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

 
Date: June 2nd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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


153/12:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 9

154/09:16:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 214 0

156/19:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 214 1

157/11:12:41 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 214 2

159/13:07:21 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 214 3

164/10:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 1
000/00:00:00 000 0 0 0 0 214 7

Coasting Arc #1 (Orbit 3606)
---------------------------------------

Vector Time (GMT): 2018/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3183834
19                 A    =         6780632
67  meter
 Y    =        3880142
26  meter          E    =           
0012859
 Z    =       -4571961
21                 I    =           52
00692
 XDOT =      -3117
872559                 Wp   =          118
23844
 YDOT =       6251
681973  meter/sec      RA   =           95
98603  deg
 ZDOT =       3135
240652                 TA   =          183
05923
                                          MA   =          183
06710
                                          Ha   =            221
978  n
mi
                                          Hp   =            213
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10445650
24                 X    =         3162417
05
 Y    =       12730125
54  feet           Y    =         3915627
00  meter
 Z    =      -14999872
72                 Z    =        -4556546
62
 XDOT =     -10229
240679                 XDOT =       -3202
778280
 YDOT =      20510
767627  feet/sec       YDOT =        6216
340588  meter/sec
 ZDOT =      10286
222612                 ZDOT =        3119
889696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15657907
01                 X    =         4772530
06
 Y    =       -5295853
03  feet           Y    =        -1614176
00  meter
 Z    =      -14931435
82                 Z    =        -4551101
64
 XDOT =      15087
145939                 XDOT =        4598
562082
 YDOT =      15809
073506  feet/sec       YDOT =        4818
605605  meter/sec
 ZDOT =      10216
636469                 ZDOT =        3114
030796


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   18152
51051540  
00016717  00000-0  10270-3 0  9005
2 25544  51
6394  96
8676 0003386 141
7912 218
3481 15
54106849 36073


Satellite: ISS
Catalog Number: 25544
Epoch time:      18152
51051540   =   yrday
fracday
Element set:     900
Inclination:       51
6394  deg
RA of node:        96
8676  deg
Eccentricity:     
0003386     
Arg of perigee:   141
7912  deg
Mean anomaly:     218
3481  deg
Mean motion:   15
54106849  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3607
Checksum:              312


Coasting Arc #2 (Orbit 3622)
---------------------------------------

Vector Time (GMT): 2018/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2592120
98                 A    =         6784357
76  meter
 Y    =       -5231904
67  meter          E    =           
0014619
 Z    =        3439761
55                 I    =           52
02243
 XDOT =       3697
765400                 Wp   =          100
26117
 YDOT =      -4881
498871  meter/sec      RA   =           91
02467  deg
 ZDOT =      -4624
164857                 TA   =           39
65273
                                          MA   =           39
54592
                                          Ha   =            221
986  n
mi
                                          Hp   =            213
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8504333
91                 X    =        -2550132
33
 Y    =      -17165041
58  feet           Y    =        -5260657
26  meter
 Z    =       11285306
93                 Z    =         3427271
15
 XDOT =      12131
776247                 XDOT =        3774
538645
 YDOT =     -16015
416243  feet/sec       YDOT =       -4839
718008  meter/sec
 ZDOT =     -15171
144545                 ZDOT =       -4606
016547

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19061854
38                 X    =        -5810053
22
 Y    =        2202235
06  feet           Y    =          671241
25  meter
 Z    =       11230154
42                 Z    =         3422951
07
 XDOT =     -10716
559890                 XDOT =       -3266
407454
 YDOT =     -15575
844711  feet/sec       YDOT =       -4747
517468  meter/sec
 ZDOT =     -15089
217787                 ZDOT =       -4599
193582


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   18153
53935357  
00016717  00000-0  10270-3 0  9016
2 25544  51
6399  91
7391 0003322 143
1796 216
9586 15
54128076 36236


Satellite: ISS
Catalog Number: 25544
Epoch time:      18153
53935357   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:        91
7391  deg
Eccentricity:     
0003322     
Arg of perigee:   143
1796  deg
Mean anomaly:     216
9586  deg
Mean motion:   15
54128076  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3623
Checksum:              326


