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

 
Date: August 15th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15438 0847 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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


227/05:57:52 433 -0 9 1 8 1 8
N/A 0 8 0 0 224 2
000/00:09:44 866 1 4 -0 1 222 4

227/08:59:52 374 -0 6 1 8 1 8
N/A 1 2 0 0 225 5
000/00:09:44 748 1 3 -0 0 223 5

227/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 6
000/00:00:00 000 0 0 0 0 223 7

234/03:38:33 000 0 0 0 0 0 0
N/A 0 0 0 0 226 8
000/00:00:00 000 0 0 0 0 222 3

235/16:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 9
000/00:00:00 000 0 0 0 0 222 2

236/05:30:59 000 0 0 0 0 0 0
N/A 0 0 0 0 227 1
000/00:00:00 000 0 0 0 0 221 9

239/14:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 6
000/00:00:00 000 0 0 0 0 221 5

Coasting Arc #1 (Orbit 2429)
---------------------------------------

Vector Time (GMT): 2019/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937553
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4496317
82                 A    =         6790256
58  meter
 Y    =       -2610755
01  meter          E    =           
0003673
 Z    =        4366094
17                 I    =           52
00130
 XDOT =        557
072066                 Wp   =           55
84043
 YDOT =      -6799
891592  meter/sec      RA   =           71
14051  deg
 ZDOT =      -3488
285937                 TA   =           69
46709
                                          MA   =           69
42767
                                          Ha   =            223
895  n
mi
                                          Hp   =            221
810

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14751698
89                 X    =        -4487997
00
 Y    =       -8565469
18  feet           Y    =        -2660989
61  meter
 Z    =       14324455
95                 Z    =         4344273
39
 XDOT =       1827
664258                 XDOT =         650
012766
 YDOT =     -22309
355616  feet/sec       YDOT =       -6793
142244  meter/sec
 ZDOT =     -11444
507666                 ZDOT =       -3485
354440

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6352957
93                 X    =         1936381
58
 Y    =       15920097
71  feet           Y    =         4852445
78  meter
 Z    =       14225341
30                 Z    =         4335884
03
 XDOT =     -14152
050856                 XDOT =       -4313
545101
 YDOT =      15873
216749  feet/sec       YDOT =        4838
156465  meter/sec
 ZDOT =     -11430
529171                 ZDOT =       -3484
025291


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   19226
54198608  
00016717  00000-0  10270-3 0  9008
2 25544  51
6416  71
7524 0006223 261
3850  98
6597 15
51081975 24304


Satellite: ISS
Catalog Number: 25544
Epoch time:      19226
54198608   =   yrday
fracday
Element set:     900
Inclination:       51
6416  deg
RA of node:        71
7524  deg
Eccentricity:     
0006223     
Arg of perigee:   261
3850  deg
Mean anomaly:      98
6597  deg
Mean motion:   15
51081975  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2430
Checksum:              316


Coasting Arc #2 (Orbit 2441)
---------------------------------------

Vector Time (GMT): 2019/227/06:02:44
866
Vector Time (MET): N/A
Weight (LBS)     : 937363
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2150771
77                 A    =         6799161
18  meter
 Y    =        6414894
86  meter          E    =           
0009678
 Z    =         605453
87                 I    =           52
01794
 XDOT =      -4661
055058                 Wp   =           23
95140
 YDOT =        993
942076  meter/sec      RA   =           67
45834  deg
 ZDOT =       6001
663995                 TA   =          342
54154
                                          MA   =          342
57479
                                          Ha   =            224
247  n
mi
                                          Hp   =            222
442

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7056337
81                 X    =         2075937
83
 Y    =       21046242
97  feet           Y    =         6438527
87  meter
 Z    =        1986397
21                 Z    =          615719
62
 XDOT =     -15292
175386                 XDOT =       -4700
975249
 YDOT =       3260
964817  feet/sec       YDOT =         941
595569  meter/sec
 ZDOT =      19690
498672                 ZDOT =        5978
925932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21066422
99                 X    =         6421045
73
 Y    =        6982594
33  feet           Y    =         2128294
75  meter
 Z    =        2032540
11                 Z    =          619518
22
 XDOT =      -6128
254909                 XDOT =       -1867
892096
 YDOT =      12764
132717  feet/sec       YDOT =        3890
507652  meter/sec
 ZDOT =      19586
872224                 ZDOT =        5970
078654


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   19227
31515998  
00016717  00000-0  10270-3 0  9010
2 25544  51
6409  67
9166 0006349 276
6704  83
3724 15
50697373 24421


Satellite: ISS
Catalog Number: 25544
Epoch time:      19227
31515998   =   yrday
fracday
Element set:     901
Inclination:       51
6409  deg
RA of node:        67
9166  deg
Eccentricity:     
0006349     
Arg of perigee:   276
6704  deg
Mean anomaly:      83
3724  deg
Mean motion:   15
50697373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2442
Checksum:              335


