[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: February 7th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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


040/08:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 5

042/08:58:45 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 6

042/12:24:48 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 6

043/19:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 6

048/05:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 6

052/22:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 7

Coasting Arc #1 (Orbit 1833)
---------------------------------------

Vector Time (GMT): 2018/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1935716
39                 A    =         6787233
71  meter
 Y    =       -6079270
90  meter          E    =           
0008787
 Z    =       -2312645
11                 I    =           51
34474
 XDOT =       5442
699076                 Wp   =           54
44526
 YDOT =       -309
113911  meter/sec      RA   =          304
51644  deg
 ZDOT =       5387
663486                 TA   =          279
68095
                                          MA   =          279
78020
                                          Ha   =            222
228  n
mi
                                          Hp   =            213
620

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6350775
56                 X    =         2014786
04
 Y    =      -19945114
51  feet           Y    =        -6057182
37  meter
 Z    =       -7587418
33                 Z    =        -2303049
92
 XDOT =      17856
624264                 XDOT =        5419
581078
 YDOT =      -1014
153251  feet/sec       YDOT =        -248
378975  meter/sec
 ZDOT =      17676
061307                 ZDOT =        5414
045743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18339436
67                 X    =         5589860
30
 Y    =      -10122532
88  feet           Y    =        -3085348
02  meter
 Z    =       -7543755
73                 Z    =        -2299336
75
 XDOT =      12864
517020                 XDOT =        3921
104788
 YDOT =      10094
601844  feet/sec       YDOT =        3076
834642  meter/sec
 ZDOT =      17793
512524                 ZDOT =        5423
462617


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   18038
50457807  
00016717  00000-0  10270-3 0  9003
2 25544  51
6413 305
2130 0003198  73
6773 286
4731 15
54076518 18349


Satellite: ISS
Catalog Number: 25544
Epoch time:      18038
50457807   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:       305
2130  deg
Eccentricity:     
0003198     
Arg of perigee:    73
6773  deg
Mean anomaly:     286
4731  deg
Mean motion:   15
54076518  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1834
Checksum:              306


Coasting Arc #2 (Orbit 1849)
---------------------------------------

Vector Time (GMT): 2018/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2851963
13                 A    =         6789399
53  meter
 Y    =        6118308
78  meter          E    =           
0015391
 Z    =         666632
08                 I    =           51
33386
 XDOT =      -4615
896481                 Wp   =          119
09115
 YDOT =      -1493
945761  meter/sec      RA   =          299
52426  deg
 ZDOT =      -5939
546583                 TA   =           53
67803
                                          MA   =           53
53602
                                          Ha   =            222
247  n
mi
                                          Hp   =            213
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9356834
41                 X    =        -2923405
85
 Y    =       20073191
52  feet           Y    =         6086016
72  meter
 Z    =        2187113
13                 Z    =          652604
75
 XDOT =     -15144
017325                 XDOT =       -4569
996925
 YDOT =      -4901
396855  feet/sec       YDOT =       -1545
307396  meter/sec
 ZDOT =     -19486
701389                 ZDOT =       -5961
857180

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20444625
44                 X    =        -6231521
84
 Y    =        8530761
18  feet           Y    =         2600176
01  meter
 Z    =        2123731
64                 Z    =          647313
40
 XDOT =      -7177
611758                 XDOT =       -2187
736064
 YDOT =     -12244
504752  feet/sec       YDOT =       -3732
125048  meter/sec
 ZDOT =     -19585
748687                 ZDOT =       -5969
736200


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   18039
53345236  
00016717  00000-0  10270-3 0  9010
2 25544  51
6413 300
0852 0003111  79
5421 280
6082 15
54043852 18501


Satellite: ISS
Catalog Number: 25544
Epoch time:      18039
53345236   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:       300
0852  deg
Eccentricity:     
0003111     
Arg of perigee:    79
5421  deg
Mean anomaly:     280
6082  deg
Mean motion:   15
54043852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1850
Checksum:              275


Coasting Arc #3 (Orbit 1862)
---------------------------------------

Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4453664
41                 A    =         6778281
96  meter
 Y    =        -184143
45  meter          E    =           
0016799
 Z    =       -5121553
73                 I    =           51
28226
 XDOT =       2053
598762                 Wp   =           78
47087
 YDOT =      -7215
161926  meter/sec      RA   =          295
28129  deg
 ZDOT =      -1527
352915                 TA   =          176
71953
                                          MA   =          176
70850
                                          Ha   =            222
213  n
mi
                                          Hp   =            213
460