Coasting Arc #3 (Orbit 3622)
---------------------------------------

Vector Time (GMT): 2018/153/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3570849
37                 A    =         6780864
26  meter
 Y    =       -3624996
98  meter          E    =           
0010861
 Z    =       -4491700
59                 I    =           52
01109
 XDOT =       2451
422463                 Wp   =           86
74909
 YDOT =       6472
768643  meter/sec      RA   =           90
98662  deg
 ZDOT =      -3281
175822                 TA   =          150
35817
                                          MA   =          150
29657
                                          Ha   =            221
958  n
mi
                                          Hp   =            213
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11715385
09                 X    =         3632938
06
 Y    =      -11893034
71  feet           Y    =        -3584717
50  meter
 Z    =      -14736550
48                 Z    =        -4474204
28
 XDOT =       8042
724616                 XDOT =        2394
798261
 YDOT =      21236
117596  feet/sec       YDOT =        6499
865985  meter/sec
 ZDOT =     -10765
012539                 ZDOT =       -3269
404265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8758346
67                 X    =        -2669544
07
 Y    =      -14293459
63  feet           Y    =        -4356646
50  meter
 Z    =      -14657722
12                 Z    =        -4467673
70
 XDOT =      21510
409646                 XDOT =        6556
372860
 YDOT =      -2215
319961  feet/sec       YDOT =        -675
229524  meter/sec
 ZDOT =     -10713
255453                 ZDOT =       -3265
400262


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   18153
53935371  
00016717  00000-0  10270-3 0  9023
2 25544  51
6401  91
7390 0003374 142
3116 217
8273 15
54133805 36232


Satellite: ISS
Catalog Number: 25544
Epoch time:      18153
53935371   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:        91
7390  deg
Eccentricity:     
0003374     
Arg of perigee:   142
3116  deg
Mean anomaly:     217
8273  deg
Mean motion:   15
54133805  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3623
Checksum:              289


Coasting Arc #4 (Orbit 3636)
---------------------------------------

Vector Time (GMT): 2018/154/09:16:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3515933
79                 A    =         6779831
84  meter
 Y    =        3329642
75  meter          E    =           
0010855
 Z    =        4740689
24                 I    =           52
00527
 XDOT =      -2561
691049                 Wp   =          126
68075
 YDOT =      -6675
862684  meter/sec      RA   =           86
67505  deg
 ZDOT =       2778
238628                 TA   =          295
90475
                                          MA   =          296
01660
                                          Ha   =            221
929  n
mi
                                          Hp   =            213
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11535215
84                 X    =        -3575933
24
 Y    =       10924024
75  feet           Y    =         3289989
06  meter
 Z    =       15553442
38                 Z    =         4723464
74
 XDOT =      -8404
498192                 XDOT =       -2500
344564
 YDOT =     -21902
436627  feet/sec       YDOT =       -6704
166629  meter/sec
 ZDOT =       9114
956128                 ZDOT =        2765
942940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4607433
81                 X    =        -1404345
82
 Y    =       15283137
12  feet           Y    =         4658300
19  meter
 Z    =       15475863
94                 Z    =         4717043
33
 XDOT =     -17175
340350                 XDOT =       -5235
043739
 YDOT =     -14388
764320  feet/sec       YDOT =       -4385
695365  meter/sec
 ZDOT =       9060
889951                 ZDOT =        2761
759257


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   18154
43958439  
00016717  00000-0  10270-3 0  9034
2 25544  51
6379  87
2520 0003393 149
5773 210
5577 15
54145778 36374


Satellite: ISS
Catalog Number: 25544
Epoch time:      18154
43958439   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:        87
2520  deg
Eccentricity:     
0003393     
Arg of perigee:   149
5773  deg
Mean anomaly:     210
5577  deg
Mean motion:   15
54145778  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3637
Checksum:              342


Coasting Arc #5 (Orbit 3651)
---------------------------------------

Vector Time (GMT): 2018/155/09:16:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3938837
81                 A    =         6777662
59  meter
 Y    =       -1617797
23  meter          E    =           
0016021
 Z    =       -5286631
41                 I    =           51
99517
 XDOT =       1803
335058                 Wp   =           94
33389
 YDOT =       7384
425134  meter/sec      RA   =           81
70187  deg
 ZDOT =       -919
741771                 TA   =          166
91832
                                          MA   =          166
87672
                                          Ha   =            221
865  n
mi
                                          Hp   =            214
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12922696
22                 X    =         3982315
38
 Y    =       -5307733
71  feet           Y    =        -1573506
71  meter
 Z    =      -17344591
25                 Z    =        -5267392
50
 XDOT =       5916
453601                 XDOT =        1725
093986
 YDOT =      24227
116582  feet/sec       YDOT =        7404
153905  meter/sec
 ZDOT =      -3017
525497                 ZDOT =        -911
170957

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8437129
27                 X    =         2571637
00
 Y    =      -11268141
48  feet           Y    =        -3434529
52  meter
 Z    =      -17258238
55                 Z    =        -5260311
11
 XDOT =      16750
070049                 XDOT =        5105
421351
 YDOT =      17088
274112  feet/sec       YDOT =        5208
505949  meter/sec
 ZDOT =      -2980
245027                 ZDOT =        -908
378684


