[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 29th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10 7639 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 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
062/01:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
4
064/09:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 214
6
065/04:04:36
465 -2
0 3
0 3
0
N/A -2
0 -0
3 220
5
000/00:09:12
930 1
1 0
0 216
2
067/19:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
4
070/23:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 216
4
Coasting Arc #1 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2016/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1469150
35 A = 6788790
05 meter
Y = 6601788
17 meter E =
0013945
Z = -496159
42 I = 51
30314
XDOT = -4787
376626 Wp = 146
08104
YDOT = 624
330302 meter/sec RA = 254
08493 deg
ZDOT = -5960
932712 TA = 39
29801
MA = 39
19689
Ha = 221
243 n
mi
Hp = 214
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4820047
08 X = 1397628
43
Y = 21659410
01 feet Y = 6617817
22 meter
Z = -1627819
63 Z = -489197
34
XDOT = -15706
616226 XDOT = -4765
046899
YDOT = 2048
327762 feet/sec YDOT = 570
918726 meter/sec
ZDOT = -19556
865852 ZDOT = -5984
134184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4801329
10 X = -1463445
11
Y = 21665730
05 feet Y = 6603714
52 meter
Z = -1598772
27 Z = -487305
79
XDOT = -13400
308534 XDOT = -4084
414041
YDOT = -4397
416329 feet/sec YDOT = -1340
332497 meter/sec
ZDOT = -19657
543280 ZDOT = -5991
619192
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 16057
53124938
00016717 00000-0 10270-3 0 9001
2 25544 51
6390 254
8482 0003315 172
1707 187
9498 15
54279789 27615
Satellite: ISS
Catalog Number: 25544
Epoch time: 16057
53124938 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 254
8482 deg
Eccentricity:
0003315
Arg of perigee: 172
1707 deg
Mean anomaly: 187
9498 deg
Mean motion: 15
54279789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 340
Coasting Arc #2 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2016/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -573581
37 A = 6786800
42 meter
Y = -6396394
71 meter E =
0013368
Z = 2181349
26 I = 51
30505
XDOT = 5209
193566 Wp = 85
49237
YDOT = 1401
188985 meter/sec RA = 249
08813 deg
ZDOT = 5450
566779 TA = 298
84287
MA = 298
97698
Ha = 221
182 n
mi
Hp = 214
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1881828
65 X = -512608
64
Y = -20985546
96 feet Y = -6402467
68 meter
Z = 7156657
69 Z = 2178711
88
XDOT = 17090
530073 XDOT = 5166
661676
YDOT = 4597
076721 feet/sec YDOT = 1459
204531 meter/sec
ZDOT = 17882
436938 ZDOT = 5475
768043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6802772
88 X = 2073485
18
Y = -19945042
88 feet Y = -6079249
07 meter
Z = 7146310
61 Z = 2178195
47
XDOT = 12166
933426 XDOT = 3708
481308
YDOT = 10629
029812 feet/sec YDOT = 3239
728287 meter/sec
ZDOT = 17991
441840 ZDOT = 5483
791473
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 16058
55997731
00016717 00000-0 10270-3 0 9014
2 25544 51
6376 249
7179 0003500 176
8313 183
2863 15
54307526 27778
Satellite: ISS
Catalog Number: 25544
Epoch time: 16058
55997731 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 249
7179 deg
Eccentricity:
0003500
Arg of perigee: 176
8313 deg
Mean anomaly: 183
2863 deg
Mean motion: 15
54307526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 336
Coasting Arc #3 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2016/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -496928
70 A = 6783089
79 meter
Y = 5689480
89 meter E =
0006098
Z = -3662301
83 I = 51
30492
XDOT = -5429
637110 Wp = 113
63345
YDOT = -3251
521740 meter/sec RA = 244
08422 deg
ZDOT = -4322
719921 TA = 110
12555
MA = 110
05993
Ha = 221
091 n
mi
Hp = 214
