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

 
Date: December 11th 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


344/13:26:46 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 216 7

345/20:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 216 4

348/10:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 216 0

349/01:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 215 9

352/04:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 215 3

Coasting Arc #1 (Orbit 3224)
---------------------------------------

Vector Time (GMT): 2016/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1679329
87                 A    =         6789657
34  meter
 Y    =        6484502
12  meter          E    =           
0007431
 Z    =        1090643
70                 I    =           51
29025
 XDOT =      -4461
744983                 Wp   =          114
87721
 YDOT =       2144
618366  meter/sec      RA   =          262
97865  deg
 ZDOT =      -5852
585652                 TA   =           53
23790
                                          MA   =           53
16971
                                          Ha   =            221
020  n
mi
                                          Hp   =            216
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5509612
44                 X    =         1601395
76
 Y    =       21274613
25  feet           Y    =         6502845
72  meter
 Z    =        3578227
35                 Z    =         1098612
46
 XDOT =     -14638
270941                 XDOT =       -4456
965416
 YDOT =       7036
149495  feet/sec       YDOT =        2094
751044  meter/sec
 ZDOT =     -19201
396497                 ZDOT =       -5874
248240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21953810
19                 X    =        -6691521
35
 Y    =         867656
16  feet           Y    =          264461
60  meter
 Z    =        3611938
51                 Z    =         1100918
86
 XDOT =      -3746
056701                 XDOT =       -1141
798082
 YDOT =     -14071
038694  feet/sec       YDOT =       -4288
852594  meter/sec
 ZDOT =     -19296
617776                 ZDOT =       -5881
609098


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   16344
53431104  
00016717  00000-0  10270-3 0  9006
2 25544  51
6418 263
7075 0006369 312
7073  47
3542 15
53838484 32250


Satellite: ISS
Catalog Number: 25544
Epoch time:      16344
53431104   =   yrday
fracday
Element set:     900
Inclination:       51
6418  deg
RA of node:       263
7075  deg
Eccentricity:     
0006369     
Arg of perigee:   312
7073  deg
Mean anomaly:      47
3542  deg
Mean motion:   15
53838484  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3225
Checksum:              300


Coasting Arc #2 (Orbit 3225)
---------------------------------------

Vector Time (GMT): 2016/344/13:26:46
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3102520
32                 A    =         6786319
21  meter
 Y    =        5232253
00  meter          E    =           
0008835
 Z    =        3004817
12                 I    =           51
27970
 XDOT =      -3356
794137                 Wp   =           71
85645
 YDOT =       4824
976100  meter/sec      RA   =          262
66432  deg
 ZDOT =      -4921
068984                 TA   =           73
55693
                                          MA   =           73
45985
                                          Ha   =            221
007  n
mi
                                          Hp   =            216
682

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10178872
46                 X    =         3029185
08
 Y    =       17166184
38  feet           Y    =         5266537
33  meter
 Z    =        9858323
88                 Z    =         3019710
59
 XDOT =     -11013
104123                 XDOT =       -3386
594090
 YDOT =      15829
974081  feet/sec       YDOT =        4787
271709  meter/sec
 ZDOT =     -16145
239450                 ZDOT =       -4937
447848

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15250134
18                 X    =        -4648240
90
 Y    =       12823796
43  feet           Y    =         3908693
15  meter
 Z    =        9922576
94                 Z    =         3024401
45
 XDOT =     -16484
330699                 XDOT =       -5024
423997
 YDOT =      -7017
537016  feet/sec       YDOT =       -2138
945283  meter/sec
 ZDOT =     -16217
814973                 ZDOT =       -4943
190004


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   16344
59862517  
00016717  00000-0  10270-3 0  9019
2 25544  51
6422 263
3881 0006288 312
7239  47
3383 15
53831250 32268


Satellite: ISS
Catalog Number: 25544
Epoch time:      16344
59862517   =   yrday
fracday
Element set:     901
Inclination:       51
6422  deg
RA of node:       263
3881  deg
Eccentricity:     
0006288     
Arg of perigee:   312
7239  deg
Mean anomaly:      47
3383  deg
Mean motion:   15
53831250  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3226
Checksum:              311


Coasting Arc #3 (Orbit 3240)
---------------------------------------

Vector Time (GMT): 2016/345/13:26:46
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2602295
75                 A    =         6789021
19  meter
 Y    =       -6066641
61  meter          E    =           
0011038
 Z    =       -1555256
93                 I    =           51
29560
 XDOT =       3998
263648                 Wp   =            2
36538
 YDOT =      -3178
867881  meter/sec      RA   =          257
66473  deg
 ZDOT =       5722
200203                 TA   =          340
54546
                                          MA   =          340
58755
                                          Ha   =            221
044  n
mi
                                          Hp   =            216
530

