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

 
Date: February 24th 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

065/04:03:17 853 -2 4 3 4 3 4
N/A -2 1 -0 4 220 6
000/00:10:35 706 1 0 0 0 216 5

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 7

Coasting Arc #1 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2016/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906097
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2874508
45                 A    =         6785325
71  meter
 Y    =        5425713
71  meter          E    =           
0014994
 Z    =        2868562
16                 I    =           51
28154
 XDOT =      -3578
481052                 Wp   =          110
53403
 YDOT =       4562
053504  meter/sec      RA   =          264
08098  deg
 ZDOT =      -5026
760028                 TA   =           36
61240
                                          MA   =           36
51002
                                          Ha   =            221
311  n
mi
                                          Hp   =            213
982

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9430802
01                 X    =         2799689
14
 Y    =       17800898
00  feet           Y    =         5457440
42  meter
 Z    =        9411293
17                 Z    =         2882343
09
 XDOT =     -11740
423400                 XDOT =       -3604
811694
 YDOT =      14967
367139  feet/sec       YDOT =        4521
888645  meter/sec
 ZDOT =     -16491
994842                 ZDOT =       -5044
207661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         253413
83                 X    =           77240
53
 Y    =       20115612
66  feet           Y    =         6131238
74  meter
 Z    =        9470076
25                 Z    =         2886479
24
 XDOT =     -15699
146421                 XDOT =       -4785
099829
 YDOT =       8022
751316  feet/sec       YDOT =        2445
334601  meter/sec
 ZDOT =     -16568
420802                 ZDOT =       -5050
054661


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   16055
53805988  
00016717  00000-0  10270-3 0  9000
2 25544  51
6400 264
7880 0003356 164
5960 195
5295 15
54289957 27304


Satellite: ISS
Catalog Number: 25544
Epoch time:      16055
53805988   =   yrday
fracday
Element set:     900
Inclination:       51
6400  deg
RA of node:       264
7880  deg
Eccentricity:     
0003356     
Arg of perigee:   164
5960  deg
Mean anomaly:     195
5295  deg
Mean motion:   15
54289957  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2730
Checksum:              338


Coasting Arc #2 (Orbit 2744)
---------------------------------------

Vector Time (GMT): 2016/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906097
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2251845
98                 A    =         6788230
36  meter
 Y    =       -6273922
52  meter          E    =           
0007047
 Z    =       -1276102
22                 I    =           51
29442
 XDOT =       4219
158626                 Wp   =           59
34204
 YDOT =      -2689
646643  meter/sec      RA   =          259
08004  deg
 ZDOT =       5805
836576                 TA   =          286
71567
                                          MA   =          286
79300
                                          Ha   =            221
362  n
mi
                                          Hp   =            214
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7387946
11                 X    =        -2175323
39
 Y    =      -20583735
31  feet           Y    =        -6298676
47  meter
 Z    =       -4186687
07                 Z    =        -1286854
24
 XDOT =      13842
383943                 XDOT =        4220
719482
 YDOT =      -8824
300011  feet/sec       YDOT =       -2642
455679  meter/sec
 ZDOT =      19048
020262                 ZDOT =        5826
336067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2427723
74                 X    =          739970
19
 Y    =      -21725442
30  feet           Y    =        -6621914
81  meter
 Z    =       -4232206
26                 Z    =        -1289976
47
 XDOT =      14616
309101                 XDOT =        4455
051014
 YDOT =      -2077
333442  feet/sec       YDOT =        -633
171233  meter/sec
 ZDOT =      19137
342195                 ZDOT =        5833
061901


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   16056
50251098  
00016717  00000-0  10270-3 0  9016
2 25544  51
6392 259
9784 0003500 170
1793 189
9429 15
54261730 27452


Satellite: ISS
Catalog Number: 25544
Epoch time:      16056
50251098   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       259
9784  deg
Eccentricity:     
0003500     
Arg of perigee:   170
1793  deg
Mean anomaly:     189
9429  deg
Mean motion:   15
54261730  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2745
Checksum:              322