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1630343
51 X = -542723
19
Y = 18666275
89 feet Y = 5683667
42 meter
Z = -12015425
95 Z = -3664827
67
XDOT = -17813
770046 XDOT = -5371
876473
YDOT = -10667
722244 feet/sec YDOT = -3311
917098 meter/sec
ZDOT = -14182
151971 ZDOT = -4348
954884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8750592
34 X = -2667180
55
Y = 16559853
07 feet Y = 5047443
22 meter
Z = -12027332
90 Z = -3665931
07
XDOT = -10909
001096 XDOT = -3325
063534
YDOT = -16127
827139 feet/sec YDOT = -4915
761712 meter/sec
ZDOT = -14295
334003 ZDOT = -4357
217804
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 16059
52440408
00016717 00000-0 10270-3 0 9027
2 25544 51
6375 244
9087 0003376 178
3122 181
8042 15
54314381 27925
Satellite: ISS
Catalog Number: 25544
Epoch time: 16059
52440408 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 244
9087 deg
Eccentricity:
0003376
Arg of perigee: 178
3122 deg
Mean anomaly: 181
8042 deg
Mean motion: 15
54314381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 306
Coasting Arc #4 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2016/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1644417
51 A = 6779365
94 meter
Y = -4590524
11 meter E =
0009666
Z = 4707100
86 I = 51
30763
XDOT = 5383
018913 Wp = 135
89868
YDOT = 4734
722375 meter/sec RA = 239
06981 deg
ZDOT = 2726
704878 TA = 286
95314
MA = 287
05907
Ha = 220
983 n
mi
Hp = 214
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5395070
58 X = 1672762
75
Y = -15060774
65 feet Y = -4571976
16 meter
Z = 15443244
28 Z = 4715158
31
XDOT = 17660
823207 XDOT = 5316
428921
YDOT = 15533
866059 feet/sec YDOT = 4794
546831 meter/sec
ZDOT = 8945
882145 ZDOT = 2752
691827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10574611
29 X = 3223141
52
Y = -11958572
58 feet Y = -3644972
92 meter
Z = 15478942
20 Z = 4717981
58
XDOT = 9589
172221 XDOT = 2922
779693
YDOT = 20246
850353 feet/sec YDOT = 6171
239988 meter/sec
ZDOT = 9057
753020 ZDOT = 2760
803121
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 16060
55311616
00016717 00000-0 10270-3 0 9031
2 25544 51
6379 239
7784 0003352 183
9262 176
1865 15
54305612 28081
Satellite: ISS
Catalog Number: 25544
Epoch time: 16060
55311616 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 239
7784 deg
Eccentricity:
0003352
Arg of perigee: 183
9262 deg
Mean anomaly: 176
1865 deg
Mean motion: 15
54305612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2808
Checksum: 316
Coasting Arc #5 (Orbit 2822)
---------------------------------------
Vector Time (GMT): 2016/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2869146
58 A = 6776988
54 meter
Y = 3203430
11 meter E =
0014380
Z = -5249866
33 I = 51
31713
XDOT = -4976
002245 Wp = 97
59219
YDOT = -5766
179107 meter/sec RA = 234
04791 deg
ZDOT = -802
764224 TA = 164
71275
MA = 164
66926
Ha = 220
996 n
mi
Hp = 214
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9413210
57 X = -2879253
48
Y = 10509941
31 feet Y = 3171288
40 meter
Z = -17223970
91 Z = -5263828
69
XDOT = -16325
466682 XDOT = -4907
254119
YDOT = -18917
910456 feet/sec YDOT = -5821
439751 meter/sec
ZDOT = -2633
740893 ZDOT = -826
768695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12464487
43 X = -3799175
77
Y = 6449542
86 feet Y = 1965820
66 meter
Z = -17285037
56 Z = -5268479
45
XDOT = -7923
696913 XDOT = -2415
142819
YDOT = -22615
425651 feet/sec YDOT = -6893
181738 meter/sec
ZDOT = -2736
860692 ZDOT = -834
195139
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 16061
51752507
00016717 00000-0 10270-3 0 9047
2 25544 51
6378 234
9695 0003463 182
7513 177
3622 15
54333947 28230
Satellite: ISS
Catalog Number: 25544
Epoch time: 16061
51752507 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 234
9695 deg
Eccentricity:
0003463
Arg of perigee: 182
7513 deg
Mean anomaly: 177
