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

 
Date: May 31st 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 3575)
---------------------------------------

Vector Time (GMT): 2018/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4183137
12                 A    =         6777563
51  meter
 Y    =         506948
25  meter          E    =           
0017225
 Z    =       -5323140
46                 I    =           51
98181
 XDOT =      -1648
805805                 Wp   =           94
15048
 YDOT =       7453
002930  meter/sec      RA   =          105
93156  deg
 ZDOT =       -588
761298                 TA   =          170
26434
                                          MA   =          170
23092
                                          Ha   =            222
120  n
mi
                                          Hp   =            213
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13724203
15                 X    =         4203014
70
 Y    =        1663216
03  feet           Y    =          553838
84  meter
 Z    =      -17464371
59                 Z    =        -5302771
63
 XDOT =      -5409
467864                 XDOT =       -1729
164854
 YDOT =      24452
109350  feet/sec       YDOT =        7434
115613  meter/sec
 ZDOT =      -1931
631554                 ZDOT =        -596
964885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6920983
21                 X    =         2109515
68
 Y    =      -12099289
30  feet           Y    =        -3687863
38  meter
 Z    =      -17373298
61                 Z    =        -5295381
42
 XDOT =      19536
719999                 XDOT =        5954
792256
 YDOT =      13989
612018  feet/sec       YDOT =        4264
033743  meter/sec
 ZDOT =      -1969
360475                 ZDOT =        -600
261073


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   18150
51713072  
00016717  00000-0  10270-3 0  9008
2 25544  51
6380 106
8032 0003494 133
3371 226
8074 15
54099358 35765


Satellite: ISS
Catalog Number: 25544
Epoch time:      18150
51713072   =   yrday
fracday
Element set:     900
Inclination:       51
6380  deg
RA of node:       106
8032  deg
Eccentricity:     
0003494     
Arg of perigee:   133
3371  deg
Mean anomaly:     226
8074  deg
Mean motion:   15
54099358  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3576
Checksum:              297


Coasting Arc #2 (Orbit 3591)
---------------------------------------

Vector Time (GMT): 2018/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3706288
59                 A    =         6777993
24  meter
 Y    =       -2252175
01  meter          E    =           
0005910
 Z    =        5203768
22                 I    =           51
99200
 XDOT =       2453
121689                 Wp   =           90
96923
 YDOT =      -7145
074038  meter/sec      RA   =          100
95701  deg
 ZDOT =      -1343
960626                 TA   =           11
88168
                                          MA   =           11
86774
                                          Ha   =            222
207  n
mi
                                          Hp   =            213
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12159739
47                 X    =        -3706106
08
 Y    =       -7389025
62  feet           Y    =        -2293621
01  meter
 Z    =       17072730
37                 Z    =         5185764
31
 XDOT =       8048
299504                 XDOT =        2539
365849
 YDOT =     -23441
843956  feet/sec       YDOT =       -7117
159129  meter/sec
 ZDOT =      -4409
319638                 ZDOT =       -1331
835654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11437651
71                 X    =        -3486196
24
 Y    =        8623859
08  feet           Y    =         2628552
25  meter
 Z    =       16992476
68                 Z    =         5179306
89
 XDOT =     -18098
303094                 XDOT =       -5516
362783
 YDOT =     -15416
266883  feet/sec       YDOT =       -4698
878146  meter/sec
 ZDOT =      -4354
064480                 ZDOT =       -1327
118853


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   18151
54597554  
00016717  00000-0  10270-3 0  9018
2 25544  51
6386 101
6756 0003477 137
1598 222
9826 15
54105649 35922


Satellite: ISS
Catalog Number: 25544
Epoch time:      18151
54597554   =   yrday
fracday
Element set:     901
Inclination:       51
6386  deg
RA of node:       101
6756  deg
Eccentricity:     
0003477     
Arg of perigee:   137
1598  deg
Mean anomaly:     222
9826  deg
Mean motion:   15
54105649  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3592
Checksum:              334


