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

 
Date: December 5th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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


340/13:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 215 1

341/18:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 215 2

342/18:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 215 4

344/22:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 215 5

348/01:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 5

348/05:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 6

351/07:21:01 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 7

353/08:42:47 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 215 7

Coasting Arc #1 (Orbit 823)
---------------------------------------

Vector Time (GMT): 2017/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         740626
73                 A    =         6788930
92  meter
 Y    =       -6644976
48  meter          E    =           
0011371
 Z    =        1151109
69                 I    =           51
28152
 XDOT =       4724
433862                 Wp   =           67
48881
 YDOT =       1545
169511  meter/sec      RA   =          268
42643  deg
 ZDOT =       5838
010655                 TA   =          305
07103
                                          MA   =          305
17762
                                          Ha   =            221
049  n
mi
                                          Hp   =            215
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2429877
74                 X    =          809285
99
 Y    =      -21801103
94  feet           Y    =        -6636310
53  meter
 Z    =        3776606
61                 Z    =         1154873
46
 XDOT =      15500
111095                 XDOT =        4678
445631
 YDOT =       5069
453776  feet/sec       YDOT =        1597
743530  meter/sec
 ZDOT =      19153
578265                 ZDOT =        5860
849310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20087612
90                 X    =         6122704
41
 Y    =        8806006
68  feet           Y    =         2684070
84  meter
 Z    =        3794370
92                 Z    =         1156524
26
 XDOT =      -8788
909147                 XDOT =       -2678
859508
 YDOT =      11692
950779  feet/sec       YDOT =        3564
011397  meter/sec
 ZDOT =      19254
632739                 ZDOT =        5868
812059


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   17338
56206329  
00016717  00000-0  10270-3 0  9002
2 25544  51
6402 268
9807 0003151 199
7850 160
3181 15
54071038  8247


Satellite: ISS
Catalog Number: 25544
Epoch time:      17338
56206329   =   yrday
fracday
Element set:     900
Inclination:       51
6402  deg
RA of node:       268
9807  deg
Eccentricity:     
0003151     
Arg of perigee:   199
7850  deg
Mean anomaly:     160
3181  deg
Mean motion:   15
54071038  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             824
Checksum:              303


Coasting Arc #2 (Orbit 838)
---------------------------------------

Vector Time (GMT): 2017/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1517235
16                 A    =         6786244
09  meter
 Y    =        6018419
28  meter          E    =           
0006035
 Z    =       -2738831
25                 I    =           51
27573
 XDOT =      -4531
817886                 Wp   =          152
03017
 YDOT =      -3467
781674  meter/sec      RA   =          263
42761  deg
 ZDOT =      -5119
579459                 TA   =           59
13241
                                          MA   =           59
07306
                                          Ha   =            220
893  n
mi
                                          Hp   =            215
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4977805
66                 X    =        -1571117
97
 Y    =       19745470
08  feet           Y    =         6001151
57  meter
 Z    =       -8985666
83                 Z    =        -2746331
72
 XDOT =     -14868
168916                 XDOT =       -4467
834803
 YDOT =     -11377
236462  feet/sec       YDOT =       -3518
101190  meter/sec
 ZDOT =     -16796
520534                 ZDOT =       -5141
438817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17554280
58                 X    =        -5350544
72
 Y    =      -10290434
42  feet           Y    =        -3136524
41  meter
 Z    =       -9019896
84                 Z    =        -2749264
56
 XDOT =      14330
219745                 XDOT =        4367
850978
 YDOT =      -9666
652562  feet/sec       YDOT =       -2946
395701  meter/sec
 ZDOT =     -16892
937595                 ZDOT =       -5148
967379


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   17339
52662648  
00016717  00000-0  10270-3 0  9010
2 25544  51
6413 264
1729 0003044 203
9830 156
1182 15
54086385  8398


Satellite: ISS
Catalog Number: 25544
Epoch time:      17339
52662648   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:       264
1729  deg
Eccentricity:     
0003044     
Arg of perigee:   203
9830  deg
Mean anomaly:     156
1182  deg
Mean motion:   15
54086385  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             839
Checksum:              312


Coasting Arc #3 (Orbit 854)
---------------------------------------

Vector Time (GMT): 2017/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2273007
90                 A    =         6782557
94  meter
 Y    =       -4965020
87  meter          E    =           
0010424
 Z    =        4018736
70                 I    =           51
26740
 XDOT =       4223
149536                 Wp   =          118
19387
 YDOT =       5087
901693  meter/sec      RA   =          258
42038  deg
 ZDOT =       3884
751414                 TA   =          291
25659
                                          MA   =          291
36788
                                          Ha   =            220
844  n
mi
                                          Hp   =            215
164

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7457374
99                 X    =         2308838
06
 Y    =      -16289438
55  feet           Y    =        -4939402
64  meter
 Z    =       13184831
69                 Z    =         4029864
78
 XDOT =      13855
477480                 XDOT =        4147
071119
 YDOT =      16692
590855  feet/sec       YDOT =        5134
702034  meter/sec
 ZDOT =      12745
247420                 ZDOT =        3905
081990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13745151
73                 X    =         4189522
25
 Y    =       11432591
25  feet           Y    =         3484653
81  meter
 Z    =       13234980
09                 Z    =         4034021
93
 XDOT =     -18918
511039                 XDOT =       -5766
362165
 YDOT =       7839
694823  feet/sec       YDOT =        2389
538982  meter/sec
 ZDOT =      12834
645572                 ZDOT =        3911
999970


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   17340
55548899  
00016717  00000-0  10270-3 0  9027
2 25544  51
6406 259
0450 0003021 206
6352 153
4646 15
54083935  8559


