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

 
Date: September 23rd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13923 1181 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


266/16:46:57 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 4

268/13:57:43 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 3

268/17:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

271/11:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

272/00:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

275/04:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 218 3

276/07:34:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 4

Coasting Arc #1 (Orbit 3003)
---------------------------------------

Vector Time (GMT): 2019/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4650881
04                 A    =         6794411
10  meter
 Y    =        2999516
07  meter          E    =           
0018248
 Z    =        3930244
02                 I    =           51
27849
 XDOT =       -787
264699                 Wp   =           74
06783
 YDOT =       6491
668548  meter/sec      RA   =          247
52712  deg
 ZDOT =      -4002
274990                 TA   =           58
01823
                                          MA   =           57
84099
                                          Ha   =            229
854  n
mi
                                          Hp   =            218
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15258796
07                 X    =         4597902
77
 Y    =        9840931
98  feet           Y    =         3051229
45  meter
 Z    =       12894501
39                 Z    =         3952707
70
 XDOT =      -2582
889432                 XDOT =        -840
356856
 YDOT =      21298
125157  feet/sec       YDOT =        6482
567763  meter/sec
 ZDOT =     -13130
823457                 ZDOT =       -4006
228512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14854846
50                 X    =        -4527757
21
 Y    =      -10313506
54  feet           Y    =        -3143556
79  meter
 Z    =       12996464
29                 Z    =         3961322
31
 XDOT =       2410
133417                 XDOT =         734
608665
 YDOT =     -20125
224194  feet/sec       YDOT =       -6134
168334  meter/sec
 ZDOT =     -13149
212671                 ZDOT =       -4007
880022


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   19263
54091017  
00016717  00000-0  10270-3 0  9005
2 25544  51
6391 248
3577 0007403  65
2740 294
9180 15
50109248 30046


Satellite: ISS
Catalog Number: 25544
Epoch time:      19263
54091017   =   yrday
fracday
Element set:     900
Inclination:       51
6391  deg
RA of node:       248
3577  deg
Eccentricity:     
0007403     
Arg of perigee:    65
2740  deg
Mean anomaly:     294
9180  deg
Mean motion:   15
50109248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3004
Checksum:              295


Coasting Arc #2 (Orbit 3018)
---------------------------------------

Vector Time (GMT): 2019/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4877789
76                 A    =         6795284
65  meter
 Y    =       -2966140
54  meter          E    =           
0012727
 Z    =       -3695445
69                 I    =           51
29448
 XDOT =        596
771782                 Wp   =           83
21939
 YDOT =      -6309
019630  meter/sec      RA   =          242
54875  deg
 ZDOT =       4290
471786                 TA   =          232
64621
                                          MA   =          232
76221
                                          Ha   =            230
020  n
mi
                                          Hp   =            218
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16003247
23                 X    =        -4826308
41
 Y    =       -9731432
21  feet           Y    =        -3020399
68  meter
 Z    =      -12124165
65                 Z    =        -3719015
24
 XDOT =       1957
912671                 XDOT =         646
435799
 YDOT =     -20698
883301  feet/sec       YDOT =       -6302
068288  meter/sec
 ZDOT =      14076
351003                 ZDOT =        4293
491521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15781159
42                 X    =         4810097
39
 Y    =        9957583
59  feet           Y    =         3035071
48  meter
 Z    =      -12231174
25                 Z    =        -3728061
91
 XDOT =      -1431
008161                 XDOT =        -436
171287
 YDOT =      19518
671403  feet/sec       YDOT =        5949
291044  meter/sec
 ZDOT =      14090
472662                 ZDOT =        4294
776067


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   19264
50795400  
00016717  00000-0  10270-3 0  9010
2 25544  51
6386 243
5671 0007492  68
9882 291
2069 15
50073353 30196


Satellite: ISS
Catalog Number: 25544
Epoch time:      19264
50795400   =   yrday
fracday
Element set:     901
Inclination:       51
6386  deg
RA of node:       243
5671  deg
Eccentricity:     
0007492     
Arg of perigee:    68
9882  deg
Mean anomaly:     291
2069  deg
Mean motion:   15
50073353  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3019
Checksum:              320


Coasting Arc #3 (Orbit 3034)
---------------------------------------

Vector Time (GMT): 2019/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5089282
08                 A    =         6796100
95  meter
 Y    =        2950056
95  meter          E    =           
0019526
 Z    =        3388842
10                 I    =           51
31384
 XDOT =       -471
028829                 Wp   =           83
50323
 YDOT =       6119
293614  meter/sec      RA   =          237
57066  deg
 ZDOT =      -4594
541026                 TA   =           56
74231
                                          MA   =           56
55535
                                          Ha   =            229
903  n
mi
                                          Hp   =            218
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16697119
70                 X    =         5039454
25
 Y    =        9678664
52  feet           Y    =         3006690
36  meter
 Z    =       11118248
37                 Z    =         3413442
97
 XDOT =      -1545
370175                 XDOT =        -517
103686
 YDOT =      20076
422617  feet/sec       YDOT =        6113
768511  meter/sec
 ZDOT =     -15073
953496                 ZDOT =       -4596
941168

