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

 
Date: January 6th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 25336 0914 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


008/21:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 212 4

015/23:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 8
000/00:00:00 000 0 0 0 0 212 0

Coasting Arc #1 (Orbit 3660)
---------------------------------------

Vector Time (GMT): 2017/006/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3800842
17                 A    =         6789674
83  meter
 Y    =       -5620750
86  meter          E    =           
0014876
 Z    =        -145347
22                 I    =           51
97062
 XDOT =       3846
478778                 Wp   =          108
13765
 YDOT =       2743
943268  meter/sec      RA   =          123
10723  deg
 ZDOT =      -6035
922462                 TA   =           73
42033
                                          MA   =           73
25700
                                          Ha   =            223
599  n
mi
                                          Hp   =            212
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12469954
62                 X    =         3864118
39
 Y    =      -18440783
65  feet           Y    =        -5577893
48  meter
 Z    =        -476860
95                 Z    =         -126730
34
 XDOT =      12619
681030                 XDOT =        3844
829050
 YDOT =       9002
438542  feet/sec       YDOT =        2786
948150  meter/sec
 ZDOT =     -19802
895215                 ZDOT =       -6017
241327

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22218135
50                 X    =         6772087
70
 Y    =        1410239
95  feet           Y    =          429841
14  meter
 Z    =        -394137
60                 Z    =         -120133
14
 XDOT =      -1198
147649                 XDOT =        -365
195403
 YDOT =      13930
787824  feet/sec       YDOT =        4246
104129  meter/sec
 ZDOT =     -19721
308182                 ZDOT =       -6011
054734


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   17006
57365116  
00016717  00000-0  10270-3 0  9005
2 25544  51
6418 123
9690 0007015  56
3626 303
8195 15
54006317 36615


Satellite: ISS
Catalog Number: 25544
Epoch time:      17006
57365116   =   yrday
fracday
Element set:     900
Inclination:       51
6418  deg
RA of node:       123
9690  deg
Eccentricity:     
0007015     
Arg of perigee:    56
3626  deg
Mean anomaly:     303
8195  deg
Mean motion:   15
54006317  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3661
Checksum:              294


Coasting Arc #2 (Orbit 3676)
---------------------------------------

Vector Time (GMT): 2017/007/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4238635
67                 A    =         6788357
90  meter
 Y    =        4983661
82  meter          E    =           
0021064
 Z    =        1771613
59                 I    =           51
98358
 XDOT =      -2722
520444                 Wp   =           63
14983
 YDOT =      -4357
265870  meter/sec      RA   =          118
16001  deg
 ZDOT =       5700
836118                 TA   =          316
22614
                                          MA   =          316
39294
                                          Ha   =            223
677  n
mi
                                          Hp   =            212
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13906285
00                 X    =        -4302654
90
 Y    =       16350596
53  feet           Y    =         4935904
51  meter
 Z    =        5812380
53                 Z    =         1750868
26
 XDOT =      -8932
153687                 XDOT =       -2701
286005
 YDOT =     -14295
491700  feet/sec       YDOT =       -4387
592464  meter/sec
 ZDOT =      18703
530572                 ZDOT =        5687
662276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21222934
70                 X    =        -6468750
50
 Y    =       -3372627
23  feet           Y    =        -1027976
78  meter
 Z    =        5720399
02                 Z    =         1743577
62
 XDOT =       7230
432325                 XDOT =        2203
835773
 YDOT =     -13630
732554  feet/sec       YDOT =       -4154
647283  meter/sec
 ZDOT =      18646
410446                 ZDOT =        5683
425904


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   17007
60255895  
00016717  00000-0  10270-3 0  9013
2 25544  51
6422 118
8414 0007140  59
2484 300
9371 15
54021756 36775


Satellite: ISS
Catalog Number: 25544
Epoch time:      17007
60255895   =   yrday
fracday
Element set:     901
Inclination:       51
6422  deg
RA of node:       118
8414  deg
Eccentricity:     
0007140     
Arg of perigee:    59
2484  deg
Mean anomaly:     300
9371  deg
Mean motion:   15
54021756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3677
Checksum:              302


