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

 
Date: October 31st 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16550 5887 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


306/13:59:45 869 0 0 0 0 0 0
N/A 0 0 0 0 227 1
000/00:00:00 000 0 0 0 0 222 1

308/07:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 7
000/00:00:00 000 0 0 0 0 222 3

308/09:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 7
000/00:00:00 000 0 0 0 0 222 2

311/22:40:57 510 1 0 1 3 1 3
N/A 0 6 -0 0 225 9
000/00:05:51 019 0 6 0 0 223 7

312/03:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 9
000/00:00:00 000 0 0 0 0 223 5

317/14:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 2
000/00:00:00 000 0 0 0 0 223 6

Coasting Arc #1 (Orbit 3623)
---------------------------------------

Vector Time (GMT): 2019/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5096648
19                 A    =         6792409
81  meter
 Y    =         602062
95  meter          E    =           
0010660
 Z    =       -4459526
12                 I    =           51
93310
 XDOT =       2144
989204                 Wp   =          149
01957
 YDOT =       6548
248950  meter/sec      RA   =           49
62244  deg
 ZDOT =       3330
143930                 TA   =          154
55905
                                          MA   =          154
50653
                                          Ha   =            227
538  n
mi
                                          Hp   =            221
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16721286
71                 X    =         5111199
44
 Y    =        1975272
16  feet           Y    =          659138
71  meter
 Z    =      -14630991
19                 Z    =        -4434732
48
 XDOT =       7037
366156                 XDOT =        2055
428932
 YDOT =      21483
756396  feet/sec       YDOT =        6571
734911  meter/sec
 ZDOT =      10925
669063                 ZDOT =        3340
346352

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14527033
17                 X    =        -4427839
71
 Y    =        8704240
06  feet           Y    =         2653052
37  meter
 Z    =      -14517938
72                 Z    =        -4425067
72
 XDOT =     -17996
353581                 XDOT =       -5485
288571
 YDOT =     -11705
986932  feet/sec       YDOT =       -3567
984817  meter/sec
 ZDOT =      10971
611937                 ZDOT =        3344
147318


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   19303
51006657  
00016717  00000-0  10270-3 0  9003
2 25544  51
6442  50
2951 0006725 207
0625 153
0176 15
50240737 36240


Satellite: ISS
Catalog Number: 25544
Epoch time:      19303
51006657   =   yrday
fracday
Element set:     900
Inclination:       51
6442  deg
RA of node:        50
2951  deg
Eccentricity:     
0006725     
Arg of perigee:   207
0625  deg
Mean anomaly:     153
0176  deg
Mean motion:   15
50240737  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3624
Checksum:              277


Coasting Arc #2 (Orbit 3639)
---------------------------------------

Vector Time (GMT): 2019/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5293200
16                 A    =         6793367
23  meter
 Y    =        -596584
80  meter          E    =           
0007382
 Z    =        4208288
40                 I    =           51
91386
 XDOT =      -2244
672874                 Wp   =          114
66768
 YDOT =      -6317
136362  meter/sec      RA   =           44
68520  deg
 ZDOT =      -3716
792461                 TA   =           13
36960
                                          MA   =           13
35005
                                          Ha   =            227
582  n
mi
                                          Hp   =            221
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17366142
26                 X    =        -5306577
58
 Y    =       -1957299
22  feet           Y    =         -655852
04  meter
 Z    =       13806720
47                 Z    =         4182542
90
 XDOT =      -7364
412317                 XDOT =       -2155
811455
 YDOT =     -20725
512999  feet/sec       YDOT =       -6341
740897  meter/sec
 ZDOT =     -12194
200989                 ZDOT =       -3727
480879

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14863519
43                 X    =         4530400
72
 Y    =       -9365764
68  feet           Y    =        -2854685
07  meter
 Z    =       13689327
57                 Z    =         4172507
04
 XDOT =      17940
694581                 XDOT =        5468
323708
 YDOT =      10567
909893  feet/sec       YDOT =        3221
098935  meter/sec
 ZDOT =     -12242
366654                 ZDOT =       -3731
473356


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   19304
54148842  
00016717  00000-0  10270-3 0  9011
2 25544  51
6445  45
1838 0006579 209
9298 150
1478 15
50216720 36400


Satellite: ISS
Catalog Number: 25544
Epoch time:      19304
54148842   =   yrday
fracday
Element set:     901
Inclination:       51
6445  deg
RA of node:        45
1838  deg
Eccentricity:     
0006579     
Arg of perigee:   209
9298  deg
Mean anomaly:     150
1478  deg
Mean motion:   15
50216720  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3640
Checksum:              315