Coasting Arc #3 (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    =        1469335
02                 A    =         6788802
77  meter
 Y    =        6601711
37  meter          E    =           
0014046
 Z    =        -495877
26                 I    =           51
30346
 XDOT =      -4787
295422                 Wp   =          146
21643
 YDOT =        624
729683  meter/sec      RA   =          254
08520  deg
 ZDOT =      -5961
045856                 TA   =           39
15958
                                          MA   =           39
05802
                                          Ha   =            221
279  n
mi
                                          Hp   =            214
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4820652
97                 X    =         1397812
58
 Y    =       21659158
03  feet           Y    =         6617742
48  meter
 Z    =       -1626893
90                 Z    =         -488914
28
 XDOT =     -15706
349811                 XDOT =       -4764
969618
 YDOT =       2049
638067  feet/sec       YDOT =         571
318993  meter/sec
 ZDOT =     -19557
237062                 ZDOT =       -5984
246944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4800678
96                 X    =        -1463246
95
 Y    =       21665756
07  feet           Y    =         6603722
45  meter
 Z    =       -1597842
64                 Z    =         -487022
44
 XDOT =     -13400
618306                 XDOT =       -4084
508460
 YDOT =      -4396
162998  feet/sec       YDOT =       -1339
950482  meter/sec
 ZDOT =     -19657
912889                 ZDOT =       -5991
731849


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
53125014  
00016717  00000-0  10270-3 0  9029
2 25544  51
6393 254
8483 0003421 171
9326 188
1882 15
54275479 27613


Satellite: ISS
Catalog Number: 25544
Epoch time:      16057
53125014   =   yrday
fracday
Element set:     902
Inclination:       51
6393  deg
RA of node:       254
8483  deg
Eccentricity:     
0003421     
Arg of perigee:   171
9326  deg
Mean anomaly:     188
1882  deg
Mean motion:   15
54275479  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2761
Checksum:              316


Coasting Arc #4 (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    =        -575426
89                 A    =         6786822
03  meter
 Y    =       -6396967
10  meter          E    =           
0013382
 Z    =        2179433
02                 I    =           51
30539
 XDOT =       5208
845693                 Wp   =           85
92358
 YDOT =       1398
336020  meter/sec      RA   =          249
08847  deg
 ZDOT =       5451
521602                 TA   =          298
38847
                                          MA   =          298
52331
                                          Ha   =            221
221  n
mi
                                          Hp   =            214
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1887883
49                 X    =         -514438
31
 Y    =      -20987424
86  feet           Y    =        -6403060
62  meter
 Z    =        7150370
79                 Z    =         2176786
71
 XDOT =      17089
388758                 XDOT =        5166
341093
 YDOT =       4587
716602  feet/sec       YDOT =        1456
347830  meter/sec
 ZDOT =      17885
569559                 ZDOT =        5476
721242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6798048
53                 X    =         2072045
19
 Y    =      -19949211
95  feet           Y    =        -6080519
80  meter
 Z    =        7139985
12                 Z    =         2176267
46
 XDOT =      12169
388302                 XDOT =        3709
229554
 YDOT =      10620
355229  feet/sec       YDOT =        3237
084274  meter/sec
 ZDOT =      17994
567908                 ZDOT =        5484
744298


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
55998160  
00016717  00000-0  10270-3 0  9033
2 25544  51
6379 249
7182 0003607 176
5612 183
5567 15
54301321 27773


Satellite: ISS
Catalog Number: 25544
Epoch time:      16058
55998160   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:       249
7182  deg
Eccentricity:     
0003607     
Arg of perigee:   176
5612  deg
Mean anomaly:     183
5567  deg
Mean motion:   15
54301321  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2777
Checksum:              330


