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

 
Date: November 28th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 ET - UTC (sec) : 67 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


There are no maneuvers



Coasting Arc #1 (Orbit 1344)
---------------------------------------

Vector Time (GMT): 2015/331/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5033539
81                 A    =         6782093
08  meter
 Y    =       -2197562
38  meter          E    =           
0005388
 Z    =       -3976943
15                 I    =           51
57244
 XDOT =       4993
892198                 Wp   =          155
94703
 YDOT =      -4239
756663  meter/sec      RA   =          348
52256  deg
 ZDOT =      -3984
603646                 TA   =           72
52604
                                          MA   =           72
46715
                                          Ha   =            221
311  n
mi
                                          Hp   =            215
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16514238
24                 X    =        -4989273
25
 Y    =       -7209850
32  feet           Y    =        -2253602
93  meter
 Z    =      -13047713
76                 Z    =        -4001288
11
 XDOT =      16384
160754                 XDOT =        5060
287022
 YDOT =     -13909
962806  feet/sec       YDOT =       -4183
540126  meter/sec
 ZDOT =     -13072
846607                 ZDOT =       -3960
182992

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14313746
69                 X    =         4362829
99
 Y    =      -10820118
65  feet           Y    =        -3297972
16  meter
 Z    =      -13152434
32                 Z    =        -4008861
98
 XDOT =       3314
114626                 XDOT =        1010
142138
 YDOT =      20119
000449  feet/sec       YDOT =        6132
271337  meter/sec
 ZDOT =     -12966
432443                 ZDOT =       -3952
168609


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   15331
51108185  
00016717  00000-0  10270-3 0  9009
2 25544  51
6438 348
9392 0008373 212
5375 147
5263 15
54271498 13450


Satellite: ISS
Catalog Number: 25544
Epoch time:      15331
51108185   =   yrday
fracday
Element set:     900
Inclination:       51
6438  deg
RA of node:       348
9392  deg
Eccentricity:     
0008373     
Arg of perigee:   212
5375  deg
Mean anomaly:     147
5263  deg
Mean motion:   15
54271498  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1345
Checksum:              313


Coasting Arc #2 (Orbit 1360)
---------------------------------------

Vector Time (GMT): 2015/332/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3601195
62                 A    =         6778585
64  meter
 Y    =        2996804
88  meter          E    =           
0010201
 Z    =        4901887
21                 I    =           51
52844
 XDOT =      -6272
329333                 Wp   =          175
31787
 YDOT =       3760
229181  meter/sec      RA   =          343
52255  deg
 ZDOT =       2298
856355                 TA   =          252
10502
                                          MA   =          252
21629
                                          Ha   =            221
158  n
mi
                                          Hp   =            215
534

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11814946
26                 X    =         3543605
20
 Y    =        9832037
01  feet           Y    =         3036753
44  meter
 Z    =       16082307
11                 Z    =         4919241
64
 XDOT =     -20578
508310                 XDOT =       -6325
078051
 YDOT =      12336
709911  feet/sec       YDOT =        3689
792743  meter/sec
 ZDOT =       7542
179641                 ZDOT =        2268
258464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14203916
72                 X    =        -4329353
82
 Y    =        5666901
85  feet           Y    =         1727271
68  meter
 Z    =       16156654
42                 Z    =         4924548
27
 XDOT =       -699
437533                 XDOT =        -213
188560
 YDOT =     -22972
980646  feet/sec       YDOT =       -7002
164501  meter/sec
 ZDOT =       7409
178841                 ZDOT =        2258
317711


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   15332
53981436  
00016717  00000-0  10270-3 0  9011
2 25544  51
6425 343
8089 0008262 215
8803 144
1795 15
54287604 13619


Satellite: ISS
Catalog Number: 25544
Epoch time:      15332
53981436   =   yrday
fracday
Element set:     901
Inclination:       51
6425  deg
RA of node:       343
8089  deg
Eccentricity:     
0008262     
Arg of perigee:   215
8803  deg
Mean anomaly:     144
1795  deg
Mean motion:   15
54287604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1361
Checksum:              314


