[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 15th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 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
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
0 212
9
Coasting Arc #1 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2016/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3731851
05 A = 6783982
00 meter
Y = -4926420
86 meter E =
0014518
Z = 2780710
23 I = 51
29846
XDOT = 2805
334270 Wp = 77
21308
YDOT = 5009
314616 meter/sec RA = 286
01479 deg
ZDOT = 5090
467273 TA = 314
50645
MA = 314
62501
Ha = 220
224 n
mi
Hp = 213
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12243605
80 X = 3773154
75
Y = -16162798
08 feet Y = -4884458
07 meter
Z = 9123065
07 Z = 2798938
50
XDOT = 9203
852593 XDOT = 2724
383184
YDOT = 16434
759239 feet/sec YDOT = 5040
232737 meter/sec
ZDOT = 16701
008113 ZDOT = 5103
898566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19449805
91 X = -5928300
84
Y = -5601272
31 feet Y = -1707267
80 meter
Z = 9203425
43 Z = 2805204
07
XDOT = 11689
841753 XDOT = 3563
063766
YDOT = -12952
445835 feet/sec YDOT = -3947
905491 meter/sec
ZDOT = 16758
543864 ZDOT = 5108
004170
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
55859090
00016717 00000-0 10270-3 0 9000
2 25544 51
6439 286
4667 0001288 48
6373 311
4891 15
54820021 9081
Satellite: ISS
Catalog Number: 25544
Epoch time: 16195
55859090 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 286
4667 deg
Eccentricity:
0001288
Arg of perigee: 48
6373 deg
Mean anomaly: 311
4891 deg
Mean motion: 15
54820021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 908
Checksum: 325
Coasting Arc #2 (Orbit 922)
---------------------------------------
Vector Time (GMT): 2016/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4106216
09 A = 6779691
17 meter
Y = 3366124
70 meter E =
0009313
Z = -4225561
69 I = 51
27517
XDOT = -1668
096714 Wp = 67
32933
YDOT = -6552
376219 meter/sec RA = 281
00233 deg
ZDOT = -3601
551570 TA = 165
62710
MA = 165
60059
Ha = 220
269 n
mi
Hp = 213
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13471837
57 X = -4123025
90
Y = 11043716
22 feet Y = 3320112
63 meter
Z = -13863391
37 Z = -4245549
11
XDOT = -5472
758249 XDOT = -1577
207715
YDOT = -21497
297306 feet/sec YDOT = -6570
521492 meter/sec
ZDOT = -11816
114074 ZDOT = -3609
434530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15241601
18 X = 4645640
04
Y = 8289020
63 feet Y = 2526493
49 meter
Z = -13951108
42 Z = -4252297
85
XDOT = -17322
381912 XDOT = -5279
862007
YDOT = 11924
321748 feet/sec YDOT = 3634
533269 meter/sec
ZDOT = -11849
191902 ZDOT = -3611
633692
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
52269591
00016717 00000-0 10270-3 0 9010
2 25544 51
6430 281
6566 0001187 50
4865 309
6393 15
54809062 9237
Satellite: ISS
Catalog Number: 25544
Epoch time: 16196
52269591 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 281
6566 deg
Eccentricity:
0001187
Arg of perigee: 50
4865 deg
Mean anomaly: 309
6393 deg
Mean motion: 15
54809062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 923
Checksum: 321
Coasting Arc #3 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2016/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4246828
93 A = 6776112
94 meter
Y = -1430373
57 meter E =
0005460
Z = 5078859
70 I = 51
25948
XDOT = 545
189129 Wp = 112
28810
YDOT = 7474
565158 meter/sec RA = 275
97591 deg
ZDOT = 1645
749133 TA = 321
73134
MA = 321
77008
Ha = 220
056 n
mi
Hp = 213
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13933165
79 X = 4237837
32
Y = -4692826
66 feet Y = -1382933
47 meter
Z = 16662925
51 Z = 5099467
64
XDOT = 1788
678245 XDOT = 453
571844
YDOT = 24522
851569 feet/sec YDOT = 7480
149403 meter/sec
ZDOT = 5399
439414 ZDOT = 1648
175717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9704726
