[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: June 17th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


170/05:52:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 0

171/22:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 0

Coasting Arc #1 (Orbit 471)
---------------------------------------

Vector Time (GMT): 2016/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906675
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3099108
36                 A    =         6788052
22  meter
 Y    =       -6015870
17  meter          E    =           
0012446
 Z    =         448739
30                 I    =           52
00260
 XDOT =       4020
676907                 Wp   =          130
16810
 YDOT =      -2528
093028  meter/sec      RA   =           65
71391  deg
 ZDOT =      -6022
236523                 TA   =           45
01554
                                          MA   =           44
91473
                                          Ha   =            220
242  n
mi
                                          Hp   =            214
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10167678
33                 X    =        -3033786
85
 Y    =      -19737106
87  feet           Y    =        -6050161
27  meter
 Z    =        1472241
80                 Z    =          433842
61
 XDOT =      13191
197200                 XDOT =        4077
901484
 YDOT =      -8294
268466  feet/sec       YDOT =       -2482
810628  meter/sec
 ZDOT =     -19757
993842                 ZDOT =       -6002
566182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20782750
41                 X    =        -6334582
33
 Y    =        7822783
15  feet           Y    =         2384384
30  meter
 Z    =        1408515
23                 Z    =          429315
44
 XDOT =      -6127
486161                 XDOT =       -1867
657782
 YDOT =     -12673
952105  feet/sec       YDOT =       -3863
020602  meter/sec
 ZDOT =     -19671
755978                 ZDOT =       -5995
951222


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   16167
53300640  
00016717  00000-0  10270-3 0  9009
2 25544  51
6439  66
2889 0000407 309
6139  50
4978 15
54541352  4722


Satellite: ISS
Catalog Number: 25544
Epoch time:      16167
53300640   =   yrday
fracday
Element set:     900
Inclination:       51
6439  deg
RA of node:        66
2889  deg
Eccentricity:     
0000407     
Arg of perigee:   309
6139  deg
Mean anomaly:      50
4978  deg
Mean motion:   15
54541352  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             472
Checksum:              305


Coasting Arc #2 (Orbit 487)
---------------------------------------

Vector Time (GMT): 2016/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906675
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2245121
81                 A    =         6787205
34  meter
 Y    =        6243886
53  meter          E    =           
0013845
 Z    =        1394848
66                 I    =           51
98698
 XDOT =      -4960
146649                 Wp   =           57
77820
 YDOT =        472
706356  meter/sec      RA   =           60
76532  deg
 ZDOT =       5832
802230                 TA   =          317
35776
                                          MA   =          317
46515
                                          Ha   =            220
200  n
mi
                                          Hp   =            214
085

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7365885
22                 X    =         2168358
62
 Y    =       20485192
01  feet           Y    =         6268563
62  meter
 Z    =        4576275
13                 Z    =         1405569
20
 XDOT =     -16273
447011                 XDOT =       -4993
397381
 YDOT =       1550
873870  feet/sec       YDOT =         417
052163  meter/sec
 ZDOT =      19136
490255                 ZDOT =        5808
626173

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21109715
12                 X    =         6434241
17
 Y    =       -5278360
63  feet           Y    =        -1608844
32  meter
 Z    =        4621740
76                 Z    =         1408706
58
 XDOT =       -458
240342                 XDOT =        -139
671656
 YDOT =      14930
333509  feet/sec       YDOT =        4550
765653  meter/sec
 ZDOT =      19031
023805                 ZDOT =        5800
656056


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   16168
56154377  
00016717  00000-0  10270-3 0  9018
2 25544  51
6448  61
1581 0000646 329
2521  30
8594 15
54571040  4883


Satellite: ISS
Catalog Number: 25544
Epoch time:      16168
56154377   =   yrday
fracday
Element set:     901
Inclination:       51
6448  deg
RA of node:        61
1581  deg
Eccentricity:     
0000646     
Arg of perigee:   329
2521  deg
Mean anomaly:      30
8594  deg
Mean motion:   15
54571040  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             488
Checksum:              305