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   18155
40411758  
00016717  00000-0  10270-3 0  9041
2 25544  51
6383  82
4431 0003407 151
3898 208
7442 15
54117553 36529


Satellite: ISS
Catalog Number: 25544
Epoch time:      18155
40411758   =   yrday
fracday
Element set:     904
Inclination:       51
6383  deg
RA of node:        82
4431  deg
Eccentricity:     
0003407     
Arg of perigee:   151
3898  deg
Mean anomaly:     208
7442  deg
Mean motion:   15
54117553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3652
Checksum:              304


Coasting Arc #6 (Orbit 3667)
---------------------------------------

Vector Time (GMT): 2018/156/09:16:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4264879
91                 A    =         6777702
56  meter
 Y    =        -171187
60  meter          E    =           
0004621
 Z    =        5260832
24                 I    =           51
99034
 XDOT =       -958
316188                 Wp   =          102
63272
 YDOT =      -7543
265046  meter/sec      RA   =           76
72657  deg
 ZDOT =      -1022
581440                 TA   =          357
10486
                                          MA   =          357
10754
                                          Ha   =            221
925  n
mi
                                          Hp   =            214
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13992388
17                 X    =        -4288203
02
 Y    =        -561639
09  feet           Y    =         -219011
38  meter
 Z    =       17259948
30                 Z    =         5240058
27
 XDOT =      -3144
081981                 XDOT =        -868
926948
 YDOT =     -24748
244903  feet/sec       YDOT =       -7553
481685  meter/sec
 ZDOT =      -3354
925985                 ZDOT =       -1027
020289

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12259296
91                 X    =        -3736633
70
 Y    =        7000888
67  feet           Y    =         2133870
87  meter
 Z    =       17166985
10                 Z    =         5232497
06
 XDOT =     -15252
891270                 XDOT =       -4649
081259
 YDOT =     -18438
647780  feet/sec       YDOT =       -5620
099843  meter/sec
 ZDOT =      -3373
676491                 ZDOT =       -1028
296595


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   18156
43294854  
00016717  00000-0  10270-3 0  9052
2 25544  51
6390  77
3147 0003306 154
7890 205
3425 15
54125428 36682


Satellite: ISS
Catalog Number: 25544
Epoch time:      18156
43294854   =   yrday
fracday
Element set:     905
Inclination:       51
6390  deg
RA of node:        77
3147  deg
Eccentricity:     
0003306     
Arg of perigee:   154
7890  deg
Mean anomaly:     205
3425  deg
Mean motion:   15
54125428  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3668
Checksum:              318


Coasting Arc #7 (Orbit 3673)
---------------------------------------

Vector Time (GMT): 2018/156/19:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4062030
01                 A    =         6783776
01  meter
 Y    =        4043187
57  meter          E    =           
0007962
 Z    =       -3639049
83                 I    =           52
00660
 XDOT =      -1949
751942                 Wp   =          121
29702
 YDOT =       5939
531467  meter/sec      RA   =           74
59966  deg
 ZDOT =       4425
881485                 TA   =          195
84663
                                          MA   =          195
87156
                                          Ha   =            221
833  n
mi
                                          Hp   =            214
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13326870
11                 X    =         4034192
67
 Y    =       13265051
10  feet           Y    =         4088456
71  meter
 Z    =      -11939139
85                 Z    =        -3619385
09
 XDOT =      -6396
823956                 XDOT =       -2037
523104
 YDOT =      19486
651794  feet/sec       YDOT =        5917
236798  meter/sec
 ZDOT =      14520
608548                 ZDOT =        4416
197672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14572940
84                 X    =        -4441832
37
 Y    =      -11969806
76  feet           Y    =        -3648397
10  meter
 Z    =      -11851718
40                 Z    =        -3612403
77
 XDOT =       3793
062176                 XDOT =        1156
125351
 YDOT =     -18941
343720  feet/sec       YDOT =       -5773
321566  meter/sec
 ZDOT =      14476
376670                 ZDOT =        4412
399609


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   18156
81875918  
00016717  00000-0  10270-3 0  9061
2 25544  51
6382  75
3876 0003706 156
8528 203
2792 15
54137797 36748


Satellite: ISS
Catalog Number: 25544
Epoch time:      18156
81875918   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:        75
3876  deg
Eccentricity:     
0003706     
Arg of perigee:   156
8528  deg
Mean anomaly:     203
2792  deg
Mean motion:   15
54137797  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3674
Checksum:              353


