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

 
Date: July 27th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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


209/15:41:12 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 3

209/22:00:48 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 4

212/23:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 212 1

216/02:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 4

219/05:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 3

221/12:26:03 848 -0 5 0 8 0 8
N/A 0 6 -0 0 222 8
000/00:02:03 697 0 0 -0 0 213 0

Coasting Arc #1 (Orbit 2785)
---------------------------------------

Vector Time (GMT): 2017/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -868076
90                 A    =         6777281
45  meter
 Y    =        4176186
38  meter          E    =           
0020755
 Z    =       -5284704
77                 I    =           51
47650
 XDOT =      -7274
222968                 Wp   =           81
41110
 YDOT =      -2296
414862  meter/sec      RA   =          201
22386  deg
 ZDOT =       -618
894159                 TA   =          182
65042
                                          MA   =          182
66144
                                          Ha   =            223
105  n
mi
                                          Hp   =            212
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2848021
34                 X    =         -889041
61
 Y    =       13701398
89  feet           Y    =         4166361
87  meter
 Z    =      -17338270
23                 Z    =        -5288972
35
 XDOT =     -23865
560918                 XDOT =       -7244
996995
 YDOT =      -7534
169494  feet/sec       YDOT =       -2377
596738  meter/sec
 ZDOT =      -2030
492647                 ZDOT =        -654
158452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12932618
05                 X    =         3941861
98
 Y    =       -5283143
99  feet           Y    =        -1610302
29  meter
 Z    =      -17357734
63                 Z    =        -5290637
51
 XDOT =       6500
123386                 XDOT =        1981
237608
 YDOT =      23104
067965  feet/sec       YDOT =        7042
119916  meter/sec
 ZDOT =      -2186
039888                 ZDOT =        -666
304958


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   17207
51724625  
00016717  00000-0  10270-3 0  9006
2 25544  51
6373 202
2739 0006226  71
9117 288
2714 15
54207307 27863


Satellite: ISS
Catalog Number: 25544
Epoch time:      17207
51724625   =   yrday
fracday
Element set:     900
Inclination:       51
6373  deg
RA of node:       202
2739  deg
Eccentricity:     
0006226     
Arg of perigee:    71
9117  deg
Mean anomaly:     288
2714  deg
Mean motion:   15
54207307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2786
Checksum:              303


Coasting Arc #2 (Orbit 2801)
---------------------------------------

Vector Time (GMT): 2017/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2617168
40                 A    =         6777625
52  meter
 Y    =       -3514706
67  meter          E    =           
0010296
 Z    =        5163053
02                 I    =           51
50829
 XDOT =       6879
098138                 Wp   =           66
89464
 YDOT =       3122
563315  meter/sec      RA   =          196
21276  deg
 ZDOT =      -1355
263904                 TA   =           36
17829
                                          MA   =           36
10869
                                          Ha   =            222
976  n
mi
                                          Hp   =            212
316

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8586510
51                 X    =         2631197
10
 Y    =      -11531189
87  feet           Y    =        -3485361
35  meter
 Z    =       16939150
32                 Z    =         5175800
23
 XDOT =      22569
219612                 XDOT =        6850
252643
 YDOT =      10244
630299  feet/sec       YDOT =        3199
328798  meter/sec
 ZDOT =      -4446
403883                 ZDOT =       -1321
917949

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14302427
14                 X    =        -4359379
79
 Y    =        -455823
44  feet           Y    =         -138934
98  meter
 Z    =       16996003
03                 Z    =         5180381
72
 XDOT =      -4387
666462                 XDOT =       -1337
360738
 YDOT =     -23383
397956  feet/sec       YDOT =       -7127
259697  meter/sec
 ZDOT =      -4299
435594                 ZDOT =       -1310
467969


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   17208
54601384  
00016717  00000-0  10270-3 0  9017
2 25544  51
6368 197
1444 0006160  74
2742 285
9089 15
54227558 28027


Satellite: ISS
Catalog Number: 25544
Epoch time:      17208
54601384   =   yrday
fracday
Element set:     901
Inclination:       51
6368  deg
RA of node:       197
1444  deg
Eccentricity:     
0006160     
Arg of perigee:    74
2742  deg
Mean anomaly:     285
9089  deg
Mean motion:   15
54227558  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2802
Checksum:              318


Coasting Arc #3 (Orbit 2816)
---------------------------------------

Vector Time (GMT): 2017/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4213437
21                 A    =         6780382
51  meter
 Y    =        2820628
94  meter          E    =           
0015390
 Z    =       -4515987
89                 I    =           51
54883
 XDOT =      -5886
836052                 Wp   =           98
09537
 YDOT =      -3731
742258  meter/sec      RA   =          191
20950  deg
 ZDOT =       3168
797435                 TA   =          203
77160
                                          MA   =          203
84276
                                          Ha   =            223
114  n
mi
                                          Hp   =            212
199