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14611759
87                 X    =        -4426396
83
 Y    =        -604145
19  feet           Y    =         -233795
02  meter
 Z    =      -16802997
79                 Z    =        -5143121
53
 XDOT =       6737
528746                 XDOT =        2141
546991
 YDOT =     -23671
791097  feet/sec       YDOT =       -7191
705456  meter/sec
 ZDOT =      -5011
000376                 ZDOT =       -1517
163650

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1926687
76                 X    =          587254
43
 Y    =      -14384810
14  feet           Y    =        -4384490
13  meter
 Z    =      -16898945
65                 Z    =        -5150798
63
 XDOT =      21906
357141                 XDOT =        6677
057657
 YDOT =       8762
595487  feet/sec       YDOT =        2670
839104  meter/sec
 ZDOT =      -4964
536768                 ZDOT =       -1513
190807


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   18040
36940892  
00016717  00000-0  10270-3 0  9023
2 25544  51
6397 295
9164 0003117  79
5094 280
6409 15
54072086 18630


Satellite: ISS
Catalog Number: 25544
Epoch time:      18040
36940892   =   yrday
fracday
Element set:     902
Inclination:       51
6397  deg
RA of node:       295
9164  deg
Eccentricity:     
0003117     
Arg of perigee:    79
5094  deg
Mean anomaly:     280
6409  deg
Mean motion:   15
54072086  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1863
Checksum:              327


Coasting Arc #4 (Orbit 1878)
---------------------------------------

Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3820633
53                 A    =         6777513
19  meter
 Y    =        1864620
71  meter          E    =           
0005744
 Z    =        5273533
64                 I    =           51
26678
 XDOT =      -2934
310276                 Wp   =           76
70467
 YDOT =       7079
936782  meter/sec      RA   =          290
25768  deg
 ZDOT =       -375
800440                 TA   =           16
90455
                                          MA   =           16
88542
                                          Ha   =            222
060  n
mi
                                          Hp   =            213
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12534886
92                 X    =         3773883
28
 Y    =        6117522
00  feet           Y    =         1907084
33  meter
 Z    =       17301619
57                 Z    =         5291979
07
 XDOT =      -9627
002217                 XDOT =       -3011
436552
 YDOT =      23228
139047  feet/sec       YDOT =        7046
692066  meter/sec
 ZDOT =      -1232
941076                 ZDOT =        -390
241482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7022980
14                 X    =        -2140604
35
 Y    =       11932648
08  feet           Y    =         3637071
13  meter
 Z    =       17383416
38                 Z    =         5298465
31
 XDOT =     -21580
807013                 XDOT =       -6577
829978
 YDOT =     -10802
250599  feet/sec       YDOT =       -3292
525983  meter/sec
 ZDOT =      -1298
291065                 ZDOT =        -395
719117


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   18041
39827660  
00016717  00000-0  10270-3 0  9035
2 25544  51
6397 290
7888 0003128  80
7539 279
3967 15
54087921 18791


Satellite: ISS
Catalog Number: 25544
Epoch time:      18041
39827660   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       290
7888  deg
Eccentricity:     
0003128     
Arg of perigee:    80
7539  deg
Mean anomaly:     279
3967  deg
Mean motion:   15
54087921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1879
Checksum:              360


Coasting Arc #5 (Orbit 1893)
---------------------------------------

Vector Time (GMT): 2018/042/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3133570
00                 A    =         6779197
84  meter
 Y    =       -3487115
60  meter          E    =           
0015194
 Z    =       -4910796
51                 I    =           51
26141
 XDOT =       3596
791885                 Wp   =          101
98946
 YDOT =      -6378
219918  meter/sec      RA   =          285
23363  deg
 ZDOT =       2236
809245                 TA   =          189
99135
                                          MA   =          190
02159
                                          Ha   =            222
221  n
mi
                                          Hp   =            213
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10280741
46                 X    =        -3070489
64
 Y    =      -11440667
96  feet           Y    =        -3521804
69  meter
 Z    =      -16111537
12                 Z    =        -4925864
75
 XDOT =      11800
498312                 XDOT =        3656
982520
 YDOT =     -20925
918367  feet/sec       YDOT =       -6337
661544  meter/sec
 ZDOT =       7338
613009                 ZDOT =        2254
427153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12003096
86                 X    =         3658543
92
 Y    =       -9505788
57  feet           Y    =        -2897364
36  meter
 Z    =      -16178065
58                 Z    =        -4931074
39
 XDOT =      19528
557568                 XDOT =        5952
304347
 YDOT =      12049
744129  feet/sec       YDOT =        3672
762011  meter/sec
 ZDOT =       7417
980329                 ZDOT =        2261
000404


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   18042
36283944  
00016717  00000-0  10270-3 0  9045
2 25544  51
6393 285
9809 0003152  85
0655 275
0858 15
54077546 18941