Coasting Arc #3 (Orbit 3654)
---------------------------------------

Vector Time (GMT): 2019/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5511792
34                 A    =         6794240
08  meter
 Y    =         564442
71  meter          E    =           
0007515
 Z    =       -3940111
47                 I    =           51
89228
 XDOT =       2293
721796                 Wp   =          160
63152
 YDOT =       6061
710485  meter/sec      RA   =           39
74765  deg
 ZDOT =       4072
370373                 TA   =          151
93234
                                          MA   =          151
89180
                                          Ha   =            227
201  n
mi
                                          Hp   =            222
029

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18083308
19                 X    =         5524210
16
 Y    =        1851846
16  feet           Y    =          626149
05  meter
 Z    =      -12926874
90                 Z    =        -3913306
55
 XDOT =       7525
333976                 XDOT =        2205
985821
 YDOT =      19887
501591  feet/sec       YDOT =        6086
869776  meter/sec
 ZDOT =      13360
795186                 ZDOT =        4083
299770

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15181077
61                 X    =        -4627192
46
 Y    =       10154571
75  feet           Y    =         3095113
47  meter
 Z    =      -12804648
34                 Z    =        -3902856
81
 XDOT =     -17664
701488                 XDOT =       -5384
201013
 YDOT =      -9479
449338  feet/sec       YDOT =       -2889
336158  meter/sec
 ZDOT =      13410
072050                 ZDOT =        4087
389961


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   19305
50844297  
00016717  00000-0  10270-3 0  9026
2 25544  51
6443  40
3928 0006551 215
0847 144
9873 15
50239705 36557


Satellite: ISS
Catalog Number: 25544
Epoch time:      19305
50844297   =   yrday
fracday
Element set:     902
Inclination:       51
6443  deg
RA of node:        40
3928  deg
Eccentricity:     
0006551     
Arg of perigee:   215
0847  deg
Mean anomaly:     144
9873  deg
Mean motion:   15
50239705  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3655
Checksum:              317


Coasting Arc #4 (Orbit 3670)
---------------------------------------

Vector Time (GMT): 2019/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916487
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5711398
96                 A    =         6795212
58  meter
 Y    =        -493099
10  meter          E    =           
0009126
 Z    =        3637544
95                 I    =           51
86859
 XDOT =      -2310
573261                 Wp   =          118
70354
 YDOT =      -5826
029802  meter/sec      RA   =           34
80872  deg
 ZDOT =      -4413
544201                 TA   =           18
36450
                                          MA   =           18
33158
                                          Ha   =            227
234  n
mi
                                          Hp   =            222
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18738185
55                 X    =        -5723129
94
 Y    =       -1617779
21  feet           Y    =         -557033
72  meter
 Z    =       11934202
60                 Z    =         3609772
18
 XDOT =      -7580
620934                 XDOT =       -2223
814301
 YDOT =     -19114
271005  feet/sec       YDOT =       -5851
383003  meter/sec
 ZDOT =     -14480
131893                 ZDOT =       -4424
557760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15344208
42                 X    =         4676914
73
 Y    =      -11013576
39  feet           Y    =        -3356938
08  meter
 Z    =       11807556
99                 Z    =         3598943
37
 XDOT =      17314
728220                 XDOT =        5277
529161
 YDOT =       8531
140022  feet/sec       YDOT =        2600
291479  meter/sec
 ZDOT =     -14529
805962                 ZDOT =       -4428
684857


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   19306
53986195  
00016717  00000-0  10270-3 0  9035
2 25544  51
6439  35
2820 0006496 218
0103 142
0590 15
50230480 36716


Satellite: ISS
Catalog Number: 25544
Epoch time:      19306
53986195   =   yrday
fracday
Element set:     903
Inclination:       51
6439  deg
RA of node:        35
2820  deg
Eccentricity:     
0006496     
Arg of perigee:   218
0103  deg
Mean anomaly:     142
0590  deg
Mean motion:   15
50230480  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3671
Checksum:              295


Coasting Arc #5 (Orbit 3671)
---------------------------------------

Vector Time (GMT): 2019/306/13:59:45
869
Vector Time (MET): N/A
Weight (LBS)     : 916487
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -578277
40                 A    =         6791376
59  meter
 Y    =       -4872795
32  meter          E    =           
0006225
 Z    =       -4699713
41                 I    =           51
85241
 XDOT =       6826
934177                 Wp   =          103
01034
 YDOT =       1951
184245  meter/sec      RA   =           34
44518  deg
 ZDOT =      -2867
625983                 TA   =          138
57648
                                          MA   =          138
52928
                                          Ha   =            227
056  n
mi
                                          Hp   =            222
068