Coasting Arc #3 (Orbit 502)
---------------------------------------

Vector Time (GMT): 2016/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906675
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1096818
08                 A    =         6783935
80  meter
 Y    =       -5933956
68  meter          E    =           
0004013
 Z    =       -3102108
70                 I    =           51
95952
 XDOT =       5680
448027                 Wp   =           99
54691
 YDOT =       1516
855090  meter/sec      RA   =           55
81096  deg
 ZDOT =      -4916
055336                 TA   =          115
93925
                                          MA   =          115
89789
                                          Ha   =            220
154  n
mi
                                          Hp   =            214
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3598484
50                 X    =        -1015312
75
 Y    =      -19468361
81  feet           Y    =        -5945765
93  meter
 Z    =      -10177522
00                 Z    =        -3107239
56
 XDOT =      18636
640510                 XDOT =        5686
944247
 YDOT =       4976
558694  feet/sec       YDOT =        1580
414557  meter/sec
 ZDOT =     -16128
790474                 ZDOT =       -4888
444966

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19692621
32                 X    =        -6002310
98
 Y    =        1932834
56  feet           Y    =          589127
97  meter
 Z    =      -10198675
04                 Z    =        -3108556
15
 XDOT =       6628
118175                 XDOT =        2020
250420
 YDOT =     -16835
952376  feet/sec       YDOT =       -5131
598284  meter/sec
 ZDOT =     -16008
760333                 ZDOT =       -4879
470149


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   16169
52578985  
00016717  00000-0  10270-3 0  9021
2 25544  51
6447  56
3493 0000635 319
9558  40
1548 15
54573728  5030


Satellite: ISS
Catalog Number: 25544
Epoch time:      16169
52578985   =   yrday
fracday
Element set:     902
Inclination:       51
6447  deg
RA of node:        56
3493  deg
Eccentricity:     
0000635     
Arg of perigee:   319
9558  deg
Mean anomaly:      40
1548  deg
Mean motion:   15
54573728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             503
Checksum:              335


Coasting Arc #4 (Orbit 514)
---------------------------------------

Vector Time (GMT): 2016/170/05:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1354115
18                 A    =         6777816
58  meter
 Y    =        4493456
09  meter          E    =           
0006330
 Z    =        4886519
88                 I    =           51
92159
 XDOT =      -5812
513016                 Wp   =          118
23132
 YDOT =      -4385
285050  meter/sec      RA   =           52
10476  deg
 ZDOT =       2416
527418                 TA   =          308
15216
                                          MA   =          308
20919
                                          Ha   =            220
191  n
mi
                                          Hp   =            214
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4442635
10                 X    =        -1427998
25
 Y    =       14742310
01  feet           Y    =         4477899
73  meter
 Z    =       16031889
36                 Z    =         4879763
02
 XDOT =     -19069
924593                 XDOT =       -5774
782184
 YDOT =     -14387
418143  feet/sec       YDOT =       -4450
073793  meter/sec
 ZDOT =       7928
239562                 ZDOT =        2388
382562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6017544
29                 X    =        -1834147
50
 Y    =       14206857
63  feet           Y    =         4330250
21  meter
 Z    =       16001516
95                 Z    =         4877262
37
 XDOT =     -16527
266696                 XDOT =       -5037
510889
 YDOT =     -15812
598857  feet/sec       YDOT =       -4819
680132  meter/sec
 ZDOT =       7806
471032                 ZDOT =        2379
412371


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   16170
29718212  
00016717  00000-0  10270-3 0  9037
2 25544  51
6407  52
5004 0000593 327
5830  32
5287 15
54611970  5153


Satellite: ISS
Catalog Number: 25544
Epoch time:      16170
29718212   =   yrday
fracday
Element set:     903
Inclination:       51
6407  deg
RA of node:        52
5004  deg
Eccentricity:     
0000593     
Arg of perigee:   327
5830  deg
Mean anomaly:      32
5287  deg
Mean motion:   15
54611970  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             515
Checksum:              284


