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

 
Date: September 23rd 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 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


273/17:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 213 6

278/01:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 213 3

Coasting Arc #1 (Orbit 2028)
---------------------------------------

Vector Time (GMT): 2016/267/13:52:19
901
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1924217
74                 A    =         6782802
06  meter
 Y    =        5059089
68  meter          E    =           
0013212
 Z    =        4085773
28                 I    =           51
28141
 XDOT =      -4593
369540                 Wp   =           46
87101
 YDOT =       4825
469298  meter/sec      RA   =          286
41567  deg
 ZDOT =      -3795
053593                 TA   =           82
57890
                                          MA   =           82
42879
                                          Ha   =            222
376  n
mi
                                          Hp   =            214
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6313050
33                 X    =         1847655
70
 Y    =       16598063
24  feet           Y    =         5080179
79  meter
 Z    =       13404767
98                 Z    =         4094934
35
 XDOT =     -15070
110040                 XDOT =       -4628
552971
 YDOT =      15831
592185  feet/sec       YDOT =        4773
906157  meter/sec
 ZDOT =     -12450
963230                 ZDOT =       -3817
452926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13705556
72                 X    =        -4177453
69
 Y    =      -11245361
75  feet           Y    =        -3427586
26  meter
 Z    =       13443870
97                 Z    =         4097691
87
 XDOT =       4219
575863                 XDOT =        1286
126723
 YDOT =     -20211
028162  feet/sec       YDOT =       -6160
321384  meter/sec
 ZDOT =     -12549
626154                 ZDOT =       -3825
126052


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   16267
61921095  
00016717  00000-0  10270-3 0  9002
2 25544  51
6396 287
0031 0006645 354
8215   5
2868 15
53926117 20294


Satellite: ISS
Catalog Number: 25544
Epoch time:      16267
61921095   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:       287
0031  deg
Eccentricity:     
0006645     
Arg of perigee:   354
8215  deg
Mean anomaly:       5
2868  deg
Mean motion:   15
53926117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2029
Checksum:              310


Coasting Arc #2 (Orbit 2043)
---------------------------------------

Vector Time (GMT): 2016/268/13:52:19
901
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1136137
68                 A    =         6786433
43  meter
 Y    =       -6035734
29  meter          E    =           
0009572
 Z    =       -2879011
40                 I    =           51
28543
 XDOT =       4770
757465                 Wp   =           25
58052
 YDOT =      -3286
903520  meter/sec      RA   =          281
41002  deg
 ZDOT =       5022
933824                 TA   =          301
46530
                                          MA   =          301
55883
                                          Ha   =            222
515  n
mi
                                          Hp   =            214
568

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3727485
83                 X    =        -1054575
12
 Y    =      -19802277
85  feet           Y    =        -6047983
53  meter
 Z    =       -9445575
46                 Z    =        -2884331
88
 XDOT =      15652
091419                 XDOT =        4782
758622
 YDOT =     -10783
804198  feet/sec       YDOT =       -3233
486204  meter/sec
 ZDOT =      16479
441680                 ZDOT =        5046
138391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13356821
20                 X    =         4071159
10
 Y    =       15073165
88  feet           Y    =         4594300
96  meter
 Z    =       -9467748
01                 Z    =        -2885769
59
 XDOT =      -6655
312574                 XDOT =       -2028
539273
 YDOT =      16282
241898  feet/sec       YDOT =        4962
827330  meter/sec
 ZDOT =      16581
343799                 ZDOT =        5053
993590


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   16268
58387757  
00016717  00000-0  10270-3 0  9011
2 25544  51
6398 282
1968 0006602    
0430    
0722 15
53908413 20441


Satellite: ISS
Catalog Number: 25544
Epoch time:      16268
58387757   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:       282
1968  deg
Eccentricity:     
0006602     
Arg of perigee:      
0430  deg
Mean anomaly:        
0722  deg
Mean motion:   15
53908413  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2044
Checksum:              296


