[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 8th 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) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
288/01:13:55
615 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
3
288/09:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
2
290/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
5
000/00:00:00
000 0
0 0
0 212
2
290/21:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
1
293/08:05:14
000 0
0 0
0 0
0
N/A 0
0 0
0 223
5
000/00:00:00
000 0
0 0
0 212
0
294/03:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
0
295/09:59:58
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
1
Coasting Arc #1 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2016/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5249107
39 A = 6781613
32 meter
Y = 355601
94 meter E =
0013024
Z = -4289029
57 I = 51
40806
XDOT = -3277
382367 Wp = 81
33278
YDOT = -5956
343008 meter/sec RA = 216
71130 deg
ZDOT = 3528
290277 TA = 224
72564
MA = 224
83074
Ha = 223
289 n
mi
Hp = 212
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17221480
95 X = -5231859
11
Y = 1166673
04 feet Y = 296999
02 meter
Z = -14071619
32 Z = -4314486
95
XDOT = -10752
566821 XDOT = -3227
672623
YDOT = -19541
807769 feet/sec YDOT = -5992
714684 meter/sec
ZDOT = 11575
755502 ZDOT = 3512
490519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16174618
05 X = 4930023
58
Y = -5760030
08 feet Y = -1755657
17 meter
Z = -14182904
74 Z = -4322949
36
XDOT = 15293
694870 XDOT = 4661
518197
YDOT = 14699
794952 feet/sec YDOT = 4480
497501 meter/sec
ZDOT = 11507
643572 ZDOT = 3507
529761
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 16281
50971034
00016717 00000-0 10270-3 0 9004
2 25544 51
6409 217
7761 0006985 43
9332 316
2374 15
54060925 22456
Satellite: ISS
Catalog Number: 25544
Epoch time: 16281
50971034 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 217
7761 deg
Eccentricity:
0006985
Arg of perigee: 43
9332 deg
Mean anomaly: 316
2374 deg
Mean motion: 15
54060925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 304
Coasting Arc #2 (Orbit 2260)
---------------------------------------
Vector Time (GMT): 2016/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5992786
70 A = 6785380
67 meter
Y = 837624
57 meter E =
0018449
Z = 3058733
89 I = 51
44811
XDOT = 1722
902914 Wp = 79
17736
YDOT = 5649
230388 meter/sec RA = 211
71214 deg
ZDOT = -4894
057801 TA = 65
59280
MA = 65
40040
Ha = 223
299 n
mi
Hp = 212
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19661373
70 X = 5968116
56
Y = 2748112
11 feet Y = 904502
21 meter
Z = 10035216
16 Z = 3087785
75
XDOT = 5652
568617 XDOT = 1683
377272
YDOT = 18534
220433 feet/sec YDOT = 5668
275694 meter/sec
ZDOT = -16056
620082 ZDOT = -4885
784666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19559699
73 X = -5961796
48
Y = 2996402
77 feet Y = 913303
56 meter
Z = 10162038
00 Z = 3097389
18
XDOT = -10619
339394 XDOT = -3236
774647
YDOT = -14671
568577 feet/sec YDOT = -4471
894102 meter/sec
ZDOT = -16021
336953 ZDOT = -4883
303503
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 16282
53857775
00016717 00000-0 10270-3 0 9014
2 25544 51
6417 212
6475 0007043 47
2090 312
9653 15
54088585 22618
Satellite: ISS
Catalog Number: 25544
Epoch time: 16282
53857775 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 212
6475 deg
Eccentricity:
0007043
Arg of perigee: 47
2090 deg
Mean anomaly: 312
9653 deg
Mean motion: 15
54088585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2261
Checksum: 316
Coasting Arc #3 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2016/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6349605
06 A = 6788376
06 meter
