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

 
Date: October 21st 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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


294/08:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 3

299/12:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 212 8

303/19:34:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 212 6

306/03:16:27 095 0 6 1 1 1 1
N/A 1 0 -0 1 222 6
000/00:02:54 191 -0 1 0 0 213 3

307/06:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 213 2

Coasting Arc #1 (Orbit 123)
---------------------------------------

Vector Time (GMT): 2017/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4463721
43                 A    =         6778643
28  meter
 Y    =        -944136
29  meter          E    =           
0008216
 Z    =        5006063
42                 I    =           51
89611
 XDOT =       3680
849818                 Wp   =           84
24406
 YDOT =      -6407
516202  meter/sec      RA   =          132
57517  deg
 ZDOT =       2071
521390                 TA   =          345
68281
                                          MA   =          345
70607
                                          Ha   =            222
566  n
mi
                                          Hp   =            213
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14644755
34                 X    =        -4477149
72
 Y    =       -3097560
00  feet           Y    =         -994127
30  meter
 Z    =       16424092
58                 Z    =         4984346
96
 XDOT =      12076
278929                 XDOT =        3742
164110
 YDOT =     -21022
034783  feet/sec       YDOT =       -6366
011411  meter/sec
 ZDOT =       6796
330021                 ZDOT =        2089
551776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14459036
25                 X    =         4407114
25
 Y    =       -4260395
42  feet           Y    =        -1298568
52  meter
 Z    =       16327885
83                 Z    =         4976739
60
 XDOT =       -950
284557                 XDOT =        -289
646733
 YDOT =      23158
188771  feet/sec       YDOT =        7058
615937  meter/sec
 ZDOT =       6877
170669                 ZDOT =        2096
161620


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   17293
55189421  
00016717  00000-0  10270-3 0  9004
2 25544  51
6380 133
3720 0005197  35
8378 324
3123 15
54181626  1244


Satellite: ISS
Catalog Number: 25544
Epoch time:      17293
55189421   =   yrday
fracday
Element set:     900
Inclination:       51
6380  deg
RA of node:       133
3720  deg
Eccentricity:     
0005197     
Arg of perigee:    35
8378  deg
Mean anomaly:     324
3123  deg
Mean motion:   15
54181626  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             124
Checksum:              292


Coasting Arc #2 (Orbit 136)
---------------------------------------

Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3330068
65                 A    =         6777048
83  meter
 Y    =        2540471
77  meter          E    =           
0018660
 Z    =       -5343459
76                 I    =           51
91221
 XDOT =      -4703
107471                 Wp   =           77
01735
 YDOT =       6039
867976  meter/sec      RA   =          128
23274  deg
 ZDOT =        -55
514602                 TA   =          192
43168
                                          MA   =          192
47777
                                          Ha   =            222
405  n
mi
                                          Hp   =            213
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10925422
09                 X    =         3327369
53
 Y    =        8334881
15  feet           Y    =         2577695
39  meter
 Z    =      -17531035
95                 Z    =        -5327289
63
 XDOT =     -15430
142623                 XDOT =       -4770
027670
 YDOT =      19815
839816  feet/sec       YDOT =        5986
900439  meter/sec
 ZDOT =       -182
134520                 ZDOT =         -78
524443

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8097902
32                 X    =        -2468240
63
 Y    =      -11214144
67  feet           Y    =        -3418071
30  meter
 Z    =      -17459646
34                 Z    =        -5321700
21
 XDOT =      19760
490240                 XDOT =        6022
997425
 YDOT =     -13805
492284  feet/sec       YDOT =       -4207
914048  meter/sec
 ZDOT =       -285
033701                 ZDOT =         -86
878272


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   17294
38777368  
00016717  00000-0  10270-3 0  9010
2 25544  51
6401 129
2064 0005264  38
7494 321
4036 15
54236441  1370


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
38777368   =   yrday
fracday
Element set:     901
Inclination:       51
6401  deg
RA of node:       129
2064  deg
Eccentricity:     
0005264     
Arg of perigee:    38
7494  deg
Mean anomaly:     321
4036  deg
Mean motion:   15
54236441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             137
Checksum:              304