Coasting Arc #3 (Orbit 3691)
---------------------------------------

Vector Time (GMT): 2017/008/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4470384
66                 A    =         6785166
58  meter
 Y    =       -3921793
35  meter          E    =           
0011122
 Z    =       -3279195
60                 I    =           51
98681
 XDOT =       1579
007529                 Wp   =           76
92040
 YDOT =       5779
066816  meter/sec      RA   =          113
20775  deg
 ZDOT =      -4770
091652                 TA   =          140
87794
                                          MA   =          140
79747
                                          Ha   =            223
643  n
mi
                                          Hp   =            212
550

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14666616
33                 X    =         4529835
68
 Y    =      -12866776
09  feet           Y    =        -3871469
88  meter
 Z    =      -10758515
74                 Z    =        -3257335
64
 XDOT =       5180
470896                 XDOT =        1537
437998
 YDOT =      18960
192967  feet/sec       YDOT =        5796
492223  meter/sec
 ZDOT =     -15649
906995                 ZDOT =       -4762
521887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18761881
69                 X    =         5718621
54
 Y    =        5543191
82  feet           Y    =         1689564
87  meter
 Z    =      -10661802
96                 Z    =        -3249717
54
 XDOT =     -12769
717964                 XDOT =       -3892
210035
 YDOT =      13253
149249  feet/sec       YDOT =        4039
559891  meter/sec
 ZDOT =     -15617
656977                 ZDOT =       -4760
261847


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   17008
56715417  
00016717  00000-0  10270-3 0  9021
2 25544  51
6416 114
0341 0007027  63
1231 297
0639 15
54021625 36928


Satellite: ISS
Catalog Number: 25544
Epoch time:      17008
56715417   =   yrday
fracday
Element set:     902
Inclination:       51
6416  deg
RA of node:       114
0341  deg
Eccentricity:     
0007027     
Arg of perigee:    63
1231  deg
Mean anomaly:     297
0639  deg
Mean motion:   15
54021625  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3692
Checksum:              283


Coasting Arc #4 (Orbit 3697)
---------------------------------------

Vector Time (GMT): 2017/008/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3463948
56                 A    =         6777893
94  meter
 Y    =       -2464281
30  meter          E    =           
0010798
 Z    =        5271640
24                 I    =           51
96580
 XDOT =       3432
856891                 Wp   =           60
62926
 YDOT =      -6803
080129  meter/sec      RA   =          111
36882  deg
 ZDOT =       -917
898338                 TA   =           38
14225
                                          MA   =           38
06588
                                          Ha   =            223
854  n
mi
                                          Hp   =            212
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11364660
64                 X    =        -3461741
99
 Y    =       -8084912
39  feet           Y    =        -2503005
54  meter
 Z    =       17295407
60                 Z    =         5254818
59
 XDOT =      11262
653842                 XDOT =        3513
134259
 YDOT =     -22319
816695  feet/sec       YDOT =       -6764
242690  meter/sec
 ZDOT =      -3011
477486                 ZDOT =        -901
028050

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10930263
34                 X    =        -3331544
26
 Y    =        8808329
18  feet           Y    =         2684778
74  meter
 Z    =       17221937
29                 Z    =         5249246
49
 XDOT =     -17709
893550                 XDOT =       -5397
975554
 YDOT =     -16193
124900  feet/sec       YDOT =       -4935
664470  meter/sec
 ZDOT =      -2936
175620                 ZDOT =        -894
946329


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   17008
95299118  
00016717  00000-0  10270-3 0  9030
2 25544  51
6401 112
1128 0007394  61
1525 299
0372 15
54030463 36987


Satellite: ISS
Catalog Number: 25544
Epoch time:      17008
95299118   =   yrday
fracday
Element set:     903
Inclination:       51
6401  deg
RA of node:       112
1128  deg
Eccentricity:     
0007394     
Arg of perigee:    61
1525  deg
Mean anomaly:     299
0372  deg
Mean motion:   15
54030463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3698
Checksum:              301


