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

 
Date: May 3rd 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 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


132/13:26:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 213 5

135/07:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 213 2

Coasting Arc #1 (Orbit 3787)
---------------------------------------

Vector Time (GMT): 2016/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1846502
81                 A    =         6788487
13  meter
 Y    =       -6525656
92  meter          E    =           
0013723
 Z    =          92827
51                 I    =           51
30510
 XDOT =       4589
531329                 Wp   =           51
12275
 YDOT =       1392
177921  meter/sec      RA   =          285
17122  deg
 ZDOT =       5984
877192                 TA   =          309
88201
                                          MA   =          310
00261
                                          Ha   =            221
185  n
mi
                                          Hp   =            213
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6058080
07                 X    =         1918886
17
 Y    =      -21409635
57  feet           Y    =        -6504603
38  meter
 Z    =         304552
21                 Z    =          101973
54
 XDOT =      15057
517482                 XDOT =        4544
550288
 YDOT =       4567
512864  feet/sec       YDOT =        1443
249859  meter/sec
 ZDOT =      19635
423858                 ZDOT =        6007
062902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9116582
91                 X    =        -2778734
47
 Y    =      -20296160
62  feet           Y    =        -6186269
76  meter
 Z    =         345487
72                 Z    =          105304
66
 XDOT =      12896
597607                 XDOT =        3930
882951
 YDOT =      -5427
961712  feet/sec       YDOT =       -1654
442730  meter/sec
 ZDOT =      19731
500589                 ZDOT =        6014
161380


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   16123
56409040  
00016717  00000-0  10270-3 0  9008
2 25544  51
6397 285
6196 0001772  86
3933 273
7423 15
54417256 37883


Satellite: ISS
Catalog Number: 25544
Epoch time:      16123
56409040   =   yrday
fracday
Element set:     900
Inclination:       51
6397  deg
RA of node:       285
6196  deg
Eccentricity:     
0001772     
Arg of perigee:    86
3933  deg
Mean anomaly:     273
7423  deg
Mean motion:   15
54417256  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3788
Checksum:              325


Coasting Arc #2 (Orbit 3802)
---------------------------------------

Vector Time (GMT): 2016/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2607990
13                 A    =         6786878
61  meter
 Y    =        5972979
71  meter          E    =           
0008174
 Z    =       -1886443
35                 I    =           51
29175
 XDOT =      -3928
501157                 Wp   =          130
18479
 YDOT =      -3474
372689  meter/sec      RA   =          280
17539  deg
 ZDOT =      -5590
931299                 TA   =           70
68792
                                          MA   =           70
59955
                                          Ha   =            221
138  n
mi
                                          Hp   =            213
493

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8556398
06                 X    =        -2665423
99
 Y    =       19596390
12  feet           Y    =         5943494
21  meter
 Z    =       -6189118
60                 Z    =        -1899252
26
 XDOT =     -12888
783324                 XDOT =       -3862
199167
 YDOT =     -11398
860529  feet/sec       YDOT =       -3517
933345  meter/sec
 ZDOT =     -18342
950455                 ZDOT =       -5609
854034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6417385
98                 X    =         1956019
25
 Y    =       20379946
45  feet           Y    =         6211807
68  meter
 Z    =       -6245845
19                 Z    =        -1903733
61
 XDOT =     -15631
170463                 XDOT =       -4764
380757
 YDOT =       -703
310070  feet/sec       YDOT =        -214
368909  meter/sec
 ZDOT =     -18424
474313                 ZDOT =       -5615
779771


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   16124
52844374  
00016717  00000-0  10270-3 0  9019
2 25544  51
6390 280
8104 0001793  84
6744 275
4613 15
54441332 38036


Satellite: ISS
Catalog Number: 25544
Epoch time:      16124
52844374   =   yrday
fracday
Element set:     901
Inclination:       51
6390  deg
RA of node:       280
8104  deg
Eccentricity:     
0001793     
Arg of perigee:    84
6744  deg
Mean anomaly:     275
4613  deg
Mean motion:   15
54441332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3803
Checksum:              299


