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

 
Date: January 12th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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


There are no maneuvers



Coasting Arc #1 (Orbit 2046)
---------------------------------------

Vector Time (GMT): 2016/011/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4859875
05                 A    =         6786336
27  meter
 Y    =        4099771
16  meter          E    =           
0016845
 Z    =        2343311
93                 I    =           51
96000
 XDOT =      -1715
888292                 Wp   =           54
21096
 YDOT =      -5147
118315  meter/sec      RA   =          123
08949  deg
 ZDOT =       5428
945139                 TA   =          331
83435
                                          MA   =          331
92536
                                          Ha   =            221
767  n
mi
                                          Hp   =            213
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15944471
96                 X    =        -4916741
14
 Y    =       13450692
80  feet           Y    =         4045106
75  meter
 Z    =        7688031
27                 Z    =         2319566
32
 XDOT =      -5629
554763                 XDOT =       -1684
575501
 YDOT =     -16886
871111  feet/sec       YDOT =       -5166
131712  meter/sec
 ZDOT =      17811
499800                 ZDOT =        5420
685696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20814945
51                 X    =        -6344395
39
 Y    =       -1862481
55  feet           Y    =         -567684
38  meter
 Z    =        7584349
25                 Z    =         2311709
65
 XDOT =       7792
347201                 XDOT =        2375
107427
 YDOT =     -14458
499110  feet/sec       YDOT =       -4406
950529  meter/sec
 ZDOT =      17776
623942                 ZDOT =        5418
314978


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   16011
62957874  
00016717  00000-0  10270-3 0  9004
2 25544  51
6429 123
7794 0005805   4
3594 355
7608 15
54379431 20474


Satellite: ISS
Catalog Number: 25544
Epoch time:      16011
62957874   =   yrday
fracday
Element set:     900
Inclination:       51
6429  deg
RA of node:       123
7794  deg
Eccentricity:     
0005805     
Arg of perigee:     4
3594  deg
Mean anomaly:     355
7608  deg
Mean motion:   15
54379431  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2047
Checksum:              322


Coasting Arc #2 (Orbit 2061)
---------------------------------------

Vector Time (GMT): 2016/012/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4875317
06                 A    =         6782512
00  meter
 Y    =       -2779917
04  meter          E    =           
0009761
 Z    =       -3820414
42                 I    =           51
96310
 XDOT =        331
666571                 Wp   =           42
91678
 YDOT =       6382
329489  meter/sec      RA   =          118
12985  deg
 ZDOT =      -4220
219868                 TA   =          182
68289
                                          MA   =          182
68813
                                          Ha   =            221
771  n
mi
                                          Hp   =            213
798

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15995134
71                 X    =         4924598
07
 Y    =       -9120462
74  feet           Y    =        -2725122
35  meter
 Z    =      -12534168
04                 Z    =        -3796612
12
 XDOT =       1088
144917                 XDOT =         280
772828
 YDOT =      20939
401212  feet/sec       YDOT =        6385
753978  meter/sec
 ZDOT =     -13845
865710                 ZDOT =       -4218
732146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17884310
54                 X    =         5451137
85
 Y    =        4665561
54  feet           Y    =         1422063
16  meter
 Z    =      -12430467
22                 Z    =        -3788806
41
 XDOT =     -13411
479958                 XDOT =       -4087
819091
 YDOT =      14528
729832  feet/sec       YDOT =        4428
356853  meter/sec
 ZDOT =     -13840
573310                 ZDOT =       -4218
606745


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   16012
59395133  
00016717  00000-0  10270-3 0  9016
2 25544  51
6420 118
9706 0005847   7
6472 352
4769 15
54383432 20626


Satellite: ISS
Catalog Number: 25544
Epoch time:      16012
59395133   =   yrday
fracday
Element set:     901
Inclination:       51
6420  deg
RA of node:       118
9706  deg
Eccentricity:     
0005847     
Arg of perigee:     7
6472  deg
Mean anomaly:     352
4769  deg
Mean motion:   15
54383432  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2062
Checksum:              306