Coasting Arc #3 (Orbit 2442)
---------------------------------------

Vector Time (GMT): 2019/227/09:04:44
748
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3150901
30                 A    =         6800110
13  meter
 Y    =        5977842
19  meter          E    =           
0010160
 Z    =        -696658
82                 I    =           52
01844
 XDOT =      -3906
880348                 Wp   =          358
62017
 YDOT =       2756
381591  meter/sec      RA   =           66
82336  deg
 ZDOT =       5989
490695                 TA   =          353
90403
                                          MA   =          353
91639
                                          Ha   =            225
479  n
mi
                                          Hp   =            223
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10337602
68                 X    =         3087205
07
 Y    =       19612343
14  feet           Y    =         6012721
65  meter
 Z    =       -2285626
05                 Z    =         -681507
90
 XDOT =     -12817
848912                 XDOT =       -3966
505569
 YDOT =       9043
246691  feet/sec       YDOT =        2712
358633  meter/sec
 ZDOT =      19650
560022                 ZDOT =        5970
368207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17801189
80                 X    =         5425802
65
 Y    =      -13226329
32  feet           Y    =        -4031385
18  meter
 Z    =       -2217199
51                 Z    =         -675802
41
 XDOT =       9951
506536                 XDOT =        3033
219192
 YDOT =      10118
716289  feet/sec       YDOT =        3084
184725  meter/sec
 ZDOT =      19563
231199                 ZDOT =        5962
872869


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   19227
37960322  
00016717  00000-0  10270-3 0  9022
2 25544  51
6431  67
5982 0007375 286
5776  73
4565 15
50361002 24438


Satellite: ISS
Catalog Number: 25544
Epoch time:      19227
37960322   =   yrday
fracday
Element set:     902
Inclination:       51
6431  deg
RA of node:        67
5982  deg
Eccentricity:     
0007375     
Arg of perigee:   286
5776  deg
Mean anomaly:      73
4565  deg
Mean motion:   15
50361002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2443
Checksum:              314


Coasting Arc #4 (Orbit 2444)
---------------------------------------

Vector Time (GMT): 2019/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4676310
09                 A    =         6793798
79  meter
 Y    =        2928482
94  meter          E    =           
0000829
 Z    =       -3962958
37                 I    =           51
99265
 XDOT =       -612
394750                 Wp   =          284
53730
 YDOT =       6468
779048  meter/sec      RA   =           66
20203  deg
 ZDOT =       4057
059136                 TA   =           27
69956
                                          MA   =           27
69515
                                          Ha   =            225
576  n
mi
                                          Hp   =            223
665

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15342224
70                 X    =         4662464
80
 Y    =        9607883
66  feet           Y    =         2980699
36  meter
 Z    =      -13001831
92                 Z    =        -3940276
73
 XDOT =      -2009
169126                 XDOT =        -704
391462
 YDOT =      21223
028373  feet/sec       YDOT =        6461
416383  meter/sec
 ZDOT =      13310
561469                 ZDOT =        4053
861064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6457137
93                 X    =        -1968135
64
 Y    =      -16990246
00  feet           Y    =        -5178626
98  meter
 Z    =      -12898830
61                 Z    =        -3931563
57
 XDOT =      13287
185017                 XDOT =        4049
933993
 YDOT =     -15144
794510  feet/sec       YDOT =       -4616
133367  meter/sec
 ZDOT =      13295
392630                 ZDOT =        4052
435674


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   19227
50852013  
00016717  00000-0  10270-3 0  9035
2 25544  51
6401  66
9569 0007416 286
1475  73
8859 15
50354204 24455


Satellite: ISS
Catalog Number: 25544
Epoch time:      19227
50852013   =   yrday
fracday
Element set:     903
Inclination:       51
6401  deg
RA of node:        66
9569  deg
Eccentricity:     
0007416     
Arg of perigee:   286
1475  deg
Mean anomaly:      73
8859  deg
Mean motion:   15
50354204  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2445
Checksum:              314


Coasting Arc #5 (Orbit 2460)
---------------------------------------

Vector Time (GMT): 2019/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4889419
09                 A    =         6794779
01  meter
 Y    =       -3005842
59  meter          E    =           
0005884
 Z    =        3635960
10                 I    =           51
98258
 XDOT =        531
524629                 Wp   =           54
90870
 YDOT =      -6228
803688  meter/sec      RA   =           61
26833  deg
 ZDOT =      -4426
234740                 TA   =           82
30385
                                          MA   =           82
23703
                                          Ha   =            225
672  n
mi
                                          Hp   =            223
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16041401
22                 X    =        -4873104
59
 Y    =       -9861688
29  feet           Y    =        -3060428
27  meter
 Z    =       11929002
95                 Z    =         3612249
30
 XDOT =       1743
847209                 XDOT =         622
637118
 YDOT =     -20435
707637  feet/sec       YDOT =       -6222
350390  meter/sec
 ZDOT =     -14521
767520                 ZDOT =       -4423
431522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7155826
43                 X    =         2181095
90
 Y    =       17490880
55  feet           Y    =         5331220
39  meter
 Z    =       11821328
44                 Z    =         3603140
91
 XDOT =     -12306
633904                 XDOT =       -3751
062014
 YDOT =      14859
141360  feet/sec       YDOT =        4529
066287  meter/sec
 ZDOT =     -14508
412728                 ZDOT =       -4422
164200