Satellite: ISS
Catalog Number: 25544
Epoch time:      17340
55548899   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:       259
0450  deg
Eccentricity:     
0003021     
Arg of perigee:   206
6352  deg
Mean anomaly:     153
4646  deg
Mean motion:   15
54083935  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             855
Checksum:              310


Coasting Arc #4 (Orbit 854)
---------------------------------------

Vector Time (GMT): 2017/340/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3673105
23                 A    =         6784767
61  meter
 Y    =       -4667291
59  meter          E    =           
0004020
 Z    =       -3285309
29                 I    =           51
27671
 XDOT =       2701
001893                 Wp   =          125
17226
 YDOT =      -5424
627248  meter/sec      RA   =          258
12659  deg
 ZDOT =       4688
504305                 TA   =          196
48141
                                          MA   =          196
49449
                                          Ha   =            220
846  n
mi
                                          Hp   =            215
090

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12050870
19                 X    =        -3604682
88
 Y    =      -15312636
46  feet           Y    =        -4707983
84  meter
 Z    =      -10778573
79                 Z    =        -3302986
46
 XDOT =       8861
554766                 XDOT =        2738
686279
 YDOT =     -17797
333490  feet/sec       YDOT =       -5394
212598  meter/sec
 ZDOT =      15382
231972                 ZDOT =        4701
715913

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14854957
56                 X    =         4527791
07
 Y    =      -12543909
30  feet           Y    =        -3823383
55  meter
 Z    =      -10856267
13                 Z    =        -3308990
22
 XDOT =      17196
380133                 XDOT =        5241
456664
 YDOT =       7005
487241  feet/sec       YDOT =        2135
272511  meter/sec
 ZDOT =      15441
695505                 ZDOT =        4706
628790


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   17340
55548870  
00016717  00000-0  10270-3 0  9037
2 25544  51
6420 259
0452 0003040 206
9584 153
1412 15
54101475  8556


Satellite: ISS
Catalog Number: 25544
Epoch time:      17340
55548870   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:       259
0452  deg
Eccentricity:     
0003040     
Arg of perigee:   206
9584  deg
Mean anomaly:     153
1412  deg
Mean motion:   15
54101475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             855
Checksum:              287


Coasting Arc #5 (Orbit 870)
---------------------------------------

Vector Time (GMT): 2017/341/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3224002
01                 A    =         6788115
65  meter
 Y    =        5689924
74  meter          E    =           
0014000
 Z    =        1789088
81                 I    =           51
29427
 XDOT =      -3564
687244                 Wp   =          127
27694
 YDOT =       3797
870775  meter/sec      RA   =          253
12630  deg
 ZDOT =      -5632
737553                 TA   =           32
95959
                                          MA   =           32
87239
                                          Ha   =            220
789  n
mi
                                          Hp   =            215
262

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10577434
41                 X    =         3151445
62
 Y    =       18667732
08  feet           Y    =         5725571
89  meter
 Z    =        5869713
94                 Z    =         1804574
27
 XDOT =     -11695
168122                 XDOT =       -3579
530068
 YDOT =      12460
205956  feet/sec       YDOT =        3757
925508  meter/sec
 ZDOT =     -18480
110083                 ZDOT =       -5650
089405

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18065307
01                 X    =        -5506305
58
 Y    =       11541669
30  feet           Y    =         3517900
80  meter
 Z    =        5937544
46                 Z    =         1809763
55
 XDOT =     -12230
004316                 XDOT =       -3727
705315
 YDOT =      -9558
907785  feet/sec       YDOT =       -2913
555093  meter/sec
 ZDOT =     -18557
684568                 ZDOT =       -5656
382256


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   17341
58434790  
00016717  00000-0  10270-3 0  9047
2 25544  51
6410 253
9179 0003142 209
9504 150
1469 15
54069337  8719


Satellite: ISS
Catalog Number: 25544
Epoch time:      17341
58434790   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       253
9179  deg
Eccentricity:     
0003142     
Arg of perigee:   209
9504  deg
Mean anomaly:     150
1469  deg
Mean motion:   15
54069337  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             871
Checksum:              310


Coasting Arc #6 (Orbit 873)
---------------------------------------

Vector Time (GMT): 2017/341/18:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2244851
39                 A    =         6781026
00  meter
 Y    =        4621227
61  meter          E    =           
0007087
 Z    =       -4432162
53                 I    =           51
26879
 XDOT =      -4464
203017                 Wp   =           86
15061
 YDOT =      -5300
183056  meter/sec      RA   =          252
12712  deg
 ZDOT =      -3269
265812                 TA   =          150
71080
                                          MA   =          150
67105
                                          Ha   =            220
747  n
mi
                                          Hp   =            215
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7364998
01                 X    =        -2274831
11
 Y    =       15161507
90  feet           Y    =         4595956
89  meter
 Z    =      -14541215
65                 Z    =        -4443139
74
 XDOT =     -14646
335356                 XDOT =       -4388
722691
 YDOT =     -17389
052022  feet/sec       YDOT =       -5349
682518  meter/sec
 ZDOT =     -10725
937705                 ZDOT =       -3290
768612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10330344
91                 X    =        -3148689
13
 Y    =       13264950
30  feet           Y    =         4043156
85  meter
 Z    =      -14590631
84                 Z    =        -4447224
58
 XDOT =      -9571
455811                 XDOT =       -2917
379731
 YDOT =     -19341
246648  feet/sec       YDOT =       -5895
211978  meter/sec
 ZDOT =     -10820
531418                 ZDOT =       -3298
097976


