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

 
Date: October 7th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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


288/01:13:55 615 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 212 3

288/09:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 212 2

290/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 212 1

Coasting Arc #1 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2016/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3040680
30                 A    =         6777620
73  meter
 Y    =        2957468
22  meter          E    =           
0019913
 Z    =       -5302820
71                 I    =           51
34739
 XDOT =      -5279
326362                 Wp   =           73
54482
 YDOT =      -5541
821127  meter/sec      RA   =          226
73808  deg
 ZDOT =        -58
207808                 TA   =          195
86598
                                          MA   =          195
92846
                                          Ha   =            223
256  n
mi
                                          Hp   =            212
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9975985
24                 X    =        -3047766
18
 Y    =        9702979
72  feet           Y    =         2923425
15  meter
 Z    =      -17397705
74                 Z    =        -5317609
35
 XDOT =     -17320
624548                 XDOT =       -5216
681179
 YDOT =     -18181
827844  feet/sec       YDOT =       -5600
507831  meter/sec
 ZDOT =       -190
970498                 ZDOT =         -83
701215

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7277009
61                 X    =         2218032
53
 Y    =      -11766266
75  feet           Y    =        -3586358
11  meter
 Z    =      -17462770
68                 Z    =        -5322652
50
 XDOT =      20283
502017                 XDOT =        6182
411415
 YDOT =      13017
967013  feet/sec       YDOT =        3967
876346  meter/sec
 ZDOT =       -301
468186                 ZDOT =         -91
887503


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   16279
51625692  
00016717  00000-0  10270-3 0  9008
2 25544  51
6414 227
7106 0006964  37
1260 323
0373 15
54040264 22143


Satellite: ISS
Catalog Number: 25544
Epoch time:      16279
51625692   =   yrday
fracday
Element set:     900
Inclination:       51
6414  deg
RA of node:       227
7106  deg
Eccentricity:     
0006964     
Arg of perigee:    37
1260  deg
Mean anomaly:     323
0373  deg
Mean motion:   15
54040264  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2214
Checksum:              285


Coasting Arc #2 (Orbit 2229)
---------------------------------------

Vector Time (GMT): 2016/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4233550
91                 A    =         6778655
82  meter
 Y    =       -1616213
32  meter          E    =           
0012392
 Z    =        5035732
81                 I    =           51
37355
 XDOT =       4473
688095                 Wp   =           47
59549
 YDOT =       5956
676030  meter/sec      RA   =          221
72109  deg
 ZDOT =      -1838
143286                 TA   =           60
32327
                                          MA   =           60
19996
                                          Ha   =            223
208  n
mi
                                          Hp   =            212
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13889602
73                 X    =         4226847
32
 Y    =       -5302537
14  feet           Y    =        -1568907
96  meter
 Z    =       16521433
11                 Z    =         5056282
56
 XDOT =      14677
454381                 XDOT =        4415
675596
 YDOT =      19542
900361  feet/sec       YDOT =        6006
379286  meter/sec
 ZDOT =      -6030
653827                 ZDOT =       -1816
552270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11982448
67                 X    =        -3652250
36
 Y    =        8629945
52  feet           Y    =         2630407
39  meter
 Z    =       16611462
32                 Z    =         5063173
71
 XDOT =     -18570
555351                 XDOT =       -5660
305271
 YDOT =     -14286
561278  feet/sec       YDOT =       -4354
543878  meter/sec
 ZDOT =      -5937
253883                 ZDOT =       -1809
674983


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   16280
54514032  
00016717  00000-0  10270-3 0  9019
2 25544  51
6411 222
5832 0007047  41
0883 319
0799 15
54052873 22301


Satellite: ISS
Catalog Number: 25544
Epoch time:      16280
54514032   =   yrday
fracday
Element set:     901
Inclination:       51
6411  deg
RA of node:       222
5832  deg
Eccentricity:     
0007047     
Arg of perigee:    41
0883  deg
Mean anomaly:     319
0799  deg
Mean motion:   15
54052873  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2230
Checksum:              284


