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

 
Date: October 14th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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


286/19:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 214 0

287/08:46:53 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 9

289/11:09:57 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 7

290/03:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 213 7

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 5
000/00:00:00 000 0 0 0 0 212 8

Coasting Arc #1 (Orbit 14)
---------------------------------------

Vector Time (GMT): 2017/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2359486
05                 A    =         6779774
99  meter
 Y    =       -4308312
00  meter          E    =           
0011717
 Z    =        4669865
29                 I    =           51
70738
 XDOT =       7071
400624                 Wp   =           44
15826
 YDOT =        740
852767  meter/sec      RA   =          167
35078  deg
 ZDOT =      -2876
824957                 TA   =           74
45387
                                          MA   =           74
32455
                                          Ha   =            221
808  n
mi
                                          Hp   =            213
981

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7741095
96                 X    =         2384803
27
 Y    =      -14134881
87  feet           Y    =        -4281784
77  meter
 Z    =       15321080
34                 Z    =         4681388
79
 XDOT =      23200
133280                 XDOT =        7076
564976
 YDOT =       2430
619315  feet/sec       YDOT =         819
958697  meter/sec
 ZDOT =      -9438
402089                 ZDOT =       -2842
461487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1964475
23                 X    =         -598772
05
 Y    =       15946016
56  feet           Y    =         4860345
85  meter
 Z    =       15372714
40                 Z    =         4685603
35
 XDOT =     -21384
682885                 XDOT =       -6518
051343
 YDOT =       6357
402622  feet/sec       YDOT =        1937
736319  meter/sec
 ZDOT =      -9286
161121                 ZDOT =       -2830
421910


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   17286
54323982  
00016717  00000-0  10270-3 0  9007
2 25544  51
6417 168
3158 0005003  10
6567 349
4691 15
54209732   151


Satellite: ISS
Catalog Number: 25544
Epoch time:      17286
54323982   =   yrday
fracday
Element set:     900
Inclination:       51
6417  deg
RA of node:       168
3158  deg
Eccentricity:     
0005003     
Arg of perigee:    10
6567  deg
Mean anomaly:     349
4691  deg
Mean motion:   15
54209732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              15
Checksum:              302


Coasting Arc #2 (Orbit 19)
---------------------------------------

Vector Time (GMT): 2017/286/19:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         264904
82                 A    =         6777694
06  meter
 Y    =       -4315897
40  meter          E    =           
0007863
 Z    =        5216385
94                 I    =           51
70859
 XDOT =       7521
391993                 Wp   =           35
11151
 YDOT =       -957
017412  meter/sec      RA   =          165
77128  deg
 ZDOT =      -1166
609768                 TA   =           66
10190
                                          MA   =           66
01953
                                          Ha   =            221
909  n
mi
                                          Hp   =            214
008

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         869110
31                 X    =          287807
79
 Y    =      -14159768
38  feet           Y    =        -4312806
66  meter
 Z    =       17114127
09                 Z    =         5217728
69
 XDOT =      24676
482917                 XDOT =        7537
201476
 YDOT =      -3139
820907  feet/sec       YDOT =        -872
819754  meter/sec
 ZDOT =      -3827
459868                 ZDOT =       -1130
034416

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10327103
67                 X    =         3147701
20
 Y    =       -9715075
12  feet           Y    =        -2961154
90  meter
 Z    =       17120630
39                 Z    =         5218368
14
 XDOT =      19321
804497                 XDOT =        5889
286011
 YDOT =      14038
576694  feet/sec       YDOT =        4278
958176  meter/sec
 ZDOT =      -3665
189988                 ZDOT =       -1117
149908


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   17286
86474550  
00016717  00000-0  10270-3 0  9011
2 25544  51
6403 166
7073 0004523  16
2452 343
8845 15
54151771   209


Satellite: ISS
Catalog Number: 25544
Epoch time:      17286
86474550   =   yrday
fracday
Element set:     901
Inclination:       51
6403  deg
RA of node:       166
7073  deg
Eccentricity:     
0004523     
Arg of perigee:    16
2452  deg
Mean anomaly:     343
8845  deg
Mean motion:   15
54151771  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              20
Checksum:              294