Satellite: ISS
Catalog Number: 25544
Epoch time:      18042
36283944   =   yrday
fracday
Element set:     904
Inclination:       51
6393  deg
RA of node:       285
9809  deg
Eccentricity:     
0003152     
Arg of perigee:    85
0655  deg
Mean anomaly:     275
0858  deg
Mean motion:   15
54077546  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1894
Checksum:              340


Coasting Arc #6 (Orbit 1894)
---------------------------------------

Vector Time (GMT): 2018/042/08:58:45
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4450781
68                 A    =         6779829
92  meter
 Y    =       -1962295
48  meter          E    =           
0010402
 Z    =        4715859
25                 I    =           51
26413
 XDOT =        297
687801                 Wp   =          108
96630
 YDOT =       7177
276614  meter/sec      RA   =          285
15541  deg
 ZDOT =       2697
336070                 TA   =          314
20530
                                          MA   =          314
29070
                                          Ha   =            222
014  n
mi
                                          Hp   =            213
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14602302
10                 X    =         4449487
10
 Y    =       -6437977
28  feet           Y    =        -1912530
95  meter
 Z    =       15471979
18                 Z    =         4737476
07
 XDOT =        976
666014                 XDOT =         204
305450
 YDOT =      23547
495452  feet/sec       YDOT =        7180
083470  meter/sec
 ZDOT =       8849
527790                 ZDOT =        2698
555195

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7723000
84                 X    =         2353970
66
 Y    =       13857661
66  feet           Y    =         4223815
27  meter
 Z    =       15568474
20                 Z    =         4745270
94
 XDOT =     -22357
861557                 XDOT =       -6814
676203
 YDOT =       2483
219501  feet/sec       YDOT =         756
885304  meter/sec
 ZDOT =       8853
867584                 ZDOT =        2698
658840


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   18042
42714253  
00016717  00000-0  10270-3 0  9055
2 25544  51
6397 285
6610 0003053  86
9527 273
1975 15
54105122 18952


Satellite: ISS
Catalog Number: 25544
Epoch time:      18042
42714253   =   yrday
fracday
Element set:     905
Inclination:       51
6397  deg
RA of node:       285
6610  deg
Eccentricity:     
0003053     
Arg of perigee:    86
9527  deg
Mean anomaly:     273
1975  deg
Mean motion:   15
54105122  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1895
Checksum:              311


Coasting Arc #7 (Orbit 1896)
---------------------------------------

Vector Time (GMT): 2018/042/12:24:48
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1016853
54                 A    =         6785396
11  meter
 Y    =        5954633
78  meter          E    =           
0016107
 Z    =        3075222
82                 I    =           51
28275
 XDOT =      -4889
194041                 Wp   =           93
20633
 YDOT =       3358
816153  meter/sec      RA   =          284
39454  deg
 ZDOT =      -4865
882361                 TA   =           51
24122
                                          MA   =           51
09741
                                          Ha   =            222
167  n
mi
                                          Hp   =            213
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3336133
66                 X    =          935254
13
 Y    =       19536200
07  feet           Y    =         5965548
73  meter
 Z    =       10089313
72                 Z    =         3079963
97
 XDOT =     -16040
662865                 XDOT =       -4902
754443
 YDOT =      11019
738036  feet/sec       YDOT =        3304
065936  meter/sec
 ZDOT =     -15964
180975                 ZDOT =       -4889
664879

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7946808
96                 X    =        -2422187
37
 Y    =       18144781
71  feet           Y    =         5530529
47  meter
 Z    =       10109514
14                 Z    =         3081379
91
 XDOT =     -18043
589677                 XDOT =       -5499
686133
 YDOT =       1090
044087  feet/sec       YDOT =         332
245438  meter/sec
 ZDOT =     -16070
524113                 ZDOT =       -4898
295750


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   18042
55575086  
00016717  00000-0  10270-3 0  9069
2 25544  51
6412 285
0209 0003140  84
1101 276
0409 15
54096686 18973


Satellite: ISS
Catalog Number: 25544
Epoch time:      18042
55575086   =   yrday
fracday
Element set:     906
Inclination:       51
6412  deg
RA of node:       285
0209  deg
Eccentricity:     
0003140     
Arg of perigee:    84
1101  deg
Mean anomaly:     276
0409  deg
Mean motion:   15
54096686  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1897
Checksum:              306