Coasting Arc #5 (Orbit 529)
---------------------------------------

Vector Time (GMT): 2016/171/05:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2796651
93                 A    =         6776010
98  meter
 Y    =       -3132070
04  meter          E    =           
0014660
 Z    =       -5330841
40                 I    =           51
89545
 XDOT =       5402
647656                 Wp   =           85
12889
 YDOT =       5416
957687  meter/sec      RA   =           47
11979  deg
 ZDOT =       -347
954501                 TA   =          181
55881
                                          MA   =          181
56338
                                          Ha   =            220
188  n
mi
                                          Hp   =            214
085

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9175367
23                 X    =         2857362
71
 Y    =      -10275820
34  feet           Y    =        -3100455
80  meter
 Z    =      -17489637
15                 Z    =        -5317108
90
 XDOT =      17725
221969                 XDOT =        5343
362559
 YDOT =      17772
170888  feet/sec       YDOT =        5477
042257  meter/sec
 ZDOT =      -1141
583007                 ZDOT =        -321
852896

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10121046
63                 X    =         3084895
01
 Y    =       -9458166
88  feet           Y    =        -2882849
27  meter
 Z    =      -17429135
08                 Z    =        -5312400
37
 XDOT =      15481
695253                 XDOT =        4718
820713
 YDOT =      18465
190673  feet/sec       YDOT =        5628
190117  meter/sec
 ZDOT =      -1028
941113                 ZDOT =        -313
621251


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   16171
26141712  
00016717  00000-0  10270-3 0  9041
2 25544  51
6413  47
6902 0000570 339
2026  20
9104 15
54602132  5300


Satellite: ISS
Catalog Number: 25544
Epoch time:      16171
26141712   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:        47
6902  deg
Eccentricity:     
0000570     
Arg of perigee:   339
2026  deg
Mean anomaly:      20
9104  deg
Mean motion:   15
54602132  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             530
Checksum:              255


Coasting Arc #6 (Orbit 540)
---------------------------------------

Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5685330
18                 A    =         6784427
90  meter
 Y    =       -2303937
77  meter          E    =           
0012981
 Z    =        2884372
47                 I    =           51
91143
 XDOT =       -255
795244                 Wp   =           97
82590
 YDOT =      -5746
131499  meter/sec      RA   =           43
68477  deg
 ZDOT =      -5076
238135                 TA   =           49
44771
                                          MA   =           49
33476
                                          Ha   =            220
165  n
mi
                                          Hp   =            214
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18652658
07                 X    =        -5673155
49
 Y    =       -7558850
94  feet           Y    =        -2367447
27  meter
 Z    =        9463164
27                 Z    =         2856783
72
 XDOT =       -839
223241                 XDOT =        -166
863322
 YDOT =     -18852
137465  feet/sec       YDOT =       -5748
493972  meter/sec
 ZDOT =     -16654
324591                 ZDOT =       -5077
265574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15295175
89                 X    =         4661969
61
 Y    =      -13166923
40  feet           Y    =        -4013278
25  meter
 Z    =        9343397
74                 Z    =         2847867
63
 XDOT =      16131
543536                 XDOT =        4916
894470
 YDOT =       6876
665304  feet/sec       YDOT =        2096
007585  meter/sec
 ZDOT =     -16657
606050                 ZDOT =       -5077
238324


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   16171
96851632  
00016717  00000-0  10270-3 0  9058
2 25544  51
6442  44
1620 0000458 314
6802  45
4314 15
54631366  5413


Satellite: ISS
Catalog Number: 25544
Epoch time:      16171
96851632   =   yrday
fracday
Element set:     905
Inclination:       51
6442  deg
RA of node:        44
1620  deg
Eccentricity:     
0000458     
Arg of perigee:   314
6802  deg
Mean anomaly:      45
4314  deg
Mean motion:   15
54631366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             541
Checksum:              285


