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

 
Date: November 18th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


322/07:14:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 216 8

322/20:20:13 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 217 0

324/22:01:46 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 217 2

326/13:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 217 3

328/20:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 217 7

332/03:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 217 7

Coasting Arc #1 (Orbit 2866)
---------------------------------------

Vector Time (GMT): 2016/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5300072
58                 A    =         6784153
40  meter
 Y    =       -1558724
20  meter          E    =           
0007335
 Z    =       -3944950
35                 I    =           51
75861
 XDOT =       4418
816507                 Wp   =          162
60346
 YDOT =       4773
523295  meter/sec      RA   =           17
85860  deg
 ZDOT =       4045
721306                 TA   =          149
67341
                                          MA   =          149
63095
                                          Ha   =            221
679  n
mi
                                          Hp   =            216
737

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17388689
57                 X    =         5336271
98
 Y    =       -5113924
55  feet           Y    =        -1499252
62  meter
 Z    =      -12942750
50                 Z    =        -3919115
55
 XDOT =      14497
429485                 XDOT =        4345
456551
 YDOT =      15661
165665  feet/sec       YDOT =        4822
527070  meter/sec
 ZDOT =      13273
363866                 ZDOT =        4067
009329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5791239
06                 X    =        -1765169
67
 Y    =       17259896
93  feet           Y    =         5260816
58  meter
 Z    =      -12829304
26                 Z    =        -3910371
94
 XDOT =     -19830
470818                 XDOT =       -6044
327505
 YDOT =       3292
952732  feet/sec       YDOT =        1003
691993  meter/sec
 ZDOT =      13365
617806                 ZDOT =        4073
840307


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   16321
50846220  
00016717  00000-0  10270-3 0  9007
2 25544  51
6422  18
4205 0006655 218
3134 141
7547 15
53683217 28679


Satellite: ISS
Catalog Number: 25544
Epoch time:      16321
50846220   =   yrday
fracday
Element set:     900
Inclination:       51
6422  deg
RA of node:        18
4205  deg
Eccentricity:     
0006655     
Arg of perigee:   218
3134  deg
Mean anomaly:     141
7547  deg
Mean motion:   15
53683217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2867
Checksum:              290


Coasting Arc #2 (Orbit 2879)
---------------------------------------

Vector Time (GMT): 2016/322/07:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4112701
28                 A    =         6781753
01  meter
 Y    =        2750787
95  meter          E    =           
0003756
 Z    =        4634279
20                 I    =           51
72589
 XDOT =      -5923
617726                 Wp   =          116
14433
 YDOT =      -3868
686580  meter/sec      RA   =           13
87100  deg
 ZDOT =      -2960
332539                 TA   =            3
30770
                                          MA   =            3
30522
                                          Ha   =            221
799  n
mi
                                          Hp   =            216
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13493114
45                 X    =        -4165667
33
 Y    =        9024894
86  feet           Y    =         2704500
55  meter
 Z    =       15204328
08                 Z    =         4614171
90
 XDOT =     -19434
441358                 XDOT =       -5865
536568
 YDOT =     -12692
541272  feet/sec       YDOT =       -3934
603530  meter/sec
 ZDOT =      -9712
377095                 ZDOT =       -2988
967612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15504879
92                 X    =         4725887
40
 Y    =       -5079189
84  feet           Y    =        -1548137
06  meter
 Z    =       15115719
84                 Z    =         4607271
41
 XDOT =      14918
965472                 XDOT =        4547
300676
 YDOT =      16264
711753  feet/sec       YDOT =        4957
484142  meter/sec
 ZDOT =      -9836
983483                 ZDOT =       -2998
312565


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   16322
34464254  
00016717  00000-0  10270-3 0  9014
2 25544  51
6427  14
2518 0006734 219
9861 140
0796 15
53636502 28805


Satellite: ISS
Catalog Number: 25544
Epoch time:      16322
34464254   =   yrday
fracday
Element set:     901
Inclination:       51
6427  deg
RA of node:        14
2518  deg
Eccentricity:     
0006734     
Arg of perigee:   219
9861  deg
Mean anomaly:     140
0796  deg
Mean motion:   15
53636502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2880
Checksum:              303


Coasting Arc #3 (Orbit 2887)
---------------------------------------

Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3389340
35                 A    =         6780636
04  meter
 Y    =       -3266360
97  meter          E    =           
0010407
 Z    =       -4889439
39                 I    =           51
70502
 XDOT =       6535
283154                 Wp   =          138
96193
 YDOT =       3207
400119  meter/sec      RA   =           11
16321  deg
 ZDOT =       2382
764938                 TA   =          154
41405
                                          MA   =          154
36251
                                          Ha   =            221
339  n
mi
                                          Hp   =            217
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11119883
04                 X    =         3449364
85
 Y    =      -10716407
38  feet           Y    =        -3228123
21  meter
 Z    =      -16041467
83                 Z    =        -4872828
98
 XDOT =      21441
217698                 XDOT =        6487
356862
 YDOT =      10522
966271  feet/sec       YDOT =        3280
213941  meter/sec
 ZDOT =       7817
470269                 ZDOT =        2414
395913

