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

 
Date: February 10th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 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


042/08:58:44 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 6

042/12:24:48 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 6

043/19:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 6

048/05:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 6

052/22:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 7

Coasting Arc #1 (Orbit 1865)
---------------------------------------

Vector Time (GMT): 2018/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3494274
82                 A    =         6789062
28  meter
 Y    =       -5725334
94  meter          E    =           
0016458
 Z    =        1001337
84                 I    =           51
31852
 XDOT =       3675
281224                 Wp   =           60
07942
 YDOT =       3282
512552  meter/sec      RA   =          294
53188  deg
 ZDOT =       5878
457137                 TA   =          310
82341
                                          MA   =          310
96602
                                          Ha   =            222
189  n
mi
                                          Hp   =            213
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11464156
23                 X    =         3553173
47
 Y    =      -18783907
30  feet           Y    =        -5685930
23  meter
 Z    =        3285229
13                 Z    =         1018454
71
 XDOT =      12058
009265                 XDOT =        3609
748120
 YDOT =      10769
398136  feet/sec       YDOT =        3323
245755  meter/sec
 ZDOT =      19286
276697                 ZDOT =        5896
150880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20997997
18                 X    =         6400189
54
 Y    =       -6544762
76  feet           Y    =        -1994843
69  meter
 Z    =        3362287
42                 Z    =         1024825
21
 XDOT =       1365
626502                 XDOT =         416
242958
 YDOT =      14436
136220  feet/sec       YDOT =        4400
134320  meter/sec
 ZDOT =      19364
504288                 ZDOT =        5902
300907


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   18040
56232320  
00016717  00000-0  10270-3 0  9003
2 25544  51
6421 294
9562 0003081  79
1822 280
9678 15
54068781 18665


Satellite: ISS
Catalog Number: 25544
Epoch time:      18040
56232320   =   yrday
fracday
Element set:     900
Inclination:       51
6421  deg
RA of node:       294
9562  deg
Eccentricity:     
0003081     
Arg of perigee:    79
1822  deg
Mean anomaly:     280
9678  deg
Mean motion:   15
54068781  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1866
Checksum:              312


Coasting Arc #2 (Orbit 1880)
---------------------------------------

Vector Time (GMT): 2018/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3947777
55                 A    =         6786587
60  meter
 Y    =        4863324
98  meter          E    =           
0007512
 Z    =       -2613741
69                 I    =           51
29731
 XDOT =      -2666
409906                 Wp   =          110
58710
 YDOT =      -4953
099685  meter/sec      RA   =          289
53615  deg
 ZDOT =      -5203
550833                 TA   =           98
98046
                                          MA   =           98
89542
                                          Ha   =            222
183  n
mi
                                          Hp   =            213
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12952026
08                 X    =        -3989171
20
 Y    =       15955790
61  feet           Y    =         4818946
74  meter
 Z    =       -8575268
01                 Z    =        -2633018
89
 XDOT =      -8748
063997                 XDOT =       -2585
549171
 YDOT =     -16250
327049  feet/sec       YDOT =       -4982
465263  meter/sec
 ZDOT =     -17072
017170                 ZDOT =       -5216
306638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20157991
87                 X    =        -6144155
92
 Y    =        3808684
78  feet           Y    =         1160887
12  meter
 Z    =       -8661797
68                 Z    =        -2640115
93
 XDOT =       4220
519205                 XDOT =        1286
414254
 YDOT =     -16506
173862  feet/sec       YDOT =       -5031
081793  meter/sec
 ZDOT =     -17128
022444                 ZDOT =       -5220
621241


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   18041
52688660  
00016717  00000-0  10270-3 0  9013
2 25544  51
6419 290
1489 0003003  84
4747 275
6748 15
54054067 18815


Satellite: ISS
Catalog Number: 25544
Epoch time:      18041
52688660   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:       290
1489  deg
Eccentricity:     
0003003     
Arg of perigee:    84
4747  deg
Mean anomaly:     275
6748  deg
Mean motion:   15
54054067  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1881
Checksum:              322


