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

 
Date: February 22nd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


057/02:24:45 635 -2 8 2 9 2 9
N/A -0 5 0 3 224 4
000/00:07:31 270 -0 6 -0 2 215 6

057/14:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 215 6

060/17:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 224 6
000/00:00:00 000 0 0 0 0 215 5

061/07:48:58 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 215 6

062/10:55:42 000 0 0 0 0 0 0
N/A 0 0 0 0 224 4
000/00:00:00 000 0 0 0 0 215 5

066/23:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 224 6
000/00:00:00 000 0 0 0 0 215 4

067/07:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 5
000/00:00:00 000 0 0 0 0 215 4

Coasting Arc #1 (Orbit 3742)
---------------------------------------

Vector Time (GMT): 2019/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2592687
11                 A    =         6779869
69  meter
 Y    =        3375784
38  meter          E    =           
0019561
 Z    =       -5293898
85                 I    =           51
41968
 XDOT =      -6394
433964                 Wp   =           83
49147
 YDOT =      -4178
001846  meter/sec      RA   =          210
33948  deg
 ZDOT =        471
142403                 TA   =          191
00400
                                          MA   =          191
04685
                                          Ha   =            224
225  n
mi
                                          Hp   =            214
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8506191
31                 X    =        -2604529
04
 Y    =       11075408
07  feet           Y    =         3346724
34  meter
 Z    =      -17368434
56                 Z    =        -5306522
06
 XDOT =     -20979
114054                 XDOT =       -6349
527630
 YDOT =     -13707
355138  feet/sec       YDOT =       -4249
257735  meter/sec
 ZDOT =       1545
742793                 ZDOT =         440
190735

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12685030
65                 X    =        -3866397
34
 Y    =        5667245
38  feet           Y    =         1727376
39  meter
 Z    =      -17425693
70                 Z    =        -5311351
44
 XDOT =     -11384
121267                 XDOT =       -3469
880162
 YDOT =     -21193
947891  feet/sec       YDOT =       -6459
915317  meter/sec
 ZDOT =       1406
311328                 ZDOT =         428
643693


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   19053
51537774  
00016717  00000-0  10270-3 0  9004
2 25544  51
6372 211
4134 0005671  55
5374 304
6313 15
53288374 37433


Satellite: ISS
Catalog Number: 25544
Epoch time:      19053
51537774   =   yrday
fracday
Element set:     900
Inclination:       51
6372  deg
RA of node:       211
4134  deg
Eccentricity:     
0005671     
Arg of perigee:    55
5374  deg
Mean anomaly:     304
6313  deg
Mean motion:   15
53288374  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3743
Checksum:              301


Coasting Arc #2 (Orbit 3758)
---------------------------------------

Vector Time (GMT): 2019/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3809259
31                 A    =         6781258
99  meter
 Y    =       -2581632
60  meter          E    =           
0011688
 Z    =        4974315
73                 I    =           51
45368
 XDOT =       5806
610228                 Wp   =           58
27972
 YDOT =       4569
704580  meter/sec      RA   =          205
33415  deg
 ZDOT =      -2065
369073                 TA   =           51
90566
                                          MA   =           51
80031
                                          Ha   =            224
218  n
mi
                                          Hp   =            214
164

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12497569
91                 X    =         3813682
62
 Y    =       -8469923
23  feet           Y    =        -2539009
57  meter
 Z    =       16319933
50                 Z    =         4992830
43
 XDOT =      19050
558490                 XDOT =        5765
111220
 YDOT =      14992
469094  feet/sec       YDOT =        4634
405910  meter/sec
 ZDOT =      -6776
145254                 ZDOT =       -2037
264386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14907843
67                 X    =         4543910
75
 Y    =       -1715420
20  feet           Y    =         -522860
08  meter
 Z    =       16403737
78                 Z    =         4999859
28
 XDOT =       9776
880469                 XDOT =        2979
993167
 YDOT =      21079
275586  feet/sec       YDOT =        6424
963199  meter/sec
 ZDOT =      -6649
582406                 ZDOT =       -2026
792717


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   19054
54477186  
00016717  00000-0  10270-3 0  9019
2 25544  51
6375 206
2868 0005718  59
3685 300
8030 15
53253893 37590


Satellite: ISS
Catalog Number: 25544
Epoch time:      19054
54477186   =   yrday
fracday
Element set:     901
Inclination:       51
6375  deg
RA of node:       206
2868  deg
Eccentricity:     
0005718     
Arg of perigee:    59
3685  deg
Mean anomaly:     300
8030  deg
Mean motion:   15
53253893  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3759
Checksum:              333


Coasting Arc #3 (Orbit 3773)
---------------------------------------

Vector Time (GMT): 2019/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4898087
10                 A    =         6783766
10  meter
 Y    =        1853250
39  meter          E    =           
0013234
 Z    =       -4323801
26                 I    =           51
49360
 XDOT =      -4873
891156                 Wp   =           92
04229
 YDOT =      -4765
701502  meter/sec      RA   =          200
33818  deg
 ZDOT =       3487
380215                 TA   =          213
50864
                                          MA   =          213
59243
                                          Ha   =            224
282  n
mi
                                          Hp   =            213
961