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10936111
83                 X    =         3333326
88
 Y    =      -11011092
96  feet           Y    =        -3356181
13  meter
 Z    =      -15968067
07                 Z    =        -4867066
84
 XDOT =      20858
116429                 XDOT =        6357
553888
 YDOT =       9156
560197  feet/sec       YDOT =        2790
919548  meter/sec
 ZDOT =       7955
328328                 ZDOT =        2424
784074


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   16322
85921119  
00016717  00000-0  10270-3 0  9029
2 25544  51
6423  11
6924 0006272 225
8980 134
1657 15
53671837 28886


Satellite: ISS
Catalog Number: 25544
Epoch time:      16322
85921119   =   yrday
fracday
Element set:     902
Inclination:       51
6423  deg
RA of node:        11
6924  deg
Eccentricity:     
0006272     
Arg of perigee:   225
8980  deg
Mean anomaly:     134
1657  deg
Mean motion:   15
53671837  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2888
Checksum:              319


Coasting Arc #4 (Orbit 2903)
---------------------------------------

Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4701773
54                 A    =         6783785
95  meter
 Y    =        2717311
70  meter          E    =           
0006073
 Z    =        4059278
16                 I    =           51
68339
 XDOT =      -5488
950511                 Wp   =          107
57060
 YDOT =      -3684
836839  meter/sec      RA   =            6
18076  deg
 ZDOT =      -3888
074739                 TA   =           22
69237
                                          MA   =           22
66553
                                          Ha   =            221
274  n
mi
                                          Hp   =            217
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15425766
22                 X    =        -4751528
19
 Y    =        8915064
64  feet           Y    =         2664454
95  meter
 Z    =       13317841
74                 Z    =         4036317
16
 XDOT =     -18008
367818                 XDOT =       -5428
450990
 YDOT =     -12089
359708  feet/sec       YDOT =       -3745
879530  meter/sec
 ZDOT =     -12756
150719                 ZDOT =       -3914
592165

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15107786
05                 X    =        -4604853
19
 Y    =        9584884
01  feet           Y    =         2921472
65  meter
 Z    =       13216745
01                 Z    =         4028463
88
 XDOT =     -17737
035106                 XDOT =       -5406
248300
 YDOT =     -10194
877830  feet/sec       YDOT =       -3107
398763  meter/sec
 ZDOT =     -12871
516982                 ZDOT =       -3923
238376


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   16323
88834744  
00016717  00000-0  10270-3 0  9031
2 25544  51
6421   6
5669 0006279 229
7739 130
2865 15
53667259 29045


Satellite: ISS
Catalog Number: 25544
Epoch time:      16323
88834744   =   yrday
fracday
Element set:     903
Inclination:       51
6421  deg
RA of node:         6
5669  deg
Eccentricity:     
0006279     
Arg of perigee:   229
7739  deg
Mean anomaly:     130
2865  deg
Mean motion:   15
53667259  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2904
Checksum:              340


Coasting Arc #5 (Orbit 2918)
---------------------------------------

Vector Time (GMT): 2016/324/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5752158
36                 A    =         6787180
16  meter
 Y    =       -2160467
05  meter          E    =           
0001861
 Z    =       -2884123
77                 I    =           51
66335
 XDOT =       4067
317386                 Wp   =          211
99602
 YDOT =       4081
162947  meter/sec      RA   =            1
20284  deg
 ZDOT =       5051
751591                 TA   =          115
20413
                                          MA   =          115
18483
                                          Ha   =            220
975  n
mi
                                          Hp   =            217
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18871910
64                 X    =         5789899
68
 Y    =       -7088146
49  feet           Y    =        -2095931
45  meter
 Z    =       -9462348
34                 Z    =        -2856089
39
 XDOT =      13344
217146                 XDOT =        3996
839058
 YDOT =      13389
642216  feet/sec       YDOT =        4126
252217  meter/sec
 ZDOT =      16573
988161                 ZDOT =        5071
338684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18466576
75                 X    =         5628612
59
 Y    =       -8227552
73  feet           Y    =        -2507758
07  meter
 Z    =       -9339153
42                 Z    =        -2846573
96
 XDOT =      13426
592509                 XDOT =        4092
425397
 YDOT =      11214
594524  feet/sec       YDOT =        3418
208411  meter/sec
 ZDOT =      16658
924795                 ZDOT =        5077
640278