Coasting Arc #3 (Orbit 1894)
---------------------------------------

Vector Time (GMT): 2018/042/08:58:44
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4450433
48                 A    =         6779846
07  meter
 Y    =       -1970755
61  meter          E    =           
0010439
 Z    =        4712691
12                 I    =           51
26416
 XDOT =        304
384005                 Wp   =          109
15716
 YDOT =       7174
310001  meter/sec      RA   =          285
15538  deg
 ZDOT =       2704
425340                 TA   =          313
93800
                                          MA   =          314
02410
                                          Ha   =            222
017  n
mi
                                          Hp   =            213
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14601159
72                 X    =         4449248
93
 Y    =       -6465733
62  feet           Y    =        -1920994
36  meter
 Z    =       15461585
02                 Z    =         4734306
50
 XDOT =        998
635186                 XDOT =         210
999894
 YDOT =      23537
762471  feet/sec       YDOT =        7177
191729  meter/sec
 ZDOT =       8872
786550                 ZDOT =        2705
676988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7749536
55                 X    =         2362058
74
 Y    =       13854644
49  feet           Y    =         4222895
64  meter
 Z    =       15558074
99                 Z    =         4742101
26
 XDOT =     -22346
639056                 XDOT =       -6811
255584
 YDOT =       2500
426014  feet/sec       YDOT =         762
129849  meter/sec
 ZDOT =       8877
271525                 ZDOT =        2705
792361


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   18042
42714455  
00016717  00000-0  10270-3 0  9026
2 25544  51
6398 285
6610 0003053  87
8044 272
3458 15
54104000 18958


Satellite: ISS
Catalog Number: 25544
Epoch time:      18042
42714455   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       285
6610  deg
Eccentricity:     
0003053     
Arg of perigee:    87
8044  deg
Mean anomaly:     272
3458  deg
Mean motion:   15
54104000  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1895
Checksum:              298


Coasting Arc #4 (Orbit 1896)
---------------------------------------

Vector Time (GMT): 2018/042/12:24:48
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1017757
32                 A    =         6785396
93  meter
 Y    =        5953998
55  meter          E    =           
0016110
 Z    =        3076100
51                 I    =           51
28273
 XDOT =      -4888
968993                 Wp   =           93
35439
 YDOT =       3360
213671  meter/sec      RA   =          284
39441  deg
 ZDOT =      -4865
187275                 TA   =           51
08132
                                          MA   =           50
93781
                                          Ha   =            222
168  n
mi
                                          Hp   =            213
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3339098
83                 X    =          936160
69
 Y    =       19534115
98  feet           Y    =         5964923
62  meter
 Z    =       10092193
29                 Z    =         3080846
06
 XDOT =     -16039
924518                 XDOT =       -4902
548416
 YDOT =      11024
323069  feet/sec       YDOT =        3305
465865  meter/sec
 ZDOT =     -15961
900508                 ZDOT =       -4888
968746

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7943202
83                 X    =        -2421088
22
 Y    =       18144648
20  feet           Y    =         5530488
77  meter
 Z    =       10112413
37                 Z    =         3082263
59
 XDOT =     -18045
501356                 XDOT =       -5500
268813
 YDOT =       1094
015505  feet/sec       YDOT =         333
455926  meter/sec
 ZDOT =     -16068
239198                 ZDOT =       -4897
599307


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   18042
55575296  
00016717  00000-0  10270-3 0  9039
2 25544  51
6412 285
0208 0003137  84
9338 275
2173 15
54095595 18975


Satellite: ISS
Catalog Number: 25544
Epoch time:      18042
55575296   =   yrday
fracday
Element set:     903
Inclination:       51
6412  deg
RA of node:       285
0208  deg
Eccentricity:     
0003137     
Arg of perigee:    84
9338  deg
Mean anomaly:     275
2173  deg
Mean motion:   15
54095595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1897
Checksum:              328


Coasting Arc #5 (Orbit 1911)
---------------------------------------

Vector Time (GMT): 2018/043/12:24:48
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -192295
17                 A    =         6788390
67  meter
 Y    =       -6596500
77  meter          E    =           
0010191
 Z    =       -1579878
21                 I    =           51
28550
 XDOT =       4888
207407                 Wp   =           50
52680
 YDOT =      -1502
744049  meter/sec      RA   =          279
39367  deg
 ZDOT =       5710
547351                 TA   =          292
11254
                                          MA   =          292
22071
                                          Ha   =            222
138  n
mi
                                          Hp   =            213
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -630889
65                 X    =         -110842
98
 Y    =      -21642062
88  feet           Y    =        -6598195
75  meter
 Z    =       -5183327
48                 Z    =        -1580614
33
 XDOT =      16037
425877                 XDOT =        4876
909997
 YDOT =      -4930
262627  feet/sec       YDOT =       -1448
143804  meter/sec
 ZDOT =      18735
391572                 ZDOT =        5734
264625

