16193
43753891
00016717 00000-0 10270-3 0 9007
2 25544 51
6410 297
0485 0001119 48
0339 312
0909 15
54774331 8757
Satellite: ISS
Catalog Number: 25544
Epoch time: 16193
43753891 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 297
0485 deg
Eccentricity:
0001119
Arg of perigee: 48
0339 deg
Mean anomaly: 312
0909 deg
Mean motion: 15
54774331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 875
Checksum: 308
Coasting Arc #2 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2016/194/09:36:08
422
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1845622
01 A = 6787104
40 meter
Y = -6474483
18 meter E =
0011514
Z = -818619
47 I = 51
31924
XDOT = 4838
817047 Wp = 40
27677
YDOT = 638
377618 meter/sec RA = 291
49726 deg
ZDOT = 5915
742820 TA = 310
82831
MA = 310
92808
Ha = 220
303 n
mi
Hp = 213
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6055190
33 X = 1921860
62
Y = -21241742
73 feet Y = -6453417
88 meter
Z = -2685759
41 Z = -809469
19
XDOT = 15875
384012 XDOT = 4802
582977
YDOT = 2094
414758 feet/sec YDOT = 692
285525 meter/sec
ZDOT = 19408
605052 ZDOT = 5939
160463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18724469
38 X = -5707218
27
Y = -11725631
50 feet Y = -3573972
48 meter
Z = -2644632
32 Z = -806083
93
XDOT = 5527
139162 XDOT = 1684
672017
YDOT = -13185
083255 feet/sec YDOT = -4018
813376 meter/sec
ZDOT = 19510
489389 ZDOT = 5946
797166
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16194
40165705
00016717 00000-0 10270-3 0 9017
2 25544 51
6426 292
2379 0001253 47
6318 312
4941 15
54798310 8904
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
40165705 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 292
2379 deg
Eccentricity:
0001253
Arg of perigee: 47
6318 deg
Mean anomaly: 312
4941 deg
Mean motion: 15
54798310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 305
Coasting Arc #3 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2016/194/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3712134
83 A = 6785206
78 meter
Y = -5235997
64 meter E =
0015176
Z = 2177767
70 I = 51
30679
XDOT = 3056
772537 Wp = 68
20460
YDOT = 4446
511613 meter/sec RA = 289
56590 deg
ZDOT = 5455
178740 TA = 316
10515
MA = 316
22563
Ha = 220
223 n
mi
Hp = 213
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12178920
04 X = 3759830
58
Y = -17178469
94 feet Y = -5194219
53 meter
Z = 7144907
14 Z = 2195915
71
XDOT = 10028
781288 XDOT = 2980
324588
YDOT = 14588
292694 feet/sec YDOT = 4480
266673 meter/sec
ZDOT = 17897
568046 ZDOT = 5469
842305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5691
70 X = 1734
83
Y = 21030340
05 feet Y = 6410047
65 meter
Z = 7224983
44 Z = 2202174
95
XDOT = -14982
234382 XDOT = -4566
585040
YDOT = -6194
286393 feet/sec YDOT = -1888
018493 meter/sec
ZDOT = 17960
575864 ZDOT = 5474
383523
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16194
85157384
00016717 00000-0 10270-3 0 9021
2 25544 51
6406 289
9975 0001462 41
7146 318
4118 15
54840272 8977
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
85157384 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 289
9975 deg
Eccentricity:
0001462
Arg of perigee: 41
7146 deg
Mean anomaly: 318
4118 deg
Mean motion: 15
54840272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 332
Coasting Arc #4 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2016/195/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4126849
66 A = 6781223
71 meter
Y = 3838828
13 meter E =
0007573
Z = -3779072
28 I = 51
28255
XDOT = -1875
591772 Wp = 69
05176
YDOT = -6135
159217 meter/sec RA = 284
55711 deg
ZDOT = -4188
132161 TA = 156
48927
MA = 156
45464
Ha = 220
395 n
mi
Hp = 213
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13539532
99 X = -4151112
67
Y = 12594580
49 feet Y = 3792543
58 meter
Z = -12398531
11 Z = -3799178