Coasting Arc #7 (Orbit 555)
---------------------------------------

Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5734637
98                 A    =         6787451
38  meter
 Y    =        3431356
72  meter          E    =           
0009610
 Z    =       -1161207
58                 I    =           51
89650
 XDOT =      -1592
443314                 Wp   =           34
07868
 YDOT =       4644
217446  meter/sec      RA   =           38
72607  deg
 ZDOT =       5890
592255                 TA   =          313
35577
                                          MA   =          313
43580
                                          Ha   =            220
187  n
mi
                                          Hp   =            214
094

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18814429
06                 X    =         5701482
11
 Y    =       11257732
03  feet           Y    =         3495300
05  meter
 Z    =       -3809736
16                 Z    =        -1133430
19
 XDOT =      -5224
551554                 XDOT =       -1672
871682
 YDOT =      15236
933879  feet/sec       YDOT =        4625
959101  meter/sec
 ZDOT =      19326
090074                 ZDOT =        5882
661918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18438481
07                 X    =        -5620049
03
 Y    =       11901437
22  feet           Y    =         3627558
06  meter
 Z    =       -3689385
92                 Z    =        -1124524
83
 XDOT =     -10423
892500                 XDOT =       -3177
202434
 YDOT =     -10202
246227  feet/sec       YDOT =       -3109
644650  meter/sec
 ZDOT =      19290
552201                 ZDOT =        5879
760311


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   16172
93273834  
00016717  00000-0  10270-3 0  9069
2 25544  51
6434  39
3524 0000653 325
2664  34
8446 15
54588906  5569


Satellite: ISS
Catalog Number: 25544
Epoch time:      16172
93273834   =   yrday
fracday
Element set:     906
Inclination:       51
6434  deg
RA of node:        39
3524  deg
Eccentricity:     
0000653     
Arg of perigee:   325
2664  deg
Mean anomaly:      34
8446  deg
Mean motion:   15
54588906  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             556
Checksum:              322


Coasting Arc #8 (Orbit 571)
---------------------------------------

Vector Time (GMT): 2016/173/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5260380
62                 A    =         6787580
88  meter
 Y    =       -4217761
59  meter          E    =           
0009890
 Z    =        -741423
48                 I    =           51
87107
 XDOT =       3487
675321                 Wp   =          139
49841
 YDOT =      -3308
778254  meter/sec      RA   =           33
77111  deg
 ZDOT =      -5974
127686                 TA   =           48
48888
                                          MA   =           48
40406
                                          Ha   =            220
089  n
mi
                                          Hp   =            213
957

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17258466
59                 X    =        -5209224
09
 Y    =      -13837800
49  feet           Y    =        -4276300
53  meter
 Z    =       -2432491
74                 Z    =         -766853
34
 XDOT =      11442
504333                 XDOT =        3553
435295
 YDOT =     -10855
571699  feet/sec       YDOT =       -3269
408194  meter/sec
 ZDOT =     -19600
156451                 ZDOT =       -5957
026268

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19881474
71                 X    =         6059873
49
 Y    =       -9670540
88  feet           Y    =        -2947580
86  meter
 Z    =       -2542441
67                 Z    =         -774936
22
 XDOT =       4163
634352                 XDOT =        1269
075751
 YDOT =      13650
300923  feet/sec       YDOT =        4160
611721  meter/sec
 ZDOT =     -19524
922775                 ZDOT =       -5951
196462


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   16173
96123690  
00016717  00000-0  10270-3 0  9078
2 25544  51
6426  34
2220 0000465 327
8844  32
2281 15
54641721  5728


Satellite: ISS
Catalog Number: 25544
Epoch time:      16173
96123690   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:        34
2220  deg
Eccentricity:     
0000465     
Arg of perigee:   327
8844  deg
Mean anomaly:      32
2281  deg
Mean motion:   15
54641721  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             572
Checksum:              290


