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

 
Date: May 5th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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


124/06:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 217 3

128/05:34:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 2

131/09:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 217 3

134/18:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 217 1

Coasting Arc #1 (Orbit 831)
---------------------------------------

Vector Time (GMT): 2019/123/13:11:49
422
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1667613
40                 A    =         6787973
34  meter
 Y    =       -5450814
55  meter          E    =           
0010557
 Z    =        3677446
38                 I    =           51
38239
 XDOT =       6261
991120                 Wp   =           95
39522
 YDOT =       1000
592426  meter/sec      RA   =          221
96923  deg
 ZDOT =       4311
062379                 TA   =          308
53953
                                          MA   =          308
63410
                                          Ha   =            222
893  n
mi
                                          Hp   =            217
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5471172
57                 X    =        -1624400
21
 Y    =      -17883249
84  feet           Y    =        -5469221
34  meter
 Z    =       12065112
81                 Z    =         3669450
57
 XDOT =      20544
590290                 XDOT =        6229
395689
 YDOT =       3282
783550  feet/sec       YDOT =        1070
436151  meter/sec
 ZDOT =      14143
905443                 ZDOT =        4341
402150

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18125327
20                 X    =        -5524599
73
 Y    =       -4698728
24  feet           Y    =        -1432172
37  meter
 Z    =       12029371
05                 Z    =         3666552
30
 XDOT =      13218
902679                 XDOT =        4029
121536
 YDOT =     -14332
128929  feet/sec       YDOT =       -4368
432898  meter/sec
 ZDOT =      14281
057094                 ZDOT =        4352
866202


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   19123
60645597  
00016717  00000-0  10270-3 0  9005
2 25544  51
6417 222
7752 0001270 271
2755  88
8251 15
52638134  8325


Satellite: ISS
Catalog Number: 25544
Epoch time:      19123
60645597   =   yrday
fracday
Element set:     900
Inclination:       51
6417  deg
RA of node:       222
7752  deg
Eccentricity:     
0001270     
Arg of perigee:   271
2755  deg
Mean anomaly:      88
8251  deg
Mean motion:   15
52638134  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             832
Checksum:              304


Coasting Arc #2 (Orbit 842)
---------------------------------------

Vector Time (GMT): 2019/124/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5001036
51                 A    =         6793434
23  meter
 Y    =        4552217
82  meter          E    =           
0009743
 Z    =        -594684
31                 I    =           51
41624
 XDOT =      -3613
714709                 Wp   =          141
82867
 YDOT =       3199
930712  meter/sec      RA   =          218
28710  deg
 ZDOT =      -5954
612864                 TA   =           44
60555
                                          MA   =           44
52719
                                          Ha   =            222
921  n
mi
                                          Hp   =            217
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16407600
11                 X    =         4952649
33
 Y    =       14935097
84  feet           Y    =         4607872
37  meter
 Z    =       -1951064
01                 Z    =         -570508
15
 XDOT =     -11856
019386                 XDOT =       -3620
303898
 YDOT =      10498
460342  feet/sec       YDOT =        3159
482850  meter/sec
 ZDOT =     -19536
131445                 ZDOT =       -5972
183246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4120401
65                 X    =         1255898
42
 Y    =       21810599
62  feet           Y    =         6647870
76  meter
 Z    =       -1842057
10                 Z    =         -561459
00
 XDOT =     -14091
068624                 XDOT =       -4294
957717
 YDOT =       1022
910213  feet/sec       YDOT =         311
783033  meter/sec
 ZDOT =     -19615
856433                 ZDOT =       -5978
913041


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   19124
31446565  
00016717  00000-0  10270-3 0  9019
2 25544  51
6384 219
2524 0001223 298
0719  62
0310 15
52670987  8435


Satellite: ISS
Catalog Number: 25544
Epoch time:      19124
31446565   =   yrday
fracday
Element set:     901
Inclination:       51
6384  deg
RA of node:       219
2524  deg
Eccentricity:     
0001223     
Arg of perigee:   298
0719  deg
Mean anomaly:      62
0310  deg
Mean motion:   15
52670987  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             843
Checksum:              298