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16069839
55                 X    =        -4897444
25
 Y    =        6080217
83  feet           Y    =         1798479
80  meter
 Z    =      -14185699
67                 Z    =        -4347592
64
 XDOT =     -15990
456547                 XDOT =       -4837
177058
 YDOT =     -15635
503614  feet/sec       YDOT =       -4819
999186  meter/sec
 ZDOT =      11441
536140                 ZDOT =        3463
794527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16999449
88                 X    =        -5181432
32
 Y    =       -1778632
04  feet           Y    =         -542127
05  meter
 Z    =      -14293286
51                 Z    =        -4356593
73
 XDOT =      -7418
330728                 XDOT =       -2261
107206
 YDOT =     -19960
791821  feet/sec       YDOT =       -6084
049347  meter/sec
 ZDOT =      11335
380242                 ZDOT =        3455
023898


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   19055
50982470  
00016717  00000-0  10270-3 0  9024
2 25544  51
6382 201
4830 0005726  62
0299 298
1432 15
53282347 37743


Satellite: ISS
Catalog Number: 25544
Epoch time:      19055
50982470   =   yrday
fracday
Element set:     902
Inclination:       51
6382  deg
RA of node:       201
4830  deg
Eccentricity:     
0005726     
Arg of perigee:    62
0299  deg
Mean anomaly:     298
1432  deg
Mean motion:   15
53282347  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3774
Checksum:              311


Coasting Arc #4 (Orbit 3789)
---------------------------------------

Vector Time (GMT): 2019/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5804983
42                 A    =         6787056
77  meter
 Y    =       -1136953
81  meter          E    =           
0017832
 Z    =        3314385
42                 I    =           51
53536
 XDOT =       3641
122364                 Wp   =           83
89329
 YDOT =       4860
259273  meter/sec      RA   =          195
34982  deg
 ZDOT =      -4686
429553                 TA   =           57
47711
                                          MA   =           57
30494
                                          Ha   =            224
257  n
mi
                                          Hp   =            214
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19045221
20                 X    =         5801166
46
 Y    =       -3730163
41  feet           Y    =        -1072059
55  meter
 Z    =       10873967
92                 Z    =         3342574
34
 XDOT =      11945
939515                 XDOT =        3609
266773
 YDOT =      15945
732523  feet/sec       YDOT =        4900
798423  meter/sec
 ZDOT =     -15375
425043                 ZDOT =       -4668
820237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18702162
55                 X    =         5700419
15
 Y    =        4906790
83  feet           Y    =         1495589
84  meter
 Z    =       11001375
72                 Z    =         3353219
32
 XDOT =       4258
121224                 XDOT =        1297
875349
 YDOT =      18236
923272  feet/sec       YDOT =        5558
614213  meter/sec
 ZDOT =     -15296
255092                 ZDOT =       -4662
298552


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   19056
53921464  
00016717  00000-0  10270-3 0  9035
2 25544  51
6374 196
3574 0005659  66
5760 293
5987 15
53272150 37901


Satellite: ISS
Catalog Number: 25544
Epoch time:      19056
53921464   =   yrday
fracday
Element set:     903
Inclination:       51
6374  deg
RA of node:       196
3574  deg
Eccentricity:     
0005659     
Arg of perigee:    66
5760  deg
Mean anomaly:     293
5987  deg
Mean motion:   15
53272150  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3790
Checksum:              340


Coasting Arc #5 (Orbit 3798)
---------------------------------------

Vector Time (GMT): 2019/057/02:28:31
270
Vector Time (MET): N/A
Weight (LBS)     : 900442
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1603454
85                 A    =         6781502
45  meter
 Y    =        3950284
39  meter          E    =           
0017613
 Z    =       -5288949
98                 I    =           51
53297
 XDOT =      -7324
984425                 Wp   =           86
84043
 YDOT =      -2124
289312  meter/sec      RA   =          192
36835  deg
 ZDOT =        636
888559                 TA   =          189
24450
                                          MA   =          189
27696
                                          Ha   =            224
368  n
mi
                                          Hp   =            215
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5260678
66                 X    =        -1621818
40
 Y    =       12960250
62  feet           Y    =         3932250
46  meter
 Z    =      -17352198
11                 Z    =        -5296783
70
 XDOT =     -24032
101131                 XDOT =       -7303
779231
 YDOT =      -6969
453124  feet/sec       YDOT =       -2206
083803  meter/sec
 ZDOT =       2089
529393                 ZDOT =         601
358580

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2361082
90                 X    =          719658
07
 Y    =      -13741487
72  feet           Y    =        -4188405
46  meter
 Z    =      -17387881
35                 Z    =        -5299826
24
 XDOT =      23963
921331                 XDOT =        7304
203222
 YDOT =       1687
938516  feet/sec       YDOT =         514
483660  meter/sec
 ZDOT =       1929
196747                 ZDOT =         588
019168


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   19057
11824695  
00016717  00000-0  10270-3 0  9049
2 25544  51
6395 193
4802 0003722  52
2544 307
8945 15
52745985 37999