Coasting Arc #3 (Orbit 2077)
---------------------------------------

Vector Time (GMT): 2016/013/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4601571
02                 A    =         6778603
67  meter
 Y    =        1130371
10  meter          E    =           
0007801
 Z    =        4840076
50                 I    =           51
96518
 XDOT =        910
148087                 Wp   =           73
29754
 YDOT =      -7183
628291  meter/sec      RA   =          113
15868  deg
 ZDOT =       2541
802454                 TA   =          351
82899
                                          MA   =          351
84169
                                          Ha   =            221
956  n
mi
                                          Hp   =            213
467

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15097017
77                 X    =        -4637379
77
 Y    =        3708566
59  feet           Y    =         1078713
00  meter
 Z    =       15879516
09                 Z    =         4817636
59
 XDOT =       2986
050154                 XDOT =         978
062744
 YDOT =     -23568
334288  feet/sec       YDOT =       -7173
070716  meter/sec
 ZDOT =       8339
246895                 ZDOT =        2546
388511

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13617945
63                 X    =        -4150749
83
 Y    =       -7701432
34  feet           Y    =        -2347396
58  meter
 Z    =       15782013
17                 Z    =         4810357
61
 XDOT =      17711
225579                 XDOT =        5398
381557
 YDOT =     -14177
095348  feet/sec       YDOT =       -4321
178662  meter/sec
 ZDOT =       8360
440505                 ZDOT =        2548
262266


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   16013
62260016  
00016717  00000-0  10270-3 0  9023
2 25544  51
6424 113
8400 0005945  11
1108 349
0175 15
54433299 20787


Satellite: ISS
Catalog Number: 25544
Epoch time:      16013
62260016   =   yrday
fracday
Element set:     902
Inclination:       51
6424  deg
RA of node:       113
8400  deg
Eccentricity:     
0005945     
Arg of perigee:    11
1108  deg
Mean anomaly:     349
0175  deg
Mean motion:   15
54433299  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2078
Checksum:              274


Coasting Arc #4 (Orbit 2092)
---------------------------------------

Vector Time (GMT): 2016/014/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4152686
22                 A    =         6776639
86  meter
 Y    =         700526
57  meter          E    =           
0017656
 Z    =       -5323689
94                 I    =           51
96906
 XDOT =      -1965
112539                 Wp   =           66
71641
 YDOT =       7379
103496  meter/sec      RA   =          108
18015  deg
 ZDOT =       -556
549769                 TA   =          197
95737
                                          MA   =          198
01983
                                          Ha   =            221
975  n
mi
                                          Hp   =            213
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13624298
62                 X    =         4170404
00
 Y    =        2298315
51  feet           Y    =          747063
72  meter
 Z    =      -17466174
34                 Z    =        -5303474
44
 XDOT =      -6447
219615                 XDOT =       -2044
777994
 YDOT =      24209
657139  feet/sec       YDOT =        7356
682872  meter/sec
 ZDOT =      -1825
950685                 ZDOT =        -566
289167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8628791
83                 X    =         2630055
75
 Y    =       10931497
49  feet           Y    =         3331920
44  meter
 Z    =      -17378645
72                 Z    =        -5297011
22
 XDOT =     -20237
456978                 XDOT =       -6168
376887
 YDOT =      12974
414684  feet/sec       YDOT =        3954
601596  meter/sec
 ZDOT =      -1869
534641                 ZDOT =        -569
834159


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   16014
58694774  
00016717  00000-0  10270-3 0  9032
2 25544  51
6413 109
0306 0006082  14
6935 345
4393 15
54412995 20935


Satellite: ISS
Catalog Number: 25544
Epoch time:      16014
58694774   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:       109
0306  deg
Eccentricity:     
0006082     
Arg of perigee:    14
6935  deg
Mean anomaly:     345
4393  deg
Mean motion:   15
54412995  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2093
Checksum:              311


Coasting Arc #5 (Orbit 2108)
---------------------------------------

Vector Time (GMT): 2016/015/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3545023
18                 A    =         6777042
20  meter
 Y    =       -2575734
85  meter          E    =           
0010294
 Z    =        5166742
67                 I    =           51
98071
 XDOT =       2845
122353                 Wp   =           33
90510
 YDOT =      -6963
028809  meter/sec      RA   =          103
19910  deg
 ZDOT =      -1509
352885                 TA   =           70
61220
                                          MA   =           70
50096
                                          Ha   =            222
035  n
mi
                                          Hp   =            213
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11630653
47                 X    =        -3541054
79
 Y    =       -8450573
66  feet           Y    =        -2615355
44  meter
 Z    =       16951255
49                 Z    =         5149531
64
 XDOT =       9334
390923                 XDOT =        2930
104923
 YDOT =     -22844
582707  feet/sec       YDOT =       -6930
737609  meter/sec
 ZDOT =      -4951
945161                 ZDOT =       -1495
325673