Coasting Arc #3 (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    =        3183545
28                 A    =         6780636
78  meter
 Y    =        3880747
88  meter          E    =           
0012862
 Z    =       -4571657
36                 I    =           52
00682
 XDOT =      -3118
265933                 Wp   =          118
23297
 YDOT =       6251
201772  meter/sec      RA   =           95
98602  deg
 ZDOT =       3135
795850                 TA   =          183
07092
                                          MA   =          183
07883
                                          Ha   =            221
982  n
mi
                                          Hp   =            213
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10444702
35                 X    =         3162119
91
 Y    =       12732112
48  feet           Y    =         3916229
34  meter
 Z    =      -14998875
86                 Z    =        -4556244
20
 XDOT =     -10230
531275                 XDOT =       -3203
168951
 YDOT =      20509
192166  feet/sec       YDOT =        6215
856004  meter/sec
 ZDOT =      10288
044126                 ZDOT =        3120
442989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15659421
34                 X    =         4772991
63
 Y    =       -5294251
15  feet           Y    =        -1613687
75  meter
 Z    =      -14930445
41                 Z    =        -4550799
76
 XDOT =      15085
325797                 XDOT =        4598
007303
 YDOT =      15809
616269  feet/sec       YDOT =        4818
771039  meter/sec
 ZDOT =      10218
449528                 ZDOT =        3114
583416


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
51051430  
00016717  00000-0  10270-3 0  9025
2 25544  51
6393  96
8675 0003390 141
7330 218
4064 15
54105838 36075


Satellite: ISS
Catalog Number: 25544
Epoch time:      18152
51051430   =   yrday
fracday
Element set:     902
Inclination:       51
6393  deg
RA of node:        96
8675  deg
Eccentricity:     
0003390     
Arg of perigee:   141
7330  deg
Mean anomaly:     218
4064  deg
Mean motion:   15
54105838  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3607
Checksum:              294


Coasting Arc #4 (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    =       -2591974
39                 A    =         6784361
27  meter
 Y    =       -5232107
16  meter          E    =           
0014624
 Z    =        3439564
95                 I    =           52
02233
 XDOT =       3697
910517                 Wp   =          100
26471
 YDOT =      -4881
223955  meter/sec      RA   =           91
02466  deg
 ZDOT =      -4624
341412                 TA   =           39
65188
                                          MA   =           39
54503
                                          Ha   =            221
989  n
mi
                                          Hp   =            213
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8503853
00                 X    =        -2549982
54
 Y    =      -17165705
89  feet           Y    =        -5260858
08  meter
 Z    =       11284661
92                 Z    =         3427075
27
 XDOT =      12132
252352                 XDOT =        3774
681534
 YDOT =     -16014
514287  feet/sec       YDOT =       -4839
441481  meter/sec
 ZDOT =     -15171
723794                 ZDOT =       -4606
192403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19062313
15                 X    =        -5810193
05
 Y    =        2201552
20  feet           Y    =          671033
11  meter
 Z    =       11229512
66                 Z    =         3422755
46
 XDOT =     -10715
598106                 XDOT =       -3266
114303
 YDOT =     -15575
954368  feet/sec       YDOT =       -4747
550891  meter/sec
 ZDOT =     -15089
793945                 ZDOT =       -4599
369194


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
53935313  
00016717  00000-0  10270-3 0  9030
2 25544  51
6398  91
7390 0003326 143
1230 217
0152 15
54127066 36230


Satellite: ISS
Catalog Number: 25544
Epoch time:      18153
53935313   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:        91
7390  deg
Eccentricity:     
0003326     
Arg of perigee:   143
1230  deg
Mean anomaly:     217
0152  deg
Mean motion:   15
54127066  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3623
Checksum:              284


Coasting Arc #5 (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    =        3570959
30                 A    =         6780866
72  meter
 Y    =       -3624737
11  meter          E    =           
0010867
 Z    =       -4491831
20                 I    =           52
01098
 XDOT =       2451
244563                 Wp   =           86
75574
 YDOT =       6472
950744  meter/sec      RA   =           90
98661  deg
 ZDOT =      -3280
938274                 TA   =          150
35415
                                          MA   =          150
29252
                                          Ha   =            221
962  n
mi
                                          Hp   =            213
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11715745
75                 X    =         3633045
71
 Y    =      -11892182
11  feet           Y    =        -3584456
41  meter
 Z    =      -14736979
00                 Z    =        -4474334
37
 XDOT =       8042
140956                 XDOT =        2394
617184
 YDOT =      21236
715039  feet/sec       YDOT =        6500
046078  meter/sec
 ZDOT =     -10764
233181                 ZDOT =       -3269
167588

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8757432
28                 X    =        -2669265
36
 Y    =      -14293610
88  feet           Y    =        -4356692
59  meter
 Z    =      -14658148
31                 Z    =        -4467803
60
 XDOT =      21510
839682                 XDOT =        6556
503935
 YDOT =      -2214
673081  feet/sec       YDOT =        -675
032355  meter/sec
 ZDOT =     -10712
480023                 ZDOT =       -3265
163911