Satellite: ISS
Catalog Number: 25544
Epoch time:      19057
11824695   =   yrday
fracday
Element set:     904
Inclination:       51
6395  deg
RA of node:       193
4802  deg
Eccentricity:     
0003722     
Arg of perigee:    52
2544  deg
Mean anomaly:     307
8945  deg
Mean motion:   15
52745985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3799
Checksum:              342


Coasting Arc #6 (Orbit 3806)
---------------------------------------

Vector Time (GMT): 2019/057/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900442
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2325386
13                 A    =         6782008
95  meter
 Y    =        3756277
67  meter          E    =           
0016504
 Z    =       -5160214
82                 I    =           51
55234
 XDOT =      -7118
137871                 Wp   =           93
21902
 YDOT =      -2404
642174  meter/sec      RA   =          189
78826  deg
 ZDOT =       1460
426644                 TA   =          190
86413
                                          MA   =          190
89982
                                          Ha   =            224
285  n
mi
                                          Hp   =            215
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7629219
59                 X    =        -2342151
93
 Y    =       12323745
65  feet           Y    =         3730179
58  meter
 Z    =      -16929838
66                 Z    =        -5171551
44
 XDOT =     -23353
470706                 XDOT =       -7097
813303
 YDOT =      -7889
245977  feet/sec       YDOT =       -2484
128447  meter/sec
 ZDOT =       4791
425998                 ZDOT =        1425
899330

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3271099
98                 X    =         -997031
27
 Y    =       14058212
95  feet           Y    =         4284943
31  meter
 Z    =      -16981333
55                 Z    =        -5175910
47
 XDOT =     -23654
189287                 XDOT =       -7209
796895
 YDOT =         83
198352  feet/sec       YDOT =          25
358858  meter/sec
 ZDOT =       4635
631928                 ZDOT =        1412
940612


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   19057
63312079  
00016717  00000-0  10270-3 0  9055
2 25544  51
6401 190
9166 0003410  58
3581 301
7904 15
52759016 38072


Satellite: ISS
Catalog Number: 25544
Epoch time:      19057
63312079   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:       190
9166  deg
Eccentricity:     
0003410     
Arg of perigee:    58
3581  deg
Mean anomaly:     301
7904  deg
Mean motion:   15
52759016  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3807
Checksum:              301


Coasting Arc #7 (Orbit 3822)
---------------------------------------

Vector Time (GMT): 2019/058/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900442
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3464741
12                 A    =         6783801
76  meter
 Y    =       -3447060
26  meter          E    =           
0011284
 Z    =        4698326
50                 I    =           51
59194
 XDOT =       6577
344776                 Wp   =           62
42359
 YDOT =       2780
310098  meter/sec      RA   =          184
80055  deg
 ZDOT =      -2800
280660                 TA   =           55
39807
                                          MA   =           55
29169
                                          Ha   =            224
200  n
mi
                                          Hp   =            215
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11367260
90                 X    =         3480208
11
 Y    =      -11309252
81  feet           Y    =        -3408228
41  meter
 Z    =       15414457
03                 Z    =         4715194
37
 XDOT =      21579
215144                 XDOT =        6559
367725
 YDOT =       9121
752289  feet/sec       YDOT =        2853
761922  meter/sec
 ZDOT =      -9187
272506                 ZDOT =       -2768
374660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6901680
45                 X    =         2103632
20
 Y    =      -14391571
14  feet           Y    =        -4386550
88  meter
 Z    =       15490926
12                 Z    =         4721634
28
 XDOT =      22388
405081                 XDOT =        6823
985869
 YDOT =        966
438547  feet/sec       YDOT =         294
570469  meter/sec
 ZDOT =      -9043
326326                 ZDOT =       -2756
405864


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   19058
66286881  
00016717  00000-0  10270-3 0  9061
2 25544  51
6405 185
7934 0003473  60
0172 300
1324 15
52778871 38233


Satellite: ISS
Catalog Number: 25544
Epoch time:      19058
66286881   =   yrday
fracday
Element set:     906
Inclination:       51
6405  deg
RA of node:       185
7934  deg
Eccentricity:     
0003473     
Arg of perigee:    60
0172  deg
Mean anomaly:     300
1324  deg
Mean motion:   15
52778871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3823
Checksum:              318


Coasting Arc #8 (Orbit 3837)
---------------------------------------

Vector Time (GMT): 2019/059/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900442
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4468530
71                 A    =         6786387
98  meter
 Y    =        3183321
83  meter          E    =           
0009953
 Z    =       -4003423
36                 I    =           51
63256
 XDOT =      -5763
895595                 Wp   =           94
70254
 YDOT =      -3118
360471  meter/sec      RA   =          179
82133  deg
 ZDOT =       3961
672231                 TA   =          216
55064
                                          MA   =          216
61860
                                          Ha   =            224
322  n
mi
                                          Hp   =            215
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14660533
81                 X    =        -4484349
35
 Y    =       10443969
25  feet           Y    =         3133262
97  meter
 Z    =      -13134591
06                 Z    =        -4025167
97
 XDOT =     -18910
418618                 XDOT =       -5747
840079
 YDOT =     -10230
841440  feet/sec       YDOT =       -3182
726433  meter/sec
 ZDOT =      12997
612305                 ZDOT =        3933
713029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10056483
18                 X    =        -3065216
07
 Y    =       14841757
21  feet           Y    =         4523767
60  meter
 Z    =      -13233087
95                 Z    =        -4033445
21
 XDOT =     -20281
391116                 XDOT =       -6181
768012
 YDOT =      -2288
261123  feet/sec       YDOT =        -697
461990  meter/sec
 ZDOT =      12871
503423                 ZDOT =        3923
234243


