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

 
Date: June 8th 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) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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


160/01:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 8
000/00:00:00 000 0 0 0 0 216 6

165/09:20:13 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 7

167/11:41:08 000 0 0 0 0 0 0
N/A 0 0 0 0 219 7
000/00:00:00 000 0 0 0 0 216 6

167/16:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 216 4

Coasting Arc #1 (Orbit 2022)
---------------------------------------

Vector Time (GMT): 2017/158/10:33:06
005
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4189354
27                 A    =         6778058
45  meter
 Y    =         781670
93  meter          E    =           
0010542
 Z    =       -5279744
42                 I    =           51
99484
 XDOT =       -219
814101                 Wp   =          109
42935
 YDOT =       7598
510355  meter/sec      RA   =           86
06058  deg
 ZDOT =        948
677806                 TA   =          169
62382
                                          MA   =          169
60205
                                          Ha   =            219
889  n
mi
                                          Hp   =            216
655

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13744600
62                 X    =         4205948
80
 Y    =        2564537
17  feet           Y    =          828612
52  meter
 Z    =      -17321996
13                 Z    =        -5259353
16
 XDOT =       -721
174871                 XDOT =        -309
374572
 YDOT =      24929
495915  feet/sec       YDOT =        7595
551373  meter/sec
 ZDOT =       3112
459993                 ZDOT =         947
393342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10314928
28                 X    =         3143990
14
 Y    =       -9602079
11  feet           Y    =        -2926713
71  meter
 Z    =      -17232085
72                 Z    =        -5252339
73
 XDOT =      18879
562919                 XDOT =        5754
490778
 YDOT =      14696
983131  feet/sec       YDOT =        4479
640458  meter/sec
 ZDOT =       3105
451376                 ZDOT =         946
541580


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   17158
45412224  
00016717  00000-0  10270-3 0  9003
2 25544  51
6400  86
8441 0004666 248
9342 111
1312 15
53988886 20231


Satellite: ISS
Catalog Number: 25544
Epoch time:      17158
45412224   =   yrday
fracday
Element set:     900
Inclination:       51
6400  deg
RA of node:        86
8441  deg
Eccentricity:     
0004666     
Arg of perigee:   248
9342  deg
Mean anomaly:     111
1312  deg
Mean motion:   15
53988886  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2023
Checksum:              298


Coasting Arc #2 (Orbit 2038)
---------------------------------------

Vector Time (GMT): 2017/159/10:33:06
005
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4149037
95                 A    =         6780236
20  meter
 Y    =       -2476336
54  meter          E    =           
0003350
 Z    =        4755404
77                 I    =           51
99910
 XDOT =       1066
587655                 Wp   =           47
95653
 YDOT =      -7077
679096  meter/sec      RA   =           81
09039  deg
 ZDOT =      -2751
633521                 TA   =           69
15021
                                          MA   =           69
11435
                                          Ha   =            219
907  n
mi
                                          Hp   =            216
528

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13612329
22                 X    =        -4144138
24
 Y    =       -8124463
70  feet           Y    =        -2522707
11  meter
 Z    =       15601721
68                 Z    =         4735261
36
 XDOT =       3499
303331                 XDOT =        1159
019094
 YDOT =     -23220
731943  feet/sec       YDOT =       -7065
234620  meter/sec
 ZDOT =      -9027
669033                 ZDOT =       -2746
228716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14586451
96                 X    =        -4445950
56
 Y    =        6425884
02  feet           Y    =         1958609
45  meter
 Z    =       15513206
33                 Z    =         4728425
29
 XDOT =     -16345
715721                 XDOT =       -4982
174152
 YDOT =     -15343
045199  feet/sec       YDOT =       -4676
560177  meter/sec
 ZDOT =      -9002
537587                 ZDOT =       -2743
973456


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   17159
48304412  
00016717  00000-0  10270-3 0  9017
2 25544  51
6401  81
7170 0004620 253
4044 106
6601 15
53993597 20397


Satellite: ISS
Catalog Number: 25544
Epoch time:      17159
48304412   =   yrday
fracday
Element set:     901
Inclination:       51
6401  deg
RA of node:        81
7170  deg
Eccentricity:     
0004620     
Arg of perigee:   253
4044  deg
Mean anomaly:     106
6601  deg
Mean motion:   15
53993597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2039
Checksum:              288