3622 deg
Mean motion: 15
54333947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2823
Checksum: 321
Coasting Arc #6 (Orbit 2831)
---------------------------------------
Vector Time (GMT): 2016/062/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2063637
29 A = 6777612
49 meter
Y = -3954741
97 meter E =
0007003
Z = 5100998
27 I = 51
32980
XDOT = 5612
372664 Wp = 149
08250
YDOT = 4982
153077 meter/sec RA = 231
32812 deg
ZDOT = 1585
212517 TA = 285
52950
MA = 285
60680
Ha = 220
792 n
mi
Hp = 214
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6770463
54 X = 2082928
56
Y = -12974875
22 feet Y = -3931556
68 meter
Z = 16735558
62 Z = 5111070
03
XDOT = 18413
296143 XDOT = 5548
543652
YDOT = 16345
646579 feet/sec YDOT = 5044
557608 meter/sec
ZDOT = 5200
828469 ZDOT = 1612
320321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7624990
23 X = -2324097
02
Y = 12432240
61 feet Y = 3789346
94 meter
Z = 16779880
91 Z = 5114507
70
XDOT = -16183
902572 XDOT = -4932
853504
YDOT = -17133
454879 feet/sec YDOT = -5222
277047 meter/sec
ZDOT = 5317
542486 ZDOT = 1620
786950
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 16062
09616651
00016717 00000-0 10270-3 0 9051
2 25544 51
6379 232
0874 0003156 188
5293 171
5806 15
54337768 28322
Satellite: ISS
Catalog Number: 25544
Epoch time: 16062
09616651 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 232
0874 deg
Eccentricity:
0003156
Arg of perigee: 188
5293 deg
Mean anomaly: 171
5806 deg
Mean motion: 15
54337768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2832
Checksum: 327
Coasting Arc #7 (Orbit 2846)
---------------------------------------
Vector Time (GMT): 2016/063/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3391662
71 A = 6776795
80 meter
Y = 2570402
66 meter E =
0014652
Z = -5286449
97 I = 51
34820
XDOT = -5031
206996 Wp = 105
65184
YDOT = -5758
118911 meter/sec RA = 226
30498 deg
ZDOT = 425
274802 TA = 168
44255
MA = 168
40888
Ha = 220
768 n
mi
Hp = 214
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11127502
34 X = -3394474
48
Y = 8433079
60 feet Y = 2532458
67 meter
Z = -17343995
98 Z = -5302932
70
XDOT = -16506
584632 XDOT = -4968
510135
YDOT = -18891
466244 feet/sec YDOT = -5814
030613 meter/sec
ZDOT = 1395
258537 ZDOT = 400
987469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11490017
05 X = 3502157
20
Y = -7772939
79 feet Y = -2369192
05 meter
Z = -17415890
78 Z = -5308363
51
XDOT = 14815
483265 XDOT = 4515
759299
YDOT = 18986
871821 feet/sec YDOT = 5787
198531 meter/sec
ZDOT = 1290
883255 ZDOT = 393
461216
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 16063
06056284
00016717 00000-0 10270-3 0 9060
2 25544 51
6382 227
2780 0003151 191
8472 168
2607 15
54339399 28479
Satellite: ISS
Catalog Number: 25544
Epoch time: 16063
06056284 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 227
2780 deg
Eccentricity:
0003151
Arg of perigee: 191
8472 deg
Mean anomaly: 168
2607 deg
Mean motion: 15
54339399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2847
Checksum: 323
Coasting Arc #8 (Orbit 2862)
---------------------------------------
Vector Time (GMT): 2016/064/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4590134
67 A = 6778495
76 meter
Y = -1130358
54 meter E =
0004977
Z = 4854010
96 I = 51
37766
XDOT = 4026
712756 Wp = 83
32954
YDOT = 6076
819669 meter/sec RA = 221
28541 deg
ZDOT = -2390
016390 TA = 30
18519
MA = 30
15652
Ha = 220
477 n
mi
Hp = 214
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15059496
95 X = 4578855
08
Y = -3708525
39 feet Y = -1079091
27 meter
Z = 15925232
80 Z = 4876281
09
XDOT = 13210
999856 XDOT = 3970
070501
YDOT = 19937
072406 feet/sec YDOT = 6121
532142 meter/sec
ZDOT = -7841
261122 ZDOT = -2370
593957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15097186
26 X = -4601622
37
Y = 3086296
63 feet Y = 940703