Coasting Arc #3 (Orbit 152)
---------------------------------------

Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2137025
34                 A    =         6778117
83  meter
 Y    =       -3966187
93  meter          E    =           
0010680
 Z    =        5059182
42                 I    =           51
93530
 XDOT =       5241
079136                 Wp   =           49
06881
 YDOT =      -5269
126260  meter/sec      RA   =          123
25204  deg
 ZDOT =      -1907
477288                 TA   =           59
39065
                                          MA   =           59
28537
                                          Ha   =            222
424  n
mi
                                          Hp   =            213
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7011238
00                 X    =        -2117091
24
 Y    =      -13012427
58  feet           Y    =        -3989973
86  meter
 Z    =       16598367
52                 Z    =         5048849
78
 XDOT =      17195
141521                 XDOT =        5308
876222
 YDOT =     -17287
159646  feet/sec       YDOT =       -5210
137965  meter/sec
 ZDOT =      -6258
127585                 ZDOT =       -1881
852093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3223923
11                 X    =          982651
76
 Y    =       14477174
98  feet           Y    =         4412642
93  meter
 Z    =       16553073
99                 Z    =         5045376
95
 XDOT =     -20305
367163                 XDOT =       -6189
075911
 YDOT =      11581
968632  feet/sec       YDOT =        3530
184039  meter/sec
 ZDOT =      -6143
708568                 ZDOT =       -1872
602371


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   17295
41654521  
00016717  00000-0  10270-3 0  9021
2 25544  51
6398 124
0772 0005168  41
4959 318
6586 15
54263929  1531


Satellite: ISS
Catalog Number: 25544
Epoch time:      17295
41654521   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       124
0772  deg
Eccentricity:     
0005168     
Arg of perigee:    41
4959  deg
Mean anomaly:     318
6586  deg
Mean motion:   15
54263929  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             153
Checksum:              326


Coasting Arc #4 (Orbit 167)
---------------------------------------

Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         993643
09                 A    =         6781347
35  meter
 Y    =        5188781
40  meter          E    =           
0011340
 Z    =       -4260774
56                 I    =           51
96325
 XDOT =      -5403
665488                 Wp   =           85
82447
 YDOT =       4022
148608  meter/sec      RA   =          118
27854  deg
 ZDOT =       3647
153912                 TA   =          221
32566
                                          MA   =          221
41153
                                          Ha   =            222
453  n
mi
                                          Hp   =            213
087

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3259983
88                 X    =          956244
19
 Y    =       17023561
02  feet           Y    =         5199683
71  meter
 Z    =      -13978919
17                 Z    =        -4256038
68
 XDOT =     -17728
561311                 XDOT =       -5465
957160
 YDOT =      13196
025616  feet/sec       YDOT =        3961
372987  meter/sec
 ZDOT =      11965
728059                 ZDOT =        3620
752431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1213210
21                 X    =          369786
47
 Y    =      -17306758
79  feet           Y    =        -5275100
08  meter
 Z    =      -13958636
29                 Z    =        -4254592
34
 XDOT =      19374
636656                 XDOT =        5905
389253
 YDOT =      -8173
525718  feet/sec       YDOT =       -2491
290639  meter/sec
 ZDOT =      11848
017500                 ZDOT =        3611
275734


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   17296
38101740  
00016717  00000-0  10270-3 0  9039
2 25544  51
6401 119
2683 0005168  44
4352 315
7214 15
54237005  1681


Satellite: ISS
Catalog Number: 25544
Epoch time:      17296
38101740   =   yrday
fracday
Element set:     903
Inclination:       51
6401  deg
RA of node:       119
2683  deg
Eccentricity:     
0005168     
Arg of perigee:    44
4352  deg
Mean anomaly:     315
7214  deg
Mean motion:   15
54237005  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             168
Checksum:              284


Coasting Arc #5 (Orbit 183)
---------------------------------------

Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         107087
30                 A    =         6785210
42  meter
 Y    =       -6097529
94  meter          E    =           
0017101
 Z    =        2962256
09                 I    =           51
99147
 XDOT =       5293
415725                 Wp   =           83
77634
 YDOT =      -2360
878496  meter/sec      RA   =          113
31607  deg
 ZDOT =      -5024
389409                 TA   =           62
54565
                                          MA   =           62
37186
                                          Ha   =            222
493  n
mi
                                          Hp   =            212
920

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         351336
28                 X    =          160874
01
 Y    =      -20005019
50  feet           Y    =        -6096031
59  meter
 Z    =        9718687
96                 Z    =         2962907
13
 XDOT =      17366
849493                 XDOT =        5343
828892
 YDOT =      -7745
664356  feet/sec       YDOT =       -2301
402181  meter/sec
 ZDOT =     -16484
217222                 ZDOT =       -4998
552493

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5173511
76                 X    =        -1576886
38
 Y    =       19325783
04  feet           Y    =         5890498
67  meter
 Z    =        9722449
49                 Z    =         2963402
61
 XDOT =     -17429
805576                 XDOT =       -5312
604739
 YDOT =       3613
023812  feet/sec       YDOT =        1101
249658  meter/sec
 ZDOT =     -16369
229909                 ZDOT =       -4989
341276