Coasting Arc #8 (Orbit 1911)
---------------------------------------

Vector Time (GMT): 2018/043/12:24:48
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -191060
22                 A    =         6788388
09  meter
 Y    =       -6596842
87  meter          E    =           
0010225
 Z    =       -1578447
04                 I    =           51
28552
 XDOT =       4888
294087                 Wp   =           50
32753
 YDOT =      -1500
629184  meter/sec      RA   =          279
39380  deg
 ZDOT =       5711
080938                 TA   =          292
32795
                                          MA   =          292
43630
                                          Ha   =            222
136  n
mi
                                          Hp   =            213
634

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -626838
00                 X    =         -109611
25
 Y    =      -21643185
27  feet           Y    =        -6598524
06  meter
 Z    =       -5178632
01                 Z    =        -1579177
16
 XDOT =      16037
710258                 XDOT =        4876
970429
 YDOT =      -4923
324096  feet/sec       YDOT =       -1446
028118  meter/sec
 ZDOT =      18737
142185                 ZDOT =        5734
798569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11020991
76                 X    =         3359198
29
 Y    =      -18636915
39  feet           Y    =        -5680531
81  meter
 Z    =       -5180902
39                 Z    =        -1579139
05
 XDOT =      14732
323457                 XDOT =        4490
412190
 YDOT =       3502
237421  feet/sec       YDOT =        1067
481966  meter/sec
 ZDOT =      18842
915910                 ZDOT =        5743
320769


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   18043
52031029  
00016717  00000-0  10270-3 0  9072
2 25544  51
6412 280
2128 0002959  87
0254 273
1237 15
54086717 19127


Satellite: ISS
Catalog Number: 25544
Epoch time:      18043
52031029   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       280
2128  deg
Eccentricity:     
0002959     
Arg of perigee:    87
0254  deg
Mean anomaly:     273
1237  deg
Mean motion:   15
54086717  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1912
Checksum:              293


Coasting Arc #9 (Orbit 1916)
---------------------------------------

Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3608113
87                 A    =         6779007
04  meter
 Y    =        2889377
16  meter          E    =           
0008819
 Z    =        4952292
30                 I    =           51
25140
 XDOT =      -2653
760503                 Wp   =           71
11091
 YDOT =       6892
233187  meter/sec      RA   =          277
98329  deg
 ZDOT =      -2081
901954                 TA   =           39
27922
                                          MA   =           39
21527
                                          Ha   =            222
158  n
mi
                                          Hp   =            213
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11837643
92                 X    =         3551480
84
 Y    =        9479583
87  feet           Y    =         2929409
03  meter
 Z    =       16247678
15                 Z    =         4969681
24
 XDOT =      -8706
563331                 XDOT =       -2720
521541
 YDOT =      22612
313606  feet/sec       YDOT =        6862
183682  meter/sec
 ZDOT =      -6830
386989                 ZDOT =       -2094
955017

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13066852
35                 X    =         3982776
60
 Y    =       -7532788
76  feet           Y    =        -2295994
01  meter
 Z    =       16324638
81                 Z    =         4975749
91
 XDOT =      17431
022482                 XDOT =        5312
975653
 YDOT =      15264
980594  feet/sec       YDOT =        4652
766085  meter/sec
 ZDOT =      -6889
495501                 ZDOT =       -2099
918229


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   18043
84183171  
00016717  00000-0  10270-3 0  9084
2 25544  51
6402 278
6047 0003234  99
2397 260
9122 15
54059746 19171


Satellite: ISS
Catalog Number: 25544
Epoch time:      18043
84183171   =   yrday
fracday
Element set:     908
Inclination:       51
6402  deg
RA of node:       278
6047  deg
Eccentricity:     
0003234     
Arg of perigee:    99
2397  deg
Mean anomaly:     260
9122  deg
Mean motion:   15
54059746  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1917
Checksum:              319


Coasting Arc #10 (Orbit 1931)
---------------------------------------

Vector Time (GMT): 2018/044/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3089479
61                 A    =         6782171
12  meter
 Y    =       -4414494
60  meter          E    =           
0010742
 Z    =       -4130025
62                 I    =           51
25841
 XDOT =       3305
892448                 Wp   =          107
14687
 YDOT =      -5808
247755  meter/sec      RA   =          272
96517  deg
 ZDOT =       3740
308163                 TA   =          201
59675
                                          MA   =          201
64209
                                          Ha   =            222
184  n
mi
                                          Hp   =            213
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10136087
96                 X    =        -3019824
94
 Y    =      -14483249
99  feet           Y    =        -4448653
97  meter
 Z    =      -13549952
83                 Z    =        -4144863
53
 XDOT =      10846
103832                 XDOT =        3352
428157
 YDOT =     -19055
930956  feet/sec       YDOT =       -5771
018662  meter/sec
 ZDOT =      12271
352242                 ZDOT =        3756
479878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17055131
77                 X    =        -5198404
16
 Y    =        4455418
33  feet           Y    =         1358011
51  meter
 Z    =      -13615350
11                 Z    =        -4149958
71
 XDOT =     -13868
556400                 XDOT =       -4227
135991
 YDOT =     -15415
253950  feet/sec       YDOT =       -4698
569404  meter/sec
 ZDOT =      12344
166340                 ZDOT =        3762
501900