Coasting Arc #3 (Orbit 2048)
---------------------------------------

Vector Time (GMT): 2017/160/01:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3525478
99                 A    =         6778597
70  meter
 Y    =        2688800
99  meter          E    =           
0004528
 Z    =        5129005
57                 I    =           51
99204
 XDOT =      -2822
963719                 Wp   =          186
34857
 YDOT =      -6926
030445  meter/sec      RA   =           77
97301  deg
 ZDOT =       1686
229680                 TA   =          247
41912
                                          MA   =          247
46704
                                          Ha   =            219
803  n
mi
                                          Hp   =            216
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11566532
11                 X    =        -3580198
30
 Y    =        8821525
56  feet           Y    =         2649070
04  meter
 Z    =       16827446
09                 Z    =         5111747
16
 XDOT =      -9261
691993                 XDOT =       -2753
496185
 YDOT =     -22723
196997  feet/sec       YDOT =       -6957
210551  meter/sec
 ZDOT =       5532
249606                 ZDOT =        1672
684229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11347978
69                 X    =        -3458863
90
 Y    =       -9241368
09  feet           Y    =        -2816768
99  meter
 Z    =       16750743
73                 Z    =         5105626
69
 XDOT =      19183
760467                 XDOT =        5847
210190
 YDOT =     -13609
976843  feet/sec       YDOT =       -4148
320942  meter/sec
 ZDOT =       5473
674916                 ZDOT =        1668
376114


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   17160
12611751  
00016717  00000-0  10270-3 0  9028
2 25544  51
6418  78
5109 0004946 251
6310 108
4305 15
54017123 20493


Satellite: ISS
Catalog Number: 25544
Epoch time:      17160
12611751   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:        78
5109  deg
Eccentricity:     
0004946     
Arg of perigee:   251
6310  deg
Mean anomaly:     108
4305  deg
Mean motion:   15
54017123  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2049
Checksum:              275


Coasting Arc #4 (Orbit 2063)
---------------------------------------

Vector Time (GMT): 2017/161/01:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4059392
01                 A    =         6777788
88  meter
 Y    =       -1007458
09  meter          E    =           
0010192
 Z    =       -5342077
62                 I    =           51
98085
 XDOT =       2090
701793                 Wp   =           98
80539
 YDOT =       7367
542558  meter/sec      RA   =           72
99894  deg
 ZDOT =        198
069139                 TA   =          173
08232
                                          MA   =          173
06825
                                          Ha   =            219
636  n
mi
                                          Hp   =            216
814

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13318215
27                 X    =         4096305
37
 Y    =       -3305308
70  feet           Y    =         -961856
05  meter
 Z    =      -17526501
39                 Z    =        -5322268
68
 XDOT =       6859
257851                 XDOT =        2007
198484
 YDOT =      24171
727551  feet/sec       YDOT =        7390
455277  meter/sec
 ZDOT =        649
833132                 ZDOT =         208
023450

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6618096
92                 X    =         2017195
94
 Y    =       12147679
36  feet           Y    =         3702612
67  meter
 Z    =      -17438831
78                 Z    =        -5315355
93
 XDOT =     -20743
855606                 XDOT =       -6322
727189
 YDOT =      12301
047927  feet/sec       YDOT =        3749
359408  meter/sec
 ZDOT =        692
454028                 ZDOT =         211
059988


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   17161
09072902  
00016717  00000-0  10270-3 0  9035
2 25544  51
6414  73
7038 0004918 256
4367 103
6238 15
53984110 20648


Satellite: ISS
Catalog Number: 25544
Epoch time:      17161
09072902   =   yrday
fracday
Element set:     903
Inclination:       51
6414  deg
RA of node:        73
7038  deg
Eccentricity:     
0004918     
Arg of perigee:   256
4367  deg
Mean anomaly:     103
6238  deg
Mean motion:   15
53984110  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2064
Checksum:              297