Coasting Arc #3 (Orbit 2059)
---------------------------------------

Vector Time (GMT): 2016/269/13:52:19
901
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         348142
30                 A    =         6789080
16  meter
 Y    =        6640728
39  meter          E    =           
0012314
 Z    =        1356903
35                 I    =           51
28948
 XDOT =      -4823
334090                 Wp   =           90
38480
 YDOT =       1443
105613  meter/sec      RA   =          276
41123  deg
 ZDOT =      -5779
540043                 TA   =           74
76946
                                          MA   =           74
63334
                                          Ha   =            222
643  n
mi
                                          Hp   =            214
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1142199
16                 X    =          267266
87
 Y    =       21787166
64  feet           Y    =         6644169
48  meter
 Z    =        4451782
66                 Z    =         1358397
49
 XDOT =     -15824
586908                 XDOT =       -4811
038315
 YDOT =       4734
598467  feet/sec       YDOT =        1389
236069  meter/sec
 ZDOT =     -18961
745548                 ZDOT =       -5802
940818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12502950
26                 X    =        -3810899
24
 Y    =      -17877740
69  feet           Y    =        -5449135
36  meter
 Z    =        4457156
09                 Z    =         1358541
18
 XDOT =       9494
882998                 XDOT =        2894
040338
 YDOT =     -11430
480349  feet/sec       YDOT =       -3484
010410  meter/sec
 ZDOT =     -19064
180410                 ZDOT =       -5810
762189


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   16269
61284809  
00016717  00000-0  10270-3 0  9021
2 25544  51
6401 277
0682 0006810   3
0117 357
1075 15
53944959 20608


Satellite: ISS
Catalog Number: 25544
Epoch time:      16269
61284809   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:       277
0682  deg
Eccentricity:     
0006810     
Arg of perigee:     3
0117  deg
Mean anomaly:     357
1075  deg
Mean motion:   15
53944959  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2060
Checksum:              303


Coasting Arc #4 (Orbit 2075)
---------------------------------------

Vector Time (GMT): 2016/270/13:52:19
901
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         376165
20                 A    =         6789791
75  meter
 Y    =       -6763853
53  meter          E    =           
0018080
 Z    =         260315
13                 I    =           51
28829
 XDOT =       4782
191169                 Wp   =           34
19815
 YDOT =        503
347868  meter/sec      RA   =          271
41826  deg
 ZDOT =       5980
366047                 TA   =          328
62250
                                          MA   =          328
73024
                                          Ha   =            222
612  n
mi
                                          Hp   =            214
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1234137
80                 X    =          450507
88
 Y    =      -22191120
50  feet           Y    =        -6759231
29  meter
 Z    =         854052
27                 Z    =          262323
74
 XDOT =      15689
603572                 XDOT =        4747
157206
 YDOT =       1651
403767  feet/sec       YDOT =         556
630299  meter/sec
 ZDOT =      19620
623513                 ZDOT =        6003
511528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11065029
54                 X    =         3372621
01
 Y    =       19274776
02  feet           Y    =         5874951
73  meter
 Z    =         863979
61                 Z    =          263340
99
 XDOT =     -12543
041372                 XDOT =       -3823
119010
 YDOT =       6289
241703  feet/sec       YDOT =        1916
960871  meter/sec
 ZDOT =      19721
610056                 ZDOT =        6011
146745


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   16270
64181344  
00016717  00000-0  10270-3 0  9037
2 25544  51
6390 271
9413 0006583   7
2994 352
8254 15
53961783 20768


Satellite: ISS
Catalog Number: 25544
Epoch time:      16270
64181344   =   yrday
fracday
Element set:     903
Inclination:       51
6390  deg
RA of node:       271
9413  deg
Eccentricity:     
0006583     
Arg of perigee:     7
2994  deg
Mean anomaly:     352
8254  deg
Mean motion:   15
53961783  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2076
Checksum:              319


Coasting Arc #5 (Orbit 2090)
---------------------------------------

Vector Time (GMT): 2016/271/13:52:19
901
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1117460
47                 A    =         6788338
15  meter
 Y    =        6425293
84  meter          E    =           
0005752
 Z    =       -1891397
43                 I    =           51
28389
 XDOT =      -4638
095121                 Wp   =           77
77030
 YDOT =      -2446
562277  meter/sec      RA   =          266
42290  deg
 ZDOT =      -5584
259479                 TA   =          123
14467
                                          MA   =          123
08947
                                          Ha   =            222
817  n
mi
                                          Hp   =            214
090