Coasting Arc #3 (Orbit 27)
---------------------------------------

Vector Time (GMT): 2017/287/08:46:53
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -643725
66                 A    =         6778133
78  meter
 Y    =        4415003
92  meter          E    =           
0014701
 Z    =       -5114720
14                 I    =           51
72731
 XDOT =      -7418
954273                 Wp   =           82
76260
 YDOT =        868
362517  meter/sec      RA   =          163
04582  deg
 ZDOT =       1689
267843                 TA   =          203
52186
                                          MA   =          203
58916
                                          Ha   =            222
061  n
mi
                                          Hp   =            213
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2111960
82                 X    =         -668202
57
 Y    =       14484920
99  feet           Y    =         4407668
09  meter
 Z    =      -16780577
89                 Z    =        -5117906
97
 XDOT =     -24340
401157                 XDOT =       -7436
318841
 YDOT =       2848
958390  feet/sec       YDOT =         785
301743  meter/sec
 ZDOT =       5542
217332                 ZDOT =        1653
186341

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8159809
12                 X    =         2487109
82
 Y    =      -12132498
85  feet           Y    =        -3697985
65  meter
 Z    =      -16795270
04                 Z    =        -5119198
31
 XDOT =      22265
935526                 XDOT =        6786
657148
 YDOT =       7551
621461  feet/sec       YDOT =        2301
734221  meter/sec
 ZDOT =       5382
136977                 ZDOT =        1640
475350


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   17287
37914935  
00016717  00000-0  10270-3 0  9025
2 25544  51
6401 164
1471 0005056  16
1207 344
0105 15
54166171   280


Satellite: ISS
Catalog Number: 25544
Epoch time:      17287
37914935   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:       164
1471  deg
Eccentricity:     
0005056     
Arg of perigee:    16
1207  deg
Mean anomaly:     344
0105  deg
Mean motion:   15
54166171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              28
Checksum:              279


Coasting Arc #4 (Orbit 43)
---------------------------------------

Vector Time (GMT): 2017/288/08:46:53
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2343374
33                 A    =         6781132
94  meter
 Y    =       -4639249
03  meter          E    =           
0013287
 Z    =        4350804
90                 I    =           51
76812
 XDOT =       6839
434982                 Wp   =           54
35048
 YDOT =        189
441502  meter/sec      RA   =          158
05972  deg
 ZDOT =      -3466
774846                 TA   =           70
84856
                                          MA   =           70
70478
                                          Ha   =            222
087  n
mi
                                          Hp   =            213
774

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7688236
00                 X    =         2373943
22
 Y    =      -15220633
30  feet           Y    =        -4612872
49  meter
 Z    =       14274294
31                 Z    =         4362263
07
 XDOT =      22439
091147                 XDOT =        6853
648316
 YDOT =        621
527236  feet/sec       YDOT =         266
003881  meter/sec
 ZDOT =     -11373
933222                 ZDOT =       -3433
516198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13327506
22                 X    =        -4062223
90
 Y    =       10568076
05  feet           Y    =         3221149
58  meter
 Z    =       14325692
85                 Z    =         4366471
18
 XDOT =     -19358
973280                 XDOT =       -5900
615056
 YDOT =      -9129
147354  feet/sec       YDOT =       -2782
564114  meter/sec
 ZDOT =     -11226
486216                 ZDOT =       -3421
832999


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   17288
40795562  
00016717  00000-0  10270-3 0  9034
2 25544  51
6399 159
0194 0005039  20
1249 340
0101 15
54165100   444


Satellite: ISS
Catalog Number: 25544
Epoch time:      17288
40795562   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       159
0194  deg
Eccentricity:     
0005039     
Arg of perigee:    20
1249  deg
Mean anomaly:     340
0101  deg
Mean motion:   15
54165100  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              44
Checksum:              282


Coasting Arc #5 (Orbit 58)
---------------------------------------

Vector Time (GMT): 2017/289/08:46:53
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3750214
14                 A    =         6784868
53  meter
 Y    =        4689648
65  meter          E    =           
0008429
 Z    =       -3157865
94                 I    =           51
81133
 XDOT =      -5772
663287                 Wp   =           49
73504
 YDOT =      -1354
608801  meter/sec      RA   =          153
08422  deg
 ZDOT =       4857
650817                 TA   =          273
95184
                                          MA   =          274
04819
                                          Ha   =            222
102  n
mi
                                          Hp   =            213
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12303852
18                 X    =        -3787036
78
 Y    =       15385986
40  feet           Y    =         4647504
97  meter
 Z    =      -10360452
57                 Z    =        -3176173
47
 XDOT =     -18939
184011                 XDOT =       -5780
683010
 YDOT =      -4444
254598  feet/sec       YDOT =       -1419
206987  meter/sec
 ZDOT =      15937
174596                 ZDOT =        4829
589356

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17448568
60                 X    =         5318323
71
 Y    =       -9053146
12  feet           Y    =        -2759398
94  meter
 Z    =      -10442237
92                 Z    =        -3182794
12
 XDOT =      14912
627215                 XDOT =        4545
368775
 YDOT =      10554
618094  feet/sec       YDOT =        3217
047595  meter/sec
 ZDOT =      15812
909280                 ZDOT =        4819
774749