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8537715
71                 X    =        -2526708
73
 Y    =      -19903679
81  feet           Y    =        -6095319
52  meter
 Z    =       -5102548
99                 Z    =        -1567715
09
 XDOT =      13117
662886                 XDOT =        4005
717061
 YDOT =     -10429
356565  feet/sec       YDOT =       -3134
115202  meter/sec
 ZDOT =      18773
622712                 ZDOT =        5741
640975

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18012716
46                 X    =         5490275
98
 Y    =      -12001782
00  feet           Y    =        -3658143
15  meter
 Z    =       -5156000
43                 Z    =        -1571548
93
 XDOT =      11753
629336                 XDOT =        3582
506222
 YDOT =       9555
401388  feet/sec       YDOT =        2912
486343  meter/sec
 ZDOT =      18859
304217                 ZDOT =        5748
315925


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   16345
56332608  
00016717  00000-0  10270-3 0  9021
2 25544  51
6436 258
5804 0006469 315
9693  44
0943 15
53873998 32412


Satellite: ISS
Catalog Number: 25544
Epoch time:      16345
56332608   =   yrday
fracday
Element set:     902
Inclination:       51
6436  deg
RA of node:       258
5804  deg
Eccentricity:     
0006469     
Arg of perigee:   315
9693  deg
Mean anomaly:      44
0943  deg
Mean motion:   15
53873998  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3241
Checksum:              337


Coasting Arc #4 (Orbit 3245)
---------------------------------------

Vector Time (GMT): 2016/345/20:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4427812
23                 A    =         6779372
71  meter
 Y    =       -1202259
67  meter          E    =           
0008265
 Z    =       -4997718
16                 I    =           51
26324
 XDOT =       -206
468273                 Wp   =           83
10574
 YDOT =      -7402
394146  meter/sec      RA   =          256
09643  deg
 ZDOT =       1967
440545                 TA   =          206
09268
                                          MA   =          206
13436
                                          Ha   =            220
905  n
mi
                                          Hp   =            216
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14526943
01                 X    =        -4389762
08
 Y    =       -3944421
48  feet           Y    =        -1251561
42  meter
 Z    =      -16396713
12                 Z    =        -5019135
30
 XDOT =       -677
389348                 XDOT =        -133
234563
 YDOT =     -24286
070032  feet/sec       YDOT =       -7404
293642  meter/sec
 ZDOT =       6454
857432                 ZDOT =        1966
615048

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14230556
26                 X    =        -4337473
55
 Y    =        4583148
45  feet           Y    =         1396943
65  meter
 Z    =      -16490262
40                 Z    =        -5026231
98
 XDOT =     -13550
032944                 XDOT =       -4130
050041
 YDOT =     -18900
431178  feet/sec       YDOT =       -5760
851423  meter/sec
 ZDOT =       6452
570281                 ZDOT =        1966
743422


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   16345
88489186  
00016717  00000-0  10270-3 0  9031
2 25544  51
6413 256
9736 0006012 315
0477  45
0189 15
53873166 32463


Satellite: ISS
Catalog Number: 25544
Epoch time:      16345
88489186   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:       256
9736  deg
Eccentricity:     
0006012     
Arg of perigee:   315
0477  deg
Mean anomaly:      45
0189  deg
Mean motion:   15
53873166  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3246
Checksum:              328


Coasting Arc #5 (Orbit 3261)
---------------------------------------

Vector Time (GMT): 2016/346/20:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4528251
82                 A    =         6782480
05  meter
 Y    =        2764929
21  meter          E    =           
0009233
 Z    =        4224974
87                 I    =           51
28179
 XDOT =       -741
904295                 Wp   =           38
13310
 YDOT =       6729
128161  meter/sec      RA   =          251
07958  deg
 ZDOT =      -3597
189687                 TA   =           88
88937
                                          MA   =           88
78359
                                          Ha   =            221
116  n
mi
                                          Hp   =            216
355

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14856469
21                 X    =         4476473
74
 Y    =        9071290
06  feet           Y    =         2815277
34  meter
 Z    =       13861466
12                 Z    =         4246846
73
 XDOT =      -2434
069210                 XDOT =        -799
622162
 YDOT =      22077
192129  feet/sec       YDOT =        6720
509242  meter/sec
 ZDOT =     -11801
803435                 ZDOT =       -3600
933401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17313201
60                 X    =         5277063
85
 Y    =        -778326
62  feet           Y    =         -237233
95  meter
 Z    =       13956736
08                 Z    =         4254013
16
 XDOT =      10381
967177                 XDOT =        3164
423596
 YDOT =      18332
006916  feet/sec       YDOT =        5587
595708  meter/sec
 ZDOT =     -11819
393885                 ZDOT =       -3602
551256


