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

 
Date: December 20th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16915 4846 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


There are no maneuvers



Coasting Arc #1 (Orbit 3379)
---------------------------------------

Vector Time (GMT): 2016/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6088304
07                 A    =         6789182
47  meter
 Y    =       -2664185
81  meter          E    =           
0014158
 Z    =       -1347680
72                 I    =           51
45040
 XDOT =        882
638408                 Wp   =           16
64833
 YDOT =      -4938
559346  meter/sec      RA   =          212
93313  deg
 ZDOT =       5803
869730                 TA   =          328
62984
                                          MA   =          328
71422
                                          Ha   =            222
259  n
mi
                                          Hp   =            215
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19974750
87                 X    =        -6051513
57
 Y    =       -8740767
09  feet           Y    =        -2732063
55  meter
 Z    =       -4421524
67                 Z    =        -1377166
67
 XDOT =       2895
795303                 XDOT =         909
604612
 YDOT =     -16202
622527  feet/sec       YDOT =       -4928
538570  meter/sec
 ZDOT =      19041
567357                 ZDOT =        5808
222606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9548517
81                 X    =         2910388
23
 Y    =      -19571972
55  feet           Y    =        -5965537
23  meter
 Z    =       -4550303
33                 Z    =        -1386932
45
 XDOT =      14646
913456                 XDOT =        4464
379221
 YDOT =       2735
190591  feet/sec       YDOT =         833
686092  meter/sec
 ZDOT =      19061
463040                 ZDOT =        5809
933935


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   16354
50270128  
00016717  00000-0  10270-3 0  9001
2 25544  51
6405 214
0357 0006887 349
0887  11
0115 15
53898308 33806


Satellite: ISS
Catalog Number: 25544
Epoch time:      16354
50270128   =   yrday
fracday
Element set:     900
Inclination:       51
6405  deg
RA of node:       214
0357  deg
Eccentricity:     
0006887     
Arg of perigee:   349
0887  deg
Mean anomaly:      11
0115  deg
Mean motion:   15
53898308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3380
Checksum:              301


Coasting Arc #2 (Orbit 3395)
---------------------------------------

Vector Time (GMT): 2016/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5874598
18                 A    =         6790002
12  meter
 Y    =        3389578
39  meter          E    =           
0007206
 Z    =        -302223
62                 I    =           51
48129
 XDOT =      -2613
700079                 Wp   =          104
19167
 YDOT =       4007
024742  meter/sec      RA   =          207
95184  deg
 ZDOT =      -5986
023734                 TA   =           79
07003
                                          MA   =           78
98895
                                          Ha   =            222
421  n
mi
                                          Hp   =            214
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19273616
07                 X    =         5837726
49
 Y    =       11120664
01  feet           Y    =         3455065
95  meter
 Z    =        -991547
31                 Z    =         -273775
92
 XDOT =      -8575
131494                 XDOT =       -2629
236083
 YDOT =      13146
406634  feet/sec       YDOT =        3977
709945  meter/sec
 ZDOT =     -19639
185479                 ZDOT =       -5998
757934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11573422
21                 X    =        -3527579
09
 Y    =       19011262
16  feet           Y    =         5794632
71  meter
 Z    =        -867421
38                 Z    =         -264390
04
 XDOT =     -11554
813891                 XDOT =       -3521
907274
 YDOT =      -7911
995145  feet/sec       YDOT =       -2411
576120  meter/sec
 ZDOT =     -19695
657867                 ZDOT =       -6003
236518


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   16355
53168127  
00016717  00000-0  10270-3 0  9011
2 25544  51
6412 208
9078 0006763 352
1561   7
9485 15
53884875 33968


Satellite: ISS
Catalog Number: 25544
Epoch time:      16355
53168127   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       208
9078  deg
Eccentricity:     
0006763     
Arg of perigee:   352
1561  deg
Mean anomaly:       7
9485  deg
Mean motion:   15
53884875  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3396
Checksum:              333