Y = -1804979
56 meter E =
0014974
Z = -1562212
50 I = 51
48525
XDOT = 45
851485 Wp = 44
32573
YDOT = -5088
430154 meter/sec RA = 206
72488 deg
ZDOT = 5736
568122 TA = 298
55707
MA = 298
70770
Ha = 223
378 n
mi
Hp = 212
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20832037
60 X = -6321360
76
Y = -5921848
95 feet Y = -1875827
29 meter
Z = -5125369
09 Z = -1592988
88
XDOT = 150
431380 XDOT = 74
882122
YDOT = -16694
324651 feet/sec YDOT = -5087
754672 meter/sec
ZDOT = 18820
761555 ZDOT = 5736
861744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21614661
64 X = 6588148
87
Y = -674198
41 feet Y = -205495
67 meter
Z = -5259596
24 Z = -1603124
94
XDOT = 4993
385113 XDOT = 1521
983782
YDOT = 14336
666650 feet/sec YDOT = 4369
815995 meter/sec
ZDOT = 18822
822118 ZDOT = 5737
196182
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 16283
50313512
00016717 00000-0 10270-3 0 9029
2 25544 51
6410 207
8401 0007098 50
7797 309
3985 15
54079946 22764
Satellite: ISS
Catalog Number: 25544
Epoch time: 16283
50313512 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 207
8401 deg
Eccentricity:
0007098
Arg of perigee: 50
7797 deg
Mean anomaly: 309
3985 deg
Mean motion: 15
54079946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 317
Coasting Arc #4 (Orbit 2291)
---------------------------------------
Vector Time (GMT): 2016/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6255059
80 A = 6789430
13 meter
Y = 2628339
59 meter E =
0014754
Z = -155881
03 I = 51
51892
XDOT = -1965
274251 Wp = 107
87962
YDOT = 4349
352566 meter/sec RA = 201
74543 deg
ZDOT = -5998
200428 TA = 73
80176
MA = 73
63946
Ha = 223
453 n
mi
Hp = 212
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20521849
73 X = 6225961
35
Y = 8623161
38 feet Y = 2698125
15 meter
Z = -511420
69 Z = -125566
14
XDOT = -6447
750166 XDOT = -1984
626824
YDOT = 14269
529415 feet/sec YDOT = 4327
266849 meter/sec
ZDOT = -19679
135262 ZDOT = -6007
794685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22204987
84 X = -6768080
29
Y = -1600441
46 feet Y = -487814
56 meter
Z = -379317
31 Z = -115615
92
XDOT = 1304
542353 XDOT = 397
624509
YDOT = -13920
887404 feet/sec YDOT = -4243
086481 meter/sec
ZDOT = -19721
730155 ZDOT = -6011
183351
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 16284
53199105
00016717 00000-0 10270-3 0 9034
2 25544 51
6419 202
7117 0007018 54
9455 305
2356 15
54090624 22921
Satellite: ISS
Catalog Number: 25544
Epoch time: 16284
53199105 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 202
7117 deg
Eccentricity:
0007018
Arg of perigee: 54
9455 deg
Mean anomaly: 305
2356 deg
Mean motion: 15
54090624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2292
Checksum: 299
Coasting Arc #5 (Orbit 2307)
---------------------------------------
Vector Time (GMT): 2016/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5689840
79 A = 6788097
65 meter
Y = -3210692
15 meter E =
0020951
Z = 1804137
44 I = 51
54495
XDOT = 3801
958513 Wp = 63
20354
YDOT = -3540
035603 meter/sec RA = 196
76717 deg
ZDOT = 5649
183410 TA = 316
66812
MA = 316
83268
Ha = 223
488 n
mi
Hp = 212
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18667456
66 X = -5662278
92
Y = -10533766
90 feet Y = -3274165
49 meter
Z = 5919086
08 Z = 1776564
65
XDOT = 12473
617170 XDOT = 3813
820002
YDOT = -11614
290035 feet/sec YDOT = -3497
452679 meter/sec
ZDOT = 18534
066305 ZDOT = 5667
681674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21158248
25 X = 6449034
07
Y = 3628972
52 feet Y = 1106110
82 meter
Z = 5799038
93 Z = 1767547
07
XDOT = -7463
774096 XDOT = -2274
958344
YDOT = 13547
869187 feet/sec YDOT = 4129
390528 meter/sec
ZDOT = 18615
462214 ZDOT = 5673
992883