Coasting Arc #3 (Orbit 3818)
---------------------------------------

Vector Time (GMT): 2016/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3199603
98                 A    =         6783352
94  meter
 Y    =       -4896116
65  meter          E    =           
0013996
 Z    =        3423830
64                 I    =           51
27634
 XDOT =       3190
916574                 Wp   =           90
95099
 YDOT =       5283
570253  meter/sec      RA   =          275
17072  deg
 ZDOT =       4557
211961                 TA   =          309
40510
                                          MA   =          309
52894
                                          Ha   =            221
028  n
mi
                                          Hp   =            213
532

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10497388
39                 X    =         3237483
99
 Y    =      -16063374
83  feet           Y    =        -4860124
61  meter
 Z    =       11233040
16                 Z    =         3439466
00
 XDOT =      10468
886396                 XDOT =        3109
459844
 YDOT =      17334
548074  feet/sec       YDOT =        5318
797942  meter/sec
 ZDOT =      14951
482813                 ZDOT =        4572
514842

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2985439
24                 X    =         -909961
88
 Y    =      -18914652
66  feet           Y    =        -5765186
13  meter
 Z    =       11301833
15                 Z    =         3444798
75
 XDOT =      17924
176923                 XDOT =        5463
289126
 YDOT =       6175
762923  feet/sec       YDOT =        1882
372539  meter/sec
 ZDOT =      15016
960479                 ZDOT =        4577
169554


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   16125
55707889  
00016717  00000-0  10270-3 0  9023
2 25544  51
6400 275
6800 0001653  93
9357 266
1985 15
54452266 38195


Satellite: ISS
Catalog Number: 25544
Epoch time:      16125
55707889   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:       275
6800  deg
Eccentricity:     
0001653     
Arg of perigee:    93
9357  deg
Mean anomaly:     266
1985  deg
Mean motion:   15
54452266  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3819
Checksum:              332


Coasting Arc #4 (Orbit 3833)
---------------------------------------

Vector Time (GMT): 2016/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3696527
83                 A    =         6779348
82  meter
 Y    =        3357811
67  meter          E    =           
0011927
 Z    =       -4596441
75                 I    =           51
26205
 XDOT =      -2361
238451                 Wp   =           73
15279
 YDOT =      -6654
991245  meter/sec      RA   =          270
15474  deg
 ZDOT =      -2965
703439                 TA   =          167
09870
                                          MA   =          167
06816
                                          Ha   =            221
118  n
mi
                                          Hp   =            213
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12127715
99                 X    =        -3711472
97
 Y    =       11016442
47  feet           Y    =         3316390
95  meter
 Z    =      -15080189
46                 Z    =        -4614435
32
 XDOT =      -7746
845311                 XDOT =       -2272
238765
 YDOT =     -21833
960776  feet/sec       YDOT =       -6680
898634  meter/sec
 ZDOT =      -9729
998160                 ZDOT =       -2976
957645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1303363
57                 X    =         -397265
21
 Y    =       16259258
72  feet           Y    =         4955822
06  meter
 Z    =      -15158936
74                 Z    =        -4620443
92
 XDOT =     -19314
153114                 XDOT =       -5886
953869
 YDOT =     -10655
035383  feet/sec       YDOT =       -3247
654785  meter/sec
 ZDOT =      -9777
651201                 ZDOT =       -2980
228086


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   16126
52141624  
00016717  00000-0  10270-3 0  9031
2 25544  51
6410 270
8708 0001757  91
6095 268
5259 15
54453556 38349


Satellite: ISS
Catalog Number: 25544
Epoch time:      16126
52141624   =   yrday
fracday
Element set:     903
Inclination:       51
6410  deg
RA of node:       270
8708  deg
Eccentricity:     
0001757     
Arg of perigee:    91
6095  deg
Mean anomaly:     268
5259  deg
Mean motion:   15
54453556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3834
Checksum:              314