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3666208
88                 X    =        -1180039
10
 Y    =       21080360
35  feet           Y    =         6412447
51  meter
 Z    =       -6205372
16                 Z    =        -1896978
56
 XDOT =     -15216
847509                 XDOT =       -4583
266431
 YDOT =      -8026
779123  feet/sec       YDOT =       -2498
122694  meter/sec
 ZDOT =     -18321
061284                 ZDOT =       -5606
656676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8786125
15                 X    =        -2678010
94
 Y    =      -19501541
52  feet           Y    =        -5944069
85  meter
 Z    =       -6230827
16                 Z    =        -1899156
12
 XDOT =      15583
706328                 XDOT =        4749
913689
 YDOT =      -1150
059145  feet/sec       YDOT =        -350
538027  meter/sec
 ZDOT =     -18418
456117                 ZDOT =       -5613
945425


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   16271
60646641  
00016717  00000-0  10270-3 0  9041
2 25544  51
6394 267
1333 0006790   9
9757 350
1529 15
53941752 20913


Satellite: ISS
Catalog Number: 25544
Epoch time:      16271
60646641   =   yrday
fracday
Element set:     904
Inclination:       51
6394  deg
RA of node:       267
1333  deg
Eccentricity:     
0006790     
Arg of perigee:     9
9757  deg
Mean anomaly:     350
1529  deg
Mean motion:   15
53941752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2091
Checksum:              318


Coasting Arc #6 (Orbit 2106)
---------------------------------------

Vector Time (GMT): 2016/272/13:52:19
901
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1834645
40                 A    =         6785082
56  meter
 Y    =       -5621156
28  meter          E    =           
0015620
 Z    =        3308201
60                 I    =           51
27714
 XDOT =       4418
091792                 Wp   =           64
18565
 YDOT =       4195
481065  meter/sec      RA   =          261
42214  deg
 ZDOT =       4668
087080                 TA   =          334
55731
                                          MA   =          334
63413
                                          Ha   =            222
706  n
mi
                                          Hp   =            213
975

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6019177
83                 X    =         1881296
41
 Y    =      -18442113
78  feet           Y    =        -5600378
75  meter
 Z    =       10853679
79                 Z    =         3317227
94
 XDOT =      14495
051812                 XDOT =        4348
172908
 YDOT =      13764
701656  feet/sec       YDOT =        4244
496831  meter/sec
 ZDOT =      15315
246324                 ZDOT =        4689
378684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5704068
76                 X    =         1738600
16
 Y    =       18518317
80  feet           Y    =         5644383
27  meter
 Z    =       10894031
97                 Z    =         3320500
94
 XDOT =     -18337
654087                 XDOT =       -5589
316966
 YDOT =      -3435
841432  feet/sec       YDOT =       -1047
244468  meter/sec
 ZDOT =      15407
529897                 ZDOT =        4696
215113


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   16272
63542080  
00016717  00000-0  10270-3 0  9058
2 25544  51
6402 262
0059 0006646  12
9506 347
1816 15
53979321 21074


Satellite: ISS
Catalog Number: 25544
Epoch time:      16272
63542080   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       262
0059  deg
Eccentricity:     
0006646     
Arg of perigee:    12
9506  deg
Mean anomaly:     347
1816  deg
Mean motion:   15
53979321  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2107
Checksum:              296


Coasting Arc #7 (Orbit 2121)
---------------------------------------

Vector Time (GMT): 2016/273/13:52:19
901
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2580456
35                 A    =         6781458
97  meter
 Y    =        4452066
87  meter          E    =           
0014518
 Z    =       -4431745
73                 I    =           51
27028
 XDOT =      -4055
047434                 Wp   =           47
40417
 YDOT =      -5609
409134  meter/sec      RA   =          256
41075  deg
 ZDOT =      -3271
235659                 TA   =          189
37030
                                          MA   =          189
39742
                                          Ha   =            222
990  n
mi
                                          Hp   =            213
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8466064
14                 X    =        -2608521
10
 Y    =       14606518
62  feet           Y    =         4423052
92  meter
 Z    =      -14539848
20                 Z    =        -4444349
81
 XDOT =     -13303
961396                 XDOT =       -3976
129886
 YDOT =     -18403
573275  feet/sec       YDOT =       -5654
314617  meter/sec
 ZDOT =     -10732
400456                 ZDOT =       -3290
741649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1807293
17                 X    =         -550862
96
 Y    =      -16737184
09  feet           Y    =        -5101493
71  meter
 Z    =      -14595621
73                 Z    =        -4448745
50
 XDOT =      20302
194129                 XDOT =        6188
108771
 YDOT =       7248
316144  feet/sec       YDOT =        2209
286761  meter/sec
 ZDOT =     -10816
664729                 ZDOT =       -3296
919410