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 16285
56084030
00016717 00000-0 10270-3 0 9049
2 25544 51
6421 197
5833 0007038 58
0706 302
1130 15
54098938 23086
Satellite: ISS
Catalog Number: 25544
Epoch time: 16285
56084030 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 197
5833 deg
Eccentricity:
0007038
Arg of perigee: 58
0706 deg
Mean anomaly: 302
1130 deg
Mean motion: 15
54098938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2308
Checksum: 299
Coasting Arc #6 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2016/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4652325
82 A = 6784745
87 meter
Y = 3664449
07 meter E =
0011210
Z = -3323132
39 I = 51
56656
XDOT = -5438
791383 Wp = 75
34831
YDOT = 2664
406453 meter/sec RA = 191
78472 deg
ZDOT = -4686
634595 TA = 143
31264
MA = 143
23584
Ha = 223
474 n
mi
Hp = 212
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15263536
14 X = 4627145
73
Y = 12022470
71 feet Y = 3716333
33 meter
Z = -10902665
33 Z = -3300593
94
XDOT = -17843
803750 XDOT = -5445
415377
YDOT = 8741
490987 feet/sec YDOT = 2603
548663 meter/sec
ZDOT = -15376
097752 ZDOT = -4713
071504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18586865
31 X = -5665276
55
Y = -5845578
75 feet Y = -1781732
40 meter
Z = -10804679
34 Z = -3293266
26
XDOT = 13098
448236 XDOT = 3992
407022
YDOT = -13077
818915 feet/sec YDOT = -3986
119205 meter/sec
ZDOT = -15492
074436 ZDOT = -4721
984288
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 16286
52537891
00016717 00000-0 10270-3 0 9055
2 25544 51
6435 192
7755 0007053 61
3850 298
8011 15
54124847 23230
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
52537891 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 192
7755 deg
Eccentricity:
0007053
Arg of perigee: 61
3850 deg
Mean anomaly: 298
8011 deg
Mean motion: 15
54124847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 319
Coasting Arc #7 (Orbit 2338)
---------------------------------------
Vector Time (GMT): 2016/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3240107
95 A = 6780998
53 meter
Y = -3942205
70 meter E =
0015099
Z = 4452890
22 I = 51
58528
XDOT = 6706
448115 Wp = 91
55431
YDOT = -1810
250097 meter/sec RA = 186
79460 deg
ZDOT = 3267
276609 TA = 325
49453
MA = 325
59245
Ha = 223
591 n
mi
Hp = 212
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10630275
42 X = -3217414
86
Y = -12933745
75 feet Y = -3978311
31 meter
Z = 14609219
88 Z = 4437206
03
XDOT = 22002
782530 XDOT = 6710
321150
YDOT = -5939
140737 feet/sec YDOT = -1735
232017 meter/sec
ZDOT = 10719
411448 ZDOT = 3299
864859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14735547
32 X = 4491394
82
Y = 8070319
89 feet Y = 2459833
50 meter
Z = 14541231
79 Z = 4432167
45
XDOT = -17612
710359 XDOT = -5368
354117
YDOT = 12528
077708 feet/sec YDOT = 3818
558086 meter/sec
ZDOT = 10862
165682 ZDOT = 3310
788100
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 16287
55421620
00016717 00000-0 10270-3 0 9062
2 25544 51
6430 187
6475 0007091 65
6276 294
5616 15
54120990 23394
Satellite: ISS
Catalog Number: 25544
Epoch time: 16287
55421620 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 187
6475 deg
Eccentricity:
0007091
Arg of perigee: 65
6276 deg
Mean anomaly: 294
5616 deg
Mean motion: 15
54120990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2339
Checksum: 320
Coasting Arc #8 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2016/288/01:13:55
615
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 433273
91 A = 6777588
22 meter
Y = 4236135
31 meter E =
0021196
Z = -5291284
34 I = 51
59037
XDOT = -7625
531420 Wp = 80
24766
YDOT = -25
288812 meter/sec RA = 184
02552 deg
ZDOT = -643
353382 TA = 183
58576
MA = 183
60098