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11016990
97                 X    =         3357978
85
 Y    =      -18638106
10  feet           Y    =        -5680894
74  meter
 Z    =       -5185624
56                 Z    =        -1580578
37
 XDOT =      14735
699710                 XDOT =        4491
441272
 YDOT =       3496
510302  feet/sec       YDOT =        1065
736340  meter/sec
 ZDOT =      18841
164021                 ZDOT =        5742
786794


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   18043
52031321  
00016717  00000-0  10270-3 0  9044
2 25544  51
6412 280
2128 0002956  87
8977 272
2514 15
54085162 19125


Satellite: ISS
Catalog Number: 25544
Epoch time:      18043
52031321   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:       280
2128  deg
Eccentricity:     
0002956     
Arg of perigee:    87
8977  deg
Mean anomaly:     272
2514  deg
Mean motion:   15
54085162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1912
Checksum:              293


Coasting Arc #6 (Orbit 1916)
---------------------------------------

Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3608873
09                 A    =         6779009
31  meter
 Y    =        2887406
60  meter          E    =           
0008798
 Z    =        4952880
25                 I    =           51
25139
 XDOT =      -2652
452543                 Wp   =           71
38352
 YDOT =       6893
283186  meter/sec      RA   =          277
98319  deg
 ZDOT =      -2080
121174                 TA   =           38
98813
                                          MA   =           38
92473
                                          Ha   =            222
161  n
mi
                                          Hp   =            213
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11840134
79                 X    =         3552259
18
 Y    =        9473118
77  feet           Y    =         2927447
07  meter
 Z    =       16249607
13                 Z    =         4970272
93
 XDOT =      -8702
272123                 XDOT =       -2719
234069
 YDOT =      22615
758485  feet/sec       YDOT =        6863
248193  meter/sec
 ZDOT =      -6824
544534                 ZDOT =       -2093
167933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13061712
22                 X    =         3981209
88
 Y    =       -7537427
22  feet           Y    =        -2297407
82  meter
 Z    =       16326584
70                 Z    =         4976343
02
 XDOT =      17435
429064                 XDOT =        5314
318779
 YDOT =      15262
627501  feet/sec       YDOT =        4652
048862  meter/sec
 ZDOT =      -6883
625147                 ZDOT =       -2098
128945


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   18043
84183497  
00016717  00000-0  10270-3 0  9052
2 25544  51
6402 278
6047 0003239 100
0300 260
1218 15
54058089 19178


Satellite: ISS
Catalog Number: 25544
Epoch time:      18043
84183497   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       278
6047  deg
Eccentricity:     
0003239     
Arg of perigee:   100
0300  deg
Mean anomaly:     260
1218  deg
Mean motion:   15
54058089  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1917
Checksum:              294


Coasting Arc #7 (Orbit 1931)
---------------------------------------

Vector Time (GMT): 2018/044/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3090741
52                 A    =         6782172
25  meter
 Y    =       -4412320
92  meter          E    =           
0010758
 Z    =       -4131443
80                 I    =           51
25838
 XDOT =       3304
380686                 Wp   =          107
39282
 YDOT =      -5810
365572  meter/sec      RA   =          272
96507  deg
 ZDOT =       3738
299562                 TA   =          201
32650
                                          MA   =          201
37137
                                          Ha   =            222
187  n
mi
                                          Hp   =            213
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10140228
07                 X    =        -3021104
17
 Y    =      -14476118
50  feet           Y    =        -4446494
50  meter
 Z    =      -13554605
63                 Z    =        -4146287
87
 XDOT =      10841
143984                 XDOT =        3350
949947
 YDOT =     -19062
879173  feet/sec       YDOT =       -5773
153197  meter/sec
 ZDOT =      12264
762341                 ZDOT =        3754
464015

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17049847
75                 X    =        -5196793
59
 Y    =        4461728
52  feet           Y    =         1359934
85  meter
 Z    =      -13620030
70                 Z    =        -4151385
36
 XDOT =     -13876
311505                 XDOT =       -4229
499747
 YDOT =     -15413
411150  feet/sec       YDOT =       -4698
007719  meter/sec
 ZDOT =      12337
544426                 ZDOT =        3760
483541


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   18044
80639156  
00016717  00000-0  10270-3 0  9068
2 25544  51
6399 273
7977 0003125 102
6557 257
4945 15
54081421 19326