21 meter
Z = 16021997
03 Z = 4883504
70
XDOT = -12201
497294 XDOT = -3719
016375
YDOT = -19366
062128 feet/sec YDOT = -5902
775737 meter/sec
ZDOT = -7758
015472 ZDOT = -2364
643116
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 16064
08924174
00016717 00000-0 10270-3 0 9076
2 25544 51
6388 222
1484 0003041 197
3349 162
7701 15
54369680 28630
Satellite: ISS
Catalog Number: 25544
Epoch time: 16064
08924174 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 222
1484 deg
Eccentricity:
0003041
Arg of perigee: 197
3349 deg
Mean anomaly: 162
7701 deg
Mean motion: 15
54369680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2863
Checksum: 320
Coasting Arc #9 (Orbit 2867)
---------------------------------------
Vector Time (GMT): 2016/064/09:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1034104
21 A = 6781126
37 meter
Y = 5219094
33 meter E =
0006449
Z = -4209648
12 I = 51
39351
XDOT = -6540
176833 Wp = 92
03659
YDOT = -1637
839370 meter/sec RA = 219
61278 deg
ZDOT = -3642
249630 TA = 140
52540
MA = 140
47840
Ha = 220
563 n
mi
Hp = 214
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3392730
33 X = 996114
52
Y = 17123012
91 feet Y = 5230445
61 meter
Z = -13811181
49 Z = -4204717
48
XDOT = -21457
273074 XDOT = -6503
683794
YDOT = -5373
488746 feet/sec YDOT = -1710
772230 meter/sec
ZDOT = -11949
637894 ZDOT = -3673
930955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12811626
80 X = -3904983
85
Y = 11880124
64 feet Y = 3621061
99 meter
Z = -13790641
08 Z = -4203387
40
XDOT = -5665
641899 XDOT = -1726
887651
YDOT = -20121
075892 feet/sec YDOT = -6132
903932 meter/sec
ZDOT = -12086
773799 ZDOT = -3684
048654
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 16064
41070077
00016717 00000-0 10270-3 0 9088
2 25544 51
6378 220
5441 0003053 199
4906 160
6130 15
54374273 28681
Satellite: ISS
Catalog Number: 25544
Epoch time: 16064
41070077 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 220
5441 deg
Eccentricity:
0003053
Arg of perigee: 199
4906 deg
Mean anomaly: 160
6130 deg
Mean motion: 15
54374273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2868
Checksum: 303
Coasting Arc #10 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/065/04:09:12
930
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5402071
41 A = 6782957
20 meter
Y = 157308
81 meter E =
0005868
Z = -4105445
81 I = 51
41753
XDOT = -3055
700006 Wp = 138
61164
YDOT = -5913
797323 meter/sec RA = 215
63598 deg
ZDOT = 3792
981035 TA = 170
68962
MA = 170
67874
Ha = 220
513 n
mi
Hp = 216
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17723331
39 X = -5383486
81
Y = 516105
02 feet Y = 97002
80 meter
Z = -13469310
41 Z = -4131642
18
XDOT = -10025
262487 XDOT = -3007
767729
YDOT = -19402
222189 feet/sec YDOT = -5947
699840 meter/sec
ZDOT = 12444
163500 ZDOT = 3778
254404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12151716
94 X = 3703843
32
Y = -12792348
25 feet Y = -3899107
75 meter
Z = -13582958
61 Z = -4140085
78
XDOT = 19907
952671 XDOT = 6067
943974
YDOT = 5760
381840 feet/sec YDOT = 1755
764385 meter/sec
ZDOT = 12381
237099 ZDOT = 3773
801068
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 16065
18220322
00016717 00000-0 10270-3 0 9094
2 25544 51
6411 216
6980 0003760 240
2454 119
8324 15
53824211 28807
Satellite: ISS
Catalog Number: 25544
Epoch time: 16065
18220322 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 216
6980 deg
Eccentricity:
0003760
Arg of perigee: 240
2454 deg
Mean anomaly: 119
8324 deg
Mean motion: 15
53824211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 285
Coasting Arc #11 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2016/066/04:09:12
930
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6062109
48 A = 6786591
42 meter
Y = 905258
52 meter E =
0010294
Z = 2900484
84 I = 51
45593