Coasting Arc #3 (Orbit 2244)
---------------------------------------

Vector Time (GMT): 2016/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5248755
60                 A    =         6781616
98  meter
 Y    =         356269
15  meter          E    =           
0013015
 Z    =       -4289438
96                 I    =           51
40812
 XDOT =      -3278
151032                 Wp   =           81
53311
 YDOT =      -5956
266637  meter/sec      RA   =          216
71122  deg
 ZDOT =       3527
656489                 TA   =          224
51812
                                          MA   =          224
62276
                                          Ha   =            223
283  n
mi
                                          Hp   =            212
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17220326
77                 X    =        -5231512
82
 Y    =        1168862
04  feet           Y    =          297670
13  meter
 Z    =      -14072962
46                 Z    =        -4314894
64
 XDOT =     -10755
088689                 XDOT =       -3228
439007
 YDOT =     -19541
557207  feet/sec       YDOT =       -5992
646895  meter/sec
 ZDOT =      11573
676145                 ZDOT =        3511
853002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16172905
98                 X    =         4929501
74
 Y    =       -5761822
34  feet           Y    =        -1756203
45  meter
 Z    =      -14184240
56                 Z    =        -4323356
52
 XDOT =      15295
911044                 XDOT =        4662
193686
 YDOT =      14698
999609  feet/sec       YDOT =        4480
255081  meter/sec
 ZDOT =      11505
547912                 ZDOT =        3506
891003


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   16281
50971171  
00016717  00000-0  10270-3 0  9028
2 25544  51
6409 217
7759 0006949  44
1688 316
0018 15
54059183 22457


Satellite: ISS
Catalog Number: 25544
Epoch time:      16281
50971171   =   yrday
fracday
Element set:     902
Inclination:       51
6409  deg
RA of node:       217
7759  deg
Eccentricity:     
0006949     
Arg of perigee:    44
1688  deg
Mean anomaly:     316
0018  deg
Mean motion:   15
54059183  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2245
Checksum:              319


Coasting Arc #4 (Orbit 2260)
---------------------------------------

Vector Time (GMT): 2016/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5992600
30                 A    =         6785370
84  meter
 Y    =         837102
99  meter          E    =           
0018429
 Z    =        3059164
86                 I    =           51
44817
 XDOT =       1723
589720                 Wp   =           79
32525
 YDOT =       5649
340848  meter/sec      RA   =          211
71206  deg
 ZDOT =      -4893
741293                 TA   =           65
43905
                                          MA   =           65
24709
                                          Ha   =            223
282  n
mi
                                          Hp   =            212
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19660762
15                 X    =         5967933
92
 Y    =        2746400
89  feet           Y    =          903978
57  meter
 Z    =       10036630
11                 Z    =         3088215
82
 XDOT =       5654
821917                 XDOT =        1684
061254
 YDOT =      18534
582836  feet/sec       YDOT =        5668
393819  meter/sec
 ZDOT =     -16055
581671                 ZDOT =       -4885
464829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19558613
64                 X    =        -5961465
44
 Y    =        2997863
43  feet           Y    =          913748
77  meter
 Z    =       10163448
11                 Z    =         3097818
98
 XDOT =     -10621
488851                 XDOT =       -3237
429802
 YDOT =     -14671
349609  feet/sec       YDOT =       -4471
827361  meter/sec
 ZDOT =     -16020
284009                 ZDOT =       -4882
982566


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   16282
53857863  
00016717  00000-0  10270-3 0  9034
2 25544  51
6417 212
6474 0007000  47
4683 312
7059 15
54091560 22615


Satellite: ISS
Catalog Number: 25544
Epoch time:      16282
53857863   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:       212
6474  deg
Eccentricity:     
0007000     
Arg of perigee:    47
4683  deg
Mean anomaly:     312
7059  deg
Mean motion:   15
54091560  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2261
Checksum:              303


Coasting Arc #5 (Orbit 2275)
---------------------------------------

Vector Time (GMT): 2016/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6349608
65                 A    =         6788355
51  meter
 Y    =       -1806075
48  meter          E    =           
0014925
 Z    =       -1560974
13                 I    =           51
48532
 XDOT =         47
574732                 Wp   =           44
43438
 YDOT =      -5087
913703  meter/sec      RA   =          206
72478  deg
 ZDOT =       5736
981596                 TA   =          298
46245
                                          MA   =          298
61272
                                          Ha   =            223
352  n
mi
                                          Hp   =            212
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20832049
39                 X    =        -6321358
12
 Y    =       -5925444
48  feet           Y    =        -1876923
22  meter
 Z    =       -5121306
19                 Z    =        -1591750
51
 XDOT =        156
085079                 XDOT =          76
597458
 YDOT =     -16692
630258  feet/sec       YDOT =       -5087
218994  meter/sec
 ZDOT =      18822
118097                 ZDOT =        5737
283570