Coasting Arc #5 (Orbit 2079)
---------------------------------------

Vector Time (GMT): 2017/162/01:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4506535
03                 A    =         6779037
40  meter
 Y    =        -679925
01  meter          E    =           
0002593
 Z    =        5018988
74                 I    =           51
97571
 XDOT =      -1200
873568                 Wp   =            5
24767
 YDOT =      -7286
569883  meter/sec      RA   =           68
02495  deg
 ZDOT =      -2062
779036                 TA   =          104
73582
                                          MA   =          104
70709
                                          Ha   =            219
593  n
mi
                                          Hp   =            216
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14785219
90                 X    =        -4522976
89
 Y    =       -2230725
08  feet           Y    =         -730412
80  meter
 Z    =       16466498
48                 Z    =         4997057
24
 XDOT =      -3939
873911                 XDOT =       -1109
283964
 YDOT =     -23906
069171  feet/sec       YDOT =       -7299
486452  meter/sec
 ZDOT =      -6767
647757                 ZDOT =       -2068
391153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1893451
54                 X    =         -577124
03
 Y    =      -14938883
46  feet           Y    =        -4553371
68  meter
 Z    =       16369759
82                 Z    =         4989502
79
 XDOT =      20864
668676                 XDOT =        6359
551012
 YDOT =     -10095
473490  feet/sec       YDOT =       -3077
100320  meter/sec
 ZDOT =      -6791
092560                 ZDOT =       -2069
925012


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   17162
11964228  
00016717  00000-0  10270-3 0  9041
2 25544  51
6420  68
5761 0004895 261
3362  98
7236 15
54036081 20800


Satellite: ISS
Catalog Number: 25544
Epoch time:      17162
11964228   =   yrday
fracday
Element set:     904
Inclination:       51
6420  deg
RA of node:        68
5761  deg
Eccentricity:     
0004895     
Arg of perigee:   261
3362  deg
Mean anomaly:      98
7236  deg
Mean motion:   15
54036081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2080
Checksum:              305


Coasting Arc #6 (Orbit 2094)
---------------------------------------

Vector Time (GMT): 2017/163/01:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4829132
49                 A    =         6782225
90  meter
 Y    =        2237536
66  meter          E    =           
0004120
 Z    =       -4208193
15                 I    =           51
97211
 XDOT =        139
928596                 Wp   =          137
56190
 YDOT =       6697
657256  meter/sec      RA   =           63
05659  deg
 ZDOT =       3720
943563                 TA   =          170
49749
                                          MA   =          170
48969
                                          Ha   =            219
507  n
mi
                                          Hp   =            216
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15843610
54                 X    =         4824194
23
 Y    =        7340999
54  feet           Y    =         2291512
29  meter
 Z    =      -13806407
96                 Z    =        -4184746
34
 XDOT =        459
083321                 XDOT =          46
948686
 YDOT =      21973
941129  feet/sec       YDOT =        6698
701612  meter/sec
 ZDOT =      12207
820088                 ZDOT =        3721
398428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2444714
79                 X    =         -745149
07
 Y    =       17371559
68  feet           Y    =         5294851
39  meter
 Z    =      -13703264
34                 Z    =        -4176754
97
 XDOT =     -19669
803604                 XDOT =       -5995
356139
 YDOT =       6864
581197  feet/sec       YDOT =        2092
324349  meter/sec
 ZDOT =      12208
584238                 ZDOT =        3721
176476


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   17163
08424924  
00016717  00000-0  10270-3 0  9053
2 25544  51
6409  63
7691 0004591 264
5882  95
4747 15
54029594 20959


Satellite: ISS
Catalog Number: 25544
Epoch time:      17163
08424924   =   yrday
fracday
Element set:     905
Inclination:       51
6409  deg
RA of node:        63
7691  deg
Eccentricity:     
0004591     
Arg of perigee:   264
5882  deg
Mean anomaly:      95
4747  deg
Mean motion:   15
54029594  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2095
Checksum:              336


Coasting Arc #7 (Orbit 2110)
---------------------------------------

Vector Time (GMT): 2017/164/01:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4950812
80                 A    =         6785907
68  meter
 Y    =       -3559521
74  meter          E    =           
0008509
 Z    =        2968406
61                 I    =           51
96912
 XDOT =       1079
187015                 Wp   =          102
21875
 YDOT =      -5696
077460  meter/sec      RA   =           58
09633  deg
 ZDOT =      -5020
108797                 TA   =           44
02303
                                          MA   =           43
95530
                                          Ha   =            219
443  n
mi
                                          Hp   =            216
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16242824
14                 X    =        -4925060
39
 Y    =      -11678220
92  feet           Y    =        -3614741
49  meter
 Z    =        9738866
84                 Z    =         2944419
18
 XDOT =       3540
639812                 XDOT =        1167
187046
 YDOT =     -18687
918176  feet/sec       YDOT =       -5683
516537  meter/sec
 ZDOT =     -16470
173217                 ZDOT =       -5014
653482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6164260
90                 X    =         1878866
72
 Y    =      -19085377
92  feet           Y    =        -5817223
19  meter
 Z    =        9633584
20                 Z    =         2936316
46
 XDOT =      17521
790022                 XDOT =        5340
641599
 YDOT =      -2658
911834  feet/sec       YDOT =        -810
436327  meter/sec
 ZDOT =     -16445
011079                 ZDOT =       -5012
439377