Coasting Arc #5 (Orbit 3849)
---------------------------------------

Vector Time (GMT): 2016/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4059256
76                 A    =         6776700
47  meter
 Y    =       -1530776
11  meter          E    =           
0005236
 Z    =        5202218
82                 I    =           51
25419
 XDOT =       1474
160135                 Wp   =          114
21329
 YDOT =       7457
416658  meter/sec      RA   =          265
12813  deg
 ZDOT =       1041
158267                 TA   =          325
75021
                                          MA   =          325
78396
                                          Ha   =            220
916  n
mi
                                          Hp   =            213
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13317771
51                 X    =         4050801
87
 Y    =       -5022231
32  feet           Y    =        -1485430
06  meter
 Z    =       17067647
04                 Z    =         5221917
59
 XDOT =       4836
483383                 XDOT =        1385
602262
 YDOT =      24466
590085  feet/sec       YDOT =        7473
406543  meter/sec
 ZDOT =       3415
873578                 ZDOT =        1048
104416

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6029820
73                 X    =         1837889
36
 Y    =      -12778508
32  feet           Y    =        -3894889
34  meter
 Z    =       17153466
35                 Z    =         5228376
54
 XDOT =      19508
896784                 XDOT =        5946
311740
 YDOT =      13842
627573  feet/sec       YDOT =        4219
232884  meter/sec
 ZDOT =       3444
680521                 ZDOT =        1049
938623


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   16127
55003334  
00016717  00000-0  10270-3 0  9041
2 25544  51
6409 265
7403 0001662  94
8688 265
2655 15
54475246 38502


Satellite: ISS
Catalog Number: 25544
Epoch time:      16127
55003334   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:       265
7403  deg
Eccentricity:     
0001662     
Arg of perigee:    94
8688  deg
Mean anomaly:     265
2655  deg
Mean motion:   15
54475246  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3850
Checksum:              317


Coasting Arc #6 (Orbit 3864)
---------------------------------------

Vector Time (GMT): 2016/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4322110
87                 A    =         6776658
33  meter
 Y    =        -419565
26  meter          E    =           
0016077
 Z    =       -5216716
54                 I    =           51
25843
 XDOT =       -492
813770                 Wp   =           98
02098
 YDOT =      -7573
107129  meter/sec      RA   =          260
09900  deg
 ZDOT =       1017
885745                 TA   =          181
78915
                                          MA   =          181
79491
                                          Ha   =            221
063  n
mi
                                          Hp   =            213
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14180153
79                 X    =        -4291756
85
 Y    =       -1376526
43  feet           Y    =         -467728
13  meter
 Z    =      -17115211
73                 Z    =        -5237639
01
 XDOT =      -1616
843079                 XDOT =        -413
037326
 YDOT =     -24846
151999  feet/sec       YDOT =       -7578
172069  meter/sec
 ZDOT =       3339
520161                 ZDOT =        1015
685316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10937201
26                 X    =        -3333658
94
 Y    =        8957309
83  feet           Y    =         2730188
04  meter
 Z    =      -17205995
71                 Z    =        -5244387
49
 XDOT =     -18048
397022                 XDOT =       -5501
151412
 YDOT =     -15641
764325  feet/sec       YDOT =       -4767
609766  meter/sec
 ZDOT =       3331
335682                 ZDOT =        1015
391116


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   16128
51435497  
00016717  00000-0  10270-3 0  9058
2 25544  51
6415 260
9320 0001735  99
0960 261
0389 15
54486147 38651


Satellite: ISS
Catalog Number: 25544
Epoch time:      16128
51435497   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       260
9320  deg
Eccentricity:     
0001735     
Arg of perigee:    99
0960  deg
Mean anomaly:     261
0389  deg
Mean motion:   15
54486147  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3865
Checksum:              323