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   16273
60006292  
00016717  00000-0  10270-3 0  9067
2 25544  51
6399 257
1977 0006901  17
0339 343
1044 15
53958786 21225


Satellite: ISS
Catalog Number: 25544
Epoch time:      16273
60006292   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       257
1977  deg
Eccentricity:     
0006901     
Arg of perigee:    17
0339  deg
Mean anomaly:     343
1044  deg
Mean motion:   15
53958786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2122
Checksum:              316


Coasting Arc #8 (Orbit 2123)
---------------------------------------

Vector Time (GMT): 2016/273/17:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3980632
05                 A    =         6777886
51  meter
 Y    =        1537195
32  meter          E    =           
0018429
 Z    =       -5281180
56                 I    =           51
26196
 XDOT =      -2227
260139                 Wp   =           66
01140
 YDOT =      -7310
834900  meter/sec      RA   =          255
72228  deg
 ZDOT =       -443
070362                 TA   =          199
69772
                                          MA   =          199
76899
                                          Ha   =            222
971  n
mi
                                          Hp   =            213
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13059816
43                 X    =        -3971871
68
 Y    =        5043291
74  feet           Y    =         1492729
43  meter
 Z    =      -17326707
87                 Z    =        -5300496
51
 XDOT =      -7307
283922                 XDOT =       -2143
190731
 YDOT =     -23985
678806  feet/sec       YDOT =       -7335
271622  meter/sec
 ZDOT =      -1453
642921                 ZDOT =        -453
684620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3727028
29                 X    =        -1135998
22
 Y    =      -13385207
94  feet           Y    =        -4079811
38  meter
 Z    =      -17411314
45                 Z    =        -5306968
64
 XDOT =      23617
368224                 XDOT =        7198
573835
 YDOT =      -4600
480875  feet/sec       YDOT =       -1402
226571  meter/sec
 ZDOT =      -1498
799167                 ZDOT =        -456
833986


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   16273
72868167  
00016717  00000-0  10270-3 0  9078
2 25544  51
6424 256
5580 0006928  17
5952 342
5439 15
53971620 21247


Satellite: ISS
Catalog Number: 25544
Epoch time:      16273
72868167   =   yrday
fracday
Element set:     907
Inclination:       51
6424  deg
RA of node:       256
5580  deg
Eccentricity:     
0006928     
Arg of perigee:    17
5952  deg
Mean anomaly:     342
5439  deg
Mean motion:   15
53971620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2124
Checksum:              329


Coasting Arc #9 (Orbit 2139)
---------------------------------------

Vector Time (GMT): 2016/274/17:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4421557
65                 A    =         6778381
14  meter
 Y    =         175326
70  meter          E    =           
0010866
 Z    =        5131440
45                 I    =           51
27266
 XDOT =       1378
995700                 Wp   =           33
65895
 YDOT =       7409
357913  meter/sec      RA   =          250
69855  deg
 ZDOT =      -1431
027386                 TA   =           70
23416
                                          MA   =           70
11701
                                          Ha   =            222
830  n
mi
                                          Hp   =            213
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14506422
73                 X    =         4394341
93
 Y    =         575218
84  feet           Y    =          224620
11  meter
 Z    =       16835434
55                 Z    =         5152853
32
 XDOT =       4524
264107                 XDOT =        1302
991257
 YDOT =      24308
917036  feet/sec       YDOT =        7424
353589  meter/sec
 ZDOT =      -4694
971738                 ZDOT =       -1424
514218