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13823612
90                 X    =        -4222728
92
 Y    =        9254031
95  feet           Y    =         2773459
51  meter
 Z    =      -14816233
23                 Z    =        -4536477
73
 XDOT =     -19313
766575                 XDOT =       -5860
061466
 YDOT =     -12243
248879  feet/sec       YDOT =       -3797
423188  meter/sec
 ZDOT =      10396
317044                 ZDOT =        3140
266377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15501641
52                 X    =         4724900
34
 Y    =        5807236
12  feet           Y    =         1770045
57  meter
 Z    =      -14907221
97                 Z    =        -4543721
26
 XDOT =       1703
464067                 XDOT =         519
215848
 YDOT =      21757
948237  feet/sec       YDOT =        6631
822623  meter/sec
 ZDOT =      10270
704636                 ZDOT =        3130
510773


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   17209
51048344  
00016717  00000-0  10270-3 0  9027
2 25544  51
6367 192
3365 0006212  77
3792 282
8055 15
54202531 28171


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
51048344   =   yrday
fracday
Element set:     902
Inclination:       51
6367  deg
RA of node:       192
3365  deg
Eccentricity:     
0006212     
Arg of perigee:    77
3792  deg
Mean anomaly:     282
8055  deg
Mean motion:   15
54202531  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2817
Checksum:              302


Coasting Arc #4 (Orbit 2819)
---------------------------------------

Vector Time (GMT): 2017/209/15:41:12
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -168752
50                 A    =         6777198
86  meter
 Y    =       -4271907
30  meter          E    =           
0008742
 Z    =        5251092
62                 I    =           51
54583
 XDOT =       7595
124570                 Wp   =           93
06785
 YDOT =        729
203901  meter/sec      RA   =          190
47367  deg
 ZDOT =        835
649288                 TA   =          348
93122
                                          MA   =          348
95044
                                          Ha   =            222
944  n
mi
                                          Hp   =            212
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -553649
93                 X    =         -146477
27
 Y    =      -14015443
91  feet           Y    =        -4273669
92  meter
 Z    =       17227994
15                 Z    =         5250326
94
 XDOT =      24918
387696                 XDOT =        7582
346814
 YDOT =       2392
401250  feet/sec       YDOT =         814
066291  meter/sec
 ZDOT =       2741
631521                 ZDOT =         872
512554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         894041
79                 X    =          272503
94
 Y    =       14001274
46  feet           Y    =         4267588
46  meter
 Z    =       17225213
54                 Z    =         5250245
09
 XDOT =     -23914
503379                 XDOT =       -7289
140630
 YDOT =      -2052
959998  feet/sec       YDOT =        -625
742207  meter/sec
 ZDOT =       2904
509962                 ZDOT =         885
294636


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   17209
70337644  
00016717  00000-0  10270-3 0  9033
2 25544  51
6390 191
3754 0005968  77
3790 282
8029 15
54266576 28207


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
70337644   =   yrday
fracday
Element set:     903
Inclination:       51
6390  deg
RA of node:       191
3754  deg
Eccentricity:     
0005968     
Arg of perigee:    77
3790  deg
Mean anomaly:     282
8029  deg
Mean motion:   15
54266576  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2820
Checksum:              334


Coasting Arc #5 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2017/209/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3735690
99                 A    =         6779625
95  meter
 Y    =       -3163294
55  meter          E    =           
0013619
 Z    =        4681586
34                 I    =           51
56061
 XDOT =       6334
813500                 Wp   =           70
33178
 YDOT =       3286
940622  meter/sec      RA   =          189
12718  deg
 ZDOT =      -2822
761807                 TA   =           47
73230
                                          MA   =           47
61689
                                          Ha   =            222
875  n
mi
                                          Hp   =            212
382

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12256204
05                 X    =         3748045
57
 Y    =      -10378262
97  feet           Y    =        -3121450
50  meter
 Z    =       15359535
25                 Z    =         4699762
93
 XDOT =      20783
508858                 XDOT =        6311
298677
 YDOT =      10783
925926  feet/sec       YDOT =        3357
649367  meter/sec
 ZDOT =      -9261
029549                 ZDOT =       -2792
046685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11608087
16                 X    =         3538144
97
 Y    =       10985725
70  feet           Y    =         3348449
19  meter
 Z    =       15440348
00                 Z    =         4706218
07
 XDOT =      -7709
566604                 XDOT =       -2349
875901
 YDOT =      21023
696840  feet/sec       YDOT =        6408
022797  meter/sec
 ZDOT =      -9125
691279                 ZDOT =       -2781
510702


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   17209
96056728  
00016717  00000-0  10270-3 0  9043
2 25544  51
6374 190
0905 0005866  79
1031 281
0782 15
54227568 28247