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   17289
37245749  
00016717  00000-0  10270-3 0  9049
2 25544  51
6404 154
2109 0004999  22
6605 337
4767 15
54184005   590


Satellite: ISS
Catalog Number: 25544
Epoch time:      17289
37245749   =   yrday
fracday
Element set:     904
Inclination:       51
6404  deg
RA of node:       154
2109  deg
Eccentricity:     
0004999     
Arg of perigee:    22
6605  deg
Mean anomaly:     337
4767  deg
Mean motion:   15
54184005  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              59
Checksum:              323


Coasting Arc #6 (Orbit 60)
---------------------------------------

Vector Time (GMT): 2017/289/11:09:57
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5012447
65                 A    =         6787799
22  meter
 Y    =       -4198542
83  meter          E    =           
0014789
 Z    =        1807022
73                 I    =           51
82476
 XDOT =       4366
384890                 Wp   =           94
61459
 YDOT =       2756
480630  meter/sec      RA   =          152
59927  deg
 ZDOT =      -5668
480486                 TA   =           65
57847
                                          MA   =           65
42424
                                          Ha   =            222
168  n
mi
                                          Hp   =            213
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16445038
22                 X    =         5050246
60
 Y    =      -13774746
81  feet           Y    =        -4142278
67  meter
 Z    =        5928552
27                 Z    =         1831464
19
 XDOT =      14325
409745                 XDOT =        4362
771694
 YDOT =       9043
571622  feet/sec       YDOT =        2805
287715  meter/sec
 ZDOT =     -18597
376923                 ZDOT =       -5647
278768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13247648
55                 X    =        -4037883
28
 Y    =       16833874
89  feet           Y    =         5130965
07  meter
 Z    =        6037476
93                 Z    =         1840222
97
 XDOT =     -14761
484389                 XDOT =       -4499
300442
 YDOT =      -4935
628634  feet/sec       YDOT =       -1504
379608  meter/sec
 ZDOT =     -18503
709980                 ZDOT =       -5639
930802


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   17289
50105737  
00016717  00000-0  10270-3 0  9057
2 25544  51
6415 153
5710 0004974  23
6522 336
4859 15
54161821   619


Satellite: ISS
Catalog Number: 25544
Epoch time:      17289
50105737   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       153
5710  deg
Eccentricity:     
0004974     
Arg of perigee:    23
6522  deg
Mean anomaly:     336
4859  deg
Mean motion:   15
54161821  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              61
Checksum:              300


Coasting Arc #7 (Orbit 70)
---------------------------------------

Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2205098
61                 A    =         6777257
18  meter
 Y    =        3572493
88  meter          E    =           
0017790
 Z    =       -5335230
42                 I    =           51
80546
 XDOT =      -6558
740122                 Wp   =           75
31341
 YDOT =       3948
523934  meter/sec      RA   =          149
31973  deg
 ZDOT =        -62
617927                 TA   =          194
06548
                                          MA   =          194
11508
                                          Ha   =            222
256  n
mi
                                          Hp   =            213
653

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7234575
51                 X    =         2190902
45
 Y    =       11720780
46  feet           Y    =         3597072
83  meter
 Z    =      -17504036
81                 Z    =        -5324553
47
 XDOT =     -21518
176253                 XDOT =       -6602
101938
 YDOT =      12954
474850  feet/sec       YDOT =        3874
937165  meter/sec
 ZDOT =       -205
439394                 ZDOT =         -94
584468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13476430
06                 X    =         4107615
88
 Y    =       -3121051
32  feet           Y    =         -951296
44  meter
 Z    =      -17457146
20                 Z    =        -5320938
16
 XDOT =       4993
444292                 XDOT =        1522
001820
 YDOT =      23583
773049  feet/sec       YDOT =        7188
334025  meter/sec
 ZDOT =       -347
712432                 ZDOT =        -105
982749


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   17290
14405468  
00016717  00000-0  10270-3 0  9064
2 25544  51
6384 150
3636 0004984  27
6565 332
4852 15
54165257   715


Satellite: ISS
Catalog Number: 25544
Epoch time:      17290
14405468   =   yrday
fracday
Element set:     906
Inclination:       51
6384  deg
RA of node:       150
3636  deg
Eccentricity:     
0004984     
Arg of perigee:    27
6565  deg
Mean anomaly:     332
4852  deg
Mean motion:   15
54165257  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              71
Checksum:              313


