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

 
Date: February 27th 2019

ISS TRAJECTORY DATA

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


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

062/11:00:00 000 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 3820)
---------------------------------------

Vector Time (GMT): 2019/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6718887
75                 A    =         6792940
41  meter
 Y    =        -121820
32  meter          E    =           
0015511
 Z    =         951842
02                 I    =           51
61646
 XDOT =        934
310663                 Wp   =          113
49067
 YDOT =       4791
867796  meter/sec      RA   =          185
40337  deg
 ZDOT =      -5911
451862                 TA   =           56
20298
                                          MA   =           56
05537
                                          Ha   =            224
354  n
mi
                                          Hp   =            215
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22043594
97                 X    =         6715127
17
 Y    =        -399672
98  feet           Y    =          -46706
01  meter
 Z    =        3122841
28                 Z    =          984470
24
 XDOT =       3065
323697                 XDOT =         909
371325
 YDOT =      15721
351037  feet/sec       YDOT =        4802
176203  meter/sec
 ZDOT =     -19394
527105                 ZDOT =       -5906
974184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20303051
27                 X    =         6188370
03
 Y    =        8539521
59  feet           Y    =         2602846
18  meter
 Z    =        3270265
33                 Z    =          996776
87
 XDOT =      -2811
661611                 XDOT =        -856
994459
 YDOT =      14188
956529  feet/sec       YDOT =        4324
793950  meter/sec
 ZDOT =     -19374
656011                 ZDOT =       -5905
395152


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
53416106  
00016717  00000-0  10270-3 0  9006
2 25544  51
6388 186
4305 0003449  63
4578 296
6927 15
52743321 38211


Satellite: ISS
Catalog Number: 25544
Epoch time:      19058
53416106   =   yrday
fracday
Element set:     900
Inclination:       51
6388  deg
RA of node:       186
4305  deg
Eccentricity:     
0003449     
Arg of perigee:    63
4578  deg
Mean anomaly:     296
6927  deg
Mean motion:   15
52743321  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3821
Checksum:              321


Coasting Arc #2 (Orbit 3836)
---------------------------------------

Vector Time (GMT): 2019/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6775063
91                 A    =         6793345
54  meter
 Y    =        -272620
46  meter          E    =           
0015939
 Z    =         278912
94                 I    =           51
65125
 XDOT =        447
515819                 Wp   =           52
34559
 YDOT =      -4747
413149  meter/sec      RA   =          180
43938  deg
 ZDOT =       6004
925164                 TA   =          310
65844
                                          MA   =          310
79689
                                          Ha   =            224
406  n
mi
                                          Hp   =            215
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22227899
97                 X    =        -6772866
64
 Y    =        -894424
08  feet           Y    =         -348371
66  meter
 Z    =         915068
70                 Z    =          246008
16
 XDOT =       1468
227751                 XDOT =         471
401403
 YDOT =     -15575
502457  feet/sec       YDOT =       -4742
274901  meter/sec
 ZDOT =      19701
198046                 ZDOT =        6007
157208

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20138912
13                 X    =        -6138340
42
 Y    =       -9463283
15  feet           Y    =        -2884408
70  meter
 Z    =         766402
13                 Z    =          233599
37
 XDOT =       6592
894910                 XDOT =        2009
514368
 YDOT =     -12362
530242  feet/sec       YDOT =       -3768
099218  meter/sec
 ZDOT =      19711
638459                 ZDOT =        6008
107402


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
56391281  
00016717  00000-0  10270-3 0  9017
2 25544  51
6391 181
3083 0003560  66
6629 293
4897 15
52741033 38374


Satellite: ISS
Catalog Number: 25544
Epoch time:      19059
56391281   =   yrday
fracday
Element set:     901
Inclination:       51
6391  deg
RA of node:       181
3083  deg
Eccentricity:     
0003560     
Arg of perigee:    66
6629  deg
Mean anomaly:     293
4897  deg
Mean motion:   15
52741033  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3837
Checksum:              325