Coasting Arc #5 (Orbit 3712)
---------------------------------------

Vector Time (GMT): 2017/009/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2715303
21                 A    =         6780038
12  meter
 Y    =        3993218
24  meter          E    =           
0017151
 Z    =       -4774150
95                 I    =           51
98459
 XDOT =      -3971
857935                 Wp   =           91
22416
 YDOT =       5950
036225  meter/sec      RA   =          106
39559  deg
 ZDOT =       2725
842203                 TA   =          205
60138
                                          MA   =          205
68640
                                          Ha   =            223
766  n
mi
                                          Hp   =            212
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8908475
08                 X    =         2693638
65
 Y    =       13101109
73  feet           Y    =         4023461
87  meter
 Z    =      -15663224
89                 Z    =        -4761013
14
 XDOT =     -13031
029971                 XDOT =       -4051
338361
 YDOT =      19521
116224  feet/sec       YDOT =        5905
175601  meter/sec
 ZDOT =       8943
051848                 ZDOT =        2706
355642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14984594
12                 X    =         4567304
29
 Y    =       -5314587
12  feet           Y    =        -1619886
16  meter
 Z    =      -15606207
77                 Z    =        -4756772
13
 XDOT =      15083
866418                 XDOT =        4597
562484
 YDOT =      16600
801232  feet/sec       YDOT =        5059
924216  meter/sec
 ZDOT =       8856
383697                 ZDOT =        2699
425751


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   17009
91757564  
00016717  00000-0  10270-3 0  9042
2 25544  51
6408 107
3051 0007400  63
9375 296
2538 15
54034349 37134


Satellite: ISS
Catalog Number: 25544
Epoch time:      17009
91757564   =   yrday
fracday
Element set:     904
Inclination:       51
6408  deg
RA of node:       107
3051  deg
Eccentricity:     
0007400     
Arg of perigee:    63
9375  deg
Mean anomaly:     296
2538  deg
Mean motion:   15
54034349  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3713
Checksum:              310


Coasting Arc #6 (Orbit 3728)
---------------------------------------

Vector Time (GMT): 2017/010/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1917967
83                 A    =         6783572
79  meter
 Y    =       -5306626
27  meter          E    =           
0018931
 Z    =        3753044
54                 I    =           52
00515
 XDOT =       4359
091473                 Wp   =           77
39712
 YDOT =      -4628
967734  meter/sec      RA   =          101
43130  deg
 ZDOT =      -4295
245533                 TA   =           57
95492
                                          MA   =           57
77118
                                          Ha   =            223
805  n
mi
                                          Hp   =            212
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6292545
36                 X    =        -1876715
55
 Y    =      -17410191
17  feet           Y    =        -5327843
97  meter
 Z    =       12313138
27                 Z    =         3743827
41
 XDOT =      14301
481211                 XDOT =        4431
393864
 YDOT =     -15186
902015  feet/sec       YDOT =       -4579
816776  meter/sec
 ZDOT =     -14092
012902                 ZDOT =       -4273
895374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18433806
02                 X    =        -5618624
08
 Y    =        1969306
19  feet           Y    =          600244
53  meter
 Z    =       12273584
91                 Z    =         3740988
68
 XDOT =     -11109
394254                 XDOT =       -3386
143369
 YDOT =     -16296
726691  feet/sec       YDOT =       -4967
242296  meter/sec
 ZDOT =     -13997
371634                 ZDOT =       -4266
398874


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   17010
94645914  
00016717  00000-0  10270-3 0  9053
2 25544  51
6410 102
1772 0007500  67
1267 293
0676 15
54066023 37296


Satellite: ISS
Catalog Number: 25544
Epoch time:      17010
94645914   =   yrday
fracday
Element set:     905
Inclination:       51
6410  deg
RA of node:       102
1772  deg
Eccentricity:     
0007500     
Arg of perigee:    67
1267  deg
Mean anomaly:     293
0676  deg
Mean motion:   15
54066023  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3729
Checksum:              293