Coasting Arc #5 (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    =        -492969
18                 A    =         6783123
55  meter
 Y    =        5691830
90  meter          E    =           
0006154
 Z    =       -3659138
34                 I    =           51
30528
 XDOT =      -5430
086598                 Wp   =          114
62915
 YDOT =      -3246
211081  meter/sec      RA   =          244
08466  deg
 ZDOT =      -4326
228492                 TA   =          109
08239
                                          MA   =          109
01573
                                          Ha   =            221
132  n
mi
                                          Hp   =            214
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1617352
94                 X    =         -538805
60
 Y    =       18673985
90  feet           Y    =         5686061
48  meter
 Z    =      -12005047
05                 Z    =        -3661645
05
 XDOT =     -17815
244744                 XDOT =       -5372
368269
 YDOT =     -10650
298823  feet/sec       YDOT =       -3306
611703  meter/sec
 ZDOT =     -14193
663030                 ZDOT =       -4352
465742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8741729
43                 X    =        -2664479
13
 Y    =       16572015
62  feet           Y    =         5051150
36  meter
 Z    =      -12016871
46                 Z    =        -3662742
42
 XDOT =     -10916
237067                 XDOT =       -3327
269058
 YDOT =     -16112
996989  feet/sec       YDOT =       -4911
241482  meter/sec
 ZDOT =     -14306
855868                 ZDOT =       -4360
729668


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
52441290  
00016717  00000-0  10270-3 0  9049
2 25544  51
6378 244
9090 0003485 178
0794 182
0373 15
54306150 27920


Satellite: ISS
Catalog Number: 25544
Epoch time:      16059
52441290   =   yrday
fracday
Element set:     904
Inclination:       51
6378  deg
RA of node:       244
9090  deg
Eccentricity:     
0003485     
Arg of perigee:   178
0794  deg
Mean anomaly:     182
0373  deg
Mean motion:   15
54306150  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2792
Checksum:              313


Coasting Arc #6 (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    =        1637547
16                 A    =         6779409
24  meter
 Y    =       -4596597
74  meter          E    =           
0009769
 Z    =        4703663
52                 I    =           51
30800
 XDOT =       5385
599714                 Wp   =          136
21148
 YDOT =       4727
278437  meter/sec      RA   =          239
07040  deg
 ZDOT =       2734
370475                 TA   =          286
55718
                                          MA   =          286
66446
                                          Ha   =            221
026  n
mi
                                          Hp   =            214
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5372530
04                 X    =         1665977
51
 Y    =      -15080701
23  feet           Y    =        -4578126
13  meter
 Z    =       15431966
93                 Z    =         4711687
81
 XDOT =      17669
290401                 XDOT =        5319
055534
 YDOT =      15509
443691  feet/sec       YDOT =        4787
132010  meter/sec
 ZDOT =       8971
031743                 ZDOT =        2760
370074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10561296
69                 X    =         3219083
23
 Y    =      -11985491
44  feet           Y    =        -3653177
79  meter
 Z    =       15467522
08                 Z    =         4714500
73
 XDOT =       9604
095599                 XDOT =        2927
328339
 YDOT =      20228
323233  feet/sec       YDOT =        6165
592922  meter/sec
 ZDOT =       9082
958696                 ZDOT =        2768
485810


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
55313114  
00016717  00000-0  10270-3 0  9058
2 25544  51
6382 239
7788 0003463 183
6261 176
4867 15
54295607 28085


Satellite: ISS
Catalog Number: 25544
Epoch time:      16060
55313114   =   yrday
fracday
Element set:     905
Inclination:       51
6382  deg
RA of node:       239
7788  deg
Eccentricity:     
0003463     
Arg of perigee:   183
6261  deg
Mean anomaly:     176
4867  deg
Mean motion:   15
54295607  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2808
Checksum:              327


Coasting Arc #7 (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    =       -2859846
65                 A    =         6777031
22  meter
 Y    =        3214182
45  meter          E    =           
0014384
 Z    =       -5248398
61                 I    =           51
31749
 XDOT =      -4982
788556                 Wp   =           97
95735
 YDOT =      -5758
543125  meter/sec      RA   =          234
04868  deg
 ZDOT =       -815
362632                 TA   =          164
22644
                                          MA   =          164
18159
                                          Ha   =            221
041  n
mi
                                          Hp   =            214
201

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9382698
99                 X    =        -2870081
60
 Y    =       10545218
01  feet           Y    =         3182144
01  meter
 Z    =      -17219155
55                 Z    =        -5262316
10
 XDOT =     -16347
731484                 XDOT =       -4914
064116
 YDOT =     -18892
858022  feet/sec       YDOT =       -5813
879792  meter/sec
 ZDOT =      -2675
074252                 ZDOT =        -839
400127