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   16346
91389758  
00016717  00000-0  10270-3 0  9041
2 25544  51
6410 251
8458 0005922 318
9418  41
1288 15
53846779 32626


Satellite: ISS
Catalog Number: 25544
Epoch time:      16346
91389758   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       251
8458  deg
Eccentricity:     
0005922     
Arg of perigee:   318
9418  deg
Mean anomaly:      41
1288  deg
Mean motion:   15
53846779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3262
Checksum:              341


Coasting Arc #6 (Orbit 3276)
---------------------------------------

Vector Time (GMT): 2016/347/20:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4488017
64                 A    =         6786015
61  meter
 Y    =       -4056458
46  meter          E    =           
0006082
 Z    =       -3067701
37                 I    =           51
30567
 XDOT =       1771
056229                 Wp   =            5
93625
 YDOT =      -5643
883341  meter/sec      RA   =          246
07352  deg
 ZDOT =       4878
746098                 TA   =          318
65075
                                          MA   =          318
69678
                                          Ha   =            221
190  n
mi
                                          Hp   =            216
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14724467
31                 X    =        -4427421
99
 Y    =      -13308590
74  feet           Y    =        -4106307
37  meter
 Z    =      -10064637
02                 Z    =        -3089356
49
 XDOT =       5810
551931                 XDOT =        1810
336853
 YDOT =     -18516
677628  feet/sec       YDOT =       -5623
859053  meter/sec
 ZDOT =      16006
384836                 ZDOT =        4887
444388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19647331
88                 X    =        -5988506
76
 Y    =       -2451074
25  feet           Y    =         -747087
43  meter
 Z    =      -10158741
48                 Z    =        -3096384
40
 XDOT =      -6164
879280                 XDOT =       -1879
055204
 YDOT =     -16993
989300  feet/sec       YDOT =       -5179
767939  meter/sec
 ZDOT =      16045
472761                 ZDOT =        4890
660098


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   16347
87858286  
00016717  00000-0  10270-3 0  9055
2 25544  51
6415 247
0396 0006116 322
3078  37
7645 15
53868919 32770


Satellite: ISS
Catalog Number: 25544
Epoch time:      16347
87858286   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       247
0396  deg
Eccentricity:     
0006116     
Arg of perigee:   322
3078  deg
Mean anomaly:      37
7645  deg
Mean motion:   15
53868919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3277
Checksum:              349


Coasting Arc #7 (Orbit 3285)
---------------------------------------

Vector Time (GMT): 2016/348/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3881838
13                 A    =         6789320
05  meter
 Y    =       -5411974
51  meter          E    =           
0012656
 Z    =       -1276380
23                 I    =           51
32500
 XDOT =       3319
141128                 Wp   =            8
76328
 YDOT =      -3746
976859  meter/sec      RA   =          243
17322  deg
 ZDOT =       5812
975592                 TA   =          337
28597
                                          MA   =          337
34192
                                          Ha   =            221
462  n
mi
                                          Hp   =            216
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12735689
41                 X    =        -3814831
38
 Y    =      -17755821
87  feet           Y    =        -5455009
03  meter
 Z    =       -4187599
17                 Z    =        -1295075
22
 XDOT =      10889
570630                 XDOT =        3332
556945
 YDOT =     -12293
231164  feet/sec       YDOT =       -3709
785619  meter/sec
 ZDOT =      19071
442231                 ZDOT =        5829
131454

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21431072
07                 X    =         6532190
77
 Y    =       -4182337
47  feet           Y    =        -1274776
46  meter
 Z    =       -4268510
85                 Z    =        -1301042
11
 XDOT =       6402
639798                 XDOT =        1951
524611
 YDOT =      13336
390987  feet/sec       YDOT =        4064
931973  meter/sec
 ZDOT =      19142
851532                 ZDOT =        5834
741147


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   16348
45739194  
00016717  00000-0  10270-3 0  9067
2 25544  51
6419 244
1598 0006540 327
1130  32
9615 15
53884801 32861


Satellite: ISS
Catalog Number: 25544
Epoch time:      16348
45739194   =   yrday
fracday
Element set:     906
Inclination:       51
6419  deg
RA of node:       244
1598  deg
Eccentricity:     
0006540     
Arg of perigee:   327
1130  deg
Mean anomaly:      32
9615  deg
Mean motion:   15
53884801  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3286
Checksum:              322