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1762177
15                 X    =         -537111
60
 Y    =       14300538
99  feet           Y    =         4358804
28  meter
 Z    =       16928920
52                 Z    =         5159934
98
 XDOT =     -23558
521711                 XDOT =       -7180
637418
 YDOT =       2662
643836  feet/sec       YDOT =         811
573841  meter/sec
 ZDOT =      -4667
727360                 ZDOT =       -1422
723299


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   16274
75762549  
00016717  00000-0  10270-3 0  9080
2 25544  51
6422 251
4305 0006855  19
6630 340
4786 15
54004819 21407


Satellite: ISS
Catalog Number: 25544
Epoch time:      16274
75762549   =   yrday
fracday
Element set:     908
Inclination:       51
6422  deg
RA of node:       251
4305  deg
Eccentricity:     
0006855     
Arg of perigee:    19
6630  deg
Mean anomaly:     340
4786  deg
Mean motion:   15
54004819  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2140
Checksum:              311


Coasting Arc #10 (Orbit 2154)
---------------------------------------

Vector Time (GMT): 2016/275/17:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4759201
96                 A    =         6781056
87  meter
 Y    =       -1764009
69  meter          E    =           
0012223
 Z    =       -4505540
43                 I    =           51
29419
 XDOT =       -384
653737                 Wp   =           76
31452
 YDOT =      -6973
612810  meter/sec      RA   =          245
67964  deg
 ZDOT =       3146
669964                 TA   =          225
39718
                                          MA   =          225
49697
                                          Ha   =            223
020  n
mi
                                          Hp   =            213
436

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15614179
67                 X    =        -4717236
40
 Y    =       -5787433
37  feet           Y    =        -1816996
29  meter
 Z    =      -14781956
81                 Z    =        -4528557
54
 XDOT =      -1261
987327                 XDOT =        -321
929789
 YDOT =     -22879
307120  feet/sec       YDOT =       -6977
563103  meter/sec
 ZDOT =      10323
720354                 ZDOT =        3144
954744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6790059
68                 X    =         2069610
19
 Y    =      -15106903
48  feet           Y    =        -4604584
18  meter
 Z    =      -14882197
27                 Z    =        -4536093
73
 XDOT =      21814
722808                 XDOT =        6649
127512
 YDOT =       -326
613098  feet/sec       YDOT =         -99
551672  meter/sec
 ZDOT =      10317
347999                 ZDOT =        3144
727670


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   16275
72225637  
00016717  00000-0  10270-3 0  9091
2 25544  51
6434 246
6229 0006881  23
1679 336
9782 15
53977200 21557


Satellite: ISS
Catalog Number: 25544
Epoch time:      16275
72225637   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:       246
6229  deg
Eccentricity:     
0006881     
Arg of perigee:    23
1679  deg
Mean anomaly:     336
9782  deg
Mean motion:   15
53977200  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2155
Checksum:              332


Coasting Arc #11 (Orbit 2170)
---------------------------------------

Vector Time (GMT): 2016/276/17:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4918569
99                 A    =         6784770
03  meter
 Y    =        3200866
33  meter          E    =           
0016854
 Z    =        3397915
09                 I    =           51
32070
 XDOT =       -783
996521                 Wp   =           68
54583
 YDOT =       6097
489537  meter/sec      RA   =          240
67072  deg
 ZDOT =      -4584
581974                 TA   =           71
52236
                                          MA   =           71
33925
                                          Ha   =            223
149  n
mi
                                          Hp   =            213
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16137040
64                 X    =         4865905
66
 Y    =       10501529
94  feet           Y    =         3255575
07  meter
 Z    =       11148015
39                 Z    =         3421680
28
 XDOT =      -2572
167063                 XDOT =        -829
851668
 YDOT =      20004
886933  feet/sec       YDOT =        6088
465352  meter/sec
 ZDOT =     -15041
279441                 ZDOT =       -4588
502690

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11263814
34                 X    =        -3433210
61
 Y    =       15540243
61  feet           Y    =         4736666
25  meter
 Z    =       11251300
98                 Z    =         3429396
54
 XDOT =     -18727
994325                 XDOT =       -5708
292670
 YDOT =      -2613
650662  feet/sec       YDOT =        -796
640722  meter/sec
 ZDOT =     -15059
373421                 ZDOT =       -4590
097019