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   17297
40978182  
00016717  00000-0  10270-3 0  9046
2 25544  51
6405 114
1384 0005339  47
2134 312
9467 15
54265249  1844


Satellite: ISS
Catalog Number: 25544
Epoch time:      17297
40978182   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       114
1384  deg
Eccentricity:     
0005339     
Arg of perigee:    47
2134  deg
Mean anomaly:     312
9467  deg
Mean motion:   15
54265249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             184
Checksum:              314


Coasting Arc #6 (Orbit 198)
---------------------------------------

Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1035042
65                 A    =         6788219
84  meter
 Y    =        6558511
84  meter          E    =           
0013790
 Z    =       -1388084
16                 I    =           52
01171
 XDOT =      -4951
899659                 Wp   =           42
78419
 YDOT =        444
926306  meter/sec      RA   =          108
36477  deg
 ZDOT =       5838
376283                 TA   =          302
16688
                                          MA   =          302
30058
                                          Ha   =            222
573  n
mi
                                          Hp   =            212
935

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3395809
22                 X    =        -1101561
97
 Y    =       21517427
29  feet           Y    =         6546565
32  meter
 Z    =       -4554081
88                 Z    =        -1393273
90
 XDOT =     -16246
389957                 XDOT =       -4984
867501
 YDOT =       1459
731975  feet/sec       YDOT =         389
366585  meter/sec
 ZDOT =      19154
777830                 ZDOT =        5814
240873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8182444
26                 X    =         2494009
01
 Y    =      -20183155
75  feet           Y    =        -6151825
87  meter
 Z    =       -4578066
10                 Z    =        -1395394
55
 XDOT =      14802
029058                 XDOT =        4511
658457
 YDOT =       1712
749613  feet/sec       YDOT =         522
046082  meter/sec
 ZDOT =      19047
605006                 ZDOT =        5805
710006


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   17298
37424668  
00016717  00000-0  10270-3 0  9059
2 25544  51
6391 109
3298 0005272  50
8004 309
3617 15
54224730  1993


Satellite: ISS
Catalog Number: 25544
Epoch time:      17298
37424668   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:       109
3298  deg
Eccentricity:     
0005272     
Arg of perigee:    50
8004  deg
Mean anomaly:     309
3617  deg
Mean motion:   15
54224730  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             199
Checksum:              316


Coasting Arc #7 (Orbit 214)
---------------------------------------

Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1866736
87                 A    =         6789002
58  meter
 Y    =       -6512390
56  meter          E    =           
0013037
 Z    =        -389824
81                 I    =           52
02431
 XDOT =       4448
978544                 Wp   =          114
90399
 YDOT =       1626
326633  meter/sec      RA   =          103
42020  deg
 ZDOT =      -6027
331196                 TA   =           69
27524
                                          MA   =           69
13556
                                          Ha   =            222
571  n
mi
                                          Hp   =            212
935

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6124464
79                 X    =         1941315
03
 Y    =      -21366110
76  feet           Y    =        -6491098
45  meter
 Z    =       -1278952
79                 Z    =         -380575
32
 XDOT =      14596
386298                 XDOT =        4459
740261
 YDOT =       5335
717301  feet/sec       YDOT =        1676
138194  meter/sec
 ZDOT =     -19774
708649                 ZDOT =       -6005
692908

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10506681
51                 X    =        -3202436
53
 Y    =       19589157
60  feet           Y    =         5970775
24  meter
 Z    =       -1236942
34                 Z    =         -377020
02
 XDOT =     -11838
789376                 XDOT =       -3608
463002
 YDOT =      -7557
528975  feet/sec       YDOT =       -2303
534832  meter/sec
 ZDOT =     -19678
914534                 ZDOT =       -5998
133150


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   17299
40300614  
00016717  00000-0  10270-3 0  9069
2 25544  51
6398 104
2007 0005095  55
5843 304
5791 15
54218921  2152


Satellite: ISS
Catalog Number: 25544
Epoch time:      17299
40300614   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       104
2007  deg
Eccentricity:     
0005095     
Arg of perigee:    55
5843  deg
Mean anomaly:     304
5791  deg
Mean motion:   15
54218921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             215
Checksum:              295


