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

 
Date: December 23rd 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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


362/01:03:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 4

364/11:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 215 3

Coasting Arc #1 (Orbit 1102)
---------------------------------------

Vector Time (GMT): 2017/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6620260
22                 A    =         6788601
98  meter
 Y    =        1029854
98  meter          E    =           
0008222
 Z    =       -1064299
34                 I    =           51
65926
 XDOT =      -1661
988138                 Wp   =           20
92053
 YDOT =      -4615
751292  meter/sec      RA   =          178
37550  deg
 ZDOT =       5893
245404                 TA   =          327
54109
                                          MA   =          327
59162
                                          Ha   =            219
767  n
mi
                                          Hp   =            215
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21720013
84                 X    =        -6626114
50
 Y    =        3378789
29  feet           Y    =          955790
06  meter
 Z    =       -3491795
73                 Z    =        -1096472
36
 XDOT =      -5452
716987                 XDOT =       -1638
876284
 YDOT =     -15143
540983  feet/sec       YDOT =       -4634
208077  meter/sec
 ZDOT =      19334
794633                 ZDOT =        5885
227776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3516468
02                 X    =        -1071819
45
 Y    =      -21674628
08  feet           Y    =        -6606426
64  meter
 Z    =       -3634942
36                 Z    =        -1107930
43
 XDOT =      13525
539340                 XDOT =        4122
584391
 YDOT =      -5419
647635  feet/sec       YDOT =       -1651
908599  meter/sec
 ZDOT =      19299
788659                 ZDOT =        5882
575583


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   17356
50215061  
00016717  00000-0  10270-3 0  9009
2 25544  51
6361 179
5443 0002984 275
4930  84
5882 15
54198711 11032


Satellite: ISS
Catalog Number: 25544
Epoch time:      17356
50215061   =   yrday
fracday
Element set:     900
Inclination:       51
6361  deg
RA of node:       179
5443  deg
Eccentricity:     
0002984     
Arg of perigee:   275
4930  deg
Mean anomaly:      84
5882  deg
Mean motion:   15
54198711  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1103
Checksum:              305


Coasting Arc #2 (Orbit 1118)
---------------------------------------

Vector Time (GMT): 2017/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6745180
49                 A    =         6788821
70  meter
 Y    =        -232464
84  meter          E    =           
0008473
 Z    =        -687878
60                 I    =           51
69296
 XDOT =       -439
416987                 Wp   =          151
72244
 YDOT =       4795
683948  meter/sec      RA   =          173
40815  deg
 ZDOT =      -5966
864330                 TA   =           35
70179
                                          MA   =           35
64516
                                          Ha   =            219
822  n
mi
                                          Hp   =            215
535

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22129857
26                 X    =         6750620
01
 Y    =        -762679
91  feet           Y    =         -157005
15  meter
 Z    =       -2256819
56                 Z    =         -655099
71
 XDOT =      -1441
656780                 XDOT =        -464
027128
 YDOT =      15733
871219  feet/sec       YDOT =        4790
632924  meter/sec
 ZDOT =     -19576
326541                 ZDOT =       -5969
058280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1284436
64                 X    =          391496
29
 Y    =       22120106
45  feet           Y    =         6742208
45  meter
 Z    =       -2111068
61                 Z    =         -643453
71
 XDOT =     -14145
740978                 XDOT =       -4311
621850
 YDOT =      -1035
391019  feet/sec       YDOT =        -315
587183  meter/sec
 ZDOT =     -19586
733372                 ZDOT =       -5970
036332


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   17357
53093391  
00016717  00000-0  10270-3 0  9014
2 25544  51
6360 174
4152 0002950 283
6343  76
4481 15
54242196 11193


Satellite: ISS
Catalog Number: 25544
Epoch time:      17357
53093391   =   yrday
fracday
Element set:     901
Inclination:       51
6360  deg
RA of node:       174
4152  deg
Eccentricity:     
0002950     
Arg of perigee:   283
6343  deg
Mean anomaly:      76
4481  deg
Mean motion:   15
54242196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1119
Checksum:              301