Coasting Arc #3 (Orbit 3411)
---------------------------------------

Vector Time (GMT): 2016/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5240412
75                 A    =         6788419
78  meter
 Y    =       -3857966
92  meter          E    =           
0017446
 Z    =        1894799
83                 I    =           51
50430
 XDOT =       4269
754363                 Wp   =           45
17080
 YDOT =      -3035
308540  meter/sec      RA   =          202
97036  deg
 ZDOT =       5609
010945                 TA   =          335
75776
                                          MA   =          335
83975
                                          Ha   =            222
484  n
mi
                                          Hp   =            214
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17192955
22                 X    =        -5206086
57
 Y    =      -12657371
79  feet           Y    =        -3916376
88  meter
 Z    =        6216534
88                 Z    =         1869426
56
 XDOT =      14008
380456                 XDOT =        4276
132587
 YDOT =      -9958
361352  feet/sec       YDOT =       -2987
525822  meter/sec
 ZDOT =      18402
266880                 ZDOT =        5629
767632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12767683
87                 X    =         3891590
04
 Y    =      -17150969
46  feet           Y    =        -5227615
49  meter
 Z    =        6105945
53                 Z    =         1861092
20
 XDOT =       8616
209249                 XDOT =        2626
220579
 YDOT =      13021
496870  feet/sec       YDOT =        3968
952246  meter/sec
 ZDOT =      18493
747897                 ZDOT =        5636
894359


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   16356
56065642  
00016717  00000-0  10270-3 0  9024
2 25544  51
6401 203
7789 0006837 355
9418   4
1678 15
53938053 34122


Satellite: ISS
Catalog Number: 25544
Epoch time:      16356
56065642   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:       203
7789  deg
Eccentricity:     
0006837     
Arg of perigee:   355
9418  deg
Mean anomaly:       4
1678  deg
Mean motion:   15
53938053  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3412
Checksum:              320


Coasting Arc #4 (Orbit 3426)
---------------------------------------

Vector Time (GMT): 2016/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4213193
84                 A    =         6785324
14  meter
 Y    =        4153381
48  meter          E    =           
0007932
 Z    =       -3333468
93                 I    =           51
52254
 XDOT =      -5713
925925                 Wp   =           35
94417
 YDOT =       2047
478030  meter/sec      RA   =          197
98626  deg
 ZDOT =      -4670
161973                 TA   =          182
88859
                                          MA   =          182
89318
                                          Ha   =            222
617  n
mi
                                          Hp   =            214
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13822814
45                 X    =         4182629
05
 Y    =       13626579
66  feet           Y    =         4200325
49  meter
 Z    =      -10936577
85                 Z    =        -3313076
39
 XDOT =     -18746
476131                 XDOT =       -5713
711093
 YDOT =       6717
447604  feet/sec       YDOT =        1983
582470  meter/sec
 ZDOT =     -15322
053718                 ZDOT =       -4697
918128

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13475397
37                 X    =        -4107301
12
 Y    =       14039240
42  feet           Y    =         4279160
48  meter
 Z    =      -10847857
02                 Z    =        -3306426
82
 XDOT =      -5892
378418                 XDOT =       -1795
996942
 YDOT =     -17590
663862  feet/sec       YDOT =       -5361
634345  meter/sec
 ZDOT =     -15444
066527                 ZDOT =       -4707
351477


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   16357
52532210  
00016717  00000-0  10270-3 0  9032
2 25544  51
6388 198
9722 0006873 359
6619    
4528 15
53914412 34274


Satellite: ISS
Catalog Number: 25544
Epoch time:      16357
52532210   =   yrday
fracday
Element set:     903
Inclination:       51
6388  deg
RA of node:       198
9722  deg
Eccentricity:     
0006873     
Arg of perigee:   359
6619  deg
Mean anomaly:        
4528  deg
Mean motion:   15
53914412  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3427
Checksum:              320