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   16276
75118932  
00016717  00000-0  10270-3 0  9106
2 25544  51
6433 241
4952 0006976  28
2084 331
9445 15
53982768 21717


Satellite: ISS
Catalog Number: 25544
Epoch time:      16276
75118932   =   yrday
fracday
Element set:     910
Inclination:       51
6433  deg
RA of node:       241
4952  deg
Eccentricity:     
0006976     
Arg of perigee:    28
2084  deg
Mean anomaly:     331
9445  deg
Mean motion:   15
53982768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2171
Checksum:              327


Coasting Arc #12 (Orbit 2185)
---------------------------------------

Vector Time (GMT): 2016/277/17:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4861487
92                 A    =         6787942
33  meter
 Y    =       -4288554
12  meter          E    =           
0013503
 Z    =       -1995978
51                 I    =           51
34830
 XDOT =       2040
728433                 Wp   =           35
62987
 YDOT =      -4882
593272  meter/sec      RA   =          235
67232  deg
 ZDOT =       5549
989234                 TA   =          302
23489
                                          MA   =          302
36571
                                          Ha   =            223
115  n
mi
                                          Hp   =            213
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15949763
52                 X    =        -4803475
13
 Y    =      -14070059
45  feet           Y    =        -4342594
42  meter
 Z    =       -6548485
94                 Z    =        -2019453
37
 XDOT =       6695
303259                 XDOT =        2068
215237
 YDOT =     -16019
006798  feet/sec       YDOT =       -4859
618108  meter/sec
 ZDOT =      18208
626097                 ZDOT =        5559
970114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14556373
71                 X    =         4436782
71
 Y    =      -15463801
25  feet           Y    =        -4713366
62  meter
 Z    =       -6650340
81                 Z    =        -2027023
88
 XDOT =      14678
451363                 XDOT =        4473
991975
 YDOT =       6008
578575  feet/sec       YDOT =        1831
414750  meter/sec
 ZDOT =      18252
991806                 ZDOT =        5563
511902


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   16277
71580787  
00016717  00000-0  10270-3 0  9115
2 25544  51
6435 236
6880 0006895  30
5146 329
6407 15
54004668 21863


Satellite: ISS
Catalog Number: 25544
Epoch time:      16277
71580787   =   yrday
fracday
Element set:     911
Inclination:       51
6435  deg
RA of node:       236
6880  deg
Eccentricity:     
0006895     
Arg of perigee:    30
5146  deg
Mean anomaly:     329
6407  deg
Mean motion:   15
54004668  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2186
Checksum:              332


Coasting Arc #13 (Orbit 2191)
---------------------------------------

Vector Time (GMT): 2016/278/01:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1174398
76                 A    =         6780402
15  meter
 Y    =        4764025
52  meter          E    =           
0016333
 Z    =       -4695582
46                 I    =           51
32907
 XDOT =      -5791
896516                 Wp   =           57
61180
 YDOT =      -4164
906449  meter/sec      RA   =          233
86166  deg
 ZDOT =      -2775
532792                 TA   =          184
70847
                                          MA   =          184
72385
                                          Ha   =            223
106  n
mi
                                          Hp   =            213
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3853014
32                 X    =        -1204774
50
 Y    =       15630004
97  feet           Y    =         4750722
21  meter
 Z    =      -15405454
26                 Z    =        -4701361
84
 XDOT =     -19002
285156                 XDOT =       -5731
410418
 YDOT =     -13664
391237  feet/sec       YDOT =       -4229
337451  meter/sec
 ZDOT =      -9106
078715                 ZDOT =       -2803
521465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7505024
02                 X    =         2287531
32
 Y    =       14213225
84  feet           Y    =         4332191
24  meter
 Z    =      -15431449
10                 Z    =        -4703505
69
 XDOT =     -22212
231680                 XDOT =       -6770
288216
 YDOT =       1704
878388  feet/sec       YDOT =         519
646933  meter/sec
 ZDOT =      -9227
672835                 ZDOT =       -2812
594680


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   16278
10165448  
00016717  00000-0  10270-3 0  9123
2 25544  51
6431 234
7608 0006366  34
4766 325
6798 15
53984405 21921