Coasting Arc #3 (Orbit 858)
---------------------------------------

Vector Time (GMT): 2019/125/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4574747
22                 A    =         6792430
18  meter
 Y    =       -4690507
66  meter          E    =           
0013188
 Z    =        1765964
49                 I    =           51
43816
 XDOT =       4612
597035                 Wp   =           62
25000
 YDOT =      -2360
784609  meter/sec      RA   =          213
30800  deg
 ZDOT =       5652
208802                 TA   =          317
18989
                                          MA   =          317
29251
                                          Ha   =            223
018  n
mi
                                          Hp   =            217
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15009013
20                 X    =        -4530534
88
 Y    =      -15388804
64  feet           Y    =        -4741418
53  meter
 Z    =        5793846
75                 Z    =         1743848
85
 XDOT =      15133
192373                 XDOT =        4611
197315
 YDOT =      -7745
356329  feet/sec       YDOT =       -2309
211331  meter/sec
 ZDOT =      18543
992132                 ZDOT =        5674
612064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3118033
98                 X    =         -950376
76
 Y    =      -21295747
82  feet           Y    =        -6490943
93  meter
 Z    =        5694157
94                 Z    =         1735579
34
 XDOT =      15139
872282                 XDOT =        4614
633072
 YDOT =       2792
359242  feet/sec       YDOT =         851
111097  meter/sec
 ZDOT =      18645
523276                 ZDOT =        5683
155495


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   19125
34429743  
00016717  00000-0  10270-3 0  9023
2 25544  51
6373 214
1301 0001021 286
6165  73
4875 15
52625653  8593


Satellite: ISS
Catalog Number: 25544
Epoch time:      19125
34429743   =   yrday
fracday
Element set:     902
Inclination:       51
6373  deg
RA of node:       214
1301  deg
Eccentricity:     
0001021     
Arg of perigee:   286
6165  deg
Mean anomaly:      73
4875  deg
Mean motion:   15
52625653  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             859
Checksum:              300


Coasting Arc #4 (Orbit 873)
---------------------------------------

Vector Time (GMT): 2019/126/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3938742
06                 A    =         6790202
97  meter
 Y    =        4725286
96  meter          E    =           
0003608
 Z    =       -2875276
32                 I    =           51
45999
 XDOT =      -5553
870852                 Wp   =          118
64718
 YDOT =       1566
740516  meter/sec      RA   =          208
32829  deg
 ZDOT =      -5039
754399                 TA   =           94
12880
                                          MA   =           94
08756
                                          Ha   =            223
010  n
mi
                                          Hp   =            217
375

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12922382
07                 X    =         3899576
60
 Y    =       15502909
96  feet           Y    =         4769113
90  meter
 Z    =       -9433321
25                 Z    =        -2856237
85
 XDOT =     -18221
361063                 XDOT =       -5546
496979
 YDOT =       5140
224789  feet/sec       YDOT =        1504
674751  meter/sec
 ZDOT =     -16534
627293                 ZDOT =       -5066
715587

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1730150
57                 X    =          527349
89
 Y    =       20148095
03  feet           Y    =         6141139
36  meter
 Z    =       -9347543
59                 Z    =        -2849131
29
 XDOT =     -16308
770311                 XDOT =       -4970
913191
 YDOT =      -6317
291981  feet/sec       YDOT =       -1925
510596  meter/sec
 ZDOT =     -16656
732276                 ZDOT =       -5076
971998


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   19126
30976143  
00016717  00000-0  10270-3 0  9032
2 25544  51
6379 209
3287 0001048 296
6321  63
4723 15
52646855  8747


Satellite: ISS
Catalog Number: 25544
Epoch time:      19126
30976143   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:       209
3287  deg
Eccentricity:     
0001048     
Arg of perigee:   296
6321  deg
Mean anomaly:      63
4723  deg
Mean motion:   15
52646855  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             874
Checksum:              323