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   17341
77725664  
00016717  00000-0  10270-3 0  9052
2 25544  51
6370 252
9523 0003189 210
2567 149
8401 15
54102850  8743


Satellite: ISS
Catalog Number: 25544
Epoch time:      17341
77725664   =   yrday
fracday
Element set:     905
Inclination:       51
6370  deg
RA of node:       252
9523  deg
Eccentricity:     
0003189     
Arg of perigee:   210
2567  deg
Mean anomaly:     149
8401  deg
Mean motion:   15
54102850  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             874
Checksum:              309


Coasting Arc #7 (Orbit 889)
---------------------------------------

Vector Time (GMT): 2017/342/18:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3106511
54                 A    =         6778329
06  meter
 Y    =       -3184910
30  meter          E    =           
0005749
 Z    =        5113278
20                 I    =           51
27063
 XDOT =       4008
374279                 Wp   =          158
69282
 YDOT =       6358
945717  meter/sec      RA   =          247
10614  deg
 ZDOT =       1519
754449                 TA   =          276
55847
                                          MA   =          276
62391
                                          Ha   =            220
645  n
mi
                                          Hp   =            215
396

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10191966
98                 X    =         3117057
42
 Y    =      -10449180
78  feet           Y    =        -3150112
52  meter
 Z    =       16775847
11                 Z    =         5128394
06
 XDOT =      13150
834248                 XDOT =        3929
586722
 YDOT =      20862
682797  feet/sec       YDOT =        6403
329475  meter/sec
 ZDOT =       4986
071028                 ZDOT =        1539
034891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11934260
86                 X    =         3637562
71
 Y    =       -8268240
36  feet           Y    =        -2520159
66  meter
 Z    =       16843403
32                 Z    =         5133869
33
 XDOT =       8169
495123                 XDOT =        2490
062114
 YDOT =      22159
933161  feet/sec       YDOT =        6754
347627  meter/sec
 ZDOT =       5070
665096                 ZDOT =        1545
538721


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   17342
80611084  
00016717  00000-0  10270-3 0  9068
2 25544  51
6372 247
8228 0003166 215
5657 144
5285 15
54064643  8900


Satellite: ISS
Catalog Number: 25544
Epoch time:      17342
80611084   =   yrday
fracday
Element set:     906
Inclination:       51
6372  deg
RA of node:       247
8228  deg
Eccentricity:     
0003166     
Arg of perigee:   215
5657  deg
Mean anomaly:     144
5285  deg
Mean motion:   15
54064643  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             890
Checksum:              312


Coasting Arc #8 (Orbit 889)
---------------------------------------

Vector Time (GMT): 2017/342/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4715081
50                 A    =         6781184
15  meter
 Y    =        2110395
39  meter          E    =           
0006843
 Z    =        4387352
10                 I    =           51
28059
 XDOT =         20
354540                 Wp   =           86
29152
 YDOT =       6906
180464  meter/sec      RA   =          247
02596  deg
 ZDOT =      -3338
922501                 TA   =           37
64152
                                          MA   =           37
59365
                                          Ha   =            220
575  n
mi
                                          Hp   =            215
392

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15469427
50                 X    =         4669820
49
 Y    =        6923869
39  feet           Y    =         2162869
31  meter
 Z    =       14394199
81                 Z    =         4410146
67
 XDOT =         66
779987                 XDOT =         -40
654915
 YDOT =      22658
072388  feet/sec       YDOT =        6906
067164  meter/sec
 ZDOT =     -10954
470149                 ZDOT =       -3338
971380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14233646
27                 X    =         4338415
38
 Y    =        9040662
40  feet           Y    =         2755593
90  meter
 Z    =       14495029
50                 Z    =         4418084
99
 XDOT =      -2424
681669                 XDOT =        -739
042973
 YDOT =      21408
768028  feet/sec       YDOT =        6525
392495  meter/sec
 ZDOT =     -10955
730249                 ZDOT =       -3339
306580


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   17342
80610982  
00016717  00000-0  10270-3 0  9075
2 25544  51
6372 247
8226 0003339 215
1253 144
9680 15
54079618  8909


Satellite: ISS
Catalog Number: 25544
Epoch time:      17342
80610982   =   yrday
fracday
Element set:     907
Inclination:       51
6372  deg
RA of node:       247
8226  deg
Eccentricity:     
0003339     
Arg of perigee:   215
1253  deg
Mean anomaly:     144
9680  deg
Mean motion:   15
54079618  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             890
Checksum:              318


Coasting Arc #9 (Orbit 904)
---------------------------------------

Vector Time (GMT): 2017/343/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4809382
81                 A    =         6784869
30  meter
 Y    =       -3533642
26  meter          E    =           
0003445
 Z    =       -3232387
77                 I    =           51
30737
 XDOT =       1157
855928                 Wp   =          127
58243
 YDOT =      -5909
005572  meter/sec      RA   =          242
01555  deg
 ZDOT =       4738
392593                 TA   =          194
81501
                                          MA   =          194
82511
                                          Ha   =            220
677  n
mi
                                          Hp   =            215
244

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15778815
00                 X    =        -4753809
88
 Y    =      -11593314
51  feet           Y    =        -3587113
19  meter
 Z    =      -10604946
74                 Z    =        -3255615
44
 XDOT =       3798
739920                 XDOT =        1200
829176
 YDOT =     -19386
501221  feet/sec       YDOT =       -5895
817578  meter/sec
 ZDOT =      15545
907458                 ZDOT =        4744
121198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14134473
20                 X    =        -4308187
43
 Y    =      -13468739
98  feet           Y    =        -4105271
95  meter
 Z    =      -10707499
73                 Z    =        -3263645
92
 XDOT =       5110
883301                 XDOT =        1557
797230
 YDOT =     -17739
575165  feet/sec       YDOT =       -5407
022510  meter/sec
 ZDOT =      15572
207867                 ZDOT =        4746
408958