Coasting Arc #8 (Orbit 3295)
---------------------------------------

Vector Time (GMT): 2016/349/01:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1438486
42                 A    =         6787705
51  meter
 Y    =        6218155
46  meter          E    =           
0001577
 Z    =       -2313551
99                 I    =           51
32905
 XDOT =      -5401
033118                 Wp   =           36
57465
 YDOT =       -752
813679  meter/sec      RA   =          240
11009  deg
 ZDOT =      -5382
177467                 TA   =          169
30576
                                          MA   =          169
30241
                                          Ha   =            221
533  n
mi
                                          Hp   =            215
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4719443
65                 X    =         1380084
79
 Y    =       20400772
51  feet           Y    =         6233915
31  meter
 Z    =       -7590393
68                 Z    =        -2306705
28
 XDOT =     -17719
924928                 XDOT =       -5366
069132
 YDOT =      -2469
861151  feet/sec       YDOT =        -813
015532  meter/sec
 ZDOT =     -17658
062557                 ZDOT =       -5408
329620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17821193
73                 X    =         5431899
85
 Y    =      -11013967
97  feet           Y    =        -3357057
44  meter
 Z    =       -7561501
64                 Z    =        -2304745
70
 XDOT =       2457
569779                 XDOT =         749
067269
 YDOT =      16176
453700  feet/sec       YDOT =        4930
583088  meter/sec
 ZDOT =     -17772
461866                 ZDOT =       -5417
046377


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   16349
10050785  
00016717  00000-0  10270-3 0  9073
2 25544  51
6419 240
9537 0006282 329
8676  30
2115 15
53911936 32962


Satellite: ISS
Catalog Number: 25544
Epoch time:      16349
10050785   =   yrday
fracday
Element set:     907
Inclination:       51
6419  deg
RA of node:       240
9537  deg
Eccentricity:     
0006282     
Arg of perigee:   329
8676  deg
Mean anomaly:      30
2115  deg
Mean motion:   15
53911936  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3296
Checksum:              319


Coasting Arc #9 (Orbit 3311)
---------------------------------------

Vector Time (GMT): 2016/350/01:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -406309
03                 A    =         6784296
85  meter
 Y    =       -5694098
32  meter          E    =           
0010238
 Z    =        3653728
54                 I    =           51
33344
 XDOT =       5874
622199                 Wp   =           62
60843
 YDOT =       2363
747908  meter/sec      RA   =          235
11087  deg
 ZDOT =       4332
302292                 TA   =          341
05516
                                          MA   =          341
09322
                                          Ha   =            221
646  n
mi
                                          Hp   =            215
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1333034
88                 X    =         -360354
17
 Y    =      -18681424
92  feet           Y    =        -5698385
42  meter
 Z    =       11987298
35                 Z    =         3651865
73
 XDOT =      19273
694879                 XDOT =        5826
709127
 YDOT =       7755
078438  feet/sec       YDOT =        2429
173466  meter/sec
 ZDOT =      14213
590198                 ZDOT =        4360
723601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17131835
33                 X    =        -5221783
41
 Y    =        7579222
82  feet           Y    =         2310147
11  meter
 Z    =       11980131
08                 Z    =         3651543
95
 XDOT =       1444
890180                 XDOT =         440
402527
 YDOT =     -19421
431798  feet/sec       YDOT =       -5919
652412  meter/sec
 ZDOT =      14337
664728                 ZDOT =        4370
120209


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   16350
12948715  
00016717  00000-0  10270-3 0  9087
2 25544  51
6407 235
8265 0006297 334
2337  25
8502 15
53912771 33127


Satellite: ISS
Catalog Number: 25544
Epoch time:      16350
12948715   =   yrday
fracday
Element set:     908
Inclination:       51
6407  deg
RA of node:       235
8265  deg
Eccentricity:     
0006297     
Arg of perigee:   334
2337  deg
Mean anomaly:      25
8502  deg
Mean motion:   15
53912771  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3312
Checksum:              308


Coasting Arc #10 (Orbit 3326)
---------------------------------------

Vector Time (GMT): 2016/351/01:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -781600
28                 A    =         6780737
69  meter
 Y    =        4875210
43  meter          E    =           
0011926
 Z    =       -4658450
54                 I    =           51
34107
 XDOT =      -6068
002558                 Wp   =           38
97332
 YDOT =      -3702
070695  meter/sec      RA   =          230
10309  deg
 ZDOT =      -2851
128438                 TA   =          202
52780
                                          MA   =          202
58020
                                          Ha   =            221
760  n
mi
                                          Hp   =            215
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2564305
38                 X    =         -813429
45
 Y    =       15994784
87  feet           Y    =         4866292
59  meter
 Z    =      -15283630
38                 Z    =        -4662324
11
 XDOT =     -19908
144874                 XDOT =       -6012
304607
 YDOT =     -12145
901231  feet/sec       YDOT =       -3769
615442  meter/sec
 ZDOT =      -9354
095926                 ZDOT =       -2880
470199