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1897235
56                 X    =         -500916
47
 Y    =      -15986861
28  feet           Y    =        -4878829
30  meter
 Z    =      -15419007
27                 Z    =        -4702334
79
 XDOT =      22398
078007                 XDOT =        6818
537618
 YDOT =       6401
523113  feet/sec       YDOT =        2027
480996  meter/sec
 ZDOT =      -9408
221729                 ZDOT =       -2834
483118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15675914
00                 X    =         4778018
59
 Y    =        3618108
39  feet           Y    =         1102799
44  meter
 Z    =      -15430490
38                 Z    =        -4703213
47
 XDOT =     -13233
047211                 XDOT =       -4033
432790
 YDOT =      17917
482256  feet/sec       YDOT =        5461
248592  meter/sec
 ZDOT =      -9257
221293                 ZDOT =       -2821
601050


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   19306
60432527  
00016717  00000-0  10270-3 0  9049
2 25544  51
6426  34
9635 0006442 219
2472 140
8212 15
50223243 36722


Satellite: ISS
Catalog Number: 25544
Epoch time:      19306
60432527   =   yrday
fracday
Element set:     904
Inclination:       51
6426  deg
RA of node:        34
9635  deg
Eccentricity:     
0006442     
Arg of perigee:   219
2472  deg
Mean anomaly:     140
8212  deg
Mean motion:   15
50223243  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3672
Checksum:              285


Coasting Arc #6 (Orbit 3687)
---------------------------------------

Vector Time (GMT): 2019/307/13:59:45
869
Vector Time (MET): N/A
Weight (LBS)     : 916487
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         518194
24                 A    =         6790580
17  meter
 Y    =        4698850
80  meter          E    =           
0008257
 Z    =        4876595
99                 I    =           51
82220
 XDOT =      -7039
148619                 Wp   =          168
87102
 YDOT =      -1772
121664  meter/sec      RA   =           29
50118  deg
 ZDOT =       2446
932116                 TA   =          257
10652
                                          MA   =          257
19877
                                          Ha   =            226
786  n
mi
                                          Hp   =            222
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1700112
35                 X    =          441923
73
 Y    =       15416177
17  feet           Y    =         4704219
03  meter
 Z    =       15999330
68                 Z    =         4878928
09
 XDOT =     -23094
319617                 XDOT =       -7030
695060
 YDOT =      -5814
047454  feet/sec       YDOT =       -1850
791190  meter/sec
 ZDOT =       8027
992506                 ZDOT =        2412
758630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15130894
65                 X    =        -4611896
69
 Y    =       -3358455
48  feet           Y    =        -1023657
23  meter
 Z    =       16009506
13                 Z    =         4879697
47
 XDOT =      12581
730321                 XDOT =        3834
911402
 YDOT =     -19023
836049  feet/sec       YDOT =       -5798
465228  meter/sec
 ZDOT =       7872
279864                 ZDOT =        2399
470903


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   19307
63574008  
00016717  00000-0  10270-3 0  9055
2 25544  51
6431  29
8519 0006371 224
0273 136
0371 15
50250362 36888


Satellite: ISS
Catalog Number: 25544
Epoch time:      19307
63574008   =   yrday
fracday
Element set:     905
Inclination:       51
6431  deg
RA of node:        29
8519  deg
Eccentricity:     
0006371     
Arg of perigee:   224
0273  deg
Mean anomaly:     136
0371  deg
Mean motion:   15
50250362  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3688
Checksum:              297


Coasting Arc #7 (Orbit 3698)
---------------------------------------

Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916487
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1174344
44                 A    =         6791086
35  meter
 Y    =        4721701
10  meter          E    =           
0008391
 Z    =        4739194
42                 I    =           51
80144
 XDOT =      -7069
292945                 Wp   =          163
56741
 YDOT =      -1026
502399  meter/sec      RA   =           25
99731  deg
 ZDOT =       2765
397247                 TA   =          259
03807
                                          MA   =          259
13248
                                          Ha   =            226
709  n
mi
                                          Hp   =            222
272

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3852836
08                 X    =         1098437
08
 Y    =       15491145
36  feet           Y    =         4734408
95  meter
 Z    =       15548538
13                 Z    =         4744714
73
 XDOT =     -23193
218323                 XDOT =       -7070
721809
 YDOT =      -3367
790022  feet/sec       YDOT =       -1105
564261  meter/sec
 ZDOT =       9072
825612                 ZDOT =        2731
053389

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5203330
28                 X    =         1585975
07
 Y    =      -15065727
87  feet           Y    =        -4592033
86  meter
 Z    =       15573251
62                 Z    =         4746727
09
 XDOT =      16663
277413                 XDOT =        5078
966955
 YDOT =      15002
344253  feet/sec       YDOT =        4572
714528  meter/sec
 ZDOT =       8916
267806                 ZDOT =        2717
678427


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   19308
34483745  
00016717  00000-0  10270-3 0  9062
2 25544  51
6414  26
3342 0006391 225
3968 134
6662 15
50262263 36994