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   19059
62825756  
00016717  00000-0  10270-3 0  9079
2 25544  51
6392 180
9920 0003522  65
7271 294
4249 15
52775303 38381


Satellite: ISS
Catalog Number: 25544
Epoch time:      19059
62825756   =   yrday
fracday
Element set:     907
Inclination:       51
6392  deg
RA of node:       180
9920  deg
Eccentricity:     
0003522     
Arg of perigee:    65
7271  deg
Mean anomaly:     294
4249  deg
Mean motion:   15
52775303  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3838
Checksum:              334


Coasting Arc #9 (Orbit 3853)
---------------------------------------

Vector Time (GMT): 2019/060/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900442
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5323695
45                 A    =         6789243
40  meter
 Y    =       -2896893
73  meter          E    =           
0016179
 Z    =        3045411
55                 I    =           51
67582
 XDOT =       4729
636705                 Wp   =           90
04112
 YDOT =       3485
835869  meter/sec      RA   =          174
84879  deg
 ZDOT =      -4929
425840                 TA   =           55
04781
                                          MA   =           54
89596
                                          Ha   =            224
288  n
mi
                                          Hp   =            215
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17466192
43                 X    =         5340901
06
 Y    =       -9504244
53  feet           Y    =        -2837264
10  meter
 Z    =        9991507
70                 Z    =         3071313
46
 XDOT =      15517
180792                 XDOT =        4714
249505
 YDOT =      11436
469388  feet/sec       YDOT =        3538
639692  meter/sec
 ZDOT =     -16172
656957                 ZDOT =       -4906
489063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12774675
27                 X    =         3893721
02
 Y    =      -15160768
12  feet           Y    =        -4621002
12  meter
 Z    =       10108785
77                 Z    =         3081157
90
 XDOT =      17600
689236                 XDOT =        5364
690079
 YDOT =       4067
116231  feet/sec       YDOT =        1239
657027  meter/sec
 ZDOT =     -16069
253972                 ZDOT =       -4897
908611


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   19060
65800239  
00016717  00000-0  10270-3 0  9084
2 25544  51
6397 175
8691 0003518  66
7046 293
4476 15
52776927 38542


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
65800239   =   yrday
fracday
Element set:     908
Inclination:       51
6397  deg
RA of node:       175
8691  deg
Eccentricity:     
0003518     
Arg of perigee:    66
7046  deg
Mean anomaly:     293
4476  deg
Mean motion:   15
52776927  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3854
Checksum:              350


Coasting Arc #10 (Orbit 3855)
---------------------------------------

Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900442
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6110272
52                 A    =         6790686
86  meter
 Y    =       -1436470
03  meter          E    =           
0017610
 Z    =        2569129
74                 I    =           51
68254
 XDOT =       3284
769491                 Wp   =           74
26141
 YDOT =      -4506
991193  meter/sec      RA   =          174
35780  deg
 ZDOT =       5266
971822                 TA   =          314
60716
                                          MA   =          314
75069
                                          Ha   =            224
650  n
mi
                                          Hp   =            215
533

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20046825
86                 X    =        -6106234
53
 Y    =       -4712828
17  feet           Y    =        -1504776
65  meter
 Z    =        8428903
35                 Z    =         2539458
84
 XDOT =      10776
802792                 XDOT =        3309
340327
 YDOT =     -14786
716511  feet/sec       YDOT =       -4470
120955  meter/sec
 ZDOT =      17280
091280                 ZDOT =        5282
987568

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14074560
78                 X    =        -4289926
13
 Y    =       15107401
26  feet           Y    =         4604735
90  meter
 Z    =        8294911
33                 Z    =         2528288
97
 XDOT =      -6436
158286                 XDOT =       -1961
741045
 YDOT =     -15570
337372  feet/sec       YDOT =       -4745
838831  meter/sec
 ZDOT =      17352
809708                 ZDOT =        5289
136399


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   19060
78672222  
00016717  00000-0  10270-3 0  9098
2 25544  51
6388 175
2293 0003977  67
0908 293
0664 15
52732892 38564


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
78672222   =   yrday
fracday
Element set:     909
Inclination:       51
6388  deg
RA of node:       175
2293  deg
Eccentricity:     
0003977     
Arg of perigee:    67
0908  deg
Mean anomaly:     293
0664  deg
Mean motion:   15
52732892  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3856
Checksum:              346