Coasting Arc #7 (Orbit 3743)
---------------------------------------

Vector Time (GMT): 2017/011/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1178823
96                 A    =         6787104
28  meter
 Y    =        6237043
39  meter          E    =           
0012736
 Z    =       -2401768
47                 I    =           52
02241
 XDOT =      -4577
015945                 Wp   =           60
48570
 YDOT =       2934
489486  meter/sec      RA   =           96
47784  deg
 ZDOT =       5401
519063                 TA   =          272
83718
                                          MA   =          272
98293
                                          Ha   =            223
793  n
mi
                                          Hp   =            212
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3867532
67                 X    =         1120658
59
 Y    =       20462740
79  feet           Y    =         6249900
78  meter
 Z    =       -7879817
80                 Z    =        -2396182
89
 XDOT =     -15016
456514                 XDOT =       -4635
727603
 YDOT =       9627
590176  feet/sec       YDOT =        2882
977460  meter/sec
 ZDOT =      17721
519235                 ZDOT =        5379
143263

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20818794
07                 X    =         6345568
43
 Y    =         792443
28  feet           Y    =          241536
71  meter
 Z    =       -7856395
16                 Z    =        -2394629
25
 XDOT =       6030
121193                 XDOT =        1837
980940
 YDOT =      15393
693406  feet/sec       YDOT =        4691
997750  meter/sec
 ZDOT =      17622
659505                 ZDOT =        5371
386617


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   17011
91103169  
00016717  00000-0  10270-3 0  9063
2 25544  51
6410  97
3703 0007426  70
8183 289
3773 15
54055437 37440


Satellite: ISS
Catalog Number: 25544
Epoch time:      17011
91103169   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:        97
3703  deg
Eccentricity:     
0007426     
Arg of perigee:    70
8183  deg
Mean anomaly:     289
3773  deg
Mean motion:   15
54055437  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3744
Checksum:              307


Coasting Arc #8 (Orbit 3759)
---------------------------------------

Vector Time (GMT): 2017/012/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -400174
61                 A    =         6789258
58  meter
 Y    =       -6730822
96  meter          E    =           
0018753
 Z    =         743212
07                 I    =           52
03370
 XDOT =       4698
059637                 Wp   =          108
58079
 YDOT =       -953
210622  meter/sec      RA   =           91
53179  deg
 ZDOT =      -5985
733726                 TA   =           63
43090
                                          MA   =           63
23882
                                          Ha   =            223
788  n
mi
                                          Hp   =            212
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1312908
83                 X    =         -328489
17
 Y    =      -22082752
51  feet           Y    =        -6734897
22  meter
 Z    =        2438359
82                 Z    =          741441
80
 XDOT =      15413
581486                 XDOT =        4737
444796
 YDOT =      -3127
331436  feet/sec       YDOT =        -900
453102  meter/sec
 ZDOT =     -19638
234009                 ZDOT =       -5962
816792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21874180
27                 X    =        -6667250
15
 Y    =       -3305128
16  feet           Y    =        -1007403
06  meter
 Z    =        2431800
13                 Z    =          741212
68
 XDOT =        -60
762756                 XDOT =         -18
520488
 YDOT =     -14256
680793  feet/sec       YDOT =       -4345
436306  meter/sec
 ZDOT =     -19537
343483                 ZDOT =       -5954
982294


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   17012
93990107  
00016717  00000-0  10270-3 0  9073
2 25544  51
6423  92
2416 0007462  74
3456 285
8520 15
54073372 37608


Satellite: ISS
Catalog Number: 25544
Epoch time:      17012
93990107   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:        92
2416  deg
Eccentricity:     
0007462     
Arg of perigee:    74
3456  deg
Mean anomaly:     285
8520  deg
Mean motion:   15
54073372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3760
Checksum:              305


Coasting Arc #9 (Orbit 3775)
---------------------------------------

Vector Time (GMT): 2017/013/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -327629
59                 A    =         6789107
25  meter
 Y    =        6708482
87  meter          E    =           
0020654
 Z    =         930556
21                 I    =           52
03239
 XDOT =      -4718
437576                 Wp   =           62
95036
 YDOT =      -1069
121141  meter/sec      RA   =           86
58906  deg
 ZDOT =       5954
143557                 TA   =          307
07475
                                          MA   =          307
26341
                                          Ha   =            223
821  n
mi
                                          Hp   =            212
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1074900
24                 X    =         -407141
33
 Y    =       22009458
24  feet           Y    =         6704374
47  meter
 Z    =        3053005
95                 Z    =          928771
94
 XDOT =     -15480
438240                 XDOT =       -4735
053472
 YDOT =      -3507
615292  feet/sec       YDOT =       -1121
979094  meter/sec
 ZDOT =      19534
591722                 ZDOT =        5931
182866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21391859
65                 X    =         6520238
82
 Y    =        5292945
76  feet           Y    =         1613289
87  meter
 Z    =        3043940
53                 Z    =          927793
07
 XDOT =      -6046
221570                 XDOT =       -1842
888335
 YDOT =      13085
873096  feet/sec       YDOT =        3988
574120  meter/sec
 ZDOT =      19433
870455                 ZDOT =        5923
443715