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21615789
83                 X    =         6588492
74
 Y    =        -670784
64  feet           Y    =         -204455
16  meter
 Z    =       -5255533
18                 Z    =        -1601886
51
 XDOT =       4987
741244                 XDOT =        1520
263531
 YDOT =      14336
684310  feet/sec       YDOT =        4369
821378  meter/sec
 ZDOT =      18824
215082                 ZDOT =        5737
620757


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   16283
50313263  
00016717  00000-0  10270-3 0  9044
2 25544  51
6410 207
8400 0007050  51
0654 309
1127 15
54087584 22760


Satellite: ISS
Catalog Number: 25544
Epoch time:      16283
50313263   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       207
8400  deg
Eccentricity:     
0007050     
Arg of perigee:    51
0654  deg
Mean anomaly:     309
1127  deg
Mean motion:   15
54087584  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2276
Checksum:              278


Coasting Arc #6 (Orbit 2291)
---------------------------------------

Vector Time (GMT): 2016/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6253491
44                 A    =         6789393
87  meter
 Y    =        2631611
62  meter          E    =           
0014739
 Z    =        -160455
77                 I    =           51
51899
 XDOT =      -1971
388186                 Wp   =          108
15139
 YDOT =       4346
821314  meter/sec      RA   =          201
74529  deg
 ZDOT =      -5998
104929                 TA   =           73
57937
                                          MA   =           73
41741
                                          Ha   =            223
417  n
mi
                                          Hp   =            212
471

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20516704
19                 X    =         6224378
74
 Y    =        8633896
40  feet           Y    =         2701379
57  meter
 Z    =        -526429
70                 Z    =         -130148
54
 XDOT =      -6467
809009                 XDOT =       -1990
712464
 YDOT =      14261
224784  feet/sec       YDOT =        4324
667385  meter/sec
 ZDOT =     -19678
821947                 ZDOT =       -6007
728818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22203640
52                 X    =        -6767669
63
 Y    =       -1612226
27  feet           Y    =         -491406
57  meter
 Z    =        -394360
28                 Z    =         -120201
01
 XDOT =       1325
346178                 XDOT =         403
965515
 YDOT =     -13919
538373  feet/sec       YDOT =       -4242
675296  meter/sec
 ZDOT =     -19721
545970                 ZDOT =       -6011
127212


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   16284
53198188  
00016717  00000-0  10270-3 0  9056
2 25544  51
6419 202
7115 0006963  55
2632 304
9175 15
54102952 22921


Satellite: ISS
Catalog Number: 25544
Epoch time:      16284
53198188   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:       202
7115  deg
Eccentricity:     
0006963     
Arg of perigee:    55
2632  deg
Mean anomaly:     304
9175  deg
Mean motion:   15
54102952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2292
Checksum:              311


Coasting Arc #7 (Orbit 2307)
---------------------------------------

Vector Time (GMT): 2016/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5683820
15                 A    =         6788034
47  meter
 Y    =       -3216274
48  meter          E    =           
0020894
 Z    =        1813085
58                 I    =           51
54497
 XDOT =       3813
472097                 Wp   =           63
40987
 YDOT =      -3533
507664  meter/sec      RA   =          196
76696  deg
 ZDOT =       5645
486536                 TA   =          316
56459
                                          MA   =          316
72901
                                          Ha   =            223
443  n
mi
                                          Hp   =            212
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18647703
91                 X    =        -5656239
77
 Y    =      -10552081
61  feet           Y    =        -3279680
38  meter
 Z    =        5948443
50                 Z    =         1785542
09
 XDOT =      12511
391393                 XDOT =        3825
277691
 YDOT =     -11592
872912  feet/sec       YDOT =       -3490
796300  meter/sec
 ZDOT =      18521
937453                 ZDOT =        5664
040594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21145983
91                 X    =         6445295
90
 Y    =        3652796
91  feet           Y    =         1113372
50  meter
 Z    =        5828525
24                 Z    =         1776534
49
 XDOT =      -7504
886336                 XDOT =       -2287
489355
 YDOT =      13541
324742  feet/sec       YDOT =        4127
395781  meter/sec
 ZDOT =      18603
576276                 ZDOT =        5670
370049


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   16285
56082124  
00016717  00000-0  10270-3 0  9063
2 25544  51
6422 197
5831 0006977  58
4122 301
7711 15
54116001 23084