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16650580
70                 X    =        -5075097
00
 Y    =       -9629736
93  feet           Y    =        -2935143
82  meter
 Z    =       11229965
67                 Z    =         3422893
54
 XDOT =        681
649155                 XDOT =         207
766662
 YDOT =     -18865
551454  feet/sec       YDOT =       -5750
220083  meter/sec
 ZDOT =     -15085
235228                 ZDOT =       -4597
979697


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   19265
53946506  
00016717  00000-0  10270-3 0  9020
2 25544  51
6386 238
4556 0007374  72
2335 287
9619 15
50106833 30352


Satellite: ISS
Catalog Number: 25544
Epoch time:      19265
53946506   =   yrday
fracday
Element set:     902
Inclination:       51
6386  deg
RA of node:       238
4556  deg
Eccentricity:     
0007374     
Arg of perigee:    72
2335  deg
Mean anomaly:     287
9619  deg
Mean motion:   15
50106833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3035
Checksum:              326


Coasting Arc #4 (Orbit 3049)
---------------------------------------

Vector Time (GMT): 2019/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5325216
89                 A    =         6796911
61  meter
 Y    =       -2855470
37  meter          E    =           
0011994
 Z    =       -3119036
55                 I    =           51
33592
 XDOT =        349
512160                 Wp   =           76
37019
 YDOT =      -5919
132776  meter/sec      RA   =          232
59504  deg
 ZDOT =       4840
740693                 TA   =          247
65467
                                          MA   =          247
78184
                                          Ha   =            230
027  n
mi
                                          Hp   =            218
274

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17471184
04                 X    =        -5277739
85
 Y    =       -9368341
12  feet           Y    =        -2914755
32  meter
 Z    =      -10233059
53                 Z    =        -3144789
10
 XDOT =       1146
693438                 XDOT =         392
161974
 YDOT =     -19419
726956  feet/sec       YDOT =       -5914
985692  meter/sec
 ZDOT =      15881
695188                 ZDOT =        4842
542233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17587348
22                 X    =         5360623
74
 Y    =        9015843
70  feet           Y    =         2748029
16  meter
 Z    =      -10350040
55                 Z    =        -3154692
36
 XDOT =          9
969316                 XDOT =           3
038648
 YDOT =      18153
309400  feet/sec       YDOT =        5533
128705  meter/sec
 ZDOT =      15890
230685                 ZDOT =        4843
342313


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   19266
50650441  
00016717  00000-0  10270-3 0  9039
2 25544  51
6392 233
6645 0007464  75
4984 284
6994 15
50084060 30504


Satellite: ISS
Catalog Number: 25544
Epoch time:      19266
50650441   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:       233
6645  deg
Eccentricity:     
0007464     
Arg of perigee:    75
4984  deg
Mean anomaly:     284
6994  deg
Mean motion:   15
50084060  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3050
Checksum:              317


Coasting Arc #5 (Orbit 3052)
---------------------------------------

Vector Time (GMT): 2019/266/16:46:57
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4400579
01                 A    =         6800995
47  meter
 Y    =       -5168335
79  meter          E    =           
0017988
 Z    =        -301980
32                 I    =           51
35717
 XDOT =       3482
276247                 Wp   =           55
87006
 YDOT =      -3298
605422  meter/sec      RA   =          231
62562  deg
 ZDOT =       5975
841167                 TA   =          300
86793
                                          MA   =          301
04475
                                          Ha   =            229
950  n
mi
                                          Hp   =            218
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14437595
18                 X    =        -4340991
27
 Y    =      -16956482
25  feet           Y    =        -5217213
00  meter
 Z    =        -990749
07                 Z    =         -323211
83
 XDOT =      11424
790836                 XDOT =        3489
876058
 YDOT =     -10822
196267  feet/sec       YDOT =       -3259
621499  meter/sec
 ZDOT =      19605
778108                 ZDOT =        5992
775319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20420753
61                 X    =         6224245
70
 Y    =       -8874638
22  feet           Y    =        -2704989
73  meter
 Z    =       -1087035
92                 Z    =         -331328
55
 XDOT =       6421
480421                 XDOT =        1957
267232
 YDOT =      12462
465722  feet/sec       YDOT =        3798
559552  meter/sec
 ZDOT =      19682
999553                 ZDOT =        5999
378264


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   19266
69991212  
00016717  00000-0  10270-3 0  9044
2 25544  51
6427 232
7070 0007314  75
6101 284
5861 15
50107432 30536