Coasting Arc #8 (Orbit 86)
---------------------------------------

Vector Time (GMT): 2017/291/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -590278
76                 A    =         6778299
05  meter
 Y    =       -4469267
07  meter          E    =           
0010294
 Z    =        5057875
78                 I    =           51
83564
 XDOT =       6784
676110                 Wp   =           43
56269
 YDOT =      -3043
304191  meter/sec      RA   =          144
33216  deg
 ZDOT =      -1887
773328                 TA   =           64
72855
                                          MA   =           64
62191
                                          Ha   =            222
274  n
mi
                                          Hp   =            213
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1936610
10                 X    =         -564827
48
 Y    =      -14662949
71  feet           Y    =        -4475725
09  meter
 Z    =       16594080
63                 Z    =         5055070
66
 XDOT =      22259
436056                 XDOT =        6827
372940
 YDOT =      -9984
593801  feet/sec       YDOT =       -2967
194791  meter/sec
 ZDOT =      -6193
482046                 ZDOT =       -1854
710827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14573044
94                 X    =        -4441864
10
 Y    =       -2602388
42  feet           Y    =         -793207
99  meter
 Z    =       16582219
41                 Z    =         5054260
48
 XDOT =      -2766
753830                 XDOT =        -843
306567
 YDOT =     -23234
094757  feet/sec       YDOT =       -7081
752082  meter/sec
 ZDOT =      -6046
449935                 ZDOT =       -1842
957940


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   17291
17284810  
00016717  00000-0  10270-3 0  9075
2 25544  51
6371 145
2343 0005041  29
7025 330
4413 15
54189785   878


Satellite: ISS
Catalog Number: 25544
Epoch time:      17291
17284810   =   yrday
fracday
Element set:     907
Inclination:       51
6371  deg
RA of node:       145
2343  deg
Eccentricity:     
0005041     
Arg of perigee:    29
7025  deg
Mean anomaly:     330
4413  deg
Mean motion:   15
54189785  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              87
Checksum:              297


Coasting Arc #9 (Orbit 101)
---------------------------------------

Vector Time (GMT): 2017/292/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -906595
69                 A    =         6781459
57  meter
 Y    =        5196099
89  meter          E    =           
0010691
 Z    =       -4270539
52                 I    =           51
87158
 XDOT =      -6497
823629                 Wp   =           82
85294
 YDOT =       1833
867650  meter/sec      RA   =          139
35345  deg
 ZDOT =       3619
804043                 TA   =          224
02290
                                          MA   =          224
10809
                                          Ha   =            222
368  n
mi
                                          Hp   =            213
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2974395
30                 X    =         -943887
84
 Y    =       17047571
83  feet           Y    =         5185752
75  meter
 Z    =      -14010956
42                 Z    =        -4275034
71
 XDOT =     -21318
318994                 XDOT =       -6535
431111
 YDOT =       6016
626147  feet/sec       YDOT =        1760
994664  meter/sec
 ZDOT =      11875
997517                 ZDOT =        3588
147401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15447820
76                 X    =         4708495
77
 Y    =        7762300
65  feet           Y    =         2365949
24  meter
 Z    =      -14031577
06                 Z    =        -4276824
69
 XDOT =         33
566952                 XDOT =          10
231207
 YDOT =      21093
068306  feet/sec       YDOT =        6429
167220  meter/sec
 ZDOT =      11735
343981                 ZDOT =        3576
932845


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   17292
13733941  
00016717  00000-0  10270-3 0  9087
2 25544  51
6367 140
4263 0005111  33
2755 326
8718 15
54170491  1028


Satellite: ISS
Catalog Number: 25544
Epoch time:      17292
13733941   =   yrday
fracday
Element set:     908
Inclination:       51
6367  deg
RA of node:       140
4263  deg
Eccentricity:     
0005111     
Arg of perigee:    33
2755  deg
Mean anomaly:     326
8718  deg
Mean motion:   15
54170491  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             102
Checksum:              289