Satellite: ISS
Catalog Number: 25544
Epoch time:      18044
80639156   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       273
7977  deg
Eccentricity:     
0003125     
Arg of perigee:   102
6557  deg
Mean anomaly:     257
4945  deg
Mean motion:   15
54081421  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1932
Checksum:              328


Coasting Arc #8 (Orbit 1947)
---------------------------------------

Vector Time (GMT): 2018/045/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2488708
66                 A    =         6786010
22  meter
 Y    =        5623488
76  meter          E    =           
0016516
 Z    =        2850965
88                 I    =           51
26966
 XDOT =      -3889
508260                 Wp   =          100
79685
 YDOT =       4286
125821  meter/sec      RA   =          267
95582  deg
 ZDOT =      -5037
174411                 TA   =           46
57633
                                          MA   =           46
43900
                                          Ha   =            222
183  n
mi
                                          Hp   =            213
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8165054
66                 X    =         2411792
19
 Y    =       18449766
28  feet           Y    =         5650889
29  meter
 Z    =        9353562
60                 Z    =         2862867
74
 XDOT =     -12760
853872                 XDOT =       -3912
680501
 YDOT =      14062
092587  feet/sec       YDOT =        4242
500838  meter/sec
 ZDOT =     -16526
162765                 ZDOT =       -5056
124310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20086853
11                 X    =         6122472
83
 Y    =       -1612942
14  feet           Y    =         -491624
77  meter
 Z    =        9405736
34                 Z    =         2866868
44
 XDOT =       9023
653530                 XDOT =        2750
409596
 YDOT =      15094
350881  feet/sec       YDOT =        4600
758148  meter/sec
 ZDOT =     -16611
111387                 ZDOT =       -5063
066751


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   18045
83525220  
00016717  00000-0  10270-3 0  9079
2 25544  51
6392 268
6691 0003224 108
1875 251
9628 15
54071770 19489


Satellite: ISS
Catalog Number: 25544
Epoch time:      18045
83525220   =   yrday
fracday
Element set:     907
Inclination:       51
6392  deg
RA of node:       268
6691  deg
Eccentricity:     
0003224     
Arg of perigee:   108
1875  deg
Mean anomaly:     251
9628  deg
Mean motion:   15
54071770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1948
Checksum:              322


Coasting Arc #9 (Orbit 1962)
---------------------------------------

Vector Time (GMT): 2018/046/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1852481
07                 A    =         6788726
88  meter
 Y    =       -6394589
67  meter          E    =           
0010297
 Z    =       -1315166
13                 I    =           51
28211
 XDOT =       4377
837727                 Wp   =           54
23130
 YDOT =      -2452
259436  meter/sec      RA   =          262
95600  deg
 ZDOT =       5794
847488                 TA   =          291
38657
                                          MA   =          291
49640
                                          Ha   =            222
169  n
mi
                                          Hp   =            213
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6077693
81                 X    =        -1774449
14
 Y    =      -20979624
91  feet           Y    =        -6414869
18  meter
 Z    =       -4314849
50                 Z    =        -1323974
64
 XDOT =      14362
984667                 XDOT =        4376
786591
 YDOT =      -8045
470590  feet/sec       YDOT =       -2403
308920  meter/sec
 ZDOT =      19011
966825                 ZDOT =        5816
110581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21820650
41                 X    =        -6650934
24
 Y    =        -781091
70  feet           Y    =         -238076
75  meter
 Z    =       -4353166
80                 Z    =        -1326845
24
 XDOT =      -3270
212278                 XDOT =        -996
760702
 YDOT =     -14442
508673  feet/sec       YDOT =       -4402
076643  meter/sec
 ZDOT =      19106
946651                 ZDOT =        5823
797339


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   18046
79980584  
00016717  00000-0  10270-3 0  9084
2 25544  51
6403 263
8613 0003108 107
6566 252
4926 15
54077055 19631


Satellite: ISS
Catalog Number: 25544
Epoch time:      18046
79980584   =   yrday
fracday
Element set:     908
Inclination:       51
6403  deg
RA of node:       263
8613  deg
Eccentricity:     
0003108     
Arg of perigee:   107
6566  deg
Mean anomaly:     252
4926  deg
Mean motion:   15
54077055  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1963
Checksum:              329