03
XDOT = -6153
516313 XDOT = -1786
503437
YDOT = -20128
475123 feet/sec YDOT = -6155
634892 meter/sec
ZDOT = -13740
591081 ZDOT = -4197
027360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3412436
88 X = 1040110
76
Y = -18113521
18 feet Y = -5521001
26 meter
Z = -12486857
50 Z = -3805994
17
XDOT = 15469
443763 XDOT = 4715
086459
YDOT = 12403
172740 feet/sec YDOT = 3780
487051 meter/sec
ZDOT = -13778
151527 ZDOT = -4199
580585
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16195
81568360
00016717 00000-0 10270-3 0 9039
2 25544 51
6399 285
1860 0001707 43
1993 316
9294 15
54804995 9125
Satellite: ISS
Catalog Number: 25544
Epoch time: 16195
81568360 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 285
1860 deg
Eccentricity:
0001707
Arg of perigee: 43
1993 deg
Mean anomaly: 316
9294 deg
Mean motion: 15
54804995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 338
Coasting Arc #5 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2016/196/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4281282
68 A = 6777187
67 meter
Y = -2014319
02 meter E =
0007317
Z = 4846991
12 I = 51
26216
XDOT = 716
026155 Wp = 108
38649
YDOT = 7259
833125 meter/sec RA = 279
53569 deg
ZDOT = 2379
363690 TA = 318
16139
MA = 318
21730
Ha = 220
183 n
mi
Hp = 213
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14046203
02 X = 4279944
63
Y = -6608658
19 feet Y = -1966450
77 meter
Z = 15902201
83 Z = 4867784
99
XDOT = 2349
167176 XDOT = 623
233789
YDOT = 23818
350149 feet/sec YDOT = 7267
321163 meter/sec
ZDOT = 7806
311320 ZDOT = 2382
617215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7106747
74 X = -2166136
71
Y = 13695357
14 feet Y = 4174344
86 meter
Z = 15993171
51 Z = 4874718
68
XDOT = -15239
446711 XDOT = -4644
983357
YDOT = -17058
909886 feet/sec YDOT = -5199
555733 meter/sec
ZDOT = 7819
089673 ZDOT = 2383
258532
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16196
84405899
00016717 00000-0 10270-3 0 9041
2 25544 51
6399 280
0549 0001598 41
2592 318
8682 15
54829747 9286
Satellite: ISS
Catalog Number: 25544
Epoch time: 16196
84405899 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 280
0549 deg
Eccentricity:
0001598
Arg of perigee: 41
2592 deg
Mean anomaly: 318
8682 deg
Mean motion: 15
54829747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 361
Coasting Arc #6 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2016/197/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4252174
19 A = 6775351
81 meter
Y = -64770
79 meter E =
0016179
Z = -5288531
19 I = 51
25238
XDOT = 411
668003 Wp = 84
01500
YDOT = -7643
035388 meter/sec RA = 274
50311 deg
ZDOT = -236
358243 TA = 183
71090
MA = 183
72292
Ha = 220
401 n
mi
Hp = 212
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13950702
73 X = -4225444
63
Y = -212502
60 feet Y = -112171
45 meter
Z = -17350824
11 Z = -5309122
15
XDOT = 1350
616807 XDOT = 498
251873
YDOT = -25075
575420 feet/sec YDOT = -7637
947699 meter/sec
ZDOT = -775
453552 ZDOT = -234
148950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11006593
67 X = 3354809
75
Y = -8390573
47 feet Y = -2557446
79 meter
Z = -17440514
15 Z = -5315868
71
XDOT = 13831
845235 XDOT = 4215
946428
YDOT = 19740
155817 feet/sec YDOT = 6016
799493 meter/sec
ZDOT = -764
372939 ZDOT = -232
980872
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16197
80815446
00016717 00000-0 10270-3 0 9052
2 25544 51
6408 275
2438 0001733 46
0453 314
0843 15
54824114 9437
Satellite: ISS
Catalog Number: 25544
Epoch time: 16197
80815446 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 275
2438 deg
Eccentricity:
0001733
Arg of perigee: 46
0453 deg
Mean anomaly: 314
0843 deg
Mean motion: 15
54824114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 303
Coasting Arc #7 (Orbit 947)
---------------------------------------