Satellite: ISS
Catalog Number: 25544
Epoch time:      16285
56082124   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       197
5831  deg
Eccentricity:     
0006977     
Arg of perigee:    58
4122  deg
Mean anomaly:     301
7711  deg
Mean motion:   15
54116001  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2308
Checksum:              291


Coasting Arc #8 (Orbit 2322)
---------------------------------------

Vector Time (GMT): 2016/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4637762
21                 A    =         6784647
37  meter
 Y    =        3671438
49  meter          E    =           
0011189
 Z    =       -3335540
92                 I    =           51
56650
 XDOT =      -5454
576085                 Wp   =           75
43587
 YDOT =       2652
038846  meter/sec      RA   =          191
78433  deg
 ZDOT =      -4675
390365                 TA   =          143
39718
                                          MA   =          143
32068
                                          Ha   =            223
419  n
mi
                                          Hp   =            212
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15215755
29                 X    =         4612565
33
 Y    =       12045401
86  feet           Y    =         3723159
79  meter
 Z    =      -10943375
72                 Z    =        -3313073
26
 XDOT =     -17895
590831                 XDOT =       -5461
115229
 YDOT =       8700
914849  feet/sec       YDOT =        2591
005017  meter/sec
 ZDOT =     -15339
207234                 ZDOT =       -4701
903746

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18550479
19                 X    =        -5654186
06
 Y    =       -5883782
38  feet           Y    =        -1793376
87  meter
 Z    =      -10845700
25                 Z    =        -3305769
44
 XDOT =      13158
648871                 XDOT =        4010
756176
 YDOT =     -13060
839441  feet/sec       YDOT =       -3980
943862  meter/sec
 ZDOT =     -15455
516388                 ZDOT =       -4710
841395


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   16286
52534769  
00016717  00000-0  10270-3 0  9078
2 25544  51
6435 192
7752 0006987  61
7421 298
4436 15
54146693 23230


Satellite: ISS
Catalog Number: 25544
Epoch time:      16286
52534769   =   yrday
fracday
Element set:     907
Inclination:       51
6435  deg
RA of node:       192
7752  deg
Eccentricity:     
0006987     
Arg of perigee:    61
7421  deg
Mean anomaly:     298
4436  deg
Mean motion:   15
54146693  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2323
Checksum:              342


Coasting Arc #9 (Orbit 2338)
---------------------------------------

Vector Time (GMT): 2016/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3213334
69                 A    =         6780871
50  meter
 Y    =       -3949349
10  meter          E    =           
0014983
 Z    =        4465867
64                 I    =           51
58518
 XDOT =       6722
924759                 Wp   =           91
94272
 YDOT =      -1790
102729  meter/sec      RA   =          186
79391  deg
 ZDOT =       3244
397461                 TA   =          325
36541
                                          MA   =          325
46290
                                          Ha   =            223
525  n
mi
                                          Hp   =            212
234

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10542436
63                 X    =        -3190626
74
 Y    =      -12957182
08  feet           Y    =        -3985155
22  meter
 Z    =       14651796
71                 Z    =         4450313
55
 XDOT =      22056
839759                 XDOT =        6726
682414
 YDOT =      -5873
040451  feet/sec       YDOT =       -1714
901045  meter/sec
 ZDOT =      10644
348624                 ZDOT =        3277
065468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14662782
90                 X    =         4469216
23
 Y    =        8124369
88  feet           Y    =         2476307
94  meter
 Z    =       14584378
50                 Z    =         4445318
57
 XDOT =     -17683
828399                 XDOT =       -5390
030896
 YDOT =      12492
040138  feet/sec       YDOT =        3807
573834  meter/sec
 ZDOT =      10787
448579                 ZDOT =        3288
014327


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   16287
55416893  
00016717  00000-0  10270-3 0  9080
2 25544  51
6431 187
6470 0007018  66
0239 294
1648 15
54147526 23398


Satellite: ISS
Catalog Number: 25544
Epoch time:      16287
55416893   =   yrday
fracday
Element set:     908
Inclination:       51
6431  deg
RA of node:       187
6470  deg
Eccentricity:     
0007018     
Arg of perigee:    66
0239  deg
Mean anomaly:     294
1648  deg
Mean motion:   15
54147526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2339
Checksum:              332