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   17343
77065588  
00016717  00000-0  10270-3 0  9089
2 25544  51
6377 243
0138 0003245 214
7842 145
3098 15
54109800  9051


Satellite: ISS
Catalog Number: 25544
Epoch time:      17343
77065588   =   yrday
fracday
Element set:     908
Inclination:       51
6377  deg
RA of node:       243
0138  deg
Eccentricity:     
0003245     
Arg of perigee:   214
7842  deg
Mean anomaly:     145
3098  deg
Mean motion:   15
54109800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             905
Checksum:              314


Coasting Arc #10 (Orbit 920)
---------------------------------------

Vector Time (GMT): 2017/344/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4645559
20                 A    =         6788057
93  meter
 Y    =        4629542
70  meter          E    =           
0013381
 Z    =        1720298
56                 I    =           51
33324
 XDOT =      -2441
634804                 Wp   =          128
91086
 YDOT =       4562
582571  meter/sec      RA   =          237
01713  deg
 ZDOT =      -5663
516618                 TA   =           32
12666
                                          MA   =           32
04519
                                          Ha   =            220
452  n
mi
                                          Hp   =            215
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15241335
96                 X    =         4585088
76
 Y    =       15188788
40  feet           Y    =         4681154
34  meter
 Z    =        5644024
15                 Z    =         1742718
61
 XDOT =      -8010
612873                 XDOT =       -2464
962705
 YDOT =      14969
102922  feet/sec       YDOT =        4535
148326  meter/sec
 ZDOT =     -18581
091265                 ZDOT =       -5675
433836

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13473745
41                 X    =         4106797
60
 Y    =       16743073
60  feet           Y    =         5103288
83  meter
 Z    =        5742847
24                 Z    =         1750419
84
 XDOT =      -8238
308578                 XDOT =       -2511
036455
 YDOT =      13045
082932  feet/sec       YDOT =        3976
141278  meter/sec
 ZDOT =     -18634
649332                 ZDOT =       -5679
841116


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   17344
79950113  
00016717  00000-0  10270-3 0  9090
2 25544  51
6366 237
8853 0003293 221
7979 138
2922 15
54119923  9218


Satellite: ISS
Catalog Number: 25544
Epoch time:      17344
79950113   =   yrday
fracday
Element set:     909
Inclination:       51
6366  deg
RA of node:       237
8853  deg
Eccentricity:     
0003293     
Arg of perigee:   221
7979  deg
Mean anomaly:     138
2922  deg
Mean motion:   15
54119923  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             921
Checksum:              332


Coasting Arc #11 (Orbit 923)
---------------------------------------

Vector Time (GMT): 2017/344/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3242923
19                 A    =         6777367
97  meter
 Y    =       -2752342
30  meter          E    =           
0003473
 Z    =        5276479
39                 I    =           51
30539
 XDOT =       4542
173801                 Wp   =          176
79078
 YDOT =       6164
787012  meter/sec      RA   =          236
13948  deg
 ZDOT =        420
665603                 TA   =          269
15923
                                          MA   =          269
19903
                                          Ha   =            220
355  n
mi
                                          Hp   =            215
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10639511
76                 X    =         3247828
97
 Y    =       -9029994
41  feet           Y    =        -2716050
48  meter
 Z    =       17311284
09                 Z    =         5292244
37
 XDOT =      14902
145018                 XDOT =        4470
856522
 YDOT =      20225
679174  feet/sec       YDOT =        6215
181930  meter/sec
 ZDOT =       1380
136493                 ZDOT =         442
557161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2222268
39                 X    =         -677347
41
 Y    =      -13687958
55  feet           Y    =        -4172089
77  meter
 Z    =       17381653
56                 Z    =         5297928
01
 XDOT =      24024
902436                 XDOT =        7322
790262
 YDOT =      -2011
501705  feet/sec       YDOT =        -613
105720  meter/sec
 ZDOT =       1476
392418                 ZDOT =         450
004409


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   17344
99240845  
00016717  00000-0  10270-3 0  9108
2 25544  51
6411 236
9252 0003465 222
4298 137
6587 15
54144580  9245


Satellite: ISS
Catalog Number: 25544
Epoch time:      17344
99240845   =   yrday
fracday
Element set:     910
Inclination:       51
6411  deg
RA of node:       236
9252  deg
Eccentricity:     
0003465     
Arg of perigee:   222
4298  deg
Mean anomaly:     137
6587  deg
Mean motion:   15
54144580  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             924
Checksum:              317


Coasting Arc #12 (Orbit 938)
---------------------------------------

Vector Time (GMT): 2017/345/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4265869
39                 A    =         6778069
53  meter
 Y    =        1248347
30  meter          E    =           
0012107
 Z    =       -5127947
74                 I    =           51
32674
 XDOT =      -3717
944754                 Wp   =          114
50703
 YDOT =      -6525
937816  meter/sec      RA   =          231
11790  deg
 ZDOT =       1502
110977                 TA   =          170
05308
                                          MA   =          170
02910
                                          Ha   =            220
373  n
mi
                                          Hp   =            215
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13995634
47                 X    =        -4254602
49
 Y    =        4095627
61  feet           Y    =         1200706
63  meter
 Z    =      -16823975
52                 Z    =        -5148642
72
 XDOT =     -12197
981478                 XDOT =       -3651
990203
 YDOT =     -21410
557139  feet/sec       YDOT =       -6567
145701  meter/sec
 ZDOT =       4928
185619                 ZDOT =        1484
210180