Coasting Arc #10 (Orbit 1978)
---------------------------------------

Vector Time (GMT): 2018/047/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1094834
89                 A    =         6789367
04  meter
 Y    =        6682350
59  meter          E    =           
0014210
 Z    =        -402998
23                 I    =           51
28874
 XDOT =      -4797
409801                 Wp   =          132
30654
 YDOT =        434
850830  meter/sec      RA   =          257
96134  deg
 ZDOT =      -5967
254783                 TA   =           52
05994
                                          MA   =           51
93161
                                          Ha   =            222
153  n
mi
                                          Hp   =            213
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3591977
97                 X    =         1021987
17
 Y    =       21923722
41  feet           Y    =         6694186
44  meter
 Z    =       -1322172
68                 Z    =         -397857
53
 XDOT =     -15739
533467                 XDOT =       -4772
930781
 YDOT =       1426
675951  feet/sec       YDOT =         381
339259  meter/sec
 ZDOT =     -19577
607556                 ZDOT =       -5990
498962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22010634
74                 X    =         6708841
47
 Y    =        3023489
56  feet           Y    =          921559
62  meter
 Z    =       -1300199
92                 Z    =         -396300
94
 XDOT =      -3020
299382                 XDOT =        -920
587251
 YDOT =      13731
244553  feet/sec       YDOT =        4185
283340  meter/sec
 ZDOT =     -19681
126975                 ZDOT =       -5998
807502


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   18047
82866112  
00016717  00000-0  10270-3 0  9090
2 25544  51
6396 258
7324 0003176 112
4494 247
6995 15
54092476 19796


Satellite: ISS
Catalog Number: 25544
Epoch time:      18047
82866112   =   yrday
fracday
Element set:     909
Inclination:       51
6396  deg
RA of node:       258
7324  deg
Eccentricity:     
0003176     
Arg of perigee:   112
4494  deg
Mean anomaly:     247
6995  deg
Mean motion:   15
54092476  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1979
Checksum:              350


Coasting Arc #11 (Orbit 1985)
---------------------------------------

Vector Time (GMT): 2018/048/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4192912
30                 A    =         6782582
65  meter
 Y    =        3535843
04  meter          E    =           
0013667
 Z    =        3979366
82                 I    =           51
26767
 XDOT =      -1633
760551                 Wp   =           83
89020
 YDOT =       6381
246378  meter/sec      RA   =          255
72716  deg
 ZDOT =      -3935
479237                 TA   =           47
27556
                                          MA   =           47
16059
                                          Ha   =            222
021  n
mi
                                          Hp   =            213
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13756273
94                 X    =         4133732
69
 Y    =       11600534
92  feet           Y    =         3582400
54  meter
 Z    =       13055665
43                 Z    =         3999590
02
 XDOT =      -5360
106796                 XDOT =       -1685
879902
 YDOT =      20935
847697  feet/sec       YDOT =        6362
684769  meter/sec
 ZDOT =     -12911
677286                 ZDOT =       -3943
542466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17563781
52                 X    =        -5353440
61
 Y    =        3602091
79  feet           Y    =         1097917
58  meter
 Z    =       13145204
32                 Z    =         4006658
28
 XDOT =     -12960
228197                 XDOT =       -3950
277554
 YDOT =     -15785
133650  feet/sec       YDOT =       -4811
308736  meter/sec
 ZDOT =     -12948
427115                 ZDOT =       -3946
680585


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   18048
27878499  
00016717  00000-0  10270-3 0  9103
2 25544  51
6379 256
4914 0003019 102
4577 257
6913 15
54104604 19860


Satellite: ISS
Catalog Number: 25544
Epoch time:      18048
27878499   =   yrday
fracday
Element set:     910
Inclination:       51
6379  deg
RA of node:       256
4914  deg
Eccentricity:     
0003019     
Arg of perigee:   102
4577  deg
Mean anomaly:     257
6913  deg
Mean motion:   15
54104604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1986
Checksum:              337


Coasting Arc #12 (Orbit 2000)
---------------------------------------

Vector Time (GMT): 2018/049/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3965554
67                 A    =         6786317
33  meter
 Y    =       -4807433
43  meter          E    =           
0007134
 Z    =       -2689828
47                 I    =           51
28877
 XDOT =       2614
761219                 Wp   =           75
51935
 YDOT =      -5032
452764  meter/sec      RA   =          250
72015  deg
 ZDOT =       5152
695838                 TA   =          253
95965
                                          MA   =          254
03822
                                          Ha   =            222
099  n
mi
                                          Hp   =            213
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13010349
98                 X    =        -3898436
41
 Y    =      -15772419
40  feet           Y    =        -4851403
98  meter
 Z    =       -8824896
55                 Z    =        -2708927
88
 XDOT =       8578
612924                 XDOT =        2645
812542
 YDOT =     -16510
671798  feet/sec       YDOT =       -5003
038570  meter/sec
 ZDOT =      16905
170071                 ZDOT =        5165
473115