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3258486
56                 X    =         -993186
70
 Y    =      -14091669
85  feet           Y    =        -4295140
97  meter
 Z    =       16877098
81                 Z    =         5144139
72
 XDOT =      21074
294361                 XDOT =        6423
444921
 YDOT =     -10768
032739  feet/sec       YDOT =       -3282
096379  meter/sec
 ZDOT =      -4889
832255                 ZDOT =       -1490
420871


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   16015
61556912  
00016717  00000-0  10270-3 0  9049
2 25544  51
6417 103
8997 0006159  18
0538 342
0833 15
54487217 21098


Satellite: ISS
Catalog Number: 25544
Epoch time:      16015
61556912   =   yrday
fracday
Element set:     904
Inclination:       51
6417  deg
RA of node:       103
8997  deg
Eccentricity:     
0006159     
Arg of perigee:    18
0538  deg
Mean anomaly:     342
0833  deg
Mean motion:   15
54487217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2109
Checksum:              311


Coasting Arc #6 (Orbit 2123)
---------------------------------------

Vector Time (GMT): 2016/016/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2882094
27                 A    =         6780033
06  meter
 Y    =        4255743
64  meter          E    =           
0011359
 Z    =       -4429627
85                 I    =           51
99653
 XDOT =      -3525
254079                 Wp   =           76
60027
 YDOT =       5900
414868  meter/sec      RA   =           98
22437  deg
 ZDOT =       3384
951894                 TA   =          227
45512
                                          MA   =          227
55107
                                          Ha   =            222
160  n
mi
                                          Hp   =            212
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9455689
87                 X    =         2855808
40
 Y    =       13962413
53  feet           Y    =         4287826
16  meter
 Z    =      -14532899
76                 Z    =        -4415691
28
 XDOT =     -11565
794221                 XDOT =       -3607
414511
 YDOT =      19358
316495  feet/sec       YDOT =        5860
533756  meter/sec
 ZDOT =      11105
485218                 ZDOT =        3367
627636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1732922
25                 X    =         -528194
70
 Y    =       16825160
49  feet           Y    =         5128308
92  meter
 Z    =      -14473257
85                 Z    =        -4411448
99
 XDOT =     -20163
306758                 XDOT =       -6145
775900
 YDOT =       7382
943353  feet/sec       YDOT =        2250
321134  meter/sec
 ZDOT =      11029
258101                 ZDOT =        3361
717869


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   16016
57989191  
00016717  00000-0  10270-3 0  9055
2 25544  51
6411  99
0897 0006368  23
7673 336
3773 15
54489526 21243


Satellite: ISS
Catalog Number: 25544
Epoch time:      16016
57989191   =   yrday
fracday
Element set:     905
Inclination:       51
6411  deg
RA of node:        99
0897  deg
Eccentricity:     
0006368     
Arg of perigee:    23
7673  deg
Mean anomaly:     336
3773  deg
Mean motion:   15
54489526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2124
Checksum:              342


Coasting Arc #7 (Orbit 2139)
---------------------------------------

Vector Time (GMT): 2016/017/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2127094
33                 A    =         6784056
23  meter
 Y    =       -5626350
29  meter          E    =           
0016441
 Z    =        3129331
47                 I    =           52
01451
 XDOT =       4071
785291                 Wp   =           73
50813
 YDOT =      -4275
995834  meter/sec      RA   =           93
26020  deg
 ZDOT =      -4894
513929                 TA   =           70
64832
                                          MA   =           70
47063
                                          Ha   =            222
162  n
mi
                                          Hp   =            212
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6978655
95                 X    =        -2079221
89
 Y    =      -18459154
50  feet           Y    =        -5649869
24  meter
 Z    =       10266835
55                 Z    =         3119114
82
 XDOT =      13358
875628                 XDOT =        4143
073252
 YDOT =     -14028
857724  feet/sec       YDOT =       -4230
063777  meter/sec
 ZDOT =     -16058
116565                 ZDOT =       -4874
561201