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12448769
91                 X    =        -3794385
07
 Y    =        6493434
41  feet           Y    =         1979198
81  meter
 Z    =      -17280029
46                 Z    =        -5266952
98
 XDOT =      -7950
044376                 XDOT =       -2423
173526
 YDOT =     -22601
134987  feet/sec       YDOT =       -6888
825944  meter/sec
 ZDOT =      -2778
338495                 ZDOT =        -846
837573


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
51754711  
00016717  00000-0  10270-3 0  9068
2 25544  51
6381 234
9699 0003577 182
5729 177
5406 15
54321635 28234


Satellite: ISS
Catalog Number: 25544
Epoch time:      16061
51754711   =   yrday
fracday
Element set:     906
Inclination:       51
6381  deg
RA of node:       234
9699  deg
Eccentricity:     
0003577     
Arg of perigee:   182
5729  deg
Mean anomaly:     177
5406  deg
Mean motion:   15
54321635  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2823
Checksum:              326


Coasting Arc #8 (Orbit 2831)
---------------------------------------

Vector Time (GMT): 2016/062/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890989
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2050741
15                 A    =         6777667
12  meter
 Y    =       -3966197
82  meter          E    =           
0007135
 Z    =        5097397
63                 I    =           51
33018
 XDOT =       5618
307205                 Wp   =          149
42850
 YDOT =       4970
585633  meter/sec      RA   =          231
32898  deg
 ZDOT =       1600
193973                 TA   =          285
03396
                                          MA   =          285
11291
                                          Ha   =            220
839  n
mi
                                          Hp   =            214
441

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6728153
38                 X    =         2070178
97
 Y    =      -13012460
04  feet           Y    =        -3943155
93  meter
 Z    =       16723745
52                 Z    =         5107407
11
 XDOT =      18432
766420                 XDOT =        5554
534328
 YDOT =      16307
695647  feet/sec       YDOT =        5033
056844  meter/sec
 ZDOT =       5249
980225                 ZDOT =        1627
330742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7585720
72                 X    =        -2312127
67
 Y    =       12472913
27  feet           Y    =         3801743
96  meter
 Z    =       16767799
62                 Z    =         5110825
33
 XDOT =     -16202
906077                 XDOT =       -4938
645772
 YDOT =     -17099
929439  feet/sec       YDOT =       -5212
058493  meter/sec
 ZDOT =       5366
821739                 ZDOT =        1635
807266


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
09619336  
00016717  00000-0  10270-3 0  9076
2 25544  51
6382 232
0879 0003271 188
2145 171
8954 15
54324594 28322


Satellite: ISS
Catalog Number: 25544
Epoch time:      16062
09619336   =   yrday
fracday
Element set:     907
Inclination:       51
6382  deg
RA of node:       232
0879  deg
Eccentricity:     
0003271     
Arg of perigee:   188
2145  deg
Mean anomaly:     171
8954  deg
Mean motion:   15
54324594  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2832
Checksum:              322


Coasting Arc #9 (Orbit 2846)
---------------------------------------

Vector Time (GMT): 2016/063/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890989
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3376214
58                 A    =         6776835
67  meter
 Y    =        2588038
19  meter          E    =           
0014679
 Z    =       -5287786
21                 I    =           51
34851
 XDOT =      -5044
387479                 Wp   =          105
93606
 YDOT =      -5748
045406  meter/sec      RA   =          226
30603  deg
 ZDOT =        404
486061                 TA   =          167
95941
                                          MA   =          167
92428
                                          Ha   =            220
815  n
mi
                                          Hp   =            214
385

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11076819
50                 X    =        -3379218
21
 Y    =        8490938
95  feet           Y    =         2550265
88  meter
 Z    =      -17348379
95                 Z    =        -5304194
36
 XDOT =     -16549
827688                 XDOT =       -4981
701302
 YDOT =     -18858
416686  feet/sec       YDOT =       -5804
104562  meter/sec
 ZDOT =       1327
054007                 ZDOT =         380
134675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11442777
11                 X    =         3487758
46
 Y    =       -7833664
99  feet           Y    =        -2387701
09  meter
 Z    =      -17419954
26                 Z    =        -5309602
06
 XDOT =      14855
718017                 XDOT =        4528
022852
 YDOT =      18959
832697  feet/sec       YDOT =        5778
957006  meter/sec
 ZDOT =       1222
399323                 ZDOT =         372
587314