Coasting Arc #10 (Orbit 2346)
---------------------------------------

Vector Time (GMT): 2016/288/01:13:55
615
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         396282
96                 A    =         6777490
11  meter
 Y    =        4235863
78  meter          E    =           
0021151
 Z    =       -5294235
47                 I    =           51
59039
 XDOT =      -7628
173640                 Wp   =           80
59357
 YDOT =        -51
281043  meter/sec      RA   =          184
02454  deg
 ZDOT =       -610
722101                 TA   =          183
55351
                                          MA   =          183
56855
                                          Ha   =            223
368  n
mi
                                          Hp   =            212
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1300140
95                 X    =          374604
46
 Y    =       13897190
87  feet           Y    =         4240173
36  meter
 Z    =      -17369538
94                 Z    =        -5292363
62
 XDOT =     -25026
816403                 XDOT =       -7624
066592
 YDOT =       -168
244893  feet/sec       YDOT =        -136
561519  meter/sec
 ZDOT =      -2003
681433                 ZDOT =        -647
768370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10123588
15                 X    =         3085669
67
 Y    =        9622765
68  feet           Y    =         2933018
98  meter
 Z    =      -17361984
54                 Z    =        -5291932
89
 XDOT =     -18386
164485                 XDOT =       -5604
102935
 YDOT =      15428
031845  feet/sec       YDOT =        4702
464106  meter/sec
 ZDOT =      -2165
658190                 ZDOT =        -660
092616


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   16288
06857481  
00016717  00000-0  10270-3 0  9090
2 25544  51
6419 185
0812 0006666  69
6873 290
4996 15
54134326 23475


Satellite: ISS
Catalog Number: 25544
Epoch time:      16288
06857481   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:       185
0812  deg
Eccentricity:     
0006666     
Arg of perigee:    69
6873  deg
Mean anomaly:     290
4996  deg
Mean motion:   15
54134326  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2347
Checksum:              349


Coasting Arc #11 (Orbit 2352)
---------------------------------------

Vector Time (GMT): 2016/288/09:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 878052
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2612439
73                 A    =         6779214
18  meter
 Y    =       -3945793
44  meter          E    =           
0012544
 Z    =        4843917
11                 I    =           51
60805
 XDOT =       7079
839925                 Wp   =           95
61947
 YDOT =      -1664
189395  meter/sec      RA   =          182
29252  deg
 ZDOT =       2456
026443                 TA   =          330
25233
                                          MA   =          330
32359
                                          Ha   =            223
359  n
mi
                                          Hp   =            212
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8570996
49                 X    =        -2591652
72
 Y    =      -12945516
55  feet           Y    =        -3974890
62  meter
 Z    =       15892116
51                 Z    =         4831277
36
 XDOT =      23227
821275                 XDOT =        7085
992624
 YDOT =      -5459
938961  feet/sec       YDOT =       -1584
983142  meter/sec
 ZDOT =       8057
829538                 ZDOT =        2490
434212

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5574416
42                 X    =         1699082
13
 Y    =       14550233
58  feet           Y    =         4434911
19  meter
 Z    =       15837434
49                 Z    =         4827250
03
 XDOT =     -22747
901383                 XDOT =       -6933
560342
 YDOT =       -243
545780  feet/sec       YDOT =         -74
232754  meter/sec
 ZDOT =       8208
529253                 ZDOT =        2501
959716


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   16288
45437815  
00016717  00000-0  10270-3 0  9100
2 25544  51
6420 183
1594 0006735  69
0120 291
1752 15
54198156 23535


Satellite: ISS
Catalog Number: 25544
Epoch time:      16288
45437815   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:       183
1594  deg
Eccentricity:     
0006735     
Arg of perigee:    69
0120  deg
Mean anomaly:     291
1752  deg
Mean motion:   15
54198156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2353
Checksum:              309