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   16324
85315836  
00016717  00000-0  10270-3 0  9046
2 25544  51
6427   1
7602 0006343 233
7619 126
2947 15
53686646 29192


Satellite: ISS
Catalog Number: 25544
Epoch time:      16324
85315836   =   yrday
fracday
Element set:     904
Inclination:       51
6427  deg
RA of node:         1
7602  deg
Eccentricity:     
0006343     
Arg of perigee:   233
7619  deg
Mean anomaly:     126
2947  deg
Mean motion:   15
53686646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2919
Checksum:              322


Coasting Arc #6 (Orbit 2920)
---------------------------------------

Vector Time (GMT): 2016/324/22:01:46
000
Vector Time (MET): N/A
Weight (LBS)     : 909067
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6780764
47                 A    =         6790590
26  meter
 Y    =         240799
25  meter          E    =           
0006210
 Z    =         173254
49                 I    =           51
67386
 XDOT =       -325
031657                 Wp   =           39
50837
 YDOT =       4746
536676  meter/sec      RA   =             
87724  deg
 ZDOT =       6010
114861                 TA   =          322
35630
                                          MA   =          322
39974
                                          Ha   =            220
935  n
mi
                                          Hp   =            217
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22246602
60                 X    =         6776726
23
 Y    =         790023
79  feet           Y    =          316603
73  meter
 Z    =         568420
24                 Z    =          206184
20
 XDOT =      -1066
376827                 XDOT =        -407
279265
 YDOT =      15572
626889  feet/sec       YDOT =        4742
441924  meter/sec
 ZDOT =      19718
224610                 ZDOT =        6008
336278

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19846505
01                 X    =         6049214
73
 Y    =      -10073085
97  feet           Y    =        -3070276
60  meter
 Z    =         712561
75                 Z    =          217188
82
 XDOT =       5757
858840                 XDOT =        1754
995375
 YDOT =      12759
731027  feet/sec       YDOT =        3889
166017  meter/sec
 ZDOT =      19709
471123                 ZDOT =        6007
446798


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   16324
98179855  
00016717  00000-0  10270-3 0  9050
2 25544  51
6439   1
1199 0006400 235
2005 124
8546 15
53687433 29217


Satellite: ISS
Catalog Number: 25544
Epoch time:      16324
98179855   =   yrday
fracday
Element set:     905
Inclination:       51
6439  deg
RA of node:         1
1199  deg
Eccentricity:     
0006400     
Arg of perigee:   235
2005  deg
Mean anomaly:     124
8546  deg
Mean motion:   15
53687433  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2921
Checksum:              311


Coasting Arc #7 (Orbit 2935)
---------------------------------------

Vector Time (GMT): 2016/325/22:01:46
000
Vector Time (MET): N/A
Weight (LBS)     : 909067
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6497559
98                 A    =         6789371
16  meter
 Y    =        -904355
43  meter          E    =           
0009314
 Z    =       -1725147
06                 I    =           51
63788
 XDOT =       2158
383956                 Wp   =          184
92841
 YDOT =      -4668
550794  meter/sec      RA   =          355
91001  deg
 ZDOT =      -5688
737859                 TA   =           13
99787
                                          MA   =           13
97207
                                          Ha   =            220
771  n
mi
                                          Hp   =            217
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21317454
00                 X    =        -6478584
25
 Y    =       -2967045
38  feet           Y    =         -976909
39  meter
 Z    =       -5659931
31                 Z    =        -1756664
75
 XDOT =       7081
312190                 XDOT =        2238
062119
 YDOT =     -15316
767698  feet/sec       YDOT =       -4643
968725  meter/sec
 ZDOT =     -18663
838119                 ZDOT =       -5678
059411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19922914
82                 X    =        -6072504
44
 Y    =        8045843
42  feet           Y    =         2452373
07  meter
 Z    =       -5797749
10                 Z    =        -1767153
93
 XDOT =       -814
670485                 XDOT =        -248
311564
 YDOT =     -15416
189600  feet/sec       YDOT =       -4698
854590  meter/sec
 ZDOT =     -18616
134431                 ZDOT =       -5674
197775


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   16325
94660461  
00016717  00000-0  10270-3 0  9066
2 25544  51
6445 356
3143 0006484 238
2276 121
8246 15
53658725 29365


Satellite: ISS
Catalog Number: 25544
Epoch time:      16325
94660461   =   yrday
fracday
Element set:     906
Inclination:       51
6445  deg
RA of node:       356
3143  deg
Eccentricity:     
0006484     
Arg of perigee:   238
2276  deg
Mean anomaly:     121
8246  deg
Mean motion:   15
53658725  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2936
Checksum:              325