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   19228
53986236  
00016717  00000-0  10270-3 0  9045
2 25544  51
6410  61
8442 0007613 290
6552  69
3782 15
50377469 24615


Satellite: ISS
Catalog Number: 25544
Epoch time:      19228
53986236   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:        61
8442  deg
Eccentricity:     
0007613     
Arg of perigee:   290
6552  deg
Mean anomaly:      69
3782  deg
Mean motion:   15
50377469  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2461
Checksum:              324


Coasting Arc #6 (Orbit 2475)
---------------------------------------

Vector Time (GMT): 2019/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5111526
47                 A    =         6795853
44  meter
 Y    =        3032535
06  meter          E    =           
0004173
 Z    =       -3289587
78                 I    =           51
96746
 XDOT =       -487
521331                 Wp   =          328
89695
 YDOT =       5984
091928  meter/sec      RA   =           56
33365  deg
 ZDOT =       4759
737437                 TA   =          353
16522
                                          MA   =          353
17091
                                          Ha   =            225
974  n
mi
                                          Hp   =            223
316

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16770099
97                 X    =         5093214
58
 Y    =        9949262
01  feet           Y    =         3089593
29  meter
 Z    =      -10792610
83                 Z    =        -3264802
92
 XDOT =      -1599
479432                 XDOT =        -577
520651
 YDOT =      19632
847532  feet/sec       YDOT =        5978
137005  meter/sec
 ZDOT =      15615
936473                 ZDOT =        4757
150572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7993351
05                 X    =        -2436373
40
 Y    =      -17853494
16  feet           Y    =        -5441745
02  meter
 Z    =      -10680056
25                 Z    =        -3255281
15
 XDOT =      11437
788873                 XDOT =        3486
238048
 YDOT =     -14453
507157  feet/sec       YDOT =       -4405
428982  meter/sec
 ZDOT =      15603
583997                 ZDOT =        4755
972402


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   19229
50674670  
00016717  00000-0  10270-3 0  9050
2 25544  51
6396  57
0504 0007336 293
8790  66
1592 15
50352361 24769


Satellite: ISS
Catalog Number: 25544
Epoch time:      19229
50674670   =   yrday
fracday
Element set:     905
Inclination:       51
6396  deg
RA of node:        57
0504  deg
Eccentricity:     
0007336     
Arg of perigee:   293
8790  deg
Mean anomaly:      66
1592  deg
Mean motion:   15
50352361  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2476
Checksum:              323


Coasting Arc #7 (Orbit 2491)
---------------------------------------

Vector Time (GMT): 2019/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5337594
45                 A    =         6796779
18  meter
 Y    =       -3036814
49  meter          E    =           
0006598
 Z    =        2909093
35                 I    =           51
95131
 XDOT =        495
020426                 Wp   =           77
41136
 YDOT =      -5728
557920  meter/sec      RA   =           51
39984  deg
 ZDOT =      -5060
736445                 TA   =           69
65692
                                          MA   =           69
58603
                                          Ha   =            226
028  n
mi
                                          Hp   =            223
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17511792
83                 X    =        -5317369
76
 Y    =       -9963302
15  feet           Y    =        -3096390
05  meter
 Z    =        9544269
52                 Z    =         2883214
95
 XDOT =       1624
082764                 XDOT =         583
623880
 YDOT =     -18794
481364  feet/sec       YDOT =       -5722
527005  meter/sec
 ZDOT =     -16603
466026                 ZDOT =       -5058
116475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8896878
53                 X    =         2711768
58
 Y    =       18138505
01  feet           Y    =         5528616
33  meter
 Z    =        9426746
35                 Z    =         2873272
29
 XDOT =     -10709
568268                 XDOT =       -3264
276408
 YDOT =      13894
598361  feet/sec       YDOT =        4235
073580  meter/sec
 ZDOT =     -16590
981363                 ZDOT =       -5056
931120


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   19230
53808705  
00016717  00000-0  10270-3 0  9064
2 25544  51
6396  51
9384 0007540 297
7166  62
3220 15
50375310 24928