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   17013
96876279  
00016717  00000-0  10270-3 0  9081
2 25544  51
6415  87
1138 0007534  77
5391 282
6605 15
54081498 37760


Satellite: ISS
Catalog Number: 25544
Epoch time:      17013
96876279   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:        87
1138  deg
Eccentricity:     
0007534     
Arg of perigee:    77
5391  deg
Mean anomaly:     282
6605  deg
Mean motion:   15
54081498  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3776
Checksum:              345


Coasting Arc #10 (Orbit 3790)
---------------------------------------

Vector Time (GMT): 2017/014/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1123940
89                 A    =         6786608
07  meter
 Y    =       -6180407
12  meter          E    =           
0011601
 Z    =       -2575142
76                 I    =           52
02215
 XDOT =       4625
859816                 Wp   =          100
16033
 YDOT =       3038
963688  meter/sec      RA   =           81
64253  deg
 ZDOT =      -5296
811854                 TA   =          108
60343
                                          MA   =          108
47741
                                          Ha   =            223
775  n
mi
                                          Hp   =            212
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3687470
12                 X    =         1205476
81
 Y    =      -20276926
26  feet           Y    =        -6167382
50  meter
 Z    =       -8448631
09                 Z    =        -2569485
23
 XDOT =      15176
705433                 XDOT =        4617
262368
 YDOT =       9970
353308  feet/sec       YDOT =        3090
645233  meter/sec
 ZDOT =     -17377
991647                 ZDOT =       -5274
362087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19311670
70                 X    =        -5886197
23
 Y    =       -7228360
50  feet           Y    =        -2203204
28  meter
 Z    =       -8422631
47                 Z    =        -2567218
07
 XDOT =      11960
170694                 XDOT =        3645
460027
 YDOT =     -11903
755199  feet/sec       YDOT =       -3628
264585  meter/sec
 ZDOT =     -17279
874351                 ZDOT =       -5266
905702


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   17014
93331423  
00016717  00000-0  10270-3 0  9097
2 25544  51
6422  82
3061 0007477  81
1170 279
0828 15
54101952 37914


Satellite: ISS
Catalog Number: 25544
Epoch time:      17014
93331423   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:        82
3061  deg
Eccentricity:     
0007477     
Arg of perigee:    81
1170  deg
Mean anomaly:     279
0828  deg
Mean motion:   15
54101952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3791
Checksum:              295


Coasting Arc #11 (Orbit 3806)
---------------------------------------

Vector Time (GMT): 2017/015/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1900126
92                 A    =         6782971
06  meter
 Y    =        5202410
53  meter          E    =           
0018552
 Z    =        3900627
26                 I    =           52
00426
 XDOT =      -4427
935001                 Wp   =           93
14075
 YDOT =      -4722
612269  meter/sec      RA   =           76
68687  deg
 ZDOT =       4123
899889                 TA   =          313
80109
                                          MA   =          313
95437
                                          Ha   =            223
827  n
mi
                                          Hp   =            211
979

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6234012
21                 X    =        -1977107
41
 Y    =       17068276
03  feet           Y    =         5180731
59  meter
 Z    =       12797333
54                 Z    =         3891210
25
 XDOT =     -14527
345803                 XDOT =       -4394
827980
 YDOT =     -15494
134740  feet/sec       YDOT =       -4771
943325  meter/sec
 ZDOT =      13529
855278                 ZDOT =        4102
471113

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15858806
58                 X    =         4833764
25
 Y    =        8931369
72  feet           Y    =         2722281
49  meter
 Z    =       12754982
92                 Z    =         3887718
80
 XDOT =     -16953
675272                 XDOT =       -5167
480223
 YDOT =      10830
791380  feet/sec       YDOT =        3301
225213  meter/sec
 ZDOT =      13436
537635                 ZDOT =        4095
456671