Ha = 223
437 n
mi
Hp = 212
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1421502
33 X = 411575
29
Y = 13898081
74 feet Y = 4240858
45 meter
Z = -17359856
77 Z = -5289232
84
XDOT = -25018
147705 XDOT = -7621
556710
YDOT = -82
968544 feet/sec YDOT = -110
540485 meter/sec
ZDOT = -2110
739442 ZDOT = -680
387140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10216199
09 X = 3113897
48
Y = 9544428
18 feet Y = 2909141
71 meter
Z = -17351516
90 Z = -5288742
35
XDOT = -18329
229920 XDOT = -5586
749279
YDOT = 15479
874066 feet/sec YDOT = 4718
265615 meter/sec
ZDOT = -2272
665361 ZDOT = -692
708402
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 16288
06863127
00016717 00000-0 10270-3 0 9072
2 25544 51
6419 185
0817 0006739 69
2648 290
9226 15
54105688 23477
Satellite: ISS
Catalog Number: 25544
Epoch time: 16288
06863127 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 185
0817 deg
Eccentricity:
0006739
Arg of perigee: 69
2648 deg
Mean anomaly: 290
9226 deg
Mean motion: 15
54105688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 343
Coasting Arc #9 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2016/288/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2650635
36 A = 6779358
00 meter
Y = -3936770
97 meter E =
0012687
Z = 4830571
77 I = 51
60817
XDOT = 7061
637709 Wp = 95
26319
YDOT = -1691
437769 meter/sec RA = 182
29351 deg
ZDOT = 2489
630754 TA = 330
25726
MA = 330
32933
Ha = 223
433 n
mi
Hp = 212
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8696310
23 X = -2629881
57
Y = -12915915
26 feet Y = -3966295
47 meter
Z = 15848332
58 Z = 4817746
39
XDOT = 23168
102721 XDOT = 7067
933222
YDOT = -5549
336512 feet/sec YDOT = -1612
434262 meter/sec
ZDOT = 8168
079903 ZDOT = 2523
950450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5702895
49 X = 1738242
55
Y = 14549212
69 feet Y = 4434600
03 meter
Z = 15792837
53 Z = 4813656
88
XDOT = -22708
960803 XDOT = -6921
691253
YDOT = -152
316738 feet/sec YDOT = -46
426142 meter/sec
ZDOT = 8318
398560 ZDOT = 2535
447881
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 16288
45444193
00016717 00000-0 10270-3 0 9084
2 25544 51
6419 183
1600 0006814 68
6114 291
5765 15
54167962 23536
Satellite: ISS
Catalog Number: 25544
Epoch time: 16288
45444193 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 183
1600 deg
Eccentricity:
0006814
Arg of perigee: 68
6114 deg
Mean anomaly: 291
5765 deg
Mean motion: 15
54167962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 324
Coasting Arc #10 (Orbit 2367)
---------------------------------------
Vector Time (GMT): 2016/289/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 885635
16 A = 6777447
42 meter
Y = 4156775
94 meter E =
0021564
Z = -5297985
85 I = 51
63441
XDOT = -7581
954561 Wp = 80
95697
YDOT = 839
724511 meter/sec RA = 177
29390 deg
ZDOT = -607
396546 TA = 183
22593
MA = 183
23986
Ha = 223
494 n
mi
Hp = 212
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2905627
18 X = 864823
06
Y = 13637716
33 feet Y = 4166562
66 meter
Z = -17381843
33 Z = -5293734
66
XDOT = -24875
179005 XDOT = -7587
830534
YDOT = 2755
001675 feet/sec YDOT = 754
905072 meter/sec
ZDOT = -1992
770821 ZDOT = -644
242891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -146915
67 X = -44779
90
Y = -13965415
23 feet Y = -4256658
56 meter
Z = -17363871
89 Z = -5292508
15
XDOT = 23878
088164 XDOT = 7278
041272
YDOT = 2431
878125 feet/sec YDOT = 741
236452 meter/sec
ZDOT = -2154
025254 ZDOT = -656
546897
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 16289
41896755
00016717 00000-0 10270-3 0 9097
2 25544 51
6424 178
3515 0007048 71
3265 288
8652 15
54148504 23682
Satellite: ISS
Catalog Number: 25544
Epoch time: 16289