Coasting Arc #3 (Orbit 3851)
---------------------------------------

Vector Time (GMT): 2019/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6574599
13                 A    =         6792356
44  meter
 Y    =         704886
29  meter          E    =           
0009922
 Z    =       -1545234
49                 I    =           51
68157
 XDOT =      -1849
965801                 Wp   =          123
39639
 YDOT =       4708
741751  meter/sec      RA   =          175
47699  deg
 ZDOT =      -5755
201407                 TA   =           73
46410
                                          MA   =           73
35512
                                          Ha   =            224
414  n
mi
                                          Hp   =            215
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21570207
12                 X    =         6573734
00
 Y    =        2312619
07  feet           Y    =          778403
14  meter
 Z    =       -5069666
98                 Z    =        -1513300
35
 XDOT =      -6069
441604                 XDOT =       -1874
527792
 YDOT =      15448
627793  feet/sec       YDOT =        4687
916527  meter/sec
 ZDOT =     -18881
894381                 ZDOT =       -5764
247546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19185805
43                 X    =         5847833
49
 Y    =       10196514
24  feet           Y    =         3107897
54  meter
 Z    =       -4925396
73                 Z    =        -1501260
92
 XDOT =     -10527
942539                 XDOT =       -3208
916886
 YDOT =      10720
893421  feet/sec       YDOT =        3267
728315  meter/sec
 ZDOT =     -18923
127394                 ZDOT =       -5767
769230


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
52930132  
00016717  00000-0  10270-3 0  9020
2 25544  51
6394 176
5059 0003472  70
5348 289
6179 15
52758268 38525


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
52930132   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:       176
5059  deg
Eccentricity:     
0003472     
Arg of perigee:    70
5348  deg
Mean anomaly:     289
6179  deg
Mean motion:   15
52758268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3852
Checksum:              329


Coasting Arc #4 (Orbit 3855)
---------------------------------------

Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6114897
17                 A    =         6790711
32  meter
 Y    =       -1430029
49  meter          E    =           
0017591
 Z    =        2561759
25                 I    =           51
68256
 XDOT =       3273
709606                 Wp   =           74
07242
 YDOT =      -4509
635379  meter/sec      RA   =          174
35656  deg
 ZDOT =       5271
581189                 TA   =          314
70547
                                          MA   =          314
84860
                                          Ha   =            224
644  n
mi
                                          Hp   =            215
550

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20061998
58                 X    =        -6110895
05
 Y    =       -4691697
79  feet           Y    =        -1498388
03  meter
 Z    =        8404721
94                 Z    =         2532065
79
 XDOT =      10740
517079                 XDOT =        3298
288442
 YDOT =     -14795
391664  feet/sec       YDOT =       -4472
888776  meter/sec
 ZDOT =      17295
213876                 ZDOT =        5287
543231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14063677
89                 X    =        -4286609
02
 Y    =       15130923
67  feet           Y    =         4611905
53  meter
 Z    =        8270627
52                 Z    =         2520887
27
 XDOT =      -6460
043792                 XDOT =       -1969
021348
 YDOT =     -15543
858504  feet/sec       YDOT =       -4737
768072  meter/sec
 ZDOT =      17367
689785                 ZDOT =        5293
671846


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
78673855  
00016717  00000-0  10270-3 0  9035
2 25544  51
6387 175
2282 0003955  66
5842 293
5726 15
52729939 38560


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
78673855   =   yrday
fracday
Element set:     903
Inclination:       51
6387  deg
RA of node:       175
2282  deg
Eccentricity:     
0003955     
Arg of perigee:    66
5842  deg
Mean anomaly:     293
5726  deg
Mean motion:   15
52729939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3856
Checksum:              359


Coasting Arc #5 (Orbit 3864)
---------------------------------------

Vector Time (GMT): 2019/061/07:48:58
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4324312
77                 A    =         6787323
82  meter
 Y    =       -3647673
14  meter          E    =           
0014963
 Z    =        3739423
75                 I    =           51
68954
 XDOT =       5844
233709                 Wp   =           80
40217
 YDOT =       2526
783800  meter/sec      RA   =          171
33235  deg
 ZDOT =      -4276
529298                 TA   =           54
95030
                                          MA   =           54
81002
                                          Ha   =            224
323  n
mi
                                          Hp   =            215
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14187377
87                 X    =         4346617
06
 Y    =      -11967431
55  feet           Y    =        -3599190
72  meter
 Z    =       12268450
62                 Z    =         3760483
55
 XDOT =      19173
995107                 XDOT =        5836
316689
 YDOT =       8289
973098  feet/sec       YDOT =        2592
093594  meter/sec
 ZDOT =     -14030
607932                 ZDOT =       -4248
160208

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13414545
52                 X    =         4088753
48
 Y    =       12735764
43  feet           Y    =         3881861
00  meter
 Z    =       12363909
66                 Z    =         3768519
66
 XDOT =      -5239
447834                 XDOT =       -1596
983700
 YDOT =      19069
143744  feet/sec       YDOT =        5812
275013  meter/sec
 ZDOT =     -13902
568693                 ZDOT =       -4237
502938


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
36596774  
00016717  00000-0  10270-3 0  9045
2 25544  51
6366 172
3436 0003504  68
3199 291
8325 15
52749935 38655