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   18044
80638712  
00016717  00000-0  10270-3 0  9098
2 25544  51
6399 273
7977 0003119 101
8330 258
3173 15
54083504 19326


Satellite: ISS
Catalog Number: 25544
Epoch time:      18044
80638712   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       273
7977  deg
Eccentricity:     
0003119     
Arg of perigee:   101
8330  deg
Mean anomaly:     258
3173  deg
Mean motion:   15
54083504  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1932
Checksum:              318


Coasting Arc #11 (Orbit 1947)
---------------------------------------

Vector Time (GMT): 2018/045/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2486686
13                 A    =         6786009
01  meter
 Y    =        5625727
48  meter          E    =           
0016518
 Z    =        2848360
95                 I    =           51
26968
 XDOT =      -3891
147723                 Wp   =          100
67366
 YDOT =       4282
392280  meter/sec      RA   =          267
95592  deg
 ZDOT =      -5039
047424                 TA   =           46
73316
                                          MA   =           46
59546
                                          Ha   =            222
179  n
mi
                                          Hp   =            213
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8158419
08                 X    =         2409757
44
 Y    =       18457111
15  feet           Y    =         5653105
33  meter
 Z    =        9345016
23                 Z    =         2860252
95
 XDOT =     -12766
232686                 XDOT =       -3914
268994
 YDOT =      14049
843439  feet/sec       YDOT =        4238
749249  meter/sec
 ZDOT =     -16532
307823                 ZDOT =       -5058
005163

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20091637
28                 X    =         6123931
04
 Y    =       -1604320
50  feet           Y    =         -488996
89  meter
 Z    =        9397145
79                 Z    =         2864250
04
 XDOT =       9010
959850                 XDOT =        2746
540562
 YDOT =      15095
033487  feet/sec       YDOT =        4600
966207  meter/sec
 ZDOT =     -16617
290807                 ZDOT =       -5064
950238


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   18045
83524620  
00016717  00000-0  10270-3 0  9106
2 25544  51
6392 268
6691 0003217 107
3962 252
7542 15
54074388 19481


Satellite: ISS
Catalog Number: 25544
Epoch time:      18045
83524620   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:       268
6691  deg
Eccentricity:     
0003217     
Arg of perigee:   107
3962  deg
Mean anomaly:     252
7542  deg
Mean motion:   15
54074388  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1948
Checksum:              321


Coasting Arc #12 (Orbit 1962)
---------------------------------------

Vector Time (GMT): 2018/046/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1849542
83                 A    =         6788722
30  meter
 Y    =       -6396190
42  meter          E    =           
0010341
 Z    =       -1311298
75                 I    =           51
28213
 XDOT =       4379
440718                 Wp   =           54
04974
 YDOT =      -2446
808726  meter/sec      RA   =          262
95610  deg
 ZDOT =       5795
998424                 TA   =          291
61124
                                          MA   =          291
72138
                                          Ha   =            222
165  n
mi
                                          Hp   =            213
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6068053
90                 X    =        -1771512
00
 Y    =      -20984876
72  feet           Y    =        -6416437
08  meter
 Z    =       -4302161
27                 Z    =        -1320093
00
 XDOT =      14368
243826                 XDOT =        4378
322922
 YDOT =      -8027
587685  feet/sec       YDOT =       -2397
840657  meter/sec
 ZDOT =      19015
742862                 ZDOT =        5817
269141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21822666
22                 X    =        -6651548
66
 Y    =        -791807
31  feet           Y    =         -241342
87  meter
 Z    =       -4340414
83                 Z    =        -1322958
44
 XDOT =      -3252
369623                 XDOT =        -991
322261
 YDOT =     -14441
769928  feet/sec       YDOT =       -4401
851474  meter/sec
 ZDOT =      19110
755865                 ZDOT =        5824
958388


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   18046
79979810  
00016717  00000-0  10270-3 0  9118
2 25544  51
6403 263
8613 0003104 106
8308 253
3185 15
54080142 19630


Satellite: ISS
Catalog Number: 25544
Epoch time:      18046
79979810   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:       263
8613  deg
Eccentricity:     
0003104     
Arg of perigee:   106
8308  deg
Mean anomaly:     253
3185  deg
Mean motion:   15
54080142  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1963
Checksum:              302