22 X = -2958000
55
Y = -10907106
60 feet Y = -3324486
09 meter
Z = 16752973
83 Z = 5106306
42
XDOT = 21109
229717 XDOT = 6434
093218
YDOT = -10457
435479 feet/sec YDOT = -3187
426334 meter/sec
ZDOT = 5408
582867 ZDOT = 1648
536058
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
55106456
00016717 00000-0 10270-3 0 9025
2 25544 51
6440 276
5251 0001234 48
1670 311
9588 15
54860965 9391
Satellite: ISS
Catalog Number: 25544
Epoch time: 16197
55106456 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 276
5251 deg
Eccentricity:
0001234
Arg of perigee: 48
1670 deg
Mean anomaly: 311
9588 deg
Mean motion: 15
54860965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 320
Coasting Arc #4 (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 = 2427181
07 A = 6782288
75 meter
Y = 5355330
00 meter E =
0013554
Z = 3370337
53 I = 51
27856
XDOT = -3943
873389 Wp = 84
22249
YDOT = 4698
276591 meter/sec RA = 272
97904 deg
ZDOT = -4607
794462 TA = 56
17826
MA = 56
04930
Ha = 220
214 n
mi
Hp = 213
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7963192
47 X = 2350744
49
Y = 17569980
32 feet Y = 5382044
62 meter
Z = 11057537
82 Z = 3381943
00
XDOT = -12939
217157 XDOT = -3973
735056
YDOT = 15414
293276 feet/sec YDOT = 4654
007084 meter/sec
ZDOT = -15117
435900 ZDOT = -4627
024725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3283155
99 X = -1000705
95
Y = 18979975
42 feet Y = 5785096
51 meter
Z = 11107079
06 Z = 3385437
70
XDOT = -17880
689431 XDOT = -5450
034139
YDOT = 5836
446783 feet/sec YDOT = 1778
948979 meter/sec
ZDOT = -15202
104399 ZDOT = -4633
601421
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
12951925
00016717 00000-0 10270-3 0 9039
2 25544 51
6441 273
6411 0001766 35
1673 324
9596 15
54877240 9484
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
12951925 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 273
6411 deg
Eccentricity:
0001766
Arg of perigee: 35
1673 deg
Mean anomaly: 324
9596 deg
Mean motion: 15
54877240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 327
Coasting Arc #5 (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 = 1191739
54 A = 6786114
90 meter
Y = -6469096
98 meter E =
0015651
Z = 1636280
07 I = 51
28805
XDOT = 4604
949862 Wp = 61
59423
YDOT = 2296
547693 meter/sec RA = 268
93771 deg
ZDOT = 5691
351291 TA = 316
42660
MA = 316
55012
Ha = 220
366 n
mi
Hp = 213
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3909906
63 X = 1256041
77
Y = -21224071
45 feet Y = -6455410
80 meter
Z = 5368372
95 Z = 1642224
65
XDOT = 15108
103221 XDOT = 4551
281151
YDOT = 7534
605291 feet/sec YDOT = 2347
742598 meter/sec
ZDOT = 18672
412372 ZDOT = 5713
590695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20194446
04 X = 6155267
15
Y = 7592168
92 feet Y = 2314093
09 meter
Z = 5395491
35 Z = 1644545
76
XDOT = -9530
832134 XDOT = -2904
997635
YDOT = 11933
263226 feet/sec YDOT = 3637
258631 meter/sec
ZDOT = 18768
869006 ZDOT = 5720
751273
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
96506370
00016717 00000-0 10270-3 0 9042
2 25544 51
6419 269
4715 0001793 45
7565 314
3735 15
54841399 9615
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
96506370 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 269
4715 deg
Eccentricity:
0001793
Arg of perigee: 45
7565 deg
Mean anomaly: 314
3735 deg
Mean motion: 15
54841399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 961
Checksum: 341
Coasting Arc #6 (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 = -2126178
70 A = 6782350
56 meter
Y = 5497425
82 meter E =
0006203
Z = -3361728
13 I = 51
27811
XDOT = -4197
380746 Wp = 80
12096
YDOT = -4444
599736 meter/sec RA = 263
93233 deg
ZDOT = -4619
802290 TA = 139
29938
MA = 139
25301
Ha = 220
352 n
mi
Hp = 212
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6975651