Coasting Arc #8 (Orbit 216)
---------------------------------------

Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2968209
52                 A    =         6787100
76  meter
 Y    =       -5738587
09  meter          E    =           
0009062
 Z    =       -2082127
82                 I    =           52
01722
 XDOT =       3579
987301                 Wp   =          104
47011
 YDOT =       3862
916565  meter/sec      RA   =          102
77565  deg
 ZDOT =      -5565
537017                 TA   =           98
43233
                                          MA   =           98
32960
                                          Ha   =            222
577  n
mi
                                          Hp   =            212
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9738220
20                 X    =         3042273
48
 Y    =      -18827385
45  feet           Y    =        -5704980
47  meter
 Z    =       -6831128
02                 Z    =        -2067528
89
 XDOT =      11745
365160                 XDOT =        3563
560235
 YDOT =      12673
610777  feet/sec       YDOT =        3902
858460  meter/sec
 ZDOT =     -18259
635884                 ZDOT =       -5548
186194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2946377
66                 X    =          898055
91
 Y    =       21012251
60  feet           Y    =         6404534
29  meter
 Z    =       -6765487
93                 Z    =        -2062120
72
 XDOT =     -15482
231607                 XDOT =       -4718
984194
 YDOT =      -3659
760675  feet/sec       YDOT =       -1115
495054  meter/sec
 ZDOT =     -18183
200119                 ZDOT =       -5542
239396


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   17299
53160086  
00016717  00000-0  10270-3 0  9071
2 25544  51
6375 103
5550 0005255  58
9769 301
1899 15
54273006  2173


Satellite: ISS
Catalog Number: 25544
Epoch time:      17299
53160086   =   yrday
fracday
Element set:     907
Inclination:       51
6375  deg
RA of node:       103
5550  deg
Eccentricity:     
0005255     
Arg of perigee:    58
9769  deg
Mean anomaly:     301
1899  deg
Mean motion:   15
54273006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             217
Checksum:              318


Coasting Arc #9 (Orbit 232)
---------------------------------------

Vector Time (GMT): 2017/300/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3434146
32                 A    =         6783649
09  meter
 Y    =        4639046
42  meter          E    =           
0016889
 Z    =        3548091
54                 I    =           52
01193
 XDOT =      -2799
026091                 Wp   =           84
04248
 YDOT =      -5538
730775  meter/sec      RA   =           97
82149  deg
 ZDOT =       4515
954051                 TA   =          317
59871
                                          MA   =          317
72909
                                          Ha   =            222
662  n
mi
                                          Hp   =            212
726

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11266884
26                 X    =        -3503001
33
 Y    =       15219968
58  feet           Y    =         4600258
55  meter
 Z    =       11640720
28                 Z    =         3531241
88
 XDOT =      -9183
156466                 XDOT =       -2758
819161
 YDOT =     -18171
688894  feet/sec       YDOT =       -5569
806471  meter/sec
 ZDOT =      14816
122215                 ZDOT =        4502
454815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          89709
66                 X    =           27343
51
 Y    =      -18982456
98  feet           Y    =        -5785852
89  meter
 Z    =       11565239
82                 Z    =         3525085
10
 XDOT =      16871
834407                 XDOT =        5142
535127
 YDOT =       9104
134918  feet/sec       YDOT =        2774
940323  meter/sec
 ZDOT =      14757
034601                 ZDOT =        4497
944146


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   17300
56035485  
00016717  00000-0  10270-3 0  9082
2 25544  51
6376  98
4251 0005143  64
6694 295
4991 15
54267769  2336


Satellite: ISS
Catalog Number: 25544
Epoch time:      17300
56035485   =   yrday
fracday
Element set:     908
Inclination:       51
6376  deg
RA of node:        98
4251  deg
Eccentricity:     
0005143     
Arg of perigee:    64
6694  deg
Mean anomaly:     295
4991  deg
Mean motion:   15
54267769  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             233
Checksum:              332


Coasting Arc #10 (Orbit 247)
---------------------------------------

Vector Time (GMT): 2017/301/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3809130
39                 A    =         6779812
78  meter
 Y    =       -3128668
15  meter          E    =           
0015692
 Z    =       -4670174
55                 I    =           52
00284
 XDOT =       1965
646695                 Wp   =           69
47761
 YDOT =       6787
171400  meter/sec      RA   =           92
85847  deg
 ZDOT =      -2946
304552                 TA   =          171
30301
                                          MA   =          171
27579
                                          Ha   =            222
656  n
mi
                                          Hp   =            212
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12497146
96                 X    =         3866518
67
 Y    =      -10264659
27  feet           Y    =        -3085751
14  meter
 Z    =      -15322094
98                 Z    =        -4651531
18
 XDOT =       6448
972097                 XDOT =        1903
916568
 YDOT =      22267
622703  feet/sec       YDOT =        6808
807345  meter/sec
 ZDOT =      -9666
353517                 ZDOT =       -2936
906075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3769758
33                 X    =        -1149022
34
 Y    =       15807412
36  feet           Y    =         4818099
29  meter
 Z    =      -15238869
49                 Z    =        -4644807
42
 XDOT =     -17547
329094                 XDOT =       -5348
425908
 YDOT =     -13455
740762  feet/sec       YDOT =       -4101
309784  meter/sec
 ZDOT =      -9625
663629                 ZDOT =       -2933
902274