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
53935327  
00016717  00000-0  10270-3 0  9046
2 25544  51
6400  91
7389 0003378 142
2574 217
8816 15
54132793 36238


Satellite: ISS
Catalog Number: 25544
Epoch time:      18153
53935327   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:        91
7389  deg
Eccentricity:     
0003378     
Arg of perigee:   142
2574  deg
Mean anomaly:     217
8816  deg
Mean motion:   15
54132793  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3623
Checksum:              318


Coasting Arc #6 (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    =       -3515918
80                 A    =         6779834
90  meter
 Y    =        3329703
85  meter          E    =           
0010860
 Z    =        4740658
15                 I    =           52
00517
 XDOT =      -2561
736667                 Wp   =          126
67064
 YDOT =      -6675
826148  meter/sec      RA   =           86
67503  deg
 ZDOT =       2778
287558                 TA   =          295
91427
                                          MA   =          296
02616
                                          Ha   =            221
933  n
mi
                                          Hp   =            213
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11535166
65                 X    =        -3575918
78
 Y    =       10924225
24  feet           Y    =         3290050
33  meter
 Z    =       15553340
40                 Z    =         4723433
72
 XDOT =      -8404
647857                 XDOT =       -2500
390825
 YDOT =     -21902
316758  feet/sec       YDOT =       -6704
130607  meter/sec
 ZDOT =       9115
116661                 ZDOT =        2765
991647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4607290
30                 X    =        -1404302
08
 Y    =       15283285
73  feet           Y    =         4658345
49  meter
 Z    =       15475762
27                 Z    =         4717012
34
 XDOT =     -17175
400001                 XDOT =       -5235
061920
 YDOT =     -14388
595562  feet/sec       YDOT =       -4385
643927  meter/sec
 ZDOT =       9061
049480                 ZDOT =        2761
807882


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
43958453  
00016717  00000-0  10270-3 0  9052
2 25544  51
6378  87
2520 0003396 149
5186 210
6164 15
54144770 36378


Satellite: ISS
Catalog Number: 25544
Epoch time:      18154
43958453   =   yrday
fracday
Element set:     905
Inclination:       51
6378  deg
RA of node:        87
2520  deg
Eccentricity:     
0003396     
Arg of perigee:   149
5186  deg
Mean anomaly:     210
6164  deg
Mean motion:   15
54144770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3637
Checksum:              324


Coasting Arc #7 (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    =        3938735
55                 A    =         6777665
83  meter
 Y    =       -1618270
02  meter          E    =           
0016026
 Z    =       -5286570
30                 I    =           51
99507
 XDOT =       1803
656789                 Wp   =           94
33627
 YDOT =       7384
288498  meter/sec      RA   =           81
70186  deg
 ZDOT =       -920
168844                 TA   =          166
91184
                                          MA   =          166
87020
                                          Ha   =            221
869  n
mi
                                          Hp   =            214
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12922360
72                 X    =         3982218
11
 Y    =       -5309284
84  feet           Y    =        -1573980
61  meter
 Z    =      -17344390
76                 Z    =        -5267331
87
 XDOT =       5917
509151                 XDOT =        1725
419296
 YDOT =      24226
668302  feet/sec       YDOT =        7404
020887  meter/sec
 ZDOT =      -3018
926655                 ZDOT =        -911
596459

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8436041
31                 X    =         2571305
39
 Y    =      -11269297
22  feet           Y    =        -3434881
79  meter
 Z    =      -17258040
16                 Z    =        -5260250
64
 XDOT =      16750
667250                 XDOT =        5105
603378
 YDOT =      17087
420472  feet/sec       YDOT =        5208
245760  meter/sec
 ZDOT =      -2981
639130                 ZDOT =        -908
803607


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
40411834  
00016717  00000-0  10270-3 0  9068
2 25544  51
6382  82
4430 0003411 151
3338 208
8003 15
54116540 36520


Satellite: ISS
Catalog Number: 25544
Epoch time:      18155
40411834   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:        82
4430  deg
Eccentricity:     
0003411     
Arg of perigee:   151
3338  deg
Mean anomaly:     208
8003  deg
Mean motion:   15
54116540  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3652
Checksum:              272


