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

 
Date: January 10th 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


013/12:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 7
000/00:00:00 000 0 0 0 0 212 3

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 1

Coasting Arc #1 (Orbit 3706)
---------------------------------------

Vector Time (GMT): 2017/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2334872
66                 A    =         6789586
77  meter
 Y    =       -6366609
97  meter          E    =           
0015552
 Z    =        -258960
92                 I    =           52
01434
 XDOT =       4357
369612                 Wp   =          111
43965
 YDOT =       1831
463151  meter/sec      RA   =          108
43104  deg
 ZDOT =      -6035
349035                 TA   =           71
33548
                                          MA   =           71
16670
                                          Ha   =            223
671  n
mi
                                          Hp   =            212
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7660343
39                 X    =         2407150
11
 Y    =      -20887827
98  feet           Y    =        -6340095
70  meter
 Z    =        -849609
33                 Z    =         -247443
80
 XDOT =      14295
832059                 XDOT =        4365
882643
 YDOT =       6008
737372  feet/sec       YDOT =        1880
238279  meter/sec
 ZDOT =     -19801
013894                 ZDOT =       -6014
161449

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22239184
76                 X    =         6778503
52
 Y    =         697199
57  feet           Y    =          212506
43  meter
 Z    =        -797889
88                 Z    =         -243196
84
 XDOT =      -1107
661362                 XDOT =        -337
615183
 YDOT =      13960
291376  feet/sec       YDOT =        4255
096811  meter/sec
 ZDOT =     -19708
249322                 ZDOT =       -6007
074393


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
53174972  
00016717  00000-0  10270-3 0  9002
2 25544  51
6428 109
2258 0007065  66
9496 293
2401 15
54030195 37074


Satellite: ISS
Catalog Number: 25544
Epoch time:      17009
53174972   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:       109
2258  deg
Eccentricity:     
0007065     
Arg of perigee:    66
9496  deg
Mean anomaly:     293
2401  deg
Mean motion:   15
54030195  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3707
Checksum:              310


Coasting Arc #2 (Orbit 3722)
---------------------------------------

Vector Time (GMT): 2017/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2910134
21                 A    =         6788104
10  meter
 Y    =        5824392
13  meter          E    =           
0021150
 Z    =        1884848
08                 I    =           52
01964
 XDOT =      -3660
589581                 Wp   =           67
56547
 YDOT =      -3673
329309  meter/sec      RA   =          103
48631  deg
 ZDOT =       5656
626099                 TA   =          313
09220
                                          MA   =          313
26899
                                          Ha   =            223
737  n
mi
                                          Hp   =            212
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9547684
42                 X    =        -2984203
40
 Y    =       19108898
06  feet           Y    =         5791434
73  meter
 Z    =        6183884
76                 Z    =         1870532
24
 XDOT =     -12009
808336                 XDOT =       -3646
718396
 YDOT =     -12051
605344  feet/sec       YDOT =       -3714
187442  meter/sec
 ZDOT =      18558
484576                 ZDOT =        5638
877521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21206423
42                 X    =        -6463717
86
 Y    =       -2717085
62  feet           Y    =         -828167
70  meter
 Z    =        6119946
48                 Z    =         1865359
69
 XDOT =       7153
873896                 XDOT =        2180
500764
 YDOT =     -13890
217097  feet/sec       YDOT =       -4233
738171  meter/sec
 ZDOT =      18481
152095                 ZDOT =        5633
055159


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
56064190  
00016717  00000-0  10270-3 0  9018
2 25544  51
6436 104
0983 0007200  69
4885 290
7040 15
54044827 37238


Satellite: ISS
Catalog Number: 25544
Epoch time:      17010
56064190   =   yrday
fracday
Element set:     901
Inclination:       51
6436  deg
RA of node:       104
0983  deg
Eccentricity:     
0007200     
Arg of perigee:    69
4885  deg
Mean anomaly:     290
7040  deg
Mean motion:   15
54044827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3723
Checksum:              290