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20393099
69                 X    =         6215816
79
 Y    =        -814540
27  feet           Y    =         -248271
87  meter
 Z    =       -8909277
67                 Z    =        -2715547
83
 XDOT =       7999
910174                 XDOT =        2438
372621
 YDOT =      15224
994508  feet/sec       YDOT =        4640
578326  meter/sec
 ZDOT =      16962
709403                 ZDOT =        5170
233826


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   18049
24333529  
00016717  00000-0  10270-3 0  9112
2 25544  51
6376 251
6835 0002979 107
0946 253
0533 15
54088002 20011


Satellite: ISS
Catalog Number: 25544
Epoch time:      18049
24333529   =   yrday
fracday
Element set:     911
Inclination:       51
6376  deg
RA of node:       251
6835  deg
Eccentricity:     
0002979     
Arg of perigee:   107
0946  deg
Mean anomaly:     253
0533  deg
Mean motion:   15
54088002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2001
Checksum:              297


Coasting Arc #13 (Orbit 2016)
---------------------------------------

Vector Time (GMT): 2018/050/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3518158
50                 A    =         6788912
39  meter
 Y    =        5695715
46  meter          E    =           
0016549
 Z    =        1080343
73                 I    =           51
31073
 XDOT =      -3630
505850                 Wp   =          120
94654
 YDOT =       3365
127591  meter/sec      RA   =          245
72239  deg
 ZDOT =      -5860
118301                 TA   =           47
27643
                                          MA   =           47
13723
                                          Ha   =            222
069  n
mi
                                          Hp   =            213
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11542514
78                 X    =         3448958
34
 Y    =       18686730
51  feet           Y    =         5734671
12  meter
 Z    =        3544434
82                 Z    =         1097264
79
 XDOT =     -11911
108432                 XDOT =       -3639
400872
 YDOT =      11040
444853  feet/sec       YDOT =        3324
478434  meter/sec
 ZDOT =     -19226
109910                 ZDOT =       -5877
775715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21885277
99                 X    =        -6670632
73
 Y    =       -1709934
50  feet           Y    =         -521188
04  meter
 Z    =        3619018
38                 Z    =         1103076
80
 XDOT =      -2095
976707                 XDOT =        -638
853700
 YDOT =     -14430
159352  feet/sec       YDOT =       -4398
312570  meter/sec
 ZDOT =     -19305
146759                 ZDOT =       -5884
208732


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   18050
27218655  
00016717  00000-0  10270-3 0  9120
2 25544  51
6390 246
5542 0002965 110
5712 249
5758 15
54095796 20174


Satellite: ISS
Catalog Number: 25544
Epoch time:      18050
27218655   =   yrday
fracday
Element set:     912
Inclination:       51
6390  deg
RA of node:       246
5542  deg
Eccentricity:     
0002965     
Arg of perigee:   110
5712  deg
Mean anomaly:     249
5758  deg
Mean motion:   15
54095796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2017
Checksum:              318


Coasting Arc #14 (Orbit 2032)
---------------------------------------

Vector Time (GMT): 2018/051/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2877489
87                 A    =         6789282
34  meter
 Y    =       -6113766
90  meter          E    =           
0014747
 Z    =         598535
09                 I    =           51
32611
 XDOT =       4581
164736                 Wp   =           61
52138
 YDOT =      -1563
585214  meter/sec      RA   =          240
73001  deg
 ZDOT =       5947
932670                 TA   =          304
96783
                                          MA   =          305
10623
                                          Ha   =            222
073  n
mi
                                          Hp   =            213
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9440583
56                 X    =        -2811817
55
 Y    =      -20058290
36  feet           Y    =        -6145577
71  meter
 Z    =        1963697
79                 Z    =          584717
53
 XDOT =      15030
068033                 XDOT =        4569
417111
 YDOT =      -5129
872750  feet/sec       YDOT =       -1512
420568  meter/sec
 ZDOT =      19514
214795                 ZDOT =        5970
157736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21844147
57                 X    =         6658096
18
 Y    =        3811517
76  feet           Y    =         1161750
61  meter
 Z    =        1902968
39                 Z    =          580024
76
 XDOT =      -4102
957583                 XDOT =       -1250
581471
 YDOT =      13544
711028  feet/sec       YDOT =        4128
427921  meter/sec
 ZDOT =      19613
351909                 ZDOT =        5978
149662