Coasting Arc #8 (Orbit 3684)
---------------------------------------

Vector Time (GMT): 2018/157/11:12:41
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -95822
82                 A    =         6786314
02  meter
 Y    =        6235838
66  meter          E    =           
0014463
 Z    =        2663369
76                 I    =           52
01057
 XDOT =      -5097
961332                 Wp   =           90
42261
 YDOT =      -2325
455175  meter/sec      RA   =           71
39742  deg
 ZDOT =       5236
680876                 TA   =          299
46662
                                          MA   =          299
61084
                                          Ha   =            221
698  n
mi
                                          Hp   =            214
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -314379
32                 X    =         -178483
81
 Y    =       20458788
25  feet           Y    =         6234304
67  meter
 Z    =        8738089
77                 Z    =         2662704
09
 XDOT =     -16725
594922                 XDOT =       -5097
015634
 YDOT =      -7629
446113  feet/sec       YDOT =       -2382
459286  meter/sec
 ZDOT =      17180
711535                 ZDOT =        5211
918791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17909755
19                 X    =         5458893
38
 Y    =        9897975
95  feet           Y    =         3016903
07  meter
 Z    =        8734174
55                 Z    =         2662176
40
 XDOT =     -13896
218305                 XDOT =       -4235
567339
 YDOT =      10010
041443  feet/sec       YDOT =        3051
060632  meter/sec
 ZDOT =      17070
219514                 ZDOT =        5203
002908


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   18157
52607853  
00016717  00000-0  10270-3 0  9072
2 25544  51
6397  71
8660 0003246 158
3443 201
7848 15
54133284 36852


Satellite: ISS
Catalog Number: 25544
Epoch time:      18157
52607853   =   yrday
fracday
Element set:     907
Inclination:       51
6397  deg
RA of node:        71
8660  deg
Eccentricity:     
0003246     
Arg of perigee:   158
3443  deg
Mean anomaly:     201
7848  deg
Mean motion:   15
54133284  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3685
Checksum:              328


Coasting Arc #9 (Orbit 3699)
---------------------------------------

Vector Time (GMT): 2018/158/11:12:41
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1085673
03                 A    =         6782442
38  meter
 Y    =       -5361802
71  meter          E    =           
0007663
 Z    =       -4015104
61                 I    =           51
98752
 XDOT =       5156
800726                 Wp   =           96
67525
 YDOT =       4025
633132  meter/sec      RA   =           66
43978  deg
 ZDOT =      -3988
855977                 TA   =          132
00035
                                          MA   =          131
93507
                                          Ha   =            221
598  n
mi
                                          Hp   =            214
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3561919
38                 X    =         1165052
82
 Y    =      -17591216
23  feet           Y    =        -5349217
78  meter
 Z    =      -13172915
40                 Z    =        -4009638
43
 XDOT =      16918
637552                 XDOT =        5130
777563
 YDOT =      13207
457782  feet/sec       YDOT =        4083
154866  meter/sec
 ZDOT =     -13086
797825                 ZDOT =       -3963
868790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14037841
12                 X    =        -4278733
97
 Y    =      -11213500
22  feet           Y    =        -3417874
87  meter
 Z    =      -13147634
30                 Z    =        -4007398
94
 XDOT =      18653
313816                 XDOT =        5685
530051
 YDOT =      -8166
333073  feet/sec       YDOT =       -2489
098321  meter/sec
 ZDOT =     -12975
561367                 ZDOT =       -3954
951105


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   18158
49060212  
00016717  00000-0  10270-3 0  9082
2 25544  51
6408  67
0578 0003184 162
2036 197
9229 15
54156739 37000


Satellite: ISS
Catalog Number: 25544
Epoch time:      18158
49060212   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:        67
0578  deg
Eccentricity:     
0003184     
Arg of perigee:   162
2036  deg
Mean anomaly:     197
9229  deg
Mean motion:   15
54156739  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3700
Checksum:              316


Coasting Arc #10 (Orbit 3715)
---------------------------------------

Vector Time (GMT): 2018/159/11:12:41
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2120519
11                 A    =         6779010
38  meter
 Y    =        4153482
43  meter          E    =           
0009227
 Z    =        4916928
73                 I    =           51
96227
 XDOT =      -4988
334045                 Wp   =          135
87266
 YDOT =      -5334
187238  meter/sec      RA   =           61
47125  deg
 ZDOT =       2345
550002                 TA   =          291
23280
                                          MA   =          291
33133
                                          Ha   =            221
551  n
mi
                                          Hp   =            214
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6957083
71                 X    =        -2190690
90
 Y    =       13626910
86  feet           Y    =         4129376
55  meter
 Z    =       16131655
93                 Z    =         4906457
83
 XDOT =     -16365
925344                 XDOT =       -4939
708482
 YDOT =     -17500
614298  feet/sec       YDOT =       -5389
698544  meter/sec
 ZDOT =       7695
374022                 ZDOT =        2321
435884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9170872
80                 X    =         2795282
03
 Y    =       12309315
99  feet           Y    =         3751879
52  meter
 Z    =       16084149
60                 Z    =         4902448
80
 XDOT =     -22017
172922                 XDOT =       -6710
834307
 YDOT =       6449
177834  feet/sec       YDOT =        1965
709404  meter/sec
 ZDOT =       7588
256452                 ZDOT =        2312
900567