Satellite: ISS
Catalog Number: 25544
Epoch time:      19266
69991212   =   yrday
fracday
Element set:     904
Inclination:       51
6427  deg
RA of node:       232
7070  deg
Eccentricity:     
0007314     
Arg of perigee:    75
6101  deg
Mean anomaly:     284
5861  deg
Mean motion:   15
50107432  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3053
Checksum:              294


Coasting Arc #6 (Orbit 3068)
---------------------------------------

Vector Time (GMT): 2019/267/16:46:57
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4599258
38                 A    =         6801138
67  meter
 Y    =        5002501
99  meter          E    =           
0017263
 Z    =        -111333
06                 I    =           51
37841
 XDOT =      -3578
764493                 Wp   =          115
09317
 YDOT =       3173
519829  meter/sec      RA   =          226
65487  deg
 ZDOT =      -5984
266628                 TA   =           66
10825
                                          MA   =           65
92747
                                          Ha   =            230
074  n
mi
                                          Hp   =            218
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15089430
38                 X    =         4543517
92
 Y    =       16412408
10  feet           Y    =         5053622
47  meter
 Z    =        -365265
94                 Z    =          -89127
23
 XDOT =     -11741
353324                 XDOT =       -3584
917555
 YDOT =      10411
810462  feet/sec       YDOT =        3133
464906  meter/sec
 ZDOT =     -19633
420697                 ZDOT =       -6001
665959

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19923145
92                 X    =        -6072574
88
 Y    =       10009483
37  feet           Y    =         3050890
53  meter
 Z    =        -264513
34                 Z    =          -80623
66
 XDOT =      -6096
231914                 XDOT =       -1858
131487
 YDOT =     -12566
726048  feet/sec       YDOT =       -3830
338099  meter/sec
 ZDOT =     -19712
752942                 ZDOT =       -6008
447097


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   19267
73141889  
00016717  00000-0  10270-3 0  9058
2 25544  51
6422 227
5964 0007357  80
6293 279
5689 15
50073262 30692


Satellite: ISS
Catalog Number: 25544
Epoch time:      19267
73141889   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       227
5964  deg
Eccentricity:     
0007357     
Arg of perigee:    80
6293  deg
Mean anomaly:     279
5689  deg
Mean motion:   15
50073262  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3069
Checksum:              344


Coasting Arc #7 (Orbit 3082)
---------------------------------------

Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         841306
74                 A    =         6790601
23  meter
 Y    =       -4572030
26  meter          E    =           
0012869
 Z    =        4939774
77                 I    =           51
36288
 XDOT =       6454
971885                 Wp   =          101
70346
 YDOT =       3532
769295  meter/sec      RA   =          222
28162  deg
 ZDOT =       2163
050155                 TA   =          327
09186
                                          MA   =          327
17192
                                          Ha   =            229
896  n
mi
                                          Hp   =            218
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2760192
72                 X    =          868375
39
 Y    =      -15000099
28  feet           Y    =        -4562470
52  meter
 Z    =       16206610
13                 Z    =         4943927
53
 XDOT =      21177
729281                 XDOT =        6404
480835
 YDOT =      11590
450444  feet/sec       YDOT =        3604
671164  meter/sec
 ZDOT =       7096
621245                 ZDOT =        2194
283011

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5857045
43                 X    =         1785227
45
 Y    =       14060443
47  feet           Y    =         4285623
17  meter
 Z    =       16225745
05                 Z    =         4945607
09
 XDOT =     -23018
979578                 XDOT =       -7016
184975
 YDOT =       1207
735838  feet/sec       YDOT =         368
117883  meter/sec
 ZDOT =       7238
545159                 ZDOT =        2206
308564


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   19268
63398427  
00016717  00000-0  10270-3 0  9061
2 25544  51
6404 223
1237 0007250  83
1587 277
0388 15
50138178 30836


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
63398427   =   yrday
fracday
Element set:     906
Inclination:       51
6404  deg
RA of node:       223
1237  deg
Eccentricity:     
0007250     
Arg of perigee:    83
1587  deg
Mean anomaly:     277
0388  deg
Mean motion:   15
50138178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3083
Checksum:              321


Coasting Arc #8 (Orbit 3084)
---------------------------------------

Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1028537
46                 A    =         6790384
76  meter
 Y    =       -4449350
71  meter          E    =           
0012388
 Z    =        5015568
79                 I    =           51
36659
 XDOT =       6451
244572                 Wp   =          101
32257
 YDOT =       3672
662171  meter/sec      RA   =          221
63728  deg
 ZDOT =       1928
653007                 TA   =          329
86361
                                          MA   =          329
93483
                                          Ha   =            229
994  n
mi
                                          Hp   =            218
316

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3374466
75                 X    =         1053852
20
 Y    =      -14597607
31  feet           Y    =        -4437707
01  meter
 Z    =       16455278
17                 Z    =         5020626
79
 XDOT =      21165
500565                 XDOT =        6400
328044
 YDOT =      12049
416573  feet/sec       YDOT =        3744
519972  meter/sec
 ZDOT =       6327
601729                 ZDOT =        1959
866700