Coasting Arc #13 (Orbit 1978)
---------------------------------------

Vector Time (GMT): 2018/047/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1090733
78                 A    =         6789354
90  meter
 Y    =        6682739
82  meter          E    =           
0014176
 Z    =        -408090
85                 I    =           51
28874
 XDOT =      -4798
583553                 Wp   =          132
17003
 YDOT =        427
556232  meter/sec      RA   =          257
96143  deg
 ZDOT =      -5966
789812                 TA   =           52
25171
                                          MA   =           52
12335
                                          Ha   =            222
149  n
mi
                                          Hp   =            213
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3578522
88                 X    =         1017906
75
 Y    =       21924999
40  feet           Y    =         6694529
92  meter
 Z    =       -1338880
73                 Z    =         -402970
02
 XDOT =     -15743
384359                 XDOT =       -4774
025134
 YDOT =       1402
743544  feet/sec       YDOT =         374
031980  meter/sec
 ZDOT =     -19576
082061                 ZDOT =       -5990
039499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22007919
12                 X    =         6708013
75
 Y    =        3036617
03  feet           Y    =          925560
87  meter
 Z    =       -1316996
47                 Z    =         -401420
52
 XDOT =      -3043
348853                 XDOT =        -927
612731
 YDOT =      13728
075527  feet/sec       YDOT =        4184
317421  meter/sec
 ZDOT =     -19679
625005                 ZDOT =       -5998
349701


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   18047
82865120  
00016717  00000-0  10270-3 0  9122
2 25544  51
6396 258
7324 0003170 111
6372 248
5118 15
54096035 19798


Satellite: ISS
Catalog Number: 25544
Epoch time:      18047
82865120   =   yrday
fracday
Element set:     912
Inclination:       51
6396  deg
RA of node:       258
7324  deg
Eccentricity:     
0003170     
Arg of perigee:   111
6372  deg
Mean anomaly:     248
5118  deg
Mean motion:   15
54096035  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1979
Checksum:              314


Coasting Arc #14 (Orbit 1985)
---------------------------------------

Vector Time (GMT): 2018/048/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4191357
67                 A    =         6782584
58  meter
 Y    =        3541894
79  meter          E    =           
0013697
 Z    =        3975637
02                 I    =           51
26771
 XDOT =      -1638
831294                 Wp   =           83
77035
 YDOT =       6376
962283  meter/sec      RA   =          255
72718  deg
 ZDOT =      -3940
293499                 TA   =           47
45692
                                          MA   =           47
34136
                                          Ha   =            222
019  n
mi
                                          Hp   =            213
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13751173
46                 X    =         4132128
63
 Y    =       11620389
75  feet           Y    =         3588434
63  meter
 Z    =       13043428
54                 Z    =         3995852
54
 XDOT =      -5376
743092                 XDOT =       -1690
878978
 YDOT =      20921
792267  feet/sec       YDOT =        6358
344370  meter/sec
 ZDOT =     -12927
472108                 ZDOT =       -3948
381185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17576311
04                 X    =        -5357259
61
 Y    =        3585893
55  feet           Y    =         1092980
35  meter
 Z    =       13132932
47                 Z    =         4002917
82
 XDOT =     -12940
147848                 XDOT =       -3944
157064
 YDOT =     -15788
560017  feet/sec       YDOT =       -4812
353093  meter/sec
 ZDOT =     -12964
330220                 ZDOT =       -3951
527851


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   18048
27877403  
00016717  00000-0  10270-3 0  9130
2 25544  51
6379 256
4914 0003022 101
5998 258
5494 15
54108334 19869


Satellite: ISS
Catalog Number: 25544
Epoch time:      18048
27877403   =   yrday
fracday
Element set:     913
Inclination:       51
6379  deg
RA of node:       256
4914  deg
Eccentricity:     
0003022     
Arg of perigee:   101
5998  deg
Mean anomaly:     258
5494  deg
Mean motion:   15
54108334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1986
Checksum:              333


Coasting Arc #15 (Orbit 2000)
---------------------------------------

Vector Time (GMT): 2018/049/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3962510
22                 A    =         6786318
97  meter
 Y    =       -4813217
02  meter          E    =           
0007163
 Z    =       -2683869
32                 I    =           51
28882
 XDOT =       2620
622894                 Wp   =           75
04058
 YDOT =      -5025
374550  meter/sec      RA   =          250
72018  deg
 ZDOT =       5156
689960                 TA   =          254
51306
                                          MA   =          254
59217
                                          Ha   =            222
096  n
mi
                                          Hp   =            213
612