Coasting Arc #5 (Orbit 889)
---------------------------------------

Vector Time (GMT): 2019/127/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3137687
92                 A    =         6787549
75  meter
 Y    =       -4654897
71  meter          E    =           
0010474
 Z    =        3807302
23                 I    =           51
48117
 XDOT =       6372
220457                 Wp   =           95
80176
 YDOT =       -870
446749  meter/sec      RA   =          203
34448  deg
 ZDOT =       4176
321133                 TA   =          310
03917
                                          MA   =          310
13102
                                          Ha   =            223
010  n
mi
                                          Hp   =            217
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10294251
70                 X    =        -3103896
43
 Y    =      -15271974
13  feet           Y    =        -4689796
89  meter
 Z    =       12491149
04                 Z    =         3792141
95
 XDOT =      20906
235095                 XDOT =        6361
193817
 YDOT =      -2855
796421  feet/sec       YDOT =        -799
250091  meter/sec
 ZDOT =      13701
840988                 ZDOT =        4207
248722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -45597
43                 X    =          -13898
10
 Y    =      -18463560
08  feet           Y    =        -5627693
11  meter
 Z    =       12422901
69                 Z    =         3786500
44
 XDOT =      17496
289360                 XDOT =        5332
868997
 YDOT =       9294
357438  feet/sec       YDOT =        2832
920147  meter/sec
 ZDOT =      13841
858995                 ZDOT =        4218
998622


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   19127
33958697  
00016717  00000-0  10270-3 0  9041
2 25544  51
6381 204
2058 0001074 292
1165  67
9873 15
52653182  8900


Satellite: ISS
Catalog Number: 25544
Epoch time:      19127
33958697   =   yrday
fracday
Element set:     904
Inclination:       51
6381  deg
RA of node:       204
2058  deg
Eccentricity:     
0001074     
Arg of perigee:   292
1165  deg
Mean anomaly:      67
9873  deg
Mean motion:   15
52653182  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             890
Checksum:              325


Coasting Arc #6 (Orbit 903)
---------------------------------------

Vector Time (GMT): 2019/128/05:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5282735
19                 A    =         6786876
16  meter
 Y    =        1557693
65  meter          E    =           
0006023
 Z    =       -3972090
71                 I    =           51
50759
 XDOT =      -4416
226474                 Wp   =          104
80686
 YDOT =      -4825
859001  meter/sec      RA   =          198
56665  deg
 ZDOT =       3984
474019                 TA   =          206
83153
                                          MA   =          206
86270
                                          Ha   =            223
040  n
mi
                                          Hp   =            217
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17331808
37                 X    =        -5280466
64
 Y    =        5110543
49  feet           Y    =         1498631
46  meter
 Z    =      -13031793
66                 Z    =        -3997746
99
 XDOT =     -14488
932000                 XDOT =       -4381
288771
 YDOT =     -15832
870738  feet/sec       YDOT =       -4875
049351  meter/sec
 ZDOT =      13072
421321                 ZDOT =        3963
105739

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14711495
19                 X    =        -4484063
74
 Y    =      -10345924
13  feet           Y    =        -3153437
67  meter
 Z    =      -13148028
19                 Z    =        -4007518
99
 XDOT =       2607
248103                 XDOT =         794
689222
 YDOT =     -20183
222393  feet/sec       YDOT =       -6151
846185  meter/sec
 ZDOT =      12976
078698                 ZDOT =        3955
108787


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   19128
24068320  
00016717  00000-0  10270-3 0  9058
2 25544  51
6372 199
7244 0000991 307
9838  52
1224 15
52637409  9040


Satellite: ISS
Catalog Number: 25544
Epoch time:      19128
24068320   =   yrday
fracday
Element set:     905
Inclination:       51
6372  deg
RA of node:       199
7244  deg
Eccentricity:     
0000991     
Arg of perigee:   307
9838  deg
Mean anomaly:      52
1224  deg
Mean motion:   15
52637409  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             904
Checksum:              312