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   18159
51942264  
00016717  00000-0  10270-3 0  9093
2 25544  51
6411  61
9292 0003232 167
8824 192
2407 15
54167892 37165


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
51942264   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:        61
9292  deg
Eccentricity:     
0003232     
Arg of perigee:   167
8824  deg
Mean anomaly:     192
2407  deg
Mean motion:   15
54167892  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              322


Coasting Arc #11 (Orbit 3716)
---------------------------------------

Vector Time (GMT): 2018/159/13:07:21
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4579710
45                 A    =         6786902
40  meter
 Y    =       -4374009
08  meter          E    =           
0015639
 Z    =        2416788
83                 I    =           51
98814
 XDOT =       2000
622424                 Wp   =          116
36092
 YDOT =      -5083
199085  meter/sec      RA   =           61
03853  deg
 ZDOT =      -5388
596306                 TA   =           36
73276
                                          MA   =           36
62568
                                          Ha   =            221
633  n
mi
                                          Hp   =            214
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15025296
77                 X    =        -4542198
28
 Y    =      -14350423
48  feet           Y    =        -4425013
02  meter
 Z    =        7929097
22                 Z    =         2394632
76
 XDOT =       6563
721865                 XDOT =        2083
490606
 YDOT =     -16677
162354  feet/sec       YDOT =       -5060
362943  meter/sec
 ZDOT =     -17679
121740                 ZDOT =       -5378
677064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13587591
70                 X    =        -4141497
95
 Y    =       15767811
32  feet           Y    =         4806028
89  meter
 Z    =        7830597
53                 Z    =         2386766
13
 XDOT =     -15838
376071                 XDOT =       -4827
537026
 YDOT =      -4857
877351  feet/sec       YDOT =       -1480
681017  meter/sec
 ZDOT =     -17633
941079                 ZDOT =       -5374
825241


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   18159
58372487  
00016717  00000-0  10270-3 0  9106
2 25544  51
6423  61
6097 0003226 166
5998 193
5240 15
54133122 37178


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
58372487   =   yrday
fracday
Element set:     910
Inclination:       51
6423  deg
RA of node:        61
6097  deg
Eccentricity:     
0003226     
Arg of perigee:   166
5998  deg
Mean anomaly:     193
5240  deg
Mean motion:   15
54133122  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3717
Checksum:              318


Coasting Arc #12 (Orbit 3731)
---------------------------------------

Vector Time (GMT): 2018/160/13:07:21
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4255721
44                 A    =         6788954
14  meter
 Y    =        5227207
06  meter          E    =           
0008603
 Z    =        -787191
77                 I    =           51
97847
 XDOT =      -3249
697930                 Wp   =           55
08378
 YDOT =       3537
652896  meter/sec      RA   =           56
08845  deg
 ZDOT =       5973
497409                 TA   =          296
44893
                                          MA   =          296
53717
                                          Ha   =            221
392  n
mi
                                          Hp   =            214
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13962340
68                 X    =         4200776
88
 Y    =       17149629
45  feet           Y    =         5274490
33  meter
 Z    =       -2582650
16                 Z    =         -766651
69
 XDOT =     -10661
738616                 XDOT =       -3318
031807
 YDOT =      11606
472757  feet/sec       YDOT =        3500
929892  meter/sec
 ZDOT =      19598
088612                 ZDOT =        5957
545700

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16180887
99                 X    =         4931934
66
 Y    =      -15089664
67  feet           Y    =        -4599329
79  meter
 Z    =       -2491528
32                 Z    =         -759417
83
 XDOT =      11200
248460                 XDOT =        3413
835731
 YDOT =       8814
719723  feet/sec       YDOT =        2686
726572  meter/sec
 ZDOT =      19526
138670                 ZDOT =        5951
567067


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   18160
54824044  
00016717  00000-0  10270-3 0  9116
2 25544  51
6422  56
8011 0003112 172
2837 187
8364 15
54171599 37329


Satellite: ISS
Catalog Number: 25544
Epoch time:      18160
54824044   =   yrday
fracday
Element set:     911
Inclination:       51
6422  deg
RA of node:        56
8011  deg
Eccentricity:     
0003112     
Arg of perigee:   172
2837  deg
Mean anomaly:     187
8364  deg
Mean motion:   15
54171599  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3732
Checksum:              299