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
06059879  
00016717  00000-0  10270-3 0  9085
2 25544  51
6385 227
2786 0003267 191
4934 168
6145 15
54323845 28475


Satellite: ISS
Catalog Number: 25544
Epoch time:      16063
06059879   =   yrday
fracday
Element set:     908
Inclination:       51
6385  deg
RA of node:       227
2786  deg
Eccentricity:     
0003267     
Arg of perigee:   191
4934  deg
Mean anomaly:     168
6145  deg
Mean motion:   15
54323845  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2847
Checksum:              344


Coasting Arc #10 (Orbit 2862)
---------------------------------------

Vector Time (GMT): 2016/064/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890989
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4573808
72                 A    =         6778508
49  meter
 Y    =       -1154855
11  meter          E    =           
0004884
 Z    =        4863673
04                 I    =           51
37785
 XDOT =       4050
279977                 Wp   =           84
75704
 YDOT =       6070
969853  meter/sec      RA   =          221
28662  deg
 ZDOT =      -2364
880959                 TA   =           28
49493
                                          MA   =           28
46824
                                          Ha   =            220
528  n
mi
                                          Hp   =            214
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15005934
13                 X    =         4562757
34
 Y    =       -3788894
70  feet           Y    =        -1103769
13  meter
 Z    =       15956932
54                 Z    =         4885864
42
 XDOT =      13288
320135                 XDOT =        3993
579289
 YDOT =      19917
880096  feet/sec       YDOT =        6115
945546  meter/sec
 ZDOT =      -7758
795796                 ZDOT =       -2345
344185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15046785
34                 X    =        -4586260
17
 Y    =        3168814
73  feet           Y    =          965854
73  meter
 Z    =       16053359
23                 Z    =         4893063
89
 XDOT =     -12272
995529                 XDOT =       -3740
809037
 YDOT =     -19353
739839  feet/sec       YDOT =       -5899
019903  meter/sec
 ZDOT =      -7675
053328                 ZDOT =       -2339
356255


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
08928881  
00016717  00000-0  10270-3 0  9097
2 25544  51
6391 222
1491 0003160 196
8714 163
2335 15
54351671 28634


Satellite: ISS
Catalog Number: 25544
Epoch time:      16064
08928881   =   yrday
fracday
Element set:     909
Inclination:       51
6391  deg
RA of node:       222
1491  deg
Eccentricity:     
0003160     
Arg of perigee:   196
8714  deg
Mean anomaly:     163
2335  deg
Mean motion:   15
54351671  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2863
Checksum:              315


Coasting Arc #11 (Orbit 2867)
---------------------------------------

Vector Time (GMT): 2016/064/09:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 890989
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1062532
55                 A    =         6781237
12  meter
 Y    =        5226163
57  meter          E    =           
0006370
 Z    =       -4193739
96                 I    =           51
39403
 XDOT =      -6534
334587                 Wp   =           93
53156
 YDOT =      -1608
894526  meter/sec      RA   =          219
61395  deg
 ZDOT =      -3665
734245                 TA   =          138
74818
                                          MA   =          138
70003
                                          Ha   =            220
614  n
mi
                                          Hp   =            214
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3485999
18                 X    =         1024384
42
 Y    =       17146205
92  feet           Y    =         5237831
86  meter
 Z    =      -13758989
38                 Z    =        -4188671
61
 XDOT =     -21438
105601                 XDOT =       -6498
051574
 YDOT =      -5278
525347  feet/sec       YDOT =       -1681
763230  meter/sec
 ZDOT =     -12026
687157                 ZDOT =       -3697
387703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12783094
95                 X    =        -3896287
34
 Y    =       11971559
58  feet           Y    =         3648931
36  meter
 Z    =      -13737852
86                 Z    =        -4187297
55
 XDOT =      -5729
842592                 XDOT =       -1746
456022
 YDOT =     -20056
967171  feet/sec       YDOT =       -6113
363594  meter/sec
 ZDOT =     -12163
706878                 ZDOT =       -3707
497856