Coasting Arc #7 (Orbit 919)
---------------------------------------

Vector Time (GMT): 2019/129/05:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5969998
32                 A    =         6789662
94  meter
 Y    =       -1047504
68  meter          E    =           
0012077
 Z    =        3048324
21                 I    =           51
54724
 XDOT =       3365
073089                 Wp   =           93
30858
 YDOT =       4828
539777  meter/sec      RA   =          193
58674  deg
 ZDOT =      -4914
932732                 TA   =           51
68048
                                          MA   =           51
57196
                                          Ha   =            222
979  n
mi
                                          Hp   =            217
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19586608
67                 X    =         5966460
90
 Y    =       -3436695
13  feet           Y    =         -980764
06  meter
 Z    =       10001063
67                 Z    =         3077315
83
 XDOT =      11040
266039                 XDOT =        3334
703139
 YDOT =      15841
665936  feet/sec       YDOT =        4866
001057  meter/sec
 ZDOT =     -16125
107389                 ZDOT =       -4898
659584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15036248
34                 X    =         4583048
49
 Y    =       12911760
95  feet           Y    =         3935504
74  meter
 Z    =       10132376
45                 Z    =         3088348
34
 XDOT =      -4234
890018                 XDOT =       -1290
794478
 YDOT =      17569
254097  feet/sec       YDOT =        5355
108649  meter/sec
 ZDOT =     -16051
810069                 ZDOT =       -4892
591709


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   19129
27050561  
00016717  00000-0  10270-3 0  9061
2 25544  51
6357 194
6024 0001094 306
7009  53
4042 15
52626461  9201


Satellite: ISS
Catalog Number: 25544
Epoch time:      19129
27050561   =   yrday
fracday
Element set:     906
Inclination:       51
6357  deg
RA of node:       194
6024  deg
Eccentricity:     
0001094     
Arg of perigee:   306
7009  deg
Mean anomaly:      53
4042  deg
Mean motion:   15
52626461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             920
Checksum:              286


Coasting Arc #8 (Orbit 934)
---------------------------------------

Vector Time (GMT): 2019/130/05:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6461642
98                 A    =         6791893
43  meter
 Y    =         617001
31  meter          E    =           
0006755
 Z    =       -1989942
43                 I    =           51
58969
 XDOT =      -2169
021709                 Wp   =           32
28957
 YDOT =      -4795
706733  meter/sec      RA   =          188
61350  deg
 ZDOT =       5570
513015                 TA   =          305
74443
                                          MA   =          305
80724
                                          Ha   =            223
027  n
mi
                                          Hp   =            217
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21199616
08                 X    =        -6458396
14
 Y    =        2024282
51  feet           Y    =          544761
04  meter
 Z    =       -6528682
50                 Z    =        -2021322
90
 XDOT =      -7116
212956                 XDOT =       -2142
292154
 YDOT =     -15733
945973  feet/sec       YDOT =       -4819
813325  meter/sec
 ZDOT =      18275
961334                 ZDOT =        5560
041126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15239255
15                 X    =        -4644924
97
 Y    =      -14812517
25  feet           Y    =        -4514855
26  meter
 Z    =       -6670799
97                 Z    =        -2033259
83
 XDOT =       6223
433412                 XDOT =        1896
902504
 YDOT =     -14591
374551  feet/sec       YDOT =       -4447
450963  meter/sec
 ZDOT =      18228
910483                 ZDOT =        5556
171915


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   19130
23596319  
00016717  00000-0  10270-3 0  9076
2 25544  51
6379 189
8000 0001018 312
6501  47
4565 15
52644294  9357


Satellite: ISS
Catalog Number: 25544
Epoch time:      19130
23596319   =   yrday
fracday
Element set:     907
Inclination:       51
6379  deg
RA of node:       189
8000  deg
Eccentricity:     
0001018     
Arg of perigee:   312
6501  deg
Mean anomaly:      47
4565  deg
Mean motion:   15
52644294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             935
Checksum:              307


Coasting Arc #9 (Orbit 950)
---------------------------------------

Vector Time (GMT): 2019/131/05:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6738125
13                 A    =         6793309
06  meter
 Y    =        -199702
05  meter          E    =           
0012273
 Z    =         792852
89                 I    =           51
62707
 XDOT =        847
433208                 Wp   =          125
07522
 YDOT =       4768
974813  meter/sec      RA   =          183
64609  deg
 ZDOT =      -5942
540821                 TA   =           46
35610
                                          MA   =           46
25440
                                          Ha   =            223
076  n
mi
                                          Hp   =            217
199