Vector Time (GMT): 2016/198/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2426172
62 A = 6782296
93 meter
Y = 5356535
54 meter E =
0013550
Z = 3369180
95 I = 51
27851
XDOT = -3944
674523 Wp = 84
18789
YDOT = 4696
524831 meter/sec RA = 272
97928 deg
ZDOT = -4608
870900 TA = 56
22920
MA = 56
10020
Ha = 220
215 n
mi
Hp = 213
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7959883
92 X = 2349728
25
Y = 17573935
50 feet Y = 5383238
84 meter
Z = 11053743
26 Z = 3380781
50
XDOT = -12941
845547 XDOT = -3974
511312
YDOT = 15408
546035 feet/sec YDOT = 4652
246506 meter/sec
ZDOT = -15120
967519 ZDOT = -4628
104994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3288090
05 X = -1002209
85
Y = 18981417
73 feet Y = 5785536
12 meter
Z = 11103262
86 Z = 3384274
52
XDOT = -17879
530330 XDOT = -5449
680845
YDOT = 5830
584633 feet/sec YDOT = 1777
162196 meter/sec
ZDOT = -15205
652377 ZDOT = -4634
682844
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16198
12951636
00016717 00000-0 10270-3 0 9061
2 25544 51
6440 273
6413 0001772 34
7449 325
3820 15
54875587 9485
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
12951636 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 273
6413 deg
Eccentricity:
0001772
Arg of perigee: 34
7449 deg
Mean anomaly: 325
3820 deg
Mean motion: 15
54875587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 330
Coasting Arc #8 (Orbit 960)
---------------------------------------
Vector Time (GMT): 2016/198/21:41:46
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1192505
42 A = 6786120
92 meter
Y = -6468726
05 meter E =
0015651
Z = 1637186
88 I = 51
28798
XDOT = 4604
705465 Wp = 61
55371
YDOT = 2297
883953 meter/sec RA = 268
93796 deg
ZDOT = 5691
014757 TA = 316
47748
MA = 316
60088
Ha = 220
369 n
mi
Hp = 213
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3912419
35 X = 1256799
04
Y = -21222854
48 feet Y = -6455031
35 meter
Z = 5371348
02 Z = 1643135
16
XDOT = 15107
301395 XDOT = 4551
023465
YDOT = 7538
989348 feet/sec YDOT = 2349
076051 meter/sec
ZDOT = 18671
308258 ZDOT = 5713
252942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20192804
28 X = 6154766
74
Y = 7594405
80 feet Y = 2314774
89 meter
Z = 5398482
47 Z = 1645457
46
XDOT = -9534
841424 XDOT = -2906
219666
YDOT = 11931
820385 feet/sec YDOT = 3636
818853 meter/sec
ZDOT = 18767
759328 ZDOT = 5720
413043
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16198
96506196
00016717 00000-0 10270-3 0 9071
2 25544 51
6418 269
4716 0001796 45
3276 314
8023 15
54838889 9618
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
96506196 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 269
4716 deg
Eccentricity:
0001796
Arg of perigee: 45
3276 deg
Mean anomaly: 314
8023 deg
Mean motion: 15
54838889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 961
Checksum: 353
Coasting Arc #9 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2016/199/21:41:46
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2126160
57 A = 6782361
03 meter
Y = 5497482
29 meter E =
0006199
Z = -3361675
21 I = 51
27804
XDOT = -4197
390417 Wp = 80
00469
YDOT = -4444
534297 meter/sec RA = 263
93259 deg
ZDOT = -4619
840321 TA = 139
41486
MA = 139
36863
Ha = 220
357 n
mi
Hp = 212
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6975592
42 X = -2171147
41
Y = 18036359
22 feet Y = 5473454
99 meter
Z = -11029118
13 Z = -3372112
08
XDOT = -13770
965936 XDOT = -4124
937637
YDOT = -14581
805437 feet/sec YDOT = -4491
066683 meter/sec
ZDOT = -15156
956434 ZDOT = -4640
054479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16687470
98 X = -5086341
16
Y = -9719547
64 feet Y = -2962518
12 meter
Z = -11075617
20 Z = -3375848
12
XDOT = 15886
680877 XDOT = 4842
260331
YDOT = -9927
975716 feet/sec YDOT = -3026
046998 meter/sec
ZDOT = -15244