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15842004
12                 X    =         4828642
86
 Y    =       -3300760
27  feet           Y    =        -1006071
73  meter
 Z    =      -15301439
46                 Z    =        -4663878
75
 XDOT =      -4655
125474                 XDOT =       -1418
882244
 YDOT =      21691
245673  feet/sec       YDOT =        6611
491681  meter/sec
 ZDOT =      -9481
993479                 ZDOT =       -2890
111612


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   16351
09414837  
00016717  00000-0  10270-3 0  9098
2 25544  51
6409 231
0196 0006279 336
9421  23
1449 15
53919515 33273


Satellite: ISS
Catalog Number: 25544
Epoch time:      16351
09414837   =   yrday
fracday
Element set:     909
Inclination:       51
6409  deg
RA of node:       231
0196  deg
Eccentricity:     
0006279     
Arg of perigee:   336
9421  deg
Mean anomaly:      23
1449  deg
Mean motion:   15
53919515  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3327
Checksum:              315


Coasting Arc #11 (Orbit 3342)
---------------------------------------

Vector Time (GMT): 2016/352/01:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2074352
56                 A    =         6778296
98  meter
 Y    =       -3813267
39  meter          E    =           
0004110
 Z    =        5204165
73                 I    =           51
35395
 XDOT =       5943
855102                 Wp   =           17
97653
 YDOT =       4722
372818  meter/sec      RA   =          225
08797  deg
 ZDOT =       1094
660112                 TA   =           61
51501
                                          MA   =           61
47362
                                          Ha   =            221
810  n
mi
                                          Hp   =            215
305

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6805618
62                 X    =         2091559
98
 Y    =      -12510719
80  feet           Y    =        -3789974
84  meter
 Z    =       17074034
54                 Z    =         5214283
77
 XDOT =      19500
836949                 XDOT =        5885
289223
 YDOT =      15493
349141  feet/sec       YDOT =        4788
513441  meter/sec
 ZDOT =       3591
404568                 ZDOT =        1123
391764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14092799
71                 X    =        -4295485
35
 Y    =       -1639993
52  feet           Y    =         -499870
03  meter
 Z    =       17119013
64                 Z    =         5217875
36
 XDOT =       7150
526372                 XDOT =        2179
480438
 YDOT =     -22774
813167  feet/sec       YDOT =       -6941
763053  meter/sec
 ZDOT =       3716
479589                 ZDOT =        1132
782979


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   16352
12311047  
00016717  00000-0  10270-3 0  9104
2 25544  51
6402 225
8915 0006377 342
0370  18
0556 15
53946968 33438


Satellite: ISS
Catalog Number: 25544
Epoch time:      16352
12311047   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:       225
8915  deg
Eccentricity:     
0006377     
Arg of perigee:   342
0370  deg
Mean anomaly:      18
0556  deg
Mean motion:   15
53946968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3343
Checksum:              296


Coasting Arc #12 (Orbit 3344)
---------------------------------------

Vector Time (GMT): 2016/352/04:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2658483
38                 A    =         6777981
68  meter
 Y    =       -3309713
69  meter          E    =           
0005379
 Z    =        5283155
90                 I    =           51
35355
 XDOT =       5674
706105                 Wp   =            5
22757
 YDOT =       5145
509887  meter/sec      RA   =          224
43265  deg
 ZDOT =        373
201843                 TA   =           81
23070
                                          MA   =           81
16978
                                          Ha   =            221
853  n
mi
                                          Hp   =            215
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8722058
32                 X    =         2669632
83
 Y    =      -10858640
71  feet           Y    =        -3279922
86  meter
 Z    =       17333188
64                 Z    =         5296096
81
 XDOT =      18617
802183                 XDOT =        5614
933102
 YDOT =      16881
594117  feet/sec       YDOT =        5208
634021  meter/sec
 ZDOT =       1224
415495                 ZDOT =         400
623133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12002109
04                 X    =        -3658242
84
 Y    =        6924265
16  feet           Y    =         2110516
02  meter
 Z    =       17390449
63                 Z    =         5300609
05
 XDOT =     -10581
207451                 XDOT =       -3225
152031
 YDOT =     -21672
567268  feet/sec       YDOT =       -6605
798503  meter/sec
 ZDOT =       1343
680773                 ZDOT =         409
553900


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   16352
25173072  
00016717  00000-0  10270-3 0  9113
2 25544  51
6380 225
2508 0006508 341
7576  18
3342 15
53929318 33453