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22106709
73                 X    =         6736006
21
 Y    =        -655190
46  feet           Y    =         -124363
53  meter
 Z    =        2601223
39                 Z    =          825579
10
 XDOT =       2780
292677                 XDOT =         822
907823
 YDOT =      15646
242824  feet/sec       YDOT =        4778
314746  meter/sec
 ZDOT =     -19496
525003                 ZDOT =       -5938
483486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15080462
14                 X    =         4596524
86
 Y    =       16153097
85  feet           Y    =         4923464
23  meter
 Z    =        2749426
17                 Z    =          838025
10
 XDOT =      -8646
781212                 XDOT =       -2635
538914
 YDOT =      11418
813396  feet/sec       YDOT =        3480
454323  meter/sec
 ZDOT =     -19478
506756                 ZDOT =       -5937
048859


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   19131
26578133  
00016717  00000-0  10270-3 0  9085
2 25544  51
6374 184
6771 0001144 321
3568  38
7502 15
52658738  9510


Satellite: ISS
Catalog Number: 25544
Epoch time:      19131
26578133   =   yrday
fracday
Element set:     908
Inclination:       51
6374  deg
RA of node:       184
6771  deg
Eccentricity:     
0001144     
Arg of perigee:   321
3568  deg
Mean anomaly:      38
7502  deg
Mean motion:   15
52658738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             951
Checksum:              319


Coasting Arc #10 (Orbit 952)
---------------------------------------

Vector Time (GMT): 2019/131/09:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -320922
40                 A    =         6781678
25  meter
 Y    =        4207271
46  meter          E    =           
0014041
 Z    =       -5321278
24                 I    =           51
59619
 XDOT =      -7641
099895                 Wp   =           87
15781
 YDOT =       -465
194820  meter/sec      RA   =          182
92669  deg
 ZDOT =         93
917278                 TA   =          183
73390
                                          MA   =          183
74439
                                          Ha   =            223
053  n
mi
                                          Hp   =            217
271

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1052895
02                 X    =         -342097
59
 Y    =       13803384
06  feet           Y    =         4203564
69  meter
 Z    =      -17458261
94                 Z    =        -5322888
27
 XDOT =     -25069
225378                 XDOT =       -7635
786252
 YDOT =      -1526
229724  feet/sec       YDOT =        -550
613244  meter/sec
 ZDOT =        308
127553                 ZDOT =          56
812465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          84545
69                 X    =           25769
53
 Y    =       13833630
91  feet           Y    =         4216490
70  meter
 Z    =      -17465864
35                 Z    =        -5323595
45
 XDOT =     -24106
250911                 XDOT =       -7347
585278
 YDOT =        320
563853  feet/sec       YDOT =          97
707862  meter/sec
 ZDOT =        140
143440                 ZDOT =          42
715721


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   19131
39450806  
00016717  00000-0  10270-3 0  9096
2 25544  51
6407 184
0393 0001235 316
8885  43
2170 15
52645868  9537


Satellite: ISS
Catalog Number: 25544
Epoch time:      19131
39450806   =   yrday
fracday
Element set:     909
Inclination:       51
6407  deg
RA of node:       184
0393  deg
Eccentricity:     
0001235     
Arg of perigee:   316
8885  deg
Mean anomaly:      43
2170  deg
Mean motion:   15
52645868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             953
Checksum:              317


Coasting Arc #11 (Orbit 968)
---------------------------------------

Vector Time (GMT): 2019/132/09:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1511517
23                 A    =         6782236
17  meter
 Y    =       -4138019
44  meter          E    =           
0004590
 Z    =        5154881
99                 I    =           51
63188
 XDOT =       7472
408273                 Wp   =           39
41773
 YDOT =        894
776375  meter/sec      RA   =          177
94099  deg
 ZDOT =      -1468
606120                 TA   =           64
74574
                                          MA   =           64
69818
                                          Ha   =            222
964  n
mi
                                          Hp   =            217
234

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4959046
04                 X    =         1532637
81
 Y    =      -13576179
28  feet           Y    =        -4120998
79  meter
 Z    =       16912342
48                 Z    =         5162275
46
 XDOT =      24515
775173                 XDOT =        7468
980949
 YDOT =       2935
618029  feet/sec       YDOT =         978
318993  meter/sec
 ZDOT =      -4818
261549                 ZDOT =       -1432
316176