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13740605
41                 X    =         4188136
53
 Y    =        5908243
63  feet           Y    =         1800832
66  meter
 Z    =       16478524
35                 Z    =         5022654
22
 XDOT =     -15319
615204                 XDOT =       -4669
418714
 YDOT =      17525
704091  feet/sec       YDOT =        5341
834607  meter/sec
 ZDOT =       6469
434321                 ZDOT =        1971
883581


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   19268
76292307  
00016717  00000-0  10270-3 0  9076
2 25544  51
6420 222
4854 0007370  83
3018 276
8971 15
50100696 30856


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
76292307   =   yrday
fracday
Element set:     907
Inclination:       51
6420  deg
RA of node:       222
4854  deg
Eccentricity:     
0007370     
Arg of perigee:    83
3018  deg
Mean anomaly:     276
8971  deg
Mean motion:   15
50100696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3085
Checksum:              316


Coasting Arc #9 (Orbit 3099)
---------------------------------------

Vector Time (GMT): 2019/269/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932083
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1076582
42                 A    =         6789829
07  meter
 Y    =        4320196
29  meter          E    =           
0020743
 Z    =       -5144813
89                 I    =           51
39109
 XDOT =      -6654
014039                 Wp   =           81
22707
 YDOT =      -3451
589948  meter/sec      RA   =          216
66195  deg
 ZDOT =      -1508
109916                 TA   =          174
16499
                                          MA   =          174
14078
                                          Ha   =            229
931  n
mi
                                          Hp   =            218
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3532094
57                 X    =        -1099821
52
 Y    =       14173872
33  feet           Y    =         4308026
77  meter
 Z    =      -16879310
67                 Z    =        -5150100
35
 XDOT =     -21830
754720                 XDOT =       -6607
597283
 YDOT =     -11324
114002  feet/sec       YDOT =       -3525
740432  meter/sec
 ZDOT =      -4947
867178                 ZDOT =       -1540
319466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13396458
81                 X    =        -4083240
64
 Y    =       -5752329
97  feet           Y    =        -1753310
18  meter
 Z    =      -16903581
54                 Z    =        -5152211
65
 XDOT =      14408
297562                 XDOT =        4391
649097
 YDOT =     -18605
879323  feet/sec       YDOT =       -5671
072018  meter/sec
 ZDOT =      -5094
265888                 ZDOT =       -1552
732243


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   19269
72995607  
00016717  00000-0  10270-3 0  9087
2 25544  51
6424 217
6935 0007197  85
8295 274
3678 15
50129536 31006


Satellite: ISS
Catalog Number: 25544
Epoch time:      19269
72995607   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:       217
6935  deg
Eccentricity:     
0007197     
Arg of perigee:    85
8295  deg
Mean anomaly:     274
3678  deg
Mean motion:   15
50129536  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3100
Checksum:              347


Coasting Arc #10 (Orbit 3115)
---------------------------------------

Vector Time (GMT): 2019/270/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932083
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1127268
12                 A    =         6789498
20  meter
 Y    =       -4191063
78  meter          E    =           
0010715
 Z    =        5212491
59                 I    =           51
41798
 XDOT =       6875
605983                 Wp   =          101
59318
 YDOT =       3217
195704  meter/sec      RA   =          211
68852  deg
 ZDOT =       1095
796039                 TA   =          337
85269
                                          MA   =          337
89895
                                          Ha   =            229
947  n
mi
                                          Hp   =            218
329

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3698386
21                 X    =         1148730
62
 Y    =      -13750209
26  feet           Y    =        -4178337
28  meter
 Z    =       17101350
36                 Z    =         5218020
04
 XDOT =      22557
762412                 XDOT =        6833
796588
 YDOT =      10555
104015  feet/sec       YDOT =        3293
849934  meter/sec
 ZDOT =       3595
131362                 ZDOT =        1129
093264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13049712
37                 X    =         3977552
33
 Y    =        5619904
49  feet           Y    =         1712946
89  meter
 Z    =       17126709
54                 Z    =         5220221
07
 XDOT =     -13429
911341                 XDOT =       -4093
436977
 YDOT =      19727
220066  feet/sec       YDOT =        6012
856676  meter/sec
 ZDOT =       3746
511658                 ZDOT =        1141
936753


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   19270
76145623  
00016717  00000-0  10270-3 0  9099
2 25544  51
6430 212
5822 0007261  89
5602 270
6381 15
50110248 31164


Satellite: ISS
Catalog Number: 25544
Epoch time:      19270
76145623   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:       212
5822  deg
Eccentricity:     
0007261     
Arg of perigee:    89
5602  deg
Mean anomaly:     270
6381  deg
Mean motion:   15
50110248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3116
Checksum:              287