XDOT = 1573
870847 Wp = 110
46708
YDOT = 5581
162860 meter/sec RA = 210
64161 deg
ZDOT = -5020
416896 TA = 36
37895
MA = 36
30903
Ha = 220
343 n
mi
Hp = 216
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19888810
64 X = 6037447
06
Y = 2970008
26 feet Y = 972911
47 meter
Z = 9516026
37 Z = 2929872
52
XDOT = 5163
618266 XDOT = 1535
730519
YDOT = 18310
901773 feet/sec YDOT = 5598
549141 meter/sec
ZDOT = -16471
184043 ZDOT = -5012
864792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15955990
68 X = -4863385
96
Y = 12138880
73 feet Y = 3699930
85 meter
Z = 9643362
05 Z = 2939296
75
XDOT = -15912
225490 XDOT = -4850
046329
YDOT = -7828
034248 feet/sec YDOT = -2385
984839 meter/sec
ZDOT = -16439
309519 ZDOT = -5010
701541
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 16066
21124100
00016717 00000-0 10270-3 0 9108
2 25544 51
6409 211
5715 0003836 243
5958 116
4801 15
53810521 28962
Satellite: ISS
Catalog Number: 25544
Epoch time: 16066
21124100 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 211
5715 deg
Eccentricity:
0003836
Arg of perigee: 243
5958 deg
Mean anomaly: 116
4801 deg
Mean motion: 15
53810521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 284
Coasting Arc #12 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2016/067/04:09:12
930
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6383801
29 A = 6789191
64 meter
Y = -1797218
06 meter E =
0005472
Z = -1437804
95 I = 51
49452
XDOT = 120
349262 Wp = 15
96347
YDOT = -5039
533171 meter/sec RA = 205
65566 deg
ZDOT = 5775
326833 TA = 328
32746
MA = 328
36037
Ha = 220
217 n
mi
Hp = 216
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20944229
95 X = -6356245
79
Y = -5896384
71 feet Y = -1868452
08 meter
Z = -4717207
84 Z = -1468748
14
XDOT = 394
846661 XDOT = 148
640080
YDOT = -16533
901481 feet/sec YDOT = -5038
028434 meter/sec
ZDOT = 18947
922679 ZDOT = 5775
980798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18620693
39 X = 5675587
35
Y = -11198934
29 feet Y = -3413435
17 meter
Z = -4851166
78 Z = -1478635
63
XDOT = 11041
885563 XDOT = 3365
566720
YDOT = 10164
470527 feet/sec YDOT = 3098
130617 meter/sec
ZDOT = 18951
550635 ZDOT = 5776
432634
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 16067
17595295
00016717 00000-0 10270-3 0 9112
2 25544 51
6424 206
7636 0003871 249
7320 110
3417 15
53855856 29111
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
17595295 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 206
7636 deg
Eccentricity:
0003871
Arg of perigee: 249
7320 deg
Mean anomaly: 110
3417 deg
Mean motion: 15
53855856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 317
Coasting Arc #13 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2016/067/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6197138
26 A = 6790109
16 meter
Y = -2753569
00 meter E =
0009167
Z = 225412
93 I = 51
51531
XDOT = 2124
492389 Wp = 38
75443
YDOT = -4280
224119 meter/sec RA = 202
44270 deg
ZDOT = 5996
344908 TA = 323
67800
MA = 323
74018
Ha = 220
264 n
mi
Hp = 216
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20331818
42 X = -6166981
52
Y = -9034019
02 feet Y = -2822700
87 meter
Z = 739543
73 Z = 195382
93
XDOT = 6970
119385 XDOT = 2143
069854
YDOT = -14042
730048 feet/sec YDOT = -4256
361926 meter/sec
ZDOT = 19673
047599 ZDOT = 6006
710700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5326406
70 X = -1623488
76
Y = 21605576
60 feet Y = 6585379
75 meter
Z = 609685
69 Z = 185832
20
XDOT = -13448
256271 XDOT = -4099
028511
YDOT = -3885
891024 feet/sec YDOT = -1184
419584 meter/sec
ZDOT = 19718
687716 ZDOT = 6010
256016
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 16067
88340302
00016717 00000-0 10270-3 0 9128
2 25544 51
6415 203
2376 0003683 250
3330 109
7425 15
53855434 29229
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