Coasting Arc #8 (Orbit 2945)
---------------------------------------

Vector Time (GMT): 2016/326/13:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6466518
63                 A    =         6790104
31  meter
 Y    =        1716038
65  meter          E    =           
0012321
 Z    =        1112240
35                 I    =           51
61722
 XDOT =      -2186
059497                 Wp   =          149
57136
 YDOT =      -4415
236844  meter/sec      RA   =          352
70469  deg
 ZDOT =      -5879
411067                 TA   =           18
35263
                                          MA   =           18
30821
                                          Ha   =            220
749  n
mi
                                          Hp   =            217
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21215612
30                 X    =        -6490630
03
 Y    =        5630048
07  feet           Y    =         1643590
88  meter
 Z    =        3649082
52                 Z    =         1080768
81
 XDOT =      -7172
111211                 XDOT =       -2107
964832
 YDOT =     -14485
685184  feet/sec       YDOT =       -4439
246154  meter/sec
 ZDOT =     -19289
406388                 ZDOT =       -5889
840818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1901403
64                 X    =         -579547
83
 Y    =      -21890029
98  feet           Y    =        -6672081
14  meter
 Z    =        3510940
26                 Z    =         1070134
59
 XDOT =      13885
733780                 XDOT =        4232
371656
 YDOT =      -4317
057410  feet/sec       YDOT =       -1315
839098  meter/sec
 ZDOT =     -19334
176948                 ZDOT =       -5893
057134


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   16326
58980534  
00016717  00000-0  10270-3 0  9074
2 25544  51
6418 353
1088 0006111 238
6602 121
3953 15
53695993 29461


Satellite: ISS
Catalog Number: 25544
Epoch time:      16326
58980534   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:       353
1088  deg
Eccentricity:     
0006111     
Arg of perigee:   238
6602  deg
Mean anomaly:     121
3953  deg
Mean motion:   15
53695993  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2946
Checksum:              329


Coasting Arc #9 (Orbit 2961)
---------------------------------------

Vector Time (GMT): 2016/327/13:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6683707
35                 A    =         6790358
17  meter
 Y    =       -1086825
03  meter          E    =           
0006855
 Z    =         451277
22                 I    =           51
58591
 XDOT =        369
580320                 Wp   =           39
23508
 YDOT =       4776
361274  meter/sec      RA   =          347
73471  deg
 ZDOT =       5984
750996                 TA   =          325
63326
                                          MA   =          325
67758
                                          Ha   =            220
534  n
mi
                                          Hp   =            217
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21928173
72                 X    =         6693171
62
 Y    =       -3565698
92  feet           Y    =        -1012030
41  meter
 Z    =        1480568
32                 Z    =          483768
33
 XDOT =       1212
533859                 XDOT =         287
070715
 YDOT =      15670
476622  feet/sec       YDOT =        4780
032852  meter/sec
 ZDOT =      19635
009829                 ZDOT =        5986
345918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         132624
60                 X    =           40423
98
 Y    =       22205838
27  feet           Y    =         6768339
51  meter
 Z    =        1623037
73                 Z    =          494701
90
 XDOT =     -14032
250327                 XDOT =       -4277
029900
 YDOT =      -1361
519467  feet/sec       YDOT =        -414
991133  meter/sec
 ZDOT =      19641
026925                 ZDOT =        5986
585007


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   16327
61892302  
00016717  00000-0  10270-3 0  9085
2 25544  51
6410 347
9828 0006333 242
1014 117
9497 15
53738734 29622


Satellite: ISS
Catalog Number: 25544
Epoch time:      16327
61892302   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:       347
9828  deg
Eccentricity:     
0006333     
Arg of perigee:   242
1014  deg
Mean anomaly:     117
9497  deg
Mean motion:   15
53738734  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2962
Checksum:              321


Coasting Arc #10 (Orbit 2976)
---------------------------------------

Vector Time (GMT): 2016/328/13:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6475802
89                 A    =         6788823
24  meter
 Y    =         355637
83  meter          E    =           
0007573
 Z    =       -1989336
75                 I    =           51
54878
 XDOT =       1430
734458                 Wp   =          189
60213
 YDOT =      -5073
818133  meter/sec      RA   =          342
75981  deg
 ZDOT =      -5568
711046                 TA   =           12
38836
                                          MA   =           12
36976
                                          Ha   =            220
231  n
mi
                                          Hp   =            217
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21246072
47                 X    =        -6469634
96
 Y    =        1166790
77  feet           Y    =          283255
53  meter
 Z    =       -6526695
37                 Z    =        -2020780
01
 XDOT =       4694
010688                 XDOT =        1514
415608
 YDOT =     -16646
384951  feet/sec       YDOT =       -5057
350839  meter/sec
 ZDOT =     -18270
049364                 ZDOT =       -5561
557525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1763560
88                 X    =          537533
36
 Y    =      -21161996
75  feet           Y    =        -6450176
61  meter
 Z    =       -6664420
11                 Z    =        -2031315
25
 XDOT =      14283
995376                 XDOT =        4353
761791
 YDOT =       6929
570286  feet/sec       YDOT =        2112
133023  meter/sec
 ZDOT =     -18237
709121                 ZDOT =       -5558
853740