Coasting Arc #5 (Orbit 3442)
---------------------------------------

Vector Time (GMT): 2016/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2839064
45                 A    =         6781732
78  meter
 Y    =       -4267045
23  meter          E    =           
0009848
 Z    =        4431164
58                 I    =           51
54165
 XDOT =       6836
065675                 Wp   =           68
16544
 YDOT =      -1115
361422  meter/sec      RA   =          192
99354  deg
 ZDOT =       3303
536076                 TA   =          348
47337
                                          MA   =          348
49591
                                          Ha   =            222
807  n
mi
                                          Hp   =            214
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9314515
90                 X    =        -2812662
92
 Y    =      -13999492
21  feet           Y    =        -4298646
17  meter
 Z    =       14537941
52                 Z    =         4417437
02
 XDOT =      22428
036991                 XDOT =        6831
982717
 YDOT =      -3659
322251  feet/sec       YDOT =       -1038
938942  meter/sec
 ZDOT =      10838
372952                 ZDOT =        3336
733979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13729698
18                 X    =         4184812
01
 Y    =       -9796306
57  feet           Y    =        -2985914
24  meter
 Z    =       14478449
42                 Z    =         4413031
38
 XDOT =       3567
437061                 XDOT =        1087
354816
 YDOT =      21245
015399  feet/sec       YDOT =        6475
480693  meter/sec
 ZDOT =      10984
106349                 ZDOT =        3347
955615


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   16358
55429689  
00016717  00000-0  10270-3 0  9042
2 25544  51
6390 193
8435 0006940   3
1153 357
0042 15
53895154 34432


Satellite: ISS
Catalog Number: 25544
Epoch time:      16358
55429689   =   yrday
fracday
Element set:     904
Inclination:       51
6390  deg
RA of node:       193
8435  deg
Eccentricity:     
0006940     
Arg of perigee:     3
1153  deg
Mean anomaly:     357
0042  deg
Mean motion:   15
53895154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3443
Checksum:              318


Coasting Arc #6 (Orbit 3457)
---------------------------------------

Vector Time (GMT): 2016/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1239484
96                 A    =         6778869
62  meter
 Y    =        4279996
09  meter          E    =           
0017087
 Z    =       -5123210
88                 I    =           51
56280
 XDOT =      -7481
519308                 Wp   =           55
79851
 YDOT =        236
894504  meter/sec      RA   =          187
99419  deg
 ZDOT =      -1606
590642                 TA   =          198
62999
                                          MA   =          198
69261
                                          Ha   =            222
823  n
mi
                                          Hp   =            214
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4066551
71                 X    =         1216419
17
 Y    =       14041981
94  feet           Y    =         4293728
21  meter
 Z    =      -16808434
64                 Z    =        -5117245
52
 XDOT =     -24545
667021                 XDOT =       -7475
808156
 YDOT =        777
212940  feet/sec       YDOT =         153
263162  meter/sec
 ZDOT =      -5270
966674                 ZDOT =       -1642
920105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13837622
03                 X    =        -4217707
20
 Y    =        4805162
15  feet           Y    =         1464613
42  meter
 Z    =      -16782973
74                 Z    =        -5115450
40
 XDOT =      -1531
992155                 XDOT =        -466
951209
 YDOT =     -23441
819735  feet/sec       YDOT =       -7145
066655  meter/sec
 ZDOT =      -5430
307086                 ZDOT =       -1655
157600


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   16359
51895655  
00016717  00000-0  10270-3 0  9050
2 25544  51
6377 189
0355 0006872   7
8782 352
2477 15
53923426 34587


Satellite: ISS
Catalog Number: 25544
Epoch time:      16359
51895655   =   yrday
fracday
Element set:     905
Inclination:       51
6377  deg
RA of node:       189
0355  deg
Eccentricity:     
0006872     
Arg of perigee:     7
8782  deg
Mean anomaly:     352
2477  deg
Mean motion:   15
53923426  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3458
Checksum:              351


Coasting Arc #7 (Orbit 3473)
---------------------------------------

Vector Time (GMT): 2016/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         503444
32                 A    =         6778049
76  meter
 Y    =       -4185178
54  meter          E    =           
0008052
 Z    =        5304720
01                 I    =           51
59147
 XDOT =       7644
106212                 Wp   =           28
62350
 YDOT =        596
401863  meter/sec      RA   =          182
99264  deg
 ZDOT =       -247
854860                 TA   =           63
78095
                                          MA   =           63
69819
                                          Ha   =            222
911  n
mi
                                          Hp   =            214
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1651720
21                 X    =          524438
62
 Y    =      -13730900
71  feet           Y    =        -4179431
71  meter
 Z    =       17403937
04                 Z    =         5307216
28
 XDOT =      25079
088621                 XDOT =        7638
072937
 YDOT =       1956
699025  feet/sec       YDOT =         681
849683  meter/sec
 ZDOT =       -813
172112                 ZDOT =        -210
736330