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
41075163  
00016717  00000-0  10270-3 0  9102
2 25544  51
6381 220
5449 0003171 199
0015 161
1020 15
54355801 28681


Satellite: ISS
Catalog Number: 25544
Epoch time:      16064
41075163   =   yrday
fracday
Element set:     910
Inclination:       51
6381  deg
RA of node:       220
5449  deg
Eccentricity:     
0003171     
Arg of perigee:   199
0015  deg
Mean anomaly:     161
1020  deg
Mean motion:   15
54355801  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2868
Checksum:              277


Coasting Arc #12 (Orbit 2879)
---------------------------------------

Vector Time (GMT): 2016/065/04:08:35
706
Vector Time (MET): N/A
Weight (LBS)     : 890633
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5266454
52                 A    =         6782712
71  meter
 Y    =         407779
80  meter          E    =           
0006544
 Z    =       -4261669
48                 I    =           51
41595
 XDOT =      -3344
028478                 Wp   =          140
45822
 YDOT =      -5898
532265  meter/sec      RA   =          215
63987  deg
 ZDOT =       3566
135631                 TA   =          166
09788
                                          MA   =          166
07986
                                          Ha   =            220
615  n
mi
                                          Hp   =            216
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17278394
11                 X    =        -5249921
98
 Y    =        1337860
22  feet           Y    =          348978
86  meter
 Z    =      -13981855
24                 Z    =        -4287212
07
 XDOT =     -10971
222040                 XDOT =       -3295
143570
 YDOT =     -19352
139977  feet/sec       YDOT =       -5935
653756  meter/sec
 ZDOT =      11699
920048                 ZDOT =        3550
010707

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11290080
22                 X    =         3441216
45
 Y    =      -13028995
37  feet           Y    =        -3971237
79  meter
 Z    =      -14092707
94                 Z    =        -4295457
38
 XDOT =      20507
060887                 XDOT =        6250
552158
 YDOT =       5182
829627  feet/sec       YDOT =        1579
726470  meter/sec
 ZDOT =      11630
926320                 ZDOT =        3545
106342


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
18226397  
00016717  00000-0  10270-3 0  9115
2 25544  51
6413 216
6987 0004243 240
3697 119
7033 15
53718119 28808


Satellite: ISS
Catalog Number: 25544
Epoch time:      16065
18226397   =   yrday
fracday
Element set:     911
Inclination:       51
6413  deg
RA of node:       216
6987  deg
Eccentricity:     
0004243     
Arg of perigee:   240
3697  deg
Mean anomaly:     119
7033  deg
Mean motion:   15
53718119  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2880
Checksum:              317


Coasting Arc #13 (Orbit 2895)
---------------------------------------

Vector Time (GMT): 2016/066/04:08:35
706
Vector Time (MET): N/A
Weight (LBS)     : 890633
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5977054
23                 A    =         6786280
49  meter
 Y    =         633666
33  meter          E    =           
0009395
 Z    =        3139548
49                 I    =           51
45412
 XDOT =       1946
511627                 Wp   =          107
83542
 YDOT =       5628
667477  meter/sec      RA   =          210
64478  deg
 ZDOT =      -4832
699397                 TA   =           35
86774
                                          MA   =           35
80469
                                          Ha   =            220
418  n
mi
                                          Hp   =            216
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19609757
96                 X    =         5954273
88
 Y    =        2078957
78  feet           Y    =          700378
68  meter
 Z    =       10300355
95                 Z    =         3168527
61
 XDOT =       6386
193002                 XDOT =        1906
900560
 YDOT =      18466
756815  feet/sec       YDOT =        5650
212671  meter/sec
 ZDOT =     -15855
312981                 ZDOT =       -4823
340706

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15153322
77                 X    =        -4618732
78
 Y    =       12515515
27  feet           Y    =         3814729
05  meter
 Z    =       10425962
41                 Z    =         3177833
34
 XDOT =     -16823
904422                 XDOT =       -5127
926068
 YDOT =      -7170
073671  feet/sec       YDOT =       -2185
438455  meter/sec
 ZDOT =     -15815
609311                 ZDOT =       -4820
597718


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
21137203  
00016717  00000-0  10270-3 0  9128
2 25544  51
6412 211
5727 0004313 243
7288 116
3421 15
53704619 28965