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   17301
52480916  
00016717  00000-0  10270-3 0  9093
2 25544  51
6379  93
6175 0005288  68
0067 292
1648 15
54264810  2486


Satellite: ISS
Catalog Number: 25544
Epoch time:      17301
52480916   =   yrday
fracday
Element set:     909
Inclination:       51
6379  deg
RA of node:        93
6175  deg
Eccentricity:     
0005288     
Arg of perigee:    68
0067  deg
Mean anomaly:     292
1648  deg
Mean motion:   15
54264810  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             248
Checksum:              323


Coasting Arc #11 (Orbit 263)
---------------------------------------

Vector Time (GMT): 2017/302/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4055416
53                 A    =         6777328
05  meter
 Y    =        1358812
39  meter          E    =           
0008020
 Z    =        5250481
78                 I    =           51
99534
 XDOT =      -1120
500381                 Wp   =           92
43119
 YDOT =      -7515
887907  meter/sec      RA   =           87
88438  deg
 ZDOT =       1077
886503                 TA   =          347
29183
                                          MA   =          347
31204
                                          Ha   =            222
779  n
mi
                                          Hp   =            212
649

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13305172
35                 X    =        -4095814
39
 Y    =        4458045
90  feet           Y    =         1313236
33  meter
 Z    =       17225990
08                 Z    =         5230683
33
 XDOT =      -3676
182351                 XDOT =       -1041
608361
 YDOT =     -24658
424891  feet/sec       YDOT =       -7527
976942  meter/sec
 ZDOT =       3536
373041                 ZDOT =        1072
635368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7746631
38                 X    =         2361173
24
 Y    =      -11828719
22  feet           Y    =        -3605393
62  meter
 Z    =       17137900
18                 Z    =         5223631
97
 XDOT =      17351
409555                 XDOT =        5288
709632
 YDOT =      16463
308078  feet/sec       YDOT =        5018
016302  meter/sec
 ZDOT =       3514
214175                 ZDOT =        1071
132480


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   17302
55355632  
00016717  00000-0  10270-3 0  9105
2 25544  51
6380  88
4871 0005154  70
9138 289
2572 15
54263905  2641


Satellite: ISS
Catalog Number: 25544
Epoch time:      17302
55355632   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:        88
4871  deg
Eccentricity:     
0005154     
Arg of perigee:    70
9138  deg
Mean anomaly:     289
2572  deg
Mean motion:   15
54263905  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             264
Checksum:              310


Coasting Arc #12 (Orbit 278)
---------------------------------------

Vector Time (GMT): 2017/303/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4228236
48                 A    =         6777201
03  meter
 Y    =         512229
21  meter          E    =           
0019411
 Z    =       -5288382
37                 I    =           51
99389
 XDOT =        223
161967                 Wp   =           91
09713
 YDOT =       7595
980370  meter/sec      RA   =           82
90801  deg
 ZDOT =        916
705076                 TA   =          187
63055
                                          MA   =          187
66013
                                          Ha   =            222
660  n
mi
                                          Hp   =            212
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13872166
93                 X    =         4247883
14
 Y    =        1680542
04  feet           Y    =          559621
76  meter
 Z    =      -17350335
87                 Z    =        -5267794
88
 XDOT =        732
158684                 XDOT =         133
752121
 YDOT =      24921
195441  feet/sec       YDOT =        7597
976058  meter/sec
 ZDOT =       3007
562586                 ZDOT =         917
571494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11875630
36                 X    =        -3619692
13
 Y    =        7575664
98  feet           Y    =         2309062
69  meter
 Z    =      -17259029
39                 Z    =        -5260552
16
 XDOT =     -15810
086161                 XDOT =       -4818
914262
 YDOT =     -17945
026918  feet/sec       YDOT =       -5469
644205  meter/sec
 ZDOT =       3010
233247                 ZDOT =         917
519094


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   17303
51800243  
00016717  00000-0  10270-3 0  9116
2 25544  51
6391  83
6790 0005265  74
7725 285
4009 15
54279015  2795


Satellite: ISS
Catalog Number: 25544
Epoch time:      17303
51800243   =   yrday
fracday
Element set:     911
Inclination:       51
6391  deg
RA of node:        83
6790  deg
Eccentricity:     
0005265     
Arg of perigee:    74
7725  deg
Mean anomaly:     285
4009  deg
Mean motion:   15
54279015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             279
Checksum:              305