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13798491
16                 X    =         4205780
11
 Y    =         680085
80  feet           Y    =          207290
15  meter
 Z    =       17415566
69                 Z    =         5308264
73
 XDOT =       -340
041320                 XDOT =        -103
644594
 YDOT =      24150
818235  feet/sec       YDOT =        7361
169398  meter/sec
 ZDOT =       -650
485304                 ZDOT =        -198
267921


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   16360
54792694  
00016717  00000-0  10270-3 0  9065
2 25544  51
6371 183
9075 0006834  11
6977 348
4333 15
53891349 34744


Satellite: ISS
Catalog Number: 25544
Epoch time:      16360
54792694   =   yrday
fracday
Element set:     906
Inclination:       51
6371  deg
RA of node:       183
9075  deg
Eccentricity:     
0006834     
Arg of perigee:    11
6977  deg
Mean anomaly:     348
4333  deg
Mean motion:   15
53891349  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3474
Checksum:              343


Coasting Arc #8 (Orbit 3488)
---------------------------------------

Vector Time (GMT): 2016/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2188737
00                 A    =         6779279
47  meter
 Y    =        4036872
86  meter          E    =           
0014519
 Z    =       -4998450
85                 I    =           51
62796
 XDOT =      -7244
446904                 Wp   =           77
74529
 YDOT =      -1381
734661  meter/sec      RA   =          177
99325  deg
 ZDOT =       2064
380265                 TA   =          212
31995
                                          MA   =          212
40898
                                          Ha   =            222
936  n
mi
                                          Hp   =            213
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7180895
68                 X    =        -2209435
42
 Y    =       13244333
53  feet           Y    =         4012281
65  meter
 Z    =      -16399116
96                 Z    =        -5009133
07
 XDOT =     -23767
870421                 XDOT =       -7238
485417
 YDOT =      -4533
250201  feet/sec       YDOT =       -1462
713790  meter/sec
 ZDOT =       6772
901132                 ZDOT =        2029
202982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13763163
00                 X    =        -4195012
08
 Y    =       -5999363
90  feet           Y    =        -1828606
12  meter
 Z    =      -16446630
27                 Z    =        -5012932
91
 XDOT =       2188
345231                 XDOT =         667
007626
 YDOT =     -23092
645628  feet/sec       YDOT =       -7038
638388  meter/sec
 ZDOT =       6618
833654                 ZDOT =        2017
420498


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   16361
51258384  
00016717  00000-0  10270-3 0  9077
2 25544  51
6367 179
0992 0006741  15
7908 344
3454 15
53928703 34899


Satellite: ISS
Catalog Number: 25544
Epoch time:      16361
51258384   =   yrday
fracday
Element set:     907
Inclination:       51
6367  deg
RA of node:       179
0992  deg
Eccentricity:     
0006741     
Arg of perigee:    15
7908  deg
Mean anomaly:     344
3454  deg
Mean motion:   15
53928703  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3489
Checksum:              340


Coasting Arc #9 (Orbit 3504)
---------------------------------------

Vector Time (GMT): 2016/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3756435
81                 A    =         6782443
81  meter
 Y    =       -3791271
59  meter          E    =           
0015027
 Z    =        4181019
73                 I    =           51
67116
 XDOT =       6348
298038                 Wp   =           53
21729
 YDOT =       2177
017091  meter/sec      RA   =          173
00234  deg
 ZDOT =      -3711
507252                 TA   =           74
95761
                                          MA   =           74
79136
                                          Ha   =            222
977  n
mi
                                          Hp   =            213
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12324264
46                 X    =         3778242
10
 Y    =      -12438555
09  feet           Y    =        -3749143
09  meter
 Z    =       13717256
34                 Z    =         4199320
06
 XDOT =      20827
749467                 XDOT =        6341
511069
 YDOT =       7142
444523  feet/sec       YDOT =        2247
970449  meter/sec
 ZDOT =     -12176
861062                 ZDOT =       -3680
685219

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13561145
43                 X    =         4133437
13
 Y    =       10976085
49  feet           Y    =         3345510
86  meter
 Z    =       13798157
51                 Z    =         4205678
41
 XDOT =      -4287
704771                 XDOT =       -1306
892414
 YDOT =      20509
640379  feet/sec       YDOT =        6251
338388  meter/sec
 ZDOT =     -12042
006302                 ZDOT =       -3670
403521