Coasting Arc #10 (Orbit 117)
---------------------------------------

Vector Time (GMT): 2017/293/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2254660
11                 A    =         6785249
82  meter
 Y    =       -5653139
41  meter          E    =           
0016231
 Z    =        2989030
46                 I    =           51
90899
 XDOT =       5809
947762                 Wp   =           81
14662
 YDOT =       -337
723934  meter/sec      RA   =          134
38512  deg
 ZDOT =      -4995
713491                 TA   =           64
78995
                                          MA   =           64
62176
                                          Ha   =            222
319  n
mi
                                          Hp   =            213
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7397178
85                 X    =         2303187
85
 Y    =      -18547045
31  feet           Y    =        -5627654
64  meter
 Z    =        9806530
38                 Z    =         3000101
58
 XDOT =      19061
508407                 XDOT =        5837
559802
 YDOT =      -1108
018157  feet/sec       YDOT =        -272
599220  meter/sec
 ZDOT =     -16390
136126                 ZDOT =       -4967
422769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15786260
06                 X    =        -4811652
07
 Y    =      -12187070
66  feet           Y    =        -3714619
14  meter
 Z    =        9856393
08                 Z    =         3004228
61
 XDOT =       3359
852493                 XDOT =        1024
083040
 YDOT =     -17573
645606  feet/sec       YDOT =       -5356
447181  meter/sec
 ZDOT =     -16264
598253                 ZDOT =       -4957
449548


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
16612469  
00016717  00000-0  10270-3 0  9093
2 25544  51
6368 135
2963 0005117  35
7243 324
4251 15
54216276  1188


Satellite: ISS
Catalog Number: 25544
Epoch time:      17293
16612469   =   yrday
fracday
Element set:     909
Inclination:       51
6368  deg
RA of node:       135
2963  deg
Eccentricity:     
0005117     
Arg of perigee:    35
7243  deg
Mean anomaly:     324
4251  deg
Mean motion:   15
54216276  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             118
Checksum:              305


Coasting Arc #11 (Orbit 132)
---------------------------------------

Vector Time (GMT): 2017/294/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3286977
68                 A    =         6788170
03  meter
 Y    =        5758598
43  meter          E    =           
0013600
 Z    =       -1428599
50                 I    =           51
94100
 XDOT =      -4817
429275                 Wp   =           39
09129
 YDOT =      -1315
917472  meter/sec      RA   =          129
42906  deg
 ZDOT =       5820
082236                 TA   =          305
39336
                                          MA   =          305
52033
                                          Ha   =            222
404  n
mi
                                          Hp   =            213
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10784047
52                 X    =        -3344187
95
 Y    =       18893039
47  feet           Y    =         5721521
21  meter
 Z    =       -4687006
23                 Z    =        -1444706
45
 XDOT =     -15805
214156                 XDOT =       -4830
628151
 YDOT =      -4317
314541  feet/sec       YDOT =       -1369
862598  meter/sec
 ZDOT =      19094
757993                 ZDOT =        5796
648081

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15436376
60                 X    =         4705007
59
 Y    =       15306161
05  feet           Y    =         4665317
89  meter
 Z    =       -4759239
41                 Z    =        -1450616
17
 XDOT =      -7203
025918                 XDOT =       -2195
482300
 YDOT =      13128
763460  feet/sec       YDOT =        4001
647103  meter/sec
 ZDOT =      18990
977895                 ZDOT =        5788
450062


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
13060686  
00016717  00000-0  10270-3 0  9101
2 25544  51
6369 130
4880 0005168  40
6948 319
4590 15
54219057  1334


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
13060686   =   yrday
fracday
Element set:     910
Inclination:       51
6369  deg
RA of node:       130
4880  deg
Eccentricity:     
0005168     
Arg of perigee:    40
6948  deg
Mean anomaly:     319
4590  deg
Mean motion:   15
54219057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             133
Checksum:              309


Coasting Arc #12 (Orbit 136)
---------------------------------------

Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3341067
14                 A    =         6777065
25  meter
 Y    =        2526240
42  meter          E    =           
0018566
 Z    =       -5343295
02                 I    =           51
91247
 XDOT =      -4693
209288                 Wp   =           77
06442
 YDOT =       6047
457377  meter/sec      RA   =          128
23368  deg
 ZDOT =        -71
587623                 TA   =          192
23223
                                          MA   =          192
27737
                                          Ha   =            222
374  n
mi
                                          Hp   =            213
297

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10961506
37                 X    =         3338525
54
 Y    =        8288190
35  feet           Y    =         2563587
90  meter
 Z    =      -17530495
49                 Z    =        -5327071
08
 XDOT =     -15397
668268                 XDOT =       -4760
137012
 YDOT =      19840
739427  feet/sec       YDOT =        5994
600485  meter/sec
 ZDOT =       -234
867529                 ZDOT =         -94
549400

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8146128
13                 X    =        -2482939
85
 Y    =      -11180143
78  feet           Y    =        -3407707
83  meter
 Z    =      -17458865
21                 Z    =        -5321462
12
 XDOT =      19738
932645                 XDOT =        6016
426670
 YDOT =     -13835
429045  feet/sec       YDOT =       -4217
038773  meter/sec
 ZDOT =       -337
554510                 ZDOT =        -102
886615