Satellite: ISS
Catalog Number: 25544
Epoch time:      19308
34483745   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:        26
3342  deg
Eccentricity:     
0006391     
Arg of perigee:   225
3968  deg
Mean anomaly:     134
6662  deg
Mean motion:   15
50262263  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3699
Checksum:              320


Coasting Arc #8 (Orbit 3699)
---------------------------------------

Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931200
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4646170
71                 A    =         6798093
40  meter
 Y    =       -4326718
30  meter          E    =           
0008226
 Z    =       -2416039
39                 I    =           51
82431
 XDOT =       4948
025869                 Wp   =          182
88450
 YDOT =      -2316
999073  meter/sec      RA   =           25
55134  deg
 ZDOT =      -5373
167633                 TA   =           24
01544
                                          MA   =           23
97710
                                          Ha   =            226
723  n
mi
                                          Hp   =            222
248

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15243342
22                 X    =        -4585706
86
 Y    =      -14195270
02  feet           Y    =        -4378336
95  meter
 Z    =       -7926638
42                 Z    =        -2438462
22
 XDOT =      16233
680672                 XDOT =        4999
667638
 YDOT =      -7601
702997  feet/sec       YDOT =       -2261
377919  meter/sec
 ZDOT =     -17628
502732                 ZDOT =       -5349
006312

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15173575
10                 X    =         4624905
69
 Y    =       14212766
07  feet           Y    =         4332051
10  meter
 Z    =       -8028491
06                 Z    =        -2447084
08
 XDOT =     -15324
401081                 XDOT =       -4670
877449
 YDOT =       6477
964317  feet/sec       YDOT =        1974
483524  meter/sec
 ZDOT =     -17518
061859                 ZDOT =       -5339
505255


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   19308
40930122  
00016717  00000-0  10270-3 0  9076
2 25544  51
6437  26
0152 0006422 224
8887 135
1745 15
50251487 37001


Satellite: ISS
Catalog Number: 25544
Epoch time:      19308
40930122   =   yrday
fracday
Element set:     907
Inclination:       51
6437  deg
RA of node:        26
0152  deg
Eccentricity:     
0006422     
Arg of perigee:   224
8887  deg
Mean anomaly:     135
1745  deg
Mean motion:   15
50251487  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3700
Checksum:              291


Coasting Arc #9 (Orbit 3715)
---------------------------------------

Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931200
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4663868
39                 A    =         6797238
13  meter
 Y    =        4088677
59  meter          E    =           
0008621
 Z    =        2776298
65                 I    =           51
79123
 XDOT =      -5156
700090                 Wp   =          102
58237
 YDOT =       2382
442776  meter/sec      RA   =           20
60871  deg
 ZDOT =       5138
730434                 TA   =          288
74666
                                          MA   =          288
84018
                                          Ha   =            226
591  n
mi
                                          Hp   =            222
343

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15301405
49                 X    =         4604315
11
 Y    =       13414296
57  feet           Y    =         4140499
27  meter
 Z    =        9108591
37                 Z    =         2798809
60
 XDOT =     -16918
307382                 XDOT =       -5207
919384
 YDOT =       7816
413306  feet/sec       YDOT =        2324
490509  meter/sec
 ZDOT =      16859
351819                 ZDOT =        5113
556438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15453325
75                 X    =        -4710173
69
 Y    =      -13168050
39  feet           Y    =        -4013621
76  meter
 Z    =        9210861
59                 Z    =         2807470
61
 XDOT =      15943
583488                 XDOT =        4859
604247
 YDOT =      -6963
429903  feet/sec       YDOT =       -2122
453434  meter/sec
 ZDOT =      16744
290762                 ZDOT =        5103
659824


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   19309
44071199  
00016717  00000-0  10270-3 0  9082
2 25544  51
6439  20
9042 0006411 228
3326 131
7276 15
50272663 37166


Satellite: ISS
Catalog Number: 25544
Epoch time:      19309
44071199   =   yrday
fracday
Element set:     908
Inclination:       51
6439  deg
RA of node:        20
9042  deg
Eccentricity:     
0006411     
Arg of perigee:   228
3326  deg
Mean anomaly:     131
7276  deg
Mean motion:   15
50272663  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              302


Coasting Arc #10 (Orbit 3730)
---------------------------------------

Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931200
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4623113
06                 A    =         6796393
02  meter
 Y    =       -3864501
74  meter          E    =           
0004937
 Z    =       -3137439
83                 I    =           51
75657
 XDOT =       5372
352324                 Wp   =          187
00798
 YDOT =      -2478
147566  meter/sec      RA   =           15
66385  deg
 ZDOT =      -4867
867736                 TA   =           29
00943
                                          MA   =           28
98200
                                          Ha   =            226
407  n
mi
                                          Hp   =            222
531