Satellite: ISS
Catalog Number: 25544
Epoch time:      16066
21137203   =   yrday
fracday
Element set:     912
Inclination:       51
6412  deg
RA of node:       211
5727  deg
Eccentricity:     
0004313     
Arg of perigee:   243
7288  deg
Mean anomaly:     116
3421  deg
Mean motion:   15
53704619  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2896
Checksum:              287


Coasting Arc #14 (Orbit 2910)
---------------------------------------

Vector Time (GMT): 2016/067/04:08:35
706
Vector Time (MET): N/A
Weight (LBS)     : 890633
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6378575
69                 A    =         6789076
42  meter
 Y    =       -1520519
19  meter          E    =           
0004287
 Z    =       -1748724
73                 I    =           51
49338
 XDOT =       -322
578915                 Wp   =            7
44534
 YDOT =      -5154
551402  meter/sec      RA   =          205
65803  deg
 ZDOT =       5664
239475                 TA   =          333
32924
                                          MA   =          333
35129
                                          Ha   =            220
295  n
mi
                                          Hp   =            216
745

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20927085
59                 X    =        -6352604
40
 Y    =       -4988580
03  feet           Y    =        -1591703
67  meter
 Z    =       -5737285
85                 Z    =        -1779646
42
 XDOT =      -1058
329775                 XDOT =        -292
429411
 YDOT =     -16911
257879  feet/sec       YDOT =       -5157
989402  meter/sec
 ZDOT =      18583
462843                 ZDOT =        5662
746374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17975063
57                 X    =         5478799
38
 Y    =      -11754635
29  feet           Y    =        -3582812
84  meter
 Z    =       -5871194
92                 Z    =        -1789540
21
 XDOT =      12240
871403                 XDOT =        3731
017604
 YDOT =       9448
554130  feet/sec       YDOT =        2879
919299  meter/sec
 ZDOT =      18577
794231                 ZDOT =        5662
511682


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
17615119  
00016717  00000-0  10270-3 0  9132
2 25544  51
6427 206
7653 0004354 249
4130 110
6556 15
53747510 29110


Satellite: ISS
Catalog Number: 25544
Epoch time:      16067
17615119   =   yrday
fracday
Element set:     913
Inclination:       51
6427  deg
RA of node:       206
7653  deg
Eccentricity:     
0004354     
Arg of perigee:   249
4130  deg
Mean anomaly:     110
6556  deg
Mean motion:   15
53747510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2911
Checksum:              296


Coasting Arc #15 (Orbit 2921)
---------------------------------------

Vector Time (GMT): 2016/067/19:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890633
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6240432
78                 A    =         6790437
28  meter
 Y    =       -2663047
54  meter          E    =           
0008565
 Z    =          99069
50                 I    =           51
51568
 XDOT =       1956
851177                 Wp   =           35
17435
 YDOT =      -4352
968887  meter/sec      RA   =          202
44482  deg
 ZDOT =       6000
502639                 TA   =          325
89436
                                          MA   =          325
94936
                                          Ha   =            220
321  n
mi
                                          Hp   =            216
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20473860
84                 X    =        -6210671
35
 Y    =       -8737032
61  feet           Y    =        -2732665
79  meter
 Z    =         325031
17                 Z    =           68828
22
 XDOT =       6420
115409                 XDOT =        1976
234356
 YDOT =     -14281
393987  feet/sec       YDOT =       -4330
976864  meter/sec
 ZDOT =      19686
688449                 ZDOT =        6010
056053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5009612
32                 X    =        -1526929
83
 Y    =       21690698
84  feet           Y    =         6611325
01  meter
 Z    =         194242
35                 Z    =           59205
07
 XDOT =     -13580
513345                 XDOT =       -4139
340468
 YDOT =      -3325
574521  feet/sec       YDOT =       -1013
635114  meter/sec
 ZDOT =      19728
815345                 ZDOT =        6013
342917


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
88365127  
00016717  00000-0  10270-3 0  9142
2 25544  51
6418 203
2397 0004178 250
1695 109
9007 15
53746994 29225