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   16328
58372049  
00016717  00000-0  10270-3 0  9094
2 25544  51
6406 343
1760 0006121 247
0099 113
0408 15
53700669 29773


Satellite: ISS
Catalog Number: 25544
Epoch time:      16328
58372049   =   yrday
fracday
Element set:     909
Inclination:       51
6406  deg
RA of node:       343
1760  deg
Eccentricity:     
0006121     
Arg of perigee:   247
0099  deg
Mean anomaly:     113
0408  deg
Mean motion:   15
53700669  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2977
Checksum:              311


Coasting Arc #11 (Orbit 2980)
---------------------------------------

Vector Time (GMT): 2016/328/20:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4607513
43                 A    =         6786915
48  meter
 Y    =       -4022654
68  meter          E    =           
0001787
 Z    =       -2940079
03                 I    =           51
53736
 XDOT =       5289
604943                 Wp   =          262
43037
 YDOT =       2403
368619  meter/sec      RA   =          341
32478  deg
 ZDOT =       4998
386170                 TA   =           63
97676
                                          MA   =           63
95836
                                          Ha   =            220
146  n
mi
                                          Hp   =            217
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15116513
88                 X    =         4666435
18
 Y    =      -13197685
95  feet           Y    =        -3970800
93  meter
 Z    =       -9645928
59                 Z    =        -2917553
44
 XDOT =      17354
346926                 XDOT =        5238
056380
 YDOT =       7885
067648  feet/sec       YDOT =        2462
232333  meter/sec
 ZDOT =      16398
904756                 ZDOT =        5023
956884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14469960
24                 X    =         4410443
88
 Y    =      -13971982
94  feet           Y    =        -4258660
40  meter
 Z    =       -9546506
58                 Z    =        -2909775
21
 XDOT =      16616
526455                 XDOT =        5064
717263
 YDOT =       5921
441562  feet/sec       YDOT =        1804
855388  meter/sec
 ZDOT =      16510
362183                 ZDOT =        5032
358393


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   16328
84099881  
00016717  00000-0  10270-3 0  9105
2 25544  51
6442 341
8953 0006315 250
0252 110
0220 15
53724425 29812


Satellite: ISS
Catalog Number: 25544
Epoch time:      16328
84099881   =   yrday
fracday
Element set:     910
Inclination:       51
6442  deg
RA of node:       341
8953  deg
Eccentricity:     
0006315     
Arg of perigee:   250
0252  deg
Mean anomaly:     110
0220  deg
Mean motion:   15
53724425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2981
Checksum:              291


Coasting Arc #12 (Orbit 2996)
---------------------------------------

Vector Time (GMT): 2016/329/20:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5477762
02                 A    =         6789698
96  meter
 Y    =        3706242
47  meter          E    =           
0010522
 Z    =        1505654
20                 I    =           51
51545
 XDOT =      -3830
808790                 Wp   =          143
13950
 YDOT =      -3318
159791  meter/sec      RA   =          336
34488  deg
 ZDOT =      -5756
503444                 TA   =           20
38689
                                          MA   =           20
34492
                                          Ha   =            220
087  n
mi
                                          Hp   =            217
685

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17971660
17                 X    =        -5526112
99
 Y    =       12159588
16  feet           Y    =         3644716
11  meter
 Z    =        4939810
37                 Z    =         1478926
72
 XDOT =     -12568
270307                 XDOT =       -3765
456485
 YDOT =     -10886
351021  feet/sec       YDOT =       -3360
633058  meter/sec
 ZDOT =     -18886
166154                 ZDOT =       -5774
954129

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17117241
45                 X    =        -5217335
19
 Y    =       13378550
04  feet           Y    =         4077782
05  meter
 Z    =        4822066
34                 Z    =         1469765
82
 XDOT =     -12194
666262                 XDOT =       -3716
934277
 YDOT =      -8751
127494  feet/sec       YDOT =       -2667
343660  meter/sec
 ZDOT =     -18966
265634                 ZDOT =       -5780
917765


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   16329
87010880  
00016717  00000-0  10270-3 0  9112
2 25544  51
6436 336
7694 0006206 252
9426 107
1047 15
53687038 29972