41896755 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 178
3515 deg
Eccentricity:
0007048
Arg of perigee: 71
3265 deg
Mean anomaly: 288
8652 deg
Mean motion: 15
54148504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 343
Coasting Arc #11 (Orbit 2383)
---------------------------------------
Vector Time (GMT): 2016/290/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 948626
71 A = 6777761
76 meter
Y = -4259666
45 meter E =
0011056
Z = 5177888
98 I = 51
66730
XDOT = 7557
709370 Wp = 67
56492
YDOT = 46
654629 meter/sec RA = 172
29604 deg
ZDOT = -1339
834036 TA = 35
32920
MA = 35
25599
Ha = 223
414 n
mi
Hp = 212
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3112292
37 X = 971036
32
Y = -13975283
63 feet Y = -4248932
39 meter
Z = 16987824
74 Z = 5182552
19
XDOT = 24795
634415 XDOT = 7563
134450
YDOT = 153
066367 feet/sec YDOT = 131
200191 meter/sec
ZDOT = -4395
780957 ZDOT = -1303
106523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5588564
71 X = -1703394
52
Y = 13154765
46 feet Y = 4009572
51 meter
Z = 17008856
38 Z = 5184299
43
XDOT = -23388
287113 XDOT = -7128
749912
YDOT = -4432
941963 feet/sec YDOT = -1351
160710 meter/sec
ZDOT = -4235
163214 ZDOT = -1290
877748
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 16290
44778788
00016717 00000-0 10270-3 0 9109
2 25544 51
6417 173
2240 0006970 74
3218 285
8703 15
54174270 23848
Satellite: ISS
Catalog Number: 25544
Epoch time: 16290
44778788 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 173
2240 deg
Eccentricity:
0006970
Arg of perigee: 74
3218 deg
Mean anomaly: 285
8703 deg
Mean motion: 15
54174270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2384
Checksum: 321
Coasting Arc #12 (Orbit 2384)
---------------------------------------
Vector Time (GMT): 2016/290/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6728067
53 A = 6789289
05 meter
Y = 847226
97 meter E =
0018721
Z = 111723
02 I = 51
70786
XDOT = -483
770820 Wp = 56
96285
YDOT = -4730
360899 meter/sec RA = 172
07753 deg
ZDOT = 6018
635043 TA = 304
23980
MA = 304
41701
Ha = 223
496 n
mi
Hp = 212
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22073712
38 X = -6737584
11
Y = 2779616
05 feet Y = 771936
01 meter
Z = 366545
33 Z = 79015
75
XDOT = -1587
174606 XDOT = -460
075411
YDOT = -15519
556755 feet/sec YDOT = -4735
637588 meter/sec
ZDOT = 19746
177961 ZDOT = 6016
343031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21683563
99 X = 6609150
31
Y = -4988241
68 feet Y = -1520416
06 meter
Z = 223375
36 Z = 68084
81
XDOT = 2904
968236 XDOT = 885
434318
YDOT = 13685
082191 feet/sec YDOT = 4171
213052 meter/sec
ZDOT = 19736
861977 ZDOT = 6015
795531
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 16290
51209011
00016717 00000-0 10270-3 0 9116
2 25544 51
6427 172
9033 0007025 74
8805 285
3124 15
54142775 23852
Satellite: ISS
Catalog Number: 25544
Epoch time: 16290
51209011 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 172
9033 deg
Eccentricity:
0007025
Arg of perigee: 74
8805 deg
Mean anomaly: 285
3124 deg
Mean motion: 15
54142775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2385
Checksum: 292
Coasting Arc #13 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2016/290/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 581372
05 A = 6777271
16 meter
Y = 4172711
06 meter E =
0021623
Z = -5327324
63 I = 51
68171
XDOT = -7551
614126 Wp = 87
94260
YDOT = 1230
539376 meter/sec RA = 169
91062 deg
ZDOT = 140
982327 TA = 183
39556
MA = 183
41026
Ha = 223
433 n
mi
Hp = 212
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1907388
62 X = 560547
03
Y = 13689996
91 feet Y = 4179095
37 meter
Z = -17478099
18 Z = -5324551
41
XDOT = -24775
636895 XDOT = -7565
497923
YDOT = 4037