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
38780094  
00016717  00000-0  10270-3 0  9111
2 25544  51
6404 129
2067 0005156  38
4789 321
6731 15
54231097  1376


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
38780094   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:       129
2067  deg
Eccentricity:     
0005156     
Arg of perigee:    38
4789  deg
Mean anomaly:     321
6731  deg
Mean motion:   15
54231097  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             137
Checksum:              311


Coasting Arc #13 (Orbit 152)
---------------------------------------

Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2150875
97                 A    =         6778109
41  meter
 Y    =       -3952233
52  meter          E    =           
0010528
 Z    =        5064284
15                 I    =           51
93549
 XDOT =       5233
842439                 Wp   =           48
93410
 YDOT =      -5282
423664  meter/sec      RA   =          123
25303  deg
 ZDOT =      -1890
290777                 TA   =           59
35295
                                          MA   =           59
24920
                                          Ha   =            222
391  n
mi
                                          Hp   =            213
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7056679
68                 X    =        -2131121
66
 Y    =      -12966645
42  feet           Y    =        -3976175
35  meter
 Z    =       16615105
47                 Z    =         5053883
78
 XDOT =      17171
399078                 XDOT =        5301
705272
 YDOT =     -17330
786299  feet/sec       YDOT =       -5223
515926  meter/sec
 ZDOT =      -6201
741393                 ZDOT =       -1864
700576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3280402
38                 X    =          999866
65
 Y    =       14445852
86  feet           Y    =         4403095
95  meter
 Z    =       16569509
55                 Z    =         5050386
51
 XDOT =     -20296
611098                 XDOT =       -6186
407063
 YDOT =      11626
454443  feet/sec       YDOT =        3543
743314  meter/sec
 ZDOT =      -6087
475795                 ZDOT =       -1855
462622


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
41657567  
00016717  00000-0  10270-3 0  9125
2 25544  51
6401 124
0776 0005061  41
1951 318
9583 15
54259479  1536


Satellite: ISS
Catalog Number: 25544
Epoch time:      17295
41657567   =   yrday
fracday
Element set:     912
Inclination:       51
6401  deg
RA of node:       124
0776  deg
Eccentricity:     
0005061     
Arg of perigee:    41
1951  deg
Mean anomaly:     318
9583  deg
Mean motion:   15
54259479  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             153
Checksum:              315


Coasting Arc #14 (Orbit 167)
---------------------------------------

Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1008824
31                 A    =         6781319
45  meter
 Y    =        5177373
48  meter          E    =           
0011286
 Z    =       -4271064
78                 I    =           51
96339
 XDOT =      -5400
109518                 Wp   =           86
21817
 YDOT =       4040
813209  meter/sec      RA   =          118
27950  deg
 ZDOT =       3631
734379                 TA   =          220
74904
                                          MA   =          220
83351
                                          Ha   =            222
417  n
mi
                                          Hp   =            213
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3309791
06                 X    =          971601
84
 Y    =       16986133
45  feet           Y    =         5188446
54  meter
 Z    =      -14012679
73                 Z    =        -4266254
72
 XDOT =     -17716
894745                 XDOT =       -5462
535265
 YDOT =      13257
261183  feet/sec       YDOT =        3980
076603  meter/sec
 ZDOT =      11915
139038                 ZDOT =        3605
349845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1155139
42                 X    =          352086
50
 Y    =      -17283702
68  feet           Y    =        -5268072
58  meter
 Z    =      -13992066
12                 Z    =        -4264781
75
 XDOT =      19380
737900                 XDOT =        5907
248912
 YDOT =      -8231
530224  feet/sec       YDOT =       -2508
970412  meter/sec
 ZDOT =      11797
501052                 ZDOT =        3595
878321


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
38105013  
00016717  00000-0  10270-3 0  9137
2 25544  51
6404 119
2687 0005061  44
0985 316
0570 15
54234006  1685


Satellite: ISS
Catalog Number: 25544
Epoch time:      17296
38105013   =   yrday
fracday
Element set:     913
Inclination:       51
6404  deg
RA of node:       119
2687  deg
Eccentricity:     
0005061     
Arg of perigee:    44
0985  deg
Mean anomaly:     316
0570  deg
Mean motion:   15
54234006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             168
Checksum:              286