Satellite: ISS
Catalog Number: 25544
Epoch time:      19230
53808705   =   yrday
fracday
Element set:     906
Inclination:       51
6396  deg
RA of node:        51
9384  deg
Eccentricity:     
0007540     
Arg of perigee:   297
7166  deg
Mean anomaly:      62
3220  deg
Mean motion:   15
50375310  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2492
Checksum:              306


Coasting Arc #8 (Orbit 2506)
---------------------------------------

Vector Time (GMT): 2019/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5557398
12                 A    =         6797736
85  meter
 Y    =        2985744
31  meter          E    =           
0007557
 Z    =       -2518197
84                 I    =           51
93225
 XDOT =       -537
230786                 Wp   =          342
78454
 YDOT =       5486
715881  meter/sec      RA   =           46
46451  deg
 ZDOT =       5322
751974                 TA   =          349
12352
                                          MA   =          349
13985
                                          Ha   =            226
276  n
mi
                                          Hp   =            222
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18232933
46                 X    =         5535829
49
 Y    =        9795749
06  feet           Y    =         3047770
36  meter
 Z    =       -8261803
93                 Z    =        -2491254
90
 XDOT =      -1762
568196                 XDOT =        -624
399564
 YDOT =      18001
036354  feet/sec       YDOT =        5480
220999  meter/sec
 ZDOT =      17463
097029                 ZDOT =        5319
930417

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9894842
02                 X    =        -3015947
85
 Y    =      -18234461
03  feet           Y    =        -5557863
72  meter
 Z    =       -8139440
94                 Z    =        -2480901
60
 XDOT =      10135
099979                 XDOT =        3089
178474
 YDOT =     -13284
531693  feet/sec       YDOT =       -4049
125260  meter/sec
 ZDOT =      17449
711936                 ZDOT =        5318
672198


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   19231
50497148  
00016717  00000-0  10270-3 0  9078
2 25544  51
6392  47
1452 0007247 300
6877  59
3559 15
50349375 25074


Satellite: ISS
Catalog Number: 25544
Epoch time:      19231
50497148   =   yrday
fracday
Element set:     907
Inclination:       51
6392  deg
RA of node:        47
1452  deg
Eccentricity:     
0007247     
Arg of perigee:   300
6877  deg
Mean anomaly:      59
3559  deg
Mean motion:   15
50349375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2507
Checksum:              326


Coasting Arc #9 (Orbit 2522)
---------------------------------------

Vector Time (GMT): 2019/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5770010
87                 A    =         6798461
95  meter
 Y    =       -2916392
67  meter          E    =           
0006886
 Z    =        2095318
74                 I    =           51
91191
 XDOT =        632
226333                 Wp   =           95
38914
 YDOT =      -5245
802992  meter/sec      RA   =           41
52896  deg
 ZDOT =      -5545
391422                 TA   =           61
54948
                                          MA   =           61
48012
                                          Ha   =            226
356  n
mi
                                          Hp   =            222
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18930481
86                 X    =        -5747147
91
 Y    =       -9568217
43  feet           Y    =        -2980789
09  meter
 Z    =        6874405
31                 Z    =         2067346
05
 XDOT =       2074
233376                 XDOT =         717
775645
 YDOT =     -17210
639736  feet/sec       YDOT =       -5238
254858  meter/sec
 ZDOT =     -18193
541410                 ZDOT =       -5542
112354

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10910104
43                 X    =         3325399
83
 Y    =       18237711
59  feet           Y    =         5558854
49  meter
 Z    =        6747360
53                 Z    =         2056595
49
 XDOT =      -9736
713883                 XDOT =       -2967
750391
 YDOT =      12568
562996  feet/sec       YDOT =        3830
898001  meter/sec
 ZDOT =     -18178
090991                 ZDOT =       -5540
682134


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   19232
53631022  
00016717  00000-0  10270-3 0  9084
2 25544  51
6400  42
0329 0007474 305
0968  54
9481 15
50380302 25231


Satellite: ISS
Catalog Number: 25544
Epoch time:      19232
53631022   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:        42
0329  deg
Eccentricity:     
0007474     
Arg of perigee:   305
0968  deg
Mean anomaly:      54
9481  deg
Mean motion:   15
50380302  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2523
Checksum:              279


Coasting Arc #10 (Orbit 2537)
---------------------------------------

Vector Time (GMT): 2019/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5961215
26                 A    =         6799195
62  meter
 Y    =        2794232
99  meter          E    =           
0010706
 Z    =       -1670114
34                 I    =           51
88903
 XDOT =       -757
245773                 Wp   =          355
90701
 YDOT =       5034
932811  meter/sec      RA   =           36
59190  deg
 ZDOT =       5729
099261                 TA   =          345
88233
                                          MA   =          345
91223
                                          Ha   =            226
584  n
mi
                                          Hp   =            222
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19557792
86                 X    =         5937638
75
 Y    =        9167431
08  feet           Y    =         2860763
63  meter
 Z    =       -5479377
76                 Z    =        -1641214
47
 XDOT =      -2484
402143                 XDOT =        -841
320215
 YDOT =      16518
808436  feet/sec       YDOT =        5025
994825  meter/sec
 ZDOT =      18796
257417                 ZDOT =        5725
216523