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   17015
96216227  
00016717  00000-0  10270-3 0  9107
2 25544  51
6421  77
1776 0007478  84
8872 275
3134 15
54107510 38071


Satellite: ISS
Catalog Number: 25544
Epoch time:      17015
96216227   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        77
1776  deg
Eccentricity:     
0007478     
Arg of perigee:    84
8872  deg
Mean anomaly:     275
3134  deg
Mean motion:   15
54107510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3807
Checksum:              312


Coasting Arc #12 (Orbit 3807)
---------------------------------------

Vector Time (GMT): 2017/015/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3683534
09                 A    =         6785259
57  meter
 Y    =       -4746587
36  meter          E    =           
0020355
 Z    =        3134976
59                 I    =           52
01253
 XDOT =       2635
622691                 Wp   =           91
13055
 YDOT =      -5293
492559  meter/sec      RA   =           76
23364  deg
 ZDOT =      -4891
028578                 TA   =           52
92909
                                          MA   =           52
74315
                                          Ha   =            223
809  n
mi
                                          Hp   =            211
986

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12085085
60                 X    =        -3645410
68
 Y    =      -15572793
17  feet           Y    =        -4787565
97  meter
 Z    =       10285356
27                 Z    =         3117176
01
 XDOT =       8647
056072                 XDOT =        2718
377820
 YDOT =     -17367
101571  feet/sec       YDOT =       -5263
556525  meter/sec
 ZDOT =     -16046
681687                 ZDOT =       -4878
024777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10366348
23                 X    =        -3159662
94
 Y    =       16813253
12  feet           Y    =         5124679
55  meter
 Z    =       10207990
93                 Z    =         3111395
63
 XDOT =     -18102
736068                 XDOT =       -5517
713954
 YDOT =      -1400
102662  feet/sec       YDOT =        -426
751291  meter/sec
 ZDOT =     -15988
548278                 ZDOT =       -4873
309515


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   17016
02646438  
00016717  00000-0  10270-3 0  9117
2 25544  51
6433  76
8581 0007465  84
7021 275
4983 15
54116485 38080


Satellite: ISS
Catalog Number: 25544
Epoch time:      17016
02646438   =   yrday
fracday
Element set:     911
Inclination:       51
6433  deg
RA of node:        76
8581  deg
Eccentricity:     
0007465     
Arg of perigee:    84
7021  deg
Mean anomaly:     275
4983  deg
Mean motion:   15
54116485  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3808
Checksum:              321


Coasting Arc #13 (Orbit 3822)
---------------------------------------

Vector Time (GMT): 2017/016/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3281303
62                 A    =         6788193
41  meter
 Y    =        5711736
92  meter          E    =           
0013902
 Z    =       -1632493
13                 I    =           52
01391
 XDOT =      -3509
127904                 Wp   =           61
67194
 YDOT =       3648
466442  meter/sec      RA   =           71
28207  deg
 ZDOT =       5755
393050                 TA   =          280
55746
                                          MA   =          280
71404
                                          Ha   =            223
713  n
mi
                                          Hp   =            211
973

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10765431
81                 X    =         3225119
37
 Y    =       18739294
37  feet           Y    =         5748116
51  meter
 Z    =       -5355948
60                 Z    =        -1616690
32
 XDOT =     -11512
886823                 XDOT =       -3577
621671
 YDOT =      11970
034258  feet/sec       YDOT =        3608
842094  meter/sec
 ZDOT =      18882
523131                 ZDOT =        5738
180645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13517335
92                 X    =         4120083
99
 Y    =      -16883877
26  feet           Y    =        -5146205
79  meter
 Z    =       -5287549
46                 Z    =        -1611645
08
 XDOT =      14156
391291                 XDOT =        4314
868065
 YDOT =       5489
441765  feet/sec       YDOT =        1673
181850  meter/sec
 ZDOT =      18806
190296                 ZDOT =        5732
126802


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   17016
99100069  
00016717  00000-0  10270-3 0  9129
2 25544  51
6432  72
0495 0007387  87
7753 272
4245 15
54138003 38234