Coasting Arc #13 (Orbit 3747)
---------------------------------------

Vector Time (GMT): 2018/161/13:07:21
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3600489
11                 A    =         6788951
50  meter
 Y    =       -5667022
85  meter          E    =           
0012561
 Z    =        -960805
63                 I    =           51
95866
 XDOT =       4482
591341                 Wp   =          149
84834
 YDOT =      -1847
889446  meter/sec      RA   =           51
14160  deg
 ZDOT =      -5942
822301                 TA   =           40
51390
                                          MA   =           40
42046
                                          Ha   =            221
397  n
mi
                                          Hp   =            214
554

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11812628
31                 X    =        -3532184
16
 Y    =      -18592594
64  feet           Y    =        -5706903
97  meter
 Z    =       -3152249
45                 Z    =         -978130
51
 XDOT =      14706
664504                 XDOT =        4531
789251
 YDOT =      -6062
629415  feet/sec       YDOT =       -1797
486276  meter/sec
 ZDOT =     -19497
448493                 ZDOT =       -5920
927858

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17540432
22                 X    =        -5346323
74
 Y    =       13306648
77  feet           Y    =         4055866
54  meter
 Z    =       -3228897
00                 Z    =         -984167
81
 XDOT =      -6314
547328                 XDOT =       -1924
674026
 YDOT =     -12996
609056  feet/sec       YDOT =       -3961
366440  meter/sec
 ZDOT =     -19399
161235                 ZDOT =       -5912
864344


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   18161
57705683  
00016717  00000-0  10270-3 0  9128
2 25544  51
6421  51
6731 0003259 177
7925 182
3242 15
54117031 37483


Satellite: ISS
Catalog Number: 25544
Epoch time:      18161
57705683   =   yrday
fracday
Element set:     912
Inclination:       51
6421  deg
RA of node:        51
6731  deg
Eccentricity:     
0003259     
Arg of perigee:   177
7925  deg
Mean anomaly:     182
3242  deg
Mean motion:   15
54117031  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3748
Checksum:              305


Coasting Arc #14 (Orbit 3763)
---------------------------------------

Vector Time (GMT): 2018/162/13:07:21
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2660077
63                 A    =         6786391
44  meter
 Y    =        5683375
34  meter          E    =           
0013136
 Z    =        2572530
95                 I    =           51
92926
 XDOT =      -5551
749311                 Wp   =           88
89811
 YDOT =        194
936767  meter/sec      RA   =           46
18814  deg
 ZDOT =       5287
012610                 TA   =          299
90690
                                          MA   =          300
03731
                                          Ha   =            221
183  n
mi
                                          Hp   =            214
579

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8727288
83                 X    =         2583830
70
 Y    =       18646244
57  feet           Y    =         5712695
50  meter
 Z    =        8440062
18                 Z    =         2585268
43
 XDOT =     -18214
400628                 XDOT =       -5579
198393
 YDOT =        639
556321  feet/sec       YDOT =         132
699096  meter/sec
 ZDOT =      17345
841897                 ZDOT =        5259
977123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17677412
04                 X    =         5388075
19
 Y    =      -10507474
25  feet           Y    =        -3202678
15  meter
 Z    =        8496160
59                 Z    =         2589629
75
 XDOT =       1719
848686                 XDOT =         524
209879
 YDOT =      16881
719569  feet/sec       YDOT =        5145
548125  meter/sec
 ZDOT =      17224
807708                 ZDOT =        5250
121389


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   18162
60586792  
00016717  00000-0  10270-3 0  9132
2 25544  51
6423  46
5437 0002962 182
7054 177
4083 15
54162111 37645


Satellite: ISS
Catalog Number: 25544
Epoch time:      18162
60586792   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:        46
5437  deg
Eccentricity:     
0002962     
Arg of perigee:   182
7054  deg
Mean anomaly:     177
4083  deg
Mean motion:   15
54162111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3764
Checksum:              311


Coasting Arc #15 (Orbit 3778)
---------------------------------------

Vector Time (GMT): 2018/163/13:07:21
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1396267
24                 A    =         6782604
40  meter
 Y    =       -5339455
25  meter          E    =           
0006156
 Z    =       -3947117
51                 I    =           51
89198
 XDOT =       6358
998024                 Wp   =           99
02515
 YDOT =       1335
466862  meter/sec      RA   =           41
22448  deg
 ZDOT =      -4062
340358                 TA   =          128
64737
                                          MA   =          128
59226
                                          Ha   =            221
118  n
mi
                                          Hp   =            214
662