Coasting Arc #3 (Orbit 1375)
---------------------------------------

Vector Time (GMT): 2015/333/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1894629
09                 A    =         6776866
73  meter
 Y    =       -3785816
13  meter          E    =           
0011077
 Z    =       -5299818
00                 I    =           51
49323
 XDOT =       7020
497212                 Wp   =          121
00147
 YDOT =      -3051
179561  meter/sec      RA   =          338
51297  deg
 ZDOT =       -336
314738                 TA   =          145
81880
                                          MA   =          145
74744
                                          Ha   =            220
998  n
mi
                                          Hp   =            215
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6215974
72                 X    =        -1826409
67
 Y    =      -12420656
59  feet           Y    =        -3806621
32  meter
 Z    =      -17387854
33                 Z    =        -5308856
36
 XDOT =      23033
127336                 XDOT =        7055
728168
 YDOT =     -10010
431631  feet/sec       YDOT =       -2972
474718  meter/sec
 ZDOT =      -1103
394811                 ZDOT =        -302
124952

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13838780
74                 X    =         4218060
37
 Y    =         259857
61  feet           Y    =           79204
60  meter
 Z    =      -17426105
47                 Z    =        -5311476
95
 XDOT =      -1629
147363                 XDOT =        -496
564116
 YDOT =      24057
229583  feet/sec       YDOT =        7332
643577  meter/sec
 ZDOT =       -955
028283                 ZDOT =        -291
092621


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   15333
50423347  
00016717  00000-0  10270-3 0  9022
2 25544  51
6433 339
0000 0008327 220
2820 139
7717 15
54304513 13768


Satellite: ISS
Catalog Number: 25544
Epoch time:      15333
50423347   =   yrday
fracday
Element set:     902
Inclination:       51
6433  deg
RA of node:       339
0000  deg
Eccentricity:     
0008327     
Arg of perigee:   220
2820  deg
Mean anomaly:     139
7717  deg
Mean motion:   15
54304513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1376
Checksum:              274


Coasting Arc #4 (Orbit 1391)
---------------------------------------

Vector Time (GMT): 2015/334/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         136085
36                 A    =         6777655
55  meter
 Y    =        4467066
14  meter          E    =           
0003301
 Z    =        5095921
53                 I    =           51
46588
 XDOT =      -7184
536694                 Wp   =          205
53573
 YDOT =       2106
595840  meter/sec      RA   =          333
49953  deg
 ZDOT =      -1658
094091                 TA   =          260
49210
                                          MA   =          260
52941
                                          Ha   =            220
735  n
mi
                                          Hp   =            215
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         446474
29                 X    =           61369
25
 Y    =       14655728
80  feet           Y    =         4468169
90  meter
 Z    =       16718902
65                 Z    =         5096401
37
 XDOT =     -23571
314612                 XDOT =       -7199
504762
 YDOT =       6911
403674  feet/sec       YDOT =        2026
170007  meter/sec
 ZDOT =      -5439
941243                 ZDOT =       -1693
031553

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13294738
08                 X    =        -4052236
17
 Y    =       -6180758
02  feet           Y    =        -1883895
04  meter
 Z    =       16720035
92                 Z    =         5096266
95
 XDOT =       3765
293899                 XDOT =        1147
661580
 YDOT =     -23195
168670  feet/sec       YDOT =       -7069
887411  meter/sec
 ZDOT =      -5591
333970                 ZDOT =       -1704
238594


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   15334
53292939  
00016717  00000-0  10270-3 0  9038
2 25544  51
6423 333
8696 0008221 223
9605 136
0895 15
54351767 13922


Satellite: ISS
Catalog Number: 25544
Epoch time:      15334
53292939   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:       333
8696  deg
Eccentricity:     
0008221     
Arg of perigee:   223
9605  deg
Mean anomaly:     136
0895  deg
Mean motion:   15
54351767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1392
Checksum:              324


Coasting Arc #5 (Orbit 1406)
---------------------------------------

Vector Time (GMT): 2015/335/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1565712
05                 A    =         6780820
12  meter
 Y    =       -4995068
61  meter          E    =           
0008611
 Z    =       -4317016
31                 I    =           51
44850
 XDOT =       6766
656049                 Wp   =          167
07707
 YDOT =       -893
875311  meter/sec      RA   =          328
49036  deg
 ZDOT =       3481
550166                 TA   =          138
47797
                                          MA   =          138
41253
                                          Ha   =            220
576  n
mi
                                          Hp   =            216
161