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   17164
11315798  
00016717  00000-0  10270-3 0  9067
2 25544  51
6410  58
6409 0004797 270
0656  89
9947 15
54048135 21111


Satellite: ISS
Catalog Number: 25544
Epoch time:      17164
11315798   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:        58
6409  deg
Eccentricity:     
0004797     
Arg of perigee:   270
0656  deg
Mean anomaly:      89
9947  deg
Mean motion:   15
54048135  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2111
Checksum:              322


Coasting Arc #8 (Orbit 2125)
---------------------------------------

Vector Time (GMT): 2017/165/01:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4822663
78                 A    =         6788801
77  meter
 Y    =        4547161
92  meter          E    =           
0007156
 Z    =       -1446070
51                 I    =           51
96092
 XDOT =      -2396
076898                 Wp   =            4
35376
 YDOT =       4387
399601  meter/sec      RA   =           53
14370  deg
 ZDOT =       5814
031661                 TA   =          339
94404
                                          MA   =          339
97215
                                          Ha   =            219
533  n
mi
                                          Hp   =            216
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15822387
73                 X    =         4778482
08
 Y    =       14918510
24  feet           Y    =         4600845
36  meter
 Z    =       -4744325
82                 Z    =        -1422750
30
 XDOT =      -7861
144677                 XDOT =       -2473
201513
 YDOT =      14394
355647  feet/sec       YDOT =        4360
173095  meter/sec
 ZDOT =      19074
907023                 ZDOT =        5802
205509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9050038
04                 X    =        -2758451
60
 Y    =       19798118
71  feet           Y    =         6034466
58  meter
 Z    =       -4642180
09                 Z    =        -1414936
49
 XDOT =     -14752
363899                 XDOT =       -4496
520516
 YDOT =      -2290
315214  feet/sec       YDOT =        -698
088077  meter/sec
 ZDOT =      19021
845571                 ZDOT =        5797
858530


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   17165
07775873  
00016717  00000-0  10270-3 0  9078
2 25544  51
6414  53
8332 0004650 274
5213  85
5409 15
54017114 21267


Satellite: ISS
Catalog Number: 25544
Epoch time:      17165
07775873   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:        53
8332  deg
Eccentricity:     
0004650     
Arg of perigee:   274
5213  deg
Mean anomaly:      85
5409  deg
Mean motion:   15
54017114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2126
Checksum:              299


Coasting Arc #9 (Orbit 2130)
---------------------------------------

Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5025120
72                 A    =         6781131
21  meter
 Y    =         647883
79  meter          E    =           
0004970
 Z    =       -4511969
02                 I    =           51
92874
 XDOT =       2042
113178                 Wp   =          122
08923
 YDOT =       6643
071717  meter/sec      RA   =           51
57569  deg
 ZDOT =       3228
285152                 TA   =          180
26344
                                          MA   =          180
26371
                                          Ha   =            219
541  n
mi
                                          Hp   =            216
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16486616
52                 X    =         5039419
30
 Y    =        2125603
00  feet           Y    =          704158
59  meter
 Z    =      -14803047
96                 Z    =        -4487523
79
 XDOT =       6699
846383                 XDOT =        1951
995450
 YDOT =      21794
854714  feet/sec       YDOT =        6665
403745  meter/sec
 ZDOT =      10591
486720                 ZDOT =        3237
986994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13735438
25                 X    =         4186561
58
 Y    =       -9531306
60  feet           Y    =        -2905142
25  meter
 Z    =      -14695198
94                 Z    =        -4479096
64
 XDOT =      18828
409123                 XDOT =        5738
899101
 YDOT =      10739
601713  feet/sec       YDOT =        3273
430602  meter/sec
 ZDOT =      10633
084591                 ZDOT =        3240
964183


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   17165
39929216  
00016717  00000-0  10270-3 0  9086
2 25544  51
6410  52
2313 0004699 277
9274  82
1345 15
54024863 21319