Coasting Arc #3 (Orbit 1134)
---------------------------------------

Vector Time (GMT): 2017/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6334567
68                 A    =         6786842
84  meter
 Y    =        -593768
60  meter          E    =           
0011370
 Z    =        2345524
12                 I    =           51
71800
 XDOT =       2461
740015                 Wp   =           65
97987
 YDOT =      -4856
108457  meter/sec      RA   =          168
43950  deg
 ZDOT =       5402
974337                 TA   =          320
16577
                                          MA   =          320
24917
                                          Ha   =            219
906  n
mi
                                          Hp   =            215
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20782702
35                 X    =        -6338850
51
 Y    =       -1948059
71  feet           Y    =         -664630
16  meter
 Z    =        7695289
12                 Z    =         2314742
58
 XDOT =       8076
574852                 XDOT =        2489
614589
 YDOT =     -15932
114359  feet/sec       YDOT =       -4828
424064  meter/sec
 ZDOT =      17726
293755                 ZDOT =        5415
000017

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1096727
02                 X    =          334282
40
 Y    =      -20894956
68  feet           Y    =        -6368782
80  meter
 Z    =        7558511
98                 Z    =         2303834
45
 XDOT =      14718
087647                 XDOT =        4486
073115
 YDOT =       7223
878978  feet/sec       YDOT =        2201
838312  meter/sec
 ZDOT =      17780
421439                 ZDOT =        5419
472455


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   17358
55971620  
00016717  00000-0  10270-3 0  9028
2 25544  51
6356 169
2853 0002902 281
3147  78
7679 15
54210455 11357


Satellite: ISS
Catalog Number: 25544
Epoch time:      17358
55971620   =   yrday
fracday
Element set:     902
Inclination:       51
6356  deg
RA of node:       169
2853  deg
Eccentricity:     
0002902     
Arg of perigee:   281
3147  deg
Mean anomaly:      78
7679  deg
Mean motion:   15
54210455  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1135
Checksum:              319


Coasting Arc #4 (Orbit 1149)
---------------------------------------

Vector Time (GMT): 2017/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5438100
59                 A    =         6783097
90  meter
 Y    =        1490885
50  meter          E    =           
0003728
 Z    =       -3774708
31                 I    =           51
73926
 XDOT =      -4250
876538                 Wp   =           56
09352
 YDOT =       4755
605639  meter/sec      RA   =          163
46539  deg
 ZDOT =      -4246
771973                 TA   =          169
01628
                                          MA   =          169
00814
                                          Ha   =            219
930  n
mi
                                          Hp   =            215
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17841537
35                 X    =         5439360
50
 Y    =        4891356
64  feet           Y    =         1551705
30  meter
 Z    =      -12384213
62                 Z    =        -3748288
74
 XDOT =     -13946
445335                 XDOT =       -4283
110464
 YDOT =      15602
380707  feet/sec       YDOT =        4707
889410  meter/sec
 ZDOT =     -13932
978915                 ZDOT =       -4267
499336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3843708
88                 X    =        -1171562
47
 Y    =       18175882
52  feet           Y    =         5540008
99  meter
 Z    =      -12266938
03                 Z    =        -3738962
71
 XDOT =     -15052
263059                 XDOT =       -4587
929780
 YDOT =     -12646
993943  feet/sec       YDOT =       -3854
803754  meter/sec
 ZDOT =     -14025
792652                 ZDOT =       -4275
061600


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   17359
52419531  
00016717  00000-0  10270-3 0  9035
2 25544  51
6373 164
4769 0002772 288
9367  71
1485 15
54234235 11502


Satellite: ISS
Catalog Number: 25544
Epoch time:      17359
52419531   =   yrday
fracday
Element set:     903
Inclination:       51
6373  deg
RA of node:       164
4769  deg
Eccentricity:     
0002772     
Arg of perigee:   288
9367  deg
Mean anomaly:      71
1485  deg
Mean motion:   15
54234235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1150
Checksum:              321


Coasting Arc #5 (Orbit 1165)
---------------------------------------

Vector Time (GMT): 2017/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4153013
15                 A    =         6779440
17  meter
 Y    =       -2413595
37  meter          E    =           
0004825
 Z    =        4781756
40                 I    =           51
75708
 XDOT =       5646
150188                 Wp   =          123
23424
 YDOT =      -4466
667724  meter/sec      RA   =          158
48194  deg
 ZDOT =       2644
686745                 TA   =          300
69911
                                          MA   =          300
74664
                                          Ha   =            220
033  n
mi
                                          Hp   =            215
493