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15167693
76                 X    =        -4564315
34
 Y    =      -12678811
47  feet           Y    =        -3915871
92  meter
 Z    =      -10293437
75                 Z    =        -3159754
62
 XDOT =      17625
827835                 XDOT =        5423
310108
 YDOT =      -8130
405400  feet/sec       YDOT =       -2417
785243  meter/sec
 ZDOT =     -15970
694671                 ZDOT =       -4841
646738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15511444
17                 X    =         4727888
18
 Y    =       12169992
92  feet           Y    =         3709413
84  meter
 Z    =      -10394826
94                 Z    =        -3168343
25
 XDOT =     -16565
370903                 XDOT =       -5049
125051
 YDOT =       7585
870194  feet/sec       YDOT =        2312
173235  meter/sec
 ZDOT =     -15850
856388                 ZDOT =       -4831
341027


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   19310
40766063  
00016717  00000-0  10270-3 0  9092
2 25544  51
6439  16
1131 0006432 232
2757 127
7811 15
50248438 37317


Satellite: ISS
Catalog Number: 25544
Epoch time:      19310
40766063   =   yrday
fracday
Element set:     909
Inclination:       51
6439  deg
RA of node:        16
1131  deg
Eccentricity:     
0006432     
Arg of perigee:   232
2757  deg
Mean anomaly:     127
7811  deg
Mean motion:   15
50248438  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3731
Checksum:              293


Coasting Arc #11 (Orbit 3746)
---------------------------------------

Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931200
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4569275
92                 A    =         6795389
42  meter
 Y    =        3645848
78  meter          E    =           
0007913
 Z    =        3462925
17                 I    =           51
72194
 XDOT =      -5561
712358                 Wp   =          118
70907
 YDOT =       2618
221281  meter/sec      RA   =           10
71546  deg
 ZDOT =       4570
427457                 TA   =          281
77713
                                          MA   =          281
86589
                                          Ha   =            226
226  n
mi
                                          Hp   =            222
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14991062
73                 X    =         4511346
15
 Y    =       11961446
12  feet           Y    =         3696621
80  meter
 Z    =       11361303
07                 Z    =         3484980
58
 XDOT =     -18247
087790                 XDOT =       -5612
777652
 YDOT =       8589
964832  feet/sec       YDOT =        2555
740839  meter/sec
 ZDOT =      14994
840738                 ZDOT =        4543
286252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15498687
93                 X    =        -4724000
08
 Y    =      -11194264
41  feet           Y    =        -3412011
79  meter
 Z    =       11461521
67                 Z    =         3493471
80
 XDOT =      17074
684836                 XDOT =        5204
363938
 YDOT =      -8375
654865  feet/sec       YDOT =       -2552
899603  meter/sec
 ZDOT =      14870
801240                 ZDOT =        4532
620218


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   19311
43906783  
00016717  00000-0  10270-3 0  9103
2 25544  51
6448  11
0017 0006407 236
3392 123
7148 15
50281309 37476


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
43906783   =   yrday
fracday
Element set:     910
Inclination:       51
6448  deg
RA of node:        11
0017  deg
Eccentricity:     
0006407     
Arg of perigee:   236
3392  deg
Mean anomaly:     123
7148  deg
Mean motion:   15
50281309  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3747
Checksum:              293


Coasting Arc #12 (Orbit 3754)
---------------------------------------

Vector Time (GMT): 2019/311/22:43:53
019
Vector Time (MET): N/A
Weight (LBS)     : 931071
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5314107
14                 A    =         6795807
63  meter
 Y    =       -2167962
26  meter          E    =           
0002974
 Z    =       -3640971
26                 I    =           51
70231
 XDOT =       4704
224721                 Wp   =          197
58608
 YDOT =       4150
640510  meter/sec      RA   =            7
87052  deg
 ZDOT =       4390
815192                 TA   =          119
36840
                                          MA   =          119
33870
                                          Ha   =            225
937  n
mi
                                          Hp   =            223
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17434734
71                 X    =         5355641
09
 Y    =       -7112737
08  feet           Y    =        -2108304
01  meter
 Z    =      -11945443
78                 Z    =        -3615055
96
 XDOT =      15433
808140                 XDOT =        4636
132913
 YDOT =      13617
586975  feet/sec       YDOT =        4202
865838  meter/sec
 ZDOT =      14405
561654                 ZDOT =        4413
501477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12396305
95                 X    =         3778394
05
 Y    =      -14272603
64  feet           Y    =        -4350289
59  meter
 Z    =      -11827045
89                 Z    =        -3604883
59
 XDOT =      18799
355919                 XDOT =        5730
043684
 YDOT =       4295
184914  feet/sec       YDOT =        1309
172362  meter/sec
 ZDOT =      14508
600849                 ZDOT =        4422
221539