Coasting Arc #9 (Orbit 587)
---------------------------------------

Vector Time (GMT): 2016/174/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4278905
77                 A    =         6785081
14  meter
 Y    =        4613853
30  meter          E    =           
0013618
 Z    =        2520351
08                 I    =           51
83592
 XDOT =      -5196
610365                 Wp   =           73
36782
 YDOT =       1906
650228  meter/sec      RA   =           28
80968  deg
 ZDOT =       5312
214491                 TA   =          314
85467
                                          MA   =          314
96521
                                          Ha   =            220
098  n
mi
                                          Hp   =            213
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14038404
76                 X    =         4214751
80
 Y    =       15137313
97  feet           Y    =         4661343
83  meter
 Z    =        8268868
36                 Z    =         2540981
58
 XDOT =     -17049
246603                 XDOT =       -5243
349032
 YDOT =       6255
414134  feet/sec       YDOT =        1848
276223  meter/sec
 ZDOT =      17428
525234                 ZDOT =        5286
857583

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19554876
42                 X    =        -5960326
33
 Y    =        6507152
05  feet           Y    =         1983379
94  meter
 Z    =        8357813
53                 Z    =         2547461
56
 XDOT =       1842
389819                 XDOT =         561
560417
 YDOT =     -16789
139026  feet/sec       YDOT =       -5117
329575  meter/sec
 ZDOT =      17317
604557                 ZDOT =        5278
405869


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   16174
98972764  
00016717  00000-0  10270-3 0  9086
2 25544  51
6430  29
0907 0000551 339
9704  20
1427 15
54643730  5889


Satellite: ISS
Catalog Number: 25544
Epoch time:      16174
98972764   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:        29
0907  deg
Eccentricity:     
0000551     
Arg of perigee:   339
9704  deg
Mean anomaly:      20
1427  deg
Mean motion:   15
54643730  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             588
Checksum:              319


Coasting Arc #10 (Orbit 602)
---------------------------------------

Vector Time (GMT): 2016/175/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2810892
13                 A    =         6780924
44  meter
 Y    =       -4694818
50  meter          E    =           
0007183
 Z    =       -4012642
04                 I    =           51
79334
 XDOT =       6534
526999                 Wp   =           66
92861
 YDOT =       -525
421674  meter/sec      RA   =           23
83660  deg
 ZDOT =      -3965
644069                 TA   =          161
88406
                                          MA   =          161
85845
                                          Ha   =            220
144  n
mi
                                          Hp   =            213
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9222087
03                 X    =        -2738693
08
 Y    =      -15402947
83  feet           Y    =        -4725847
60  meter
 Z    =      -13164836
10                 Z    =        -4026121
73
 XDOT =      21438
736872                 XDOT =        6559
179943
 YDOT =      -1723
824389  feet/sec       YDOT =        -452
209922  meter/sec
 ZDOT =     -13010
643272                 ZDOT =       -3933
841453

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17763656
99                 X    =         5414362
65
 Y    =       -2286060
34  feet           Y    =         -696791
19  meter
 Z    =      -13222595
02                 Z    =        -4030246
96
 XDOT =      -7109
985087                 XDOT =       -2167
123455
 YDOT =      19149
023699  feet/sec       YDOT =        5836
622424  meter/sec
 ZDOT =     -12871
923090                 ZDOT =       -3923
362158


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   16175
95393233  
00016717  00000-0  10270-3 0  9093
2 25544  51
6428  24
2807 0000585 350
9581   9
1561 15
54652146  6030


Satellite: ISS
Catalog Number: 25544
Epoch time:      16175
95393233   =   yrday
fracday
Element set:     909
Inclination:       51
6428  deg
RA of node:        24
2807  deg
Eccentricity:     
0000585     
Arg of perigee:   350
9581  deg
Mean anomaly:       9
1561  deg
Mean motion:   15
54652146  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             603
Checksum:              307