Satellite: ISS
Catalog Number: 25544
Epoch time:      17016
99100069   =   yrday
fracday
Element set:     912
Inclination:       51
6432  deg
RA of node:        72
0495  deg
Eccentricity:     
0007387     
Arg of perigee:    87
7753  deg
Mean anomaly:     272
4245  deg
Mean motion:   15
54138003  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3823
Checksum:              307


Coasting Arc #14 (Orbit 3838)
---------------------------------------

Vector Time (GMT): 2017/017/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2647640
19                 A    =         6789422
99  meter
 Y    =       -6244768
28  meter          E    =           
0018033
 Z    =        -104139
44                 I    =           52
00560
 XDOT =       4378
189983                 Wp   =          119
13222
 YDOT =      -1768
737290  meter/sec      RA   =           66
33700  deg
 ZDOT =      -6042
509375                 TA   =           61
98397
                                          MA   =           61
80166
                                          Ha   =            223
765  n
mi
                                          Hp   =            212
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8686483
56                 X    =        -2577106
95
 Y    =      -20488084
89  feet           Y    =        -6273981
60  meter
 Z    =        -341664
84                 Z    =         -116829
32
 XDOT =      14364
140364                 XDOT =        4426
994279
 YDOT =      -5802
943865  feet/sec       YDOT =       -1719
504614  meter/sec
 ZDOT =     -19824
505825                 ZDOT =       -6021
123169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15647374
42                 X    =        -4769319
72
 Y    =       15822009
86  feet           Y    =         4822548
60  meter
 Z    =        -396272
76                 Z    =         -120783
94
 XDOT =      -9725
542934                 XDOT =       -2964
345486
 YDOT =     -10056
059257  feet/sec       YDOT =       -3065
086862  meter/sec
 ZDOT =     -19730
175282                 ZDOT =       -6013
757426


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   17018
01983515  
00016717  00000-0  10270-3 0  9130
2 25544  51
6425  66
9210 0007407  92
9416 267
2584 15
54094061 38390


Satellite: ISS
Catalog Number: 25544
Epoch time:      17018
01983515   =   yrday
fracday
Element set:     913
Inclination:       51
6425  deg
RA of node:        66
9210  deg
Eccentricity:     
0007407     
Arg of perigee:    92
9416  deg
Mean anomaly:     267
2584  deg
Mean motion:   15
54094061  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3839
Checksum:              314


Coasting Arc #15 (Orbit 3854)
---------------------------------------

Vector Time (GMT): 2017/018/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1850668
08                 A    =         6787904
75  meter
 Y    =        6278473
43  meter          E    =           
0020553
 Z    =        1767757
14                 I    =           51
98745
 XDOT =      -5133
304918                 Wp   =           75
18963
 YDOT =       -105
997423  meter/sec      RA   =           61
38972  deg
 ZDOT =       5700
533645                 TA   =          304
13538
                                          MA   =          304
33016
                                          Ha   =            223
599  n
mi
                                          Hp   =            211
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6071745
67                 X    =         1771736
20
 Y    =       20598666
09  feet           Y    =         6298727
52  meter
 Z    =        5799728
15                 Z    =         1776555
27
 XDOT =     -16841
551568                 XDOT =       -5159
428262
 YDOT =       -347
760574  feet/sec       YDOT =        -163
547516  meter/sec
 ZDOT =      18702
538205                 ZDOT =        5675
534414

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16524573
02                 X    =         5036689
86
 Y    =      -13699394
60  feet           Y    =        -4175575
47  meter
 Z    =        5837213
47                 Z    =         1779182
66
 XDOT =       5401
904034                 XDOT =        1646
500350
 YDOT =      14507
574392  feet/sec       YDOT =        4421
908675  meter/sec
 ZDOT =      18592
680379                 ZDOT =        5667
048979


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   17019
04865983  
00016717  00000-0  10270-3 0  9143
2 25544  51
6427  61
7920 0007233  95
2850 264
9128 15
54158993 38559