Coasting Arc #11 (Orbit 3126)
---------------------------------------

Vector Time (GMT): 2019/271/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6258852
08                 A    =         6800621
36  meter
 Y    =       -2487533
94  meter          E    =           
0015437
 Z    =        -918055
41                 I    =           51
47437
 XDOT =       1041
055269                 Wp   =           61
94998
 YDOT =      -4767
576094  meter/sec      RA   =          207
90529  deg
 ZDOT =       5903
840655                 TA   =          288
10871
                                          MA   =          288
27679
                                          Ha   =            229
992  n
mi
                                          Hp   =            218
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20534291
60                 X    =        -6226111
16
 Y    =       -8161200
58  feet           Y    =        -2557341
88  meter
 Z    =       -3011992
83                 Z    =         -948378
89
 XDOT =       3415
535659                 XDOT =        1065
612592
 YDOT =     -15641
653853  feet/sec       YDOT =       -4755
796261  meter/sec
 ZDOT =      19369
555954                 ZDOT =        5908
957954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19690051
04                 X    =         6001527
56
 Y    =        9985716
44  feet           Y    =         3043646
37  meter
 Z    =       -3149886
46                 Z    =         -960085
39
 XDOT =      -3959
728657                 XDOT =       -1206
925295
 YDOT =      13842
905026  feet/sec       YDOT =        4219
317452  meter/sec
 ZDOT =      19393
067029                 ZDOT =        5911
006830


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   19271
47061214  
00016717  00000-0  10270-3 0  9103
2 25544  51
6403 209
0676 0007397  92
2761 267
9236 15
50116790 31277


Satellite: ISS
Catalog Number: 25544
Epoch time:      19271
47061214   =   yrday
fracday
Element set:     910
Inclination:       51
6403  deg
RA of node:       209
0676  deg
Eccentricity:     
0007397     
Arg of perigee:    92
2761  deg
Mean anomaly:     267
9236  deg
Mean motion:   15
50116790  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3127
Checksum:              304


Coasting Arc #12 (Orbit 3135)
---------------------------------------

Vector Time (GMT): 2019/272/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         261172
46                 A    =         6790370
52  meter
 Y    =        4559596
71  meter          E    =           
0019719
 Z    =       -5042666
22                 I    =           51
45930
 XDOT =      -7206
526293                 Wp   =           84
17125
 YDOT =      -1697
766489  meter/sec      RA   =          205
13351  deg
 ZDOT =      -1912
886082                 TA   =          167
20190
                                          MA   =          167
15177
                                          Ha   =            229
979  n
mi
                                          Hp   =            218
343

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         856865
03                 X    =          234660
99
 Y    =       14959306
79  feet           Y    =         4562368
48  meter
 Z    =      -16544180
50                 Z    =        -5041462
47
 XDOT =     -23643
458967                 XDOT =       -7177
713957
 YDOT =      -5570
100028  feet/sec       YDOT =       -1778
194083  meter/sec
 ZDOT =      -6275
872971                 ZDOT =       -1947
822780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5508864
68                 X    =         1679101
95
 Y    =       13940654
29  feet           Y    =         4249111
43  meter
 Z    =      -16538910
30                 Z    =        -5041059
86
 XDOT =     -23155
184088                 XDOT =       -7057
700110
 YDOT =       1533
583286  feet/sec       YDOT =         467
436186  meter/sec
 ZDOT =      -6434
807751                 ZDOT =       -1961
329403


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   19272
05082929  
00016717  00000-0  10270-3 0  9115
2 25544  51
6430 206
1903 0007253  98
6253 261
5719 15
50105827 31360


Satellite: ISS
Catalog Number: 25544
Epoch time:      19272
05082929   =   yrday
fracday
Element set:     911
Inclination:       51
6430  deg
RA of node:       206
1903  deg
Eccentricity:     
0007253     
Arg of perigee:    98
6253  deg
Mean anomaly:     261
5719  deg
Mean motion:   15
50105827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3136
Checksum:              299


Coasting Arc #13 (Orbit 3151)
---------------------------------------

Vector Time (GMT): 2019/273/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -198536
79                 A    =         6789753
00  meter
 Y    =       -4426703
16  meter          E    =           
0011871
 Z    =        5135905
36                 I    =           51
48892
 XDOT =       7381
770852                 Wp   =          111
77597
 YDOT =       1430
132008  meter/sec      RA   =          200
16556  deg
 ZDOT =       1510
875108                 TA   =          323
60178
                                          MA   =          323
68244
                                          Ha   =            229
907  n
mi
                                          Hp   =            218
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -651367
42                 X    =         -173969
07
 Y    =      -14523304
35  feet           Y    =        -4428785
41  meter
 Z    =       16850083
20                 Z    =         5135001
09
 XDOT =      24218
408306                 XDOT =        7357
890979
 YDOT =       4692
034147  feet/sec       YDOT =        1512
546825  meter/sec
 ZDOT =       4956
939330                 ZDOT =        1546
675306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5414490
67                 X    =        -1650336
76
 Y    =      -13496885
33  feet           Y    =        -4113850
65  meter
 Z    =       16846166
61                 Z    =         5134711
58
 XDOT =      23419
585601                 XDOT =        7138
289691
 YDOT =      -2975
612177  feet/sec       YDOT =        -906
966592  meter/sec
 ZDOT =       5119
832395                 ZDOT =        1560
524914