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3591693
35                 X    =         1094748
13
 Y    =      -13959244
63  feet           Y    =        -4254777
76  meter
 Z    =       16946130
47                 Z    =         5165180
57
 XDOT =      23694
789840                 XDOT =        7222
171943
 YDOT =        430
200160  feet/sec       YDOT =         131
125009  meter/sec
 ZDOT =      -4653
974435                 ZDOT =       -1418
531408


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   19132
42432483  
00016717  00000-0  10270-3 0  9104
2 25544  51
6407 178
9169 0001278 320
4570  39
6489 15
52679835  9699


Satellite: ISS
Catalog Number: 25544
Epoch time:      19132
42432483   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:       178
9169  deg
Eccentricity:     
0001278     
Arg of perigee:   320
4570  deg
Mean anomaly:      39
6489  deg
Mean motion:   15
52679835  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             969
Checksum:              337


Coasting Arc #12 (Orbit 983)
---------------------------------------

Vector Time (GMT): 2019/133/09:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2633687
53                 A    =         6784030
19  meter
 Y    =        4095646
32  meter          E    =           
0010146
 Z    =       -4733264
29                 I    =           51
67062
 XDOT =      -7019
137773                 Wp   =          105
19490
 YDOT =      -1329
777703  meter/sec      RA   =          172
96132  deg
 ZDOT =       2757
294099                 TA   =          192
11591
                                          MA   =          192
14033
                                          Ha   =            223
080  n
mi
                                          Hp   =            217
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8640707
11                 X    =        -2656298
82
 Y    =       13437159
84  feet           Y    =         4066068
32  meter
 Z    =      -15529082
32                 Z    =        -4746112
58
 XDOT =     -23028
667234                 XDOT =       -7017
139592
 YDOT =      -4362
787738  feet/sec       YDOT =       -1408
259542  meter/sec
 ZDOT =       9046
240482                 ZDOT =        2723
202447

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7035308
96                 X    =        -2144362
17
 Y    =       14279472
86  feet           Y    =         4352383
33  meter
 Z    =      -15587577
25                 Z    =        -4751093
55
 XDOT =     -22383
604242                 XDOT =       -6822
522573
 YDOT =      -1329
978856  feet/sec       YDOT =        -405
377555  meter/sec
 ZDOT =       8891
920339                 ZDOT =        2710
257319


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   19133
38977886  
00016717  00000-0  10270-3 0  9112
2 25544  51
6402 174
1160 0001188 327
1266  32
9811 15
52671807  9842


Satellite: ISS
Catalog Number: 25544
Epoch time:      19133
38977886   =   yrday
fracday
Element set:     911
Inclination:       51
6402  deg
RA of node:       174
1160  deg
Eccentricity:     
0001188     
Arg of perigee:   327
1266  deg
Mean anomaly:      32
9811  deg
Mean motion:   15
52671807  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             984
Checksum:              318


Coasting Arc #13 (Orbit 999)
---------------------------------------

Vector Time (GMT): 2019/134/09:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3659979
94                 A    =         6786567
94  meter
 Y    =       -4038037
63  meter          E    =           
0010388
 Z    =        4038358
50                 I    =           51
71284
 XDOT =       6336
796293                 Wp   =           70
70798
 YDOT =       1813
631734  meter/sec      RA   =          167
98690  deg
 ZDOT =      -3917
999935                 TA   =           59
95949
                                          MA   =           59
85649
                                          Ha   =            223
038  n
mi
                                          Hp   =            217
161

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12007808
21                 X    =         3685246
17
 Y    =      -13248154
96  feet           Y    =        -3996968
00  meter
 Z    =       13249207
67                 Z    =         4056198
70
 XDOT =      20790
014086                 XDOT =        6335
076384
 YDOT =       5950
235348  feet/sec       YDOT =        1884
484708  meter/sec
 ZDOT =     -12854
330496                 ZDOT =       -3887
222070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10168009
80                 X    =         3099209
39
 Y    =      -14634095
59  feet           Y    =        -4460472
34  meter
 Z    =       13330318
62                 Z    =         4063081
12
 XDOT =      20388
834814                 XDOT =        6214
516851
 YDOT =       2549
879700  feet/sec       YDOT =         777
203332  meter/sec
 ZDOT =     -12715
039017                 ZDOT =       -3875
543892