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3498534
45                 X    =        -1066353
30
 Y    =       14046599
57  feet           Y    =         4281403
55  meter
 Z    =      -16916010
14                 Z    =        -5155999
89
 XDOT =     -23631
030299                 XDOT =       -7202
738035
 YDOT =        -36
994144  feet/sec       YDOT =         -11
275815  meter/sec
 ZDOT =       4849
676975                 ZDOT =        1478
181542


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   17345
95694862  
00016717  00000-0  10270-3 0  9118
2 25544  51
6411 232
1177 0003340 226
8057 133
2817 15
54132300  9393


Satellite: ISS
Catalog Number: 25544
Epoch time:      17345
95694862   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       232
1177  deg
Eccentricity:     
0003340     
Arg of perigee:   226
8057  deg
Mean anomaly:     133
2817  deg
Mean motion:   15
54132300  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             939
Checksum:              295


Coasting Arc #13 (Orbit 954)
---------------------------------------

Vector Time (GMT): 2017/346/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5123374
02                 A    =         6780813
16  meter
 Y    =         213695
44  meter          E    =           
0006058
 Z    =        4432333
54                 I    =           51
35792
 XDOT =       2567
937219                 Wp   =           77
88570
 YDOT =       6443
671264  meter/sec      RA   =          226
10219  deg
 ZDOT =      -3273
923787                 TA   =           45
26441
                                          MA   =           45
21511
                                          Ha   =            220
100  n
mi
                                          Hp   =            215
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16808969
88                 X    =         5099073
35
 Y    =         701100
51  feet           Y    =          270852
43  meter
 Z    =       14541776
70                 Z    =         4457162
50
 XDOT =       8424
990875                 XDOT =        2511
594754
 YDOT =      21140
653753  feet/sec       YDOT =        6472
072818  meter/sec
 ZDOT =     -10741
219773                 ZDOT =       -3261
585982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8823675
07                 X    =         2689456
16
 Y    =      -14211233
42  feet           Y    =        -4331583
95  meter
 Z    =       14651958
33                 Z    =         4465916
90
 XDOT =      21549
851015                 XDOT =        6568
394589
 YDOT =       2344
423855  feet/sec       YDOT =         714
580391  meter/sec
 ZDOT =     -10687
377293                 ZDOT =       -3257
512599


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   17346
98578697  
00016717  00000-0  10270-3 0  9120
2 25544  51
6416 226
9890 0003246 232
4610 127
6248 15
54145600  9554


Satellite: ISS
Catalog Number: 25544
Epoch time:      17346
98578697   =   yrday
fracday
Element set:     912
Inclination:       51
6416  deg
RA of node:       226
9890  deg
Eccentricity:     
0003246     
Arg of perigee:   232
4610  deg
Mean anomaly:     127
6248  deg
Mean motion:   15
54145600  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             955
Checksum:              328


Coasting Arc #14 (Orbit 969)
---------------------------------------

Vector Time (GMT): 2017/347/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5738173
86                 A    =         6784632
46  meter
 Y    =       -1521006
87  meter          E    =           
0002536
 Z    =       -3288446
02                 I    =           51
39271
 XDOT =      -1114
606655                 Wp   =          128
54511
 YDOT =      -5950
392403  meter/sec      RA   =          221
09848  deg
 ZDOT =       4698
082788                 TA   =          193
13154
                                          MA   =          193
13814
                                          Ha   =            220
207  n
mi
                                          Hp   =            215
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18826029
74                 X    =        -5704765
27
 Y    =       -4990180
03  feet           Y    =        -1584988
06  meter
 Z    =      -10788864
89                 Z    =        -3316239
52
 XDOT =      -3656
845980                 XDOT =       -1070
806138
 YDOT =     -19522
284788  feet/sec       YDOT =       -5962
612074  meter/sec
 ZDOT =      15413
657440                 ZDOT =        4692
774350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13321413
23                 X    =        -4060366
75
 Y    =       14113412
18  feet           Y    =         4301768
03  meter
 Z    =      -10912032
08                 Z    =        -3325987
38
 XDOT =     -17925
307313                 XDOT =       -5463
633669
 YDOT =      -5021
909088  feet/sec       YDOT =       -1530
677890  meter/sec
 ZDOT =      15390
938427                 ZDOT =        4691
158033


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   17347
95032193  
00016717  00000-0  10270-3 0  9135
2 25544  51
6403 222
1819 0003307 234
9296 125
1547 15
54131215  9703


Satellite: ISS
Catalog Number: 25544
Epoch time:      17347
95032193   =   yrday
fracday
Element set:     913
Inclination:       51
6403  deg
RA of node:       222
1819  deg
Eccentricity:     
0003307     
Arg of perigee:   234
9296  deg
Mean anomaly:     125
1547  deg
Mean motion:   15
54131215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             970
Checksum:              292


Coasting Arc #15 (Orbit 971)
---------------------------------------

Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2617054
20                 A    =         6777423
56  meter
 Y    =        3333932
47  meter          E    =           
0012397
 Z    =       -5299269
74                 I    =           51
37135
 XDOT =      -5901
526509                 Wp   =           96
43166
 YDOT =      -4880
158450  meter/sec      RA   =          220
52987  deg
 ZDOT =       -157
456478                 TA   =          172
07029
                                          MA   =          172
05067
                                          Ha   =            220
254  n
mi
                                          Hp   =            215
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8586135
84                 X    =        -2628399
12
 Y    =       10938098
64  feet           Y    =         3304603
67  meter
 Z    =      -17386055
58                 Z    =        -5312010
06
 XDOT =     -19361
963613                 XDOT =       -5845
751799
 YDOT =     -16011
018536  feet/sec       YDOT =       -4945
841489  meter/sec
 ZDOT =       -516
589496                 ZDOT =        -185
989386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12713988
05                 X    =         3875223
56
 Y    =        5452690
09  feet           Y    =         1661979
94  meter
 Z    =      -17443088
54                 Z    =        -5316653
39
 XDOT =     -10237
320197                 XDOT =       -3120
335196
 YDOT =      21832
284892  feet/sec       YDOT =        6654
480435  meter/sec
 ZDOT =       -642
563181                 ZDOT =        -195
853258