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   16362
54154872  
00016717  00000-0  10270-3 0  9089
2 25544  51
6371 173
9706 0006753  18
7998 341
3403 15
53917274 35056


Satellite: ISS
Catalog Number: 25544
Epoch time:      16362
54154872   =   yrday
fracday
Element set:     908
Inclination:       51
6371  deg
RA of node:       173
9706  deg
Eccentricity:     
0006753     
Arg of perigee:    18
7998  deg
Mean anomaly:     341
3403  deg
Mean motion:   15
53917274  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3505
Checksum:              329


Coasting Arc #10 (Orbit 3519)
---------------------------------------

Vector Time (GMT): 2016/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4995456
92                 A    =         6785996
68  meter
 Y    =        3477682
09  meter          E    =           
0010402
 Z    =       -2996691
60                 I    =           51
71521
 XDOT =      -5028
798845                 Wp   =           43
31792
 YDOT =      -2949
574935  meter/sec      RA   =          168
02330  deg
 ZDOT =       4977
583819                 TA   =          282
43825
                                          MA   =          282
55463
                                          Ha   =            223
076  n
mi
                                          Hp   =            213
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16389294
36                 X    =        -5019417
47
 Y    =       11409718
14  feet           Y    =         3421685
87  meter
 Z    =       -9831665
36                 Z    =        -3021015
92
 XDOT =     -16498
683876                 XDOT =       -5019
620949
 YDOT =      -9677
083121  feet/sec       YDOT =       -3005
759547  meter/sec
 ZDOT =      16330
655574                 ZDOT =        4953
177352

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13191267
37                 X    =        -4020698
30
 Y    =      -14921790
37  feet           Y    =        -4548161
70  meter
 Z    =       -9938959
64                 Z    =        -3029394
90
 XDOT =       6636
453867                 XDOT =        2022
791139
 YDOT =     -16635
063040  feet/sec       YDOT =       -5070
367214  meter/sec
 ZDOT =      16224
055327                 ZDOT =        4945
092064


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   16363
50620228  
00016717  00000-0  10270-3 0  9090
2 25544  51
6371 169
1629 0006759  24
5133 335
6340 15
53934833 35202


Satellite: ISS
Catalog Number: 25544
Epoch time:      16363
50620228   =   yrday
fracday
Element set:     909
Inclination:       51
6371  deg
RA of node:       169
1629  deg
Eccentricity:     
0006759     
Arg of perigee:    24
5133  deg
Mean anomaly:     335
6340  deg
Mean motion:   15
53934833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3520
Checksum:              306


Coasting Arc #11 (Orbit 3535)
---------------------------------------

Vector Time (GMT): 2016/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5897989
32                 A    =         6788854
72  meter
 Y    =       -3013181
32  meter          E    =           
0015266
 Z    =        1476160
36                 I    =           51
75597
 XDOT =       3369
828686                 Wp   =           92
04394
 YDOT =       3738
026487  meter/sec      RA   =          163
05577  deg
 ZDOT =      -5782
856415                 TA   =           71
87543
                                          MA   =           71
70923
                                          Ha   =            223
136  n
mi
                                          Hp   =            213
477

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19350358
66                 X    =         5924074
67
 Y    =       -9885765
47  feet           Y    =        -2947080
33  meter
 Z    =        4843045
80                 Z    =         1504874
03
 XDOT =      11055
868391                 XDOT =        3355
868954
 YDOT =      12263
866426  feet/sec       YDOT =        3775
632716  meter/sec
 ZDOT =     -18972
626033                 ZDOT =       -5766
520342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12327099
88                 X    =         3757300
04
 Y    =       17859621
50  feet           Y    =         5443612
63  meter
 Z    =        4969543
27                 Z    =         1514716
79
 XDOT =      -9392
324687                 XDOT =       -2862
780565
 YDOT =      11787
720643  feet/sec       YDOT =        3592
897252  meter/sec
 ZDOT =     -18901
553871                 ZDOT =       -5761
193620


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   16364
53516287  
00016717  00000-0  10270-3 0  9105
2 25544  51
6367 164
0348 0006800  26
3018 333
8479 15
53957722 35360