Coasting Arc #11 (Orbit 618)
---------------------------------------

Vector Time (GMT): 2016/176/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1008081
04                 A    =         6777201
27  meter
 Y    =        4487528
12  meter          E    =           
0005708
 Z    =        4974117
34                 I    =           51
75071
 XDOT =      -7333
073342                 Wp   =          118
11529
 YDOT =       -724
644068  meter/sec      RA   =           18
84931  deg
 ZDOT =       2135
423579                 TA   =          311
10169
                                          MA   =          311
15096
                                          Ha   =            220
097  n
mi
                                          Hp   =            213
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3307352
49                 X    =          933663
57
 Y    =       14722861
28  feet           Y    =         4498384
55  meter
 Z    =       16319282
63                 Z    =         4978834
02
 XDOT =     -24058
639575                 XDOT =       -7334
798049
 YDOT =      -2377
441167  feet/sec       YDOT =        -806
657243  meter/sec
 ZDOT =       7005
982872                 ZDOT =        2099
797420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14835638
17                 X    =        -4521902
51
 Y    =       -2639066
30  feet           Y    =         -804387
41  meter
 Z    =       16338891
62                 Z    =         4980094
17
 XDOT =      11173
421329                 XDOT =        3405
658821
 YDOT =     -20305
942349  feet/sec       YDOT =       -6189
251228  meter/sec
 ZDOT =       6850
867668                 ZDOT =        2088
144465


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   16176
98241094  
00016717  00000-0  10270-3 0  9106
2 25544  51
6422  19
1501 0000631 349
8427  10
2713 15
54674774  6196


Satellite: ISS
Catalog Number: 25544
Epoch time:      16176
98241094   =   yrday
fracday
Element set:     910
Inclination:       51
6422  deg
RA of node:        19
1501  deg
Eccentricity:     
0000631     
Arg of perigee:   349
8427  deg
Mean anomaly:      10
2713  deg
Mean motion:   15
54674774  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             619
Checksum:              296


Coasting Arc #12 (Orbit 633)
---------------------------------------

Vector Time (GMT): 2016/177/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         979660
33                 A    =         6775819
75  meter
 Y    =       -4088543
43  meter          E    =           
0014821
 Z    =       -5326522
63                 I    =           51
71624
 XDOT =       7440
308555                 Wp   =           86
97951
 YDOT =       1815
005320  meter/sec      RA   =           13
85101  deg
 ZDOT =        -24
031026                 TA   =          182
78732
                                          MA   =          182
79558
                                          Ha   =            220
156  n
mi
                                          Hp   =            213
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3214108
68                 X    =         1051180
38
 Y    =      -13413856
40  feet           Y    =        -4077187
86  meter
 Z    =      -17475467
95                 Z    =        -5321590
37
 XDOT =      24410
461139                 XDOT =        7419
576463
 YDOT =       5954
741862  feet/sec       YDOT =        1898
091890  meter/sec
 ZDOT =        -78
841949                 ZDOT =          12
061646

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11280931
51                 X    =         3438427
93
 Y    =        7986460
75  feet           Y    =         2434273
24  meter
 Z    =      -17453109
95                 Z    =        -5319707
91
 XDOT =     -13857
779559                 XDOT =       -4223
851210
 YDOT =      19739
760278  feet/sec       YDOT =        6016
678933  meter/sec
 ZDOT =         78
068368                 ZDOT =          23
795239


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   16177
94660474  
00016717  00000-0  10270-3 0  9111
2 25544  51
6434  14
3397 0000714 353
8669   6
2475 15
54656465  6348


Satellite: ISS
Catalog Number: 25544
Epoch time:      16177
94660474   =   yrday
fracday
Element set:     911
Inclination:       51
6434  deg
RA of node:        14
3397  deg
Eccentricity:     
0000714     
Arg of perigee:   353
8669  deg
Mean anomaly:       6
2475  deg
Mean motion:   15
54656465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             634
Checksum:              323