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5136850
55                 X    =         1642422
27
 Y    =      -16388020
36  feet           Y    =        -4977130
70  meter
 Z    =      -14163439
35                 Z    =        -4309224
23
 XDOT =      22200
315123                 XDOT =        6759
236550
 YDOT =      -2932
661781  feet/sec       YDOT =        -818
247713  meter/sec
 ZDOT =      11422
408680                 ZDOT =        3514
403315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12588481
29                 X    =         3836969
10
 Y    =       11724615
82  feet           Y    =         3573662
90  meter
 Z    =      -14128728
94                 Z    =        -4306436
58
 XDOT =      -5941
401058                 XDOT =       -1810
939042
 YDOT =      20342
248047  feet/sec       YDOT =        6200
317205  meter/sec
 ZDOT =      11564
536248                 ZDOT =        3524
870648


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   15335
49731498  
00016717  00000-0  10270-3 0  9043
2 25544  51
6425 329
0605 0008170 228
1290 131
9166 15
54353741 14077


Satellite: ISS
Catalog Number: 25544
Epoch time:      15335
49731498   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:       329
0605  deg
Eccentricity:     
0008170     
Arg of perigee:   228
1290  deg
Mean anomaly:     131
9166  deg
Mean motion:   15
54353741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1407
Checksum:              304


Coasting Arc #6 (Orbit 1422)
---------------------------------------

Vector Time (GMT): 2015/336/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3024754
51                 A    =         6784607
58  meter
 Y    =        5251396
49  meter          E    =           
0009238
 Z    =        3036631
97                 I    =           51
43433
 XDOT =      -5865
738429                 Wp   =          134
10285
 YDOT =       -534
306041  meter/sec      RA   =          323
48923  deg
 ZDOT =      -4915
793736                 TA   =           10
94124
                                          MA   =           10
92117
                                          Ha   =            220
271  n
mi
                                          Hp   =            216
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9923735
29                 X    =        -3098002
99
 Y    =       17228991
09  feet           Y    =         5217162
05  meter
 Z    =        9962703
33                 Z    =         3021760
47
 XDOT =     -19244
548652                 XDOT =       -5835
448558
 YDOT =      -1752
972577  feet/sec       YDOT =        -599
731115  meter/sec
 ZDOT =     -16127
932204                 ZDOT =       -4944
214906

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11596498
40                 X    =        -3534612
71
 Y    =      -16190663
05  feet           Y    =        -4934914
10  meter
 Z    =        9897361
70                 Z    =         3016715
85
 XDOT =       8292
079038                 XDOT =        2527
425691
 YDOT =     -15879
232065  feet/sec       YDOT =       -4839
989933  meter/sec
 ZDOT =     -16250
609566                 ZDOT =       -4953
185796


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   15336
52597428  
00016717  00000-0  10270-3 0  9052
2 25544  51
6417 323
9299 0008126 232
5517 127
4897 15
54423881 14234


Satellite: ISS
Catalog Number: 25544
Epoch time:      15336
52597428   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:       323
9299  deg
Eccentricity:     
0008126     
Arg of perigee:   232
5517  deg
Mean anomaly:     127
4897  deg
Mean motion:   15
54423881  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1423
Checksum:              330


Coasting Arc #7 (Orbit 1437)
---------------------------------------

Vector Time (GMT): 2015/337/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4160758
25                 A    =         6787576
38  meter
 Y    =       -5174255
48  meter          E    =           
0002509
 Z    =       -1401470
46                 I    =           51
41914
 XDOT =       4571
920114                 Wp   =          328
91021
 YDOT =       2110
447994  meter/sec      RA   =          318
49760  deg
 ZDOT =       5779
009638                 TA   =           15
77091
                                          MA   =           15
76310
                                          Ha   =            220
101  n
mi
                                          Hp   =            216
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13650781
66                 X    =         4225116
66
 Y    =      -16975903
80  feet           Y    =        -5127367
26  meter
 Z    =       -4598000
19                 Z    =        -1381101
96
 XDOT =      14999
737908                 XDOT =        4519
908352
 YDOT =       6924
041975  feet/sec       YDOT =        2161
283301  meter/sec
 ZDOT =      18960
005374                 ZDOT =        5801
092970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10179550
14                 X    =         3102726
88
 Y    =       19279860
31  feet           Y    =         5876501
42  meter
 Z    =       -4508935
65                 Z    =        -1374323
59
 XDOT =     -10840
768792                 XDOT =       -3304
266328
 YDOT =      10182
125846  feet/sec       YDOT =        3103
511958  meter/sec
 ZDOT =      19054
972780                 ZDOT =        5807
955703