Coasting Arc #12 (Orbit 2367)
---------------------------------------

Vector Time (GMT): 2016/289/09:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 878052
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         831075
18                 A    =         6777329
77  meter
 Y    =        4162579
14  meter          E    =           
0021514
 Z    =       -5302072
81                 I    =           51
63440
 XDOT =      -7589
880923                 Wp   =           81
38165
 YDOT =        801
878999  meter/sec      RA   =          177
29248  deg
 ZDOT =       -558
930846                 TA   =          183
26627
                                          MA   =          183
28034
                                          Ha   =            223
414  n
mi
                                          Hp   =            212
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2726624
62                 X    =          810222
09
 Y    =       13656755
71  feet           Y    =         4171755
50  meter
 Z    =      -17395252
00                 Z    =        -5298086
76
 XDOT =     -24901
184130                 XDOT =       -7595
568539
 YDOT =       2630
836612  feet/sec       YDOT =         716
971982  meter/sec
 ZDOT =      -1833
762619                 ZDOT =        -595
815234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          32084
25                 X    =            9779
28
 Y    =      -13947222
41  feet           Y    =        -4251113
39  meter
 Z    =      -17378440
89                 Z    =        -5296948
78
 XDOT =      23880
317568                 XDOT =        7278
720795
 YDOT =       2545
882330  feet/sec       YDOT =         775
984934  meter/sec
 ZDOT =      -1995
177781                 ZDOT =        -608
130188


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   16289
41888391  
00016717  00000-0  10270-3 0  9117
2 25544  51
6425 178
3508 0006965  71
7302 288
4609 15
54181908 23681


Satellite: ISS
Catalog Number: 25544
Epoch time:      16289
41888391   =   yrday
fracday
Element set:     911
Inclination:       51
6425  deg
RA of node:       178
3508  deg
Eccentricity:     
0006965     
Arg of perigee:    71
7302  deg
Mean anomaly:     288
4609  deg
Mean motion:   15
54181908  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2368
Checksum:              342


Coasting Arc #13 (Orbit 2383)
---------------------------------------

Vector Time (GMT): 2016/290/09:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 878052
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1017645
08                 A    =         6777709
81  meter
 Y    =       -4258973
91  meter          E    =           
0011097
 Z    =        5165302
96                 I    =           51
66754
 XDOT =       7546
209190                 Wp   =           67
53744
 YDOT =         96
474842  meter/sec      RA   =          172
29430  deg
 ZDOT =      -1400
623711                 TA   =           35
95139
                                          MA   =           35
87678
                                          Ha   =            223
328  n
mi
                                          Hp   =            212
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3338730
56                 X    =         1040102
95
 Y    =      -13973011
51  feet           Y    =        -4247467
76  meter
 Z    =       16946532
03                 Z    =         5170301
57
 XDOT =      24757
904166                 XDOT =        7551
373320
 YDOT =        316
518509  feet/sec       YDOT =         180
890335  meter/sec
 ZDOT =      -4595
222150                 ZDOT =       -1363
952705

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5810753
03                 X    =        -1771117
52
 Y    =       13109701
60  feet           Y    =         3995837
05  meter
 Z    =       16969030
41                 Z    =         5172160
47
 XDOT =     -23324
909773                 XDOT =       -7109
432499
 YDOT =      -4570
344908  feet/sec       YDOT =       -1393
041128  meter/sec
 ZDOT =      -4434
858981                 ZDOT =       -1351
745017


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   16290
44768063  
00016717  00000-0  10270-3 0  9126
2 25544  51
6417 173
2232 0006888  74
7443 285
4470 15
54210492 23845


Satellite: ISS
Catalog Number: 25544
Epoch time:      16290
44768063   =   yrday
fracday
Element set:     912
Inclination:       51
6417  deg
RA of node:       173
2232  deg
Eccentricity:     
0006888     
Arg of perigee:    74
7443  deg
Mean anomaly:     285
4470  deg
Mean motion:   15
54210492  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2384
Checksum:              315


Coasting Arc #14 (Orbit 2384)
---------------------------------------

Vector Time (GMT): 2016/290/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6732113
32                 A    =         6789176
45  meter
 Y    =         803404
59  meter          E    =           
0018745
 Z    =         167516
19                 I    =           51
70790
 XDOT =       -404
038144                 Wp   =           57
30219
 YDOT =      -4740
138634  meter/sec      RA   =          172
07679  deg
 ZDOT =       6016
985755                 TA   =          304
50126
                                          MA   =          304
67814
                                          Ha   =            223
409  n
mi
                                          Hp   =            212
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22086985
97                 X    =        -6741410
59
 Y    =        2635841
81  feet           Y    =          728069
61  meter
 Z    =         549593
79                 Z    =          134789
80
 XDOT =      -1325
584461                 XDOT =        -380
231312
 YDOT =     -15551
635938  feet/sec       YDOT =       -4744
523076  meter/sec
 ZDOT =      19740
766914                 ZDOT =        6015
081347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21712423
56                 X    =         6617946
70
 Y    =       -4846669
98  feet           Y    =        -1477265
01  meter
 Z    =         406346
77                 Z    =          123854
50
 XDOT =       2658
231621                 XDOT =         810
228998
 YDOT =      13741
235948  feet/sec       YDOT =        4188
328717  meter/sec
 ZDOT =      19733
147549                 ZDOT =        6014
663373