Coasting Arc #13 (Orbit 283)
---------------------------------------

Vector Time (GMT): 2017/303/19:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2304926
47                 A    =         6782532
77  meter
 Y    =       -5065951
07  meter          E    =           
0011794
 Z    =       -3888800
47                 I    =           52
01241
 XDOT =       4035
438348                 Wp   =           73
77898
 YDOT =       5015
054736  meter/sec      RA   =           81
39561  deg
 ZDOT =      -4148
493285                 TA   =          152
83254
                                          MA   =          152
77078
                                          Ha   =            222
716  n
mi
                                          Hp   =            212
565

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7562094
72                 X    =         2380294
20
 Y    =      -16620574
37  feet           Y    =        -5039754
66  meter
 Z    =      -12758531
73                 Z    =        -3877420
26
 XDOT =      13239
627125                 XDOT =        3999
210439
 YDOT =      16453
591655  feet/sec       YDOT =        5059
978921  meter/sec
 ZDOT =     -13610
542275                 ZDOT =       -4128
978371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14541888
31                 X    =         4432367
56
 Y    =      -11102643
99  feet           Y    =        -3384085
89  meter
 Z    =      -12707229
50                 Z    =        -3873163
55
 XDOT =       3257
886491                 XDOT =         993
003803
 YDOT =      19719
224764  feet/sec       YDOT =        6010
419708  meter/sec
 ZDOT =     -13524
696074                 ZDOT =       -4122
327363


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   17303
83948254  
00016717  00000-0  10270-3 0  9127
2 25544  51
6410  82
0792 0005444  72
8573 287
3175 15
54281985  2841


Satellite: ISS
Catalog Number: 25544
Epoch time:      17303
83948254   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:        82
0792  deg
Eccentricity:     
0005444     
Arg of perigee:    72
8573  deg
Mean anomaly:     287
3175  deg
Mean motion:   15
54281985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             284
Checksum:              322


Coasting Arc #14 (Orbit 299)
---------------------------------------

Vector Time (GMT): 2017/304/19:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3030929
45                 A    =         6778953
34  meter
 Y    =        3618406
30  meter          E    =           
0011773
 Z    =        4856593
50                 I    =           51
99257
 XDOT =      -3540
551089                 Wp   =          100
82187
 YDOT =      -6333
786020  meter/sec      RA   =           76
42825  deg
 ZDOT =       2502
107809                 TA   =          324
70008
                                          MA   =          324
77798
                                          Ha   =            222
893  n
mi
                                          Hp   =            212
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9943994
27                 X    =        -3094757
61
 Y    =       11871411
76  feet           Y    =         3584155
86  meter
 Z    =       15933705
72                 Z    =         4841714
59
 XDOT =     -11615
981262                 XDOT =       -3481
616120
 YDOT =     -20780
137861  feet/sec       YDOT =       -6373
049169  meter/sec
 ZDOT =       8209
015123                 ZDOT =        2485
052179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14338153
38                 X    =        -4370269
15
 Y    =        6029028
07  feet           Y    =         1837647
76  meter
 Z    =       15867091
59                 Z    =         4836289
52
 XDOT =       -544
682735                 XDOT =        -166
019297
 YDOT =     -22766
150479  feet/sec       YDOT =       -6939
122666  meter/sec
 ZDOT =       8134
302654                 ZDOT =        2479
335449


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   17304
86822042  
00016717  00000-0  10270-3 0  9138
2 25544  51
6391  76
9494 0005565  76
4648 283
7124 15
54275877  3003


Satellite: ISS
Catalog Number: 25544
Epoch time:      17304
86822042   =   yrday
fracday
Element set:     913
Inclination:       51
6391  deg
RA of node:        76
9494  deg
Eccentricity:     
0005565     
Arg of perigee:    76
4648  deg
Mean anomaly:     283
7124  deg
Mean motion:   15
54275877  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             300
Checksum:              325


Coasting Arc #15 (Orbit 314)
---------------------------------------

Vector Time (GMT): 2017/305/19:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3747125
45                 A    =         6777061
82  meter
 Y    =       -1924251
65  meter          E    =           
0020029
 Z    =       -5326258
03                 I    =           51
97827
 XDOT =       2840
128974                 Wp   =           83
94698
 YDOT =       7085
164188  meter/sec      RA   =           71
45287  deg
 ZDOT =       -561
374969                 TA   =          180
70936
                                          MA   =          180
71221
                                          Ha   =            222
719  n
mi
                                          Hp   =            212
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12293718
67                 X    =         3794237
44
 Y    =       -6313161
58  feet           Y    =        -1882085
70  meter
 Z    =      -17474599
84                 Z    =        -5307940
64
 XDOT =       9318
008444                 XDOT =        2763
416640
 YDOT =      23245
289331  feet/sec       YDOT =        7116
495485  meter/sec
 ZDOT =      -1841
781395                 ZDOT =        -547
765002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13920395
10                 X    =         4242936
43
 Y    =        -244510
77  feet           Y    =          -74526
88  meter
 Z    =      -17392986
58                 Z    =        -5301382
31
 XDOT =      -1807
153959                 XDOT =        -550
820527
 YDOT =      23968
542141  feet/sec       YDOT =        7305
611644  meter/sec
 ZDOT =      -1782
497984                 ZDOT =        -543
305385