Coasting Arc #3 (Orbit 3737)
---------------------------------------

Vector Time (GMT): 2017/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3391867
61                 A    =         6784813
57  meter
 Y    =       -4814810
84  meter          E    =           
0011716
 Z    =       -3380324
61                 I    =           52
01435
 XDOT =       2898
903907                 Wp   =           81
22279
 YDOT =       5321
254080  meter/sec      RA   =           98
53592  deg
 ZDOT =      -4682
681338                 TA   =          137
94374
                                          MA   =          137
85375
                                          Ha   =            223
716  n
mi
                                          Hp   =            212
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11128174
59                 X    =         3461875
78
 Y    =      -15796623
49  feet           Y    =        -4776488
95  meter
 Z    =      -11090303
84                 Z    =        -3363678
53
 XDOT =       9510
839589                 XDOT =        2861
930763
 YDOT =      17458
182676  feet/sec       YDOT =        5353
465272  meter/sec
 ZDOT =     -15363
127750                 ZDOT =       -4668
688814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18704597
66                 X    =         5701161
37
 Y    =        5014358
27  feet           Y    =         1528376
40  meter
 Z    =      -11016290
67                 Z    =        -3357765
40
 XDOT =     -12665
185590                 XDOT =       -3860
348568
 YDOT =      13712
436380  feet/sec       YDOT =        4179
550609  meter/sec
 ZDOT =     -15302
594740                 ZDOT =       -4664
230877


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
52522496  
00016717  00000-0  10270-3 0  9024
2 25544  51
6427  99
2915 0007115  73
5955 286
5980 15
54039102 37389


Satellite: ISS
Catalog Number: 25544
Epoch time:      17011
52522496   =   yrday
fracday
Element set:     902
Inclination:       51
6427  deg
RA of node:        99
2915  deg
Eccentricity:     
0007115     
Arg of perigee:    73
5955  deg
Mean anomaly:     286
5980  deg
Mean motion:   15
54039102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3738
Checksum:              317


Coasting Arc #4 (Orbit 3753)
---------------------------------------

Vector Time (GMT): 2017/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3727466
21                 A    =         6780995
41  meter
 Y    =        3440027
41  meter          E    =           
0015443
 Z    =        4488149
82                 I    =           52
00665
 XDOT =      -2145
934634                 Wp   =           96
08687
 YDOT =      -6605
311157  meter/sec      RA   =           93
57533  deg
 ZDOT =       3269
330086                 TA   =          321
14453
                                          MA   =          321
25545
                                          Ha   =            223
757  n
mi
                                          Hp   =            212
209

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12229219
86                 X    =        -3787457
36
 Y    =       11286179
18  feet           Y    =         3398008
59  meter
 Z    =       14724900
98                 Z    =         4469897
78
 XDOT =      -7040
467960                 XDOT =       -2087
793418
 YDOT =     -21670
968363  feet/sec       YDOT =       -6628
983619  meter/sec
 ZDOT =      10726
148576                 ZDOT =        3259
046635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14995236
74                 X    =        -4570548
16
 Y    =       -7378928
61  feet           Y    =        -2249097
44  meter
 Z    =       14644065
53                 Z    =         4463511
17
 XDOT =      17065
395982                 XDOT =        5201
532695
 YDOT =     -13406
827661  feet/sec       YDOT =       -4086
401071  meter/sec
 ZDOT =      10682
149892                 ZDOT =        3255
919287


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
55410618  
00016717  00000-0  10270-3 0  9031
2 25544  51
6435  94
1634 0007078  76
6081 283
5860 15
54081685 37547


Satellite: ISS
Catalog Number: 25544
Epoch time:      17012
55410618   =   yrday
fracday
Element set:     903
Inclination:       51
6435  deg
RA of node:        94
1634  deg
Eccentricity:     
0007078     
Arg of perigee:    76
6081  deg
Mean anomaly:     283
5860  deg
Mean motion:   15
54081685  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3754
Checksum:              312