Satellite: ISS
Catalog Number: 25544
Epoch time:      17165
39929216   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:        52
2313  deg
Eccentricity:     
0004699     
Arg of perigee:   277
9274  deg
Mean anomaly:      82
1345  deg
Mean motion:   15
54024863  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2131
Checksum:              309


Coasting Arc #10 (Orbit 2146)
---------------------------------------

Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5529290
46                 A    =         6784871
06  meter
 Y    =       -1983467
47  meter          E    =           
0007934
 Z    =        3389208
26                 I    =           51
92016
 XDOT =       -693
119713                 Wp   =           84
27353
 YDOT =      -6049
406827  meter/sec      RA   =           46
61013  deg
 ZDOT =      -4660
953596                 TA   =           56
31563
                                          MA   =           56
24000
                                          Ha   =            219
636  n
mi
                                          Hp   =            216
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18140716
73                 X    =        -5523162
92
 Y    =       -6507439
19  feet           Y    =        -2045265
83  meter
 Z    =       11119449
68                 Z    =         3362363
42
 XDOT =      -2274
014808                 XDOT =        -602
781578
 YDOT =     -19847
135259  feet/sec       YDOT =       -6056
652157  meter/sec
 ZDOT =     -15291
842508                 ZDOT =       -4664
101772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17751764
58                 X    =        -5410737
84
 Y    =        7676047
67  feet           Y    =         2339659
33  meter
 Z    =       11001257
92                 Z    =         3353183
41
 XDOT =     -14576
686055                 XDOT =       -4442
973910
 YDOT =     -11727
733123  feet/sec       YDOT =       -3574
613056  meter/sec
 ZDOT =     -15304
599786                 ZDOT =       -4664
842015


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   17166
42819554  
00016717  00000-0  10270-3 0  9095
2 25544  51
6409  47
1039 0004735 281
9479  78
1143 15
54022408 21479


Satellite: ISS
Catalog Number: 25544
Epoch time:      17166
42819554   =   yrday
fracday
Element set:     909
Inclination:       51
6409  deg
RA of node:        47
1039  deg
Eccentricity:     
0004735     
Arg of perigee:   281
9479  deg
Mean anomaly:      78
1143  deg
Mean motion:   15
54022408  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2147
Checksum:              318


Coasting Arc #11 (Orbit 2161)
---------------------------------------

Vector Time (GMT): 2017/167/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5733299
94                 A    =         6788081
72  meter
 Y    =        3062358
19  meter          E    =           
0006724
 Z    =       -1941847
81                 I    =           51
90838
 XDOT =       -846
113322                 Wp   =          357
84331
 YDOT =       5145
213779  meter/sec      RA   =           41
65151  deg
 ZDOT =       5621
936339                 TA   =          340
82847
                                          MA   =          340
85376
                                          Ha   =            219
696  n
mi
                                          Hp   =            216
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18810039
16                 X    =         5708062
27
 Y    =       10047106
93  feet           Y    =         3126330
91  meter
 Z    =       -6370891
77                 Z    =        -1914058
25
 XDOT =      -2775
962342                 XDOT =        -930
894148
 YDOT =      16880
622635  feet/sec       YDOT =        5135
277401  meter/sec
 ZDOT =      18444
673027                 ZDOT =        5617
620750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20536448
45                 X    =         6259509
49
 Y    =       -5878583
23  feet           Y    =        -1791792
17  meter
 Z    =       -6248738
86                 Z    =        -1904615
60
 XDOT =       9222
299325                 XDOT =        2810
956834
 YDOT =      12653
748836  feet/sec       YDOT =        3856
862645  meter/sec
 ZDOT =      18424
632027                 ZDOT =        5615
827842


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   17167
39279013  
00016717  00000-0  10270-3 0  9104
2 25544  51
6414  42
2959 0004832 285
2786  74
7833 15
54027708 21621


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
39279013   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:        42
2959  deg
Eccentricity:     
0004832     
Arg of perigee:   285
2786  deg
Mean anomaly:      74
7833  deg
Mean motion:   15
54027708  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2162
Checksum:              319