Satellite: ISS
Catalog Number: 25544
Epoch time:      16364
53516287   =   yrday
fracday
Element set:     910
Inclination:       51
6367  deg
RA of node:       164
0348  deg
Eccentricity:     
0006800     
Arg of perigee:    26
3018  deg
Mean anomaly:     333
8479  deg
Mean motion:   15
53957722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3536
Checksum:              319


Coasting Arc #12 (Orbit 3551)
---------------------------------------

Vector Time (GMT): 2016/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6329423
16                 A    =         6789849
07  meter
 Y    =        2426478
52  meter          E    =           
0018900
 Z    =         139735
74                 I    =           51
79204
 XDOT =      -1574
469750                 Wp   =           41
71178
 YDOT =      -4480
176858  meter/sec      RA   =          158
09518  deg
 ZDOT =       6026
966686                 TA   =          319
79119
                                          MA   =          319
93086
                                          Ha   =            223
229  n
mi
                                          Hp   =            213
382

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20765824
00                 X    =        -6356765
01
 Y    =        7960887
54  feet           Y    =         2355545
77  meter
 Z    =         458450
58                 Z    =          108923
26
 XDOT =      -5165
583170                 XDOT =       -1553
530208
 YDOT =     -14698
742974  feet/sec       YDOT =       -4497
667129  meter/sec
 ZDOT =      19773
512748                 ZDOT =        6019
368854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10943570
10                 X    =        -3335600
17
 Y    =      -19363352
39  feet           Y    =        -5901949
81  meter
 Z    =         322817
93                 Z    =           98394
91
 XDOT =      12340
864369                 XDOT =        3761
495460
 YDOT =      -6610
328802  feet/sec       YDOT =       -2014
828219  meter/sec
 ZDOT =      19740
903740                 ZDOT =        6017
027460


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   16365
56412315  
00016717  00000-0  10270-3 0  9117
2 25544  51
6390 158
9067 0006746  31
9993 328
1568 15
53950465 35520


Satellite: ISS
Catalog Number: 25544
Epoch time:      16365
56412315   =   yrday
fracday
Element set:     911
Inclination:       51
6390  deg
RA of node:       158
9067  deg
Eccentricity:     
0006746     
Arg of perigee:    31
9993  deg
Mean anomaly:     328
1568  deg
Mean motion:   15
53950465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3552
Checksum:              331


Coasting Arc #13 (Orbit 3566)
---------------------------------------

Vector Time (GMT): 2016/366/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6342613
96                 A    =         6788496
77  meter
 Y    =       -1631077
53  meter          E    =           
0008653
 Z    =       -1794096
06                 I    =           51
81697
 XDOT =       -275
871007                 Wp   =           91
88825
 YDOT =       5140
841132  meter/sec      RA   =          153
13650  deg
 ZDOT =      -5672
902407                 TA   =          107
75330
                                          MA   =          107
65885
                                          Ha   =            223
357  n
mi
                                          Hp   =            213
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20809100
92                 X    =         6369096
49
 Y    =       -5351304
24  feet           Y    =        -1560001
94  meter
 Z    =       -5886141
92                 Z    =        -1763221
58
 XDOT =       -905
088606                 XDOT =        -305
780685
 YDOT =      16866
276679  feet/sec       YDOT =        5137
589388  meter/sec
 ZDOT =     -18611
884538                 ZDOT =       -5674
314719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8714570
09                 X    =         2656200
96
 Y    =       19679724
91  feet           Y    =         5998380
15  meter
 Z    =       -5750347
86                 Z    =        -1752706
03
 XDOT =     -15328
093942                 XDOT =       -4672
003033
 YDOT =       1370
647002  feet/sec       YDOT =         417
773206  meter/sec
 ZDOT =     -18618
930796                 ZDOT =       -5675
050107


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   16366
52877001  
00016717  00000-0  10270-3 0  9122
2 25544  51
6387 154
0991 0006940  35
2680 324
8931 15
53964719 35675


Satellite: ISS
Catalog Number: 25544
Epoch time:      16366
52877001   =   yrday
fracday
Element set:     912
Inclination:       51
6387  deg
RA of node:       154
0991  deg
Eccentricity:     
0006940     
Arg of perigee:    35
2680  deg
Mean anomaly:     324
8931  deg
Mean motion:   15
53964719  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3567
Checksum:              331
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