Satellite: ISS
Catalog Number: 25544
Epoch time:      16067
88365127   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:       203
2397  deg
Eccentricity:     
0004178     
Arg of perigee:   250
1695  deg
Mean anomaly:     109
9007  deg
Mean motion:   15
53746994  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2922
Checksum:              331


Coasting Arc #16 (Orbit 2936)
---------------------------------------

Vector Time (GMT): 2016/068/19:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890633
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5742176
19                 A    =         6789334
32  meter
 Y    =        3201993
23  meter          E    =           
0007518
 Z    =       -1675256
97                 I    =           51
54043
 XDOT =      -3662
785919                 Wp   =          174
23295
 YDOT =       3592
221068  meter/sec      RA   =          197
46849  deg
 ZDOT =      -5698
279237                 TA   =           24
14774
                                          MA   =           24
11252
                                          Ha   =            220
328  n
mi
                                          Hp   =            216
789

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18839160
72                 X    =         5714081
50
 Y    =       10505227
13  feet           Y    =         3266048
71  meter
 Z    =       -5496249
89                 Z    =        -1647432
04
 XDOT =     -12017
014170                 XDOT =       -3675
003397
 YDOT =      11785
502190  feet/sec       YDOT =        3551
192163  meter/sec
 ZDOT =     -18695
141854                 ZDOT =       -5716
102116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6678499
56                 X    =         2035606
67
 Y    =      -20542119
04  feet           Y    =        -6261237
88  meter
 Z    =       -5376013
89                 Z    =        -1638609
03
 XDOT =      12353
982657                 XDOT =        3765
493914
 YDOT =       8921
087913  feet/sec       YDOT =        2719
147596  meter/sec
 ZDOT =     -18773
029939                 ZDOT =       -5722
019525


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
84842032  
00016717  00000-0  10270-3 0  9155
2 25544  51
6405 198
4335 0004206 252
5368 107
5325 15
53734852 29376


Satellite: ISS
Catalog Number: 25544
Epoch time:      16068
84842032   =   yrday
fracday
Element set:     915
Inclination:       51
6405  deg
RA of node:       198
4335  deg
Eccentricity:     
0004206     
Arg of perigee:   252
5368  deg
Mean anomaly:     107
5325  deg
Mean motion:   15
53734852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2937
Checksum:              315


Coasting Arc #17 (Orbit 2952)
---------------------------------------

Vector Time (GMT): 2016/069/19:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890633
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4859519
93                 A    =         6786410
58  meter
 Y    =       -3585930
39  meter          E    =           
0008825
 Z    =        3087197
25                 I    =           51
56185
 XDOT =       5193
194680                 Wp   =           86
92270
 YDOT =      -2821
419888  meter/sec      RA   =          192
48864  deg
 ZDOT =       4885
715491                 TA   =          308
60486
                                          MA   =          308
68386
                                          Ha   =            220
141  n
mi
                                          Hp   =            216
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15943306
86                 X    =        -4834056
14
 Y    =      -11764863
49  feet           Y    =        -3640129
89  meter
 Z    =       10128599
91                 Z    =         3063653
58
 XDOT =      17038
040288                 XDOT =        5200
626045
 YDOT =      -9256
626930  feet/sec       YDOT =       -2763
303786  meter/sec
 ZDOT =      16029
250300                 ZDOT =        4910
961001

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8155052
95                 X    =        -2485660
14
 Y    =       18114750
97  feet           Y    =         5521376
10  meter
 Z    =       10026988
15                 Z    =         3056225
99
 XDOT =     -11271
962671                 XDOT =       -3435
694222
 YDOT =     -14029
297539  feet/sec       YDOT =       -4276
129890  meter/sec
 ZDOT =      16139
232160                 ZDOT =        4919
237962


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
87749731  
00016717  00000-0  10270-3 0  9162
2 25544  51
6406 193
3065 0004258 259
0482 101
0192 15
53771263 29533


Satellite: ISS
Catalog Number: 25544
Epoch time:      16069
87749731   =   yrday
fracday
Element set:     916
Inclination:       51
6406  deg
RA of node:       193
3065  deg
Eccentricity:     
0004258     
Arg of perigee:   259
0482  deg
Mean anomaly:     101
0192  deg
Mean motion:   15
53771263  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2953
Checksum:              319
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