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   19134
41959295  
00016717  00000-0  10270-3 0  9122
2 25544  51
6410 168
9935 0001389 332
4422  27
6656 15
52674468 10002


Satellite: ISS
Catalog Number: 25544
Epoch time:      19134
41959295   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:       168
9935  deg
Eccentricity:     
0001389     
Arg of perigee:   332
4422  deg
Mean anomaly:      27
6656  deg
Mean motion:   15
52674468  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1000
Checksum:              318


Coasting Arc #14 (Orbit 1005)
---------------------------------------

Vector Time (GMT): 2019/134/18:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3776514
06                 A    =         6783910
92  meter
 Y    =       -2963610
78  meter          E    =           
0006451
 Z    =        4789002
16                 I    =           51
71409
 XDOT =       6206
724022                 Wp   =          109
31751
 YDOT =      -3660
671528  meter/sec      RA   =          166
17434  deg
 ZDOT =       2624
176299                 TA   =          314
81054
                                          MA   =          314
86297
                                          Ha   =            223
250  n
mi
                                          Hp   =            217
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12390137
98                 X    =        -3766355
95
 Y    =       -9723132
47  feet           Y    =        -3005785
71  meter
 Z    =       15711949
33                 Z    =         4770681
71
 XDOT =      20363
267789                 XDOT =        6234
450497
 YDOT =     -12010
077193  feet/sec       YDOT =       -3591
108625  meter/sec
 ZDOT =       8609
502293                 ZDOT =        2654
393757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3942467
92                 X    =         1201664
22
 Y    =       15333171
09  feet           Y    =         4673550
55  meter
 Z    =       15629171
02                 Z    =         4763771
33
 XDOT =     -22292
113806                 XDOT =       -6794
636288
 YDOT =      -3200
458386  feet/sec       YDOT =        -975
499716  meter/sec
 ZDOT =       8746
660779                 ZDOT =        2665
982205


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   19134
80577315  
00016717  00000-0  10270-3 0  9135
2 25544  51
6391 167
0745 0001599 338
9463  21
1623 15
52684500 10065


Satellite: ISS
Catalog Number: 25544
Epoch time:      19134
80577315   =   yrday
fracday
Element set:     913
Inclination:       51
6391  deg
RA of node:       167
0745  deg
Eccentricity:     
0001599     
Arg of perigee:   338
9463  deg
Mean anomaly:      21
1623  deg
Mean motion:   15
52684500  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1006
Checksum:              304


Coasting Arc #15 (Orbit 1020)
---------------------------------------

Vector Time (GMT): 2019/135/18:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2725474
16                 A    =         6782259
44  meter
 Y    =        3407795
73  meter          E    =           
0014001
 Z    =       -5204451
20                 I    =           51
73982
 XDOT =      -6739
446296                 Wp   =           73
22952
 YDOT =       3386
550716  meter/sec      RA   =          161
19830  deg
 ZDOT =      -1310
842163                 TA   =          184
16909
                                          MA   =          184
18076
                                          Ha   =            223
302  n
mi
                                          Hp   =            217
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8941844
37                 X    =         2712445
32
 Y    =       11180432
20  feet           Y    =         3438201
19  meter
 Z    =      -17074971
14                 Z    =        -5191243
25
 XDOT =     -22111
044277                 XDOT =       -6770
447354
 YDOT =      11110
730695  feet/sec       YDOT =        3311
012205  meter/sec
 ZDOT =      -4300
663264                 ZDOT =       -1343
655497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -577555
51                 X    =         -176038
92
 Y    =      -14375551
79  feet           Y    =        -4381668
18  meter
 Z    =      -17015382
01                 Z    =        -5186288
44
 XDOT =      23295
447131                 XDOT =        7100
452285
 YDOT =       4334
716337  feet/sec       YDOT =        1321
221540  meter/sec
 ZDOT =      -4449
580298                 ZDOT =       -1356
232075


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   19135
77122435  
00016717  00000-0  10270-3 0  9142
2 25544  51
6385 162
2722 0001678 349
5769  10
5347 15
52655895 10212