Satellite: ISS
Catalog Number: 25544
Epoch time:      19061
36596774   =   yrday
fracday
Element set:     904
Inclination:       51
6366  deg
RA of node:       172
3436  deg
Eccentricity:     
0003504     
Arg of perigee:    68
3199  deg
Mean anomaly:     291
8325  deg
Mean motion:   15
52749935  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3865
Checksum:              344


Coasting Arc #6 (Orbit 3879)
---------------------------------------

Vector Time (GMT): 2019/062/07:48:58
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5127765
88                 A    =         6789970
51  meter
 Y    =        3488804
67  meter          E    =           
0008418
 Z    =       -2765649
42                 I    =           51
73188
 XDOT =      -4813
413698                 Wp   =           66
84101
 YDOT =      -3008
626068  meter/sec      RA   =          166
36498  deg
 ZDOT =       5144
873191                 TA   =          261
91188
                                          MA   =          262
00740
                                          Ha   =            224
454  n
mi
                                          Hp   =            215
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16823378
87                 X    =        -5152963
90
 Y    =       11446209
55  feet           Y    =         3431321
32  meter
 Z    =       -9073652
94                 Z    =        -2790619
04
 XDOT =     -15792
039692                 XDOT =       -4804
403003
 YDOT =      -9870
820434  feet/sec       YDOT =       -3062
402276  meter/sec
 ZDOT =      16879
505220                 ZDOT =        5121
514081

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13445965
41                 X    =        -4098330
26
 Y    =      -15204668
05  feet           Y    =        -4634382
82  meter
 Z    =       -9186786
76                 Z    =        -2800132
60
 XDOT =       6701
208120                 XDOT =        2042
528235
 YDOT =     -16030
457879  feet/sec       YDOT =       -4886
083561  meter/sec
 ZDOT =      16774
130780                 ZDOT =        5112
755062


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
33135000  
00016717  00000-0  10270-3 0  9055
2 25544  51
6373 167
5408 0003762  74
3769 285
7798 15
52765976 38800


Satellite: ISS
Catalog Number: 25544
Epoch time:      19062
33135000   =   yrday
fracday
Element set:     905
Inclination:       51
6373  deg
RA of node:       167
5408  deg
Eccentricity:     
0003762     
Arg of perigee:    74
3769  deg
Mean anomaly:     285
7798  deg
Mean motion:   15
52765976  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3880
Checksum:              339


Coasting Arc #7 (Orbit 3881)
---------------------------------------

Vector Time (GMT): 2019/062/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6328051
81                 A    =         6792975
05  meter
 Y    =        2304155
58  meter          E    =           
0013173
 Z    =        -852611
56                 I    =           51
74897
 XDOT =      -2335
610557                 Wp   =           48
97746
 YDOT =      -4240
468397  meter/sec      RA   =          165
72077  deg
 ZDOT =       5943
351204                 TA   =          301
81918
                                          MA   =          301
94738
                                          Ha   =            224
437  n
mi
                                          Hp   =            215
517

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20761324
85                 X    =        -6349205
81
 Y    =        7559565
55  feet           Y    =         2233272
54  meter
 Z    =       -2797282
03                 Z    =         -883401
69
 XDOT =      -7662
764294                 XDOT =       -2316
887676
 YDOT =     -13912
297892  feet/sec       YDOT =       -4266
481706  meter/sec
 ZDOT =      19499
183741                 ZDOT =        5932
051735

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21331861
64                 X    =        -6501951
43
 Y    =       -5686144
20  feet           Y    =        -1733136
75  meter
 Z    =       -2936642
71                 Z    =         -895088
70
 XDOT =       1166
694768                 XDOT =         355
608565
 YDOT =     -14310
983051  feet/sec       YDOT =       -4361
987634  meter/sec
 ZDOT =      19448
415300                 ZDOT =        5927
876983


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
46006716  
00016717  00000-0  10270-3 0  9061
2 25544  51
6402 166
9009 0003663  74
9022 285
2535 15
52757416 38827


Satellite: ISS
Catalog Number: 25544
Epoch time:      19062
46006716   =   yrday
fracday
Element set:     906
Inclination:       51
6402  deg
RA of node:       166
9009  deg
Eccentricity:     
0003663     
Arg of perigee:    74
9022  deg
Mean anomaly:     285
2535  deg
Mean motion:   15
52757416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3882
Checksum:              312