Coasting Arc #13 (Orbit 649)
---------------------------------------

Vector Time (GMT): 2016/178/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2938455
98                 A    =         6777173
31  meter
 Y    =        3526483
81  meter          E    =           
0006770
 Z    =        4982757
64                 I    =           51
68944
 XDOT =      -6852
165978                 Wp   =           50
89651
 YDOT =      -2741
706581  meter/sec      RA   =            8
85148  deg
 ZDOT =      -2094
401789                 TA   =           59
49723
                                          MA   =           59
43040
                                          Ha   =            220
213  n
mi
                                          Hp   =            213
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9640603
61                 X    =        -3001875
58
 Y    =       11569828
77  feet           Y    =         3493269
05  meter
 Z    =       16347630
07                 Z    =         4968329
67
 XDOT =     -22480
859509                 XDOT =       -6810
824610
 YDOT =      -8995
100330  feet/sec       YDOT =       -2818
100753  meter/sec
 ZDOT =      -6871
396947                 ZDOT =       -2127
587532

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7452134
52                 X    =        -2271410
60
 Y    =      -13166010
49  feet           Y    =        -4013000
00  meter
 Z    =       16284011
90                 Z    =         4963366
83
 XDOT =      15287
113415                 XDOT =        4659
512169
 YDOT =     -17354
328472  feet/sec       YDOT =       -5289
599318  meter/sec
 ZDOT =      -7015
434296                 ZDOT =       -2138
304373


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   16178
97506980  
00016717  00000-0  10270-3 0  9127
2 25544  51
6431   9
2094 0000842   2
5605 357
5552 15
54708982  6500


Satellite: ISS
Catalog Number: 25544
Epoch time:      16178
97506980   =   yrday
fracday
Element set:     912
Inclination:       51
6431  deg
RA of node:         9
2094  deg
Eccentricity:     
0000842     
Arg of perigee:     2
5605  deg
Mean anomaly:     357
5552  deg
Mean motion:   15
54708982  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             650
Checksum:              311


Coasting Arc #14 (Orbit 664)
---------------------------------------

Vector Time (GMT): 2016/179/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4644168
77                 A    =         6780903
20  meter
 Y    =       -2875781
57  meter          E    =           
0006868
 Z    =       -4024453
80                 I    =           51
67038
 XDOT =       5569
622425                 Wp   =           99
63862
 YDOT =       3493
812242  meter/sec      RA   =            3
85748  deg
 ZDOT =       3935
279863                 TA   =          211
23724
                                          MA   =          211
27807
                                          Ha   =            220
215  n
mi
                                          Hp   =            213
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15236774
19                 X    =         4695530
35
 Y    =       -9434978
90  feet           Y    =        -2823559
89  meter
 Z    =      -13203588
57                 Z    =        -4001769
09
 XDOT =      18273
039451                 XDOT =        5511
023926
 YDOT =      11462
638589  feet/sec       YDOT =        3555
767526  meter/sec
 ZDOT =      12911
023171                 ZDOT =        3962
193598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3811645
71                 X    =         1161789
61
 Y    =       17585958
09  feet           Y    =         5360200
03  meter
 Z    =      -13104132
96                 Z    =        -3994139
73
 XDOT =     -15572
043329                 XDOT =       -4746
358807
 YDOT =      13071
258072  feet/sec       YDOT =        3984
119460  meter/sec
 ZDOT =      13027
561637                 ZDOT =        3970
800787


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   16179
93925259  
00016717  00000-0  10270-3 0  9139
2 25544  51
6436   4
3994 0000887  11
6023 348
5151 15
54700714  6650


Satellite: ISS
Catalog Number: 25544
Epoch time:      16179
93925259   =   yrday
fracday
Element set:     913
Inclination:       51
6436  deg
RA of node:         4
3994  deg
Eccentricity:     
0000887     
Arg of perigee:    11
6023  deg
Mean anomaly:     348
5151  deg
Mean motion:   15
54700714  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             665
Checksum:              313