91 X = -2171164
65
Y = 18036173
94 feet Y = 5473398
32 meter
Z = -11029291
77 Z = -3372165
09
XDOT = -13770
934205 XDOT = -4124
927419
YDOT = -14582
020132 feet/sec YDOT = -4491
132011 meter/sec
ZDOT = -15156
831659 ZDOT = -4640
016399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16687278
70 X = -5086282
55
Y = -9719575
39 feet Y = -2962526
58 meter
Z = -11075791
20 Z = -3375901
16
XDOT = 15886
885750 XDOT = 4842
322776
YDOT = -9927
924631 feet/sec YDOT = -3026
031427 meter/sec
ZDOT = -15244
074748 ZDOT = -4646
393983
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
92914574
00016717 00000-0 10270-3 0 9059
2 25544 51
6428 264
6611 0001786 47
5456 312
5848 15
54866597 9766
Satellite: ISS
Catalog Number: 25544
Epoch time: 16199
92914574 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 264
6611 deg
Eccentricity:
0001786
Arg of perigee: 47
5456 deg
Mean anomaly: 312
5848 deg
Mean motion: 15
54866597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 976
Checksum: 359
Coasting Arc #7 (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 = 3531888
59 A = 6777058
23 meter
Y = -3107985
19 meter E =
0007449
Z = 4872843
98 I = 51
25755
XDOT = 2767
479370 Wp = 110
21772
YDOT = 6774
100187 meter/sec RA = 262
44599 deg
ZDOT = 2309
331281 TA = 317
05635
MA = 317
11449
Ha = 220
237 n
mi
Hp = 213
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11587560
99 X = 3542710
50
Y = -10196801
80 feet Y = -3068429
30 meter
Z = 15987020
94 Z = 4890026
72
XDOT = 9079
656725 XDOT = 2680
306403
YDOT = 22224
738145 feet/sec YDOT = 6804
560313 meter/sec
ZDOT = 7576
546196 ZDOT = 2322
563863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10168878
23 X = 3099474
08
Y = -11507488
47 feet Y = -3507482
49 meter
Z = 16062465
56 Z = 4895839
50
XDOT = 10809
223082 XDOT = 3294
651195
YDOT = 20230
766282 feet/sec YDOT = 6166
337563 meter/sec
ZDOT = 7632
941842 ZDOT = 2326
520673
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
25050479
00016717 00000-0 10270-3 0 9064
2 25544 51
6391 263
0536 0001562 53
6176 306
5120 15
54843961 9815
Satellite: ISS
Catalog Number: 25544
Epoch time: 16200
25050479 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 263
0536 deg
Eccentricity:
0001562
Arg of perigee: 53
6176 deg
Mean anomaly: 306
5120 deg
Mean motion: 15
54843961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 293
Coasting Arc #8 (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 = -3404450
89 A = 6783660
09 meter
Y = -5120757
24 meter E =
0006248
Z = -2864759
75 I = 51
28822
XDOT = 3109
248692 Wp = 58
51097
YDOT = -4875
698249 meter/sec RA = 258
30785 deg
ZDOT = 5031
648286 TA = 268
72385
MA = 268
79543
Ha = 220
288 n
mi
Hp = 213
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11169458
29 X = -3333020
72
Y = -16800384
65 feet Y = -5158428
39 meter
Z = -9398818
07 Z = -2881124
51
XDOT = 10200
947153 XDOT = 3139
097706
YDOT = -15996
385333 feet/sec YDOT = -4840
762197 meter/sec
ZDOT = 16508
032433 ZDOT = 5046
823977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8328298
54 X = 2538465
40
Y = -18339071
09 feet Y = -5589748
87 meter
Z = -9469182
58 Z = -2886206
85
XDOT = 17576
282096 XDOT = 5357
250783
YDOT = -557
394006 feet/sec YDOT = -169
893693 meter/sec
ZDOT = 16575
056209 ZDOT = 5052
077133
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
02176335
00016717 00000-0 10270-3 0 9071
2 25544 51
6435 259
2097 0001715 43
3948 316
7340 15
54861815 9934
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
02176335 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 259
2097 deg
Eccentricity:
0001715
Arg of perigee: 43
3948 deg
Mean anomaly: 316
7340 deg
Mean motion: 15
54861815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 309
Coasting Arc #9 (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 = 4204662