Satellite: ISS
Catalog Number: 25544
Epoch time:      16278
10165448   =   yrday
fracday
Element set:     912
Inclination:       51
6431  deg
RA of node:       234
7608  deg
Eccentricity:     
0006366     
Arg of perigee:    34
4766  deg
Mean anomaly:     325
6798  deg
Mean motion:   15
53984405  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2192
Checksum:              328


Coasting Arc #14 (Orbit 2207)
---------------------------------------

Vector Time (GMT): 2016/279/01:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2405845
94                 A    =         6777938
21  meter
 Y    =       -3588083
27  meter          E    =           
0007682
 Z    =        5216282
82                 I    =           51
34199
 XDOT =       5577
700018                 Wp   =           66
29507
 YDOT =       5177
276585  meter/sec      RA   =          228
84462  deg
 ZDOT =        990
590676                 TA   =           14
20131
                                          MA   =           14
17972
                                          Ha   =            222
990  n
mi
                                          Hp   =            213
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7893195
33                 X    =         2420451
06
 Y    =      -11771926
73  feet           Y    =        -3561097
28  meter
 Z    =       17113788
78                 Z    =         5228005
88
 XDOT =      18299
540743                 XDOT =        5514
579892
 YDOT =      16985
815566  feet/sec       YDOT =        5239
297345  meter/sec
 ZDOT =       3249
969409                 ZDOT =        1017
532389

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2171698
07                 X    =         -661933
57
 Y    =      -13942375
30  feet           Y    =        -4249635
99  meter
 Z    =       17165560
18                 Z    =         5232062
74
 XDOT =      23934
351617                 XDOT =        7295
190373
 YDOT =        409
559065  feet/sec       YDOT =         124
833603  meter/sec
 ZDOT =       3366
844658                 ZDOT =        1026
214252


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
13057100  
00016717  00000-0  10270-3 0  9133
2 25544  51
6438 229
6325 0006434  37
8877 322
2727 15
54042426 22085


Satellite: ISS
Catalog Number: 25544
Epoch time:      16279
13057100   =   yrday
fracday
Element set:     913
Inclination:       51
6438  deg
RA of node:       229
6325  deg
Eccentricity:     
0006434     
Arg of perigee:    37
8877  deg
Mean anomaly:     322
2727  deg
Mean motion:   15
54042426  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2208
Checksum:              302


Coasting Arc #15 (Orbit 2222)
---------------------------------------

Vector Time (GMT): 2016/280/01:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3634144
52                 A    =         6777887
48  meter
 Y    =        2322519
72  meter          E    =           
0019044
 Z    =       -5244522
42                 I    =           51
36339
 XDOT =      -4964
129421                 Wp   =           80
40361
 YDOT =      -5757
713018  meter/sec      RA   =          223
82743  deg
 ZDOT =        895
963798                 TA   =          198
18010
                                          MA   =          198
24828
                                          Ha   =            223
206  n
mi
                                          Hp   =            212
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11923046
33                 X    =        -3634369
34
 Y    =        7619815
36  feet           Y    =         2281878
55  meter
 Z    =      -17206438
39                 Z    =        -5262177
26
 XDOT =     -16286
513847                 XDOT =       -4903
728544
 YDOT =     -18890
134574  feet/sec       YDOT =       -5812
887440  meter/sec
 ZDOT =       2939
513772                 ZDOT =         871
996101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3368761
78                 X    =        -1026798
59
 Y    =       13645491
11  feet           Y    =         4159145
69  meter
 Z    =      -17283927
75                 Z    =        -5268141
18
 XDOT =     -23826
935435                 XDOT =       -7262
449920
 YDOT =      -2314
916357  feet/sec       YDOT =        -705
586506  meter/sec
 ZDOT =       2835
706141                 ZDOT =         864
323232


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
09517518  
00016717  00000-0  10270-3 0  9145
2 25544  51
6435 224
8264 0006611  41
3824 318
7828 15
54031173 22236