Coasting Arc #7 (Orbit 3880)
---------------------------------------

Vector Time (GMT): 2016/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4421228
95                 A    =         6779302
84  meter
 Y    =        2303390
03  meter          E    =           
0009882
 Z    =        4587545
43                 I    =           51
27452
 XDOT =       -584
148223                 Wp   =           71
51625
 YDOT =       7051
094882  meter/sec      RA   =          255
07232  deg
 ZDOT =      -2969
008612                 TA   =           48
26078
                                          MA   =           48
17632
                                          Ha   =            220
992  n
mi
                                          Hp   =            213
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14505344
34                 X    =         4372858
55
 Y    =        7557053
91  feet           Y    =         2352560
49  meter
 Z    =       15051002
07                 Z    =         4608905
67
 XDOT =      -1916
496795                 XDOT =        -648
529482
 YDOT =      23133
513392  feet/sec       YDOT =        7044
202706  meter/sec
 ZDOT =      -9740
841903                 ZDOT =       -2972
002366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15455063
82                 X    =         4710703
45
 Y    =       -5085914
57  feet           Y    =        -1550186
76  meter
 Z    =       15143355
53                 Z    =         4615694
77
 XDOT =      14950
145063                 XDOT =        4556
804215
 YDOT =      16303
450048  feet/sec       YDOT =        4969
291575  meter/sec
 ZDOT =      -9755
114141                 ZDOT =       -2973
358790


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   16129
54295501  
00016717  00000-0  10270-3 0  9063
2 25544  51
6425 255
8013 0001797 101
3969 258
7386 15
54463350 38817


Satellite: ISS
Catalog Number: 25544
Epoch time:      16129
54295501   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:       255
8013  deg
Eccentricity:     
0001797     
Arg of perigee:   101
3969  deg
Mean anomaly:     258
7386  deg
Mean motion:   15
54463350  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3881
Checksum:              324


Coasting Arc #8 (Orbit 3895)
---------------------------------------

Vector Time (GMT): 2016/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4348471
78                 A    =         6783209
37  meter
 Y    =       -3918536
70  meter          E    =           
0006615
 Z    =       -3433721
59                 I    =           51
29689
 XDOT =       1736
822977                 Wp   =           94
07557
 YDOT =      -5911
905281  meter/sec      RA   =          250
05795  deg
 ZDOT =       4554
253820                 TA   =          225
50668
                                          MA   =          225
56077
                                          Ha   =            221
009  n
mi
                                          Hp   =            213
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14266639
69                 X    =        -4287650
76
 Y    =      -12856091
53  feet           Y    =        -3966823
94  meter
 Z    =      -11265490
79                 Z    =        -3454698
18
 XDOT =       5698
238114                 XDOT =        1780
679382
 YDOT =     -19396
014703  feet/sec       YDOT =       -5892
238018  meter/sec
 ZDOT =      14941
777626                 ZDOT =        4562
797174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19086563
97                 X    =        -5817584
70
 Y    =        1572889
87  feet           Y    =          479416
83  meter
 Z    =      -11355900
40                 Z    =        -3461278
44
 XDOT =     -10213
453691                 XDOT =       -3113
060685
 YDOT =     -15953
577829  feet/sec       YDOT =       -4862
650522  meter/sec
 ZDOT =      14979
943315                 ZDOT =        4565
886722


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   16130
50725549  
00016717  00000-0  10270-3 0  9072
2 25544  51
6424 250
9928 0001648  99
3931 260
7408 15
54486318 38960


Satellite: ISS
Catalog Number: 25544
Epoch time:      16130
50725549   =   yrday
fracday
Element set:     907
Inclination:       51
6424  deg
RA of node:       250
9928  deg
Eccentricity:     
0001648     
Arg of perigee:    99
3931  deg
Mean anomaly:     260
7408  deg
Mean motion:   15
54486318  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3896
Checksum:              336


Coasting Arc #9 (Orbit 3911)
---------------------------------------

Vector Time (GMT): 2016/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4011068
60                 A    =         6786771
83  meter
 Y    =        5150169
11  meter          E    =           
0015683
 Z    =        1829751
31                 I    =           51
32015
 XDOT =      -2955
539638                 Wp   =          113
19317
 YDOT =       4309
090052  meter/sec      RA   =          245
05533  deg
 ZDOT =      -5617
422339                 TA   =           46
58026
                                          MA   =           46
44983
                                          Ha   =            220
977  n
mi
                                          Hp   =            213
435

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13159673
89                 X    =         3944291
78
 Y    =       16896880
27  feet           Y    =         5194650
07  meter
 Z    =        6003121
11                 Z    =         1849074
38
 XDOT =      -9696
652357                 XDOT =       -2976
218013
 YDOT =      14137
434553  feet/sec       YDOT =        4275
923948  meter/sec
 ZDOT =     -18429
863317                 ZDOT =       -5631
829728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21333099
23                 X    =         6502328
65
 Y    =        1605230
46  feet           Y    =          489274
24  meter
 Z    =        6086144
54                 Z    =         1855056
86
 XDOT =       4174
855540                 XDOT =        1272
495968
 YDOT =      15030
122846  feet/sec       YDOT =        4581
181443  meter/sec
 ZDOT =     -18493
212429                 ZDOT =       -5636
731148