Coasting Arc #11 (Orbit 3864)
---------------------------------------

Vector Time (GMT): 2019/061/07:48:58
000
Vector Time (MET): N/A
Weight (LBS)     : 900442
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4333015
44                 A    =         6787339
11  meter
 Y    =       -3643813
20  meter          E    =           
0015005
 Z    =        3733073
46                 I    =           51
68963
 XDOT =       5836
024594                 Wp   =           80
61762
 YDOT =       2533
810745  meter/sec      RA   =          171
33353  deg
 ZDOT =      -4283
629948                 TA   =           54
83080
                                          MA   =           54
69033
                                          Ha   =            224
331  n
mi
                                          Hp   =            215
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14215929
91                 X    =         4355306
76
 Y    =      -11954767
72  feet           Y    =        -3595233
54  meter
 Z    =       12247616
34                 Z    =         3754175
50
 XDOT =      19147
062316                 XDOT =        5828
064097
 YDOT =       8313
027380  feet/sec       YDOT =        2599
028495  meter/sec
 ZDOT =     -14053
904030                 ZDOT =       -4255
300841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13405043
11                 X    =         4085857
14
 Y    =       12765650
93  feet           Y    =         3890970
40  meter
 Z    =       12343266
02                 Z    =         3762227
48
 XDOT =      -5263
067952                 XDOT =       -1604
183112
 YDOT =      19045
695730  feet/sec       YDOT =        5805
128058  meter/sec
 ZDOT =     -13926
046029                 ZDOT =       -4244
658830


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   19061
36595064  
00016717  00000-0  10270-3 0  9103
2 25544  51
6368 172
3447 0003524  68
9073 291
2455 15
52751573 38657


Satellite: ISS
Catalog Number: 25544
Epoch time:      19061
36595064   =   yrday
fracday
Element set:     910
Inclination:       51
6368  deg
RA of node:       172
3447  deg
Eccentricity:     
0003524     
Arg of perigee:    68
9073  deg
Mean anomaly:     291
2455  deg
Mean motion:   15
52751573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3865
Checksum:              324


Coasting Arc #12 (Orbit 3879)
---------------------------------------

Vector Time (GMT): 2019/062/07:48:58
000
Vector Time (MET): N/A
Weight (LBS)     : 900442
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5135031
12                 A    =         6789991
48  meter
 Y    =        3484218
91  meter          E    =           
0008441
 Z    =       -2757995
61                 I    =           51
73197
 XDOT =      -4803
587223                 Wp   =           66
93301
 YDOT =      -3015
332647  meter/sec      RA   =          166
36621  deg
 ZDOT =       5150
107780                 TA   =          261
91620
                                          MA   =          262
01198
                                          Ha   =            224
465  n
mi
                                          Hp   =            215
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16847214
97                 X    =        -5160214
51
 Y    =       11431164
42  feet           Y    =         3426654
40  meter
 Z    =       -9048542
03                 Z    =        -2783000
49
 XDOT =     -15759
800599                 XDOT =       -4794
527689
 YDOT =      -9892
823644  feet/sec       YDOT =       -3068
998695  meter/sec
 ZDOT =      16896
679068                 ZDOT =        5126
796521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13434031
72                 X    =        -4094692
87
 Y    =      -15230359
76  feet           Y    =        -4642213
66  meter
 Z    =       -9161834
88                 Z    =        -2792527
27
 XDOT =       6725
169704                 XDOT =        2049
831726
 YDOT =     -16002
198106  feet/sec       YDOT =       -4877
469983  meter/sec
 ZDOT =      16791
521439                 ZDOT =        5118
055735


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   19062
33133280  
00016717  00000-0  10270-3 0  9110
2 25544  51
6374 167
5419 0003782  74
9672 285
1898 15
52764949 38808


Satellite: ISS
Catalog Number: 25544
Epoch time:      19062
33133280   =   yrday
fracday
Element set:     911
Inclination:       51
6374  deg
RA of node:       167
5419  deg
Eccentricity:     
0003782     
Arg of perigee:    74
9672  deg
Mean anomaly:     285
1898  deg
Mean motion:   15
52764949  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3880
Checksum:              342


Coasting Arc #13 (Orbit 3881)
---------------------------------------

Vector Time (GMT): 2019/062/10:55:42
000
Vector Time (MET): N/A
Weight (LBS)     : 935659
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5473692
83                 A    =         6790999
95  meter
 Y    =        3280660
94  meter          E    =           
0009059
 Z    =       -2320287
89                 I    =           51
74211
 XDOT =      -4279
074916                 Wp   =           57
45424
 YDOT =      -3320
892171  meter/sec      RA   =          165
72502  deg
 ZDOT =       5419
337191                 TA   =          276
74978
                                          MA   =          276
85286
                                          Ha   =            224
446  n
mi
                                          Hp   =            215
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17958309
80                 X    =        -5498700
89
 Y    =       10763323
29  feet           Y    =         3219310
28  meter
 Z    =       -7612493
07                 Z    =        -2346937
39
 XDOT =     -14038
959699                 XDOT =       -4267
945247
 YDOT =     -10895
315522  feet/sec       YDOT =       -3368
681151  meter/sec
 ZDOT =      17779
977662                 ZDOT =        5398
578814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20812387
22                 X    =        -6343615
62
 Y    =       -1828144
16  feet           Y    =         -557218
34  meter
 Z    =       -7733207
42                 Z    =        -2357081
62
 XDOT =      -5175
437841                 XDOT =       -1577
473454
 YDOT =     -15619
920147  feet/sec       YDOT =       -4760
951661  meter/sec
 ZDOT =      17686
381249                 ZDOT =        5390
809005