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13625371
23                 X    =        -4148942
36
 Y    =       -7918620
00  feet           Y    =        -2460014
67  meter
 Z    =       15688177
15                 Z    =         4761592
20
 XDOT =      18524
114790                 XDOT =        5682
831491
 YDOT =     -14654
421668  feet/sec       YDOT =       -4403
323633  meter/sec
 ZDOT =       8676
793784                 ZDOT =        2672
202783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6863921
99                 X    =         2092123
42
 Y    =      -14284157
87  feet           Y    =        -4353811
32  meter
 Z    =       15598833
13                 Z    =         4754524
34
 XDOT =      14957
535994                 XDOT =        4559
056971
 YDOT =      16813
422572  feet/sec       YDOT =        5124
731200  meter/sec
 ZDOT =       8799
770766                 ZDOT =        2682
170129


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   17360
55296918  
00016717  00000-0  10270-3 0  9043
2 25544  51
6362 159
3469 0002848 290
0024  70
0822 15
54229424 11662


Satellite: ISS
Catalog Number: 25544
Epoch time:      17360
55296918   =   yrday
fracday
Element set:     904
Inclination:       51
6362  deg
RA of node:       159
3469  deg
Eccentricity:     
0002848     
Arg of perigee:   290
0024  deg
Mean anomaly:      70
0822  deg
Mean motion:   15
54229424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1166
Checksum:              309


Coasting Arc #6 (Orbit 1180)
---------------------------------------

Vector Time (GMT): 2017/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2614581
05                 A    =         6777256
35  meter
 Y    =        3350734
27  meter          E    =           
0012287
 Z    =       -5289639
75                 I    =           51
78087
 XDOT =      -6538
413727                 Wp   =           78
02898
 YDOT =       3919
177891  meter/sec      RA   =          153
49397  deg
 ZDOT =       -748
200863                 TA   =          184
82299
                                          MA   =          184
83484
                                          Ha   =            219
996  n
mi
                                          Hp   =            215
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8578021
82                 X    =         2602612
37
 Y    =       10993222
68  feet           Y    =         3379905
65  meter
 Z    =      -17354461
14                 Z    =        -5276967
85
 XDOT =     -21451
488605                 XDOT =       -6578
118690
 YDOT =      12858
195181  feet/sec       YDOT =        3845
838908  meter/sec
 ZDOT =      -2454
727240                 ZDOT =        -780
058669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10143109
70                 X    =        -3091619
84
 Y    =        9668911
39  feet           Y    =         2947084
19  meter
 Z    =      -17298560
71                 Z    =        -5272601
31
 XDOT =     -14075
298195                 XDOT =       -4290
150890
 YDOT =     -19417
778605  feet/sec       YDOT =       -5918
538919  meter/sec
 ZDOT =      -2596
957161                 ZDOT =        -791
552543


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   17361
51744294  
00016717  00000-0  10270-3 0  9056
2 25544  51
6370 154
5396 0002695 293
8689  66
2181 15
54234431 11811


Satellite: ISS
Catalog Number: 25544
Epoch time:      17361
51744294   =   yrday
fracday
Element set:     905
Inclination:       51
6370  deg
RA of node:       154
5396  deg
Eccentricity:     
0002695     
Arg of perigee:   293
8689  deg
Mean anomaly:      66
2181  deg
Mean motion:   15
54234431  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1181
Checksum:              321


Coasting Arc #7 (Orbit 1189)
---------------------------------------

Vector Time (GMT): 2017/362/01:03:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4012785
87                 A    =         6778534
23  meter
 Y    =       -2245344
26  meter          E    =           
0003197
 Z    =        4978755
97                 I    =           51
80191
 XDOT =       5437
767176                 Wp   =          125
04446
 YDOT =      -4967
593724  meter/sec      RA   =          150
80146  deg
 ZDOT =       2139
668794                 TA   =          304
14773
                                          MA   =          304
17804
                                          Ha   =            220
068  n
mi
                                          Hp   =            215
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13165307
98                 X    =        -4011563
95
 Y    =       -7366615
02  feet           Y    =        -2290211
41  meter
 Z    =       16334501
20                 Z    =         4959265
93
 XDOT =      17840
443491                 XDOT =        5482
518533
 YDOT =     -16297
879672  feet/sec       YDOT =       -4906
534788  meter/sec
 ZDOT =       7019
910742                 ZDOT =        2166
192217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1934772
79                 X    =         -589718
75
 Y    =       15055348
30  feet           Y    =         4588870
16  meter
 Z    =       16248120
58                 Z    =         4952427
15
 XDOT =     -20624
410304                 XDOT =       -6286
320261
 YDOT =     -10364
414660  feet/sec       YDOT =       -3159
073588  meter/sec
 ZDOT =       7138
569456                 ZDOT =        2175
835970