19 A = 6775118
97 meter
Y = -608815
57 meter E =
0004000
Z = 5274320
52 I = 51
26196
XDOT = 1512
618140 Wp = 70
79446
YDOT = 7514
986671 meter/sec RA = 256
59907 deg
ZDOT = -336
891678 TA = 22
44106
MA = 22
42356
Ha = 220
116 n
mi
Hp = 212
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13794823
47 X = 4185537
69
Y = -1997426
41 feet Y = -561903
71 meter
Z = 17304201
17 Z = 5294698
85
XDOT = 4962
657941 XDOT = 1430
107692
YDOT = 24655
468082 feet/sec YDOT = 7531
440468 meter/sec
ZDOT = -1105
287657 ZDOT = -329
743515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3690353
58 X = 1124819
77
Y = -13326035
13 feet Y = -4061775
51 meter
Z = 17393111
37 Z = 5301420
35
XDOT = 23594
516172 XDOT = 7191
608529
YDOT = 5123
814501 feet/sec YDOT = 1561
738660 meter/sec
ZDOT = -1075
517065 ZDOT = -327
817601
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
40739137
00016717 00000-0 10270-3 0 9089
2 25544 51
6431 257
2803 0001462 63
1348 296
9954 15
54904965 9996
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
40739137 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 257
2803 deg
Eccentricity:
0001462
Arg of perigee: 63
1348 deg
Mean anomaly: 296
9954 deg
Mean motion: 15
54904965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 999
Checksum: 329
Coasting Arc #10 (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 = -4554173
97 A = 6777133
51 meter
Y = -1446431
75 meter E =
0012946
Z = -4818062
06 I = 51
27636
XDOT = -318
845151 Wp = 103
60356
YDOT = -7240
544322 meter/sec RA = 251
56901 deg
ZDOT = 2477
706615 TA = 190
87872
MA = 190
90675
Ha = 220
307 n
mi
Hp = 212
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14941515
66 X = -4514257
53
Y = -4745510
98 feet Y = -1497135
95 meter
Z = -15807290
22 Z = -4840087
84
XDOT = -1046
079891 XDOT = -249
891256
YDOT = -23755
066674 feet/sec YDOT = -7243
724534 meter/sec
ZDOT = 8128
958710 ZDOT = 2476
324618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10124826
23 X = -3086047
04
Y = 11841504
25 feet Y = 3609290
50 meter
Z = -15903014
16 Z = -4847238
72
XDOT = -21461
569356 XDOT = -6541
486340
YDOT = -7451
041126 feet/sec YDOT = -2271
077335 meter/sec
ZDOT = 8124
245173 ZDOT = 2476
269929
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
37146004
00016717 00000-0 10270-3 0 9092
2 25544 51
6424 252
4710 0001545 69
4415 290
6904 15
54901820 10140
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
37146004 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 252
4710 deg
Eccentricity:
0001545
Arg of perigee: 69
4415 deg
Mean anomaly: 290
6904 deg
Mean motion: 15
54901820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 276
Coasting Arc #11 (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 = 4524197
21 A = 6779364
76 meter
Y = 2755584
38 meter E =
0011435
Z = 4223535
45 I = 51
28440
XDOT = -736
340258 Wp = 71
68931
YDOT = 6738
019067 meter/sec RA = 251
07023 deg
ZDOT = -3595
804217 TA = 55
27873
MA = 55
17108
Ha = 220
141 n
mi
Hp = 212
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14843166
68 X = 4472531
61
Y = 9040631
17 feet Y = 2805887
73 meter
Z = 13856743
61 Z = 4245387
19
XDOT = -2415
814494 XDOT = -794
165239
YDOT = 22106
361767 feet/sec YDOT = 6729
461809 meter/sec
ZDOT = -11797
257929 ZDOT = -3599
520971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5547179
30 X = 1690780
25
Y = -16390458
54 feet Y = -4995811
76 meter
Z = 13951473
87 Z = 4252409
24
XDOT = 20878
815967 XDOT = 6363
863107
YDOT = -3022
434911 feet/sec YDOT = -921
238161 meter/sec
ZDOT = -11814
671616 ZDOT = -3601
111908
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
50000058
00016717 00000-0 10270-3 0 9107
2 25544 51
6419 251
8305 0001497 58
3939 301
7361 15
54913364 10160
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
50000058 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 251