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4580929
26                 X    =        -1317282
97
 Y    =      -17517897
79  feet           Y    =        -5354627
02  meter
 Z    =      -12949860
61                 Z    =        -3953709
18
 XDOT =      20862
854411                 XDOT =        6363
324796
 YDOT =       4381
452958  feet/sec       YDOT =        1406
602389  meter/sec
 ZDOT =     -13327
888313                 ZDOT =       -4031
439452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16866496
48                 X    =        -5140908
13
 Y    =        6529969
55  feet           Y    =         1990334
72  meter
 Z    =      -12978495
28                 Z    =        -3955845
36
 XDOT =       2354
970418                 XDOT =         717
794983
 YDOT =     -20091
136563  feet/sec       YDOT =       -6123
778424  meter/sec
 ZDOT =     -13189
803362                 ZDOT =       -4020
252065


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   18163
57037559  
00016717  00000-0  10270-3 0  9142
2 25544  51
6412  41
7351 0002977 187
0698 173
0414 15
54160335 37795


Satellite: ISS
Catalog Number: 25544
Epoch time:      18163
57037559   =   yrday
fracday
Element set:     914
Inclination:       51
6412  deg
RA of node:        41
7351  deg
Eccentricity:     
0002977     
Arg of perigee:   187
0698  deg
Mean anomaly:     173
0414  deg
Mean motion:   15
54160335  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3779
Checksum:              321


Coasting Arc #16 (Orbit 3792)
---------------------------------------

Vector Time (GMT): 2018/164/10:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -73562
63                 A    =         6779324
65  meter
 Y    =       -4776847
51  meter          E    =           
0010553
 Z    =       -4819311
83                 I    =           51
85923
 XDOT =       6759
445570                 Wp   =           86
17245
 YDOT =       2505
638463  meter/sec      RA   =           36
73212  deg
 ZDOT =      -2590
935861                 TA   =          158
37965
                                          MA   =          158
33506
                                          Ha   =            221
066  n
mi
                                          Hp   =            214
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -241347
20                 X    =            3268
73
 Y    =      -15672071
88  feet           Y    =        -4777239
70  meter
 Z    =      -15811390
52                 Z    =        -4819483
40
 XDOT =      22176
658693                 XDOT =        6743
509963
 YDOT =       8220
598633  feet/sec       YDOT =        2581
138591  meter/sec
 ZDOT =      -8500
445738                 ZDOT =       -2558
138798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14005814
18                 X    =        -4268972
16
 Y    =       -7036317
92  feet           Y    =        -2144669
70  meter
 Z    =      -15811374
23                 Z    =        -4819306
87
 XDOT =      16952
916684                 XDOT =        5167
249005
 YDOT =     -15003
283938  feet/sec       YDOT =       -4573
000944  meter/sec
 ZDOT =      -8354
068632                 ZDOT =       -2546
320119


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   18164
47058227  
00016717  00000-0  10270-3 0  9158
2 25544  51
6421  37
2485 0002967 188
0661 172
0444 15
54187671 37933


Satellite: ISS
Catalog Number: 25544
Epoch time:      18164
47058227   =   yrday
fracday
Element set:     915
Inclination:       51
6421  deg
RA of node:        37
2485  deg
Eccentricity:     
0002967     
Arg of perigee:   188
0661  deg
Mean anomaly:     172
0444  deg
Mean motion:   15
54187671  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3793
Checksum:              325


Coasting Arc #17 (Orbit 3808)
---------------------------------------

Vector Time (GMT): 2018/165/10:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1500795
45                 A    =         6777315
95  meter
 Y    =        3961239
98  meter          E    =           
0004762
 Z    =        5289055
09                 I    =           51
82582
 XDOT =      -6772
676079                 Wp   =          154
37465
 YDOT =      -3528
404613  meter/sec      RA   =           31
74797  deg
 ZDOT =        716
389827                 TA   =          288
77622
                                          MA   =          288
82788
                                          Ha   =            221
025  n
mi
                                          Hp   =            214
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4923869
60                 X    =        -1570671
09
 Y    =       12996194
15  feet           Y    =         3944065
37  meter
 Z    =       17352542
94                 Z    =         5281595
74
 XDOT =     -22220
065876                 XDOT =       -6736
196986
 YDOT =     -11576
130620  feet/sec       YDOT =       -3603
937506  meter/sec
 ZDOT =       2350
360326                 ZDOT =         683
578364

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9439714
88                 X    =         2877225
10
 Y    =       10257563
03  feet           Y    =         3126505
21  meter
 Z    =       17318501
22                 Z    =         5278679
17
 XDOT =     -19452
505852                 XDOT =       -5929
123784
 YDOT =      14155
638476  feet/sec       YDOT =        4314
638608  meter/sec
 ZDOT =       2204
090811                 ZDOT =         671
806879