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11958371
72                 X    =        -3644911
70
 Y    =      -18026859
49  feet           Y    =        -5494586
77  meter
 Z    =       -5348113
47                 Z    =        -1630104
99
 XDOT =       9514
137225                 XDOT =        2899
909026
 YDOT =     -11874
208036  feet/sec       YDOT =       -3619
258609  meter/sec
 ZDOT =      18778
073876                 ZDOT =        5723
556917


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   19233
50319201  
00016717  00000-0  10270-3 0  9095
2 25544  51
6406  37
2401 0007111 308
9581  51
0936 15
50355863 25388


Satellite: ISS
Catalog Number: 25544
Epoch time:      19233
50319201   =   yrday
fracday
Element set:     909
Inclination:       51
6406  deg
RA of node:        37
2401  deg
Eccentricity:     
0007111     
Arg of perigee:   308
9581  deg
Mean anomaly:      51
0936  deg
Mean motion:   15
50355863  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2538
Checksum:              287


Coasting Arc #11 (Orbit 2548)
---------------------------------------

Vector Time (GMT): 2019/234/03:38:33
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4396704
01                 A    =         6798609
08  meter
 Y    =        4774937
77  meter          E    =           
0012725
 Z    =        1993989
18                 I    =           51
87102
 XDOT =      -4808
504796                 Wp   =           35
96576
 YDOT =       2088
248599  meter/sec      RA   =           33
40845  deg
 ZDOT =       5593
941090                 TA   =          345
95430
                                          MA   =          345
98966
                                          Ha   =            226
766  n
mi
                                          Hp   =            222
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14424881
91                 X    =         4333296
84
 Y    =       15665806
32  feet           Y    =         4823750
31  meter
 Z    =        6541959
27                 Z    =         2015192
56
 XDOT =     -15775
934371                 XDOT =       -4858
670987
 YDOT =       6851
209315  feet/sec       YDOT =        2034
196121  meter/sec
 ZDOT =      18352
825099                 ZDOT =        5570
461371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19496115
00                 X    =         5942415
85
 Y    =        8492976
17  feet           Y    =         2588659
14  meter
 Z    =        6637981
04                 Z    =         2023256
62
 XDOT =     -11137
925538                 XDOT =       -3394
839704
 YDOT =      11286
804273  feet/sec       YDOT =        3440
217943  meter/sec
 ZDOT =      18245
740494                 ZDOT =        5561
301702


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   19234
21223786  
00016717  00000-0  10270-3 0  9108
2 25544  51
6421  33
7300 0007476 314
0013  46
0521 15
50350247 25493


Satellite: ISS
Catalog Number: 25544
Epoch time:      19234
21223786   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        33
7300  deg
Eccentricity:     
0007476     
Arg of perigee:   314
0013  deg
Mean anomaly:      46
0521  deg
Mean motion:   15
50350247  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2549
Checksum:              265


Coasting Arc #12 (Orbit 2563)
---------------------------------------

Vector Time (GMT): 2019/235/03:38:33
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4424482
67                 A    =         6797774
94  meter
 Y    =       -4560482
72  meter          E    =           
0002150
 Z    =       -2417928
09                 I    =           51
84091
 XDOT =       5056
437454                 Wp   =          329
41792
 YDOT =      -2057
074957  meter/sec      RA   =           28
46902  deg
 ZDOT =      -5368
822878                 TA   =          237
47426
                                          MA   =          237
49504
                                          Ha   =            226
930  n
mi
                                          Hp   =            222
109

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14516019
25                 X    =        -4361412
28
 Y    =      -14962213
65  feet           Y    =        -4609607
76  meter
 Z    =       -7932834
93                 Z    =        -2439267
32
 XDOT =      16589
361726                 XDOT =        5105
143150
 YDOT =      -6748
933586  feet/sec       YDOT =       -2000
257994  meter/sec
 ZDOT =     -17614
248289                 ZDOT =       -5344
142361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19417324
28                 X    =        -5918400
44
 Y    =       -7483810
44  feet           Y    =        -2281065
42  meter
 Z    =       -8029484
49                 Z    =        -2447386
87
 XDOT =      11767
556655                 XDOT =        3586
751269
 YDOT =     -11740
437575  feet/sec       YDOT =       -3578
485373  meter/sec
 ZDOT =     -17501
705211                 ZDOT =       -5334
519748


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   19235
17911755  
00016717  00000-0  10270-3 0  9115
2 25544  51
6431  28
9382 0007531 317
2235  42
8329 15
50360968 25641