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
96056728   =   yrday
fracday
Element set:     904
Inclination:       51
6374  deg
RA of node:       190
0905  deg
Eccentricity:     
0005866     
Arg of perigee:    79
1031  deg
Mean anomaly:     281
0782  deg
Mean motion:   15
54227568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2824
Checksum:              324


Coasting Arc #6 (Orbit 2838)
---------------------------------------

Vector Time (GMT): 2017/210/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5144423
12                 A    =         6783290
85  meter
 Y    =        2521828
92  meter          E    =           
0011495
 Z    =       -3641879
63                 I    =           51
60497
 XDOT =      -4974
377118                 Wp   =           91
95227
 YDOT =      -3839
215846  meter/sec      RA   =          184
13259  deg
 ZDOT =       4379
784337                 TA   =          224
85364
                                          MA   =          224
94661
                                          Ha   =            222
996  n
mi
                                          Hp   =            212
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16878028
59                 X    =        -5154550
23
 Y    =        8273716
92  feet           Y    =         2464243
93  meter
 Z    =      -11948423
97                 Z    =        -3666893
95
 XDOT =     -16320
134903                 XDOT =       -4952
350931
 YDOT =     -12595
852513  feet/sec       YDOT =       -3894
719640  meter/sec
 ZDOT =      14369
371183                 ZDOT =        4355
674006

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10279228
98                 X    =        -3133108
99
 Y    =      -15652336
84  feet           Y    =        -4770832
27  meter
 Z    =      -12059389
67                 Z    =        -3675701
97
 XDOT =       9335
223842                 XDOT =        2845
376227
 YDOT =     -17090
831238  feet/sec       YDOT =       -5209
285361  meter/sec
 ZDOT =      14263
300400                 ZDOT =        4347
453962


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   17210
92503431  
00016717  00000-0  10270-3 0  9050
2 25544  51
6370 185
2808 0006019  83
5427 276
6411 15
54236691 28392


Satellite: ISS
Catalog Number: 25544
Epoch time:      17210
92503431   =   yrday
fracday
Element set:     905
Inclination:       51
6370  deg
RA of node:       185
2808  deg
Eccentricity:     
0006019     
Arg of perigee:    83
5427  deg
Mean anomaly:     276
6411  deg
Mean motion:   15
54236691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2839
Checksum:              306


Coasting Arc #7 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2017/211/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6169491
71                 A    =         6786876
81  meter
 Y    =       -1798851
82  meter          E    =           
0019425
 Z    =        2157955
00                 I    =           51
64960
 XDOT =       3189
300277                 Wp   =          102
48210
 YDOT =       4300
958974  meter/sec      RA   =          179
15188  deg
 ZDOT =      -5495
192615                 TA   =           53
56967
                                          MA   =           53
39074
                                          Ha   =            222
887  n
mi
                                          Hp   =            212
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20241114
53                 X    =         6178666
22
 Y    =       -5901744
83  feet           Y    =        -1729809
14  meter
 Z    =        7079904
84                 Z    =         2187946
46
 XDOT =      10463
583586                 XDOT =        3167
661518
 YDOT =      14110
757790  feet/sec       YDOT =        4336
503069  meter/sec
 ZDOT =     -18028
847162                 ZDOT =       -5479
752537

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8674950
78                 X    =         2644125
00
 Y    =       19167138
97  feet           Y    =         5842143
96  meter
 Z    =        7212792
44                 Z    =         2198459
14
 XDOT =     -11088
081024                 XDOT =       -3379
647096
 YDOT =      11822
982254  feet/sec       YDOT =        3603
644991  meter/sec
 ZDOT =     -17961
172214                 ZDOT =       -5474
565291


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   17211
95379458  
00016717  00000-0  10270-3 0  9065
2 25544  51
6368 180
1512 0005888  85
5379 274
6446 15
54268642 28551


Satellite: ISS
Catalog Number: 25544
Epoch time:      17211
95379458   =   yrday
fracday
Element set:     906
Inclination:       51
6368  deg
RA of node:       180
1512  deg
Eccentricity:     
0005888     
Arg of perigee:    85
5379  deg
Mean anomaly:     274
6446  deg
Mean motion:   15
54268642  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              350


Coasting Arc #8 (Orbit 2869)
---------------------------------------

Vector Time (GMT): 2017/212/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6680936
91                 A    =         6788886
55  meter
 Y    =        1072269
32  meter          E    =           
0015573
 Z    =        -492887
47                 I    =           51
68776
 XDOT =      -1175
496808                 Wp   =           59
45245
 YDOT =      -4638
418861  meter/sec      RA   =          174
18135  deg
 ZDOT =       5991
262502                 TA   =          295
23491
                                          MA   =          295
39625
                                          Ha   =            223
042  n
mi
                                          Hp   =            212
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21919084
34                 X    =        -6690036
58
 Y    =        3517943
97  feet           Y    =          997507
69  meter
 Z    =       -1617084
87                 Z    =         -525363
20
 XDOT =      -3856
616824                 XDOT =       -1152
643804
 YDOT =     -15217
909648  feet/sec       YDOT =       -4651
436526  meter/sec
 ZDOT =      19656
373037                 ZDOT =        5985
607667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6919181
18                 X    =        -2108966
42
 Y    =      -21082253
28  feet           Y    =        -6425870
80  meter
 Z    =       -1760874
76                 Z    =         -536714
63
 XDOT =      12862
845313                 XDOT =        3920
595251
 YDOT =      -5823
932220  feet/sec       YDOT =       -1775
134541  meter/sec
 ZDOT =      19632
017783                 ZDOT =        5983
839020