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   19273
08232414  
00016717  00000-0  10270-3 0  9126
2 25544  51
6434 201
0795 0007259 102
4002 257
7961 15
50152295 31524


Satellite: ISS
Catalog Number: 25544
Epoch time:      19273
08232414   =   yrday
fracday
Element set:     912
Inclination:       51
6434  deg
RA of node:       201
0795  deg
Eccentricity:     
0007259     
Arg of perigee:   102
4002  deg
Mean anomaly:     257
7961  deg
Mean motion:   15
50152295  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3152
Checksum:              284


Coasting Arc #14 (Orbit 3166)
---------------------------------------

Vector Time (GMT): 2019/274/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          87441
67                 A    =         6789497
39  meter
 Y    =        4339345
18  meter          E    =           
0020946
 Z    =       -5239276
01                 I    =           51
51934
 XDOT =      -7482
895905                 Wp   =           89
75343
 YDOT =      -1145
588149  meter/sec      RA   =          195
19963  deg
 ZDOT =      -1077
356935                 TA   =          169
89859
                                          MA   =          169
85643
                                          Ha   =            229
914  n
mi
                                          Hp   =            218
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         286882
11                 X    =           64361
28
 Y    =       14236696
80  feet           Y    =         4340193
50  meter
 Z    =      -17189225
76                 Z    =        -5238907
69
 XDOT =     -24550
183415                 XDOT =       -7464
296170
 YDOT =      -3758
491304  feet/sec       YDOT =       -1229
163270  meter/sec
 ZDOT =      -3534
635615                 ZDOT =       -1113
661370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5207909
45                 X    =         1587370
80
 Y    =       13254978
37  feet           Y    =         4040117
41  meter
 Z    =      -17187744
09                 Z    =        -5238824
40
 XDOT =     -23380
051221                 XDOT =       -7126
239612
 YDOT =       4404
019100  feet/sec       YDOT =        1342
345022  meter/sec
 ZDOT =      -3699
854462                 ZDOT =       -1127
715640


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   19274
04934909  
00016717  00000-0  10270-3 0  9132
2 25544  51
6434 196
2886 0007174 105
1822 255
0122 15
50113500 31678


Satellite: ISS
Catalog Number: 25544
Epoch time:      19274
04934909   =   yrday
fracday
Element set:     913
Inclination:       51
6434  deg
RA of node:       196
2886  deg
Eccentricity:     
0007174     
Arg of perigee:   105
1822  deg
Mean anomaly:     255
0122  deg
Mean motion:   15
50113500  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3167
Checksum:              294


Coasting Arc #15 (Orbit 3182)
---------------------------------------

Vector Time (GMT): 2019/275/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          14604
34                 A    =         6789081
21  meter
 Y    =       -4257575
24  meter          E    =           
0010263
 Z    =        5280208
15                 I    =           51
55091
 XDOT =       7594
698180                 Wp   =          111
26503
 YDOT =        843
405373  meter/sec      RA   =          190
23564  deg
 ZDOT =        654
382856                 TA   =          332
45309
                                          MA   =          332
50744
                                          Ha   =            229
850  n
mi
                                          Hp   =            218
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          47914
49                 X    =           36563
92
 Y    =      -13968422
70  feet           Y    =        -4257288
79  meter
 Z    =       17323517
54                 Z    =         5280332
70
 XDOT =      24916
988778                 XDOT =        7581
523836
 YDOT =       2767
077995  feet/sec       YDOT =         928
261026  meter/sec
 ZDOT =       2146
925379                 ZDOT =         691
243646

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5027717
46                 X    =        -1532448
28
 Y    =      -13031303
61  feet           Y    =        -3971941
34  meter
 Z    =       17324276
95                 Z    =         5280439
61
 XDOT =      23309
746029                 XDOT =        7104
810590
 YDOT =      -5895
694609  feet/sec       YDOT =       -1797
007717  meter/sec
 ZDOT =       2314
711327                 ZDOT =         705
524013


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   19275
08083759  
00016717  00000-0  10270-3 0  9146
2 25544  51
6433 191
1779 0007221 108
3644 251
8292 15
50161593 31837


Satellite: ISS
Catalog Number: 25544
Epoch time:      19275
08083759   =   yrday
fracday
Element set:     914
Inclination:       51
6433  deg
RA of node:       191
1779  deg
Eccentricity:     
0007221     
Arg of perigee:   108
3644  deg
Mean anomaly:     251
8292  deg
Mean motion:   15
50161593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3183
Checksum:              317