Coasting Arc #5 (Orbit 3768)
---------------------------------------

Vector Time (GMT): 2017/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4009293
64                 A    =         6778344
26  meter
 Y    =       -1782306
10  meter          E    =           
0020853
 Z    =       -5185212
59                 I    =           51
99772
 XDOT =       1348
794324                 Wp   =           78
80041
 YDOT =       7382
665666  meter/sec      RA   =           88
60607  deg
 ZDOT =      -1495
876896                 TA   =          176
84285
                                          MA   =          176
82967
                                          Ha   =            223
725  n
mi
                                          Hp   =            212
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13153850
52                 X    =         4054112
63
 Y    =       -5847460
97  feet           Y    =        -1737220
57  meter
 Z    =      -17011852
32                 Z    =        -5165628
28
 XDOT =       4425
178229                 XDOT =        1273
405314
 YDOT =      24221
344048  feet/sec       YDOT =        7397
327357  meter/sec
 ZDOT =      -4907
732600                 ZDOT =       -1489
507646

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10444651
40                 X    =         3183529
75
 Y    =       10052759
74  feet           Y    =         3064081
17  meter
 Z    =      -16925453
66                 Z    =        -5158878
27
 XDOT =     -19985
219880                 XDOT =       -6091
495020
 YDOT =      12552
623654  feet/sec       YDOT =        3826
039690  meter/sec
 ZDOT =      -4881
082531                 ZDOT =       -1487
753956


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
51867920  
00016717  00000-0  10270-3 0  9041
2 25544  51
6428  89
3564 0007131  79
1012 281
0943 15
54042778 37690


Satellite: ISS
Catalog Number: 25544
Epoch time:      17013
51867920   =   yrday
fracday
Element set:     904
Inclination:       51
6428  deg
RA of node:        89
3564  deg
Eccentricity:     
0007131     
Arg of perigee:    79
1012  deg
Mean anomaly:     281
0943  deg
Mean motion:   15
54042778  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3769
Checksum:              315


Coasting Arc #6 (Orbit 3768)
---------------------------------------

Vector Time (GMT): 2017/013/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4179627
97                 A    =         6777680
91  meter
 Y    =         491356
81  meter          E    =           
0021723
 Z    =       -5331501
36                 I    =           51
99558
 XDOT =       -224
006815                 Wp   =           88
96294
 YDOT =       7630
615721  meter/sec      RA   =           88
57234  deg
 ZDOT =        529
878154                 TA   =          186
06542
                                          MA   =          186
09177
                                          Ha   =            223
728  n
mi
                                          Hp   =            212
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13712690
19                 X    =         4199720
21
 Y    =        1612063
04  feet           Y    =          538208
89  meter
 Z    =      -17491802
38                 Z    =        -5311149
56
 XDOT =       -734
930495                 XDOT =        -311
891520
 YDOT =      25034
828482  feet/sec       YDOT =        7627
619301  meter/sec
 ZDOT =       1738
445388                 ZDOT =         528
577027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4048567
23                 X    =         1234003
29
 Y    =       13317800
49  feet           Y    =         4059265
59  meter
 Z    =      -17402444
18                 Z    =        -5304264
99
 XDOT =     -22276
380859                 XDOT =       -6789
840886
 YDOT =       9024
632127  feet/sec       YDOT =        2750
707872  meter/sec
 ZDOT =       1731
338420                 ZDOT =         527
711950


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
51867900  
00016717  00000-0  10270-3 0  9050
2 25544  51
6428  89
3565 0007173  78
4663 281
7295 15
54050517 37698


Satellite: ISS
Catalog Number: 25544
Epoch time:      17013
51867900   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:        89
3565  deg
Eccentricity:     
0007173     
Arg of perigee:    78
4663  deg
Mean anomaly:     281
7295  deg
Mean motion:   15
54050517  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3769
Checksum:              332


Coasting Arc #7 (Orbit 3784)
---------------------------------------

Vector Time (GMT): 2017/014/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4101424
12                 A    =         6779304
24  meter
 Y    =       -2254269
61  meter          E    =           
0013762
 Z    =        4895155
61                 I    =           51
99971
 XDOT =       1081
265773                 Wp   =           70
77662
 YDOT =      -7208
875918  meter/sec      RA   =           83
59940  deg
 ZDOT =      -2403
919172                 TA   =           42
69514
                                          MA   =           42
58828
                                          Ha   =            223
769  n
mi
                                          Hp   =            212
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13456115
87                 X    =        -4099689
28
 Y    =       -7395897
68  feet           Y    =        -2300124
98  meter
 Z    =       16060221
83                 Z    =         4875236
68
 XDOT =       3547
459884                 XDOT =        1173
473758
 YDOT =     -23651
167711  feet/sec       YDOT =       -7196
268824  meter/sec
 ZDOT =      -7886
873924                 ZDOT =       -2398
443122