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   17348
07892702  
00016717  00000-0  10270-3 0  9140
2 25544  51
6405 221
5415 0003046 236
0285 124
0579 15
54109464  9727


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
07892702   =   yrday
fracday
Element set:     914
Inclination:       51
6405  deg
RA of node:       221
5415  deg
Eccentricity:     
0003046     
Arg of perigee:   236
0285  deg
Mean anomaly:     124
0579  deg
Mean motion:   15
54109464  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             972
Checksum:              301


Coasting Arc #16 (Orbit 974)
---------------------------------------

Vector Time (GMT): 2017/348/05:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925316
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         464787
09                 A    =         6779197
08  meter
 Y    =       -4683364
23  meter          E    =           
0005960
 Z    =        4878383
18                 I    =           51
37826
 XDOT =       6621
405208                 Wp   =          147
71079
 YDOT =       3089
256553  meter/sec      RA   =          219
76251  deg
 ZDOT =       2328
642069                 TA   =          279
38428
                                          MA   =          279
45165
                                          Ha   =            220
132  n
mi
                                          Hp   =            215
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1524892
03                 X    =          493426
15
 Y    =      -15365368
21  feet           Y    =        -4678006
85  meter
 Z    =       16005194
16                 Z    =         4880710
26
 XDOT =      21723
770366                 XDOT =        6575
056679
 YDOT =      10135
356146  feet/sec       YDOT =        3163
042334  meter/sec
 ZDOT =       7639
901800                 ZDOT =        2360
694755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6294360
92                 X    =        -1918521
21
 Y    =       14087183
44  feet           Y    =         4293773
51  meter
 Z    =       16016190
55                 Z    =         4881734
88
 XDOT =     -16223
946388                 XDOT =       -4945
058859
 YDOT =     -16119
791828  feet/sec       YDOT =       -4913
312549  meter/sec
 ZDOT =       7781
758516                 ZDOT =        2371
879996


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   17348
27183326  
00016717  00000-0  10270-3 0  9158
2 25544  51
6374 220
5805 0003046 240
6766 119
4082 15
54135378  9752


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
27183326   =   yrday
fracday
Element set:     915
Inclination:       51
6374  deg
RA of node:       220
5805  deg
Eccentricity:     
0003046     
Arg of perigee:   240
6766  deg
Mean anomaly:     119
4082  deg
Mean motion:   15
54135378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             975
Checksum:              314


Coasting Arc #17 (Orbit 989)
---------------------------------------

Vector Time (GMT): 2017/349/05:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925316
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1994641
47                 A    =         6777453
97  meter
 Y    =        3754645
25  meter          E    =           
0012090
 Z    =       -5288516
40                 I    =           51
39871
 XDOT =      -6478
076424                 Wp   =           91
96695
 YDOT =      -4063
255715  meter/sec      RA   =          214
74648  deg
 ZDOT =       -442
740315                 TA   =          173
79902
                                          MA   =          173
78404
                                          Ha   =            220
132  n
mi
                                          Hp   =            215
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6544099
31                 X    =        -2010789
40
 Y    =       12318389
91  feet           Y    =         3732249
94  meter
 Z    =      -17350775
58                 Z    =        -5298244
77
 XDOT =     -21253
531576                 XDOT =       -6430
007906
 YDOT =     -13330
891454  feet/sec       YDOT =       -4135
429191  meter/sec
 ZDOT =      -1452
560088                 ZDOT =        -474
092692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9889159
07                 X    =         3014215
68
 Y    =       -9759778
74  feet           Y    =        -2974780
56  meter
 Z    =      -17394500
02                 Z    =        -5301843
61
 XDOT =      15435
891934                 XDOT =        4704
859861
 YDOT =      18468
940942  feet/sec       YDOT =        5629
333199  meter/sec
 ZDOT =      -1591
188760                 ZDOT =        -484
994334


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   17349
23636473  
00016717  00000-0  10270-3 0  9162
2 25544  51
6379 215
7719 0002940 243
8228 116
2623 15
54121596  9907


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
23636473   =   yrday
fracday
Element set:     916
Inclination:       51
6379  deg
RA of node:       215
7719  deg
Eccentricity:     
0002940     
Arg of perigee:   243
8228  deg
Mean anomaly:     116
2623  deg
Mean motion:   15
54121596  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             990
Checksum:              323