Coasting Arc #16 (Orbit 3184)
---------------------------------------

Vector Time (GMT): 2019/275/04:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3953517
96                 A    =         6791850
34  meter
 Y    =       -3037687
89  meter          E    =           
0014697
 Z    =        4600062
19                 I    =           51
56296
 XDOT =       6156
556496                 Wp   =           84
84295
 YDOT =       3451
009143  meter/sec      RA   =          189
53816  deg
 ZDOT =      -3002
774483                 TA   =           35
19275
                                          MA   =           35
09578
                                          Ha   =            229
814  n
mi
                                          Hp   =            218
295

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12970859
45                 X    =         3964847
49
 Y    =       -9966167
62  feet           Y    =        -2993413
23  meter
 Z    =       15092067
55                 Z    =         4619294
94
 XDOT =      20198
676167                 XDOT =        6132
094810
 YDOT =      11322
208473  feet/sec       YDOT =        3519
719140  meter/sec
 ZDOT =      -9851
622321                 ZDOT =       -2972
927346

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4881235
31                 X    =        -1487800
52
 Y    =      -15526953
06  feet           Y    =        -4732615
29  meter
 Z    =       15179771
59                 Z    =         4626794
38
 XDOT =      16517
131067                 XDOT =        5034
421549
 YDOT =     -14721
672651  feet/sec       YDOT =       -4487
165824  meter/sec
 ZDOT =      -9715
884288                 ZDOT =       -2961
401531


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   19275
20977433  
00016717  00000-0  10270-3 0  9152
2 25544  51
6416 190
5409 0007357 106
3245 253
8715 15
50153444 31856


Satellite: ISS
Catalog Number: 25544
Epoch time:      19275
20977433   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       190
5409  deg
Eccentricity:     
0007357     
Arg of perigee:   106
3245  deg
Mean anomaly:     253
8715  deg
Mean motion:   15
50153444  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3185
Checksum:              312


Coasting Arc #17 (Orbit 3199)
---------------------------------------

Vector Time (GMT): 2019/276/04:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4078089
07                 A    =         6792676
18  meter
 Y    =        3185666
66  meter          E    =           
0016565
 Z    =       -4417000
54                 I    =           51
59887
 XDOT =      -6101
353279                 Wp   =          110
53301
 YDOT =      -3159
532076  meter/sec      RA   =          184
57819  deg
 ZDOT =       3359
031810                 TA   =          193
53066
                                          MA   =          193
57513
                                          Ha   =            229
948  n
mi
                                          Hp   =            218
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13379557
33                 X    =        -4091953
35
 Y    =       10451662
28  feet           Y    =         3139984
88  meter
 Z    =      -14491471
58                 Z    =        -4436844
49
 XDOT =     -20017
563251                 XDOT =       -6081
885580
 YDOT =     -10365
918883  feet/sec       YDOT =       -3227
652716  meter/sec
 ZDOT =      11020
445570                 ZDOT =        3329
440675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5469270
88                 X    =         1667033
77
 Y    =       15990794
39  feet           Y    =         4873994
13  meter
 Z    =      -14581979
22                 Z    =        -4444587
27
 XDOT =     -15261
515426                 XDOT =       -4651
709902
 YDOT =      15133
022876  feet/sec       YDOT =        4612
545373  meter/sec
 ZDOT =      10885
841698                 ZDOT =        3318
004550


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   19276
17679487  
00016717  00000-0  10270-3 0  9168
2 25544  51
6419 185
7494 0007407 109
4806 250
7146 15
50128232 32001


Satellite: ISS
Catalog Number: 25544
Epoch time:      19276
17679487   =   yrday
fracday
Element set:     916
Inclination:       51
6419  deg
RA of node:       185
7494  deg
Eccentricity:     
0007407     
Arg of perigee:   109
4806  deg
Mean anomaly:     250
7146  deg
Mean motion:   15
50128232  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3200
Checksum:              323


Coasting Arc #18 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2019/276/07:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950247
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3762547
74                 A    =         6793177
52  meter
 Y    =       -3667667
35  meter          E    =           
0017123
 Z    =        4295106
74                 I    =           51
60251
 XDOT =       6374
195602                 Wp   =          108
86150
 YDOT =      -2376
554838  meter/sec      RA   =          183
89012  deg
 ZDOT =       3537
486998                 TA   =          304
99535
                                          MA   =          305
15597
                                          Ha   =            229
909  n
mi
                                          Hp   =            218
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12344316
72                 X    =        -3742118
74
 Y    =      -12033029
36  feet           Y    =        -3709628
41  meter
 Z    =       14091557
53                 Z    =         4276879
18
 XDOT =      20912
715229                 XDOT =        6383
113767
 YDOT =      -7797
095925  feet/sec       YDOT =       -2305
224077  meter/sec
 ZDOT =      11605
928471                 ZDOT =        3568
472687