Coasting Arc #15 (Orbit 680)
---------------------------------------

Vector Time (GMT): 2016/180/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5927236
31                 A    =         6784989
91  meter
 Y    =        2112417
21  meter          E    =           
0013763
 Z    =        2522344
10                 I    =           51
65118
 XDOT =      -3728
365137                 Wp   =          100
45413
 YDOT =      -4114
964957  meter/sec      RA   =          358
87388  deg
 ZDOT =      -5292
945348                 TA   =           51
22330
                                          MA   =           51
10043
                                          Ha   =            220
235  n
mi
                                          Hp   =            213
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19446313
34                 X    =        -5962669
84
 Y    =        6930502
64  feet           Y    =         2045936
56  meter
 Z    =        8275407
14                 Z    =         2493465
14
 XDOT =     -12232
169086                 XDOT =       -3656
362578
 YDOT =     -13500
541199  feet/sec       YDOT =       -4156
254973  meter/sec
 ZDOT =     -17365
306259                 ZDOT =       -5310
882314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -417315
65                 X    =         -127197
81
 Y    =      -20690357
21  feet           Y    =        -6306420
88  meter
 Z    =        8149128
73                 Z    =         2483854
44
 XDOT =      15130
390273                 XDOT =        4611
742955
 YDOT =      -7204
136059  feet/sec       YDOT =       -2195
820671  meter/sec
 ZDOT =     -17442
591404                 ZDOT =       -5316
501860


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   16180
96770693  
00016717  00000-0  10270-3 0  9145
2 25544  51
6427 359
2686 0000946  15
6001 344
5181 15
54721686  6814


Satellite: ISS
Catalog Number: 25544
Epoch time:      16180
96770693   =   yrday
fracday
Element set:     914
Inclination:       51
6427  deg
RA of node:       359
2686  deg
Eccentricity:     
0000946     
Arg of perigee:    15
6001  deg
Mean anomaly:     344
5181  deg
Mean motion:   15
54721686  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             681
Checksum:              323


Coasting Arc #16 (Orbit 695)
---------------------------------------

Vector Time (GMT): 2016/181/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6619205
57                 A    =         6787340
76  meter
 Y    =       -1285788
43  meter          E    =           
0011436
 Z    =        -726126
44                 I    =           51
62829
 XDOT =       1536
641503                 Wp   =           37
86582
 YDOT =       4579
450480  meter/sec      RA   =          353
89840  deg
 ZDOT =       5957
212010                 TA   =          314
28498
                                          MA   =          314
37874
                                          Ha   =            220
178  n
mi
                                          Hp   =            213
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21716553
70                 X    =         6636618
84
 Y    =       -4218465
97  feet           Y    =        -1211670
62  meter
 Z    =       -2382304
58                 Z    =         -693929
73
 XDOT =       5041
474749                 XDOT =        1456
381076
 YDOT =      15024
443831  feet/sec       YDOT =        4596
184849  meter/sec
 ZDOT =      19544
658825                 ZDOT =        5964
482185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2483447
74                 X    =         -756954
87
 Y    =       21997421
93  feet           Y    =         6704814
20  meter
 Z    =       -2241751
72                 Z    =         -683285
92
 XDOT =     -14204
568979                 XDOT =       -4329
552625
 YDOT =        370
444565  feet/sec       YDOT =         112
911503  meter/sec
 ZDOT =      19575
365065                 ZDOT =        5966
571272


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   16181
93187655  
00016717  00000-0  10270-3 0  9154
2 25544  51
6438 354
4586 0000929  15
2607 344
8573 15
54743834  6964


Satellite: ISS
Catalog Number: 25544
Epoch time:      16181
93187655   =   yrday
fracday
Element set:     915
Inclination:       51
6438  deg
RA of node:       354
4586  deg
Eccentricity:     
0000929     
Arg of perigee:    15
2607  deg
Mean anomaly:     344
8573  deg
Mean motion:   15
54743834  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             696
Checksum:              342
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