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   16131
53583413  
00016717  00000-0  10270-3 0  9089
2 25544  51
6418 245
8628 0001734 108
0165 252
1177 15
54507439 39121


Satellite: ISS
Catalog Number: 25544
Epoch time:      16131
53583413   =   yrday
fracday
Element set:     908
Inclination:       51
6418  deg
RA of node:       245
8628  deg
Eccentricity:     
0001734     
Arg of perigee:   108
0165  deg
Mean anomaly:     252
1177  deg
Mean motion:   15
54507439  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3912
Checksum:              304


Coasting Arc #10 (Orbit 3926)
---------------------------------------

Vector Time (GMT): 2016/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3410806
35                 A    =         6788151
04  meter
 Y    =       -5862641
81  meter          E    =           
0012959
 Z    =         -37218
25                 I    =           51
34053
 XDOT =       4128
417801                 Wp   =           51
69135
 YDOT =      -2430
809745  meter/sec      RA   =          240
06125  deg
 ZDOT =       5988
413029                 TA   =          307
90603
                                          MA   =          308
02313
                                          Ha   =            220
951  n
mi
                                          Hp   =            213
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11190309
56                 X    =        -3344814
54
 Y    =      -19234389
14  feet           Y    =        -5900414
73  meter
 Z    =        -122107
13                 Z    =          -53627
21
 XDOT =      13544
677825                 XDOT =        4126
203567
 YDOT =      -7975
097588  feet/sec       YDOT =       -2384
655708  meter/sec
 ZDOT =      19647
024372                 ZDOT =        6008
462485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21846470
17                 X    =        -6658804
11
 Y    =       -4230177
46  feet           Y    =        -1289358
09  meter
 Z    =        -192362
79                 Z    =          -58632
18
 XDOT =       2516
275231                 XDOT =         766
960691
 YDOT =     -13757
313269  feet/sec       YDOT =       -4193
229085  meter/sec
 ZDOT =      19734
553558                 ZDOT =        6015
091924


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   16132
50011570  
00016717  00000-0  10270-3 0  9098
2 25544  51
6430 241
0535 0001693 103
7978 256
3363 15
54532849 39270


Satellite: ISS
Catalog Number: 25544
Epoch time:      16132
50011570   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:       241
0535  deg
Eccentricity:     
0001693     
Arg of perigee:   103
7978  deg
Mean anomaly:     256
3363  deg
Mean motion:   15
54532849  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3927
Checksum:              302


Coasting Arc #11 (Orbit 3927)
---------------------------------------

Vector Time (GMT): 2016/132/13:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4675787
86                 A    =         6785875
52  meter
 Y    =       -4337186
14  meter          E    =           
0006679
 Z    =       -2316298
17                 I    =           51
33357
 XDOT =       2035
197175                 Wp   =           55
98602
 YDOT =      -5061
592096  meter/sec      RA   =          239
74369  deg
 ZDOT =       5384
152717                 TA   =          278
08788
                                          MA   =          278
16364
                                          Ha   =            220
893  n
mi
                                          Hp   =            213
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15340511
37                 X    =        -4615689
20
 Y    =      -14229613
31  feet           Y    =        -4389137
76  meter
 Z    =       -7599403
43                 Z    =        -2338866
36
 XDOT =       6677
156086                 XDOT =        2065
491839
 YDOT =     -16606
273282  feet/sec       YDOT =       -5038
664043  meter/sec
 ZDOT =      17664
543034                 ZDOT =        5394
112595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18533215
02                 X    =        -5648923
94
 Y    =        9635615
08  feet           Y    =         2936935
48  meter
 Z    =       -7696686
24                 Z    =        -2345949
97
 XDOT =     -12740
710827                 XDOT =       -3883
368660
 YDOT =     -10398
728234  feet/sec       YDOT =       -3169
532366  meter/sec
 ZDOT =      17708
701757                 ZDOT =        5397
612296