Satellite: ISS
Catalog Number: 25544
Epoch time:      19235
17911755   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:        28
9382  deg
Eccentricity:     
0007531     
Arg of perigee:   317
2235  deg
Mean anomaly:      42
8329  deg
Mean motion:   15
50360968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2564
Checksum:              310


Coasting Arc #13 (Orbit 2571)
---------------------------------------

Vector Time (GMT): 2019/235/16:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4291329
02                 A    =         6790568
08  meter
 Y    =       -2133805
96  meter          E    =           
0005897
 Z    =       -4814899
32                 I    =           51
80158
 XDOT =       5325
927840                 Wp   =           73
06997
 YDOT =       4848
802050  meter/sec      RA   =           25
79828  deg
 ZDOT =       2602
266707                 TA   =          222
52626
                                          MA   =          222
57195
                                          Ha   =            226
877  n
mi
                                          Hp   =            222
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14079163
44                 X    =         4338258
95
 Y    =       -7000675
74  feet           Y    =        -2085554
87  meter
 Z    =      -15796913
78                 Z    =        -4793939
74
 XDOT =      17473
516536                 XDOT =        5258
670974
 YDOT =      15908
143208  feet/sec       YDOT =        4907
984248  meter/sec
 ZDOT =       8537
620430                 ZDOT =        2627
974677

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7168550
23                 X    =        -2184974
11
 Y    =       14101626
55  feet           Y    =         4298175
77  meter
 Z    =      -15701299
47                 Z    =        -4785756
08
 XDOT =     -22445
924521                 XDOT =       -6841
517794
 YDOT =      -1790
372699  feet/sec       YDOT =        -545
705599  meter/sec
 ZDOT =       8654
116902                 ZDOT =        2637
774832


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   19235
69478492  
00016717  00000-0  10270-3 0  9129
2 25544  51
6435  26
3802 0007252 316
3392  43
7192 15
50385853 25725


Satellite: ISS
Catalog Number: 25544
Epoch time:      19235
69478492   =   yrday
fracday
Element set:     912
Inclination:       51
6435  deg
RA of node:        26
3802  deg
Eccentricity:     
0007252     
Arg of perigee:   316
3392  deg
Mean anomaly:      43
7192  deg
Mean motion:   15
50385853  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2572
Checksum:              318


Coasting Arc #14 (Orbit 2580)
---------------------------------------

Vector Time (GMT): 2019/236/05:30:59
000
Vector Time (MET): N/A
Weight (LBS)     : 952598
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3500100
23                 A    =         6789408
54  meter
 Y    =        2850736
27  meter          E    =           
0009106
 Z    =        5074196
30                 I    =           51
78252
 XDOT =      -6128
150480                 Wp   =          357
91088
 YDOT =      -4203
708720  meter/sec      RA   =           23
10321  deg
 ZDOT =      -1856
644237                 TA   =          110
10771
                                          MA   =          110
00970
                                          Ha   =            227
102  n
mi
                                          Hp   =            221
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11483268
47                 X    =        -3556365
39
 Y    =        9352809
30  feet           Y    =         2811281
01  meter
 Z    =       16647625
64                 Z    =         5057057
57
 XDOT =     -20105
480576                 XDOT =       -6071
669427
 YDOT =     -13791
695277  feet/sec       YDOT =       -4271
922176  meter/sec
 ZDOT =      -6091
352484                 ZDOT =       -1886
275275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         769537
20                 X    =          234554
94
 Y    =       14877808
13  feet           Y    =         4534755
92  meter
 Z    =       16569326
29                 Z    =         5050330
65
 XDOT =     -21856
836400                 XDOT =       -6661
963735
 YDOT =       8096
310554  feet/sec       YDOT =        2467
755457  meter/sec
 ZDOT =      -6225
764695                 ZDOT =       -1897
613079


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   19236
27491077  
00016717  00000-0  10270-3 0  9139
2 25544  51
6446  23
5075 0007722 320
3374  39
7212 15
50406474 25816


Satellite: ISS
Catalog Number: 25544
Epoch time:      19236
27491077   =   yrday
fracday
Element set:     913
Inclination:       51
6446  deg
RA of node:        23
5075  deg
Eccentricity:     
0007722     
Arg of perigee:   320
3374  deg
Mean anomaly:      39
7212  deg
Mean motion:   15
50406474  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2581
Checksum:              299