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   17212
91825970  
00016717  00000-0  10270-3 0  9078
2 25544  51
6360 175
3425 0006126  91
8840 268
3014 15
54237558 28701


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
91825970   =   yrday
fracday
Element set:     907
Inclination:       51
6360  deg
RA of node:       175
3425  deg
Eccentricity:     
0006126     
Arg of perigee:    91
8840  deg
Mean anomaly:     268
3014  deg
Mean motion:   15
54237558  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2870
Checksum:              313


Coasting Arc #9 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2655469
31                 A    =         6779409
47  meter
 Y    =        4062127
16  meter          E    =           
0017220
 Z    =       -4749968
94                 I    =           51
65936
 XDOT =      -7015
296188                 Wp   =          103
67875
 YDOT =      -1412
215539  meter/sec      RA   =          173
89677  deg
 ZDOT =       2718
504308                 TA   =          193
22051
                                          MA   =          193
26570
                                          Ha   =            223
091  n
mi
                                          Hp   =            212
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8712169
67                 X    =        -2677622
90
 Y    =       13327188
85  feet           Y    =         4032308
22  meter
 Z    =      -15583887
61                 Z    =        -4762921
93
 XDOT =     -23016
063610                 XDOT =       -7012
188088
 YDOT =      -4633
253082  feet/sec       YDOT =       -1490
648080  meter/sec
 ZDOT =       8918
977387                 ZDOT =        2684
433930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15819823
76                 X    =        -4821882
28
 Y    =       -1200900
03  feet           Y    =         -366034
33  meter
 Z    =      -15641752
82                 Z    =        -4767606
26
 XDOT =      -7036
534478                 XDOT =       -2144
735709
 YDOT =     -21331
505512  feet/sec       YDOT =       -6501
842880  meter/sec
 ZDOT =       8768
484664                 ZDOT =        2672
634126


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   17212
98255778  
00016717  00000-0  10270-3 0  9089
2 25544  51
6375 175
0218 0006201  93
3056 266
8806 15
54236209 28719


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
98255778   =   yrday
fracday
Element set:     908
Inclination:       51
6375  deg
RA of node:       175
0218  deg
Eccentricity:     
0006201     
Arg of perigee:    93
3056  deg
Mean anomaly:     266
8806  deg
Mean motion:   15
54236209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2871
Checksum:              322


Coasting Arc #10 (Orbit 2886)
---------------------------------------

Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4227268
45                 A    =         6783182
72  meter
 Y    =       -3797292
35  meter          E    =           
0017765
 Z    =        3689228
90                 I    =           51
70439
 XDOT =       5890
905378                 Wp   =           89
23407
 YDOT =       2331
183119  meter/sec      RA   =          168
90828  deg
 ZDOT =      -4332
331990                 TA   =           46
83115
                                          MA   =           46
68281
                                          Ha   =            223
030  n
mi
                                          Hp   =            212
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13868990
98                 X    =         4251496
29
 Y    =      -12458308
22  feet           Y    =        -3749884
88  meter
 Z    =       12103769
37                 Z    =         3709822
14
 XDOT =      19327
117381                 XDOT =        5885
443809
 YDOT =       7648
238579  feet/sec       YDOT =        2397
028906  meter/sec
 ZDOT =     -14213
687631                 ZDOT =       -4303
729193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17633653
89                 X    =         5374737
71
 Y    =        5863955
08  feet           Y    =         1787333
51  meter
 Z    =       12195403
59                 Z    =         3717159
02
 XDOT =       3338
857168                 XDOT =        1017
683665
 YDOT =      19381
236398  feet/sec       YDOT =        5907
400854  meter/sec
 ZDOT =     -14087
491564                 ZDOT =       -4293
867429


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   17214
01131638  
00016717  00000-0  10270-3 0  9094
2 25544  51
6376 169
8912 0006174  97
2662 262
9193 15
54224576 28874


Satellite: ISS
Catalog Number: 25544
Epoch time:      17214
01131638   =   yrday
fracday
Element set:     909
Inclination:       51
6376  deg
RA of node:       169
8912  deg
Eccentricity:     
0006174     
Arg of perigee:    97
2662  deg
Mean anomaly:     262
9193  deg
Mean motion:   15
54224576  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2887
Checksum:              332