Coasting Arc #15 (Orbit 183)
---------------------------------------

Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          91275
37                 A    =         6785177
37  meter
 Y    =       -6090407
93  meter          E    =           
0016987
 Z    =        2977357
71                 I    =           51
99160
 XDOT =       5293
796425                 Wp   =           83
69823
 YDOT =      -2384
158964  meter/sec      RA   =          113
31697  deg
 ZDOT =      -5012
984563                 TA   =           62
42887
                                          MA   =           62
25642
                                          Ha   =            222
454  n
mi
                                          Hp   =            212
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         299459
88                 X    =          144910
26
 Y    =      -19981653
32  feet           Y    =        -6089087
25  meter
 Z    =        9768233
96                 Z    =         2977931
57
 XDOT =      17368
098507                 XDOT =        5344
414491
 YDOT =      -7822
043845  feet/sec       YDOT =       -2324
677246  meter/sec
 ZDOT =     -16446
799747                 ZDOT =       -4987
145299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5117179
69                 X    =        -1559716
37
 Y    =       19315895
78  feet           Y    =         5887485
03  meter
 Z    =        9771651
99                 Z    =         2978399
53
 XDOT =     -17450
187547                 XDOT =       -5318
817164
 YDOT =       3682
725247  feet/sec       YDOT =        1122
494655  meter/sec
 ZDOT =     -16331
798685                 ZDOT =       -4977
932239


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
40981609  
00016717  00000-0  10270-3 0  9145
2 25544  51
6409 114
1389 0005231  46
8319 313
3265 15
54263594  1846


Satellite: ISS
Catalog Number: 25544
Epoch time:      17297
40981609   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:       114
1389  deg
Eccentricity:     
0005231     
Arg of perigee:    46
8319  deg
Mean anomaly:     313
3265  deg
Mean motion:   15
54263594  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             184
Checksum:              315


Coasting Arc #16 (Orbit 198)
---------------------------------------

Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1020080
66                 A    =         6788201
53  meter
 Y    =        6557112
77  meter          E    =           
0013636
 Z    =       -1405837
27                 I    =           52
01190
 XDOT =      -4955
883164                 Wp   =           42
58403
 YDOT =        470
442566  meter/sec      RA   =          108
36563  deg
 ZDOT =       5832
924919                 TA   =          302
17006
                                          MA   =          302
30226
                                          Ha   =            222
533  n
mi
                                          Hp   =            212
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3346721
33                 X    =        -1086499
21
 Y    =       21512837
16  feet           Y    =         6545334
13  meter
 Z    =       -4612326
99                 Z    =        -1410954
09
 XDOT =     -16259
459199                 XDOT =       -4989
109559
 YDOT =       1543
446740  feet/sec       YDOT =         414
836853  meter/sec
 ZDOT =      19136
892778                 ZDOT =        5808
769530

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8133230
21                 X    =         2479008
57
 Y    =      -20189959
24  feet           Y    =        -6153899
58  meter
 Z    =       -4635987
36                 Z    =        -1413048
95
 XDOT =      14833
227535                 XDOT =        4521
167753
 YDOT =       1637
781965  feet/sec       YDOT =         499
195943  meter/sec
 ZDOT =      19029
627580                 ZDOT =        5800
230486


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
37428188  
00016717  00000-0  10270-3 0  9151
2 25544  51
6394 109
3303 0005165  50
3991 309
7618 15
54223788  1991


Satellite: ISS
Catalog Number: 25544
Epoch time:      17298
37428188   =   yrday
fracday
Element set:     915
Inclination:       51
6394  deg
RA of node:       109
3303  deg
Eccentricity:     
0005165     
Arg of perigee:    50
3991  deg
Mean anomaly:     309
7618  deg
Mean motion:   15
54223788  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             199
Checksum:              336


Coasting Arc #17 (Orbit 214)
---------------------------------------

Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1853076
65                 A    =         6789007
10  meter
 Y    =       -6517318
37  meter          E    =           
0013004
 Z    =        -371210
73                 I    =           52
02459
 XDOT =       4456
259797                 Wp   =          115
18737
 YDOT =       1600
772103  meter/sec      RA   =          103
42106  deg
 ZDOT =      -6028
878025                 TA   =           68
79199
                                          MA   =           68
65313
                                          Ha   =            222
529  n
mi
                                          Hp   =            212
974

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6079647
81                 X    =         1927620
52
 Y    =      -21382278
13  feet           Y    =        -6496179
21  meter
 Z    =       -1217882
97                 Z    =         -362027
68
 XDOT =      14620
274924                 XDOT =        4467
314244
 YDOT =       5251
876978  feet/sec       YDOT =        1650
666724  meter/sec
 ZDOT =     -19779
783546                 ZDOT =       -6007
203655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10465897
73                 X    =        -3190005
63
 Y    =       19614504
61  feet           Y    =         5978501
00  meter
 Z    =       -1176166
67                 Z    =         -358495
60
 XDOT =     -11878
029033                 XDOT =       -3620
423249
 YDOT =      -7483
605121  feet/sec       YDOT =       -2281
002841  meter/sec
 ZDOT =     -19683
825525                 ZDOT =       -5999
630020