Satellite: ISS
Catalog Number: 25544
Epoch time:      16352
25173072   =   yrday
fracday
Element set:     911
Inclination:       51
6380  deg
RA of node:       225
2508  deg
Eccentricity:     
0006508     
Arg of perigee:   341
7576  deg
Mean anomaly:      18
3342  deg
Mean motion:   15
53929318  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3345
Checksum:              300


Coasting Arc #13 (Orbit 3359)
---------------------------------------

Vector Time (GMT): 2016/353/04:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3897676
95                 A    =         6778623
88  meter
 Y    =        2110046
20  meter          E    =           
0012479
 Z    =       -5138417
49                 I    =           51
37949
 XDOT =      -4984
932409                 Wp   =           72
73616
 YDOT =      -5625
298681  meter/sec      RA   =          219
41641  deg
 ZDOT =       1477
880589                 TA   =          211
52276
                                          MA   =          211
59759
                                          Ha   =            222
057  n
mi
                                          Hp   =            215
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12787654
03                 X    =        -3896022
40
 Y    =        6922723
74  feet           Y    =         2066469
34  meter
 Z    =      -16858325
10                 Z    =        -5157347
07
 XDOT =     -16354
765121                 XDOT =       -4928
837213
 YDOT =     -18455
704335  feet/sec       YDOT =       -5680
729995  meter/sec
 ZDOT =       4848
689596                 ZDOT =        1453
801176

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14303139
13                 X    =         4359596
81
 Y    =       -2013167
79  feet           Y    =         -613613
54  meter
 Z    =      -16941626
00                 Z    =        -5163807
61
 XDOT =       8690
281699                 XDOT =        2648
797862
 YDOT =      22000
444260  feet/sec       YDOT =        6705
735410  meter/sec
 ZDOT =       4744
123880                 ZDOT =        1446
008959


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   16353
21637487  
00016717  00000-0  10270-3 0  9126
2 25544  51
6380 220
4436 0006614 345
6330  14
4633 15
53929005 33609


Satellite: ISS
Catalog Number: 25544
Epoch time:      16353
21637487   =   yrday
fracday
Element set:     912
Inclination:       51
6380  deg
RA of node:       220
4436  deg
Eccentricity:     
0006614     
Arg of perigee:   345
6330  deg
Mean anomaly:      14
4633  deg
Mean motion:   15
53929005  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3360
Checksum:              289


Coasting Arc #14 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2016/354/04:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5017367
82                 A    =         6781208
69  meter
 Y    =        -890087
58  meter          E    =           
0012075
 Z    =        4473550
71                 I    =           51
41362
 XDOT =       3896
846737                 Wp   =           35
40969
 YDOT =       5771
450208  meter/sec      RA   =          214
40595  deg
 ZDOT =      -3208
218498                 TA   =           87
02371
                                          MA   =           86
88553
                                          Ha   =            222
081  n
mi
                                          Hp   =            214
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16461180
52                 X    =         5005217
74
 Y    =       -2920234
85  feet           Y    =         -834048
15  meter
 Z    =       14677003
63                 Z    =         4497894
03
 XDOT =      12784
930238                 XDOT =        3847
603266
 YDOT =      18935
204096  feet/sec       YDOT =        5814
752185  meter/sec
 ZDOT =     -10525
651241                 ZDOT =       -3189
408105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16394812
64                 X    =        -4997138
89
 Y    =       -2749746
51  feet           Y    =         -838122
74  meter
 Z    =       14783831
83                 Z    =         4506111
94
 XDOT =      -5944
231410                 XDOT =       -1811
801734
 YDOT =     -20956
549866  feet/sec       YDOT =       -6387
556399  meter/sec
 ZDOT =     -10444
178592                 ZDOT =       -3183
385635


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   16354
24532401  
00016717  00000-0  10270-3 0  9131
2 25544  51
6376 215
3156 0006674 348
5673  11
5327 15
53960996 33763


Satellite: ISS
Catalog Number: 25544
Epoch time:      16354
24532401   =   yrday
fracday
Element set:     913
Inclination:       51
6376  deg
RA of node:       215
3156  deg
Eccentricity:     
0006674     
Arg of perigee:   348
5673  deg
Mean anomaly:      11
5327  deg
Mean motion:   15
53960996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3376
Checksum:              318