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   17362
09612385  
00016717  00000-0  10270-3 0  9066
2 25544  51
6377 151
6576 0003150 300
6033  59
4809 15
54259969 11907


Satellite: ISS
Catalog Number: 25544
Epoch time:      17362
09612385   =   yrday
fracday
Element set:     906
Inclination:       51
6377  deg
RA of node:       151
6576  deg
Eccentricity:     
0003150     
Arg of perigee:   300
6033  deg
Mean anomaly:      59
4809  deg
Mean motion:   15
54259969  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1190
Checksum:              317


Coasting Arc #8 (Orbit 1204)
---------------------------------------

Vector Time (GMT): 2017/363/01:03:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2540055
73                 A    =         6777090
54  meter
 Y    =        3341786
99  meter          E    =           
0012578
 Z    =       -5331400
45                 I    =           51
82521
 XDOT =      -6245
605338                 Wp   =           79
49330
 YDOT =       4429
826485  meter/sec      RA   =          145
81267  deg
 ZDOT =       -197
103727                 TA   =          188
62005
                                          MA   =          188
64167
                                          Ha   =            220
138  n
mi
                                          Hp   =            215
487

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8333516
16                 X    =         2528395
56
 Y    =       10963868
09  feet           Y    =         3370126
82  meter
 Z    =      -17491471
28                 Z    =        -5319089
70
 XDOT =     -20490
831162                 XDOT =       -6293
719228
 YDOT =      14533
551459  feet/sec       YDOT =        4359
714846  meter/sec
 ZDOT =       -646
665772                 ZDOT =        -227
559550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6855099
39                 X    =         2089434
30
 Y    =      -12023230
42  feet           Y    =        -3664680
63  meter
 Z    =      -17437173
09                 Z    =        -5314850
36
 XDOT =      20434
237157                 XDOT =        6228
355486
 YDOT =      12794
690710  feet/sec       YDOT =        3899
821728  meter/sec
 ZDOT =       -782
764041                 ZDOT =        -238
586480


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   17363
06059234  
00016717  00000-0  10270-3 0  9073
2 25544  51
6380 146
8478 0003129 307
3957  52
6911 15
54226422 12057


Satellite: ISS
Catalog Number: 25544
Epoch time:      17363
06059234   =   yrday
fracday
Element set:     907
Inclination:       51
6380  deg
RA of node:       146
8478  deg
Eccentricity:     
0003129     
Arg of perigee:   307
3957  deg
Mean anomaly:      52
6911  deg
Mean motion:   15
54226422  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1205
Checksum:              304


Coasting Arc #9 (Orbit 1220)
---------------------------------------

Vector Time (GMT): 2017/364/01:03:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -980143
36                 A    =         6778047
62  meter
 Y    =       -4362029
38  meter          E    =           
0005512
 Z    =        5094085
32                 I    =           51
85499
 XDOT =       6562
075632                 Wp   =           21
89731
 YDOT =      -3551
083155  meter/sec      RA   =          140
82667  deg
 ZDOT =      -1772
566651                 TA   =           85
22555
                                          MA   =           85
16261
                                          Ha   =            220
259  n
mi
                                          Hp   =            215
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3215693
43                 X    =         -956037
73
 Y    =      -14311120
01  feet           Y    =        -4372855
71  meter
 Z    =       16712878
36                 Z    =         5089382
22
 XDOT =      21529
119527                 XDOT =        6609
907364
 YDOT =     -11650
535285  feet/sec       YDOT =       -3477
433928  meter/sec
 ZDOT =      -5815
507386                 ZDOT =       -1740
574222

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11769937
27                 X    =        -3587476
88
 Y    =        8791805
59  feet           Y    =         2679742
35  meter
 Z    =       16692569
43                 Z    =         5087895
16
 XDOT =     -18689
536129                 XDOT =       -5696
570612
 YDOT =     -14215
045480  feet/sec       YDOT =       -4332
745862  meter/sec
 ZDOT =      -5672
671245                 ZDOT =       -1729
030195