Coasting Arc #8 (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    =       -4264774
10                 A    =         6777704
98  meter
 Y    =        -170280
47  meter          E    =           
0004625
 Z    =        5260946
97                 I    =           51
99024
 XDOT =       -958
970260                 Wp   =          102
66417
 YDOT =      -7543
293215  meter/sec      RA   =           76
72656  deg
 ZDOT =      -1021
773676                 TA   =          357
06564
                                          MA   =          357
06835
                                          Ha   =            221
929  n
mi
                                          Hp   =            214
078

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13992041
01                 X    =        -4288107
91
 Y    =        -558662
95  feet           Y    =         -218103
13  meter
 Z    =       17260324
70                 Z    =         5240173
48
 XDOT =      -3146
227888                 XDOT =        -869
584580
 YDOT =     -24748
337318  feet/sec       YDOT =       -7553
517187  meter/sec
 ZDOT =      -3352
275840                 ZDOT =       -1026
215710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12257427
34                 X    =        -3736063
85
 Y    =        7003229
85  feet           Y    =         2134584
46  meter
 Z    =       17167363
55                 Z    =         5232612
41
 XDOT =     -15254
604011                 XDOT =       -4649
603302
 YDOT =     -18437
715752  feet/sec       YDOT =       -5619
815761  meter/sec
 ZDOT =      -3371
040603                 ZDOT =       -1027
493176


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
43294997  
00016717  00000-0  10270-3 0  9072
2 25544  51
6389  77
3146 0003310 154
7313 205
4002 15
54124416 36682


Satellite: ISS
Catalog Number: 25544
Epoch time:      18156
43294997   =   yrday
fracday
Element set:     907
Inclination:       51
6389  deg
RA of node:        77
3146  deg
Eccentricity:     
0003310     
Arg of perigee:   154
7313  deg
Mean anomaly:     205
4002  deg
Mean motion:   15
54124416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3668
Checksum:              308


Coasting Arc #9 (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    =        4062321
62                 A    =         6783777
03  meter
 Y    =        4042335
44  meter          E    =           
0007970
 Z    =       -3639682
78                 I    =           52
00649
 XDOT =      -1949
014246                 Wp   =          121
30096
 YDOT =       5940
267840  meter/sec      RA   =           74
59964  deg
 ZDOT =       4425
206662                 TA   =          195
83341
                                          MA   =          195
85835
                                          Ha   =            221
836  n
mi
                                          Hp   =            214
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13327826
82                 X    =         4034496
86
 Y    =       13262255
37  feet           Y    =         4087607
90  meter
 Z    =      -11941216
48                 Z    =        -3620016
60
 XDOT =      -6394
403693                 XDOT =       -2036
790419
 YDOT =      19489
067717  feet/sec       YDOT =        5917
981393  meter/sec
 ZDOT =      14518
394561                 ZDOT =        4415
526420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14573649
01                 X    =        -4442048
22
 Y    =      -11966933
22  feet           Y    =        -3647521
25  meter
 Z    =      -11853788
43                 Z    =        -3613034
71
 XDOT =       3790
624222                 XDOT =        1155
382263
 YDOT =     -18943
472715  feet/sec       YDOT =       -5773
970483  meter/sec
 ZDOT =      14474
178560                 ZDOT =        4411
729625


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
81876085  
00016717  00000-0  10270-3 0  9089
2 25544  51
6381  75
3875 0003710 156
8007 203
3314 15
54136786 36741


Satellite: ISS
Catalog Number: 25544
Epoch time:      18156
81876085   =   yrday
fracday
Element set:     908
Inclination:       51
6381  deg
RA of node:        75
3875  deg
Eccentricity:     
0003710     
Arg of perigee:   156
8007  deg
Mean anomaly:     203
3314  deg
Mean motion:   15
54136786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3674
Checksum:              324


Coasting Arc #10 (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    =         -94903
61                 A    =         6786319
09  meter
 Y    =        6236262
32  meter          E    =           
0014468
 Z    =        2662422
07                 I    =           52
01047
 XDOT =      -5097
992518                 Wp   =           90
41781
 YDOT =      -2324
013423  meter/sec      RA   =           71
39739  deg
 ZDOT =       5237
287222                 TA   =          299
45973
                                          MA   =          299
60401
                                          Ha   =            221
702  n
mi
                                          Hp   =            214
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -311363
56                 X    =         -177564
81
 Y    =       20460178
21  feet           Y    =         6234738
61  meter
 Z    =        8734980
53                 Z    =         2661760
86
 XDOT =     -16725
697236                 XDOT =       -5097
065884
 YDOT =      -7624
715954  feet/sec       YDOT =       -2381
017989  meter/sec
 ZDOT =      17182
700859                 ZDOT =        5212
524940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17912403
61                 X    =         5459700
62
 Y    =        9895942
20  feet           Y    =         3016283
18  meter
 Z    =        8731085
23                 Z    =         2661234
78
 XDOT =     -13892
239560                 XDOT =       -4234
354618
 YDOT =      10012
162776  feet/sec       YDOT =        3051
707214  meter/sec
 ZDOT =      17072
207737                 ZDOT =        5203
608918