Coasting Arc #11 (Orbit 2901)
---------------------------------------

Vector Time (GMT): 2017/214/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5405998
40                 A    =         6786725
78  meter
 Y    =        3419663
14  meter          E    =           
0010691
 Z    =       -2270634
43                 I    =           51
74945
 XDOT =      -4317
763160                 Wp   =           73
63737
 YDOT =      -3225
133658  meter/sec      RA   =          163
93434  deg
 ZDOT =       5446
892875                 TA   =          261
15084
                                          MA   =          261
27191
                                          Ha   =            223
050  n
mi
                                          Hp   =            212
191

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17736215
23                 X    =        -5432806
68
 Y    =       11219367
26  feet           Y    =         3359059
83  meter
 Z    =       -7449588
01                 Z    =        -2296959
73
 XDOT =     -14165
889633                 XDOT =       -4307
836015
 YDOT =     -10581
147171  feet/sec       YDOT =       -3273
362626  meter/sec
 ZDOT =      17870
383447                 ZDOT =        5425
942664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18642733
59                 X    =        -5682305
20
 Y    =       -9546717
03  feet           Y    =        -2909839
35  meter
 Z    =       -7566542
94                 Z    =        -2306282
29
 XDOT =       1171
482386                 XDOT =         357
067831
 YDOT =     -16316
320881  feet/sec       YDOT =       -4973
214604  meter/sec
 ZDOT =      17778
154232                 ZDOT =        5418
781410


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   17214
97577431  
00016717  00000-0  10270-3 0  9106
2 25544  51
6388 165
0831 0006224  99
8134 260
3721 15
54246201 29029


Satellite: ISS
Catalog Number: 25544
Epoch time:      17214
97577431   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:       165
0831  deg
Eccentricity:     
0006224     
Arg of perigee:    99
8134  deg
Mean anomaly:     260
3721  deg
Mean motion:   15
54246201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2902
Checksum:              299


Coasting Arc #12 (Orbit 2917)
---------------------------------------

Vector Time (GMT): 2017/215/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6140603
36                 A    =         6788826
73  meter
 Y    =       -2823933
36  meter          E    =           
0018841
 Z    =         549096
48                 I    =           51
78672
 XDOT =       2442
152004                 Wp   =          121
24499
 YDOT =       4117
226256  meter/sec      RA   =          158
97051  deg
 ZDOT =      -5994
382260                 TA   =           52
83967
                                          MA   =           52
66776
                                          Ha   =            223
035  n
mi
                                          Hp   =            212
248

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20146336
47                 X    =         6169057
74
 Y    =       -9264873
23  feet           Y    =        -2755105
90  meter
 Z    =        1801497
65                 Z    =          578994
19
 XDOT =       8012
309723                 XDOT =        2425
047978
 YDOT =      13507
960156  feet/sec       YDOT =        4144
440787  meter/sec
 ZDOT =     -19666
608465                 ZDOT =       -5982
560488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18415769
24                 X    =         5613126
46
 Y    =       12331929
42  feet           Y    =         3758772
09  meter
 Z    =        1934193
16                 Z    =          589542
08
 XDOT =      -6367
337421                 XDOT =       -1940
764446
 YDOT =      12653
185955  feet/sec       YDOT =        3856
691079  meter/sec
 ZDOT =     -19614
886444                 ZDOT =       -5978
617388


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   17216
00452833  
00016717  00000-0  10270-3 0  9111
2 25544  51
6380 159
9535 0006148 103
9616 256
2220 15
54251976 29181


Satellite: ISS
Catalog Number: 25544
Epoch time:      17216
00452833   =   yrday
fracday
Element set:     911
Inclination:       51
6380  deg
RA of node:       159
9535  deg
Eccentricity:     
0006148     
Arg of perigee:   103
9616  deg
Mean anomaly:     256
2220  deg
Mean motion:   15
54251976  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2918
Checksum:              306


Coasting Arc #13 (Orbit 2919)
---------------------------------------

Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         859529
44                 A    =         6777159
17  meter
 Y    =        4156263
18  meter          E    =           
0020600
 Z    =       -5301504
52                 I    =           51
75388
 XDOT =      -7257
452829                 Wp   =           97
58971
 YDOT =       2339
149511  meter/sec      RA   =          158
24266  deg
 ZDOT =        656
731658                 TA   =          178
68578
                                          MA   =          178
68036
                                          Ha   =            222
979  n
mi
                                          Hp   =            212
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2819978
49                 X    =          838740
89
 Y    =       13636034
06  feet           Y    =         4165759
11  meter
 Z    =      -17393387
55                 Z    =        -5297379
49
 XDOT =     -23810
540778                 XDOT =       -7286
260469
 YDOT =       7674
375036  feet/sec       YDOT =        2257
830629  meter/sec
 ZDOT =       2154
631424                 ZDOT =         621
407842