8305 deg
Eccentricity:
0001497
Arg of perigee: 58
3939 deg
Mean anomaly: 301
7361 deg
Mean motion: 15
54913364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 281
Coasting Arc #12 (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 = -4384655
00 A = 6783712
22 meter
Y = -4356555
29 meter E =
0006240
Z = -2796130
53 I = 51
30903
XDOT = 2079
418112 Wp = 62
52329
YDOT = -5347
528544 meter/sec RA = 246
05756 deg
ZDOT = 5082
604184 TA = 265
60248
MA = 265
67377
Ha = 220
289 n
mi
Hp = 212
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14385351
03 X = -4322030
91
Y = -14293160
39 feet Y = -4405237
09 meter
Z = -9173656
59 Z = -2817277
83
XDOT = 6822
237900 XDOT = 2114
372398
YDOT = -17544
384987 feet/sec YDOT = -5324
080006 meter/sec
ZDOT = 16675
210579 ZDOT = 5092
789802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10467030
00 X = -3190350
74
Y = 17320188
32 feet Y = 5279193
40 meter
Z = -9265046
85 Z = -2823986
28
XDOT = -17374
668717 XDOT = -5295
799025
YDOT = -1575
773906 feet/sec YDOT = -480
295886 meter/sec
ZDOT = 16720
553510 ZDOT = 5096
424710
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
46406409
00016717 00000-0 10270-3 0 9114
2 25544 51
6408 247
0197 0001557 66
0218 294
1098 15
54895739 10311
Satellite: ISS
Catalog Number: 25544
Epoch time: 16203
46406409 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 247
0197 deg
Eccentricity:
0001557
Arg of perigee: 66
0218 deg
Mean anomaly: 294
1098 deg
Mean motion: 15
54895739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1031
Checksum: 309
Coasting Arc #13 (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 = 3890886
98 A = 6786624
59 meter
Y = 5471819
44 meter E =
0014478
Z = 945924
73 I = 51
33347
XDOT = -3458
284565 Wp = 118
52993
YDOT = 3488
328175 meter/sec RA = 241
05725 deg
ZDOT = -5891
686463 TA = 51
17756
MA = 51
04838
Ha = 220
341 n
mi
Hp = 212
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12765377
23 X = 3824815
74
Y = 17952163
51 feet Y = 5514960
46 meter
Z = 3103427
60 Z = 964665
09
XDOT = -11346
077968 XDOT = -3468
416220
YDOT = 11444
646244 feet/sec YDOT = 3449
598967 meter/sec
ZDOT = -19329
679996 ZDOT = -5908
510037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14108161
11 X = 4300167
51
Y = -16902286
09 feet Y = -5151816
80 meter
Z = 3184149
59 Z = 970528
80
XDOT = 12693
763371 XDOT = 3869
059076
YDOT = 6902
658069 feet/sec YDOT = 2103
930180 meter/sec
ZDOT = -19403
618621 ZDOT = -5914
222956
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
49239063
00016717 00000-0 10270-3 0 9129
2 25544 51
6414 241
8872 0001787 63
5222 296
6114 15
54922553 10470
Satellite: ISS
Catalog Number: 25544
Epoch time: 16204
49239063 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 241
8872 deg
Eccentricity:
0001787
Arg of perigee: 63
5222 deg
Mean anomaly: 296
6114 deg
Mean motion: 15
54922553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 303
Coasting Arc #14 (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 = -3054946
41 A = 6786788
13 meter
Y = -5969400
81 meter E =
0015433
Z = 997830
34 I = 51
34889
XDOT = 4715
230507 Wp = 57
10602
YDOT = -1420
043003 meter/sec RA = 236
06339 deg
ZDOT = 5882
820991 TA = 313
75707
MA = 313
88470
Ha = 220
489 n
mi
Hp = 212
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10022790
07 X = -2992814
96
Y = -19584648
34 feet Y = -6003215
90 meter
Z = 3273721
58 Z = 983141
16
XDOT = 15469
916360 XDOT = 4702
183660
YDOT = -4658
933737 feet/sec YDOT = -1367
387283 meter/sec
ZDOT = 19300
593804 ZDOT = 5905
694246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16119659
68 X = -4913272
27
Y = 14985988
03 feet Y = 4567729
15 meter
Z = 3210725
61 Z = 978629
17
XDOT = -7557
549379 XDOT = -2303
541051
YDOT = -12327
403021 feet/sec YDOT = -3757
392441 meter/sec
ZDOT = 19400