Coasting Arc #8 (Orbit 3897)
---------------------------------------

Vector Time (GMT): 2019/063/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6501766
20                 A    =         6793202
95  meter
 Y    =       -1902202
26  meter          E    =           
0013518
 Z    =        -439193
73                 I    =           51
78139
 XDOT =        969
490703                 Wp   =          125
19868
 YDOT =       4667
771710  meter/sec      RA   =          160
76593  deg
 ZDOT =      -6002
420766                 TA   =           59
52480
                                          MA   =           59
39137
                                          Ha   =            224
454  n
mi
                                          Hp   =            215
498

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21331253
94                 X    =         6524687
25
 Y    =       -6240821
05  feet           Y    =        -1829366
84  meter
 Z    =       -1440924
30                 Z    =         -407555
49
 XDOT =       3180
743776                 XDOT =         946
378052
 YDOT =      15314
211647  feet/sec       YDOT =        4678
483468  meter/sec
 ZDOT =     -19692
981517                 ZDOT =       -5997
768005

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21186132
84                 X    =         6457533
29
 Y    =        6746120
85  feet           Y    =         2056217
63  meter
 Z    =       -1297741
76                 Z    =         -395551
69
 XDOT =      -5315
622258                 XDOT =       -1620
201664
 YDOT =      13005
996460  feet/sec       YDOT =        3964
227721  meter/sec
 ZDOT =     -19672
288170                 ZDOT =       -5996
113434


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
48980308  
00016717  00000-0  10270-3 0  9073
2 25544  51
6398 161
7785 0003578  79
9887 280
1669 15
52773444 38982


Satellite: ISS
Catalog Number: 25544
Epoch time:      19063
48980308   =   yrday
fracday
Element set:     907
Inclination:       51
6398  deg
RA of node:       161
7785  deg
Eccentricity:     
0003578     
Arg of perigee:    79
9887  deg
Mean anomaly:     280
1669  deg
Mean motion:   15
52773444  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3898
Checksum:              379


Coasting Arc #9 (Orbit 3913)
---------------------------------------

Vector Time (GMT): 2019/064/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6416389
18                 A    =         6792148
47  meter
 Y    =        1451562
72  meter          E    =           
0017416
 Z    =        1658799
55                 I    =           51
81031
 XDOT =        339
501147                 Wp   =           67
56902
 YDOT =      -5090
491711  meter/sec      RA   =          155
81211  deg
 ZDOT =       5726
289958                 TA   =          310
55542
                                          MA   =          310
70692
                                          Ha   =            224
482  n
mi
                                          Hp   =            215
494

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21051145
61                 X    =        -6440201
44
 Y    =        4762344
87  feet           Y    =         1379677
20  meter
 Z    =        5442255
73                 Z    =         1627573
84
 XDOT =       1113
848906                 XDOT =         368
584705
 YDOT =     -16701
088290  feet/sec       YDOT =       -5086
531959  meter/sec
 ZDOT =      18787
040543                 ZDOT =        5728
010257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20281909
35                 X    =        -6181925
97
 Y    =       -7482835
65  feet           Y    =        -2280768
31  meter
 Z    =        5300955
68                 Z    =         1615731
29
 XDOT =       9373
323334                 XDOT =        2856
988952
 YDOT =     -11992
265512  feet/sec       YDOT =       -3655
242528  meter/sec
 ZDOT =      18795
192750                 ZDOT =        5728
774750


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
51953441  
00016717  00000-0  10270-3 0  9087
2 25544  51
6413 156
6562 0003657  82
1875 277
9692 15
52781324 39142


Satellite: ISS
Catalog Number: 25544
Epoch time:      19064
51953441   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       156
6562  deg
Eccentricity:     
0003657     
Arg of perigee:    82
1875  deg
Mean anomaly:     277
9692  deg
Mean motion:   15
52781324  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3914
Checksum:              333


Coasting Arc #10 (Orbit 3928)
---------------------------------------

Vector Time (GMT): 2019/065/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6111744
98                 A    =         6789948
27  meter
 Y    =        -856439
06  meter          E    =           
0007983
 Z    =       -2835021
21                 I    =           51
83260
 XDOT =      -1593
538341                 Wp   =          105
56406
 YDOT =       5483
452108  meter/sec      RA   =          150
85714  deg
 ZDOT =      -5105
913344                 TA   =          106
50562
                                          MA   =          106
41790
                                          Ha   =            224
485  n
mi
                                          Hp   =            215
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20051656
76                 X    =         6134638
38
 Y    =       -2809839
42  feet           Y    =         -787965
58  meter
 Z    =       -9301250
69                 Z    =        -2805277
52
 XDOT =      -5228
144164                 XDOT =       -1629
936206
 YDOT =      17990
328437  feet/sec       YDOT =        5465
427939  meter/sec
 ZDOT =     -16751
684200                 ZDOT =       -5113
743047