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   15337
49032623  
00016717  00000-0  10270-3 0  9061
2 25544  51
6413 319
1207 0008084 234
4024 125
6376 15
54454511 14385


Satellite: ISS
Catalog Number: 25544
Epoch time:      15337
49032623   =   yrday
fracday
Element set:     906
Inclination:       51
6413  deg
RA of node:       319
1207  deg
Eccentricity:     
0008084     
Arg of perigee:   234
4024  deg
Mean anomaly:     125
6376  deg
Mean motion:   15
54454511  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1438
Checksum:              290


Coasting Arc #8 (Orbit 1453)
---------------------------------------

Vector Time (GMT): 2015/338/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4891508
86                 A    =         6788284
25  meter
 Y    =        4676784
32  meter          E    =           
0012366
 Z    =        -410646
65                 I    =           51
39823
 XDOT =      -3052
703403                 Wp   =          177
26127
 YDOT =      -3716
035225  meter/sec      RA   =          313
50893  deg
 ZDOT =      -5977
896921                 TA   =            7
18372
                                          MA   =            7
16601
                                          Ha   =            219
778  n
mi
                                          Hp   =            216
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16048257
41                 X    =        -4941447
47
 Y    =       15343780
56  feet           Y    =         4621805
02  meter
 Z    =       -1347265
90                 Z    =         -434530
05
 XDOT =     -10015
431111                 XDOT =       -2981
884289
 YDOT =     -12191
716617  feet/sec       YDOT =       -3749
776496  meter/sec
 ZDOT =     -19612
522706                 ZDOT =       -5992
554528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8103334
76                 X    =        -2469896
43
 Y    =      -20664527
28  feet           Y    =        -6298547
92  meter
 Z    =       -1451403
14                 Z    =         -442387
68
 XDOT =      13528
861410                 XDOT =        4123
596958
 YDOT =      -3927
449855  feet/sec       YDOT =       -1197
086716  meter/sec
 ZDOT =     -19675
080220                 ZDOT =       -5996
964451


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   15338
51894958  
00016717  00000-0  10270-3 0  9073
2 25544  51
6412 313
9895 0008035 239
8860 120
1497 15
54460498 14545


Satellite: ISS
Catalog Number: 25544
Epoch time:      15338
51894958   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       313
9895  deg
Eccentricity:     
0008035     
Arg of perigee:   239
8860  deg
Mean anomaly:     120
1497  deg
Mean motion:   15
54460498  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1454
Checksum:              342


Coasting Arc #9 (Orbit 1469)
---------------------------------------

Vector Time (GMT): 2015/339/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5212508
76                 A    =         6786100
64  meter
 Y    =       -3758068
14  meter          E    =           
0005860
 Z    =        2174819
99                 I    =           51
37003
 XDOT =       1452
665000                 Wp   =           83
00505
 YDOT =       5181
657617  meter/sec      RA   =          308
51760  deg
 ZDOT =       5460
193811                 TA   =          301
22306
                                          MA   =          301
28047
                                          Ha   =            219
636  n
mi
                                          Hp   =            216
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17101406
71                 X    =         5243580
43
 Y    =      -12329619
87  feet           Y    =        -3699604
73  meter
 Z    =        7135236
19                 Z    =         2200217
01
 XDOT =       4765
961286                 XDOT =        1368
090620
 YDOT =      17000
189032  feet/sec       YDOT =        5197
429285  meter/sec
 ZDOT =      17914
021690                 ZDOT =        5467
045326