88340302 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 203
2376 deg
Eccentricity:
0003683
Arg of perigee: 250
3330 deg
Mean anomaly: 109
7425 deg
Mean motion: 15
53855434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 291
Coasting Arc #14 (Orbit 2936)
---------------------------------------
Vector Time (GMT): 2016/068/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5638958
05 A = 6788779
14 meter
Y = 3298698
22 meter E =
0006974
Z = -1830749
37 I = 51
53939
XDOT = -3861
882525 Wp = 171
90875
YDOT = 3478
588430 meter/sec RA = 197
46552 deg
ZDOT = -5636
675832 TA = 28
24898
MA = 28
21118
Ha = 220
274 n
mi
Hp = 216
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18500518
53 X = 5610544
96
Y = 10822500
74 feet Y = 3361597
65 meter
Z = -6006395
57 Z = -1803426
63
XDOT = -12670
218258 XDOT = -3873
113776
YDOT = 11412
691698 feet/sec YDOT = 3435
338618 meter/sec
ZDOT = -18493
030946 ZDOT = -5655
463446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7054305
02 X = 2150152
17
Y = -20274036
83 feet Y = -6179526
43 meter
Z = -5888353
49 Z = -1794770
14
XDOT = 12133
579118 XDOT = 3698
314915
YDOT = 9607
654097 feet/sec YDOT = 2928
412969 meter/sec
ZDOT = -18575
087408 ZDOT = -5661
686642
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 16068
84810236
00016717 00000-0 10270-3 0 9134
2 25544 51
6402 198
4309 0003729 252
5414 107
5331 15
53847440 29370
Satellite: ISS
Catalog Number: 25544
Epoch time: 16068
84810236 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 198
4309 deg
Eccentricity:
0003729
Arg of perigee: 252
5414 deg
Mean anomaly: 107
5331 deg
Mean motion: 15
53847440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2937
Checksum: 308
Coasting Arc #15 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2016/069/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4680871
48 A = 6785644
85 meter
Y = -3677794
12 meter E =
0009068
Z = 3249213
38 I = 51
56010
XDOT = 5398
862166 Wp = 90
22037
YDOT = -2665
464308 meter/sec RA = 192
48408 deg
ZDOT = 4749
134126 TA = 307
49035
MA = 307
57277
Ha = 220
119 n
mi
Hp = 216
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15357189
91 X = -4655180
72
Y = -12066253
66 feet Y = -3729994
56 meter
Z = 10660148
90 Z = 3226538
10
XDOT = 17712
802383 XDOT = 5405
197760
YDOT = -8744
961639 feet/sec YDOT = -2605
054444 meter/sec
ZDOT = 15581
148708 ZDOT = 4775
376021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8571618
42 X = -2612629
29
Y = 17607989
64 feet Y = 5366915
24 meter
Z = 10562319
46 Z = 3219394
97
XDOT = -10950
359472 XDOT = -3337
669567
YDOT = -14768
581507 feet/sec YDOT = -4501
463643 meter/sec
ZDOT = 15695
430216 ZDOT = 4783
967130
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 16069
87710352
00016717 00000-0 10270-3 0 9147
2 25544 51
6403 193
3034 0003764 259
5112 100
5617 15
53884988 29537
Satellite: ISS
Catalog Number: 25544
Epoch time: 16069
87710352 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 193
3034 deg
Eccentricity:
0003764
Arg of perigee: 259
5112 deg
Mean anomaly: 100
5617 deg
Mean motion: 15
53884988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 318
Coasting Arc #16 (Orbit 2967)
---------------------------------------
Vector Time (GMT): 2016/070/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3354909
03 A = 6781952
57 meter
Y = 3947468
42 meter E =
0005369
Z = -4382487
60 I = 51
57939
XDOT = -6613
895821 Wp = 60
17357
YDOT = 1848
620971 meter/sec RA = 187
49566 deg
ZDOT = -3398
506037 TA = 175
34900
MA = 175
34401
Ha = 220
074 n
mi
Hp = 216
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11006919
37 X = 3331806
25
Y = 12951011
87 feet Y = 3984855
37 meter
Z = -14378240
15 Z = -4366247
11
XDOT = -21699
133270 XDOT = -6617
567597
YDOT = 6065
029434 feet/sec YDOT = 1774
638920 meter/sec
ZDOT = -11149
954190 ZDOT = -3430