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
52608066  
00016717  00000-0  10270-3 0  9091
2 25544  51
6396  71
8659 0003250 158
2862 201
8429 15
54132273 36851


Satellite: ISS
Catalog Number: 25544
Epoch time:      18157
52608066   =   yrday
fracday
Element set:     909
Inclination:       51
6396  deg
RA of node:        71
8659  deg
Eccentricity:     
0003250     
Arg of perigee:   158
2862  deg
Mean anomaly:     201
8429  deg
Mean motion:   15
54132273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3685
Checksum:              326


Coasting Arc #11 (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    =        1084467
95                 A    =         6782448
49  meter
 Y    =       -5362752
58  meter          E    =           
0007664
 Z    =       -4014166
52                 I    =           51
98743
 XDOT =       5157
132815                 Wp   =           96
71630
 YDOT =       4024
021105  meter/sec      RA   =           66
43975  deg
 ZDOT =      -3990
053323                 TA   =          131
94413
                                          MA   =          131
87878
                                          Ha   =            221
602  n
mi
                                          Hp   =            214
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3557965
73                 X    =         1163853
90
 Y    =      -17594332
63  feet           Y    =        -5350181
10  meter
 Z    =      -13169837
67                 Z    =        -4008706
17
 XDOT =      16919
727084                 XDOT =        5131
133470
 YDOT =      13202
168981  feet/sec       YDOT =        4081
546686  meter/sec
 ZDOT =     -13090
726124                 ZDOT =       -3965
064465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14042418
03                 X    =        -4280129
01
 Y    =      -11211366
11  feet           Y    =        -3417224
39  meter
 Z    =      -13144582
56                 Z    =        -4006468
76
 XDOT =      18649
257299                 XDOT =        5684
293625
 YDOT =      -8169
387092  feet/sec       YDOT =       -2490
029186  meter/sec
 ZDOT =     -12979
481942                 ZDOT =       -3956
146096


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
49060486  
00016717  00000-0  10270-3 0  9108
2 25544  51
6407  67
0577 0003188 162
1449 197
9816 15
54155722 37002


Satellite: ISS
Catalog Number: 25544
Epoch time:      18158
49060486   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:        67
0577  deg
Eccentricity:     
0003188     
Arg of perigee:   162
1449  deg
Mean anomaly:     197
9816  deg
Mean motion:   15
54155722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3700
Checksum:              324


Coasting Arc #12 (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    =       -2119069
07                 A    =         6779016
23  meter
 Y    =        4155044
20  meter          E    =           
0009236
 Z    =        4916238
50                 I    =           51
96218
 XDOT =      -4989
131204                 Wp   =          135
84822
 YDOT =      -5332
635605  meter/sec      RA   =           61
47124  deg
 ZDOT =       2347
381536                 TA   =          291
23830
                                          MA   =          291
33693
                                          Ha   =            221
554  n
mi
                                          Hp   =            214
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6952326
34                 X    =        -2189255
08
 Y    =       13632034
77  feet           Y    =         4130954
46  meter
 Z    =       16129391
41                 Z    =         4905774
61
 XDOT =     -16368
540697                 XDOT =       -4940
531830
 YDOT =     -17495
523638  feet/sec       YDOT =       -5388
155972  meter/sec
 ZDOT =       7701
382993                 ZDOT =        2323
263482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9177566
93                 X    =         2797322
40
 Y    =       12307262
78  feet           Y    =         3751253
70  meter
 Z    =       16081916
21                 Z    =         4901768
06
 XDOT =     -22013
903749                 XDOT =       -6709
837863
 YDOT =       6453
302748  feet/sec       YDOT =        1966
966678  meter/sec
 ZDOT =       7594
247568                 ZDOT =        2314
726659


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
51942605  
00016717  00000-0  10270-3 0  9115
2 25544  51
6410  61
9290 0003236 167
8200 192
3031 15
54166857 37168