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   19062
46005007  
00016717  00000-0  10270-3 0  9120
2 25544  51
6402 166
9021 0003648  74
7357 285
4198 15
52744072 38824


Satellite: ISS
Catalog Number: 25544
Epoch time:      19062
46005007   =   yrday
fracday
Element set:     912
Inclination:       51
6402  deg
RA of node:       166
9021  deg
Eccentricity:     
0003648     
Arg of perigee:    74
7357  deg
Mean anomaly:     285
4198  deg
Mean motion:   15
52744072  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3882
Checksum:              308


Coasting Arc #14 (Orbit 3897)
---------------------------------------

Vector Time (GMT): 2019/063/10:55:42
000
Vector Time (MET): N/A
Weight (LBS)     : 935659
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5985057
68                 A    =         6792778
31  meter
 Y    =       -3003936
40  meter          E    =           
0016544
 Z    =        1098163
94                 I    =           51
77968
 XDOT =       3029
427356                 Wp   =          114
79621
 YDOT =       3858
428278  meter/sec      RA   =          160
76755  deg
 ZDOT =      -5893
341438                 TA   =           53
31684
                                          MA   =           53
16492
                                          Ha   =            224
463  n
mi
                                          Hp   =            215
487

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19636016
02                 X    =         6012869
59
 Y    =       -9855434
39  feet           Y    =        -2936851
70  meter
 Z    =        3602900
08                 Z    =         1127304
24
 XDOT =       9939
066128                 XDOT =        3014
682081
 YDOT =      12658
885428  feet/sec       YDOT =        3892
222482  meter/sec
 ZDOT =     -19335
109706                 ZDOT =       -5878
662118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21715149
81                 X    =         6618777
66
 Y    =        3191648
09  feet           Y    =          972814
34  meter
 Z    =        3734869
82                 Z    =         1138388
32
 XDOT =       1208
250894                 XDOT =         368
274872
 YDOT =      14560
605507  feet/sec       YDOT =        4438
072559  meter/sec
 ZDOT =     -19269
024855                 ZDOT =       -5873
198776


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   19063
48978802  
00016717  00000-0  10270-3 0  9136
2 25544  51
6398 161
7796 0003603  81
5799 278
5761 15
52755417 38988


Satellite: ISS
Catalog Number: 25544
Epoch time:      19063
48978802   =   yrday
fracday
Element set:     913
Inclination:       51
6398  deg
RA of node:       161
7796  deg
Eccentricity:     
0003603     
Arg of perigee:    81
5799  deg
Mean anomaly:     278
5761  deg
Mean motion:   15
52755417  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3898
Checksum:              368


Coasting Arc #15 (Orbit 3913)
---------------------------------------

Vector Time (GMT): 2019/064/10:55:42
000
Vector Time (MET): N/A
Weight (LBS)     : 935659
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6233842
44                 A    =         6793286
41  meter
 Y    =        2680258
66  meter          E    =           
0015414
 Z    =         138542
58                 I    =           51
81404
 XDOT =      -1750
906242                 Wp   =           54
86539
 YDOT =      -4407
704265  meter/sec      RA   =          155
81444  deg
 ZDOT =       6024
145054                 TA   =          306
62276
                                          MA   =          306
76442
                                          Ha   =            224
463  n
mi
                                          Hp   =            215
496

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20452238
97                 X    =        -6264023
49
 Y    =        8793499
54  feet           Y    =         2610378
74  meter
 Z    =         454536
03                 Z    =          108188
00
 XDOT =      -5744
443052                 XDOT =       -1730
749227
 YDOT =     -14460
971997  feet/sec       YDOT =       -4427
170790  meter/sec
 ZDOT =      19764
255425                 ZDOT =        6015
689411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21871008
32                 X    =        -6666283
34
 Y    =       -4169504
59  feet           Y    =        -1270865
00  meter
 Z    =         317084
81                 Z    =           96647
45
 XDOT =       2924
789441                 XDOT =         891
475822
 YDOT =     -13675
703246  feet/sec       YDOT =       -4168
354350  meter/sec
 ZDOT =      19726
344886                 ZDOT =        6012
589921


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   19064
51952261  
00016717  00000-0  10270-3 0  9143
2 25544  51
6414 156
6573 0003665  82
2593 277
8975 15
52767513 39149


Satellite: ISS
Catalog Number: 25544
Epoch time:      19064
51952261   =   yrday
fracday
Element set:     914
Inclination:       51
6414  deg
RA of node:       156
6573  deg
Eccentricity:     
0003665     
Arg of perigee:    82
2593  deg
Mean anomaly:     277
8975  deg
Mean motion:   15
52767513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3914
Checksum:              336