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18547537
67                 X    =         5653289
48
 Y    =        8272737
54  feet           Y    =         2521530
40  meter
 Z    =       -9166682
09                 Z    =        -2794004
70
 XDOT =     -13266
528545                 XDOT =       -4043
637900
 YDOT =      11193
941127  feet/sec       YDOT =        3411
913256  meter/sec
 ZDOT =     -16787
494905                 ZDOT =       -5116
828447


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
48490315  
00016717  00000-0  10270-3 0  9091
2 25544  51
6410 151
8540 0003633  85
3693 274
7874 15
52779039 39292


Satellite: ISS
Catalog Number: 25544
Epoch time:      19065
48490315   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:       151
8540  deg
Eccentricity:     
0003633     
Arg of perigee:    85
3693  deg
Mean anomaly:     274
7874  deg
Mean motion:   15
52779039  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3929
Checksum:              337


Coasting Arc #11 (Orbit 3944)
---------------------------------------

Vector Time (GMT): 2019/066/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5607305
43                 A    =         6787130
34  meter
 Y    =         184768
70  meter          E    =           
0015174
 Z    =        3807657
00                 I    =           51
85185
 XDOT =       2683
391905                 Wp   =           95
06783
 YDOT =      -5818
134638  meter/sec      RA   =          145
89902  deg
 ZDOT =       4218
250197                 TA   =          310
50017
                                          MA   =          310
63230
                                          Ha   =            224
520  n
mi
                                          Hp   =            215
422

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18396671
37                 X    =        -5627450
02
 Y    =         606196
52  feet           Y    =          121951
73  meter
 Z    =       12492313
00                 Z    =         3780370
30
 XDOT =       8803
779215                 XDOT =        2727
762905
 YDOT =     -19088
368235  feet/sec       YDOT =       -5787
878452  meter/sec
 ZDOT =      13839
403533                 ZDOT =        4231
393395

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16151850
83                 X    =        -4923084
13
 Y    =       -8999503
09  feet           Y    =        -2743048
54  meter
 Z    =       12368893
84                 Z    =         3770038
84
 XDOT =      16642
736820                 XDOT =        5072
706183
 YDOT =     -10694
697210  feet/sec       YDOT =       -3259
743710  meter/sec
 ZDOT =      13899
275815                 ZDOT =        4236
499268


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
51462506  
00016717  00000-0  10270-3 0  9109
2 25544  51
6409 146
7318 0003652  88
7589 271
3981 15
52814139 39459


Satellite: ISS
Catalog Number: 25544
Epoch time:      19066
51462506   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:       146
7318  deg
Eccentricity:     
0003652     
Arg of perigee:    88
7589  deg
Mean anomaly:     271
3981  deg
Mean motion:   15
52814139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3945
Checksum:              332


Coasting Arc #12 (Orbit 3952)
---------------------------------------

Vector Time (GMT): 2019/066/23:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4260329
82                 A    =         6782751
82  meter
 Y    =       -1710348
99  meter          E    =           
0009519
 Z    =        4986189
18                 I    =           51
85077
 XDOT =       4758
140668                 Wp   =          108
44918
 YDOT =      -5628
812267  meter/sec      RA   =          143
31919  deg
 ZDOT =       2128
438186                 TA   =          320
85777
                                          MA   =          320
92659
                                          Ha   =            224
597  n
mi
                                          Hp   =            215
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13977460
04                 X    =        -4265107
39
 Y    =       -5611381
19  feet           Y    =        -1758017
05  meter
 Z    =       16358888
37                 Z    =         4965482
99
 XDOT =      15610
697731                 XDOT =        4810
391379
 YDOT =     -18467
231846  feet/sec       YDOT =       -5575
310988  meter/sec
 ZDOT =       6983
064915                 ZDOT =        2151
678749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10658519
40                 X    =         3248716
71
 Y    =       10784433
43  feet           Y    =         3287095
31  meter
 Z    =       16265367
40                 Z    =         4957683
98
 XDOT =     -20872
473564                 XDOT =       -6361
929942
 YDOT =       9906
408268  feet/sec       YDOT =        3019
473240  meter/sec
 ZDOT =       7088
595920                 ZDOT =        2160
604036


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
02948682  
00016717  00000-0  10270-3 0  9111
2 25544  51
6403 144
1737 0003769  83
3950 276
7631 15
52804188 39535


Satellite: ISS
Catalog Number: 25544
Epoch time:      19067
02948682   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:       144
1737  deg
Eccentricity:     
0003769     
Arg of perigee:    83
3950  deg
Mean anomaly:     276
7631  deg
Mean motion:   15
52804188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3953
Checksum:              330