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   19311
95477238  
00016717  00000-0  10270-3 0  9119
2 25544  51
6452   8
4501 0006580 251
1502 108
8940 15
50024087 37550


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
95477238   =   yrday
fracday
Element set:     911
Inclination:       51
6452  deg
RA of node:         8
4501  deg
Eccentricity:     
0006580     
Arg of perigee:   251
1502  deg
Mean anomaly:     108
8940  deg
Mean motion:   15
50024087  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3755
Checksum:              293


Coasting Arc #13 (Orbit 3757)
---------------------------------------

Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931071
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1882345
92                 A    =         6790755
13  meter
 Y    =       -4207464
41  meter          E    =           
0006055
 Z    =       -4992350
66                 I    =           51
67545
 XDOT =       7320
341807                 Wp   =           78
34823
 YDOT =       -777
008311  meter/sec      RA   =            7
01218  deg
 ZDOT =      -2106
230383                 TA   =          171
13088
                                          MA   =          171
12018
                                          Ha   =            225
937  n
mi
                                          Hp   =            223
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6175675
61                 X    =        -1810906
43
 Y    =      -13804017
10  feet           Y    =        -4228114
80  meter
 Z    =      -16379103
23                 Z    =        -5001320
95
 XDOT =      24016
869444                 XDOT =        7338
717555
 YDOT =      -2549
239864  feet/sec       YDOT =        -695
044376  meter/sec
 ZDOT =      -6910
204669                 ZDOT =       -2070
625624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13541421
95                 X    =        -4127425
41
 Y    =        6632640
41  feet           Y    =         2021628
80  meter
 Z    =      -16419587
47                 Z    =        -5004690
26
 XDOT =      -3062
392052                 XDOT =        -933
417098
 YDOT =     -22948
976175  feet/sec       YDOT =       -6994
847938  meter/sec
 ZDOT =      -6747
762416                 ZDOT =       -2056
717984


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   19312
14819015  
00016717  00000-0  10270-3 0  9125
2 25544  51
6411   7
4892 0006621 251
2063 108
8369 15
50015087 37584


Satellite: ISS
Catalog Number: 25544
Epoch time:      19312
14819015   =   yrday
fracday
Element set:     912
Inclination:       51
6411  deg
RA of node:         7
4892  deg
Eccentricity:     
0006621     
Arg of perigee:   251
2063  deg
Mean anomaly:     108
8369  deg
Mean motion:   15
50015087  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3758
Checksum:              293


Coasting Arc #14 (Orbit 3773)
---------------------------------------

Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931071
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1822244
10                 A    =         6790427
66  meter
 Y    =        4102743
13  meter          E    =           
0005087
 Z    =        5097799
61                 I    =           51
64012
 XDOT =      -7375
958626                 Wp   =          204
08840
 YDOT =       1111
483925  meter/sec      RA   =            2
05802  deg
 ZDOT =       1738
134887                 TA   =          229
06665
                                          MA   =          229
11070
                                          Ha   =            225
742  n
mi
                                          Hp   =            223
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5978491
14                 X    =         1751467
79
 Y    =       13460443
33  feet           Y    =         4122725
11  meter
 Z    =       16725064
32                 Z    =         5106479
59
 XDOT =     -24199
339323                 XDOT =       -7396
282438
 YDOT =       3646
600804  feet/sec       YDOT =        1028
887143  meter/sec
 ZDOT =       5702
542280                 ZDOT =        1702
255089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13094075
47                 X    =         3991074
20
 Y    =       -6645256
84  feet           Y    =        -2025474
29  meter
 Z    =       16764230
27                 Z    =         5109737
39
 XDOT =       4578
312025                 XDOT =        1395
469505
 YDOT =      23026
683409  feet/sec       YDOT =        7018
533103  meter/sec
 ZDOT =       5538
827312                 ZDOT =        1688
234565


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   19313
17975865  
00016717  00000-0  10270-3 0  9136
2 25544  51
6406   2
3788 0006562 255
3117 104
7307 15
49971846 37742


Satellite: ISS
Catalog Number: 25544
Epoch time:      19313
17975865   =   yrday
fracday
Element set:     913
Inclination:       51
6406  deg
RA of node:         2
3788  deg
Eccentricity:     
0006562     
Arg of perigee:   255
3117  deg
Mean anomaly:     104
7307  deg
Mean motion:   15
49971846  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3774
Checksum:              332