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6228462
88                 X    =         1898435
48
 Y    =      -18749250
23  feet           Y    =        -5714771
47  meter
 Z    =       10223590
45                 Z    =         3116150
37
 XDOT =      17935
052262                 XDOT =        5466
603929
 YDOT =      -2796
844589  feet/sec       YDOT =        -852
478231  meter/sec
 ZDOT =     -15970
781860                 ZDOT =       -4867
894311


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   16017
60848719  
00016717  00000-0  10270-3 0  9061
2 25544  51
6416  93
9585 0006470  26
2129 333
9350 15
54526732 21406


Satellite: ISS
Catalog Number: 25544
Epoch time:      16017
60848719   =   yrday
fracday
Element set:     906
Inclination:       51
6416  deg
RA of node:        93
9585  deg
Eccentricity:     
0006470     
Arg of perigee:    26
2129  deg
Mean anomaly:     333
9350  deg
Mean motion:   15
54526732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2140
Checksum:              311


Coasting Arc #8 (Orbit 2154)
---------------------------------------

Vector Time (GMT): 2016/018/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1358999
32                 A    =         6787292
81  meter
 Y    =        6472826
23  meter          E    =           
0014862
 Z    =       -1495406
93                 I    =           52
02612
 XDOT =      -4467
693768                 Wp   =           34
48911
 YDOT =       2270
396880  meter/sec      RA   =           88
30762  deg
 ZDOT =       5807
170930                 TA   =          309
26502
                                          MA   =          309
39678
                                          Ha   =            222
315  n
mi
                                          Hp   =            212
595

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4458659
20                 X    =         1293781
59
 Y    =       21236306
52  feet           Y    =         6487658
85  meter
 Z    =       -4906190
71                 Z    =        -1488963
49
 XDOT =     -14657
787952                 XDOT =       -4520
958472
 YDOT =       7448
808663  feet/sec       YDOT =        2220
138181  meter/sec
 ZDOT =      19052
398065                 ZDOT =        5785
338777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9630924
12                 X    =        -2935505
67
 Y    =       19451658
74  feet           Y    =         5928865
58  meter
 Z    =       -4879481
19                 Z    =        -1487265
87
 XDOT =     -14799
221012                 XDOT =       -4510
802565
 YDOT =      -2605
025631  feet/sec       YDOT =        -794
011812  meter/sec
 ZDOT =      18957
281904                 ZDOT =        5778
179524


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   16018
57278494  
00016717  00000-0  10270-3 0  9076
2 25544  51
6417  89
1485 0006564  30
5283 329
6251 15
54505270 21558


Satellite: ISS
Catalog Number: 25544
Epoch time:      16018
57278494   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:        89
1485  deg
Eccentricity:     
0006564     
Arg of perigee:    30
5283  deg
Mean anomaly:     329
6251  deg
Mean motion:   15
54505270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2155
Checksum:              318


Coasting Arc #9 (Orbit 2170)
---------------------------------------

Vector Time (GMT): 2016/019/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -492994
96                 A    =         6788044
65  meter
 Y    =       -6758373
19  meter          E    =           
0011815
 Z    =        -373673
13                 I    =           52
02792
 XDOT =       4734
011952                 Wp   =          104
13153
 YDOT =        -20
997613  meter/sec      RA   =           83
36114  deg
 ZDOT =      -6027
788271                 TA   =           79
87360
                                          MA   =           79
74034
                                          Ha   =            222
328  n
mi
                                          Hp   =            212
390

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1617437
52                 X    =         -415569
39
 Y    =      -22173140
40  feet           Y    =        -6763453
26  meter
 Z    =       -1225961
72                 Z    =         -375880
20
 XDOT =      15531
535276                 XDOT =        4763
175120
 YDOT =        -68
889808  feet/sec       YDOT =          32
104562  meter/sec
 ZDOT =     -19776
208237                 ZDOT =       -6004
720940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12154429
19                 X    =         3704670
02
 Y    =      -18614880
28  feet           Y    =        -5673815
51  meter
 Z    =       -1234230
38                 Z    =         -376193
42
 XDOT =      11142
029321                 XDOT =        3396
090537
 YDOT =       8544
714103  feet/sec       YDOT =        2604
428858  meter/sec
 ZDOT =     -19676
159197                 ZDOT =       -5997
293323