Coasting Arc #15 (Orbit 2595)
---------------------------------------

Vector Time (GMT): 2019/237/05:30:59
000
Vector Time (MET): N/A
Weight (LBS)     : 952598
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3713451
84                 A    =         6790163
72  meter
 Y    =       -2861372
29  meter          E    =           
0007468
 Z    =       -4917086
02                 I    =           51
75310
 XDOT =       6130
489071                 Wp   =           67
72812
 YDOT =       3948
970498  meter/sec      RA   =           18
15266  deg
 ZDOT =       2337
429825                 TA   =          225
11298
                                          MA   =          225
17364
                                          Ha   =            227
319  n
mi
                                          Hp   =            221
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12183240
93                 X    =         3769056
86
 Y    =       -9387704
36  feet           Y    =        -2819534
81  meter
 Z    =      -16132171
98                 Z    =        -4898912
60
 XDOT =      20113
153121                 XDOT =        6074
521051
 YDOT =      12955
939955  feet/sec       YDOT =        4017
212938  meter/sec
 ZDOT =       7668
733021                 ZDOT =        2367
073437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -654958
04                 X    =         -199631
21
 Y    =      -15453242
68  feet           Y    =        -4710148
37  meter
 Z    =      -16049163
40                 Z    =        -4891785
00
 XDOT =      20984
580779                 XDOT =        6396
100221
 YDOT =      -8974
343453  feet/sec       YDOT =       -2735
379884  meter/sec
 ZDOT =       7803
219883                 ZDOT =        2378
421420


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   19237
24178856  
00016717  00000-0  10270-3 0  9145
2 25544  51
6441  18
7148 0007705 324
7012  35
3627 15
50376565 25961


Satellite: ISS
Catalog Number: 25544
Epoch time:      19237
24178856   =   yrday
fracday
Element set:     914
Inclination:       51
6441  deg
RA of node:        18
7148  deg
Eccentricity:     
0007705     
Arg of perigee:   324
7012  deg
Mean anomaly:      35
3627  deg
Mean motion:   15
50376565  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2596
Checksum:              320


Coasting Arc #16 (Orbit 2611)
---------------------------------------

Vector Time (GMT): 2019/238/05:30:59
000
Vector Time (MET): N/A
Weight (LBS)     : 952598
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3953426
88                 A    =         6790919
45  meter
 Y    =        2888392
45  meter          E    =           
0010640
 Z    =        4707798
04                 I    =           51
72326
 XDOT =      -6079
980627                 Wp   =           16
68194
 YDOT =      -3710
099697  meter/sec      RA   =           13
20082  deg
 ZDOT =      -2817
929408                 TA   =          101
32328
                                          MA   =          101
20371
                                          Ha   =            227
430  n
mi
                                          Hp   =            221
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12970560
64                 X    =        -4008299
53
 Y    =        9476353
19  feet           Y    =         2843875
48  meter
 Z    =       15445531
63                 Z    =         4688460
79
 XDOT =     -19947
443003                 XDOT =       -6024
353550
 YDOT =     -12172
243102  feet/sec       YDOT =       -3777
779196  meter/sec
 ZDOT =      -9245
175224                 ZDOT =       -2847
328397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         556937
25                 X    =          169754
47
 Y    =       16138358
21  feet           Y    =         4918971
58  meter
 Z    =       15357225
52                 Z    =         4680882
34
 XDOT =     -20027
725249                 XDOT =       -6104
450656
 YDOT =       9651
995664  feet/sec       YDOT =        2941
928278  meter/sec
 ZDOT =      -9378
567700                 ZDOT =       -2858
587435


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   19238
27312235  
00016717  00000-0  10270-3 0  9151
2 25544  51
6435  13
6030 0007813 328
2609  31
8070 15
50409331 26129


Satellite: ISS
Catalog Number: 25544
Epoch time:      19238
27312235   =   yrday
fracday
Element set:     915
Inclination:       51
6435  deg
RA of node:        13
6030  deg
Eccentricity:     
0007813     
Arg of perigee:   328
2609  deg
Mean anomaly:      31
8070  deg
Mean motion:   15
50409331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2612
Checksum:              274


Coasting Arc #17 (Orbit 2626)
---------------------------------------

Vector Time (GMT): 2019/239/05:30:59
000
Vector Time (MET): N/A
Weight (LBS)     : 952598
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4150838
43                 A    =         6791894
73  meter
 Y    =       -2974492
90  meter          E    =           
0006102
 Z    =       -4480244
10                 I    =           51
69335
 XDOT =       5998
850218                 Wp   =           53
45727
 YDOT =       3471
369153  meter/sec      RA   =            8
24693  deg
 ZDOT =       3259
735836                 TA   =          249
35516
                                          MA   =          249
42061
                                          Ha   =            227
609  n
mi
                                          Hp   =            221
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13618236
33                 X    =         4205553
80
 Y    =       -9758834
98  feet           Y    =        -2927769
25  meter
 Z    =      -14698963
59                 Z    =        -4459948
36
 XDOT =      19681
267119                 XDOT =        5943
752765
 YDOT =      11389
006407  feet/sec       YDOT =        3538
144362  meter/sec
 ZDOT =      10694
671378                 ZDOT =        3288
741856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -721614
24                 X    =         -219948
02
 Y    =      -16819224
62  feet           Y    =        -5126499
66  meter
 Z    =      -14606290
01                 Z    =        -4451997
20
 XDOT =      19001
039480                 XDOT =        5791
516833
 YDOT =     -10198
067001  feet/sec       YDOT =       -3108
370822  meter/sec
 ZDOT =      10826
296821                 ZDOT =        3299
855271