Coasting Arc #16 (Orbit 3928)
---------------------------------------

Vector Time (GMT): 2019/065/10:55:42
000
Vector Time (MET): N/A
Weight (LBS)     : 935659
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6260229
38                 A    =         6792466
75  meter
 Y    =       -2211685
64  meter          E    =           
0011124
 Z    =       -1420593
16                 I    =           51
84076
 XDOT =        448
444440                 Wp   =          126
80253
 YDOT =       4976
973338  meter/sec      RA   =          150
86324  deg
 ZDOT =      -5810
258530                 TA   =           68
62933
                                          MA   =           68
51067
                                          Ha   =            224
515  n
mi
                                          Hp   =            215
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20538810
30                 X    =         6291396
12
 Y    =       -7256186
47  feet           Y    =        -2141505
28  meter
 Z    =       -4660738
71                 Z    =        -1390107
95
 XDOT =       1471
274409                 XDOT =         420
979652
 YDOT =      16328
652683  feet/sec       YDOT =        4981
833914  meter/sec
 ZDOT =     -19062
527986                 ZDOT =       -5808
147484

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21196907
93                 X    =         6460817
54
 Y    =        5143304
37  feet           Y    =         1567679
17  meter
 Z    =       -4522717
11                 Z    =        -1378524
17
 XDOT =      -7194
558317                 XDOT =       -2192
901375
 YDOT =      13009
035209  feet/sec       YDOT =        3965
153932  meter/sec
 ZDOT =     -19053
347779                 ZDOT =       -5807
460403


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   19065
48489564  
00016717  00000-0  10270-3 0  9152
2 25544  51
6410 151
8551 0003679  86
2280 273
9293 15
52771899 39298


Satellite: ISS
Catalog Number: 25544
Epoch time:      19065
48489564   =   yrday
fracday
Element set:     915
Inclination:       51
6410  deg
RA of node:       151
8551  deg
Eccentricity:     
0003679     
Arg of perigee:    86
2280  deg
Mean anomaly:     273
9293  deg
Mean motion:   15
52771899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3929
Checksum:              354


Coasting Arc #17 (Orbit 3944)
---------------------------------------

Vector Time (GMT): 2019/066/10:55:42
000
Vector Time (MET): N/A
Weight (LBS)     : 935659
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6053060
72                 A    =         6790522
26  meter
 Y    =        1655952
38  meter          E    =           
0017317
 Z    =        2574279
06                 I    =           51
86290
 XDOT =        748
867974                 Wp   =           78
94567
 YDOT =      -5512
659951  meter/sec      RA   =          145
91126  deg
 ZDOT =       5280
161616                 TA   =          309
90463
                                          MA   =          310
05673
                                          Ha   =            224
541  n
mi
                                          Hp   =            215
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19859123
08                 X    =        -6083632
39
 Y    =        5432914
65  feet           Y    =         1588092
21  meter
 Z    =        8445797
45                 Z    =         2544801
58
 XDOT =       2456
915924                 XDOT =         784
808751
 YDOT =     -18086
154694  feet/sec       YDOT =       -5504
083968  meter/sec
 ZDOT =      17323
364882                 ZDOT =        5283
887259

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19759496
50                 X    =        -6022694
53
 Y    =       -5974928
82  feet           Y    =        -1821158
30  meter
 Z    =        8312361
26                 Z    =         2533607
71
 XDOT =      11154
028249                 XDOT =        3399
747810
 YDOT =     -12638
369660  feet/sec       YDOT =       -3852
175072  meter/sec
 ZDOT =      17340
623096                 ZDOT =        5285
421920


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   19066
51462456  
00016717  00000-0  10270-3 0  9169
2 25544  51
6411 146
7330 0003721  88
6548 271
5030 15
52785578 39458


Satellite: ISS
Catalog Number: 25544
Epoch time:      19066
51462456   =   yrday
fracday
Element set:     916
Inclination:       51
6411  deg
RA of node:       146
7330  deg
Eccentricity:     
0003721     
Arg of perigee:    88
6548  deg
Mean anomaly:     271
5030  deg
Mean motion:   15
52785578  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3945
Checksum:              321


Coasting Arc #18 (Orbit 3952)
---------------------------------------

Vector Time (GMT): 2019/066/23:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 935659
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4261207
21                 A    =         6782788
05  meter
 Y    =       -1709399
97  meter          E    =           
0009550
 Z    =        4985818
08                 I    =           51
85081
 XDOT =       4757
264624                 Wp   =          108
71087
 YDOT =      -5629
077804  meter/sec      RA   =          143
32062  deg
 ZDOT =       2129
607948                 TA   =          320
58383
                                          MA   =          320
65328
                                          Ha   =            224
619  n
mi
                                          Hp   =            215
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13980338
61                 X    =        -4265993
52
 Y    =       -5608267
62  feet           Y    =        -1757077
90  meter
 Z    =       16357670
88                 Z    =         4965107
62
 XDOT =      15607
823570                 XDOT =        4809
512687
 YDOT =     -18468
103032  feet/sec       YDOT =       -5575
586336  meter/sec
 ZDOT =       6986
902717                 ZDOT =        2152
844249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10662396
78                 X    =         3249898
54
 Y    =       10782730
87  feet           Y    =         3286576
37  meter
 Z    =       16264130
47                 Z    =         4957306
97
 XDOT =     -20870
289846                 XDOT =       -6361
264345
 YDOT =       9908
085360  feet/sec       YDOT =        3019
984418  meter/sec
 ZDOT =       7092
414462                 ZDOT =        2161
767928