Coasting Arc #12 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2017/167/11:41:08
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5605984
98                 A    =         6789089
24  meter
 Y    =       -3614529
75  meter          E    =           
0009271
 Z    =        1237327
80                 I    =           51
91049
 XDOT =       1688
313520                 Wp   =          130
27575
 YDOT =      -4635
860304  meter/sec      RA   =           41
17262  deg
 ZDOT =      -5870
106903                 TA   =           36
32485
                                          MA   =           36
26195
                                          Ha   =            219
662  n
mi
                                          Hp   =            216
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18392339
16                 X    =        -5571160
03
 Y    =      -11858693
39  feet           Y    =        -3677025
07  meter
 Z    =        4059474
40                 Z    =         1210179
93
 XDOT =       5539
086352                 XDOT =        1768
541524
 YDOT =     -15209
515433  feet/sec       YDOT =       -4616
531311  meter/sec
 ZDOT =     -19258
880914                 ZDOT =       -5861
711174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15056787
00                 X    =        -4589308
68
 Y    =       15910800
89  feet           Y    =         4849612
11  meter
 Z    =        3940261
62                 Z    =         1200991
74
 XDOT =     -12742
692817                 XDOT =       -3883
972771
 YDOT =      -7279
412441  feet/sec       YDOT =       -2218
764912  meter/sec
 ZDOT =     -19220
916207                 ZDOT =       -5858
535260


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   17167
52140263  
00016717  00000-0  10270-3 0  9114
2 25544  51
6427  41
6562 0004767 284
6743  75
3881 15
54000906 21644


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
52140263   =   yrday
fracday
Element set:     911
Inclination:       51
6427  deg
RA of node:        41
6562  deg
Eccentricity:     
0004767     
Arg of perigee:   284
6743  deg
Mean anomaly:      75
3881  deg
Mean motion:   15
54000906  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2164
Checksum:              302


Coasting Arc #13 (Orbit 2166)
---------------------------------------

Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3172497
70                 A    =         6786557
40  meter
 Y    =       -5387883
53  meter          E    =           
0001805
 Z    =       -2635764
29                 I    =           51
89439
 XDOT =       5545
277851                 Wp   =          194
79620
 YDOT =       -699
526046  meter/sec      RA   =           40
20399  deg
 ZDOT =      -5245
466041                 TA   =           14
78518
                                          MA   =           14
77990
                                          Ha   =            219
591  n
mi
                                          Hp   =            216
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10408457
03                 X    =        -3099209
94
 Y    =      -17676783
23  feet           Y    =        -5422950
53  meter
 Z    =       -8647520
64                 Z    =        -2650997
78
 XDOT =      18193
168801                 XDOT =        5578
167891
 YDOT =      -2295
032960  feet/sec       YDOT =        -637
330614  meter/sec
 ZDOT =     -17209
534255                 ZDOT =       -5218
448983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         758271
36                 X    =          231121
11
 Y    =       20471430
08  feet           Y    =         6239691
89  meter
 Z    =       -8713772
49                 Z    =        -2655957
86
 XDOT =     -15721
282266                 XDOT =       -4791
846835
 YDOT =      -6690
898594  feet/sec       YDOT =       -2039
385892  meter/sec
 ZDOT =     -17090
077575                 ZDOT =       -5209
055645


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   17167
71431997  
00016717  00000-0  10270-3 0  9123
2 25544  51
6393  40
6891 0004654 284
4440  75
6196 15
54052859 21676


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
71431997   =   yrday
fracday
Element set:     912
Inclination:       51
6393  deg
RA of node:        40
6891  deg
Eccentricity:     
0004654     
Arg of perigee:   284
4440  deg
Mean anomaly:      75
6196  deg
Mean motion:   15
54052859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2167
Checksum:              333


Coasting Arc #14 (Orbit 2182)
---------------------------------------

Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1937177
07                 A    =         6782904
59  meter
 Y    =        5162208
41  meter          E    =           
0006389
 Z    =        3945574
42                 I    =           51
85647
 XDOT =      -6474
323059                 Wp   =           95
94178
 YDOT =       -674
603243  meter/sec      RA   =           35
23835  deg
 ZDOT =       4055
072812                 TA   =          311
78497
                                          MA   =          311
83955
                                          Ha   =            219
616  n
mi
                                          Hp   =            216
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6355567
80                 X    =         1860142
21
 Y    =       16936379
28  feet           Y    =         5183440
17  meter
 Z    =       12944797
98                 Z    =         3954797
99
 XDOT =     -21241
217386                 XDOT =       -6485
995889
 YDOT =      -2213
265233  feet/sec       YDOT =        -747
069127  meter/sec
 ZDOT =      13304
044660                 ZDOT =        4023
594061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2179033
35                 X    =          664169
36
 Y    =      -17929178
60  feet           Y    =        -5464813
64  meter
 Z    =       12984542
67                 Z    =         3957688
60
 XDOT =      16641
293144                 XDOT =        5072
266150
 YDOT =      11571
748293  feet/sec       YDOT =        3527
068880  meter/sec
 ZDOT =      13165
152386                 ZDOT =        4012
738447