Coasting Arc #13 (Orbit 3957)
---------------------------------------

Vector Time (GMT): 2019/067/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5923668
14                 A    =         6790754
20  meter
 Y    =        2249829
79  meter          E    =           
0017362
 Z    =        2421094
35                 I    =           51
88374
 XDOT =        130
398915                 Wp   =           77
89544
 YDOT =      -5470
835100  meter/sec      RA   =          141
75936  deg
 ZDOT =       5373
952601                 TA   =          309
08314
                                          MA   =          309
23745
                                          Ha   =            224
492  n
mi
                                          Hp   =            215
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19434606
76                 X    =        -5960146
30
 Y    =        7381331
33  feet           Y    =         2183383
54  meter
 Z    =        7943222
93                 Z    =         2392230
87
 XDOT =        427
817961                 XDOT =         165
462296
 YDOT =     -17948
934056  feet/sec       YDOT =       -5469
180150  meter/sec
 ZDOT =      17631
078088                 ZDOT =        5374
671883

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7318641
30                 X    =        -2230721
87
 Y    =      -19511149
95  feet           Y    =        -5946998
51  meter
 Z    =        7812509
17                 Z    =         2381252
80
 XDOT =      16523
885611                 XDOT =        5036
480334
 YDOT =        901
694945  feet/sec       YDOT =         274
836619  meter/sec
 ZDOT =      17634
741236                 ZDOT =        5375
069129


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
35127327  
00016717  00000-0  10270-3 0  9123
2 25544  51
6381 142
5678 0003734  92
1992 267
9588 15
52814952 39580


Satellite: ISS
Catalog Number: 25544
Epoch time:      19067
35127327   =   yrday
fracday
Element set:     912
Inclination:       51
6381  deg
RA of node:       142
5678  deg
Eccentricity:     
0003734     
Arg of perigee:    92
1992  deg
Mean anomaly:     267
9588  deg
Mean motion:   15
52814952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3958
Checksum:              347


Coasting Arc #14 (Orbit 3972)
---------------------------------------

Vector Time (GMT): 2019/068/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5619619
92                 A    =         6788102
82  meter
 Y    =       -1507651
21  meter          E    =           
0008764
 Z    =       -3503941
68                 I    =           51
90064
 XDOT =      -1213
544802                 Wp   =           90
48392
 YDOT =       6036
944787  meter/sec      RA   =          136
80543  deg
 ZDOT =      -4553
718806                 TA   =          130
47895
                                          MA   =          130
40253
                                          Ha   =            224
504  n
mi
                                          Hp   =            215
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18437073
22                 X    =         5653081
30
 Y    =       -4946362
22  feet           Y    =        -1444622
03  meter
 Z    =      -11495871
66                 Z    =        -3476562
45
 XDOT =      -3981
446200                 XDOT =       -1258
842183
 YDOT =      19806
249300  feet/sec       YDOT =        6023
120236  meter/sec
 ZDOT =     -14940
022330                 ZDOT =       -4559
724475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5205087
50                 X    =         1586510
67
 Y    =       18442717
74  feet           Y    =         5621340
37  meter
 Z    =      -11371915
41                 Z    =        -3466159
82
 XDOT =     -18512
643455                 XDOT =       -5642
653725
 YDOT =      -3984
087954  feet/sec       YDOT =       -1214
350009  meter/sec
 ZDOT =     -14967
647338                 ZDOT =       -4562
138909


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
31663250  
00016717  00000-0  10270-3 0  9131
2 25544  51
6385 137
7646 0003794  93
2818 266
8768 15
52802916 39732


Satellite: ISS
Catalog Number: 25544
Epoch time:      19068
31663250   =   yrday
fracday
Element set:     913
Inclination:       51
6385  deg
RA of node:       137
7646  deg
Eccentricity:     
0003794     
Arg of perigee:    93
2818  deg
Mean anomaly:     266
8768  deg
Mean motion:   15
52802916  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3973
Checksum:              347