541453 ZDOT = 5913
285035
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
52071439
00016717 00000-0 10270-3 0 9136
2 25544 51
6405 236
7556 0001920 66
0189 294
1165 15
54864709 10636
Satellite: ISS
Catalog Number: 25544
Epoch time: 16205
52071439 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 236
7556 deg
Eccentricity:
0001920
Arg of perigee: 66
0189 deg
Mean anomaly: 294
1165 deg
Mean motion: 15
54864709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1063
Checksum: 306
Coasting Arc #15 (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 = 1826429
62 A = 6783610
69 meter
Y = 5881777
44 meter E =
0006137
Z = -2846379
86 I = 51
35846
XDOT = -5725
926728 Wp = 106
36348
YDOT = -661
250303 meter/sec RA = 231
06513 deg
ZDOT = -5051
325435 TA = 106
12415
MA = 106
05659
Ha = 220
418 n
mi
Hp = 212
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5992223
15 X = 1774348
63
Y = 19297170
08 feet Y = 5901910
65 meter
Z = -9338516
59 Z = -2837634
03
XDOT = -18785
848845 XDOT = -5693
570105
YDOT = -2169
456374 feet/sec YDOT = -725
100421 meter/sec
ZDOT = -16572
590011 ZDOT = -5079
061562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16733792
52 X = 5100459
96
Y = -11356038
06 feet Y = -3461320
40 meter
Z = -9301397
25 Z = -2835065
88
XDOT = 2475
286519 XDOT = 754
467331
YDOT = 17291
478474 feet/sec YDOT = 5270
442639 meter/sec
ZDOT = -16693
384019 ZDOT = -5088
143449
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
48475995
00016717 00000-0 10270-3 0 9148
2 25544 51
6414 231
9439 0001863 73
7951 286
3407 15
54921977 10780
Satellite: ISS
Catalog Number: 25544
Epoch time: 16206
48475995 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 231
9439 deg
Eccentricity:
0001863
Arg of perigee: 73
7951 deg
Mean anomaly: 286
3407 deg
Mean motion: 15
54921977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1078
Checksum: 342
Coasting Arc #16 (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 = -321359
47 A = 6779272
17 meter
Y = -5250037
44 meter E =
0011632
Z = 4268629
21 I = 51
36483
XDOT = 6334
927936 Wp = 102
07279
YDOT = 2497
607291 meter/sec RA = 226
05616 deg
ZDOT = 3538
187484 TA = 311
70240
MA = 311
80186
Ha = 220
434 n
mi
Hp = 212
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1054328
96 X = -283363
27
Y = -17224532
30 feet Y = -5253418
73 meter
Z = 14004689
00 Z = 4267160
33
XDOT = 20783
884303 XDOT = 6289
341437
YDOT = 8194
249644 feet/sec YDOT = 2568
193734 meter/sec
ZDOT = 11608
226652 ZDOT = 3568
849959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16056204
83 X = -4893931
23
Y = 6336311
42 feet Y = 1931307
72 meter
Z = 13999174
27 Z = 4266948
32
XDOT = 1960
497589 XDOT = 597
559665
YDOT = -21049
848795 feet/sec YDOT = -6415
993913 meter/sec
ZDOT = 11741
477054 ZDOT = 3578
802206
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
51307025
00016717 00000-0 10270-3 0 9152
2 25544 51
6412 226
8117 0001953 75
3025 284
8345 15
54926365 10942
Satellite: ISS
Catalog Number: 25544
Epoch time: 16207
51307025 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 226
8117 deg
Eccentricity:
0001953
Arg of perigee: 75
3025 deg
Mean anomaly: 284
8345 deg
Mean motion: 15
54926365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1094
Checksum: 298
Coasting Arc #17 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2016/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1396009
25 A = 6775854
32 meter
Y = 4218102
60 meter E =
0015484
Z = -5129624
17 I = 51
37748
XDOT = -6382
439589 Wp = 78
51412
YDOT = -3952
003874 meter/sec RA = 221
03607 deg
ZDOT = -1513
651088 TA = 176
83617
MA = 176
82637
Ha = 220
422 n
mi
Hp = 212
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4580082
85 X = -1418156
08
Y = 13838919
28 feet Y = 4202367
79 meter
Z = -16829475
62 Z = -5136459
26
XDOT = -20939
762430 XDOT = -6330