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5279810
59                 X    =         1609286
27
 Y    =       20371854
06  feet           Y    =         6209341
12  meter
 Z    =        7245715
66                 Z    =         2208494
13
 XDOT =     -16043
466244                 XDOT =       -4890
048511
 YDOT =      -2237
434080  feet/sec       YDOT =        -681
969908  meter/sec
 ZDOT =      17942
560713                 ZDOT =        5468
892505


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   15339
54755187  
00016717  00000-0  10270-3 0  9088
2 25544  51
6409 308
8592 0008245 242
7896 117
2417 15
54527912 14705


Satellite: ISS
Catalog Number: 25544
Epoch time:      15339
54755187   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       308
8592  deg
Eccentricity:     
0008245     
Arg of perigee:   242
7896  deg
Mean anomaly:     117
2417  deg
Mean motion:   15
54527912  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1470
Checksum:              337


Coasting Arc #10 (Orbit 1484)
---------------------------------------

Vector Time (GMT): 2015/340/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5146168
50                 A    =         6782312
53  meter
 Y    =        2418366
43  meter          E    =           
0002566
 Z    =       -3693863
27                 I    =           51
33833
 XDOT =         92
446574                 Wp   =          222
27893
 YDOT =      -6355
336163  meter/sec      RA   =          303
51467  deg
 ZDOT =      -4289
745604                 TA   =            1
96113
                                          MA   =            1
96012
                                          Ha   =            219
215  n
mi
                                          Hp   =            216
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16883754
91                 X    =        -5154885
16
 Y    =        7934273
06  feet           Y    =         2360769
94  meter
 Z    =      -12118973
99                 Z    =        -3718883
78
 XDOT =        303
302408                 XDOT =         184
344866
 YDOT =     -20850
840429  feet/sec       YDOT =       -6353
788415  meter/sec
 ZDOT =     -14073
968517                 ZDOT =       -4289
073467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1594683
58                 X    =         -486059
55
 Y    =      -18515600
18  feet           Y    =        -5643554
94  meter
 Z    =      -12227548
14                 Z    =        -3726956
67
 XDOT =      18064
126341                 XDOT =        5505
945709
 YDOT =       7735
496043  feet/sec       YDOT =        2357
779194  meter/sec
 ZDOT =     -14069
773351                 ZDOT =       -4288
466917


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   15340
51185278  
00016717  00000-0  10270-3 0  9096
2 25544  51
6411 304
0484 0008020 247
6052 112
4251 15
54514395 14855


Satellite: ISS
Catalog Number: 25544
Epoch time:      15340
51185278   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:       304
0484  deg
Eccentricity:     
0008020     
Arg of perigee:   247
6052  deg
Mean anomaly:     112
4251  deg
Mean motion:   15
54514395  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1485
Checksum:              285


Coasting Arc #11 (Orbit 1500)
---------------------------------------

Vector Time (GMT): 2015/341/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4761476
31                 A    =         6778301
54  meter
 Y    =        -769604
02  meter          E    =           
0006324
 Z    =        4766220
42                 I    =           51
30877
 XDOT =      -1465
488612                 Wp   =          191
82000
 YDOT =       7061
094209  meter/sec      RA   =          298
49958  deg
 ZDOT =       2598
721684                 TA   =          232
40789
                                          MA   =          232
46532
                                          Ha   =            219
090  n
mi
                                          Hp   =            217
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15621641
44                 X    =         4746575
49
 Y    =       -2524947
56  feet           Y    =         -716441
55  meter
 Z    =       15637206
11                 Z    =         4789314
85
 XDOT =      -4808
033503                 XDOT =       -1556
962370
 YDOT =      23166
319584  feet/sec       YDOT =        7044
194587  meter/sec
 ZDOT =       8525
989776                 ZDOT =        2591
380615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2764905
15                 X    =         -842743
09
 Y    =       15480036
07  feet           Y    =         4718314
99  meter
 Z    =       15737122
97                 Z    =         4796675
08
 XDOT =     -19116
085231                 XDOT =       -5826
582778
 YDOT =     -12066
357525  feet/sec       YDOT =       -3677
825774  meter/sec
 ZDOT =       8492
850270                 ZDOT =        2588
620762