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2920963
76                 X    =         -890309
75
 Y    =       17057891
14  feet           Y    =         5199245
22  meter
 Z    =       14008721
04                 Z    =         4269858
17
 XDOT =     -16944
022185                 XDOT =       -5164
537962
 YDOT =     -12594
765667  feet/sec       YDOT =       -3838
884575  meter/sec
 ZDOT =      11747
138025                 ZDOT =        3580
527670


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   19276
37019755  
00016717  00000-0  10270-3 0  9177
2 25544  51
6389 184
7918 0007213 110
9159 249
2764 15
50162800 32031


Satellite: ISS
Catalog Number: 25544
Epoch time:      19276
37019755   =   yrday
fracday
Element set:     917
Inclination:       51
6389  deg
RA of node:       184
7918  deg
Eccentricity:     
0007213     
Arg of perigee:   110
9159  deg
Mean anomaly:     249
2764  deg
Mean motion:   15
50162800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3203
Checksum:              322


Coasting Arc #19 (Orbit 3217)
---------------------------------------

Vector Time (GMT): 2019/277/07:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950247
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3641171
88                 A    =         6792403
41  meter
 Y    =        3524250
74  meter          E    =           
0015680
 Z    =       -4536842
40                 I    =           51
63358
 XDOT =      -6457
363809                 Wp   =           88
80652
 YDOT =       2619
763020  meter/sec      RA   =          178
93163  deg
 ZDOT =      -3156
634264                 TA   =          149
48563
                                          MA   =          149
39431
                                          Ha   =            229
906  n
mi
                                          Hp   =            218
515

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11946101
98                 X    =         3623529
81
 Y    =       11562502
41  feet           Y    =         3564870
10  meter
 Z    =      -14884653
53                 Z    =        -4519197
69
 XDOT =     -21185
576801                 XDOT =       -6470
845465
 YDOT =       8595
023033  feet/sec       YDOT =        2547
476743  meter/sec
 ZDOT =     -10356
411626                 ZDOT =       -3188
034933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2470238
21                 X    =          752928
61
 Y    =      -16513019
46  feet           Y    =        -5033168
33  meter
 Z    =      -14804453
28                 Z    =        -4512397
36
 XDOT =      18015
125485                 XDOT =        5491
010248
 YDOT =      12081
083213  feet/sec       YDOT =        3682
314163  meter/sec
 ZDOT =     -10499
544996                 ZDOT =       -3200
261315


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   19277
33721548  
00016717  00000-0  10270-3 0  9185
2 25544  51
6394 179
9990 0007306 113
2381 246
9540 15
50131979 32184


Satellite: ISS
Catalog Number: 25544
Epoch time:      19277
33721548   =   yrday
fracday
Element set:     918
Inclination:       51
6394  deg
RA of node:       179
9990  deg
Eccentricity:     
0007306     
Arg of perigee:   113
2381  deg
Mean anomaly:     246
9540  deg
Mean motion:   15
50131979  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3218
Checksum:              333


Coasting Arc #20 (Orbit 3233)
---------------------------------------

Vector Time (GMT): 2019/278/07:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950247
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3532257
03                 A    =         6791547
84  meter
 Y    =       -3372975
71  meter          E    =           
0015138
 Z    =        4710733
35                 I    =           51
66506
 XDOT =       6521
340827                 Wp   =          117
20361
 YDOT =      -2909
075096  meter/sec      RA   =          173
97716  deg
 ZDOT =       2793
278993                 TA   =          305
05249
                                          MA   =          305
19440
                                          Ha   =            229
815  n
mi
                                          Hp   =            218
499

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11588769
78                 X    =        -3517159
25
 Y    =      -11066193
29  feet           Y    =        -3412391
35  meter
 Z    =       15455161
92                 Z    =         4693611
59
 XDOT =      21395
475153                 XDOT =        6539
817945
 YDOT =      -9544
209634  feet/sec       YDOT =       -2836
045467  meter/sec
 ZDOT =       9164
301158                 ZDOT =        2825
002474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1995086
65                 X    =         -608102
41
 Y    =       15974346
89  feet           Y    =         4868980
93  meter
 Z    =       15377324
85                 Z    =         4687008
61
 XDOT =     -19156
510259                 XDOT =       -5838
904327
 YDOT =     -11396
955686  feet/sec       YDOT =       -3473
792093  meter/sec
 ZDOT =       9308
941456                 ZDOT =        2837
365356


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   19278
36869477  
00016717  00000-0  10270-3 0  9194
2 25544  51
6399 174
8887 0007119 117
5065 242
6809 15
50178534 32343


Satellite: ISS
Catalog Number: 25544
Epoch time:      19278
36869477   =   yrday
fracday
Element set:     919
Inclination:       51
6399  deg
RA of node:       174
8887  deg
Eccentricity:     
0007119     
Arg of perigee:   117
5065  deg
Mean anomaly:     242
6809  deg
Mean motion:   15
50178534  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3234
Checksum:              361
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