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1094936
20                 X    =          333736
55
 Y    =      -15406451
76  feet           Y    =        -4695886
50  meter
 Z    =       15973084
89                 Z    =         4868596
28
 XDOT =      21886
774283                 XDOT =        6671
088801
 YDOT =      -6628
989701  feet/sec       YDOT =       -2020
516061  meter/sec
 ZDOT =      -7861
486482                 ZDOT =       -2396
181080


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
54754988  
00016717  00000-0  10270-3 0  9066
2 25544  51
6426  84
2283 0007142  82
1498 278
0465 15
54109525 37851


Satellite: ISS
Catalog Number: 25544
Epoch time:      17014
54754988   =   yrday
fracday
Element set:     906
Inclination:       51
6426  deg
RA of node:        84
2283  deg
Eccentricity:     
0007142     
Arg of perigee:    82
1498  deg
Mean anomaly:     278
0465  deg
Mean motion:   15
54109525  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3785
Checksum:              331


Coasting Arc #8 (Orbit 3799)
---------------------------------------

Vector Time (GMT): 2017/015/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3952567
82                 A    =         6782703
50  meter
 Y    =        3805382
03  meter          E    =           
0013939
 Z    =       -4000728
00                 I    =           52
00553
 XDOT =      -1944
514064                 Wp   =           96
17269
 YDOT =       6225
918383  meter/sec      RA   =           78
63383  deg
 ZDOT =       4011
332348                 TA   =          215
44301
                                          MA   =          215
53571
                                          Ha   =            223
750  n
mi
                                          Hp   =            212
092

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12967742
18                 X    =         3929154
52
 Y    =       12484849
16  feet           Y    =         3849451
44  meter
 Z    =      -13125748
04                 Z    =        -3981584
82
 XDOT =      -6379
639319                 XDOT =       -2033
474104
 YDOT =      20426
241413  feet/sec       YDOT =        6203
676063  meter/sec
 ZDOT =      13160
539200                 ZDOT =        4001
670681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5640943
92                 X    =        -1719359
71
 Y    =       17158002
75  feet           Y    =         5229759
24  meter
 Z    =      -13042306
20                 Z    =        -3975294
93
 XDOT =     -19968
349394                 XDOT =       -6086
352895
 YDOT =       3379
283022  feet/sec       YDOT =        1030
005465  meter/sec
 ZDOT =      13116
927355                 ZDOT =        3998
039458


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
51211420  
00016717  00000-0  10270-3 0  9074
2 25544  51
6417  79
4210 0007375  86
2694 273
9301 15
54106947 38004


Satellite: ISS
Catalog Number: 25544
Epoch time:      17015
51211420   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:        79
4210  deg
Eccentricity:     
0007375     
Arg of perigee:    86
2694  deg
Mean anomaly:     273
9301  deg
Mean motion:   15
54106947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3800
Checksum:              292


Coasting Arc #9 (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    =       -3701974
10                 A    =         6785243
55  meter
 Y    =       -4709204
57  meter          E    =           
0020241
 Z    =        3169432
35                 I    =           52
01256
 XDOT =       2602
320244                 Wp   =           90
86120
 YDOT =      -5336
087348  meter/sec      RA   =           76
23468  deg
 ZDOT =      -4862
487574                 TA   =           52
74056
                                          MA   =           52
55612
                                          Ha   =            223
826  n
mi
                                          Hp   =            212
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12145584
33                 X    =        -3664434
71
 Y    =      -15450146
23  feet           Y    =        -4750392
65  meter
 Z    =       10398400
11                 Z    =         3151540
78
 XDOT =       8537
796077                 XDOT =        2685
415519
 YDOT =     -17506
848256  feet/sec       YDOT =       -5306
521823  meter/sec
 ZDOT =     -15953
043222                 ZDOT =       -4849
644717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10230045
95                 X    =        -3118118
01
 Y    =       16827945
84  feet           Y    =         5129157
89  meter
 Z    =       10320627
92                 Z    =         3145727
39
 XDOT =     -18194
404304                 XDOT =       -5545
654432
 YDOT =      -1258
395145  feet/sec       YDOT =        -383
558840  meter/sec
 ZDOT =     -15895
609374                 ZDOT =       -4844
981737