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13000361
62                 X    =        -3895356
46
 Y    =      -15791394
44  feet           Y    =        -4857153
33  meter
 Z    =       -8805345
53                 Z    =        -2702953
85
 XDOT =       8597
844141                 XDOT =        2651
575230
 YDOT =     -16487
449311  feet/sec       YDOT =       -4995
895360  meter/sec
 ZDOT =      16918
274148                 ZDOT =        5169
495470

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20402284
40                 X    =         6218616
28
 Y    =        -795231
27  feet           Y    =         -242386
49  meter
 Z    =       -8889659
66                 Z    =        -2709568
26
 XDOT =       7971
247387                 XDOT =        2429
636204
 YDOT =      15225
583627  feet/sec       YDOT =        4640
757889  meter/sec
 ZDOT =      16975
938214                 ZDOT =        5174
265968


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   18049
24332187  
00016717  00000-0  10270-3 0  9144
2 25544  51
6376 251
6835 0002981 106
2232 253
9249 15
54092151 20016


Satellite: ISS
Catalog Number: 25544
Epoch time:      18049
24332187   =   yrday
fracday
Element set:     914
Inclination:       51
6376  deg
RA of node:       251
6835  deg
Eccentricity:     
0002981     
Arg of perigee:   106
2232  deg
Mean anomaly:     253
9249  deg
Mean motion:   15
54092151  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2001
Checksum:              294


Coasting Arc #16 (Orbit 2016)
---------------------------------------

Vector Time (GMT): 2018/050/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3513037
27                 A    =         6788906
60  meter
 Y    =        5700465
30  meter          E    =           
0016535
 Z    =        1072083
01                 I    =           51
31076
 XDOT =      -3636
830818                 Wp   =          120
86931
 YDOT =       3354
850948  meter/sec      RA   =          245
72243  deg
 ZDOT =      -5862
046875                 TA   =           47
44503
                                          MA   =           47
30557
                                          Ha   =            222
066  n
mi
                                          Hp   =            213
653

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11525712
84                 X    =         3443824
50
 Y    =       18702313
99  feet           Y    =         5739363
62  meter
 Z    =        3517332
70                 Z    =         1088979
16
 XDOT =     -11931
859640                 XDOT =       -3645
601087
 YDOT =      11006
728832  feet/sec       YDOT =        3314
131758  meter/sec
 ZDOT =     -19232
437255                 ZDOT =       -5879
734710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21888066
48                 X    =        -6671482
66
 Y    =       -1732546
85  feet           Y    =         -528080
28  meter
 Z    =        3591804
77                 Z    =         1094782
09
 XDOT =      -2058
182299                 XDOT =        -627
333965
 YDOT =     -14426
810860  feet/sec       YDOT =       -4397
291950  meter/sec
 ZDOT =     -19311
608182                 ZDOT =       -5886
178174


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   18050
27217021  
00016717  00000-0  10270-3 0  9159
2 25544  51
6390 246
5541 0002966 109
6934 250
4539 15
54100435 20174


Satellite: ISS
Catalog Number: 25544
Epoch time:      18050
27217021   =   yrday
fracday
Element set:     915
Inclination:       51
6390  deg
RA of node:       246
5541  deg
Eccentricity:     
0002966     
Arg of perigee:   109
6934  deg
Mean anomaly:     250
4539  deg
Mean motion:   15
54100435  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2017
Checksum:              287


Coasting Arc #17 (Orbit 2032)
---------------------------------------

Vector Time (GMT): 2018/051/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2869793
32                 A    =         6789262
59  meter
 Y    =       -6116335
18  meter          E    =           
0014802
 Z    =         608487
98                 I    =           51
32610
 XDOT =       4587
346623                 Wp   =           61
50002
 YDOT =      -1550
489595  meter/sec      RA   =          240
73004  deg
 ZDOT =       5946
668762                 TA   =          305
09764
                                          MA   =          305
23633
                                          Ha   =            222
070  n
mi
                                          Hp   =            213
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9415332
41                 X    =        -2804141
19
 Y    =      -20066716
47  feet           Y    =        -6148060
04  meter
 Z    =        1996351
65                 Z    =          594707
76
 XDOT =      15050
349813                 XDOT =        4575
458239
 YDOT =      -5086
908119  feet/sec       YDOT =       -1499
256605  meter/sec
 ZDOT =      19510
068117                 ZDOT =        5968
923515

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21836629
72                 X    =         6655804
74
 Y    =        3836839
64  feet           Y    =         1169468
72  meter
 Z    =        1935788
79                 Z    =          590028
42
 XDOT =      -4147
935394                 XDOT =       -1264
290708
 YDOT =      13537
143883  feet/sec       YDOT =        4126
121455  meter/sec
 ZDOT =      19609
335708                 ZDOT =        5976
925524