199746 ZDOT = -4646
432082
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16199
92914589
00016717 00000-0 10270-3 0 9088
2 25544 51
6427 264
6612 0001790 47
1315 312
9988 15
54863055 9766
Satellite: ISS
Catalog Number: 25544
Epoch time: 16199
92914589 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 264
6612 deg
Eccentricity:
0001790
Arg of perigee: 47
1315 deg
Mean anomaly: 312
9988 deg
Mean motion: 15
54863055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 976
Checksum: 348
Coasting Arc #10 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2016/200/04:45:26
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3531726
24 A = 6777070
06 meter
Y = -3108436
01 meter E =
0007441
Z = 4872690
86 I = 51
25749
XDOT = 2767
760932 Wp = 110
14559
YDOT = 6773
831025 meter/sec RA = 262
44627 deg
ZDOT = 2309
760167 TA = 317
12407
MA = 317
18206
Ha = 220
241 n
mi
Hp = 213
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11587028
33 X = 3542553
95
Y = -10198280
88 feet Y = -3068881
90 meter
Z = 15986518
57 Z = 4889872
83
XDOT = 9080
580487 XDOT = 2680
588871
YDOT = 22223
855068 feet/sec YDOT = 6804
294305 meter/sec
ZDOT = 7577
953303 ZDOT = 2322
994119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10168174
08 X = 3099259
46
Y = -11508892
84 feet Y = -3507910
54 meter
Z = 16061959
90 Z = 4895685
38
XDOT = 10809
922014 XDOT = 3294
864230
YDOT = 20229
830694 feet/sec YDOT = 6166
052395 meter/sec
ZDOT = 7634
354967 ZDOT = 2326
951394
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16200
25050571
00016717 00000-0 10270-3 0 9090
2 25544 51
6390 263
0538 0001564 53
1341 306
9956 15
54840128 9810
Satellite: ISS
Catalog Number: 25544
Epoch time: 16200
25050571 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 263
0538 deg
Eccentricity:
0001564
Arg of perigee: 53
1341 deg
Mean anomaly: 306
9956 deg
Mean motion: 15
54840128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 294
Coasting Arc #11 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2016/201/00:22:53
000
Vector Time (MET): N/A
Weight (LBS) : 908864
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3405253
74 A = 6783670
45 meter
Y = -5119487
25 meter E =
0006247
Z = -2866089
40 I = 51
28814
XDOT = 3108
129705 Wp = 58
43577
YDOT = -4877
413587 meter/sec RA = 258
30813 deg
ZDOT = 5030
675552 TA = 268
78192
MA = 268
85350
Ha = 220
294 n
mi
Hp = 213
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11172092
32 X = -3333831
25
Y = -16796218
02 feet Y = -5157167
42 meter
Z = -9403180
44 Z = -2882458
08
XDOT = 10197
275936 XDOT = 3138
002709
YDOT = -16002
013081 feet/sec YDOT = -4842
489914 meter/sec
ZDOT = 16504
841049 ZDOT = 5045
845866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8323384
52 X = 2536967
60
Y = -18339064
23 feet Y = -5589746
78 meter
Z = -9473562
27 Z = -2887541
78
XDOT = 17579
109898 XDOT = 5358
112697
YDOT = -563
119063 feet/sec YDOT = -171
638690 meter/sec
ZDOT = 16571
841710 ZDOT = 5051
097353
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16201
02176641
00016717 00000-0 10270-3 0 9105
2 25544 51
6434 259
2098 0001719 42
9887 317
1400 15
54857133 9935
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
02176641 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 259
2098 deg
Eccentricity:
0001719
Arg of perigee: 42
9887 deg
Mean anomaly: 317
1400 deg
Mean motion: 15
54857133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 304
Coasting Arc #12 (Orbit 998)
---------------------------------------
Vector Time (GMT): 2016/201/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 908864
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4204145
57 A = 6775133
02 meter
Y = -611463
80 meter E =
0003997
Z = 5274449
35 I = 51
26190
XDOT = 1514
492060 Wp = 70
66830
YDOT = 7514
703904 meter/sec RA = 256