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
02654638  
00016717  00000-0  10270-3 0  9084
2 25544  51
6436  76
8589 0007396  84
9276 275
2721 15
54090600 38086


Satellite: ISS
Catalog Number: 25544
Epoch time:      17016
02654638   =   yrday
fracday
Element set:     908
Inclination:       51
6436  deg
RA of node:        76
8589  deg
Eccentricity:     
0007396     
Arg of perigee:    84
9276  deg
Mean anomaly:     275
2721  deg
Mean motion:   15
54090600  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3808
Checksum:              334


Coasting Arc #10 (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    =        3311276
81                 A    =         6788212
82  meter
 Y    =        5680222
31  meter          E    =           
0013695
 Z    =       -1681948
78                 I    =           52
01401
 XDOT =      -3472
908438                 Wp   =           61
98637
 YDOT =       3710
961447  meter/sec      RA   =           71
28308  deg
 ZDOT =       5737
114281                 TA   =          279
68639
                                          MA   =          279
84106
                                          Ha   =            223
735  n
mi
                                          Hp   =            212
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10863769
06                 X    =         3255682
96
 Y    =       18635899
97  feet           Y    =         5716940
38  meter
 Z    =       -5518204
67                 Z    =        -1665998
94
 XDOT =     -11394
056555                 XDOT =       -3542
014944
 YDOT =      12175
070365  feet/sec       YDOT =        3671
738703  meter/sec
 ZDOT =      18822
553414                 ZDOT =        5720
076327

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13384827
35                 X    =         4079695
37
 Y    =      -16938770
69  feet           Y    =        -5162937
31  meter
 Z    =       -5449153
41                 Z    =        -1660901
96
 XDOT =      14299
906152                 XDOT =        4358
611395
 YDOT =       5313
392419  feet/sec       YDOT =        1619
522009  meter/sec
 ZDOT =      18746
975760                 ZDOT =        5714
078212


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
99110030  
00016717  00000-0  10270-3 0  9094
2 25544  51
6435  72
0504 0007317  88
0117 272
1874 15
54107818 38234


Satellite: ISS
Catalog Number: 25544
Epoch time:      17016
99110030   =   yrday
fracday
Element set:     909
Inclination:       51
6435  deg
RA of node:        72
0504  deg
Eccentricity:     
0007317     
Arg of perigee:    88
0117  deg
Mean anomaly:     272
1874  deg
Mean motion:   15
54107818  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3823
Checksum:              292


Coasting Arc #11 (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    =       -2692703
83                 A    =         6789522
26  meter
 Y    =       -6226143
67  meter          E    =           
0018141
 Z    =         -41566
77                 I    =           52
00595
 XDOT =       4342
839902                 Wp   =          119
08722
 YDOT =      -1851
149941  meter/sec      RA   =           66
33808  deg
 ZDOT =      -6043
481762                 TA   =           61
35828
                                          MA   =           61
17596
                                          Ha   =            223
792  n
mi
                                          Hp   =            212
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8834330
14                 X    =        -2622679
45
 Y    =      -20426980
54  feet           Y    =        -6255863
77  meter
 Z    =        -136373
92                 Z    =          -54476
79
 XDOT =      14248
162407                 XDOT =        4392
573108
 YDOT =      -6073
326579  feet/sec       YDOT =       -1802
307380  meter/sec
 ZDOT =     -19827
696068                 ZDOT =       -6022
265015