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   15341
54041892  
00016717  00000-0  10270-3 0  9105
2 25544  51
6413 298
9179 0008217 251
6895 108
3364 15
54566226 15015


Satellite: ISS
Catalog Number: 25544
Epoch time:      15341
54041892   =   yrday
fracday
Element set:     910
Inclination:       51
6413  deg
RA of node:       298
9179  deg
Eccentricity:     
0008217     
Arg of perigee:   251
6895  deg
Mean anomaly:     108
3364  deg
Mean motion:   15
54566226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1501
Checksum:              314


Coasting Arc #12 (Orbit 1515)
---------------------------------------

Vector Time (GMT): 2015/342/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4132990
12                 A    =         6776195
24  meter
 Y    =       -1079248
51  meter          E    =           
0006914
 Z    =       -5266147
27                 I    =           51
28749
 XDOT =       2612
215976                 Wp   =           97
49290
 YDOT =      -7182
250663  meter/sec      RA   =          293
47223  deg
 ZDOT =       -579
730485                 TA   =          166
95330
                                          MA   =          166
93541
                                          Ha   =            218
757  n
mi
                                          Hp   =            217
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13559678
86                 X    =        -4095033
18
 Y    =       -3540841
58  feet           Y    =        -1125253
82  meter
 Z    =      -17277386
06                 Z    =        -5286132
69
 XDOT =       8570
262389                 XDOT =        2695
151669
 YDOT =     -23563
814511  feet/sec       YDOT =       -7152
575387  meter/sec
 ZDOT =      -1902
002905                 ZDOT =        -566
839612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7601537
15                 X    =         2316948
52
 Y    =      -11646287
55  feet           Y    =        -3549788
44  meter
 Z    =      -17363500
17                 Z    =        -5292394
85
 XDOT =      18807
670434                 XDOT =        5732
577948
 YDOT =      15018
800927  feet/sec       YDOT =        4577
730523  meter/sec
 ZDOT =      -1844
872020                 ZDOT =        -562
316992


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   15342
50468425  
00016717  00000-0  10270-3 0  9118
2 25544  51
6416 294
1068 0008088 255
4414 104
5842 15
54561235 15168


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
50468425   =   yrday
fracday
Element set:     911
Inclination:       51
6416  deg
RA of node:       294
1068  deg
Eccentricity:     
0008088     
Arg of perigee:   255
4414  deg
Mean anomaly:     104
5842  deg
Mean motion:   15
54561235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1516
Checksum:              300


Coasting Arc #13 (Orbit 1531)
---------------------------------------

Vector Time (GMT): 2015/343/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3348673
90                 A    =         6776791
71  meter
 Y    =        2926856
70  meter          E    =           
0004205
 Z    =        5116971
23                 I    =           51
27846
 XDOT =      -3498
308765                 Wp   =          287
03827
 YDOT =       6651
043778  meter/sec      RA   =          288
44302  deg
 ZDOT =      -1514
773810                 TA   =          177
63335
                                          MA   =          177
63136
                                          Ha   =            218
542  n
mi
                                          Hp   =            217
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10986462
93                 X    =         3290839
52
 Y    =        9602548
24  feet           Y    =         2963980
04  meter
 Z    =       16787963
34                 Z    =         5133098
39
 XDOT =     -11477
390960                 XDOT =       -3565
064058
 YDOT =      21821
009771  feet/sec       YDOT =        6611
550239  meter/sec
 ZDOT =      -4969
730347                 ZDOT =       -1531
929809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12416556
40                 X    =        -3784566
39
 Y    =        7511074
30  feet           Y    =         2289375
45  meter
 Z    =       16857043
14                 Z    =         5138026
75
 XDOT =     -16854
713550                 XDOT =       -5137
316690
 YDOT =     -16538
390392  feet/sec       YDOT =       -5040
901392  meter/sec
 ZDOT =      -5045
173346                 ZDOT =       -1537
768836


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   15343
53321499  
00016717  00000-0  10270-3 0  9122
2 25544  51
6422 288
9763 0008078 259
3664 100
6580 15
54589238 15324