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   19239
23999948  
00016717  00000-0  10270-3 0  9161
2 25544  51
6434   8
8102 0007781 331
4286  28
6438 15
50375780 26273


Satellite: ISS
Catalog Number: 25544
Epoch time:      19239
23999948   =   yrday
fracday
Element set:     916
Inclination:       51
6434  deg
RA of node:         8
8102  deg
Eccentricity:     
0007781     
Arg of perigee:   331
4286  deg
Mean anomaly:      28
6438  deg
Mean motion:   15
50375780  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2627
Checksum:              338


Coasting Arc #18 (Orbit 2632)
---------------------------------------

Vector Time (GMT): 2019/239/14:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928586
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6279970
85                 A    =         6798186
29  meter
 Y    =       -1147640
52  meter          E    =           
0010859
 Z    =       -2317662
11                 I    =           51
70131
 XDOT =       2839
327862                 Wp   =            2
15281
 YDOT =       4618
388234  meter/sec      RA   =            6
30426  deg
 ZDOT =       5418
001543                 TA   =          332
07267
                                          MA   =          332
13091
                                          Ha   =            227
613  n
mi
                                          Hp   =            221
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20603578
90                 X    =         6303595
09
 Y    =       -3765224
79  feet           Y    =        -1077281
32  meter
 Z    =       -7603878
33                 Z    =        -2287099
51
 XDOT =       9315
380125                 XDOT =        2761
155472
 YDOT =      15152
192369  feet/sec       YDOT =        4649
702394  meter/sec
 ZDOT =      17775
595615                 ZDOT =        5431
603945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18362821
73                 X    =        -5596988
06
 Y    =       10177851
66  feet           Y    =         3102209
19  meter
 Z    =       -7464680
88                 Z    =        -2275234
73
 XDOT =     -12819
272923                 XDOT =       -3907
314387
 YDOT =     -10074
345135  feet/sec       YDOT =       -3070
660397  meter/sec
 ZDOT =      17837
003661                 ZDOT =        5436
718716


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   19239
62674949  
00016717  00000-0  10270-3 0  9176
2 25544  51
6437   6
8905 0007525 331
2710  28
8025 15
50336601 26331


Satellite: ISS
Catalog Number: 25544
Epoch time:      19239
62674949   =   yrday
fracday
Element set:     917
Inclination:       51
6437  deg
RA of node:         6
8905  deg
Eccentricity:     
0007525     
Arg of perigee:   331
2710  deg
Mean anomaly:      28
8025  deg
Mean motion:   15
50336601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2633
Checksum:              311


Coasting Arc #19 (Orbit 2648)
---------------------------------------

Vector Time (GMT): 2019/240/14:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928586
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6396256
69                 A    =         6798852
16  meter
 Y    =        1331995
61  meter          E    =           
0009803
 Z    =        1875417
22                 I    =           51
67067
 XDOT =      -2594
761654                 Wp   =           82
68127
 YDOT =      -4507
181236  meter/sec      RA   =            1
35319  deg
 ZDOT =      -5621
980959                 TA   =           76
72651
                                          MA   =           76
61720
                                          Ha   =            227
643  n
mi
                                          Hp   =            221
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20985094
12                 X    =        -6419785
63
 Y    =        4370064
33  feet           Y    =         1260336
61  meter
 Z    =        6152943
63                 Z    =         1844290
06
 XDOT =      -8512
997554                 XDOT =       -2516
860281
 YDOT =     -14787
340012  feet/sec       YDOT =       -4535
762122  meter/sec
 ZDOT =     -18444
819418                 ZDOT =       -5634
395880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18331746
24                 X    =         5587516
26
 Y    =      -11186747
73  feet           Y    =        -3409720
71  meter
 Z    =        6011165
27                 Z    =         1832203
17
 XDOT =      12057
452588                 XDOT =        3675
111549
 YDOT =       9769
423671  feet/sec       YDOT =        2977
720335  meter/sec
 ZDOT =     -18500
837108                 ZDOT =       -5639
055150


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   19240
65808175  
00016717  00000-0  10270-3 0  9182
2 25544  51
6438   1
7787 0007446 336
4757  23
6052 15
50372769 26499


Satellite: ISS
Catalog Number: 25544
Epoch time:      19240
65808175   =   yrday
fracday
Element set:     918
Inclination:       51
6438  deg
RA of node:         1
7787  deg
Eccentricity:     
0007446     
Arg of perigee:   336
4757  deg
Mean anomaly:      23
6052  deg
Mean motion:   15
50372769  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2649
Checksum:              335
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