59939 deg
ZDOT = -334
483377 TA = 22
54416
MA = 22
52661
Ha = 220
122 n
mi
Hp = 212
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13793128
50 X = 4185050
09
Y = -2006114
84 feet Y = -564557
55 meter
Z = 17304623
86 Z = 5294825
25
XDOT = 4968
805970 XDOT = 1431
972936
YDOT = 24654
540367 feet/sec YDOT = 7531
178607 meter/sec
ZDOT = -1097
386409 ZDOT = -327
326133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3681718
21 X = 1122187
71
Y = -13327984
63 feet Y = -4062369
71 meter
Z = 17393523
92 Z = 5301546
09
XDOT = 23595
983915 XDOT = 7192
055897
YDOT = 5118
491103 feet/sec YDOT = 1560
116088 meter/sec
ZDOT = -1067
576192 ZDOT = -325
397223
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16201
40739563
00016717 00000-0 10270-3 0 9116
2 25544 51
6430 257
2805 0001463 62
6240 297
5061 15
54899969 9996
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
40739563 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 257
2805 deg
Eccentricity:
0001463
Arg of perigee: 62
6240 deg
Mean anomaly: 297
5061 deg
Mean motion: 15
54899969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 999
Checksum: 326
Coasting Arc #13 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2016/202/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 908864
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4553966
03 A = 6777144
16 meter
Y = -1441646
02 meter E =
0012949
Z = -4819710
14 I = 51
27627
XDOT = -322
650656 Wp = 103
53903
YDOT = -7241
763647 meter/sec RA = 251
56937 deg
ZDOT = 2473
622412 TA = 190
90026
MA = 190
92834
Ha = 220
315 n
mi
Hp = 212
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14940833
43 X = -4514095
11
Y = -4729809
77 feet Y = -1492348
15 meter
Z = -15812697
32 Z = -4841735
02
XDOT = -1058
565145 XDOT = -253
663005
YDOT = -23759
067083 feet/sec YDOT = -7244
986226 meter/sec
ZDOT = 8115
559093 ZDOT = 2472
222011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10110073
68 X = -3081550
46
Y = 11846925
37 feet Y = 3610942
85 meter
Z = -15908418
21 Z = -4848885
87
XDOT = -21469
666255 XDOT = -6543
954275
YDOT = -7442
236750 feet/sec YDOT = -2268
393761 meter/sec
ZDOT = 8110
765576 ZDOT = 2472
161347
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16202
37146773
00016717 00000-0 10270-3 0 9129
2 25544 51
6423 252
4712 0001545 68
9607 291
1711 15
54895859 10144
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
37146773 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 252
4712 deg
Eccentricity:
0001545
Arg of perigee: 68
9607 deg
Mean anomaly: 291
1711 deg
Mean motion: 15
54895859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 307
Coasting Arc #14 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2016/202/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4524714
00 A = 6779373
41 meter
Y = 2750936
71 meter E =
0011425
Z = 4226042
99 I = 51
28430
XDOT = -732
352176 Wp = 71
57595
YDOT = 6740
449846 meter/sec RA = 251
07058 deg
ZDOT = -3592
022972 TA = 55
34700
MA = 55
23935
Ha = 220
149 n
mi
Hp = 212
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14844862
21 X = 4473088
16
Y = 9025382
90 feet Y = 2801246
06 meter
Z = 13864970
43 Z = 4247897
33
XDOT = -2402
730236 XDOT = -790
223003
YDOT = 22114
336765 feet/sec YDOT = 6731
936929 meter/sec
ZDOT = -11784
852271 ZDOT = -3595
720465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5531947
01 X = 1686137
45
Y = -16388680
66 feet Y = -4995269
87 meter
Z = 13959712
89 Z = 4254920
49
XDOT = 20883
841280 XDOT = 6365
394822
YDOT = -3035
772411 feet/sec YDOT = -925
303431 meter/sec
ZDOT = -11802
182457 ZDOT = -3597
305213
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16202
50000878
00016717 00000-0 10270-3 0 9130
2 25544 51
6418 251
8307 0001500 57
9107 302
2192 15
54907286 10162
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