Coasting Arc #18 (Orbit 1005)
---------------------------------------

Vector Time (GMT): 2017/350/05:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925316
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3491228
15                 A    =         6778041
89  meter
 Y    =       -2720188
21  meter          E    =           
0001899
 Z    =        5133072
42                 I    =           51
42830
 XDOT =       5863
015436                 Wp   =           32
12278
 YDOT =       4714
546144  meter/sec      RA   =          209
73158  deg
 ZDOT =      -1487
466267                 TA   =           72
25157
                                          MA   =           72
23084
                                          Ha   =            219
934  n
mi
                                          Hp   =            215
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11454160
59                 X    =         3496452
39
 Y    =       -8924502
01  feet           Y    =        -2681118
19  meter
 Z    =       16840788
78                 Z    =         5150044
30
 XDOT =      19235
614949                 XDOT =        5817
085807
 YDOT =      15467
671075  feet/sec       YDOT =        4779
853724  meter/sec
 ZDOT =      -4880
138671                 ZDOT =       -1459
096412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13440398
55                 X    =        -4096633
48
 Y    =        5257678
68  feet           Y    =         1602540
46  meter
 Z    =       16916536
28                 Z    =         5156160
26
 XDOT =     -13581
926935                 XDOT =       -4139
771330
 YDOT =     -19402
130380  feet/sec       YDOT =       -5913
769340  meter/sec
 ZDOT =      -4754
824869                 ZDOT =       -1449
270620


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   17350
26519429  
00016717  00000-0  10270-3 0  9179
2 25544  51
6378 210
6434 0002938 249
9088 110
1749 15
54129271 10061


Satellite: ISS
Catalog Number: 25544
Epoch time:      17350
26519429   =   yrday
fracday
Element set:     917
Inclination:       51
6378  deg
RA of node:       210
6434  deg
Eccentricity:     
0002938     
Arg of perigee:   249
9088  deg
Mean anomaly:     110
1749  deg
Mean motion:   15
54129271  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1006
Checksum:              314


Coasting Arc #19 (Orbit 1020)
---------------------------------------

Vector Time (GMT): 2017/351/05:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925316
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4837827
07                 A    =         6780830
01  meter
 Y    =        1676847
77  meter          E    =           
0007276
 Z    =       -4453108
55                 I    =           51
46577
 XDOT =      -4751
979496                 Wp   =          124
57347
 YDOT =      -5047
675183  meter/sec      RA   =          204
72341  deg
 ZDOT =       3261
545132                 TA   =          178
39901
                                          MA   =          178
39668
                                          Ha   =            219
992  n
mi
                                          Hp   =            215
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15872136
05                 X    =        -4834587
32
 Y    =        5501469
06  feet           Y    =         1622766
48  meter
 Z    =      -14609936
19                 Z    =        -4476601
31
 XDOT =     -15590
483912                 XDOT =       -4711
024943
 YDOT =     -16560
614116  feet/sec       YDOT =       -5100
586427  meter/sec
 ZDOT =      10700
607390                 ZDOT =        3238
560269

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16677933
40                 X    =         5083434
10
 Y    =        -985348
42  feet           Y    =         -300334
20  meter
 Z    =      -14714507
33                 Z    =        -4484981
83
 XDOT =      10474
018272                 XDOT =        3192
480769
 YDOT =      18989
294093  feet/sec       YDOT =        5787
936839  meter/sec
 ZDOT =      10599
235181                 ZDOT =        3230
646883


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   17351
22971966  
00016717  00000-0  10270-3 0  9185
2 25544  51
6371 205
8355 0002958 254
9679 105
1147 15
54122094 10215


Satellite: ISS
Catalog Number: 25544
Epoch time:      17351
22971966   =   yrday
fracday
Element set:     918
Inclination:       51
6371  deg
RA of node:       205
8355  deg
Eccentricity:     
0002958     
Arg of perigee:   254
9679  deg
Mean anomaly:     105
1147  deg
Mean motion:   15
54122094  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1021
Checksum:              314


Coasting Arc #20 (Orbit 1022)
---------------------------------------

Vector Time (GMT): 2017/351/07:21:01
000
Vector Time (MET): N/A
Weight (LBS)     : 925316
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -588557
28                 A    =         6778832
54  meter
 Y    =       -4593075
65  meter          E    =           
0004910
 Z    =        4950073
32                 I    =           51
46345
 XDOT =       7229
272016                 Wp   =          150
62038
 YDOT =       1392
534508  meter/sec      RA   =          204
33117  deg
 ZDOT =       2146
555693                 TA   =          278
38385
                                          MA   =          278
43951
                                          Ha   =            219
911  n
mi
                                          Hp   =            215
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1930962
20                 X    =         -561197
70
 Y    =      -15069145
82  feet           Y    =        -4599504
86  meter
 Z    =       16240398
03                 Z    =         4947280
23
 XDOT =      23718
084042                 XDOT =        7202
736050
 YDOT =       4568
682770  feet/sec       YDOT =        1473
228563  meter/sec
 ZDOT =       7042
505555                 ZDOT =        2181
609170

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5990263
98                 X    =         1825832
46
 Y    =       13975205
46  feet           Y    =         4259642
62  meter
 Z    =       16228637
31                 Z    =         4946488
65
 XDOT =     -23012
342263                 XDOT =       -7014
161922
 YDOT =       1485
819574  feet/sec       YDOT =         452
877806  meter/sec
 ZDOT =       7197
991533                 ZDOT =        2193
947819


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   17351
35832208  
00016717  00000-0  10270-3 0  9195
2 25544  51
6386 205
1952 0003072 254
3696 105
7118 15
54167574 10236


Satellite: ISS
Catalog Number: 25544
Epoch time:      17351
35832208   =   yrday
fracday
Element set:     919
Inclination:       51
6386  deg
RA of node:       205
1952  deg
Eccentricity:     
0003072     
Arg of perigee:   254
3696  deg
Mean anomaly:     105
7118  deg
Mean motion:   15
54167574  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1023
Checksum:              305