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   17305
83265877  
00016717  00000-0  10270-3 0  9144
2 25544  51
6399  72
1412 0005332  79
4922 280
6832 15
54265195  3159


Satellite: ISS
Catalog Number: 25544
Epoch time:      17305
83265877   =   yrday
fracday
Element set:     914
Inclination:       51
6399  deg
RA of node:        72
1412  deg
Eccentricity:     
0005332     
Arg of perigee:    79
4922  deg
Mean anomaly:     280
6832  deg
Mean motion:   15
54265195  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             315
Checksum:              317


Coasting Arc #16 (Orbit 319)
---------------------------------------

Vector Time (GMT): 2017/306/03:17:54
191
Vector Time (MET): N/A
Weight (LBS)     : 919921
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3775641
88                 A    =         6777518
37  meter
 Y    =       -1829997
13  meter          E    =           
0019115
 Z    =       -5339109
85                 I    =           51
97643
 XDOT =       2903
160742                 Wp   =           84
77158
 YDOT =       7072
636352  meter/sec      RA   =           69
85519  deg
 ZDOT =       -370
596111                 TA   =          181
70145
                                          MA   =          181
70796
                                          Ha   =            222
634  n
mi
                                          Hp   =            213
289

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12387276
53                 X    =         3821760
24
 Y    =       -6003927
60  feet           Y    =        -1787517
83  meter
 Z    =      -17516764
61                 Z    =        -5320656
34
 XDOT =       9524
805584                 XDOT =        2825
657082
 YDOT =      23204
187505  feet/sec       YDOT =        7104
668103  meter/sec
 ZDOT =      -1215
866507                 ZDOT =        -356
681827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6049506
44                 X    =        -1843889
56
 Y    =      -12480719
07  feet           Y    =        -3804123
17  meter
 Z    =      -17434561
43                 Z    =        -5314054
32
 XDOT =      22260
161833                 XDOT =        6784
897327
 YDOT =      -9173
361318  feet/sec       YDOT =       -2796
040530  meter/sec
 ZDOT =      -1155
235999                 ZDOT =        -352
115933


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   17306
15413878  
00016717  00000-0  10270-3 0  9157
2 25544  51
6416  70
5389 0004359  77
0557 283
1082 15
54088470  3200


Satellite: ISS
Catalog Number: 25544
Epoch time:      17306
15413878   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:        70
5389  deg
Eccentricity:     
0004359     
Arg of perigee:    77
0557  deg
Mean anomaly:     283
1082  deg
Mean motion:   15
54088470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             320
Checksum:              311


Coasting Arc #17 (Orbit 335)
---------------------------------------

Vector Time (GMT): 2017/307/03:17:54
191
Vector Time (MET): N/A
Weight (LBS)     : 919921
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4389970
48                 A    =         6778167
96  meter
 Y    =         138121
38  meter          E    =           
0008933
 Z    =        5156412
50                 I    =           51
96736
 XDOT =      -2052
663695                 Wp   =           66
15950
 YDOT =      -7230
359058  meter/sec      RA   =           64
87864  deg
 ZDOT =      -1548
255898                 TA   =           38
71402
                                          MA   =           38
65003
                                          Ha   =            222
721  n
mi
                                          Hp   =            213
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14402790
30                 X    =        -4416236
79
 Y    =         453154
14  feet           Y    =           88883
14  meter
 Z    =       16917363
83                 Z    =         5135022
94
 XDOT =      -6734
460943                 XDOT =       -1964
138435
 YDOT =     -23721
650453  feet/sec       YDOT =       -7252
818452  meter/sec
 ZDOT =      -5079
579718                 ZDOT =       -1558
011999

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         755373
99                 X    =          230237
99
 Y    =       14501005
06  feet           Y    =         4419906
34  meter
 Z    =       16822401
10                 Z    =         5127467
86
 XDOT =     -22520
613462                 XDOT =       -6864
282983
 YDOT =       7136
284255  feet/sec       YDOT =        2175
139441  meter/sec
 ZDOT =      -5121
708933                 ZDOT =       -1561
096883