Satellite: ISS
Catalog Number: 25544
Epoch time:      17019
04865983   =   yrday
fracday
Element set:     914
Inclination:       51
6427  deg
RA of node:        61
7920  deg
Eccentricity:     
0007233     
Arg of perigee:    95
2850  deg
Mean anomaly:     264
9128  deg
Mean motion:   15
54158993  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3855
Checksum:              336


Coasting Arc #16 (Orbit 3869)
---------------------------------------

Vector Time (GMT): 2017/019/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -788573
09                 A    =         6784629
97  meter
 Y    =       -5873993
37  meter          E    =           
0011879
 Z    =       -3310995
79                 I    =           51
95973
 XDOT =       5710
080911                 Wp   =           96
71832
 YDOT =       1896
709680  meter/sec      RA   =           56
43458  deg
 ZDOT =      -4740
796201                 TA   =          121
54344
                                          MA   =          121
42737
                                          Ha   =            223
598  n
mi
                                          Hp   =            212
034

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2587182
04                 X    =         -706746
89
 Y    =      -19271631
80  feet           Y    =        -5882354
21  meter
 Z    =      -10862847
08                 Z    =        -3314627
67
 XDOT =      18733
861258                 XDOT =        5711
475327
 YDOT =       6222
800789  feet/sec       YDOT =        1960
571451  meter/sec
 ZDOT =     -15553
793312                 ZDOT =       -4713
055211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16526146
43                 X    =        -5037169
43
 Y    =       10230007
91  feet           Y    =         3118106
41  meter
 Z    =      -10877691
49                 Z    =        -3315520
37
 XDOT =      -1341
079495                 XDOT =        -408
761030
 YDOT =     -18520
303857  feet/sec       YDOT =       -5644
988616  meter/sec
 ZDOT =     -15432
228631                 ZDOT =       -4703
743287


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   17020
01317768  
00016717  00000-0  10270-3 0  9156
2 25544  51
6423  56
9831 0007192  98
6229 261
5739 15
54142099 38701


Satellite: ISS
Catalog Number: 25544
Epoch time:      17020
01317768   =   yrday
fracday
Element set:     915
Inclination:       51
6423  deg
RA of node:        56
9831  deg
Eccentricity:     
0007192     
Arg of perigee:    98
6229  deg
Mean anomaly:     261
5739  deg
Mean motion:   15
54142099  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3870
Checksum:              321


Coasting Arc #17 (Orbit 3885)
---------------------------------------

Vector Time (GMT): 2017/020/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -410069
96                 A    =         6780883
21  meter
 Y    =        5086408
05  meter          E    =           
0016471
 Z    =        4454504
38                 I    =           51
92774
 XDOT =      -6028
650671                 Wp   =          106
35115
 YDOT =      -3402
090167  meter/sec      RA   =           51
46910  deg
 ZDOT =       3315
074668                 TA   =          310
30207
                                          MA   =          310
44590
                                          Ha   =            223
694  n
mi
                                          Hp   =            211
991

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1345373
87                 X    =         -488554
66
 Y    =       16687690
45  feet           Y    =         5081383
49  meter
 Z    =       14614515
67                 Z    =         4452321
82
 XDOT =     -19779
037634                 XDOT =       -6006
262461
 YDOT =     -11161
713146  feet/sec       YDOT =       -3469
381454  meter/sec
 ZDOT =      10876
229226                 ZDOT =        3285
843885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15703322
18                 X    =         4786372
60
 Y    =       -5831255
19  feet           Y    =        -1777366
58  meter
 Z    =       14603946
28                 Z    =         4451282
83
 XDOT =      -2030
825141                 XDOT =        -618
995503
 YDOT =      21570
093482  feet/sec       YDOT =        6574
564493  meter/sec
 ZDOT =      10748
411902                 ZDOT =        3276
115948


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   17021
04199117  
00016717  00000-0  10270-3 0  9167
2 25544  51
6416  51
8545 0007376 101
5324 258
6657 15
54137381 38864


Satellite: ISS
Catalog Number: 25544
Epoch time:      17021
04199117   =   yrday
fracday
Element set:     916
Inclination:       51
6416  deg
RA of node:        51
8545  deg
Eccentricity:     
0007376     
Arg of perigee:   101
5324  deg
Mean anomaly:     258
6657  deg
Mean motion:   15
54137381  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3886
Checksum:              315
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