420322
YDOT = -12965
891975 feet/sec YDOT = -4023
085679 meter/sec
ZDOT = -4966
046877 ZDOT = -1544
528895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14540377
88 X = 4431907
18
Y = -205968
37 feet Y = -62779
16 meter
Z = -16859984
68 Z = -5138923
33
XDOT = -5585
893133 XDOT = -1702
580227
YDOT = 22902
272513 feet/sec YDOT = 6980
612662 meter/sec
ZDOT = -5100
005814 ZDOT = -1554
481772
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 16208
47710682
00016717 00000-0 10270-3 0 9166
2 25544 51
6423 222
0008 0001858 77
8482 282
2879 15
54919886 11090
Satellite: ISS
Catalog Number: 25544
Epoch time: 16208
47710682 = yrday
fracday
Element set: 916
Inclination: 51
6423 deg
RA of node: 222
0008 deg
Eccentricity:
0001858
Arg of perigee: 77
8482 deg
Mean anomaly: 282
2879 deg
Mean motion: 15
54919886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1109
Checksum: 330
Coasting Arc #18 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2016/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3119681
00 A = 6775123
79 meter
Y = -2918465
34 meter E =
0004957
Z = 5254667
77 I = 51
39870
XDOT = 5828
061886 Wp = 70
90933
YDOT = 4940
591309 meter/sec RA = 216
01069 deg
ZDOT = -713
933946 TA = 25
94025
MA = 25
91541
Ha = 220
332 n
mi
Hp = 212
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10235173
88 X = 3126559
41
Y = -9575017
52 feet Y = -2883540
74 meter
Z = 17239723
65 Z = 5269838
89
XDOT = 19120
937947 XDOT = 5775
849756
YDOT = 16209
289071 feet/sec YDOT = 5005
472683 meter/sec
ZDOT = -2342
302974 ZDOT = -685
749468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12426196
55 X = -3787504
71
Y = -6302958
33 feet Y = -1921141
70 meter
Z = 17306362
18 Z = 5274979
19
XDOT = 8348
404722 XDOT = 2544
593759
YDOT = -22574
220363 feet/sec YDOT = -6880
622367 meter/sec
ZDOT = -2220
236122 ZDOT = -676
727970
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
50540743
00016717 00000-0 10270-3 0 9171
2 25544 51
6407 216
8689 0001996 81
0544 279
0835 15
54943427 11259
Satellite: ISS
Catalog Number: 25544
Epoch time: 16209
50540743 = yrday
fracday
Element set: 917
Inclination: 51
6407 deg
RA of node: 216
8689 deg
Eccentricity:
0001996
Arg of perigee: 81
0544 deg
Mean anomaly: 279
0835 deg
Mean motion: 15
54943427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 324
Coasting Arc #19 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2016/210/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4676461
90 A = 6777642
79 meter
Y = 1535623
56 meter E =
0012416
Z = -4671217
65 I = 51
43508
XDOT = -4613
314990 Wp = 105
46034
YDOT = -5413
912472 meter/sec RA = 210
99040 deg
ZDOT = 2841
792250 TA = 192
85059
MA = 192
88226
Ha = 220
394 n
mi
Hp = 212
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15342722
78 X = -4670595
47
Y = 5038135
02 feet Y = 1483361
31 meter
Z = -15325517
21 Z = -4693920
23
XDOT = -15135
547867 XDOT = -4566
236488
YDOT = -17762
180027 feet/sec YDOT = -5465
238577 meter/sec
ZDOT = 9323
465387 ZDOT = 2819
496104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10097547
42 X = 3077732
45
Y = 12480756
81 feet Y = 3804134
68 meter
Z = -15424774
56 Z = -4701471
28
XDOT = -10336
971737 XDOT = -3150
708986
YDOT = 19754
402881 feet/sec YDOT = 6021
141998 meter/sec
ZDOT = 9227
137229 ZDOT = 2812
431427
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
46943336
00016717 00000-0 10270-3 0 9184
2 25544 51
6421 212
0580 0001849 79
4535 280
6826 15
54928967 11408
Satellite: ISS
Catalog Number: 25544
Epoch time: 16210
46943336 = yrday
fracday
Element set: 918
Inclination: 51
6421 deg
RA of node: 212
0580 deg
Eccentricity:
0001849
Arg of perigee: 79
4535 deg
Mean anomaly: 280
6826 deg
Mean motion: 15
54928967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 316
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