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1614087
68                 X    =          491973
92
 Y    =       13852885
38  feet           Y    =         4222359
46  meter
 Z    =      -17375727
94                 Z    =        -5296121
88
 XDOT =     -23439
637524                 XDOT =       -7144
401517
 YDOT =       5239
102174  feet/sec       YDOT =        1596
878343  meter/sec
 ZDOT =       1997
991952                 ZDOT =         608
987947


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   17216
13312155  
00016717  00000-0  10270-3 0  9128
2 25544  51
6399 159
3154 0005965 103
1679 257
0140 15
54240560 29209


Satellite: ISS
Catalog Number: 25544
Epoch time:      17216
13312155   =   yrday
fracday
Element set:     912
Inclination:       51
6399  deg
RA of node:       159
3154  deg
Eccentricity:     
0005965     
Arg of perigee:   103
1679  deg
Mean anomaly:     257
0140  deg
Mean motion:   15
54240560  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2920
Checksum:              291


Coasting Arc #14 (Orbit 2935)
---------------------------------------

Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         883899
88                 A    =         6778999
84  meter
 Y    =       -4685015
78  meter          E    =           
0012064
 Z    =        4809593
87                 I    =           51
79167
 XDOT =       7110
191116                 Wp   =           81
40241
 YDOT =      -1311
715427  meter/sec      RA   =          153
25259  deg
 ZDOT =      -2577
168375                 TA   =           33
93216
                                          MA   =           33
85505
                                          Ha   =            222
847  n
mi
                                          Hp   =            212
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2899934
00                 X    =          912861
01
 Y    =      -15370786
68  feet           Y    =        -4674969
75  meter
 Z    =       15779507
46                 Z    =         4813957
59
 XDOT =      23327
398675                 XDOT =        7136
849041
 YDOT =      -4303
528304  feet/sec       YDOT =       -1232
055239  meter/sec
 ZDOT =      -8455
276822                 ZDOT =       -2542
565153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3996936
68                 X    =         1218266
30
 Y    =      -15101793
56  feet           Y    =        -4603026
68  meter
 Z    =       15799490
01                 Z    =         4815684
56
 XDOT =      22547
172935                 XDOT =        6872
378311
 YDOT =      -2742
944731  feet/sec       YDOT =        -836
049554  meter/sec
 ZDOT =      -8301
950187                 ZDOT =       -2530
434417


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   17217
16187198  
00016717  00000-0  10270-3 0  9130
2 25544  51
6410 154
1858 0005864 106
7230 253
4559 15
54288586 29368


Satellite: ISS
Catalog Number: 25544
Epoch time:      17217
16187198   =   yrday
fracday
Element set:     913
Inclination:       51
6410  deg
RA of node:       154
1858  deg
Eccentricity:     
0005864     
Arg of perigee:   106
7230  deg
Mean anomaly:     253
4559  deg
Mean motion:   15
54288586  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2936
Checksum:              332


Coasting Arc #15 (Orbit 2950)
---------------------------------------

Vector Time (GMT): 2017/218/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2444844
11                 A    =         6782631
19  meter
 Y    =        5047999
56  meter          E    =           
0012289
 Z    =       -3826940
42                 I    =           51
83205
 XDOT =      -6402
679921                 Wp   =          107
40158
 YDOT =         77
300598  meter/sec      RA   =          148
27388  deg
 ZDOT =       4199
859138                 TA   =          206
80141
                                          MA   =          206
86496
                                          Ha   =            222
918  n
mi
                                          Hp   =            212
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8021142
10                 X    =        -2482521
42
 Y    =       16561678
36  feet           Y    =         5020449
17  meter
 Z    =      -12555578
81                 Z    =        -3838907
77
 XDOT =     -21006
167719                 XDOT =       -6423
468933
 YDOT =        253
610887  feet/sec       YDOT =           5
585048  meter/sec
 ZDOT =      13779
065412                 ZDOT =        4168
706994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8942312
06                 X    =        -2725616
72
 Y    =       16040940
48  feet           Y    =         4889278
66  meter
 Z    =      -12609272
52                 Z    =        -3843306
26
 XDOT =     -19901
966790                 XDOT =       -6066
119478
 YDOT =       -391
176389  feet/sec       YDOT =        -119
230563  meter/sec
 ZDOT =      13641
169536                 ZDOT =        4157
828475


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   17218
12632516  
00016717  00000-0  10270-3 0  9147
2 25544  51
6405 149
3779 0006074 109
5120 250
6689 15
54281645 29512


Satellite: ISS
Catalog Number: 25544
Epoch time:      17218
12632516   =   yrday
fracday
Element set:     914
Inclination:       51
6405  deg
RA of node:       149
3779  deg
Eccentricity:     
0006074     
Arg of perigee:   109
5120  deg
Mean anomaly:     250
6689  deg
Mean motion:   15
54281645  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2951
Checksum:              313