Coasting Arc #21 (Orbit 1037)
---------------------------------------

Vector Time (GMT): 2017/352/07:21:01
000
Vector Time (MET): N/A
Weight (LBS)     : 925316
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1138711
54                 A    =         6777312
31  meter
 Y    =        4074282
52  meter          E    =           
0011909
 Z    =       -5305174
18                 I    =           51
48910
 XDOT =      -7286
300489                 Wp   =           90
24446
 YDOT =      -2350
646542  meter/sec      RA   =          199
32061  deg
 ZDOT =       -241
832744                 TA   =          177
44624
                                          MA   =          177
44015
                                          Ha   =            219
907  n
mi
                                          Hp   =            215
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3735930
24                 X    =        -1158416
62
 Y    =       13367068
65  feet           Y    =         4061439
11  meter
 Z    =      -17405427
11                 Z    =        -5310753
10
 XDOT =     -23905
185333                 XDOT =       -7258
298688
 YDOT =      -7712
094953  feet/sec       YDOT =       -2431
970338  meter/sec
 ZDOT =       -793
414516                 ZDOT =        -277
159698

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -320275
79                 X    =          -97620
06
 Y    =      -13843771
71  feet           Y    =        -4219581
62  meter
 Z    =      -17430777
39                 Z    =        -5312900
95
 XDOT =      24095
979261                 XDOT =        7344
454479
 YDOT =        636
551494  feet/sec       YDOT =         194
020895  meter/sec
 ZDOT =       -950
006573                 ZDOT =        -289
562003


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   17352
32284607  
00016717  00000-0  10270-3 0  9209
2 25544  51
6392 200
3865 0002963 259
5776 100
5043 15
54152928 10380


Satellite: ISS
Catalog Number: 25544
Epoch time:      17352
32284607   =   yrday
fracday
Element set:     920
Inclination:       51
6392  deg
RA of node:       200
3865  deg
Eccentricity:     
0002963     
Arg of perigee:   259
5776  deg
Mean anomaly:     100
5043  deg
Mean motion:   15
54152928  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1038
Checksum:              303


Coasting Arc #22 (Orbit 1053)
---------------------------------------

Vector Time (GMT): 2017/353/07:21:01
000
Vector Time (MET): N/A
Weight (LBS)     : 925316
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2850132
25                 A    =         6778115
07  meter
 Y    =       -3448907
54  meter          E    =           
0002886
 Z    =        5091305
99                 I    =           51
52323
 XDOT =       6798
656671                 Wp   =           23
34067
 YDOT =       3120
179266  meter/sec      RA   =          194
31240  deg
 ZDOT =      -1689
345317                 TA   =           83
01876
                                          MA   =           82
98594
                                          Ha   =            219
736  n
mi
                                          Hp   =            215
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9350827
59                 X    =         2863755
99
 Y    =      -11315313
46  feet           Y    =        -3416959
84  meter
 Z    =       16703759
81                 Z    =         5105183
73
 XDOT =      22305
304038                 XDOT =        6771
466703
 YDOT =      10236
808615  feet/sec       YDOT =        3196
054661  meter/sec
 ZDOT =      -5542
471512                 ZDOT =       -1656
385243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5417764
10                 X    =        -1651334
50
 Y    =       13566227
77  feet           Y    =         4134986
22  meter
 Z    =       16765893
46                 Z    =         5110244
33
 XDOT =     -23394
581912                 XDOT =       -7130
668567
 YDOT =      -2661
709863  feet/sec       YDOT =        -811
289166  meter/sec
 ZDOT =      -5396
474858                 ZDOT =       -1644
845537


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   17353
35166590  
00016717  00000-0  10270-3 0  9214
2 25544  51
6390 195
2582 0003018 265
6872  94
3936 15
54173248 10540


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
35166590   =   yrday
fracday
Element set:     921
Inclination:       51
6390  deg
RA of node:       195
2582  deg
Eccentricity:     
0003018     
Arg of perigee:   265
6872  deg
Mean anomaly:      94
3936  deg
Mean motion:   15
54173248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1054
Checksum:              318


Coasting Arc #23 (Orbit 1054)
---------------------------------------

Vector Time (GMT): 2017/353/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1938752
32                 A    =         6779646
39  meter
 Y    =       -4399618
47  meter          E    =           
0005394
 Z    =        4778395
77                 I    =           51
53100
 XDOT =       7203
446727                 Wp   =          136
46137
 YDOT =       -333
499992  meter/sec      RA   =          194
06251  deg
 ZDOT =       2610
022942                 TA   =          287
74385
                                          MA   =          287
80272
                                          Ha   =            219
958  n
mi
                                          Hp   =            215
714

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6360735
95                 X    =        -1912621
59
 Y    =      -14434443
79  feet           Y    =        -4421153
38  meter
 Z    =       15677151
49                 Z    =         4769040
87
 XDOT =      23633
355405                 XDOT =        7193
962441
 YDOT =      -1094
160078  feet/sec       YDOT =        -252
999463  meter/sec
 ZDOT =       8563
067394                 ZDOT =        2644
991952

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13975349
79                 X    =         4259686
62
 Y    =        7401620
92  feet           Y    =         2256014
06  meter
 Z    =       15636202
04                 Z    =         4765914
38
 XDOT =     -17374
058461                 XDOT =       -5295
613019
 YDOT =      14347
849093  feet/sec       YDOT =        4373
224404  meter/sec
 ZDOT =       8718
470602                 ZDOT =        2657
389840


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   17353
41596767  
00016717  00000-0  10270-3 0  9225
2 25544  51
6404 194
9374 0002932 264
2885  95
7934 15
54143745 10557


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
41596767   =   yrday
fracday
Element set:     922
Inclination:       51
6404  deg
RA of node:       194
9374  deg
Eccentricity:     
0002932     
Arg of perigee:   264
2885  deg
Mean anomaly:      95
7934  deg
Mean motion:   15
54143745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1055
Checksum:              336
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