Satellite: ISS
Catalog Number: 25544
Epoch time:      16329
87010880   =   yrday
fracday
Element set:     911
Inclination:       51
6436  deg
RA of node:       336
7694  deg
Eccentricity:     
0006206     
Arg of perigee:   252
9426  deg
Mean anomaly:     107
1047  deg
Mean motion:   15
53687038  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2997
Checksum:              328


Coasting Arc #13 (Orbit 3012)
---------------------------------------

Vector Time (GMT): 2016/330/20:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5975786
85                 A    =         6790486
23  meter
 Y    =       -3214217
03  meter          E    =           
0007669
 Z    =          53431
26                 I    =           51
48896
 XDOT =       2218
195673                 Wp   =           20
11983
 YDOT =       4227
885403  meter/sec      RA   =          331
36635  deg
 ZDOT =       5999
114266                 TA   =          340
45675
                                          MA   =          340
48613
                                          Ha   =            219
711  n
mi
                                          Hp   =            217
653

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19605599
89                 X    =         6011025
36
 Y    =      -10545331
48  feet           Y    =        -3147194
74  meter
 Z    =         175299
41                 Z    =           82546
24
 XDOT =       7277
544858                 XDOT =        2141
611855
 YDOT =      13871
015103  feet/sec       YDOT =        4252
262486  meter/sec
 ZDOT =      19682
133417                 ZDOT =        6009
703937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18618929
63                 X    =         5675049
75
 Y    =      -12200725
75  feet           Y    =        -3718781
21  meter
 Z    =         303387
22                 Z    =           92472
42
 XDOT =       7432
710557                 XDOT =        2265
490178
 YDOT =      11845
015110  feet/sec       YDOT =        3610
360605  meter/sec
 ZDOT =      19727
637403                 ZDOT =        6012
983880


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   16330
89921300  
00016717  00000-0  10270-3 0  9125
2 25544  51
6432 331
6423 0006336 258
5290 101
5151 15
53729435 30139


Satellite: ISS
Catalog Number: 25544
Epoch time:      16330
89921300   =   yrday
fracday
Element set:     912
Inclination:       51
6432  deg
RA of node:       331
6423  deg
Eccentricity:     
0006336     
Arg of perigee:   258
5290  deg
Mean anomaly:     101
5151  deg
Mean motion:   15
53729435  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3013
Checksum:              278


Coasting Arc #14 (Orbit 3027)
---------------------------------------

Vector Time (GMT): 2016/331/20:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6094594
28                 A    =         6789427
77  meter
 Y    =        2503152
50  meter          E    =           
0007332
 Z    =       -1618400
81                 I    =           51
45765
 XDOT =       -571
832018                 Wp   =          192
19195
 YDOT =      -5083
691733  meter/sec      RA   =          326
38652  deg
 ZDOT =      -5711
729821                 TA   =            5
56542
                                          MA   =            5
55727
                                          Ha   =            219
505  n
mi
                                          Hp   =            217
737

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19995388
05                 X    =        -6114270
55
 Y    =        8212442
60  feet           Y    =         2434888
68  meter
 Z    =       -5309713
95                 Z    =        -1648055
15
 XDOT =      -1876
089299                 XDOT =        -487
196697
 YDOT =     -16678
778652  feet/sec       YDOT =       -5089
612975  meter/sec
 ZDOT =     -18739
271067                 ZDOT =       -5714
302248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19002567
45                 X    =        -5791982
56
 Y    =       10235306
98  feet           Y    =         3119721
57  meter
 Z    =       -5440012
90                 Z    =        -1658115
93
 XDOT =      -2726
515685                 XDOT =        -831
041981
 YDOT =     -15023
349220  feet/sec       YDOT =       -4579
116842  meter/sec
 ZDOT =     -18749
511257                 ZDOT =       -5714
851031


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   16331
86399701  
00016717  00000-0  10270-3 0  9138
2 25544  51
6435 326
8365 0006469 261
1653  98
8767 15
53693600 30284


Satellite: ISS
Catalog Number: 25544
Epoch time:      16331
86399701   =   yrday
fracday
Element set:     913
Inclination:       51
6435  deg
RA of node:       326
8365  deg
Eccentricity:     
0006469     
Arg of perigee:   261
1653  deg
Mean anomaly:      98
8767  deg
Mean motion:   15
53693600  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3028
Checksum:              336