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   16019
60135484  
00016717  00000-0  10270-3 0  9083
2 25544  51
6424  84
0172 0006661  35
0364 325
1226 15
54547962 21716


Satellite: ISS
Catalog Number: 25544
Epoch time:      16019
60135484   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:        84
0172  deg
Eccentricity:     
0006661     
Arg of perigee:    35
0364  deg
Mean anomaly:     325
1226  deg
Mean motion:   15
54547962  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2171
Checksum:              293


Coasting Arc #10 (Orbit 2186)
---------------------------------------

Vector Time (GMT): 2016/020/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -402603
21                 A    =         6786215
82  meter
 Y    =        6410970
95  meter          E    =           
0020104
 Z    =        2154214
51                 I    =           52
01632
 XDOT =      -4856
251706                 Wp   =           59
98501
 YDOT =      -2173
924264  meter/sec      RA   =           78
41309  deg
 ZDOT =       5533
421377                 TA   =          323
80603
                                          MA   =          323
94191
                                          Ha   =            222
533  n
mi
                                          Hp   =            212
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1320876
69                 X    =         -484726
49
 Y    =       21033369
25  feet           Y    =         6406009
48  meter
 Z    =        7067632
92                 Z    =         2152059
65
 XDOT =     -15932
584336                 XDOT =       -4858
460127
 YDOT =      -7132
297454  feet/sec       YDOT =       -2228
242714  meter/sec
 ZDOT =      18154
269610                 ZDOT =        5509
825684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13555829
78                 X    =        -4131816
92
 Y    =       16141142
16  feet           Y    =         4919820
13  meter
 Z    =        7057037
70                 Z    =         2150985
09
 XDOT =      -7533
457267                 XDOT =       -2296
197775
 YDOT =     -14260
573201  feet/sec       YDOT =       -4346
622712  meter/sec
 ZDOT =      18052
351015                 ZDOT =        5502
356590


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   16020
62991313  
00016717  00000-0  10270-3 0  9099
2 25544  51
6418  78
8866 0006891  39
1020 321
0630 15
54526204 21876


Satellite: ISS
Catalog Number: 25544
Epoch time:      16020
62991313   =   yrday
fracday
Element set:     909
Inclination:       51
6418  deg
RA of node:        78
8866  deg
Eccentricity:     
0006891     
Arg of perigee:    39
1020  deg
Mean anomaly:     321
0630  deg
Mean motion:   15
54526204  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2187
Checksum:              299


Coasting Arc #11 (Orbit 2201)
---------------------------------------

Vector Time (GMT): 2016/021/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1398855
01                 A    =         6782172
73  meter
 Y    =       -5503957
84  meter          E    =           
0011878
 Z    =       -3721988
78                 I    =           51
99701
 XDOT =       4764
116180                 Wp   =           58
91798
 YDOT =       4140
056665  meter/sec      RA   =           73
45548  deg
 ZDOT =      -4335
914177                 TA   =          165
16140
                                          MA   =          165
12651
                                          Ha   =            222
426  n
mi
                                          Hp   =            212
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4589419
33                 X    =         1478377
22
 Y    =      -18057604
46  feet           Y    =        -5487870
09  meter
 Z    =      -12211249
27                 Z    =        -3715000
73
 XDOT =      15630
302428                 XDOT =        4738
528669
 YDOT =      13582
863074  feet/sec       YDOT =        4193
189321  meter/sec
 ZDOT =     -14225
440213                 ZDOT =       -4312
833557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14249624
90                 X    =         4343285
67
 Y    =      -12035519
40  feet           Y    =        -3668426
31  meter
 Z    =      -12179857
15                 Z    =        -3712420
46
 XDOT =       4096
859221                 XDOT =        1248
722691
 YDOT =      19131
923565  feet/sec       YDOT =        5831
410303  meter/sec
 ZDOT =     -14126
140213                 ZDOT =       -4305
647537