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15534120
53                 X    =        -4734799
94
 Y    =       15936742
90  feet           Y    =         4857519
24  meter
 Z    =        -191952
91                 Z    =          -58507
25
 XDOT =      -9923
162426                 XDOT =       -3024
579907
 YDOT =      -9854
264778  feet/sec       YDOT =       -3003
579904  meter/sec
 ZDOT =     -19734
094941                 ZDOT =       -6014
952138


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
01995538  
00016717  00000-0  10270-3 0  9105
2 25544  51
6428  66
9221 0007342  93
2086 266
9907 15
54061653 38396


Satellite: ISS
Catalog Number: 25544
Epoch time:      17018
01995538   =   yrday
fracday
Element set:     910
Inclination:       51
6428  deg
RA of node:        66
9221  deg
Eccentricity:     
0007342     
Arg of perigee:    93
2086  deg
Mean anomaly:     266
9907  deg
Mean motion:   15
54061653  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3839
Checksum:              325


Coasting Arc #12 (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    =        1913091
26                 A    =         6788106
86  meter
 Y    =        6279332
04  meter          E    =           
0020425
 Z    =        1698011
09                 I    =           51
98813
 XDOT =      -5103
774341                 Wp   =           74
61940
 YDOT =         -7
919090  meter/sec      RA   =           61
39113  deg
 ZDOT =       5727
668887                 TA   =          303
91374
                                          MA   =          304
10780
                                          Ha   =            223
626  n
mi
                                          Hp   =            212
053

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6276546
14                 X    =         1834483
94
 Y    =       20601483
06  feet           Y    =         6300286
01  meter
 Z    =        5570902
51                 Z    =         1707113
23
 XDOT =     -16744
666474                 XDOT =       -5131
128426
 YDOT =        -25
981265  feet/sec       YDOT =         -65
145833  meter/sec
 ZDOT =      18791
564591                 ZDOT =        5702
810116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16445435
41                 X    =         5012568
71
 Y    =      -13889915
15  feet           Y    =        -4233646
14  meter
 Z    =        5609723
90                 Z    =         1709843
84
 XDOT =       5645
336827                 XDOT =        1720
698665
 YDOT =      14297
463034  feet/sec       YDOT =        4357
866733  meter/sec
 ZDOT =      18682
305607                 ZDOT =        5694
366749


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
04880249  
00016717  00000-0  10270-3 0  9112
2 25544  51
6430  61
7934 0007161  95
5839 264
6131 15
54124750 38553


Satellite: ISS
Catalog Number: 25544
Epoch time:      17019
04880249   =   yrday
fracday
Element set:     911
Inclination:       51
6430  deg
RA of node:        61
7934  deg
Eccentricity:     
0007161     
Arg of perigee:    95
5839  deg
Mean anomaly:     264
6131  deg
Mean motion:   15
54124750  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3855
Checksum:              309


Coasting Arc #13 (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    =        -869819
35                 A    =         6784928
86  meter
 Y    =       -5900363
81  meter          E    =           
0011724
 Z    =       -3242968
53                 I    =           51
96072
 XDOT =       5694
933556                 Wp   =           98
20915
 YDOT =       1789
905361  meter/sec      RA   =           56
43666  deg
 ZDOT =      -4800
523143                 TA   =          119
12971
                                          MA   =          119
01231
                                          Ha   =            223
630  n
mi
                                          Hp   =            212
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2853738
03                 X    =         -788022
68
 Y    =      -19358149
00  feet           Y    =        -5909633
37  meter
 Z    =      -10639660
53                 Z    =        -3246995
15
 XDOT =      18684
165209                 XDOT =        5697
813533
 YDOT =       5872
392917  feet/sec       YDOT =        1853
606050  meter/sec
 ZDOT =     -15749
747845                 ZDOT =       -4772
852125

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16494600
62                 X    =        -5027554
27
 Y    =       10509849
61  feet           Y    =         3203402
16  meter
 Z    =      -10656234
86                 Z    =        -3248020
38
 XDOT =      -1620
063579                 XDOT =        -493
795379
 YDOT =     -18334
168321  feet/sec       YDOT =       -5588
254504  meter/sec
 ZDOT =     -15628
470365                 ZDOT =       -4763
557767


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
01334319  
00016717  00000-0  10270-3 0  9124
2 25544  51
6426  56
9846 0007118  98
9052 261
2906 15
54103701 38705