Coasting Arc #15 (Orbit 3390)
---------------------------------------

Vector Time (GMT): 2016/355/04:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5868890
95                 A    =         6784863
96  meter
 Y    =        -202633
94  meter          E    =           
0007710
 Z    =       -3395149
03                 I    =           51
45373
 XDOT =      -2466
940192                 Wp   =           31
85605
 YDOT =      -5606
884237  meter/sec      RA   =          209
40637  deg
 ZDOT =       4610
223614                 TA   =          288
35452
                                          MA   =          288
43837
                                          Ha   =            222
218  n
mi
                                          Hp   =            214
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19254891
57                 X    =        -5849696
82
 Y    =        -664809
51  feet           Y    =         -268156
37  meter
 Z    =      -11138940
37                 Z    =        -3423611
80
 XDOT =      -8093
635801                 XDOT =       -2426
453531
 YDOT =     -18395
289493  feet/sec       YDOT =       -5634
245024  meter/sec
 ZDOT =      15125
405559                 ZDOT =        4598
338049

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17962205
05                 X    =         5474880
10
 Y    =        6764475
16  feet           Y    =         2061812
03  meter
 Z    =      -11263653
02                 Z    =        -3433161
44
 XDOT =       2373
349270                 XDOT =         723
396858
 YDOT =      18737
722659  feet/sec       YDOT =        5711
257866  meter/sec
 ZDOT =      15074
238609                 ZDOT =        4594
627928


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   16355
20995878  
00016717  00000-0  10270-3 0  9140
2 25544  51
6384 210
5083 0006720 352
3781   7
7269 15
53944063 33919


Satellite: ISS
Catalog Number: 25544
Epoch time:      16355
20995878   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:       210
5083  deg
Eccentricity:     
0006720     
Arg of perigee:   352
3781  deg
Mean anomaly:       7
7269  deg
Mean motion:   15
53944063  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3391
Checksum:              323


Coasting Arc #16 (Orbit 3406)
---------------------------------------

Vector Time (GMT): 2016/356/04:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6388787
04                 A    =         6788089
94  meter
 Y    =        1197747
68  meter          E    =           
0012566
 Z    =        1948757
45                 I    =           51
49423
 XDOT =        734
967048                 Wp   =           83
06446
 YDOT =       5206
862755  meter/sec      RA   =          204
41784  deg
 ZDOT =      -5577
307816                 TA   =           75
40624
                                          MA   =           75
26692
                                          Ha   =            222
386  n
mi
                                          Hp   =            214
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20960587
40                 X    =         6365452
51
 Y    =        3929618
36  feet           Y    =         1269060
85  meter
 Z    =        6393561
18                 Z    =         1979735
79
 XDOT =       2411
309214                 XDOT =         703
779965
 YDOT =      17082
883053  feet/sec       YDOT =        5214
907477  meter/sec
 ZDOT =     -18298
253991                 ZDOT =       -5573
813108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18740077
34                 X    =        -5711975
57
 Y    =      -10091850
45  feet           Y    =        -3075996
02  meter
 Z    =        6529150
40                 Z    =         1990085
04
 XDOT =       2035
882087                 XDOT =         620
536860
 YDOT =     -15677
091083  feet/sec       YDOT =       -4778
377362  meter/sec
 ZDOT =     -18283
789077                 ZDOT =       -5572
898911


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   16356
23889623  
00016717  00000-0  10270-3 0  9155
2 25544  51
6392 205
3797 0006816 356
1096   4
0002 15
53977942 34074


Satellite: ISS
Catalog Number: 25544
Epoch time:      16356
23889623   =   yrday
fracday
Element set:     915
Inclination:       51
6392  deg
RA of node:       205
3797  deg
Eccentricity:     
0006816     
Arg of perigee:   356
1096  deg
Mean anomaly:       4
0002  deg
Mean motion:   15
53977942  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3407
Checksum:              323


Coasting Arc #17 (Orbit 3421)
---------------------------------------

Vector Time (GMT): 2016/357/04:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6470644
20                 A    =         6789690
67  meter
 Y    =       -1994764
84  meter          E    =           
0016929
 Z    =        -342782
80                 I    =           51
52870
 XDOT =       1124
426993                 Wp   =           27
07377
 YDOT =      -4655
109896  meter/sec      RA   =          199
43889  deg
 ZDOT =       5995
287826                 TA   =          329
22361
                                          MA   =          329
32276
                                          Ha   =            222
436  n
mi
                                          Hp   =            214
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21229147
63                 X    =        -6446192
23
 Y    =       -6544504
08  feet           Y    =        -2066987
20  meter
 Z    =       -1124615
50                 Z    =         -374156
18
 XDOT =       3689
064939                 XDOT =        1147
275614
 YDOT =     -15272
670261  feet/sec       YDOT =       -4642
408288  meter/sec
 ZDOT =      19669
579483                 ZDOT =        6000
805303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18450662
94                 X    =         5623762
06
 Y    =       12359322
21  feet           Y    =         3767121
41  meter
 Z    =       -1261821
90                 Z    =         -384603
32
 XDOT =      -6892
559740                 XDOT =       -2100
852209
 YDOT =      12261
102418  feet/sec       YDOT =        3737
184017  meter/sec
 ZDOT =      19694
526041                 ZDOT =        6002
891537