Coasting Arc #15 (Orbit 3988)
---------------------------------------

Vector Time (GMT): 2019/069/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5161462
33                 A    =         6785228
59  meter
 Y    =         658128
34  meter          E    =           
0013477
 Z    =        4345882
45                 I    =           51
91479
 XDOT =       2128
973316                 Wp   =          105
14830
 YDOT =      -6486
524311  meter/sec      RA   =          131
84788  deg
 ZDOT =       3498
358418                 TA   =          309
38367
                                          MA   =          309
50296
                                          Ha   =            224
551  n
mi
                                          Hp   =            215
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16933931
53                 X    =        -5189547
88
 Y    =        2159213
73  feet           Y    =          600252
73  meter
 Z    =       14258144
51                 Z    =         4320741
83
 XDOT =       6984
820589                 XDOT =        2184
356237
 YDOT =     -21281
247740  feet/sec       YDOT =       -6462
406571  meter/sec
 ZDOT =      11477
553864                 ZDOT =        3508
835388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2689688
82                 X    =         -819817
15
 Y    =      -16953386
55  feet           Y    =        -5167392
22  meter
 Z    =       14144369
34                 Z    =         4311203
78
 XDOT =      20249
120642                 XDOT =        6171
931972
 YDOT =       6437
594794  feet/sec       YDOT =        1962
178893  meter/sec
 ZDOT =      11525
452159                 ZDOT =        3512
957818


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   19069
34634375  
00016717  00000-0  10270-3 0  9142
2 25544  51
6385 132
6417 0003768  97
5741 262
5839 15
52829132 39893


Satellite: ISS
Catalog Number: 25544
Epoch time:      19069
34634375   =   yrday
fracday
Element set:     914
Inclination:       51
6385  deg
RA of node:       132
6417  deg
Eccentricity:     
0003768     
Arg of perigee:    97
5741  deg
Mean anomaly:     262
5839  deg
Mean motion:   15
52829132  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3989
Checksum:              349


Coasting Arc #16 (Orbit 4003)
---------------------------------------

Vector Time (GMT): 2019/070/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4613640
31                 A    =         6782857
82  meter
 Y    =         343989
00  meter          E    =           
0015748
 Z    =       -4974448
52                 I    =           51
92777
 XDOT =      -2885
718592                 Wp   =           80
18339
 YDOT =       6734
652942  meter/sec      RA   =          126
88671  deg
 ZDOT =      -2214
051329                 TA   =          168
27692
                                          MA   =          168
24021
                                          Ha   =            224
459  n
mi
                                          Hp   =            215
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15136615
19                 X    =         4633613
89
 Y    =        1128572
83  feet           Y    =          395693
12  meter
 Z    =      -16320369
15                 Z    =        -4951988
76
 XDOT =      -9467
580684                 XDOT =       -2950
058309
 YDOT =      22095
318050  feet/sec       YDOT =        6702
022848  meter/sec
 ZDOT =      -7263
947929                 ZDOT =       -2228
225987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -389114
93                 X    =         -118602
23
 Y    =       15282166
66  feet           Y    =         4658004
40  meter
 Z    =      -16218792
09                 Z    =        -4943487
83
 XDOT =     -21409
959291                 XDOT =       -6525
755592
 YDOT =      -8311
176534  feet/sec       YDOT =       -2533
246608  meter/sec
 ZDOT =      -7328
610623                 ZDOT =       -2233
760518


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   19070
31169719  
00016717  00000-0  10270-3 0  9157
2 25544  51
6383 127
8395 0003789 100
4177 259
7402 15
52807823 40048


Satellite: ISS
Catalog Number: 25544
Epoch time:      19070
31169719   =   yrday
fracday
Element set:     915
Inclination:       51
6383  deg
RA of node:       127
8395  deg
Eccentricity:     
0003789     
Arg of perigee:   100
4177  deg
Mean anomaly:     259
7402  deg
Mean motion:   15
52807823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4004
Checksum:              319


Coasting Arc #17 (Orbit 4019)
---------------------------------------

Vector Time (GMT): 2019/071/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4001190
11                 A    =         6781320
49  meter
 Y    =       -1404636
52  meter          E    =           
0006911
 Z    =        5286625
11                 I    =           51
94319
 XDOT =       3473
102633                 Wp   =          111
55116
 YDOT =      -6790
693841  meter/sec      RA   =          121
92166  deg
 ZDOT =        821
028512                 TA   =          330
61749
                                          MA   =          330
65633
                                          Ha   =            224
490  n
mi
                                          Hp   =            215
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13127264
12                 X    =        -4010865
14
 Y    =       -4608387
53  feet           Y    =        -1449434
28  meter
 Z    =       17344570
57                 Z    =         5267165
48
 XDOT =      11394
693679                 XDOT =        3544
791872
 YDOT =     -22279
179270  feet/sec       YDOT =       -6751
454271  meter/sec
 ZDOT =       2693
663098                 ZDOT =         838
074206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3729650
89                 X    =         1136797
59
 Y    =      -13516444
80  feet           Y    =        -4119812
37  meter
 Z    =       17256646
59                 Z    =         5259825
88
 XDOT =      21990
871027                 XDOT =        6702
817489
 YDOT =       9620
276645  feet/sec       YDOT =        2932
260321  meter/sec
 ZDOT =       2771
339975                 ZDOT =         844
704425