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   17307
18300613  
00016717  00000-0  10270-3 0  9164
2 25544  51
6422  65
4103 0004296  79
4988 280
6649 15
54122929  3364


Satellite: ISS
Catalog Number: 25544
Epoch time:      17307
18300613   =   yrday
fracday
Element set:     916
Inclination:       51
6422  deg
RA of node:        65
4103  deg
Eccentricity:     
0004296     
Arg of perigee:    79
4988  deg
Mean anomaly:     280
6649  deg
Mean motion:   15
54122929  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             336
Checksum:              312


Coasting Arc #18 (Orbit 337)
---------------------------------------

Vector Time (GMT): 2017/307/06:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919921
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         624694
61                 A    =         6786320
29  meter
 Y    =        6183435
43  meter          E    =           
0017714
 Z    =        2705579
45                 I    =           51
99062
 XDOT =      -5356
198224                 Wp   =           78
62790
 YDOT =      -1748
920162  meter/sec      RA   =           64
33982  deg
 ZDOT =       5208
398100                 TA   =          311
80957
                                          MA   =          311
96073
                                          Ha   =            222
591  n
mi
                                          Hp   =            213
201

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2049522
99                 X    =          542360
57
 Y    =       20286861
65  feet           Y    =         6189960
97  meter
 Z    =        8876573
01                 Z    =         2708413
83
 XDOT =     -17572
828819                 XDOT =       -5361
543854
 YDOT =      -5737
927041  feet/sec       YDOT =       -1808
846458  meter/sec
 ZDOT =      17087
920274                 ZDOT =        5182
365666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13525818
93                 X    =         4122669
61
 Y    =      -15251357
50  feet           Y    =        -4648613
77  meter
 Z    =        8888147
46                 Z    =         2709107
35
 XDOT =       6702
108423                 XDOT =        2042
802647
 YDOT =      15883
521054  feet/sec       YDOT =        4841
297217  meter/sec
 ZDOT =      16972
656788                 ZDOT =        5173
265789


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   17307
31161393  
00016717  00000-0  10270-3 0  9170
2 25544  51
6401  64
7677 0004205  80
0445 280
1182 15
54094067  3385


Satellite: ISS
Catalog Number: 25544
Epoch time:      17307
31161393   =   yrday
fracday
Element set:     917
Inclination:       51
6401  deg
RA of node:        64
7677  deg
Eccentricity:     
0004205     
Arg of perigee:    80
0445  deg
Mean anomaly:     280
1182  deg
Mean motion:   15
54094067  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             338
Checksum:              289


Coasting Arc #19 (Orbit 352)
---------------------------------------

Vector Time (GMT): 2017/308/06:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919921
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         449844
71                 A    =         6782584
99  meter
 Y    =       -5440507
20  meter          E    =           
0011303
 Z    =       -4036645
22                 I    =           51
96171
 XDOT =       5608
215121                 Wp   =           76
20810
 YDOT =       3395
640919  meter/sec      RA   =           59
38101  deg
 ZDOT =      -3958
254018                 TA   =          152
80768
                                          MA   =          152
74844
                                          Ha   =            222
642  n
mi
                                          Hp   =            213
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1475868
46                 X    =          530257
16
 Y    =      -17849433
08  feet           Y    =        -5435027
22  meter
 Z    =      -13243586
69                 Z    =        -4034264
49
 XDOT =      18399
655909                 XDOT =        5589
055220
 YDOT =      11140
554195  feet/sec       YDOT =        3458
248577  meter/sec
 ZDOT =     -12986
397697                 ZDOT =       -3931
056791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13963223
29                 X    =        -4255990
46
 Y    =       11229979
35  feet           Y    =         3422897
71  meter
 Z    =      -13232119
87                 Z    =        -4033150
14
 XDOT =      -3939
235673                 XDOT =       -1200
679033
 YDOT =     -20032
336716  feet/sec       YDOT =       -6105
856231  meter/sec
 ZDOT =     -12866
243728                 ZDOT =       -3921
631088


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   17308
27617560  
00016717  00000-0  10270-3 0  9189
2 25544  51
6388  59
9599 0004292  83
9224 276
2418 15
54080325  3538


Satellite: ISS
Catalog Number: 25544
Epoch time:      17308
27617560   =   yrday
fracday
Element set:     918
Inclination:       51
6388  deg
RA of node:        59
9599  deg
Eccentricity:     
0004292     
Arg of perigee:    83
9224  deg
Mean anomaly:     276
2418  deg
Mean motion:   15
54080325  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             353
Checksum:              331
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