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   18051
30101547  
00016717  00000-0  10270-3 0  9160
2 25544  51
6388 241
4254 0002960 111
1901 248
9568 15
54101510 20339


Satellite: ISS
Catalog Number: 25544
Epoch time:      18051
30101547   =   yrday
fracday
Element set:     916
Inclination:       51
6388  deg
RA of node:       241
4254  deg
Eccentricity:     
0002960     
Arg of perigee:   111
1901  deg
Mean anomaly:     248
9568  deg
Mean motion:   15
54101510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2033
Checksum:              273


Coasting Arc #18 (Orbit 2047)
---------------------------------------

Vector Time (GMT): 2018/052/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1948340
05                 A    =         6787211
22  meter
 Y    =        6089780
01  meter          E    =           
0008767
 Z    =       -2272613
40                 I    =           51
33729
 XDOT =      -5424
170426                 Wp   =          129
69927
 YDOT =       -275
870462  meter/sec      RA   =          235
73692  deg
 ZDOT =      -5408
880370                 TA   =           75
69925
                                          MA   =           75
60192
                                          Ha   =            222
038  n
mi
                                          Hp   =            213
715

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6392191
77                 X    =         1891136
74
 Y    =       19979593
20  feet           Y    =         6111247
63  meter
 Z    =       -7456080
69                 Z    =        -2263288
61
 XDOT =     -17795
834731                 XDOT =       -5394
409181
 YDOT =       -905
086817  feet/sec       YDOT =        -336
361345  meter/sec
 ZDOT =     -17745
670504                 ZDOT =       -5435
156558

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20150268
86                 X    =        -6141801
95
 Y    =       -5883609
42  feet           Y    =        -1793324
15  meter
 Z    =       -7415335
76                 Z    =        -2260194
34
 XDOT =      10244
241357                 XDOT =        3122
444766
 YDOT =     -12652
510841  feet/sec       YDOT =       -3856
485304  meter/sec
 ZDOT =     -17862
614254                 ZDOT =       -5444
524825


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   18052
26555600  
00016717  00000-0  10270-3 0  9170
2 25544  51
6398 236
6175 0002931 115
5719 244
5737 15
54110598 20483


Satellite: ISS
Catalog Number: 25544
Epoch time:      18052
26555600   =   yrday
fracday
Element set:     917
Inclination:       51
6398  deg
RA of node:       236
6175  deg
Eccentricity:     
0002931     
Arg of perigee:   115
5719  deg
Mean anomaly:     244
5737  deg
Mean motion:   15
54110598  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2048
Checksum:              317


Coasting Arc #19 (Orbit 2058)
---------------------------------------

Vector Time (GMT): 2018/052/22:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -115018
60                 A    =         6781874
20  meter
 Y    =        5331602
85  meter          E    =           
0010174
 Z    =       -4199317
86                 I    =           51
33253
 XDOT =      -6028
204023                 Wp   =           84
06134
 YDOT =      -3000
522844  meter/sec      RA   =          232
17626  deg
 ZDOT =      -3651
075060                 TA   =          148
34510
                                          MA   =          148
28388
                                          Ha   =            222
038  n
mi
                                          Hp   =            213
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -377357
60                 X    =         -154231
57
 Y    =       17492135
32  feet           Y    =         5330097
04  meter
 Z    =      -13777289
57                 Z    =        -4199972
24
 XDOT =     -19777
572255                 XDOT =       -5976
468481
 YDOT =      -9844
235053  feet/sec       YDOT =       -3067
645381  meter/sec
 ZDOT =     -11978
592717                 ZDOT =       -3680
231854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13001714
47                 X    =         3962922
57
 Y    =      -11703587
00  feet           Y    =        -3567253
32  meter
 Z    =      -13780869
98                 Z    =        -4200409
17
 XDOT =       5354
682382                 XDOT =        1632
107190
 YDOT =      20180
149311  feet/sec       YDOT =        6150
909510  meter/sec
 ZDOT =     -12108
027148                 ZDOT =       -3690
526675


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   18052
97288324  
00016717  00000-0  10270-3 0  9185
2 25544  51
6392 233
0911 0003105 120
5317 239
6142 15
54123424 20599


Satellite: ISS
Catalog Number: 25544
Epoch time:      18052
97288324   =   yrday
fracday
Element set:     918
Inclination:       51
6392  deg
RA of node:       233
0911  deg
Eccentricity:     
0003105     
Arg of perigee:   120
5317  deg
Mean anomaly:     239
6142  deg
Mean motion:   15
54123424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2059
Checksum:              288
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