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   18051
30103505  
00016717  00000-0  10270-3 0  9133
2 25544  51
6387 241
4255 0002957 112
0747 248
0720 15
54096402 20337


Satellite: ISS
Catalog Number: 25544
Epoch time:      18051
30103505   =   yrday
fracday
Element set:     913
Inclination:       51
6387  deg
RA of node:       241
4255  deg
Eccentricity:     
0002957     
Arg of perigee:   112
0747  deg
Mean anomaly:     248
0720  deg
Mean motion:   15
54096402  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2033
Checksum:              274


Coasting Arc #15 (Orbit 2047)
---------------------------------------

Vector Time (GMT): 2018/052/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1959046
38                 A    =         6787248
46  meter
 Y    =        6090296
46  meter          E    =           
0008804
 Z    =       -2261917
87                 I    =           51
33735
 XDOT =      -5419
263446                 Wp   =          130
15148
 YDOT =       -260
515294  meter/sec      RA   =          235
73696  deg
 ZDOT =      -5414
631320                 TA   =           75
11917
                                          MA   =           75
02168
                                          Ha   =            222
042  n
mi
                                          Hp   =            213
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6427317
51                 X    =         1901784
54
 Y    =       19981287
60  feet           Y    =         6111883
49  meter
 Z    =       -7420990
40                 Z    =        -2252541
22
 XDOT =     -17779
735715                 XDOT =       -5389
646336
 YDOT =       -854
708970  feet/sec       YDOT =        -320
952111  meter/sec
 ZDOT =     -17764
538453                 ZDOT =       -5440
884024

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20171259
54                 X    =        -6148199
91
 Y    =       -5855684
04  feet           Y    =        -1784812
49  meter
 Z    =       -7380014
63                 Z    =        -2249428
46
 XDOT =      10195
479743                 XDOT =        3107
582226
 YDOT =     -12665
830573  feet/sec       YDOT =       -3860
545159  meter/sec
 ZDOT =     -17881
379588                 ZDOT =       -5450
244498


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   18052
26557892  
00016717  00000-0  10270-3 0  9142
2 25544  51
6397 236
6176 0002929 116
4781 243
6672 15
54104872 20485


Satellite: ISS
Catalog Number: 25544
Epoch time:      18052
26557892   =   yrday
fracday
Element set:     914
Inclination:       51
6397  deg
RA of node:       236
6176  deg
Eccentricity:     
0002929     
Arg of perigee:   116
4781  deg
Mean anomaly:     243
6672  deg
Mean motion:   15
54104872  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2048
Checksum:              331


Coasting Arc #16 (Orbit 2058)
---------------------------------------

Vector Time (GMT): 2018/052/22:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -101751
94                 A    =         6781920
30  meter
 Y    =        5338181
35  meter          E    =           
0010107
 Z    =       -4191261
47                 I    =           51
33262
 XDOT =      -6028
525996                 Wp   =           84
37061
 YDOT =      -2985
576806  meter/sec      RA   =          232
17643  deg
 ZDOT =      -3662
880695                 TA   =          147
89342
                                          MA   =          147
83183
                                          Ha   =            222
042  n
mi
                                          Hp   =            213
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -333831
84                 X    =         -141078
59
 Y    =       17513718
35  feet           Y    =         5336823
27  meter
 Z    =      -13750857
85                 Z    =        -4191851
69
 XDOT =     -19778
628596                 XDOT =       -5976
900215
 YDOT =      -9795
199495  feet/sec       YDOT =       -3052
703558  meter/sec
 ZDOT =     -12017
325114                 ZDOT =       -3692
039320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12987992
27                 X    =         3958740
05
 Y    =      -11750029
23  feet           Y    =        -3581408
91  meter
 Z    =      -13754153
39                 Z    =        -4192265
95
 XDOT =       5387
741833                 XDOT =        1642
183711
 YDOT =      20148
339753  feet/sec       YDOT =        6141
213957  meter/sec
 ZDOT =     -12146
769570                 ZDOT =       -3702
335365


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   18052
97290880  
00016717  00000-0  10270-3 0  9152
2 25544  51
6392 233
0912 0003105 121
3785 238
7671 15
54117483 20593