202677 feet/sec YDOT = 1146
014543 meter/sec
ZDOT = 462
540442 ZDOT = 104
263698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2199566
41 X = -670427
84
Y = 13660820
04 feet Y = 4163817
95 meter
Z = -17466596
72 Z = -5323818
68
XDOT = -23846
422087 XDOT = -7268
389452
YDOT = -3459
004501 feet/sec YDOT = -1054
304572 meter/sec
ZDOT = 301
761950 ZDOT = 91
977042
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 16290
89789566
00016717 00000-0 10270-3 0 9126
2 25544 51
6426 170
9770 0006827 80
4756 279
7168 15
54160729 23915
Satellite: ISS
Catalog Number: 25544
Epoch time: 16290
89789566 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 170
9770 deg
Eccentricity:
0006827
Arg of perigee: 80
4756 deg
Mean anomaly: 279
7168 deg
Mean motion: 15
54160729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 355
Coasting Arc #14 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2016/291/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1221287
84 A = 6778542
59 meter
Y = -4409825
71 meter E =
0012418
Z = 4992141
09 I = 51
71792
XDOT = 7386
346565 Wp = 71
38583
YDOT = -302
229888 meter/sec RA = 164
91490 deg
ZDOT = -2065
908601 TA = 38
71076
MA = 38
62183
Ha = 223
382 n
mi
Hp = 212
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4006849
88 X = 1246258
56
Y = -14467932
12 feet Y = -4396028
45 meter
Z = 16378415
64 Z = 4998134
94
XDOT = 24233
420490 XDOT = 7399
212762
YDOT = -991
567873 feet/sec YDOT = -219
559023 meter/sec
ZDOT = -6777
915359 ZDOT = -2029
995365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7861673
47 X = 2396238
07
Y = -12754943
32 feet Y = -3887706
72 meter
Z = 16405301
45 Z = 5000335
88
XDOT = 22622
740558 XDOT = 6895
411322
YDOT = 5394
190938 feet/sec YDOT = 1644
149398 meter/sec
ZDOT = -6620
780492 ZDOT = -2018
013894
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 16291
92670970
00016717 00000-0 10270-3 0 9130
2 25544 51
6427 165
8476 0006825 83
6965 276
4964 15
54180459 24075
Satellite: ISS
Catalog Number: 25544
Epoch time: 16291
92670970 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 165
8476 deg
Eccentricity:
0006825
Arg of perigee: 83
6965 deg
Mean anomaly: 276
4964 deg
Mean motion: 15
54180459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 349
Coasting Arc #15 (Orbit 2421)
---------------------------------------
Vector Time (GMT): 2016/292/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2853395
62 A = 6781755
31 meter
Y = 4538840
64 meter E =
0014376
Z = -4167121
36 I = 51
75931
XDOT = -6632
203767 Wp = 99
57095
YDOT = -728
608290 meter/sec RA = 159
92965 deg
ZDOT = 3756
453486 TA = 209
04428
MA = 209
12434
Ha = 223
402 n
mi
Hp = 212
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9361534
19 X = -2883695
45
Y = 14891209
46 feet Y = 4506762
42 meter
Z = -13671658
00 Z = -4181056
62
XDOT = -21759
198709 XDOT = -6641
811040
YDOT = -2390
447145 feet/sec YDOT = -802
827555 meter/sec
ZDOT = 12324
322459 ZDOT = 3724
211817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12929700
11 X = -3940972
59
Y = 11854096
52 feet Y = 3613128
62 meter
Z = -13733314
43 Z = -4185914
24
XDOT = -19531
062065 XDOT = -5953
067717
YDOT = -7221
434928 feet/sec YDOT = -2201
093366 meter/sec
ZDOT = 12183
386447 ZDOT = 3713
496189
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 16292
89121850
00016717 00000-0 10270-3 0 9146
2 25544 51
6423 161
0404 0006839 87
0658 273
1278 15
54183687 24227
Satellite: ISS
Catalog Number: 25544
Epoch time: 16292
89121850 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 161
0404 deg
Eccentricity:
0006839
Arg of perigee: 87
0658 deg
Mean anomaly: 273
1278 deg
Mean motion: 15
54183687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2422