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
40304143  
00016717  00000-0  10270-3 0  9161
2 25544  51
6402 104
2013 0004989  55
1977 304
9644 15
54219387  2158


Satellite: ISS
Catalog Number: 25544
Epoch time:      17299
40304143   =   yrday
fracday
Element set:     916
Inclination:       51
6402  deg
RA of node:       104
2013  deg
Eccentricity:     
0004989     
Arg of perigee:    55
1977  deg
Mean anomaly:     304
9644  deg
Mean motion:   15
54219387  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             215
Checksum:              303


Coasting Arc #18 (Orbit 216)
---------------------------------------

Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2957218
10                 A    =         6787128
14  meter
 Y    =       -5750369
12  meter          E    =           
0008994
 Z    =       -2064960
48                 I    =           52
01757
 XDOT =       3591
542329                 Wp   =          105
13730
 YDOT =       3840
477458  meter/sec      RA   =          102
77657  deg
 ZDOT =      -5573
746750                 TA   =           97
56584
                                          MA   =           97
46367
                                          Ha   =            222
534  n
mi
                                          Hp   =            212
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9702159
13                 X    =         3031331
24
 Y    =      -18866040
41  feet           Y    =        -5716885
14  meter
 Z    =       -6774804
74                 Z    =        -2050414
82
 XDOT =      11783
275356                 XDOT =        3575
405204
 YDOT =      12599
991659  feet/sec       YDOT =        3880
550190  meter/sec
 ZDOT =     -18286
570701                 ZDOT =       -5556
339090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2998469
06                 X    =          913933
37
 Y    =       21022618
66  feet           Y    =         6407694
17  meter
 Z    =       -6709399
35                 Z    =        -2045024
92
 XDOT =     -15469
818699                 XDOT =       -4715
200739
 YDOT =      -3581
493563  feet/sec       YDOT =       -1091
639238  meter/sec
 ZDOT =     -18209
879369                 ZDOT =       -5550
371232


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
53163609  
00016717  00000-0  10270-3 0  9176
2 25544  51
6379 103
5556 0005147  58
6387 301
5268 15
54273820  2174


Satellite: ISS
Catalog Number: 25544
Epoch time:      17299
53163609   =   yrday
fracday
Element set:     917
Inclination:       51
6379  deg
RA of node:       103
5556  deg
Eccentricity:     
0005147     
Arg of perigee:    58
6387  deg
Mean anomaly:     301
5268  deg
Mean motion:   15
54273820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             217
Checksum:              324


Coasting Arc #19 (Orbit 232)
---------------------------------------

Vector Time (GMT): 2017/300/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3425856
91                 A    =         6783684
08  meter
 Y    =        4655538
56  meter          E    =           
0016814
 Z    =        3534634
60                 I    =           52
01233
 XDOT =      -2812
035456                 Wp   =           83
92035
 YDOT =      -5520
919944  meter/sec      RA   =           97
82253  deg
 ZDOT =       4529
537094                 TA   =          317
52702
                                          MA   =          317
65701
                                          Ha   =            222
617  n
mi
                                          Hp   =            212
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11239688
02                 X    =        -3494831
58
 Y    =       15274076
63  feet           Y    =         4616842
71  meter
 Z    =       11596570
21                 Z    =         3517824
91
 XDOT =      -9225
838109                 XDOT =       -2772
092705
 YDOT =     -18113
254408  feet/sec       YDOT =       -5552
142596  meter/sec
 ZDOT =      14860
686003                 ZDOT =        4515
974019

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          35468
95                 X    =           10810
93
 Y    =      -19009672
42  feet           Y    =        -5794148
15  meter
 Z    =       11521264
72                 Z    =         3511681
49
 XDOT =      16869
730394                 XDOT =        5141
893824
 YDOT =       9035
552586  feet/sec       YDOT =        2754
036428  meter/sec
 ZDOT =      14801
312376                 ZDOT =        4511
440012


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
56038924  
00016717  00000-0  10270-3 0  9184
2 25544  51
6380  98
4258 0005033  64
3607 295
8065 15
54269555  2338


Satellite: ISS
Catalog Number: 25544
Epoch time:      17300
56038924   =   yrday
fracday
Element set:     918
Inclination:       51
6380  deg
RA of node:        98
4258  deg
Eccentricity:     
0005033     
Arg of perigee:    64
3607  deg
Mean anomaly:     295
8065  deg
Mean motion:   15
54269555  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             233
Checksum:              316
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