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   16132
56440006  
00016717  00000-0  10270-3 0  9106
2 25544  51
6428 240
7343 0001463 100
0730 260
0588 15
54512064 39280


Satellite: ISS
Catalog Number: 25544
Epoch time:      16132
56440006   =   yrday
fracday
Element set:     910
Inclination:       51
6428  deg
RA of node:       240
7343  deg
Eccentricity:     
0001463     
Arg of perigee:   100
0730  deg
Mean anomaly:     260
0588  deg
Mean motion:   15
54512064  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3928
Checksum:              270


Coasting Arc #12 (Orbit 3943)
---------------------------------------

Vector Time (GMT): 2016/133/13:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4232469
60                 A    =         6787988
29  meter
 Y    =        5273146
49  meter          E    =           
0014530
 Z    =         516548
51                 I    =           51
35707
 XDOT =      -3456
117572                 Wp   =          126
65364
 YDOT =       3368
652154  meter/sec      RA   =          234
74958  deg
 ZDOT =      -5961
869166                 TA   =           47
74971
                                          MA   =           47
62655
                                          Ha   =            220
921  n
mi
                                          Hp   =            213
396

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13886055
11                 X    =         4170680
21
 Y    =       17300349
38  feet           Y    =         5320131
28  meter
 Z    =        1694712
98                 Z    =          536959
00
 XDOT =     -11338
968411                 XDOT =       -3464
569486
 YDOT =      11052
008378  feet/sec       YDOT =        3329
956500  meter/sec
 ZDOT =     -19559
938209                 ZDOT =       -5978
678612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20822687
64                 X    =         6346755
19
 Y    =       -7631194
36  feet           Y    =        -2325988
04  meter
 Z    =        1782475
63                 Z    =          543298
57
 XDOT =       6339
576222                 XDOT =        1932
302832
 YDOT =      12633
552203  feet/sec       YDOT =        3850
706711  meter/sec
 ZDOT =     -19633
557750                 ZDOT =       -5984
308402


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   16133
59295651  
00016717  00000-0  10270-3 0  9115
2 25544  51
6420 235
6043 0001649 104
0521 256
0815 15
54547547 39440


Satellite: ISS
Catalog Number: 25544
Epoch time:      16133
59295651   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:       235
6043  deg
Eccentricity:     
0001649     
Arg of perigee:   104
0521  deg
Mean anomaly:     256
0815  deg
Mean motion:   15
54547547  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3944
Checksum:              299


Coasting Arc #13 (Orbit 3959)
---------------------------------------

Vector Time (GMT): 2016/134/13:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3444168
84                 A    =         6787387
52  meter
 Y    =       -5691800
90  meter          E    =           
0014990
 Z    =        1311503
13                 I    =           51
37410
 XDOT =       4772
580440                 Wp   =           63
87810
 YDOT =      -1540
061820  meter/sec      RA   =          229
75853  deg
 ZDOT =       5804
468579                 TA   =          310
45594
                                          MA   =          310
58655
                                          Ha   =            220
909  n
mi
                                          Hp   =            213
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11299766
55                 X    =        -3386636
47
 Y    =      -18673887
45  feet           Y    =        -5729994
23  meter
 Z    =        4302831
79                 Z    =         1294911
76
 XDOT =      15658
072311                 XDOT =        4761
251351
 YDOT =      -5052
696259  feet/sec       YDOT =       -1486
755117  meter/sec
 ZDOT =      19043
532083                 ZDOT =        5827
625138

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21225906
52                 X    =        -6469656
31
 Y    =        5144570
73  feet           Y    =         1568065
16  meter
 Z    =        4231718
63                 Z    =         1289827
84
 XDOT =        262
738539                 XDOT =          80
082707
 YDOT =     -14787
412324  feet/sec       YDOT =       -4507
203276  meter/sec
 ZDOT =      19144
417240                 ZDOT =        5835
218375


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   16134
62150274  
00016717  00000-0  10270-3 0  9122
2 25544  51
6418 230
4739 0001627 103
7721 256
3613 15
54555235 39606