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   19067
02948932  
00016717  00000-0  10270-3 0  9175
2 25544  51
6404 144
1749 0003777  84
1787 275
9795 15
52792346 39539


Satellite: ISS
Catalog Number: 25544
Epoch time:      19067
02948932   =   yrday
fracday
Element set:     917
Inclination:       51
6404  deg
RA of node:       144
1749  deg
Eccentricity:     
0003777     
Arg of perigee:    84
1787  deg
Mean anomaly:     275
9795  deg
Mean motion:   15
52792346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3953
Checksum:              358


Coasting Arc #19 (Orbit 3957)
---------------------------------------

Vector Time (GMT): 2019/067/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910211
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5923830
40                 A    =         6790794
53  meter
 Y    =        2251877
10  meter          E    =           
0017364
 Z    =        2418982
55                 I    =           51
88379
 XDOT =        127
552165                 Wp   =           78
04472
 YDOT =      -5469
658333  meter/sec      RA   =          141
76081  deg
 ZDOT =       5375
142061                 TA   =          308
90811
                                          MA   =          309
06282
                                          Ha   =            224
516  n
mi
                                          Hp   =            215
419

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19435139
11                 X    =        -5960321
19
 Y    =        7388048
24  feet           Y    =         2185428
96  meter
 Z    =        7936294
46                 Z    =         2390118
25
 XDOT =        418
478233                 XDOT =         162
596822
 YDOT =     -17945
073270  feet/sec       YDOT =       -5468
035321  meter/sec
 ZDOT =      17634
980516                 ZDOT =        5375
847469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7325356
14                 X    =        -2232768
55
 Y    =      -19511657
70  feet           Y    =        -5947153
27  meter
 Z    =        7805576
85                 Z    =         2379139
82
 XDOT =      16520
017925                 XDOT =        5035
301464
 YDOT =        892
806500  feet/sec       YDOT =         272
127421  meter/sec
 ZDOT =      17638
580824                 ZDOT =        5376
239435


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   19067
35127831  
00016717  00000-0  10270-3 0  9189
2 25544  51
6382 142
5691 0003748  92
9767 267
1814 15
52802577 39583


Satellite: ISS
Catalog Number: 25544
Epoch time:      19067
35127831   =   yrday
fracday
Element set:     918
Inclination:       51
6382  deg
RA of node:       142
5691  deg
Eccentricity:     
0003748     
Arg of perigee:    92
9767  deg
Mean anomaly:     267
1814  deg
Mean motion:   15
52802577  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3958
Checksum:              346


Coasting Arc #20 (Orbit 3972)
---------------------------------------

Vector Time (GMT): 2019/068/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910211
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5621035
75                 A    =         6788159
40  meter
 Y    =       -1514313
34  meter          E    =           
0008761
 Z    =       -3498816
65                 I    =           51
90072
 XDOT =      -1205
623406                 Wp   =           90
95935
 YDOT =       6034
741489  meter/sec      RA   =          136
80698  deg
 ZDOT =      -4558
772167                 TA   =          129
93066
                                          MA   =          129
85364
                                          Ha   =            224
530  n
mi
                                          Hp   =            215
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18441718
35                 X    =         5654546
64
 Y    =       -4968219
63  feet           Y    =        -1451268
06  meter
 Z    =      -11479057
26                 Z    =        -3471430
43
 XDOT =      -3955
457368                 XDOT =       -1250
872192
 YDOT =      19799
020634  feet/sec       YDOT =        6021
005792  meter/sec
 ZDOT =     -14956
601597                 ZDOT =       -4564
739239

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5227004
93                 X    =         1593191
10
 Y    =       18446944
69  feet           Y    =         5622628
74  meter
 Z    =      -11355068
85                 Z    =        -3461024
99
 XDOT =     -18504
741822                 XDOT =       -5640
245307
 YDOT =      -3959
690481  feet/sec       YDOT =       -1206
913659  meter/sec
 ZDOT =     -14984
051851                 ZDOT =       -4567
139004


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   19068
31664588  
00016717  00000-0  10270-3 0  9192
2 25544  51
6386 137
7660 0003805  94
0765 266
0822 15
52788645 39737


Satellite: ISS
Catalog Number: 25544
Epoch time:      19068
31664588   =   yrday
fracday
Element set:     919
Inclination:       51
6386  deg
RA of node:       137
7660  deg
Eccentricity:     
0003805     
Arg of perigee:    94
0765  deg
Mean anomaly:     266
0822  deg
Mean motion:   15
52788645  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3973
Checksum:              353
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