Checksum: 317
Coasting Arc #16 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2016/293/08:05:14
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5093481
49 A = 6787185
90 meter
Y = 3930788
44 meter E =
0012284
Z = -2160929
50 I = 51
78898
XDOT = -4511
840475 Wp = 65
34344
YDOT = -2834
635753 meter/sec RA = 157
67327 deg
ZDOT = 5508
050259 TA = 270
75224
MA = 270
89299
Ha = 223
468 n
mi
Hp = 212
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16710897
28 X = -5126560
90
Y = 12896287
52 feet Y = 3873644
65 meter
Z = -7089663
70 Z = -2185753
45
XDOT = -14802
626229 XDOT = -4506
563875
YDOT = -9299
986066 feet/sec YDOT = -2885
060419 meter/sec
ZDOT = 18071
031033 ZDOT = 5486
145313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20939418
88 X = 6382334
88
Y = -2355555
62 feet Y = -717973
35 meter
Z = -7198871
14 Z = -2194215
92
XDOT = 7741
264358 XDOT = 2359
537376
YDOT = 14171
167730 feet/sec YDOT = 4319
371924 meter/sec
ZDOT = 17975
632759 ZDOT = 5478
972865
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 16293
34132251
00016717 00000-0 10270-3 0 9155
2 25544 51
6404 158
7987 0006986 84
4433 275
7516 15
54161329 24299
Satellite: ISS
Catalog Number: 25544
Epoch time: 16293
34132251 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 158
7987 deg
Eccentricity:
0006986
Arg of perigee: 84
4433 deg
Mean anomaly: 275
7516 deg
Mean motion: 15
54161329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 328
Coasting Arc #17 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2016/294/03:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3486980
00 A = 6784163
56 meter
Y = -4710345
02 meter E =
0019332
Z = 3400886
87 I = 51
80078
XDOT = 6018
436036 Wp = 89
44775
YDOT = 1092
272136 meter/sec RA = 153
68218 deg
ZDOT = -4635
059496 TA = 50
85926
MA = 50
68760
Ha = 223
393 n
mi
Hp = 212
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11440223
11 X = 3522872
75
Y = -15453887
85 feet Y = -4671150
45 meter
Z = 11157765
32 Z = 3417913
44
XDOT = 19745
525054 XDOT = 6028
290237
YDOT = 3583
570001 feet/sec YDOT = 1159
629246 meter/sec
ZDOT = -15206
888110 ZDOT = -4605
798964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12699247
70 X = -3870730
70
Y = -14378667
06 feet Y = -4382617
72 meter
Z = 11232992
60 Z = 3423816
14
XDOT = 6649
316970 XDOT = 2026
711813
YDOT = -17711
111399 feet/sec YDOT = -5398
346754 meter/sec
ZDOT = -15079
028582 ZDOT = -4596
087912
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 16294
17722427
00016717 00000-0 10270-3 0 9168
2 25544 51
6382 154
6308 0006948 87
9006 272
2943 15
54194373 24424
Satellite: ISS
Catalog Number: 25544
Epoch time: 16294
17722427 = yrday
fracday
Element set: 916
Inclination: 51
6382 deg
RA of node: 154
6308 deg
Eccentricity:
0006948
Arg of perigee: 87
9006 deg
Mean anomaly: 272
2943 deg
Mean motion: 15
54194373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 326
Coasting Arc #18 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2016/295/03:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4615413
87 A = 6787511
00 meter
Y = 4584389
41 meter E =
0012538
Z = -1936050
75 I = 51
84079
XDOT = -4660
569117 Wp = 67
14358
YDOT = -2333
744470 meter/sec RA = 148
71735 deg
ZDOT = 5618
059245 TA = 271
58581
MA = 271
72942
Ha = 223
495 n
mi
Hp = 211
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15142433
96 X = -4656930
00
Y = 15040647
66 feet Y = 4532544
55 meter
Z = -6351872
55 Z = -1958572
65
XDOT = -15290
581091 XDOT = -4661
416755
YDOT = -7656
641963 feet/sec YDOT = -2385
866610 meter/sec
ZDOT = 18431
952902 ZDOT = 5595
417033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11813135
76 X = 3600643
78
Y = 17739595
17 feet Y = 5407028
61 meter