50000878 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 251
8307 deg
Eccentricity:
0001500
Arg of perigee: 57
9107 deg
Mean anomaly: 302
2192 deg
Mean motion: 15
54907286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 276
Coasting Arc #15 (Orbit 1030)
---------------------------------------
Vector Time (GMT): 2016/203/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4386841
65 A = 6783719
25 meter
Y = -4350916
29 meter E =
0006235
Z = -2801516
86 I = 51
30892
XDOT = 2073
519884 Wp = 62
59208
YDOT = -5353
407196 meter/sec RA = 246
05791 deg
ZDOT = 5078
801129 TA = 265
46506
MA = 265
53629
Ha = 220
299 n
mi
Hp = 212
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14392525
09 X = -4324254
29
Y = -14274659
75 feet Y = -4399622
75 meter
Z = -9191328
29 Z = -2822674
88
XDOT = 6802
886759 XDOT = 2108
558818
YDOT = -17563
671902 feet/sec YDOT = -5330
024142 meter/sec
ZDOT = 16662
733364 ZDOT = 5088
958300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10447381
39 X = -3184361
85
Y = 17322634
85 feet Y = 5279939
10 meter
Z = -9282766
24 Z = -2829387
15
XDOT = -17388
628826 XDOT = -5300
054066
YDOT = -1553
894230 feet/sec YDOT = -473
626961 meter/sec
ZDOT = 16707
953365 ZDOT = 5092
584186
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16203
46407635
00016717 00000-0 10270-3 0 9149
2 25544 51
6407 247
0200 0001559 65
5718 294
5598 15
54888878 10311
Satellite: ISS
Catalog Number: 25544
Epoch time: 16203
46407635 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 247
0200 deg
Eccentricity:
0001559
Arg of perigee: 65
5718 deg
Mean anomaly: 294
5598 deg
Mean motion: 15
54888878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1031
Checksum: 324
Coasting Arc #16 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2016/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3895966
02 A = 6786640
20 meter
Y = 5466718
10 meter E =
0014480
Z = 954612
34 I = 51
33338
XDOT = -3450
952926 Wp = 118
40308
YDOT = 3498
621997 meter/sec RA = 241
05760 deg
ZDOT = -5889
864690 TA = 51
20885
MA = 51
07961
Ha = 220
352 n
mi
Hp = 212
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12782040
74 X = 3829909
24
Y = 17935426
83 feet Y = 5509916
00 meter
Z = 3131930
25 Z = 973377
41
XDOT = -11322
024037 XDOT = -3461
209084
YDOT = 11478
418625 feet/sec YDOT = 3459
974080 meter/sec
ZDOT = -19323
703050 ZDOT = -5906
652951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14087777
56 X = 4293954
60
Y = -16913952
21 feet Y = -5155372
63 meter
Z = 3212760
82 Z = 979249
50
XDOT = 12719
443798 XDOT = 3876
886469
YDOT = 6872
310158 feet/sec YDOT = 2094
680136 meter/sec
ZDOT = -19397
489567 ZDOT = -5912
354820
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16204
49240784
00016717 00000-0 10270-3 0 9154
2 25544 51
6413 241
8875 0001789 63
0997 297
0339 15
54914701 10478
Satellite: ISS
Catalog Number: 25544
Epoch time: 16204
49240784 = yrday
fracday
Element set: 915
Inclination: 51
6413 deg
RA of node: 241
8875 deg
Eccentricity:
0001789
Arg of perigee: 63
0997 deg
Mean anomaly: 297
0339 deg
Mean motion: 15
54914701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 326
Coasting Arc #17 (Orbit 1062)
---------------------------------------
Vector Time (GMT): 2016/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3064050
67 A = 6786823
59 meter
Y = -5966668
41 meter E =
0015426
Z = 986421
77 I = 51
34886
XDOT = 4707
641254 Wp = 56
94334
YDOT = -1434
842008 meter/sec RA = 236
06377 deg
ZDOT = 5885
284012 TA = 313
79402
MA = 313
92151
Ha = 220
502 n
mi
Hp = 212
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10052659
66 X = -3001893
67
Y = -19575683
75 feet Y = -6000585
16 meter
Z = 3236291
90 Z = 971688
43
XDOT = 15445
017239 XDOT = 4694
748494
YDOT = -4707
486902 feet/sec YDOT = -1382
270295 meter/sec