Satellite: ISS
Catalog Number: 25544
Epoch time:      17020
01334319   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:        56
9846  deg
Eccentricity:     
0007118     
Arg of perigee:    98
9052  deg
Mean anomaly:     261
2906  deg
Mean motion:   15
54103701  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3870
Checksum:              293


Coasting Arc #14 (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    =        -311009
78                 A    =         6781207
19  meter
 Y    =        5141569
42  meter          E    =           
0016645
 Z    =        4399354
49                 I    =           51
92877
 XDOT =      -6036
031355                 Wp   =          105
83327
 YDOT =      -3294
527776  meter/sec      RA   =           51
47205  deg
 ZDOT =       3408
526810                 TA   =          309
75164
                                          MA   =          309
89817
                                          Ha   =            223
725  n
mi
                                          Hp   =            212
085

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1020373
28                 X    =         -389850
78
 Y    =       16868666
06  feet           Y    =         5137650
62  meter
 Z    =       14433577
74                 Z    =         4397652
28
 XDOT =     -19803
252478                 XDOT =       -6015
299329
 YDOT =     -10808
818163  feet/sec       YDOT =       -3361
910860  meter/sec
 ZDOT =      11182
830740                 ZDOT =        3379
256153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15727502
62                 X    =         4793742
80
 Y    =       -6203476
32  feet           Y    =        -1890819
58  meter
 Z    =       14425108
86                 Z    =         4396773
18
 XDOT =      -1727
706905                 XDOT =        -526
605065
 YDOT =      21441
172916  feet/sec       YDOT =        6535
269505  meter/sec
 ZDOT =      11054
817497                 ZDOT =        3369
508373


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
04218280  
00016717  00000-0  10270-3 0  9137
2 25544  51
6419  51
8563 0007295 101
7475 258
4496 15
54096887 38860


Satellite: ISS
Catalog Number: 25544
Epoch time:      17021
04218280   =   yrday
fracday
Element set:     913
Inclination:       51
6419  deg
RA of node:        51
8563  deg
Eccentricity:     
0007295     
Arg of perigee:   101
7475  deg
Mean anomaly:     258
4496  deg
Mean motion:   15
54096887  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3886
Checksum:              331


Coasting Arc #15 (Orbit 3900)
---------------------------------------

Vector Time (GMT): 2017/021/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1662227
79                 A    =         6778178
89  meter
 Y    =       -4109552
00  meter          E    =           
0020123
 Z    =       -5145154
28                 I    =           51
89728
 XDOT =       5999
617672                 Wp   =           87
31294
 YDOT =       4463
204595  meter/sec      RA   =           46
49552  deg
 ZDOT =      -1631
169298                 TA   =          166
99870
                                          MA   =          166
94674
                                          Ha   =            223
562  n
mi
                                          Hp   =            212
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5453503
26                 X    =         1733050
79
 Y    =      -13482782
14  feet           Y    =        -4090567
74  meter
 Z    =      -16880427
44                 Z    =        -5136907
82
 XDOT =      19683
785013                 XDOT =        5957
186430
 YDOT =      14643
059695  feet/sec       YDOT =        4530
059147  meter/sec
 ZDOT =      -5351
605307                 ZDOT =       -1602
128182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14553537
55                 X    =        -4435918
25
 Y    =         984759
64  feet           Y    =          300154
74  meter
 Z    =      -16843388
49                 Z    =        -5133864
81
 XDOT =       4466
231315                 XDOT =        1361
307305
 YDOT =     -23102
770943  feet/sec       YDOT =       -7041
724583  meter/sec
 ZDOT =      -5224
835177                 ZDOT =       -1592
529762


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   17022
00671321  
00016717  00000-0  10270-3 0  9144
2 25544  51
6412  47
0476 0007133 106
3567 253
8370 15
54135175 39019


Satellite: ISS
Catalog Number: 25544
Epoch time:      17022
00671321   =   yrday
fracday
Element set:     914
Inclination:       51
6412  deg
RA of node:        47
0476  deg
Eccentricity:     
0007133     
Arg of perigee:   106
3567  deg
Mean anomaly:     253
8370  deg
Mean motion:   15
54135175  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3901
Checksum:              277