Satellite: ISS
Catalog Number: 25544
Epoch time:      16280
09517518   =   yrday
fracday
Element set:     914
Inclination:       51
6435  deg
RA of node:       224
8264  deg
Eccentricity:     
0006611     
Arg of perigee:    41
3824  deg
Mean anomaly:     318
7828  deg
Mean motion:   15
54031173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2223
Checksum:              295


Coasting Arc #16 (Orbit 2238)
---------------------------------------

Vector Time (GMT): 2016/281/01:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4758087
64                 A    =         6779989
29  meter
 Y    =       -1006763
07  meter          E    =           
0014096
 Z    =        4717547
09                 I    =           51
39427
 XDOT =       3970
896255                 Wp   =           54
53853
 YDOT =       5976
995528  meter/sec      RA   =          218
81297  deg
 ZDOT =      -2715
715535                 TA   =           62
46549
                                          MA   =           62
32232
                                          Ha   =            223
124  n
mi
                                          Hp   =            212
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15610523
74                 X    =         4746075
69
 Y    =       -3303028
46  feet           Y    =         -953621
73  meter
 Z    =       15477516
71                 Z    =         4740631
98
 XDOT =      13027
874851                 XDOT =        3916
956836
 YDOT =      19609
565382  feet/sec       YDOT =        6021
098944  meter/sec
 ZDOT =      -8909
827871                 ZDOT =       -2696
557088

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8795366
51                 X    =         2680827
71
 Y    =      -13194803
10  feet           Y    =        -4021775
98  meter
 Z    =       15578532
38                 Z    =         4748336
67
 XDOT =      22097
601330                 XDOT =        6735
348885
 YDOT =       4255
086372  feet/sec       YDOT =        1296
950326  meter/sec
 ZDOT =      -8827
050276                 ZDOT =       -2690
484924


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
12407871  
00016717  00000-0  10270-3 0  9151
2 25544  51
6432 219
6982 0006605  45
0863 315
0824 15
54047327 22390


Satellite: ISS
Catalog Number: 25544
Epoch time:      16281
12407871   =   yrday
fracday
Element set:     915
Inclination:       51
6432  deg
RA of node:       219
6982  deg
Eccentricity:     
0006605     
Arg of perigee:    45
0863  deg
Mean anomaly:     315
0824  deg
Mean motion:   15
54047327  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2239
Checksum:              305


Coasting Arc #17 (Orbit 2253)
---------------------------------------

Vector Time (GMT): 2016/282/01:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5653025
20                 A    =         6783468
34  meter
 Y    =        -185233
58  meter          E    =           
0011120
 Z    =       -3751755
28                 I    =           51
43139
 XDOT =      -2614
669039                 Wp   =           75
09463
 YDOT =      -5820
449086  meter/sec      RA   =          213
80951  deg
 ZDOT =       4240
413726                 TA   =          239
91515
                                          MA   =          240
02546
                                          Ha   =            223
189  n
mi
                                          Hp   =            212
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18546670
61                 X    =        -5632309
05
 Y    =        -607721
71  feet           Y    =         -248333
94  meter
 Z    =      -12308908
39                 Z    =        -3779166
32
 XDOT =      -8578
310494                 XDOT =       -2569
987365
 YDOT =     -19095
961568  feet/sec       YDOT =       -5849
437931  meter/sec
 ZDOT =      13912
118522                 ZDOT =        4227
821086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13426102
89                 X    =        -4092276
16
 Y    =       12693535
86  feet           Y    =         3868989
73  meter
 Z    =      -12428654
42                 Z    =        -3788253
87
 XDOT =     -18741
741247                 XDOT =       -5712
482732
 YDOT =      -6297
002089  feet/sec       YDOT =       -1919
326237  meter/sec
 ZDOT =      13857
991507                 ZDOT =        4223
915811


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
08866842  
00016717  00000-0  10270-3 0  9165
2 25544  51
6428 214
8917 0006508  48
5089 311
6622 15
54052537 22544


Satellite: ISS
Catalog Number: 25544
Epoch time:      16282
08866842   =   yrday
fracday
Element set:     916
Inclination:       51
6428  deg
RA of node:       214
8917  deg
Eccentricity:     
0006508     
Arg of perigee:    48
5089  deg
Mean anomaly:     311
6622  deg
Mean motion:   15
54052537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2254
Checksum:              323
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