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   17168
74321661  
00016717  00000-0  10270-3 0  9134
2 25544  51
6391  35
5600 0004657 285
8988  74
1651 15
54053056 21838


Satellite: ISS
Catalog Number: 25544
Epoch time:      17168
74321661   =   yrday
fracday
Element set:     913
Inclination:       51
6391  deg
RA of node:        35
5600  deg
Eccentricity:     
0004657     
Arg of perigee:   285
8988  deg
Mean anomaly:      74
1651  deg
Mean motion:   15
54053056  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2183
Checksum:              316


Coasting Arc #15 (Orbit 2197)
---------------------------------------

Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -456069
36                 A    =         6779506
53  meter
 Y    =       -4701356
98  meter          E    =           
0008753
 Z    =       -4871304
00                 I    =           51
81843
 XDOT =       7015
648370                 Wp   =           53
69496
 YDOT =       1861
568897  meter/sec      RA   =           30
26331  deg
 ZDOT =      -2451
467153                 TA   =          192
27316
                                          MA   =          192
29449
                                          Ha   =            219
793  n
mi
                                          Hp   =            216
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1496290
55                 X    =         -379801
11
 Y    =      -15424399
54  feet           Y    =        -4706030
19  meter
 Z    =      -15981968
50                 Z    =        -4873334
62
 XDOT =      23017
219063                 XDOT =        7006
218494
 YDOT =       6107
509504  feet/sec       YDOT =        1939
970123  meter/sec
 ZDOT =      -8042
871237                 ZDOT =       -2417
409844

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5576934
89                 X    =        -1699849
76
 Y    =       14449604
19  feet           Y    =         4404239
36  meter
 Z    =      -15990029
38                 Z    =        -4873760
96
 XDOT =     -16932
794018                 XDOT =       -5161
115617
 YDOT =     -15276
810269  feet/sec       YDOT =       -4656
371770  meter/sec
 ZDOT =      -7892
829298                 ZDOT =       -2405
734370


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   17169
70780700  
00016717  00000-0  10270-3 0  9145
2 25544  51
6396  30
7538 0004529 290
7697  69
2970 15
54048233 21986


Satellite: ISS
Catalog Number: 25544
Epoch time:      17169
70780700   =   yrday
fracday
Element set:     914
Inclination:       51
6396  deg
RA of node:        30
7538  deg
Eccentricity:     
0004529     
Arg of perigee:   290
7697  deg
Mean anomaly:      69
2970  deg
Mean motion:   15
54048233  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2198
Checksum:              335


Coasting Arc #16 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1163450
19                 A    =         6777754
65  meter
 Y    =        4064550
49  meter          E    =           
0001802
 Z    =        5298850
14                 I    =           51
78400
 XDOT =      -7102
489570                 Wp   =          296
18121
 YDOT =      -2824
392653  meter/sec      RA   =           25
27646  deg
 ZDOT =        607
953035                 TA   =          148
03230
                                          MA   =          148
02137
                                          Ha   =            219
993  n
mi
                                          Hp   =            216
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3817093
81                 X    =        -1234554
03
 Y    =       13335139
40  feet           Y    =         4051141
91  meter
 Z    =       17384678
95                 Z    =         5293026
11
 XDOT =     -23302
131136                 XDOT =       -7073
331760
 YDOT =      -9266
380095  feet/sec       YDOT =       -2903
654534  meter/sec
 ZDOT =       1994
596573                 ZDOT =         573
521581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9248526
61                 X    =         2818950
91
 Y    =      -10381802
71  feet           Y    =        -3164373
47  meter
 Z    =       17358172
09                 Z    =         5290770
85
 XDOT =      16369
502903                 XDOT =        4989
424485
 YDOT =      17659
096973  feet/sec       YDOT =        5382
492757  meter/sec
 ZDOT =       1843
100111                 ZDOT =         561
776914