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   16290
51198126  
00016717  00000-0  10270-3 0  9132
2 25544  51
6427 172
9024 0006939  75
2892 284
9029 15
54180020 23850


Satellite: ISS
Catalog Number: 25544
Epoch time:      16290
51198126   =   yrday
fracday
Element set:     913
Inclination:       51
6427  deg
RA of node:       172
9024  deg
Eccentricity:     
0006939     
Arg of perigee:    75
2892  deg
Mean anomaly:     284
9029  deg
Mean motion:   15
54180020  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2385
Checksum:              316


Coasting Arc #15 (Orbit 2399)
---------------------------------------

Vector Time (GMT): 2016/291/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6514836
58                 A    =         6787724
15  meter
 Y    =          49936
36  meter          E    =           
0011976
 Z    =       -1903994
63                 I    =           51
73486
 XDOT =      -1671
405447                 Wp   =          112
11768
 YDOT =       4931
767404  meter/sec      RA   =          167
11184  deg
 ZDOT =      -5622
357594                 TA   =           88
81504
                                          MA   =           88
67784
                                          Ha   =            223
411  n
mi
                                          Hp   =            212
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21374135
76                 X    =         6523043
01
 Y    =         163833
21  feet           Y    =          122835
36  meter
 Z    =       -6246701
53                 Z    =        -1872326
43
 XDOT =      -5483
613672                 XDOT =       -1699
117795
 YDOT =      16180
339252  feet/sec       YDOT =        4912
921184  meter/sec
 ZDOT =     -18446
055097                 ZDOT =       -5630
544820

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21284302
08                 X    =        -6487455
27
 Y    =        2360134
39  feet           Y    =          719368
96  meter
 Z    =       -6108195
45                 Z    =        -1861777
97
 XDOT =       3593
204718                 XDOT =        1095
208798
 YDOT =     -15145
815460  feet/sec       YDOT =       -4616
444552  meter/sec
 ZDOT =     -18482
609143                 ZDOT =       -5633
499267


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   16291
47647182  
00016717  00000-0  10270-3 0  9140
2 25544  51
6428 168
0947 0006725  80
1805 280
0107 15
54172996 24008


Satellite: ISS
Catalog Number: 25544
Epoch time:      16291
47647182   =   yrday
fracday
Element set:     914
Inclination:       51
6428  deg
RA of node:       168
0947  deg
Eccentricity:     
0006725     
Arg of perigee:    80
1805  deg
Mean anomaly:     280
0107  deg
Mean motion:   15
54172996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2400
Checksum:              312


Coasting Arc #16 (Orbit 2415)
---------------------------------------

Vector Time (GMT): 2016/292/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5795277
76                 A    =         6784369
21  meter
 Y    =        -934576
48  meter          E    =           
0019375
 Z    =        3383512
61                 I    =           51
75518
 XDOT =       3529
795616                 Wp   =           86
88497
 YDOT =      -4985
400721  meter/sec      RA   =          162
14059  deg
 ZDOT =       4646
897460                 TA   =          312
59793
                                          MA   =          312
76120
                                          Ha   =            223
483  n
mi
                                          Hp   =            212
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19013378
49                 X    =        -5800832
44
 Y    =       -3066195
80  feet           Y    =         -999414
01  meter
 Z    =       11100763
16                 Z    =         3355346
45
 XDOT =      11580
694278                 XDOT =        3562
708091
 YDOT =     -16356
301577  feet/sec       YDOT =       -4945
743858  meter/sec
 ZDOT =      15245
726576                 ZDOT =        4664
125019

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19323880
12                 X    =         5889918
66
 Y    =         463621
54  feet           Y    =          141311
85  meter
 Z    =       10977694
35                 Z    =         3346001
24
 XDOT =      -9137
586438                 XDOT =       -2785
136346
 YDOT =      16344
747823  feet/sec       YDOT =        4981
879136  meter/sec
 ZDOT =      15321
846475                 ZDOT =        4670
098806


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   16292
50525376  
00016717  00000-0  10270-3 0  9156
2 25544  51
6430 162
9653 0006862  82
1028 278
0903 15
54200652 24168