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   16357
20352089  
00016717  00000-0  10270-3 0  9165
2 25544  51
6385 200
5729 0006785 359
7555    
3593 15
53983691 34221


Satellite: ISS
Catalog Number: 25544
Epoch time:      16357
20352089   =   yrday
fracday
Element set:     916
Inclination:       51
6385  deg
RA of node:       200
5729  deg
Eccentricity:     
0006785     
Arg of perigee:   359
7555  deg
Mean anomaly:        
3593  deg
Mean motion:   15
53983691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3422
Checksum:              330


Coasting Arc #18 (Orbit 3437)
---------------------------------------

Vector Time (GMT): 2016/358/04:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6099052
68                 A    =         6788999
26  meter
 Y    =        2668144
35  meter          E    =           
0005757
 Z    =       -1335794
01                 I    =           51
55833
 XDOT =      -3011
065906                 Wp   =           92
25271
 YDOT =       3985
520633  meter/sec      RA   =          194
46301  deg
 ZDOT =      -5809
257652                 TA   =          102
29464
                                          MA   =          102
23017
                                          Ha   =            222
573  n
mi
                                          Hp   =            214
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20010015
35                 X    =         6075252
21
 Y    =        8753754
43  feet           Y    =         2736215
05  meter
 Z    =       -4382526
29                 Z    =        -1306224
04
 XDOT =      -9878
825152                 XDOT =       -3027
190391
 YDOT =      13075
855094  feet/sec       YDOT =        3951
758999  meter/sec
 ZDOT =     -19059
244265                 ZDOT =       -5823
923611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16923918
91                 X    =        -5158410
48
 Y    =      -13846505
28  feet           Y    =        -4220414
81  meter
 Z    =       -4253319
63                 Z    =        -1296411
82
 XDOT =      11917
560100                 XDOT =        3632
472319
 YDOT =      -8714
512313  feet/sec       YDOT =       -2656
183353  meter/sec
 ZDOT =     -19124
191796                 ZDOT =       -5829
053659


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   16358
23244931  
00016717  00000-0  10270-3 0  9176
2 25544  51
6396 195
4448 0006862   2
6877 357
4311 15
53994696 34388


Satellite: ISS
Catalog Number: 25544
Epoch time:      16358
23244931   =   yrday
fracday
Element set:     917
Inclination:       51
6396  deg
RA of node:       195
4448  deg
Eccentricity:     
0006862     
Arg of perigee:     2
6877  deg
Mean anomaly:     357
4311  deg
Mean motion:   15
53994696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3438
Checksum:              348


Coasting Arc #19 (Orbit 3453)
---------------------------------------

Vector Time (GMT): 2016/359/04:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930289
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5262776
63                 A    =         6786312
76  meter
 Y    =       -3174014
04  meter          E    =           
0016634
 Z    =        2853765
20                 I    =           51
58093
 XDOT =       4736
389216                 Wp   =           57
44130
 YDOT =      -3284
574044  meter/sec      RA   =          189
48458  deg
 ZDOT =       5068
696564                 TA   =          335
07485
                                          MA   =          335
15509
                                          Ha   =            222
706  n
mi
                                          Hp   =            214
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17266327
54                 X    =        -5240755
21
 Y    =      -10413431
89  feet           Y    =        -3232742
99  meter
 Z    =        9362746
71                 Z    =         2828253
24
 XDOT =      15539
334698                 XDOT =        4748
144608
 YDOT =     -10776
161562  feet/sec       YDOT =       -3231
543135  meter/sec
 ZDOT =      16629
581904                 ZDOT =        5091
733110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14115919
12                 X    =         4302532
15
 Y    =       14469937
39  feet           Y    =         4410436
92  meter
 Z    =        9251399
66                 Z    =         2819826
62
 XDOT =     -16605
555245                 XDOT =       -5061
373239
 YDOT =       5475
109163  feet/sec       YDOT =        1668
813273  meter/sec
 ZDOT =      16731
125975                 ZDOT =        5099
647197


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   16359
26137131  
00016717  00000-0  10270-3 0  9184
2 25544  51
6397 190
3169 0006841   6
5962 353
5279 15
54006165 34542


Satellite: ISS
Catalog Number: 25544
Epoch time:      16359
26137131   =   yrday
fracday
Element set:     918
Inclination:       51
6397  deg
RA of node:       190
3169  deg
Eccentricity:     
0006841     
Arg of perigee:     6
5962  deg
Mean anomaly:     353
5279  deg
Mean motion:   15
54006165  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3454
Checksum:              320
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