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
51942605   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:        61
9290  deg
Eccentricity:     
0003236     
Arg of perigee:   167
8200  deg
Mean anomaly:     192
3031  deg
Mean motion:   15
54166857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              297


Coasting Arc #13 (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    =       -4580307
43                 A    =         6786902
05  meter
 Y    =       -4372504
10  meter          E    =           
0015642
 Z    =        2418374
02                 I    =           51
98803
 XDOT =       1998
896607                 Wp   =          116
34435
 YDOT =      -5084
858874  meter/sec      RA   =           61
03848  deg
 ZDOT =      -5387
674039                 TA   =           36
73021
                                          MA   =           36
62311
                                          Ha   =            221
636  n
mi
                                          Hp   =            214
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15027255
36                 X    =        -4542819
75
 Y    =      -14345485
90  feet           Y    =        -4423514
86  meter
 Z    =        7934297
96                 Z    =         2396214
99
 XDOT =       6558
059735                 XDOT =        2081
778997
 YDOT =     -16682
607854  feet/sec       YDOT =       -5062
041951  meter/sec
 ZDOT =     -17676
095927                 ZDOT =       -5377
763146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13582561
30                 X    =        -4139964
68
 Y    =       15769557
98  feet           Y    =         4806561
27  meter
 Z    =        7835784
80                 Z    =         2388347
21
 XDOT =     -15843
406675                 XDOT =       -4829
070355
 YDOT =      -4852
300123  feet/sec       YDOT =       -1478
981078  meter/sec
 ZDOT =     -17630
952382                 ZDOT =       -5373
914286


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
58372832  
00016717  00000-0  10270-3 0  9122
2 25544  51
6422  61
6096 0003230 166
5407 193
5833 15
54132139 37171


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
58372832   =   yrday
fracday
Element set:     912
Inclination:       51
6422  deg
RA of node:        61
6096  deg
Eccentricity:     
0003230     
Arg of perigee:   166
5407  deg
Mean anomaly:     193
5833  deg
Mean motion:   15
54132139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3717
Checksum:              307


Coasting Arc #14 (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    =        4256872
88                 A    =         6788955
70  meter
 Y    =        5225962
60  meter          E    =           
0008599
 Z    =        -789290
70                 I    =           51
97836
 XDOT =      -3247
792691                 Wp   =           55
11202
 YDOT =       3540
003721  meter/sec      RA   =           56
08839  deg
 ZDOT =       5973
131120                 TA   =          296
39795
                                          MA   =          296
48618
                                          Ha   =            221
395  n
mi
                                          Hp   =            214
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13966118
38                 X    =         4201952
35
 Y    =       17145546
60  feet           Y    =         5273258
89  meter
 Z    =       -2589536
40                 Z    =         -768744
97
 XDOT =     -10655
487832                 XDOT =       -3316
151218
 YDOT =      11614
185435  feet/sec       YDOT =        3503
301885  meter/sec
 ZDOT =      19596
886875                 ZDOT =        5957
188606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16176559
16                 X    =         4930615
23
 Y    =      -15093207
59  feet           Y    =        -4600409
67  meter
 Z    =       -2498389
07                 Z    =         -761508
99
 XDOT =      11207
268988                 XDOT =        3415
975588
 YDOT =       8808
277283  feet/sec       YDOT =        2684
762916  meter/sec
 ZDOT =      19524
977726                 ZDOT =        5951
213211


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
54824451  
00016717  00000-0  10270-3 0  9130
2 25544  51
6421  56
8010 0003116 172
2192 187
9010 15
54170597 37321


Satellite: ISS
Catalog Number: 25544
Epoch time:      18160
54824451   =   yrday
fracday
Element set:     913
Inclination:       51
6421  deg
RA of node:        56
8010  deg
Eccentricity:     
0003116     
Arg of perigee:   172
2192  deg
Mean anomaly:     187
9010  deg
Mean motion:   15
54170597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3732
Checksum:              285


Coasting Arc #15 (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    =       -3602312
86                 A    =         6788956
49  meter
 Y    =       -5666270
56  meter          E    =           
0012572
 Z    =        -958393
12                 I    =           51
95856
 XDOT =       4480
726855                 Wp   =          149
82841
 YDOT =      -1850
845000  meter/sec      RA   =           51
14154  deg
 ZDOT =      -5943
314359                 TA   =           40
50754
                                          MA   =           40
41403
                                          Ha   =            221
401  n
mi
                                          Hp   =            214
554