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   17364
08935471  
00016717  00000-0  10270-3 0  9083
2 25544  51
6379 141
7192 0003125 313
1531  46
9360 15
54229644 12212


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
08935471   =   yrday
fracday
Element set:     908
Inclination:       51
6379  deg
RA of node:       141
7192  deg
Eccentricity:     
0003125     
Arg of perigee:   313
1531  deg
Mean anomaly:      46
9360  deg
Mean motion:   15
54229644  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1221
Checksum:              299


Coasting Arc #10 (Orbit 1227)
---------------------------------------

Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3501072
03                 A    =         6777300
59  meter
 Y    =       -2429458
41  meter          E    =           
0000695
 Z    =        5269343
78                 I    =           51
86345
 XDOT =       5218
032627                 Wp   =          100
18817
 YDOT =      -5546
799266  meter/sec      RA   =          138
63031  deg
 ZDOT =        909
377277                 TA   =          341
14023
                                          MA   =          341
14281
                                          Ha   =            220
239  n
mi
                                          Hp   =            215
310

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11486456
79                 X    =        -3499240
87
 Y    =       -7970664
08  feet           Y    =        -2468600
10  meter
 Z    =       17287873
30                 Z    =         5252340
84
 XDOT =      17119
529616                 XDOT =        5275
253302
 YDOT =     -18198
160321  feet/sec       YDOT =       -5488
127810  meter/sec
 ZDOT =       2983
521249                 ZDOT =         934
863288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7036796
76                 X    =         2144815
65
 Y    =      -12188181
84  feet           Y    =        -3714957
82  meter
 Z    =       17212566
73                 Z    =         5246390
34
 XDOT =      18591
693989                 XDOT =        5666
748328
 YDOT =      15109
552391  feet/sec       YDOT =        4605
391569  meter/sec
 ZDOT =       3097
703198                 ZDOT =         944
179935


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   17364
53943689  
00016717  00000-0  10270-3 0  9094
2 25544  51
6375 139
4706 0002864 306
7234  53
3656 15
54246047 12283


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
53943689   =   yrday
fracday
Element set:     909
Inclination:       51
6375  deg
RA of node:       139
4706  deg
Eccentricity:     
0002864     
Arg of perigee:   306
7234  deg
Mean anomaly:      53
3656  deg
Mean motion:   15
54246047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1228
Checksum:              331


Coasting Arc #11 (Orbit 1242)
---------------------------------------

Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2148184
34                 A    =         6777328
26  meter
 Y    =        3718453
40  meter          E    =           
0012056
 Z    =       -5253567
68                 I    =           51
88900
 XDOT =      -5811
954285                 Wp   =           91
05941
 YDOT =       4872
516154  meter/sec      RA   =          133
64637  deg
 ZDOT =       1074
146377                 TA   =          189
19589
                                          MA   =          189
21799
                                          Ha   =            220
194  n
mi
                                          Hp   =            215
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7047848
89                 X    =         2131963
10
 Y    =       12199650
27  feet           Y    =         3742385
81  meter
 Z    =      -17236114
43                 Z    =        -5243171
44
 XDOT =     -19068
091486                 XDOT =       -5871
225773
 YDOT =      15985
945387  feet/sec       YDOT =        4807
191368  meter/sec
 ZDOT =       3524
102287                 ZDOT =        1045
770434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11459300
40                 X    =        -3492794
76
 Y    =        8292306
75  feet           Y    =         2527495
10  meter
 Z    =      -17190385
81                 Z    =        -5239629
60
 XDOT =     -17130
055742                 XDOT =       -5221
240990
 YDOT =     -16642
942978  feet/sec       YDOT =       -5072
769020  meter/sec
 ZDOT =       3397
130324                 ZDOT =        1035
445323


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   17365
50389693  
00016717  00000-0  10270-3 0  9103
2 25544  51
6388 134
6628 0002807 310
7509  49
3400 15
54259598 12438


Satellite: ISS
Catalog Number: 25544
Epoch time:      17365
50389693   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:       134
6628  deg
Eccentricity:     
0002807     
Arg of perigee:   310
7509  deg
Mean anomaly:      49
3400  deg
Mean motion:   15
54259598  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1243
Checksum:              325
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