643745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10106649
06 X = 3080506
63
Y = -13738305
16 feet Y = -4187435
41 meter
Z = -14308367
78 Z = -4361190
50
XDOT = 9792
521668 XDOT = 2984
760605
YDOT = 18960
304525 feet/sec YDOT = 5779
100819 meter/sec
ZDOT = -11289
704671 ZDOT = -3441
101984
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 16070
84178242
00016717 00000-0 10270-3 0 9153
2 25544 51
6403 188
4965 0003601 264
2475 95
8267 15
53895248 29684
Satellite: ISS
Catalog Number: 25544
Epoch time: 16070
84178242 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 188
4965 deg
Eccentricity:
0003601
Arg of perigee: 264
2475 deg
Mean anomaly: 95
8267 deg
Mean motion: 15
53895248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2968
Checksum: 341
Coasting Arc #17 (Orbit 2969)
---------------------------------------
Vector Time (GMT): 2016/070/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6171658
92 A = 6787275
40 meter
Y = 1278472
54 meter E =
0003151
Z = -2513729
13 I = 51
60213
XDOT = -3106
097660 Wp = 4
57253
YDOT = -4591
236007 meter/sec RA = 186
72311 deg
ZDOT = 5294
475705 TA = 327
21822
MA = 327
23777
Ha = 219
957 n
mi
Hp = 216
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20248224
80 X = -6173285
86
Y = 4194463
70 feet Y = 1209447
45 meter
Z = -8247142
81 Z = -2543713
53
XDOT = -10190
609121 XDOT = -3080
244650
YDOT = -15063
110260 feet/sec YDOT = -4625
825065 meter/sec
ZDOT = 17370
327115 ZDOT = 5279
450644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20131700
42 X = 6136142
29
Y = 4486897
86 feet Y = 1367606
47 meter
Z = -8377462
85 Z = -2553450
68
XDOT = 3519
675355 XDOT = 1072
797048
YDOT = 16498
343253 feet/sec YDOT = 5028
695024 meter/sec
ZDOT = 17305
827133 ZDOT = 5274
816110
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 16070
97040635
00016717 00000-0 10270-3 0 9162
2 25544 51
6405 187
8555 0003807 268
0605 92
0112 15
53883471 29705
Satellite: ISS
Catalog Number: 25544
Epoch time: 16070
97040635 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 187
8555 deg
Eccentricity:
0003807
Arg of perigee: 268
0605 deg
Mean anomaly: 92
0112 deg
Mean motion: 15
53883471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2970
Checksum: 311
Coasting Arc #18 (Orbit 2985)
---------------------------------------
Vector Time (GMT): 2016/071/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890060
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6693728
75 A = 6789544
39 meter
Y = -550144
89 meter E =
0010555
Z = 953183
13 I = 51
64185
XDOT = 1234
995870 Wp = 135
69954
YDOT = 4721
477522 meter/sec RA = 181
75040 deg
ZDOT = -5915
517247 TA = 33
97776
MA = 33
91021
Ha = 219
956 n
mi
Hp = 216
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21961052
34 X = 6694752
97
Y = -1804937
29 feet Y = -475285
30 meter
Z = 3127241
23 Z = 985702
12
XDOT = 4051
823722 XDOT = 1210
842361
YDOT = 15490
411819 feet/sec YDOT = 4735
152166 meter/sec
ZDOT = -19407
864983 ZDOT = -5909
577298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20863716
13 X = -6359260
67
Y = -7024796
18 feet Y = -2141157
88 meter
Z = 3268462
05 Z = 996227
23
XDOT = 1781
260530 XDOT = 542
928209
YDOT = -14355
677717 feet/sec YDOT = -4375
610568 meter/sec
ZDOT = -19382
810530 ZDOT = -5907
880650
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 16071
99938468
00016717 00000-0 10270-3 0 9176
2 25544 51
6406 182
7283 0003768 272
0060 88
0661 15
53910241 29861
Satellite: ISS
Catalog Number: 25544
Epoch time: 16071
99938468 = yrday
fracday
Element set: 917
Inclination: 51
6406 deg
RA of node: 182
7283 deg
Eccentricity:
0003768
Arg of perigee: 272
0060 deg
Mean anomaly: 88
0661 deg
Mean motion: 15
53910241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2986
Checksum: 331
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