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   16021
59417145  
00016717  00000-0  10270-3 0  9104
2 25544  51
6427  74
0763 0006777  42
5185 317
6492 15
54583279 22023


Satellite: ISS
Catalog Number: 25544
Epoch time:      16021
59417145   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:        74
0763  deg
Eccentricity:     
0006777     
Arg of perigee:    42
5185  deg
Mean anomaly:     317
6492  deg
Mean motion:   15
54583279  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2202
Checksum:              311


Coasting Arc #12 (Orbit 2217)
---------------------------------------

Vector Time (GMT): 2016/022/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2411454
31                 A    =         6778241
55  meter
 Y    =        4120669
01  meter          E    =           
0011553
 Z    =        4801009
51                 I    =           51
97246
 XDOT =      -4449
655883                 Wp   =           83
98597
 YDOT =      -5675
222714  meter/sec      RA   =           68
48470  deg
 ZDOT =       2631
789307                 TA   =          340
19292
                                          MA   =          340
23775
                                          Ha   =            222
616  n
mi
                                          Hp   =            211
935

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7911595
50                 X    =        -2480674
23
 Y    =       13519255
29  feet           Y    =         4093315
28  meter
 Z    =       15751343
54                 Z    =         4789127
55
 XDOT =     -14598
608541                 XDOT =       -4398
647303
 YDOT =     -18619
497092  feet/sec       YDOT =       -5724
696625  meter/sec
 ZDOT =       8634
479355                 ZDOT =        2610
298018

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14242702
44                 X    =        -4341175
70
 Y    =        6644970
47  feet           Y    =         2025387
00  meter
 Z    =       15698988
03                 Z    =         4785051
55
 XDOT =      -1113
407414                 XDOT =        -339
366580
 YDOT =     -22601
066446  feet/sec       YDOT =       -6888
805053  meter/sec
 ZDOT =       8542
378025                 ZDOT =        2603
716822


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   16022
62270266  
00016717  00000-0  10270-3 0  9111
2 25544  51
6412  68
9448 0006897  46
6119 313
5608 15
54590514 22185


Satellite: ISS
Catalog Number: 25544
Epoch time:      16022
62270266   =   yrday
fracday
Element set:     911
Inclination:       51
6412  deg
RA of node:        68
9448  deg
Eccentricity:     
0006897     
Arg of perigee:    46
6119  deg
Mean anomaly:     313
5608  deg
Mean motion:   15
54590514  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2218
Checksum:              310


Coasting Arc #13 (Orbit 2232)
---------------------------------------

Vector Time (GMT): 2016/023/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3432951
45                 A    =         6776101
36  meter
 Y    =       -2448609
92  meter          E    =           
0020577
 Z    =       -5321727
88                 I    =           51
95328
 XDOT =       3807
494815                 Wp   =           74
10366
 YDOT =       6614
317759  meter/sec      RA   =           63
50420  deg
 ZDOT =       -583
596841                 TA   =          190
31919
                                          MA   =          190
36149
                                          Ha   =            222
501  n
mi
                                          Hp   =            212
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11262964
08                 X    =         3485927
38
 Y    =       -8033497
11  feet           Y    =        -2409924
00  meter
 Z    =      -17459737
15                 Z    =        -5304923
23
 XDOT =      12491
780890                 XDOT =        3736
083706
 YDOT =      21700
517583  feet/sec       YDOT =        6656
496422  meter/sec
 ZDOT =      -1914
687799                 ZDOT =        -565
274604

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13918997
96                 X    =         4242510
58
 Y    =        -458295
10  feet           Y    =         -139688
35  meter
 Z    =      -17386354
37                 Z    =        -5299360
81
 XDOT =      -1519
107255                 XDOT =        -463
023891
 YDOT =      23985
870584  feet/sec       YDOT =        7310
893354  meter/sec
 ZDOT =      -1836
522883                 ZDOT =        -559
772175


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   16023
58693794  
00016717  00000-0  10270-3 0  9123
2 25544  51
6418  64
1347 0006796  49
1790 310
9951 15
54597399 22335