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   19071
34140212  
00016717  00000-0  10270-3 0  9169
2 25544  51
6393 122
7156 0003669 103
7886 256
3675 15
52844943 40205


Satellite: ISS
Catalog Number: 25544
Epoch time:      19071
34140212   =   yrday
fracday
Element set:     916
Inclination:       51
6393  deg
RA of node:       122
7156  deg
Eccentricity:     
0003669     
Arg of perigee:   103
7886  deg
Mean anomaly:     256
3675  deg
Mean motion:   15
52844943  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4020
Checksum:              308


Coasting Arc #18 (Orbit 4034)
---------------------------------------

Vector Time (GMT): 2019/072/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3388355
79                 A    =         6781242
89  meter
 Y    =        2521741
59  meter          E    =           
0018494
 Z    =       -5321215
68                 I    =           51
96003
 XDOT =      -3890
279476                 Wp   =           97
15475
 YDOT =       6559
748153  meter/sec      RA   =          116
95779  deg
 ZDOT =        631
137591                 TA   =          178
85823
                                          MA   =          178
85400
                                          Ha   =            224
417  n
mi
                                          Hp   =            215
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11116652
86                 X    =         3385752
58
 Y    =        8273430
43  feet           Y    =         2559617
65  meter
 Z    =      -17458056
69                 Z    =        -5304762
85
 XDOT =     -12763
384106                 XDOT =       -3966
409013
 YDOT =      21521
483440  feet/sec       YDOT =        6515
818703  meter/sec
 ZDOT =       2070
661387                 ZDOT =         612
054782

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7315243
74                 X    =        -2229686
29
 Y    =       11878683
23  feet           Y    =         3620622
65  meter
 Z    =      -17383827
51                 Z    =        -5298590
62
 XDOT =     -21638
062983                 XDOT =       -6595
281597
 YDOT =     -10420
483951  feet/sec       YDOT =       -3176
163508  meter/sec
 ZDOT =       1983
764233                 ZDOT =         604
651338


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   19072
30674926  
00016717  00000-0  10270-3 0  9171
2 25544  51
6398 117
9137 0003876 105
5015 254
6565 15
52837844 40356


Satellite: ISS
Catalog Number: 25544
Epoch time:      19072
30674926   =   yrday
fracday
Element set:     917
Inclination:       51
6398  deg
RA of node:       117
9137  deg
Eccentricity:     
0003876     
Arg of perigee:   105
5015  deg
Mean anomaly:     254
6565  deg
Mean motion:   15
52837844  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4035
Checksum:              331


Coasting Arc #19 (Orbit 4050)
---------------------------------------

Vector Time (GMT): 2019/073/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2777281
20                 A    =         6782533
18  meter
 Y    =       -3606839
29  meter          E    =           
0008923
 Z    =        5021082
24                 I    =           51
97810
 XDOT =       4190
248778                 Wp   =           76
95317
 YDOT =      -6090
005885  meter/sec      RA   =          111
99490  deg
 ZDOT =      -2051
943304                 TA   =           32
92219
                                          MA   =           32
86665
                                          Ha   =            224
572  n
mi
                                          Hp   =            215
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9111814
97                 X    =        -2761131
60
 Y    =      -11833462
24  feet           Y    =        -3637806
23  meter
 Z    =       16473366
93                 Z    =         5007630
73
 XDOT =      13747
535361                 XDOT =        4268
004673
 YDOT =     -19980
334269  feet/sec       YDOT =       -6042
712940  meter/sec
 ZDOT =      -6732
097453                 ZDOT =       -2031
399581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10852897
83                 X    =         3307963
26
 Y    =      -10356738
26  feet           Y    =        -3156733
82  meter
 Z    =       16412812
07                 Z    =         5002625
12
 XDOT =      20502
327851                 XDOT =        6249
109529
 YDOT =      10937
828937  feet/sec       YDOT =        3333
850260  meter/sec
 ZDOT =      -6638
607487                 ZDOT =       -2023
447562


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   19073
33645022  
00016717  00000-0  10270-3 0  9181
2 25544  51
6397 112
7903 0003922 108
7026 251
4552 15
52813438 40510


Satellite: ISS
Catalog Number: 25544
Epoch time:      19073
33645022   =   yrday
fracday
Element set:     918
Inclination:       51
6397  deg
RA of node:       112
7903  deg
Eccentricity:     
0003922     
Arg of perigee:   108
7026  deg
Mean anomaly:     251
4552  deg
Mean motion:   15
52813438  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4051
Checksum:              295
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