Coasting Arc #16 (Orbit 2966)
---------------------------------------

Vector Time (GMT): 2017/219/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3743560
34                 A    =         6786419
37  meter
 Y    =       -5122041
39  meter          E    =           
0019739
 Z    =        2382866
32                 I    =           51
87204
 XDOT =       5289
316009                 Wp   =          108
10533
 YDOT =       1340
978432  meter/sec      RA   =          143
30758  deg
 ZDOT =      -5396
609030                 TA   =           45
34444
                                          MA   =           45
18371
                                          Ha   =            222
854  n
mi
                                          Hp   =            212
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12282022
11                 X    =         3788983
57
 Y    =      -16804597
74  feet           Y    =        -5079924
45  meter
 Z    =        7817802
90                 Z    =         2401161
18
 XDOT =      17353
398980                 XDOT =        5300
141268
 YDOT =       4399
535537  feet/sec       YDOT =        1400
187850  meter/sec
 ZDOT =     -17705
410204                 ZDOT =       -5370
889363

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12963447
03                 X    =         3951258
66
 Y    =      -16245219
39  feet           Y    =        -4951542
87  meter
 Z    =        7899525
48                 Z    =         2407775
37
 XDOT =      16072
235536                 XDOT =        4898
817391
 YDOT =       4222
787417  feet/sec       YDOT =        1287
105605  meter/sec
 ZDOT =     -17591
748845                 ZDOT =       -5361
965048


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   17219
15507189  
00016717  00000-0  10270-3 0  9159
2 25544  51
6407 144
2490 0005990 111
8796 248
2994 15
54284957 29677


Satellite: ISS
Catalog Number: 25544
Epoch time:      17219
15507189   =   yrday
fracday
Element set:     915
Inclination:       51
6407  deg
RA of node:       144
2490  deg
Eccentricity:     
0005990     
Arg of perigee:   111
8796  deg
Mean anomaly:     248
2994  deg
Mean motion:   15
54284957  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2967
Checksum:              350


Coasting Arc #17 (Orbit 2968)
---------------------------------------

Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -145338
45                 A    =         6778783
68  meter
 Y    =       -4700603
81  meter          E    =           
0011765
 Z    =        4872502
20                 I    =           51
84878
 XDOT =       6746
574882                 Wp   =           84
01950
 YDOT =      -2736
473716  meter/sec      RA   =          142
70606  deg
 ZDOT =      -2432
466937                 TA   =           29
77811
                                          MA   =           29
71121
                                          Ha   =            222
990  n
mi
                                          Hp   =            212
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -476832
18                 X    =         -116431
99
 Y    =      -15421928
51  feet           Y    =        -4702067
59  meter
 Z    =       15985899
61                 Z    =         4871866
28
 XDOT =      22134
432026                 XDOT =        6788
488927
 YDOT =      -8977
932140  feet/sec       YDOT =       -2660
794506  meter/sec
 ZDOT =      -7980
534569                 ZDOT =       -2399
593115

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10620144
38                 X    =        -3237020
01
 Y    =      -11195721
17  feet           Y    =        -3412455
81  meter
 Z    =       15983760
35                 Z    =         4871850
16
 XDOT =       9914
579208                 XDOT =        3021
963743
 YDOT =     -20619
258878  feet/sec       YDOT =       -6284
750106  meter/sec
 ZDOT =      -7834
615516                 ZDOT =       -2387
990809


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   17219
28366508  
00016717  00000-0  10270-3 0  9162
2 25544  51
6397 143
6086 0006203 111
1124 249
0692 15
54282769 29690


Satellite: ISS
Catalog Number: 25544
Epoch time:      17219
28366508   =   yrday
fracday
Element set:     916
Inclination:       51
6397  deg
RA of node:       143
6086  deg
Eccentricity:     
0006203     
Arg of perigee:   111
1124  deg
Mean anomaly:     249
0692  deg
Mean motion:   15
54282769  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2969
Checksum:              326


Coasting Arc #18 (Orbit 2983)
---------------------------------------

Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1336072
62                 A    =         6782397
32  meter
 Y    =        5376674
94  meter          E    =           
0012694
 Z    =       -3926250
96                 I    =           51
88707
 XDOT =      -6319
168916                 Wp   =          110
61466
 YDOT =       1410
255724  meter/sec      RA   =          137
73038  deg
 ZDOT =       4087
920574                 TA   =          202
08741
                                          MA   =          202
14216
                                          Ha   =            222
939  n
mi
                                          Hp   =            212
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4383440
35                 X    =        -1377025
32
 Y    =       17640009
65  feet           Y    =         5361505
13  meter
 Z    =      -12881400
80                 Z    =        -3932840
47
 XDOT =     -20732
181482                 XDOT =       -6354
325817
 YDOT =       4626
823243  feet/sec       YDOT =        1339
393867  meter/sec
 ZDOT =      13411
812908                 ZDOT =        4057
139275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8695620
97                 X    =         2650425
27
 Y    =       15937321
48  feet           Y    =         4857695
59  meter
 Z    =      -12911349
13                 Z    =        -3935379
21
 XDOT =     -11117
511832                 XDOT =       -3388
617606
 YDOT =      16803
869348  feet/sec       YDOT =        5121
819377  meter/sec
 ZDOT =      13275
332207                 ZDOT =        4046
321257