Satellite: ISS
Catalog Number: 25544
Epoch time:      16292
50525376   =   yrday
fracday
Element set:     915
Inclination:       51
6430  deg
RA of node:       162
9653  deg
Eccentricity:     
0006862     
Arg of perigee:    82
1028  deg
Mean anomaly:     278
0903  deg
Mean motion:   15
54200652  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2416
Checksum:              298


Coasting Arc #17 (Orbit 2430)
---------------------------------------

Vector Time (GMT): 2016/293/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4654209
44                 A    =         6780382
39  meter
 Y    =        1931042
22  meter          E    =           
0016297
 Z    =       -4552553
11                 I    =           51
77202
 XDOT =      -5059
900453                 Wp   =           76
40724
 YDOT =       4812
486929  meter/sec      RA   =          157
16161  deg
 ZDOT =      -3137
293504                 TA   =          162
17587
                                          MA   =          162
11864
                                          Ha   =            223
320  n
mi
                                          Hp   =            212
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15269716
02                 X    =         4654384
97
 Y    =        6335440
36  feet           Y    =         1983089
49  meter
 Z    =      -14936197
86                 Z    =        -4529943
27
 XDOT =     -16600
723271                 XDOT =       -5098
098878
 YDOT =      15788
999111  feet/sec       YDOT =        4755
690005  meter/sec
 ZDOT =     -10292
957691                 ZDOT =       -3161
966788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16149851
46                 X    =        -4922474
72
 Y    =       -3926917
18  feet           Y    =        -1196924
36  meter
 Z    =      -14837575
88                 Z    =        -4522493
13
 XDOT =      13657
769220                 XDOT =        4162
888058
 YDOT =     -16938
312941  feet/sec       YDOT =       -5162
797784  meter/sec
 ZDOT =     -10401
643639                 ZDOT =       -3170
420981


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   16293
46972882  
00016717  00000-0  10270-3 0  9161
2 25544  51
6424 158
1571 0006768  85
1828 275
0097 15
54231802 24312


Satellite: ISS
Catalog Number: 25544
Epoch time:      16293
46972882   =   yrday
fracday
Element set:     916
Inclination:       51
6424  deg
RA of node:       158
1571  deg
Eccentricity:     
0006768     
Arg of perigee:    85
1828  deg
Mean anomaly:     275
0097  deg
Mean motion:   15
54231802  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2431
Checksum:              327


Coasting Arc #18 (Orbit 2446)
---------------------------------------

Vector Time (GMT): 2016/294/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3216697
99                 A    =         6777646
07  meter
 Y    =       -2923310
73  meter          E    =           
0010669
 Z    =        5191894
51                 I    =           51
79211
 XDOT =       6141
679385                 Wp   =          103
70866
 YDOT =      -4412
716008  meter/sec      RA   =          152
17503  deg
 ZDOT =       1315
822044                 TA   =          333
66383
                                          MA   =          333
71803
                                          Ha   =            223
436  n
mi
                                          Hp   =            212
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10553471
11                 X    =        -3208990
17
 Y    =       -9590914
46  feet           Y    =        -2959238
71  meter
 Z    =       17033774
63                 Z    =         5176287
13
 XDOT =      20149
866749                 XDOT =        6184
175219
 YDOT =     -14477
414724  feet/sec       YDOT =       -4343
797971  meter/sec
 ZDOT =       4317
001457                 ZDOT =        1345
760725

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12129643
32                 X    =         3697115
28
 Y    =        7651121
92  feet           Y    =         2332061
96  meter
 Z    =       16965935
19                 Z    =         5171217
05
 XDOT =     -16830
136919                 XDOT =       -5129
825733
 YDOT =      16782
227670  feet/sec       YDOT =        5115
222994  meter/sec
 ZDOT =       4448
686534                 ZDOT =        1355
959655


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   16294
49849717  
00016717  00000-0  10270-3 0  9176
2 25544  51
6422 153
0281 0006798  89
7982 270
3950 15
54233098 24478


Satellite: ISS
Catalog Number: 25544
Epoch time:      16294
49849717   =   yrday
fracday
Element set:     917
Inclination:       51
6422  deg
RA of node:       153
0281  deg
Eccentricity:     
0006798     
Arg of perigee:    89
7982  deg
Mean anomaly:     270
3950  deg
Mean motion:   15
54233098  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2447
Checksum:              348
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