Satellite: ISS
Catalog Number: 25544
Epoch time:      18052
97290880   =   yrday
fracday
Element set:     915
Inclination:       51
6392  deg
RA of node:       233
0912  deg
Eccentricity:     
0003105     
Arg of perigee:   121
3785  deg
Mean anomaly:     238
7671  deg
Mean motion:   15
54117483  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2059
Checksum:              309


Coasting Arc #17 (Orbit 2074)
---------------------------------------

Vector Time (GMT): 2018/053/22:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1403271
15                 A    =         6778749
48  meter
 Y    =       -4360003
75  meter          E    =           
0009057
 Z    =        4992231
10                 I    =           51
34235
 XDOT =       6084
844487                 Wp   =          123
54516
 YDOT =       4233
483810  meter/sec      RA   =          227
16200  deg
 ZDOT =       1979
435255                 TA   =          307
12143
                                          MA   =          307
20415
                                          Ha   =            222
002  n
mi
                                          Hp   =            213
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4603907
98                 X    =         1427672
17
 Y    =      -14304474
26  feet           Y    =        -4344174
67  meter
 Z    =       16378710
95                 Z    =         4999107
18
 XDOT =      19963
400549                 XDOT =        6027
437314
 YDOT =      13889
382580  feet/sec       YDOT =        4301
207859  meter/sec
 ZDOT =       6494
210154                 ZDOT =        2008
853381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13421651
11                 X    =        -4090919
26
 Y    =        6682190
53  feet           Y    =         2036731
67  meter
 Z    =       16409867
03                 Z    =         5001727
47
 XDOT =      -3323
712196                 XDOT =       -1013
067477
 YDOT =     -23004
963732  feet/sec       YDOT =       -7011
912946  meter/sec
 ZDOT =       6624
671586                 ZDOT =        2019
199899


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   18054
00175185  
00016717  00000-0  10270-3 0  9169
2 25544  51
6385 227
9618 0003103 122
7891 237
3561 15
54111613 20751


Satellite: ISS
Catalog Number: 25544
Epoch time:      18054
00175185   =   yrday
fracday
Element set:     916
Inclination:       51
6385  deg
RA of node:       227
9618  deg
Eccentricity:     
0003103     
Arg of perigee:   122
7891  deg
Mean anomaly:     237
3561  deg
Mean motion:   15
54111613  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2075
Checksum:              294


Coasting Arc #18 (Orbit 2089)
---------------------------------------

Vector Time (GMT): 2018/054/22:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2784587
61                 A    =         6777452
70  meter
 Y    =        3197123
13  meter          E    =           
0017367
 Z    =       -5302554
39                 I    =           51
36032
 XDOT =      -5714
689626                 Wp   =           95
54768
 YDOT =      -5093
834376  meter/sec      RA   =          222
14393  deg
 ZDOT =        -72
110760                 TA   =          173
77218
                                          MA   =          173
75056
                                          Ha   =            222
011  n
mi
                                          Hp   =            213
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9135786
11                 X    =        -2794375
00
 Y    =       10489249
10  feet           Y    =         3165928
99  meter
 Z    =      -17396832
00                 Z    =        -5316104
73
 XDOT =     -18748
981712                 XDOT =       -5656
953992
 YDOT =     -16712
055038  feet/sec       YDOT =       -5157
417143  meter/sec
 ZDOT =       -236
583859                 ZDOT =         -99
729987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13796469
49                 X    =         4205163
90
 Y    =       -1013689
77  feet           Y    =         -308972
64  meter
 Z    =      -17457564
57                 Z    =        -5321065
68
 XDOT =       1321
965667                 XDOT =         402
935135
 YDOT =      24069
745264  feet/sec       YDOT =        7336
458356  meter/sec
 ZDOT =       -358
949472                 ZDOT =        -109
407799


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   18054
96629005  
00016717  00000-0  10270-3 0  9170
2 25544  51
6379 223
1545 0003020 126
4635 233
6796 15
54098136 20906


Satellite: ISS
Catalog Number: 25544
Epoch time:      18054
96629005   =   yrday
fracday
Element set:     917
Inclination:       51
6379  deg
RA of node:       223
1545  deg
Eccentricity:     
0003020     
Arg of perigee:   126
4635  deg
Mean anomaly:     233
6796  deg
Mean motion:   15
54098136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2090
Checksum:              310
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