Coasting Arc #15 (Orbit 3788)
---------------------------------------

Vector Time (GMT): 2019/314/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931071
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1741233
61                 A    =         6789913
37  meter
 Y    =       -4028184
16  meter          E    =           
0007429
 Z    =       -5187776
00                 I    =           51
60469
 XDOT =       7394
240478                 Wp   =           81
95561
 YDOT =      -1450
514540  meter/sec      RA   =          357
10116  deg
 ZDOT =      -1356
176633                 TA   =          174
98588
                                          MA   =          174
97843
                                          Ha   =            225
581  n
mi
                                          Hp   =            223
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5712708
70                 X    =        -1670859
91
 Y    =      -13215827
29  feet           Y    =        -4047262
44  meter
 Z    =      -17020262
48                 Z    =        -5196063
50
 XDOT =      24259
319154                 XDOT =        7416
498713
 YDOT =      -4758
905971  feet/sec       YDOT =       -1367
702481  meter/sec
 ZDOT =      -4449
398401                 ZDOT =       -1320
203206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12754247
38                 X    =        -3887494
60
 Y    =        6583958
70  feet           Y    =         2006790
61  meter
 Z    =      -17057641
35                 Z    =        -5199169
08
 XDOT =      -6107
480772                 XDOT =       -1861
560139
 YDOT =     -22927
843460  feet/sec       YDOT =       -6988
406687  meter/sec
 ZDOT =      -4285
237131                 ZDOT =       -1306
140277


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   19314
14685130  
00016717  00000-0  10270-3 0  9148
2 25544  51
6399 357
5878 0006542 257
3478 102
6941 15
50017695 37890


Satellite: ISS
Catalog Number: 25544
Epoch time:      19314
14685130   =   yrday
fracday
Element set:     914
Inclination:       51
6399  deg
RA of node:       357
5878  deg
Eccentricity:     
0006542     
Arg of perigee:   257
3478  deg
Mean anomaly:     102
6941  deg
Mean motion:   15
50017695  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3789
Checksum:              342


Coasting Arc #16 (Orbit 3804)
---------------------------------------

Vector Time (GMT): 2019/315/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931071
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1661587
18                 A    =         6789753
39  meter
 Y    =        3975992
09  meter          E    =           
0004440
 Z    =        5250447
99                 I    =           51
57061
 XDOT =      -7381
274057                 Wp   =          231
74373
 YDOT =       1797
697487  meter/sec      RA   =          352
14132  deg
 ZDOT =        972
455259                 TA   =          208
91637
                                          MA   =          208
94098
                                          Ha   =            225
335  n
mi
                                          Hp   =            223
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5451401
51                 X    =         1591498
51
 Y    =       13044593
48  feet           Y    =         3994181
22  meter
 Z    =       17225879
22                 Z    =         5258349
36
 XDOT =     -24216
778403                 XDOT =       -7405
551617
 YDOT =       5897
957634  feet/sec       YDOT =        1715
019117  meter/sec
 ZDOT =       3190
470011                 ZDOT =         936
539838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12493056
68                 X    =         3807883
68
 Y    =       -6524900
60  feet           Y    =        -1988789
70  meter
 Z    =       17261498
17                 Z    =         5261304
64
 XDOT =       7650
496215                 XDOT =        2331
871246
 YDOT =      22673
321499  feet/sec       YDOT =        6910
828393  meter/sec
 ZDOT =       3026
551589                 ZDOT =         922
492924


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   19315
17841732  
00016717  00000-0  10270-3 0  9155
2 25544  51
6401 352
4767 0006546 261
9576  98
0832 15
49975430 38053


Satellite: ISS
Catalog Number: 25544
Epoch time:      19315
17841732   =   yrday
fracday
Element set:     915
Inclination:       51
6401  deg
RA of node:       352
4767  deg
Eccentricity:     
0006546     
Arg of perigee:   261
9576  deg
Mean anomaly:      98
0832  deg
Mean motion:   15
49975430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3805
Checksum:              332


Coasting Arc #17 (Orbit 3819)
---------------------------------------

Vector Time (GMT): 2019/316/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931071
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1573860
72                 A    =         6789409
78  meter
 Y    =       -3956112
57  meter          E    =           
0008297
 Z    =       -5295724
33                 I    =           51
53771
 XDOT =       7327
848453                 Wp   =           86
39501
 YDOT =      -2139
770132  meter/sec      RA   =          347
17952  deg
 ZDOT =       -579
581685                 TA   =          178
05840
                                          MA   =          178
05518
                                          Ha   =            225
215  n
mi
                                          Hp   =            223
435

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5163585
04                 X    =        -1503780
90
 Y    =      -12979371
94  feet           Y    =        -3973320
61  meter
 Z    =      -17374423
67                 Z    =        -5303199
67
 XDOT =      24041
497548                 XDOT =        7354
046728
 YDOT =      -7020
243214  feet/sec       YDOT =       -2057
678456  meter/sec
 ZDOT =      -1901
514715                 ZDOT =        -543
921115