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   18165
49938589  
00016717  00000-0  10270-3 0  9160
2 25544  51
6425  32
1196 0003054 192
9111 167
1964 15
54190387 38090


Satellite: ISS
Catalog Number: 25544
Epoch time:      18165
49938589   =   yrday
fracday
Element set:     916
Inclination:       51
6425  deg
RA of node:        32
1196  deg
Eccentricity:     
0003054     
Arg of perigee:   192
9111  deg
Mean anomaly:     167
1964  deg
Mean motion:   15
54190387  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3809
Checksum:              334


Coasting Arc #18 (Orbit 3823)
---------------------------------------

Vector Time (GMT): 2018/166/10:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3103064
08                 A    =         6777709
54  meter
 Y    =       -3034289
98  meter          E    =           
0013930
 Z    =       -5218023
82                 I    =           51
79812
 XDOT =       6249
590723                 Wp   =          111
33145
 YDOT =       4247
800721  meter/sec      RA   =           26
75880  deg
 ZDOT =       1244
148290                 TA   =          170
61253
                                          MA   =          170
58647
                                          Ha   =            220
873  n
mi
                                          Hp   =            214
916

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10180656
44                 X    =         3162110
04
 Y    =       -9955019
62  feet           Y    =        -2999258
28  meter
 Z    =      -17119500
71                 Z    =        -5202807
40
 XDOT =      20503
906570                 XDOT =        6195
582774
 YDOT =      13936
354070  feet/sec       YDOT =        4317
385744  meter/sec
 ZDOT =       4081
851346                 ZDOT =        1274
376142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4625322
04                 X    =        -1409798
16
 Y    =      -13553559
96  feet           Y    =        -4131125
08  meter
 Z    =      -17050891
31                 Z    =        -5197111
67
 XDOT =      20340
954064                 XDOT =        6199
922799
 YDOT =     -12255
432229  feet/sec       YDOT =       -3735
455743  meter/sec
 ZDOT =       4216
435242                 ZDOT =        1285
169462


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   18166
46388663  
00016717  00000-0  10270-3 0  9171
2 25544  51
6422  27
3107 0002905 197
5494 162
5559 15
54195580 38240


Satellite: ISS
Catalog Number: 25544
Epoch time:      18166
46388663   =   yrday
fracday
Element set:     917
Inclination:       51
6422  deg
RA of node:        27
3107  deg
Eccentricity:     
0002905     
Arg of perigee:   197
5494  deg
Mean anomaly:     162
5559  deg
Mean motion:   15
54195580  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3824
Checksum:              335


Coasting Arc #19 (Orbit 3839)
---------------------------------------

Vector Time (GMT): 2018/167/10:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4550021
10                 A    =         6780258
92  meter
 Y    =        2064911
42  meter          E    =           
0006943
 Z    =        4577656
46                 I    =           51
77630
 XDOT =      -5229
328093                 Wp   =           82
86806
 YDOT =      -4696
195872  meter/sec      RA   =           21
77274  deg
 ZDOT =      -3074
542728                 TA   =           37
82987
                                          MA   =           37
78110
                                          Ha   =            220
835  n
mi
                                          Hp   =            214
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14927890
76                 X    =        -4595009
00
 Y    =        6774643
76  feet           Y    =         2013777
64  meter
 Z    =       15018557
95                 Z    =         4555445
29
 XDOT =     -17156
588231                 XDOT =       -5161
490905
 YDOT =     -15407
466771  feet/sec       YDOT =       -4754
294006  meter/sec
 ZDOT =     -10087
082440                 ZDOT =       -3099
780814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          15585
20                 X    =            4750
37
 Y    =       16484048
75  feet           Y    =         5024338
06  meter
 Z    =       14918803
48                 Z    =         4547251
30
 XDOT =     -19860
253341                 XDOT =       -6053
405218
 YDOT =       9264
009053  feet/sec       YDOT =        2823
669959  meter/sec
 ZDOT =     -10199
256725                 ZDOT =       -3108
733450


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   18167
49268432  
00016717  00000-0  10270-3 0  9187
2 25544  51
6415  22
1819 0002842 203
4128 156
6895 15
54227665 38401


Satellite: ISS
Catalog Number: 25544
Epoch time:      18167
49268432   =   yrday
fracday
Element set:     918
Inclination:       51
6415  deg
RA of node:        22
1819  deg
Eccentricity:     
0002842     
Arg of perigee:   203
4128  deg
Mean anomaly:     156
6895  deg
Mean motion:   15
54227665  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3840
Checksum:              322
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