ZDOT = 19308
674581 ZDOT = 5908
120775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16102987
54 X = -4908190
60
Y = 15012067
01 feet Y = 4575678
02 meter
Z = 3173102
95 Z = 967161
78
XDOT = -7595
596792 XDOT = -2315
137902
YDOT = -12291
417312 feet/sec YDOT = -3746
423997 meter/sec
ZDOT = 19408
465724 ZDOT = 5915
700353
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16205
52073718
00016717 00000-0 10270-3 0 9161
2 25544 51
6404 236
7558 0001923 65
6053 294
5300 15
54855757 10633
Satellite: ISS
Catalog Number: 25544
Epoch time: 16205
52073718 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 236
7558 deg
Eccentricity:
0001923
Arg of perigee: 65
6053 deg
Mean anomaly: 294
5300 deg
Mean motion: 15
54855757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1063
Checksum: 308
Coasting Arc #18 (Orbit 1077)
---------------------------------------
Vector Time (GMT): 2016/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1840461
22 A = 6783668
76 meter
Y = 5883425
83 meter E =
0006138
Z = -2833965
95 I = 51
35849
XDOT = -5720
158210 Wp = 106
68842
YDOT = -642
835394 meter/sec RA = 231
06562 deg
ZDOT = -5060
238248 TA = 105
64008
MA = 105
57234
Ha = 220
433 n
mi
Hp = 212
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6038258
61 X = 1788300
46
Y = 19302578
19 feet Y = 5903715
51 meter
Z = -9297788
54 Z = -2825152
15
XDOT = -18766
923261 XDOT = -5687
964641
YDOT = -2109
040007 feet/sec YDOT = -706
621916 meter/sec
ZDOT = -16601
831523 ZDOT = -5087
946749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16725785
56 X = 5098019
44
Y = -11401427
49 feet Y = -3475155
10 meter
Z = -9260373
20 Z = -2822561
75
XDOT = 2524
319990 XDOT = 769
412733
YDOT = 17256
350488 feet/sec YDOT = 5259
735629 meter/sec
ZDOT = -16722
508251 ZDOT = -5097
020515
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 16206
48478853
00016717 00000-0 10270-3 0 9177
2 25544 51
6413 231
9441 0001865 73
3689 286
7668 15
54912311 10783
Satellite: ISS
Catalog Number: 25544
Epoch time: 16206
48478853 = yrday
fracday
Element set: 917
Inclination: 51
6413 deg
RA of node: 231
9441 deg
Eccentricity:
0001865
Arg of perigee: 73
3689 deg
Mean anomaly: 286
7668 deg
Mean motion: 15
54912311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1078
Checksum: 334
Coasting Arc #19 (Orbit 1093)
---------------------------------------
Vector Time (GMT): 2016/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -340450
77 A = 6779343
01 meter
Y = -5257577
21 meter E =
0011675
Z = 4257928
71 I = 51
36490
XDOT = 6333
622273 Wp = 101
82138
YDOT = 2477
320849 meter/sec RA = 226
05683 deg
ZDOT = 3554
722606 TA = 311
75760
MA = 311
85734
Ha = 220
452 n
mi
Hp = 212
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1116964
45 X = -302316
86
Y = -17249269
05 feet Y = -5261171
21 meter
Z = 13969582
37 Z = 4256367
43
XDOT = 20779
600632 XDOT = 6288
182400
YDOT = 8127
693074 feet/sec YDOT = 2547
893510 meter/sec
ZDOT = 11662
475741 ZDOT = 3585
379095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16060760
99 X = -4895319
95
Y = 6403289
01 feet Y = 1951722
49 meter
Z = 13963666
08 Z = 4256125
42
XDOT = 1903
403727 XDOT = 580
157456
YDOT = -21024
832150 feet/sec YDOT = -6408
368839 meter/sec
ZDOT = 11795
703476 ZDOT = 3595
330420
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16207
51310561
00016717 00000-0 10270-3 0 9184
2 25544 51
6412 226
8120 0001957 74
8988 285
2381 15
54915529 10947
Satellite: ISS
Catalog Number: 25544
Epoch time: 16207
51310561 = yrday
fracday
Element set: 918
Inclination: 51
6412 deg
RA of node: 226
8120 deg
Eccentricity:
0001957
Arg of perigee: 74
8988 deg
Mean anomaly: 285
2381 deg
Mean motion: 15
54915529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1094
Checksum: 315
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