Coasting Arc #15 (Orbit 3032)
---------------------------------------

Vector Time (GMT): 2016/332/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4920730
47                 A    =         6781482
65  meter
 Y    =         989147
46  meter          E    =           
0004993
 Z    =        4561458
89                 I    =           51
42238
 XDOT =      -3997
629769                 Wp   =          162
46968
 YDOT =       5784
962226  meter/sec      RA   =          324
90443  deg
 ZDOT =       3052
487177                 TA   =          256
88158
                                          MA   =          256
93731
                                          Ha   =            219
598  n
mi
                                          Hp   =            217
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16144128
83                 X    =         4887145
80
 Y    =        3245234
44  feet           Y    =         1043986
45  meter
 Z    =       14965416
31                 Z    =         4585281
51
 XDOT =     -13115
583230                 XDOT =       -4076
849551
 YDOT =      18979
534861  feet/sec       YDOT =        5739
815009  meter/sec
 ZDOT =      10014
721709                 ZDOT =        3032
875052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3313071
74                 X    =        -1009824
27
 Y    =      -16033159
31  feet           Y    =        -4886906
96  meter
 Z    =       15069488
57                 Z    =         4593180
12
 XDOT =      21461
629701                 XDOT =        6541
504733
 YDOT =       4913
186846  feet/sec       YDOT =        1497
539351  meter/sec
 ZDOT =       9927
721169                 ZDOT =        3025
969412


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   16332
18558964  
00016717  00000-0  10270-3 0  9143
2 25544  51
6422 325
2281 0006432 258
5489 101
4941 15
53752341 30336


Satellite: ISS
Catalog Number: 25544
Epoch time:      16332
18558964   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       325
2281  deg
Eccentricity:     
0006432     
Arg of perigee:   258
5489  deg
Mean anomaly:     101
4941  deg
Mean motion:   15
53752341  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3033
Checksum:              303


Coasting Arc #16 (Orbit 3047)
---------------------------------------

Vector Time (GMT): 2016/333/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3858093
79                 A    =         6779094
73  meter
 Y    =       -2134400
41  meter          E    =           
0007650
 Z    =       -5156152
99                 I    =           51
38836
 XDOT =       4984
788114                 Wp   =           76
65334
 YDOT =      -5650
292860  meter/sec      RA   =          319
89707  deg
 ZDOT =      -1390
931002                 TA   =          179
91309
                                          MA   =          179
91295
                                          Ha   =            219
444  n
mi
                                          Hp   =            217
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12657788
03                 X    =        -3808892
76
 Y    =       -7002626
01  feet           Y    =        -2177268
87  meter
 Z    =      -16916512
45                 Z    =        -5174775
62
 XDOT =      16354
291713                 XDOT =        5054
357333
 YDOT =     -18537
706235  feet/sec       YDOT =       -5594
160563  meter/sec
 ZDOT =      -4563
421921                 ZDOT =       -1366
546940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1270344
79                 X    =         -387201
09
 Y    =       14314076
86  feet           Y    =         4362930
63  meter
 Z    =      -16997593
65                 Z    =        -5180866
55
 XDOT =     -22568
150886                 XDOT =       -6878
772390
 YDOT =      -7293
701839  feet/sec       YDOT =       -2223
120321  meter/sec
 ZDOT =      -4455
567492                 ZDOT =       -1358
056971


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   16333
15036811  
00016717  00000-0  10270-3 0  9154
2 25544  51
6422 320
4225 0006285 262
9051  97
1387 15
53739682 30485


Satellite: ISS
Catalog Number: 25544
Epoch time:      16333
15036811   =   yrday
fracday
Element set:     915
Inclination:       51
6422  deg
RA of node:       320
4225  deg
Eccentricity:     
0006285     
Arg of perigee:   262
9051  deg
Mean anomaly:      97
1387  deg
Mean motion:   15
53739682  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3048
Checksum:              303


Coasting Arc #17 (Orbit 3063)
---------------------------------------

Vector Time (GMT): 2016/334/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2680979
10                 A    =         6778492
10  meter
 Y    =        3295356
56  meter          E    =           
0003801
 Z    =        5285433
94                 I    =           51
36227
 XDOT =      -5619
144008                 Wp   =          277
06838
 YDOT =       5199
170602  meter/sec      RA   =          314
88261  deg
 ZDOT =       -391
106572                 TA   =          176
67811
                                          MA   =          176
67558
                                          Ha   =            219
200  n
mi
                                          Hp   =            217
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8795863
17                 X    =         2618255
47
 Y    =       10811537
28  feet           Y    =         3324986
04  meter
 Z    =       17340662
53                 Z    =         5298305
56
 XDOT =     -18435
511836                 XDOT =       -5674
964973
 YDOT =      17057
646331  feet/sec       YDOT =        5136
021470  meter/sec
 ZDOT =      -1283
158045                 ZDOT =        -418
538751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6112046
18                 X    =         1862951
68
 Y    =      -12448506
47  feet           Y    =        -3794304
77  meter
 Z    =       17396341
64                 Z    =         5302404
93
 XDOT =      22353
036891                 XDOT =        6813
205644
 YDOT =       9011
643754  feet/sec       YDOT =        2746
749016  meter/sec
 ZDOT =      -1404
258421                 ZDOT =        -428
017967