Z = -6451144
07 Z = -1966308
71
XDOT = -9214
362172 XDOT = -2808
537590
YDOT = 12763
491844 feet/sec YDOT = 3890
312314 meter/sec
ZDOT = 18333
232209 ZDOT = 5587
969177
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 16295
14172600
00016717 00000-0 10270-3 0 9179
2 25544 51
6386 149
8233 0007143 92
5176 267
6795 15
54187630 24576
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
14172600 = yrday
fracday
Element set: 917
Inclination: 51
6386 deg
RA of node: 149
8233 deg
Eccentricity:
0007143
Arg of perigee: 92
5176 deg
Mean anomaly: 267
6795 deg
Mean motion: 15
54187630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2457
Checksum: 329
Coasting Arc #19 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2016/295/09:59:58
000
Vector Time (MET): N/A
Weight (LBS) : 907105
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1252971
30 A = 6777381
94 meter
Y = -4095478
53 meter E =
0009866
Z = 5244456
51 I = 51
81928
XDOT = 6804
180394 Wp = 80
88678
YDOT = -3401
549160 meter/sec RA = 147
34102 deg
ZDOT = -1027
542696 TA = 18
93643
MA = 18
89977
Ha = 223
359 n
mi
Hp = 212
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4110798
23 X = -1232557
18
Y = -13436609
34 feet Y = -4109375
75 meter
Z = 17206222
16 Z = 5238419
54
XDOT = 22323
426488 XDOT = 6846
703115
YDOT = -11159
938188 feet/sec YDOT = -3325
222530 meter/sec
ZDOT = -3371
203070 ZDOT = -994
385780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4085368
29 X = 1245220
26
Y = 13477291
78 feet Y = 4107878
53 meter
Z = 17180441
96 Z = 5236598
71
XDOT = -21474
286739 XDOT = -6545
362598
YDOT = 10634
632097 feet/sec YDOT = 3241
435863 meter/sec
ZDOT = -3225
569574 ZDOT = -983
153606
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 16295
46322400
00016717 00000-0 10270-3 0 9180
2 25544 51
6430 148
2213 0006706 92
4035 267
7886 15
54224060 24621
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
46322400 = yrday
fracday
Element set: 918
Inclination: 51
6430 deg
RA of node: 148
2213 deg
Eccentricity:
0006706
Arg of perigee: 92
4035 deg
Mean anomaly: 267
7886 deg
Mean motion: 15
54224060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 295
Coasting Arc #20 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2016/296/09:59:58
000
Vector Time (MET): N/A
Weight (LBS) : 907105
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -313441
79 A = 6779802
84 meter
Y = 4897745
29 meter E =
0017360
Z = -4694074
76 I = 51
85365
XDOT = -6704
514139 Wp = 104
19141
YDOT = 2320
683166 meter/sec RA = 142
35704 deg
ZDOT = 2873
817975 TA = 194
29855
MA = 194
34774
Ha = 223
361 n
mi
Hp = 212
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1028352
32 X = -345384
26
Y = 16068718
14 feet Y = 4894061
35 meter
Z = -15400507
74 Z = -4695675
22
XDOT = -21996
437463 XDOT = -6743
926252
YDOT = 7613
789915 feet/sec YDOT = 2245
488561 meter/sec
ZDOT = 9428
536665 ZDOT = 2841
152896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 815486
19 X = 248560
19
Y = -16073477
88 feet Y = -4899196
06 meter
Z = -15408281
57 Z = -4696444
22
XDOT = 20830
802292 XDOT = 6349
228539
YDOT = -7829
138108 feet/sec YDOT = -2386
321295 meter/sec
ZDOT = 9285
203496 ZDOT = 2830
130026
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 16296
42771970
00016717 00000-0 10270-3 0 9198
2 25544 51
6428 143
4129 0006772 95
0008 265
1918 15
54198999 24778
Satellite: ISS
Catalog Number: 25544
Epoch time: 16296
42771970 = yrday
fracday
Element set: 919
Inclination: 51
6428 deg
RA of node: 143
4129 deg
Eccentricity:
0006772
Arg of perigee: 95
0008 deg
Mean anomaly: 265
1918 deg
Mean motion: 15
54198999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 350
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