Satellite: ISS
Catalog Number: 25544
Epoch time:      16134
62150274   =   yrday
fracday
Element set:     912
Inclination:       51
6418  deg
RA of node:       230
4739  deg
Eccentricity:     
0001627     
Arg of perigee:   103
7721  deg
Mean anomaly:     256
3613  deg
Mean motion:   15
54555235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3960
Checksum:              292


Coasting Arc #14 (Orbit 3970)
---------------------------------------

Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3669645
42                 A    =         6776235
67  meter
 Y    =        2244686
78  meter          E    =           
0016333
 Z    =       -5250006
64                 I    =           51
35105
 XDOT =      -4797
054961                 Wp   =           97
72319
 YDOT =      -5910
808308  meter/sec      RA   =          225
96094  deg
 ZDOT =        825
883912                 TA   =          180
21467
                                          MA   =          180
21537
                                          Ha   =            220
918  n
mi
                                          Hp   =            213
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12039519
09                 X    =        -3668970
92
 Y    =        7364457
95  feet           Y    =         2203654
20  meter
 Z    =      -17224431
24                 Z    =        -5267831
29
 XDOT =     -15738
369295                 XDOT =       -4734
614107
 YDOT =     -19392
415710  feet/sec       YDOT =       -5964
103052  meter/sec
 ZDOT =       2709
592888                 ZDOT =         802
732480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13453502
56                 X    =        -4100627
58
 Y    =        3937124
14  feet           Y    =         1200035
44  meter
 Z    =      -17302271
95                 Z    =        -5273732
49
 XDOT =      -9763
660049                 XDOT =       -2975
963583
 YDOT =     -21894
140030  feet/sec       YDOT =       -6673
333881  meter/sec
 ZDOT =       2609
998699                 ZDOT =         795
527603


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   16135
32862274  
00016717  00000-0  10270-3 0  9131
2 25544  51
6396 226
9446 0001815 107
5566 252
5786 15
54586410 39714


Satellite: ISS
Catalog Number: 25544
Epoch time:      16135
32862274   =   yrday
fracday
Element set:     913
Inclination:       51
6396  deg
RA of node:       226
9446  deg
Eccentricity:     
0001815     
Arg of perigee:   107
5566  deg
Mean anomaly:     252
5786  deg
Mean motion:   15
54586410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3971
Checksum:              329


Coasting Arc #15 (Orbit 3986)
---------------------------------------

Vector Time (GMT): 2016/136/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4863294
20                 A    =         6778707
34  meter
 Y    =        -711250
57  meter          E    =           
0009344
 Z    =        4661949
08                 I    =           51
38196
 XDOT =       3623
191859                 Wp   =           72
18981
 YDOT =       6141
002534  meter/sec      RA   =          220
93912  deg
 ZDOT =      -2835
272829                 TA   =           46
07264
                                          MA   =           45
99556
                                          Ha   =            220
835  n
mi
                                          Hp   =            213
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15955689
63                 X    =         4848240
22
 Y    =       -2333499
23  feet           Y    =         -656950
17  meter
 Z    =       15295108
54                 Z    =         4685537
36
 XDOT =      11887
112397                 XDOT =        3568
024987
 YDOT =      20147
646110  feet/sec       YDOT =        6181
211037  meter/sec
 ZDOT =      -9302
076211                 ZDOT =       -2817
806095

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15939032
05                 X    =         4858216
97
 Y    =        1681200
94  feet           Y    =          512430
05  meter
 Z    =       15397740
62                 Z    =         4693231
34
 XDOT =       6688
567240                 XDOT =        2038
675295
 YDOT =      21321
175305  feet/sec       YDOT =        6498
694233  meter/sec
 ZDOT =      -9227
209167                 ZDOT =       -2812
453354


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   16136
35715260  
00016717  00000-0  10270-3 0  9148
2 25544  51
6394 221
8126 0001876 110
3632 249
7722 15
54562002 39870


Satellite: ISS
Catalog Number: 25544
Epoch time:      16136
35715260   =   yrday
fracday
Element set:     914
Inclination:       51
6394  deg
RA of node:       221
8126  deg
Eccentricity:     
0001876     
Arg of perigee:   110
3632  deg
Mean anomaly:     249
7722  deg
Mean motion:   15
54562002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3987
Checksum:              302