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12345956
51                 X    =        -3763047
54
 Y    =        6444592
86  feet           Y    =         1964311
90  meter
 Z    =      -17408098
26                 Z    =        -5305988
35
 XDOT =      -9155
962386                 XDOT =       -2790
737335
 YDOT =     -22234
364612  feet/sec       YDOT =       -6777
034334  meter/sec
 ZDOT =      -1738
734845                 ZDOT =        -529
966381


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   19316
14550609  
00016717  00000-0  10270-3 0  9164
2 25544  51
6408 347
6857 0006403 264
6807  95
3613 15
50028721 38203


Satellite: ISS
Catalog Number: 25544
Epoch time:      19316
14550609   =   yrday
fracday
Element set:     916
Inclination:       51
6408  deg
RA of node:       347
6857  deg
Eccentricity:     
0006403     
Arg of perigee:   264
6807  deg
Mean anomaly:      95
3613  deg
Mean motion:   15
50028721  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3820
Checksum:              311


Coasting Arc #18 (Orbit 3835)
---------------------------------------

Vector Time (GMT): 2019/317/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931071
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1491399
79                 A    =         6789468
60  meter
 Y    =        3959510
86  meter          E    =           
0003941
 Z    =        5313292
42                 I    =           51
50368
 XDOT =      -7244
480978                 Wp   =          263
01958
 YDOT =       2479
032198  meter/sec      RA   =          342
21464  deg
 ZDOT =        185
723360                 TA   =          185
20291
                                          MA   =          185
20701
                                          Ha   =            225
150  n
mi
                                          Hp   =            223
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4893043
93                 X    =         1421202
76
 Y    =       12990521
20  feet           Y    =         3975795
99  meter
 Z    =       17432061
75                 Z    =         5320366
99
 XDOT =     -23767
982212                 XDOT =       -7272
565976
 YDOT =       8133
307736  feet/sec       YDOT =        2397
862254  meter/sec
 ZDOT =        609
328609                 ZDOT =         150
463249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12278796
47                 X    =         3742577
16
 Y    =       -6388696
35  feet           Y    =        -1947274
65  meter
 Z    =       17463906
01                 Z    =         5322998
55
 XDOT =      10624
616126                 XDOT =        3238
382995
 YDOT =      21648
773385  feet/sec       YDOT =        6598
546128  meter/sec
 ZDOT =        448
348721                 ZDOT =         136
656690


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   19317
17706903  
00016717  00000-0  10270-3 0  9179
2 25544  51
6394 342
5743 0006346 268
6313  91
4110 15
49978292 38368


Satellite: ISS
Catalog Number: 25544
Epoch time:      19317
17706903   =   yrday
fracday
Element set:     917
Inclination:       51
6394  deg
RA of node:       342
5743  deg
Eccentricity:     
0006346     
Arg of perigee:   268
6313  deg
Mean anomaly:      91
4110  deg
Mean motion:   15
49978292  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3836
Checksum:              331


Coasting Arc #19 (Orbit 3842)
---------------------------------------

Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931071
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2132566
78                 A    =         6792834
63  meter
 Y    =       -4611567
25  meter          E    =           
0003816
 Z    =       -4512395
06                 I    =           51
49981
 XDOT =       6969
184986                 Wp   =          139
91426
 YDOT =        118
984438  meter/sec      RA   =          339
76484  deg
 ZDOT =       3170
693578                 TA   =          162
03612
                                          MA   =          162
02263
                                          Ha   =            225
182  n
mi
                                          Hp   =            223
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6996610
17                 X    =         2205895
51
 Y    =      -15129813
80  feet           Y    =        -4587309
11  meter
 Z    =      -14804445
72                 Z    =        -4501857
71
 XDOT =      22864
780139                 XDOT =        6951
934585
 YDOT =        390
368891  feet/sec       YDOT =         196
822144  meter/sec
 ZDOT =      10402
537984                 ZDOT =        3204
506358

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15592979
36                 X    =         4752740
11
 Y    =        6013032
40  feet           Y    =         1832772
27  meter
 Z    =      -14755943
51                 Z    =        -4497611
58
 XDOT =       1653
953354                 XDOT =         504
124982
 YDOT =      21627
894806  feet/sec       YDOT =        6592
182337  meter/sec
 ZDOT =      10556
651757                 ZDOT =        3217
667455


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   19317
62837486  
00016717  00000-0  10270-3 0  9181
2 25544  51
6397 340
3427 0006476 273
3536  86
6873 15
49998035 38437


Satellite: ISS
Catalog Number: 25544
Epoch time:      19317
62837486   =   yrday
fracday
Element set:     918
Inclination:       51
6397  deg
RA of node:       340
3427  deg
Eccentricity:     
0006476     
Arg of perigee:   273
3536  deg
Mean anomaly:      86
6873  deg
Mean motion:   15
49998035  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3843
Checksum:              362
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