Satellite: ISS
Catalog Number: 25544
Epoch time:      19135
77122435   =   yrday
fracday
Element set:     914
Inclination:       51
6385  deg
RA of node:       162
2722  deg
Eccentricity:     
0001678     
Arg of perigee:   349
5769  deg
Mean anomaly:      10
5347  deg
Mean motion:   15
52655895  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1021
Checksum:              318


Coasting Arc #16 (Orbit 1036)
---------------------------------------

Vector Time (GMT): 2019/136/18:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1620362
64                 A    =         6781555
28  meter
 Y    =       -3870800
89  meter          E    =           
0002604
 Z    =        5325675
68                 I    =           51
76909
 XDOT =       7038
453113                 Wp   =           49
35531
 YDOT =      -3042
322251  meter/sec      RA   =          156
22330  deg
 ZDOT =        -68
055625                 TA   =           41
30190
                                          MA   =           41
28220
                                          Ha   =            223
260  n
mi
                                          Hp   =            217
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5316150
41                 X    =        -1602827
42
 Y    =      -12699477
98  feet           Y    =        -3888823
10  meter
 Z    =       17472689
23                 Z    =         5317846
86
 XDOT =      23092
037773                 XDOT =        7072
280696
 YDOT =      -9981
372215  feet/sec       YDOT =       -2963
424194  meter/sec
 ZDOT =       -223
279608                 ZDOT =         -33
782854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3003422
22                 X    =         -915443
09
 Y    =       13481316
06  feet           Y    =         4109105
13  meter
 Z    =       17437506
63                 Z    =         5314952
02
 XDOT =     -23592
676898                 XDOT =       -7191
047919
 YDOT =      -5161
300687  feet/sec       YDOT =       -1573
164449  meter/sec
 ZDOT =        -67
754455                 ZDOT =         -20
651558


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   19136
80103545  
00016717  00000-0  10270-3 0  9159
2 25544  51
6386 157
1509 0001728 345
1936  14
9165 15
52684175 10379


Satellite: ISS
Catalog Number: 25544
Epoch time:      19136
80103545   =   yrday
fracday
Element set:     915
Inclination:       51
6386  deg
RA of node:       157
1509  deg
Eccentricity:     
0001728     
Arg of perigee:   345
1936  deg
Mean anomaly:      14
9165  deg
Mean motion:   15
52684175  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1037
Checksum:              312


Coasting Arc #17 (Orbit 1051)
---------------------------------------

Vector Time (GMT): 2019/137/18:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         536087
98                 A    =         6782293
90  meter
 Y    =        4356781
56  meter          E    =           
0013445
 Z    =       -5181934
95                 I    =           51
80183
 XDOT =      -7062
303845                 Wp   =           93
81026
 YDOT =       2580
872863  meter/sec      RA   =          151
24834  deg
 ZDOT =       1441
640253                 TA   =          190
03955
                                          MA   =          190
06644
                                          Ha   =            223
358  n
mi
                                          Hp   =            217
041

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1758818
83                 X    =          512500
79
 Y    =       14293902
77  feet           Y    =         4362644
93  meter
 Z    =      -17001098
93                 Z    =        -5179387
80
 XDOT =     -23170
288205                 XDOT =       -7097
641832
 YDOT =       8467
430653  feet/sec       YDOT =        2501
699556  meter/sec
 ZDOT =       4729
790855                 ZDOT =        1407
247920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6605459
32                 X    =         2013344
00
 Y    =      -12812414
39  feet           Y    =        -3905223
91  meter
 Z    =      -16989891
40                 Z    =        -5178518
90
 XDOT =      22956
985897                 XDOT =        6997
289301
 YDOT =       5780
762060  feet/sec       YDOT =        1761
976276  meter/sec
 ZDOT =       4573
735451                 ZDOT =        1394
074566


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   19137
76648324  
00016717  00000-0  10270-3 0  9165
2 25544  51
6391 152
3476 0001770 353
7406   6
3723 15
52654756 10523


Satellite: ISS
Catalog Number: 25544
Epoch time:      19137
76648324   =   yrday
fracday
Element set:     916
Inclination:       51
6391  deg
RA of node:       152
3476  deg
Eccentricity:     
0001770     
Arg of perigee:   353
7406  deg
Mean anomaly:       6
3723  deg
Mean motion:   15
52654756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1052
Checksum:              312
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