Coasting Arc #16 (Orbit 4001)
---------------------------------------

Vector Time (GMT): 2016/137/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5758855
58                 A    =         6782591
30  meter
 Y    =        -705554
89  meter          E    =           
0006998
 Z    =       -3520252
86                 I    =           51
42097
 XDOT =      -2016
249136                 Wp   =          100
61436
 YDOT =      -5877
331885  meter/sec      RA   =          215
93123  deg
 ZDOT =       4482
742892                 TA   =          217
81476
                                          MA   =          217
86394
                                          Ha   =            220
862  n
mi
                                          Hp   =            213
198

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18893883
13                 X    =        -5733437
82
 Y    =       -2314812
65  feet           Y    =         -769812
12  meter
 Z    =      -11549386
03                 Z    =        -3548166
50
 XDOT =      -6614
990604                 XDOT =       -1972
152950
 YDOT =     -19282
584924  feet/sec       YDOT =       -5899
632389  meter/sec
 ZDOT =      14707
161718                 ZDOT =        4473
055434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17769854
72                 X    =        -5416251
72
 Y    =       -6614769
38  feet           Y    =        -2016181
71  meter
 Z    =      -11670586
28                 Z    =        -3557194
70
 XDOT =      -2540
137988                 XDOT =        -774
234059
 YDOT =     -19015
513121  feet/sec       YDOT =       -5795
928399  meter/sec
 ZDOT =      14666
047636                 ZDOT =        4470
211319


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   16137
32139050  
00016717  00000-0  10270-3 0  9154
2 25544  51
6402 217
0035 0001826 112
5324 247
6022 15
54601003 40027


Satellite: ISS
Catalog Number: 25544
Epoch time:      16137
32139050   =   yrday
fracday
Element set:     915
Inclination:       51
6402  deg
RA of node:       217
0035  deg
Eccentricity:     
0001826     
Arg of perigee:   112
5324  deg
Mean anomaly:     247
6022  deg
Mean motion:   15
54601003  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4002
Checksum:              245


Coasting Arc #17 (Orbit 4017)
---------------------------------------

Vector Time (GMT): 2016/138/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6206371
74                 A    =         6786332
07  meter
 Y    =        1950804
59  meter          E    =           
0015681
 Z    =        1904784
85                 I    =           51
45985
 XDOT =         78
515808                 Wp   =          113
51022
 YDOT =       5245
997107  meter/sec      RA   =          210
93626  deg
 ZDOT =      -5598
097534                 TA   =           45
43611
                                          MA   =           45
30820
                                          Ha   =            220
774  n
mi
                                          Hp   =            213
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20362112
01                 X    =         6174843
33
 Y    =        6400277
53  feet           Y    =         2020032
07  meter
 Z    =        6249294
12                 Z    =         1934857
69
 XDOT =        257
597795                 XDOT =          47
041432
 YDOT =      17211
276599  feet/sec       YDOT =        5246
699192  meter/sec
 ZDOT =     -18366
461727                 ZDOT =       -5597
792519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18469861
60                 X    =         5629613
82
 Y    =       10620579
41  feet           Y    =         3237152
60  meter
 Z    =        6379681
83                 Z    =         1944527
02
 XDOT =      -2558
796283                 XDOT =        -779
921107
 YDOT =      15541
026746  feet/sec       YDOT =        4736
904952  meter/sec
 ZDOT =     -18366
015386                 ZDOT =       -5597
961490


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   16138
34990463  
00016717  00000-0  10270-3 0  9161
2 25544  51
6400 211
8724 0001736 118
6080 241
5247 15
54609074 40183


Satellite: ISS
Catalog Number: 25544
Epoch time:      16138
34990463   =   yrday
fracday
Element set:     916
Inclination:       51
6400  deg
RA of node:       211
8724  deg
Eccentricity:     
0001736     
Arg of perigee:   118
6080  deg
Mean anomaly:     241
5247  deg
Mean motion:   15
54609074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4018
Checksum:              298
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