Satellite: ISS
Catalog Number: 25544
Epoch time:      16023
58693794   =   yrday
fracday
Element set:     912
Inclination:       51
6418  deg
RA of node:        64
1347  deg
Eccentricity:     
0006796     
Arg of perigee:    49
1790  deg
Mean anomaly:     310
9951  deg
Mean motion:   15
54597399  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2233
Checksum:              342


Coasting Arc #14 (Orbit 2248)
---------------------------------------

Vector Time (GMT): 2016/024/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4349108
24                 A    =         6776665
66  meter
 Y    =         623727
26  meter          E    =           
0011773
 Z    =        5152873
06                 I    =           51
93910
 XDOT =      -2841
704845                 Wp   =           53
35138
 YDOT =      -6959
762303  meter/sec      RA   =           58
51884  deg
 ZDOT =      -1546
713366                 TA   =           51
53142
                                          MA   =           51
42585
                                          Ha   =            222
661  n
mi
                                          Hp   =            211
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14268727
81                 X    =        -4380789
54
 Y    =        2046349
26  feet           Y    =          574915
43  meter
 Z    =       16905751
52                 Z    =         5131669
73
 XDOT =      -9323
178626                 XDOT =       -2756
154774
 YDOT =     -22833
865823  feet/sec       YDOT =       -6991
061766  meter/sec
 ZDOT =      -5074
518917                 ZDOT =       -1560
309656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13239717
44                 X    =        -4035465
87
 Y    =       -5966545
40  feet           Y    =        -1818603
04  meter
 Z    =       16813648
96                 Z    =         5124800
20
 XDOT =       3941
566122                 XDOT =        1201
389354
 YDOT =     -23294
886290  feet/sec       YDOT =       -7100
281341  meter/sec
 ZDOT =      -5132
110068                 ZDOT =       -1564
267149


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   16024
61544263  
00016717  00000-0  10270-3 0  9135
2 25544  51
6404  59
0024 0006919  52
8516 307
3268 15
54641214 22493


Satellite: ISS
Catalog Number: 25544
Epoch time:      16024
61544263   =   yrday
fracday
Element set:     913
Inclination:       51
6404  deg
RA of node:        59
0024  deg
Eccentricity:     
0006919     
Arg of perigee:    52
8516  deg
Mean anomaly:     307
3268  deg
Mean motion:   15
54641214  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2249
Checksum:              292


Coasting Arc #15 (Orbit 2263)
---------------------------------------

Vector Time (GMT): 2016/025/13:40:37
923
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5072165
12                 A    =         6779888
57  meter
 Y    =        1100738
40  meter          E    =           
0013870
 Z    =       -4373485
45                 I    =           51
93242
 XDOT =       1538
159126                 Wp   =           85
98976
 YDOT =       6653
312254  meter/sec      RA   =           53
53974  deg
 ZDOT =       3468
824750                 TA   =          219
07759
                                          MA   =          219
17786
                                          Ha   =            222
613  n
mi
                                          Hp   =            211
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16640961
69                 X    =         5080723
44
 Y    =        3611346
46  feet           Y    =         1157506
53  meter
 Z    =      -14348705
53                 Z    =        -4348825
93
 XDOT =       5046
453826                 XDOT =        1446
796165
 YDOT =      21828
452277  feet/sec       YDOT =        6670
002150  meter/sec
 ZDOT =      11380
658629                 ZDOT =        3476
074622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12405411
74                 X    =         3781169
50
 Y    =       11794966
50  feet           Y    =         3595105
79  meter
 Z    =      -14241955
78                 Z    =        -4340948
12
 XDOT =      -6261
005489                 XDOT =       -1908
354473
 YDOT =      20321
579669  feet/sec       YDOT =        6194
017483  meter/sec
 ZDOT =      11410
776275                 ZDOT =        3478
004609


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   16025
57965400  
00016717  00000-0  10270-3 0  9142
2 25544  51
6406  54
1921 0006949  55
5524 304
6285 15
54630673 22642


Satellite: ISS
Catalog Number: 25544
Epoch time:      16025
57965400   =   yrday
fracday
Element set:     914
Inclination:       51
6406  deg
RA of node:        54
1921  deg
Eccentricity:     
0006949     
Arg of perigee:    55
5524  deg
Mean anomaly:     304
6285  deg
Mean motion:   15
54630673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2264
Checksum:              308
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