Coasting Arc #16 (Orbit 3916)
---------------------------------------

Vector Time (GMT): 2017/022/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3015449
74                 A    =         6777391
35  meter
 Y    =        2907277
47  meter          E    =           
0009410
 Z    =        5319983
86                 I    =           51
87205
 XDOT =      -5587
047915                 Wp   =          100
61084
 YDOT =      -5255
502589  meter/sec      RA   =           41
51267  deg
 ZDOT =       -296
034022                 TA   =          352
19195
                                          MA   =          352
20659
                                          Ha   =            223
695  n
mi
                                          Hp   =            212
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9893207
80                 X    =        -3073577
21
 Y    =        9538311
91  feet           Y    =         2873231
51  meter
 Z    =       17454015
29                 Z    =         5305194
77
 XDOT =     -18330
209694                 XDOT =       -5526
426313
 YDOT =     -17242
462563  feet/sec       YDOT =       -5317
641757  meter/sec
 ZDOT =       -971
240231                 ZDOT =        -323
026864

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13064882
84                 X    =         3982176
29
 Y    =        4521968
51  feet           Y    =         1378296
00  meter
 Z    =       17388451
39                 Z    =         5299999
98
 XDOT =      -6598
393405                 XDOT =       -2011
190310
 YDOT =      23235
259614  feet/sec       YDOT =        7082
107130  meter/sec
 ZDOT =      -1088
845087                 ZDOT =        -331
879982


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   17023
03554204  
00016717  00000-0  10270-3 0  9159
2 25544  51
6417  41
9188 0007195 110
1085 250
0847 15
54122997 39176


Satellite: ISS
Catalog Number: 25544
Epoch time:      17023
03554204   =   yrday
fracday
Element set:     915
Inclination:       51
6417  deg
RA of node:        41
9188  deg
Eccentricity:     
0007195     
Arg of perigee:   110
1085  deg
Mean anomaly:     250
0847  deg
Mean motion:   15
54122997  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3917
Checksum:              299


Coasting Arc #17 (Orbit 3931)
---------------------------------------

Vector Time (GMT): 2017/023/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4316168
07                 A    =         6778942
94  meter
 Y    =       -1664422
32  meter          E    =           
0019545
 Z    =       -4973335
49                 I    =           51
85051
 XDOT =       4699
155389                 Wp   =          108
66334
 YDOT =       5627
310142  meter/sec      RA   =           36
52825  deg
 ZDOT =       2195
905186                 TA   =          182
73043
                                          MA   =          182
74111
                                          Ha   =            223
549  n
mi
                                          Hp   =            212
243

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14160656
40                 X    =         4358617
06
 Y    =       -5460703
14  feet           Y    =        -1615918
49  meter
 Z    =      -16316717
49                 Z    =        -4952266
06
 XDOT =      15417
176474                 XDOT =        4625
213588
 YDOT =      18462
303616  feet/sec       YDOT =        5679
445748  meter/sec
 ZDOT =       7204
413339                 ZDOT =        2218
552603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11566182
36                 X    =        -3525372
38
 Y    =       -9979512
50  feet           Y    =        -3041755
41  meter
 Z    =      -16223794
06                 Z    =        -4945012
43
 XDOT =       8256
734823                 XDOT =        2516
652774
 YDOT =     -21436
565083  feet/sec       YDOT =       -6533
865037  meter/sec
 ZDOT =       7302
839639                 ZDOT =        2225
905522


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   17024
00006343  
00016717  00000-0  10270-3 0  9164
2 25544  51
6397  37
1096 0007291 113
7566 246
4352 15
54149157 39322


Satellite: ISS
Catalog Number: 25544
Epoch time:      17024
00006343   =   yrday
fracday
Element set:     916
Inclination:       51
6397  deg
RA of node:        37
1096  deg
Eccentricity:     
0007291     
Arg of perigee:   113
7566  deg
Mean anomaly:     246
4352  deg
Mean motion:   15
54149157  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3932
Checksum:              300
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