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11818611
76                 X    =        -3534027
92
 Y    =      -18590126
51  feet           Y    =        -5706172
19  meter
 Z    =       -3144334
38                 Z    =         -975726
91
 XDOT =      14700
547423                 XDOT =        4529
960344
 YDOT =      -6072
326114  feet/sec       YDOT =       -1800
462481  meter/sec
 ZDOT =     -19499
062858                 ZDOT =       -5921
428887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17537466
82                 X    =        -5345419
89
 Y    =       13312456
63  feet           Y    =         4057636
78  meter
 Z    =       -3221021
92                 Z    =         -981767
48
 XDOT =      -6323
275404                 XDOT =       -1927
334343
 YDOT =     -12989
928681  feet/sec       YDOT =       -3959
330262  meter/sec
 ZDOT =     -19400
815286                 ZDOT =       -5913
368499


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
57706157  
00016717  00000-0  10270-3 0  9147
2 25544  51
6420  51
6729 0003263 177
7267 182
3901 15
54116005 37485


Satellite: ISS
Catalog Number: 25544
Epoch time:      18161
57706157   =   yrday
fracday
Element set:     914
Inclination:       51
6420  deg
RA of node:        51
6729  deg
Eccentricity:     
0003263     
Arg of perigee:   177
7267  deg
Mean anomaly:     182
3901  deg
Mean motion:   15
54116005  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3748
Checksum:              306


Coasting Arc #16 (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    =        2662652
99                 A    =         6786399
61  meter
 Y    =        5683287
64  meter          E    =           
0013139
 Z    =        2570080
44                 I    =           51
92917
 XDOT =      -5550
179890                 Wp   =           88
87602
 YDOT =        198
310859  meter/sec      RA   =           46
18808  deg
 ZDOT =       5288
528209                 TA   =          299
89898
                                          MA   =          300
02944
                                          Ha   =            221
187  n
mi
                                          Hp   =            214
579

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8735738
15                 X    =         2586418
75
 Y    =       18645956
81  feet           Y    =         5712636
66  meter
 Z    =        8432022
45                 Z    =         2582830
46
 XDOT =     -18209
251609                 XDOT =       -5577
674181
 YDOT =        650
626177  feet/sec       YDOT =         136
090486  meter/sec
 ZDOT =      17350
814335                 ZDOT =        5261
500237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17676267
68                 X    =         5387726
39
 Y    =      -10515904
20  feet           Y    =        -3205247
60  meter
 Z    =        8488177
01                 Z    =         2587196
35
 XDOT =       1729
731862                 XDOT =         527
222272
 YDOT =      16875
596725  feet/sec       YDOT =        5143
681882  meter/sec
 ZDOT =      17229
813238                 ZDOT =        5251
647075


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
60587331  
00016717  00000-0  10270-3 0  9154
2 25544  51
6422  46
5436 0002966 182
6375 177
4762 15
54161139 37645


Satellite: ISS
Catalog Number: 25544
Epoch time:      18162
60587331   =   yrday
fracday
Element set:     915
Inclination:       51
6422  deg
RA of node:        46
5436  deg
Eccentricity:     
0002966     
Arg of perigee:   182
6375  deg
Mean anomaly:     177
4762  deg
Mean motion:   15
54161139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3764
Checksum:              323


Coasting Arc #17 (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    =       -1399557
22                 A    =         6782614
37  meter
 Y    =       -5340150
30  meter          E    =           
0006153
 Z    =       -3945012
93                 I    =           51
89191
 XDOT =       6358
081357                 Wp   =           99
13109
 YDOT =       1331
931093  meter/sec      RA   =           41
22444  deg
 ZDOT =      -4064
943987                 TA   =          128
50796
                                          MA   =          128
45277
                                          Ha   =            221
121  n
mi
                                          Hp   =            214
662

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4591723
15                 X    =        -1320575
15
 Y    =      -17520178
14  feet           Y    =        -5355358
87  meter
 Z    =      -12942955
82                 Z    =        -3951620
59
 XDOT =      20859
846971                 XDOT =        6362
460382
 YDOT =       4369
852667  feet/sec       YDOT =        1403
056662  meter/sec
 ZDOT =     -13336
430405                 ZDOT =       -4034
047408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16867481
92                 X    =        -5141208
49
 Y    =        6541002
15  feet           Y    =         1993697
46  meter
 Z    =      -12971661
93                 Z    =        -3953762
56
 XDOT =       2344
602951                 XDOT =         714
634979
 YDOT =     -20086
766215  feet/sec       YDOT =       -6122
446342  meter/sec
 ZDOT =     -13198
364244                 ZDOT =       -4022
861422