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   16334
17946021  
00016717  00000-0  10270-3 0  9161
2 25544  51
6421 315
2951 0006308 266
8593  93
1837 15
53757019 30640


Satellite: ISS
Catalog Number: 25544
Epoch time:      16334
17946021   =   yrday
fracday
Element set:     916
Inclination:       51
6421  deg
RA of node:       315
2951  deg
Eccentricity:     
0006308     
Arg of perigee:   266
8593  deg
Mean anomaly:      93
1837  deg
Mean motion:   15
53757019  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3064
Checksum:              315


Coasting Arc #18 (Orbit 3078)
---------------------------------------

Vector Time (GMT): 2016/335/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1481123
79                 A    =         6779968
46  meter
 Y    =       -4399664
49  meter          E    =           
0006620
 Z    =       -4947444
30                 I    =           51
34605
 XDOT =       5900
904142                 Wp   =          120
67629
 YDOT =      -4394
617271  meter/sec      RA   =          309
86920  deg
 ZDOT =       2140
309595                 TA   =          170
28773
                                          MA   =          170
27492
                                          Ha   =            219
267  n
mi
                                          Hp   =            217
457

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4859330
02                 X    =        -1407782
58
 Y    =      -14434594
80  feet           Y    =        -4415816
97  meter
 Z    =      -16231772
62                 Z    =        -4954461
53
 XDOT =      19359
921727                 XDOT =        5939
210435
 YDOT =     -14418
035666  feet/sec       YDOT =       -4328
415374  meter/sec
 ZDOT =       7022
013107                 ZDOT =        2169
067906

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10878144
44                 X    =        -3315658
42
 Y    =       10614471
63  feet           Y    =         3235290
95  meter
 Z    =      -16261611
96                 Z    =        -4956539
32
 XDOT =     -20664
366039                 XDOT =       -6298
498769
 YDOT =     -10219
742730  feet/sec       YDOT =       -3114
977584  meter/sec
 ZDOT =       7148
753512                 ZDOT =        2178
940071


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   16335
14423051  
00016717  00000-0  10270-3 0  9173
2 25544  51
6430 310
4897 0006254 270
0872  89
9564 15
53769869 30795


Satellite: ISS
Catalog Number: 25544
Epoch time:      16335
14423051   =   yrday
fracday
Element set:     917
Inclination:       51
6430  deg
RA of node:       310
4897  deg
Eccentricity:     
0006254     
Arg of perigee:   270
0872  deg
Mean anomaly:      89
9564  deg
Mean motion:   15
53769869  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3079
Checksum:              332


Coasting Arc #19 (Orbit 3094)
---------------------------------------

Vector Time (GMT): 2016/336/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         330625
20                 A    =         6783132
40  meter
 Y    =        5347312
52  meter          E    =           
0004945
 Z    =        4158972
43                 I    =           51
33659
 XDOT =      -5874
203941                 Wp   =           51
91201
 YDOT =       3248
550885  meter/sec      RA   =          304
85907  deg
 ZDOT =      -3703
769366                 TA   =           76
33708
                                          MA   =           76
28202
                                          Ha   =            219
420  n
mi
                                          Hp   =            217
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1084728
36                 X    =          250602
84
 Y    =       17543676
26  feet           Y    =         5350562
02  meter
 Z    =       13644922
66                 Z    =         4160384
62
 XDOT =     -19272
322640                 XDOT =       -5892
101925
 YDOT =      10657
975345  feet/sec       YDOT =        3182
761824  meter/sec
 ZDOT =     -12151
474297                 ZDOT =       -3732
348374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15171806
83                 X    =         4624366
72
 Y    =       -8867558
58  feet           Y    =        -2702831
86  meter
 Z    =       13650047
96                 Z    =         4160534
62
 XDOT =      17574
034696                 XDOT =        5356
565775
 YDOT =      11139
095338  feet/sec       YDOT =        3395
196259  meter/sec
 ZDOT =     -12277
200234                 ZDOT =       -3742
090631


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   16336
17331427  
00016717  00000-0  10270-3 0  9183
2 25544  51
6433 305
3626 0006122 274
4462  85
5991 15
53736500 30958


Satellite: ISS
Catalog Number: 25544
Epoch time:      16336
17331427   =   yrday
fracday
Element set:     918
Inclination:       51
6433  deg
RA of node:       305
3626  deg
Eccentricity:     
0006122     
Arg of perigee:   274
4462  deg
Mean anomaly:      85
5991  deg
Mean motion:   15
53736500  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3095
Checksum:              305
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