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   17170
73670143  
00016717  00000-0  10270-3 0  9150
2 25544  51
6400  25
6244 0004641 294
6525  65
4144 15
54024789 22147


Satellite: ISS
Catalog Number: 25544
Epoch time:      17170
73670143   =   yrday
fracday
Element set:     915
Inclination:       51
6400  deg
RA of node:        25
6244  deg
Eccentricity:     
0004641     
Arg of perigee:   294
6525  deg
Mean anomaly:      65
4144  deg
Mean motion:   15
54024789  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2214
Checksum:              291


Coasting Arc #17 (Orbit 2228)
---------------------------------------

Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2790147
19                 A    =         6778158
58  meter
 Y    =       -3341357
79  meter          E    =           
0009704
 Z    =       -5203976
51                 I    =           51
75660
 XDOT =       6663
893031                 Wp   =           91
30047
 YDOT =       3551
242256  meter/sec      RA   =           20
28775  deg
 ZDOT =       1294
587457                 TA   =          191
11330
                                          MA   =          191
13475
                                          Ha   =            220
028  n
mi
                                          Hp   =            216
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9154026
20                 X    =         2852582
38
 Y    =      -10962459
94  feet           Y    =        -3309806
77  meter
 Z    =      -17073413
75                 Z    =        -5190271
44
 XDOT =      21863
166111                 XDOT =        6617
398298
 YDOT =      11651
057269  feet/sec       YDOT =        3625
502304  meter/sec
 ZDOT =       4247
334175                 ZDOT =        1326
846402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12955162
95                 X    =        -3948733
67
 Y    =        6182271
53  feet           Y    =         1884356
36  meter
 Z    =      -17012244
19                 Z    =        -5185332
03
 XDOT =     -14658
681890                 XDOT =       -4467
966240
 YDOT =     -18656
926046  feet/sec       YDOT =       -5686
631059  meter/sec
 ZDOT =       4389
084460                 ZDOT =        1337
792943


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   17171
70128606  
00016717  00000-0  10270-3 0  9161
2 25544  51
6409  20
8177 0004578 298
4106  61
6585 15
54055055 22297


Satellite: ISS
Catalog Number: 25544
Epoch time:      17171
70128606   =   yrday
fracday
Element set:     916
Inclination:       51
6409  deg
RA of node:        20
8177  deg
Eccentricity:     
0004578     
Arg of perigee:   298
4106  deg
Mean anomaly:      61
6585  deg
Mean motion:   15
54055055  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2229
Checksum:              312


Coasting Arc #18 (Orbit 2244)
---------------------------------------

Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4297646
39                 A    =         6780893
85  meter
 Y    =        2565170
43  meter          E    =           
0007165
 Z    =        4574405
39                 I    =           51
73381
 XDOT =      -5717
369067                 Wp   =           35
48986
 YDOT =      -4079
361469  meter/sec      RA   =           15
29967  deg
 ZDOT =      -3075
776897                 TA   =           85
27637
                                          MA   =           85
19454
                                          Ha   =            220
273  n
mi
                                          Hp   =            216
271

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14099889
72                 X    =        -4348231
81
 Y    =        8415913
48  feet           Y    =         2516827
76  meter
 Z    =       15007891
69                 Z    =         4553406
04
 XDOT =     -18757
772529                 XDOT =       -5656
386891
 YDOT =     -13383
731854  feet/sec       YDOT =       -4142
955565  meter/sec
 ZDOT =     -10091
131553                 ZDOT =       -3103
402823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16369329
64                 X    =         4989371
68
 Y    =       -2114030
30  feet           Y    =         -644356
44  meter
 Z    =       14914664
78                 Z    =         4545989
82
 XDOT =      11717
546805                 XDOT =        3571
508266
 YDOT =      18493
395848  feet/sec       YDOT =        5636
787055  meter/sec
 ZDOT =     -10212
311433                 ZDOT =       -3112
712525


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   17172
73017622  
00016717  00000-0  10270-3 0  9171
2 25544  51
6402  15
6889 0004517 302
0702  58
0012 15
54015687 22459


Satellite: ISS
Catalog Number: 25544
Epoch time:      17172
73017622   =   yrday
fracday
Element set:     917
Inclination:       51
6402  deg
RA of node:        15
6889  deg
Eccentricity:     
0004517     
Arg of perigee:   302
0702  deg
Mean anomaly:      58
0012  deg
Mean motion:   15
54015687  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2245
Checksum:              284
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