Satellite: ISS
Catalog Number: 25544
Epoch time:      15343
53321499   =   yrday
fracday
Element set:     912
Inclination:       51
6422  deg
RA of node:       288
9763  deg
Eccentricity:     
0008078     
Arg of perigee:   259
3664  deg
Mean anomaly:     100
6580  deg
Mean motion:   15
54589238  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1532
Checksum:              330


Coasting Arc #14 (Orbit 1546)
---------------------------------------

Vector Time (GMT): 2015/344/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2473731
07                 A    =         6779903
80  meter
 Y    =       -4594628
47  meter          E    =           
0004008
 Z    =       -4331158
28                 I    =           51
28001
 XDOT =       4134
238685                 Wp   =          178
78141
 YDOT =      -5466
359581  meter/sec      RA   =          283
41783  deg
 ZDOT =       3433
745720                 TA   =          126
27499
                                          MA   =          126
23796
                                          Ha   =            218
252  n
mi
                                          Hp   =            217
343

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8115915
59                 X    =        -2401129
57
 Y    =      -15074240
39  feet           Y    =        -4621885
04  meter
 Z    =      -14209836
89                 Z    =        -4342999
39
 XDOT =      13563
775212                 XDOT =        4178
377549
 YDOT =     -17934
250593  feet/sec       YDOT =       -5419
881302  meter/sec
 ZDOT =      11265
569946                 ZDOT =        3453
936010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16728222
81                 X    =         5098762
31
 Y    =       -3440510
00  feet           Y    =        -1048667
45  meter
 Z    =      -14260074
55                 Z    =        -4346470
72
 XDOT =      13142
081093                 XDOT =        4005
706317
 YDOT =      16786
941983  feet/sec       YDOT =        5116
659916  meter/sec
 ZDOT =      11353
880360                 ZDOT =        3460
662734


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   15344
49744453  
00016717  00000-0  10270-3 0  9138
2 25544  51
6423 284
1656 0008140 263
2688  96
7538 15
54614674 15471


Satellite: ISS
Catalog Number: 25544
Epoch time:      15344
49744453   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:       284
1656  deg
Eccentricity:     
0008140     
Arg of perigee:   263
2688  deg
Mean anomaly:      96
7538  deg
Mean motion:   15
54614674  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1547
Checksum:              333


Coasting Arc #15 (Orbit 1562)
---------------------------------------

Vector Time (GMT): 2015/345/11:42:12
734
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1558603
64                 A    =         6783955
31  meter
 Y    =        5880110
18  meter          E    =           
0005327
 Z    =        2996060
93                 I    =           51
28826
 XDOT =      -4544
766594                 Wp   =          111
67953
 YDOT =       3719
825152  meter/sec      RA   =          278
40449  deg
 ZDOT =      -4931
166840                 TA   =           33
83235
                                          MA   =           33
79837
                                          Ha   =            217
500  n
mi
                                          Hp   =            217
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5113529
02                 X    =         1478181
11
 Y    =       19291700
07  feet           Y    =         5897089
55  meter
 Z    =        9829596
22                 Z    =         3003437
62
 XDOT =     -14910
651555                 XDOT =       -4562
070857
 YDOT =      12204
150761  feet/sec       YDOT =        3668
906300  meter/sec
 ZDOT =     -16178
368898                 ZDOT =       -4953
286285

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19941046
61                 X    =        -6078031
01
 Y    =        -260685
80  feet           Y    =          -79457
03  meter
 Z    =        9860300
98                 Z    =         3005419
74
 XDOT =      -7845
694549                 XDOT =       -2391
367699
 YDOT =     -16064
058227  feet/sec       YDOT =       -4896
324948  meter/sec
 ZDOT =     -16274
665457                 ZDOT =       -4960
518031


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   15345
52593850  
00016717  00000-0  10270-3 0  9147
2 25544  51
6431 279
0348 0008108 267
2352  92
7873 15
54658858 15635


Satellite: ISS
Catalog Number: 25544
Epoch time:      15345
52593850   =   yrday
fracday
Element set:     914
Inclination:       51
6431  deg
RA of node:       279
0348  deg
Eccentricity:     
0008108     
Arg of perigee:   267
2352  deg
Mean anomaly:      92
7873  deg
Mean motion:   15
54658858  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1563
Checksum:              336
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