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   17220
24811309  
00016717  00000-0  10270-3 0  9175
2 25544  51
6408 138
8007 0006106 114
4192 245
7598 15
54258442 29841


Satellite: ISS
Catalog Number: 25544
Epoch time:      17220
24811309   =   yrday
fracday
Element set:     917
Inclination:       51
6408  deg
RA of node:       138
8007  deg
Eccentricity:     
0006106     
Arg of perigee:   114
4192  deg
Mean anomaly:     245
7598  deg
Mean motion:   15
54258442  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2984
Checksum:              310


Coasting Arc #19 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2017/221/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2619202
05                 A    =         6786156
07  meter
 Y    =       -5724835
79  meter          E    =           
0019704
 Z    =        2507271
07                 I    =           51
92250
 XDOT =       5520
659654                 Wp   =          108
38322
 YDOT =        179
669101  meter/sec      RA   =          132
76608  deg
 ZDOT =      -5328
742372                 TA   =           43
58051
                                          MA   =           43
42502
                                          Ha   =            222
870  n
mi
                                          Hp   =            212
339

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8593182
59                 X    =         2670845
16
 Y    =      -18782269
65  feet           Y    =        -5695257
32  meter
 Z    =        8225954
94                 Z    =         2520119
56
 XDOT =      18112
400438                 XDOT =        5544
124147
 YDOT =        589
465554  feet/sec       YDOT =         241
536025  meter/sec
 ZDOT =     -17482
750564                 ZDOT =       -5301
868261

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6666289
71                 X    =        -2031885
10
 Y    =      -19524961
97  feet           Y    =        -5951208
41  meter
 Z    =        8283671
68                 Z    =         2524863
13
 XDOT =      12244
181637                 XDOT =        3732
026563
 YDOT =     -11586
117821  feet/sec       YDOT =       -3531
448712  meter/sec
 ZDOT =     -17363
786096                 ZDOT =       -5292
482002


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   17221
27685335  
00016717  00000-0  10270-3 0  9188
2 25544  51
6399 133
6710 0006119 116
7238 243
4541 15
54290986 30006


Satellite: ISS
Catalog Number: 25544
Epoch time:      17221
27685335   =   yrday
fracday
Element set:     918
Inclination:       51
6399  deg
RA of node:       133
6710  deg
Eccentricity:     
0006119     
Arg of perigee:   116
7238  deg
Mean anomaly:     243
4541  deg
Mean motion:   15
54290986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3000
Checksum:              308


Coasting Arc #20 (Orbit 3003)
---------------------------------------

Vector Time (GMT): 2017/221/12:27:05
697
Vector Time (MET): N/A
Weight (LBS)     : 902191
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2716787
47                 A    =         6777441
08  meter
 Y    =        3227625
43  meter          E    =           
0019671
 Z    =       -5321190
15                 I    =           51
90015
 XDOT =      -5365
123488                 Wp   =          101
38678
 YDOT =       5430
753602  meter/sec      RA   =          131
39666  deg
 ZDOT =        552
815591                 TA   =          173
89133
                                          MA   =          173
86731
                                          Ha   =            222
825  n
mi
                                          Hp   =            213
001

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8913344
72                 X    =         2706340
63
 Y    =       10589322
27  feet           Y    =         3257947
91  meter
 Z    =      -17457972
94                 Z    =        -5308018
51
 XDOT =     -17602
111180                 XDOT =       -5428
138122
 YDOT =      17817
433078  feet/sec       YDOT =        5370
404813  meter/sec
 ZDOT =       1813
699445                 ZDOT =         526
600866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1104050
83                 X    =         -336514
69
 Y    =      -13870083
65  feet           Y    =        -4227601
50  meter
 Z    =      -17400118
70                 Z    =        -5303556
18
 XDOT =      23704
130176                 XDOT =        7225
018878
 YDOT =      -4023
993292  feet/sec       YDOT =       -1226
513155  meter/sec
 ZDOT =       1696
840079                 ZDOT =         517
196856


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   17221
53403967  
00016717  00000-0  10270-3 0  9197
2 25544  51
6421 132
3896 0005361 120
8319 239
3361 15
54131571 30049


Satellite: ISS
Catalog Number: 25544
Epoch time:      17221
53403967   =   yrday
fracday
Element set:     919
Inclination:       51
6421  deg
RA of node:       132
3896  deg
Eccentricity:     
0005361     
Arg of perigee:   120
8319  deg
Mean anomaly:     239
3361  deg
Mean motion:   15
54131571  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3004
Checksum:              290
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