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
57038161  
00016717  00000-0  10270-3 0  9164
2 25544  51
6411  41
7350 0002980 187
0008 173
1104 15
54159302 37791


Satellite: ISS
Catalog Number: 25544
Epoch time:      18163
57038161   =   yrday
fracday
Element set:     916
Inclination:       51
6411  deg
RA of node:        41
7350  deg
Eccentricity:     
0002980     
Arg of perigee:   187
0008  deg
Mean anomaly:     173
1104  deg
Mean motion:   15
54159302  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3779
Checksum:              289


Coasting Arc #18 (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    =         -77398
39                 A    =         6779333
56  meter
 Y    =       -4778277
09  meter          E    =           
0010546
 Z    =       -4817837
01                 I    =           51
85915
 XDOT =       6759
395241                 Wp   =           86
18932
 YDOT =       2502
172563  meter/sec      RA   =           36
73209  deg
 ZDOT =      -2594
422860                 TA   =          158
32606
                                          MA   =          158
28140
                                          Ha   =            221
070  n
mi
                                          Hp   =            214
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -253931
73                 X    =            -557
93
 Y    =      -15676762
11  feet           Y    =        -4778712
13  meter
 Z    =      -15806551
86                 Z    =        -4818027
19
 XDOT =      22176
493574                 XDOT =        6743
515333
 YDOT =       8209
227569  feet/sec       YDOT =        2577
672440  meter/sec
 ZDOT =      -8511
886023                 ZDOT =       -2561
625907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14015748
14                 X    =        -4272000
03
 Y    =       -7027235
94  feet           Y    =        -2141901
51  meter
 Z    =      -15806618
62                 Z    =        -4817857
36
 XDOT =      16943
421332                 XDOT =        5164
354822
 YDOT =     -15007
673531  feet/sec       YDOT =       -4574
338892  meter/sec
 ZDOT =      -8365
508839                 ZDOT =       -2549
807094


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
47058887  
00016717  00000-0  10270-3 0  9172
2 25544  51
6421  37
2484 0002970 187
9997 172
1109 15
54186638 37937


Satellite: ISS
Catalog Number: 25544
Epoch time:      18164
47058887   =   yrday
fracday
Element set:     917
Inclination:       51
6421  deg
RA of node:        37
2484  deg
Eccentricity:     
0002970     
Arg of perigee:   187
9997  deg
Mean anomaly:     172
1109  deg
Mean motion:   15
54186638  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3793
Checksum:              353


Coasting Arc #19 (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    =       -1496563
85                 A    =         6777321
00  meter
 Y    =        3963454
16  meter          E    =           
0004776
 Z    =        5288599
97                 I    =           51
82573
 XDOT =      -6773
877196                 Wp   =          154
36436
 YDOT =      -3525
233843  meter/sec      RA   =           31
74796  deg
 ZDOT =        720
617800                 TA   =          288
74595
                                          MA   =          288
79778
                                          Ha   =            221
029  n
mi
                                          Hp   =            214
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4909986
38                 X    =        -1566462
35
 Y    =       13003458
53  feet           Y    =         3946326
75  meter
 Z    =       17351049
76                 Z    =         5281161
12
 XDOT =     -22224
006548                 XDOT =       -6737
454008
 YDOT =     -11565
727830  feet/sec       YDOT =       -3600
780481  meter/sec
 ZDOT =       2364
231628                 ZDOT =         687
800367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9452364
65                 X    =         2881080
74
 Y    =       10248302
20  feet           Y    =         3123682
51  meter
 Z    =       17317099
42                 Z    =         5278251
90
 XDOT =     -19445
624820                 XDOT =       -5927
026445
 YDOT =      14162
926016  feet/sec       YDOT =        4316
859850  meter/sec
 ZDOT =       2217
934869                 ZDOT =         676
026548


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
49939316  
00016717  00000-0  10270-3 0  9181
2 25544  51
6425  32
1194 0003058 192
8388 167
2688 15
54189313 38098


Satellite: ISS
Catalog Number: 25544
Epoch time:      18165
49939316   =   yrday
fracday
Element set:     918
Inclination:       51
6425  deg
RA of node:        32
1194  deg
Eccentricity:     
0003058     
Arg of perigee:   192
8388  deg
Mean anomaly:     167
2688  deg
Mean motion:   15
54189313  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3809
Checksum:              343
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