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

 
Date: May 21st 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13552 8396 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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


140/01:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 222 5

141/17:30:57 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 222 4

143/00:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 222 5

145/22:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 222 3

146/12:14:26 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 2

148/20:33:31 100 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 3

149/04:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 222 2

149/15:17:02 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 222 2

152/12:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 222 0

Coasting Arc #1 (Orbit 2740)
---------------------------------------

Vector Time (GMT): 2020/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -994508
36                 A    =         6792875
37  meter
 Y    =       -4540731
55  meter          E    =           
0006382
 Z    =        4950955
82                 I    =           51
90009
 XDOT =       6229
356487                 Wp   =           46
03139
 YDOT =      -3842
674954  meter/sec      RA   =          134
27654  deg
 ZDOT =      -2266
847270                 TA   =           66
08497
                                          MA   =           66
01813
                                          Ha   =            228
237  n
mi
                                          Hp   =            222
487

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3262822
72                 X    =         -967707
80
 Y    =      -14897413
22  feet           Y    =        -4551703
30  meter
 Z    =       16243293
39                 Z    =         4946189
66
 XDOT =      20437
521282                 XDOT =        6282
874598
 YDOT =     -12607
201294  feet/sec       YDOT =       -3772
714479  meter/sec
 ZDOT =      -7437
162959                 ZDOT =       -2236
457430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14210052
72                 X    =        -4331224
07
 Y    =       -5599983
31  feet           Y    =        -1706874
91  meter
 Z    =       16221532
03                 Z    =         4944322
96
 XDOT =        708
352408                 XDOT =         215
905814
 YDOT =     -22993
928195  feet/sec       YDOT =       -7008
549314  meter/sec
 ZDOT =      -7297
290435                 ZDOT =       -2224
214125


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   20139
54450298  
00016717  00000-0  10270-3 0  9009
2 25544  51
6381 135
1920 0001375 318
7442  41
3604 15
49372117 27414


Satellite: ISS
Catalog Number: 25544
Epoch time:      20139
54450298   =   yrday
fracday
Element set:     900
Inclination:       51
6381  deg
RA of node:       135
1920  deg
Eccentricity:     
0001375     
Arg of perigee:   318
7442  deg
Mean anomaly:      41
3604  deg
Mean motion:   15
49372117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2741
Checksum:              287


Coasting Arc #2 (Orbit 2749)
---------------------------------------

Vector Time (GMT): 2020/140/01:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5409847
89                 A    =         6797330
56  meter
 Y    =        1685043
42  meter          E    =           
0010723
 Z    =        3745910
21                 I    =           51
92910
 XDOT =       1037
715506                 Wp   =           92
70456
 YDOT =      -6256
326484  meter/sec      RA   =          131
51295  deg
 ZDOT =       4301
881644                 TA   =          311
76382
                                          MA   =          311
85542
                                          Ha   =            228
252  n
mi
                                          Hp   =            222
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17748844
80                 X    =        -5446484
19
 Y    =        5528357
69  feet           Y    =         1624341
56  meter
 Z    =       12289731
66                 Z    =         3719542
09
 XDOT =       3404
578431                 XDOT =        1086
702147
 YDOT =     -20526
005525  feet/sec       YDOT =       -6244
448393  meter/sec
 ZDOT =      14113
784922                 ZDOT =        4307
041089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2644761
12                 X    =         -806123
19
 Y    =      -18481249
44  feet           Y    =        -5633084
83  meter
 Z    =       12168417
83                 Z    =         3708933
75
 XDOT =      18397
940321                 XDOT =        5607
692210
 YDOT =       6699
951256  feet/sec       YDOT =        2042
145143  meter/sec
 ZDOT =      14137
731364                 ZDOT =        4309
180520


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   20140
12500027  
00016717  00000-0  10270-3 0  9012
2 25544  51
6391 132
3147 0001139 304
2631  55
8411 15
49392374 27506


Satellite: ISS
Catalog Number: 25544
Epoch time:      20140
12500027   =   yrday
fracday
Element set:     901
Inclination:       51
6391  deg
RA of node:       132
3147  deg
Eccentricity:     
0001139     
Arg of perigee:   304
2631  deg
Mean anomaly:      55
8411  deg
Mean motion:   15
49392374  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2750
Checksum:              262


Coasting Arc #3 (Orbit 2764)
---------------------------------------

Vector Time (GMT): 2020/141/01:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5236793
59                 A    =         6797045
92  meter
 Y    =       -1997867
48  meter          E    =           
0005560
 Z    =       -3851304
25                 I    =           51
95030
 XDOT =       -647
329129                 Wp   =           66
28182
 YDOT =       6373
105140  meter/sec      RA   =          126
58374  deg
 ZDOT =      -4188
864757                 TA   =          159
70310
                                          MA   =          159
68099
                                          Ha   =            228
221  n
mi
                                          Hp   =            222
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17181081
33                 X    =         5277452
84
 Y    =       -6554683
35  feet           Y    =        -1939078
28  meter
 Z    =      -12635512
63                 Z    =        -3825766
98
 XDOT =      -2123
783232                 XDOT =        -698
199559
 YDOT =      20909
137598  feet/sec       YDOT =        6365
582146  meter/sec
 ZDOT =     -13742
994610                 ZDOT =       -4192
132322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4058022
46                 X    =         1236885
25
 Y    =       18017821
74  feet           Y    =         5491832
07  meter
 Z    =      -12517993
54                 Z    =        -3815484
43
 XDOT =     -19100
114194                 XDOT =       -5821
714806
 YDOT =      -5250
858104  feet/sec       YDOT =       -1600
461550  meter/sec
 ZDOT =     -13758
261704                 ZDOT =       -4193
518167


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   20141
09249398  
00016717  00000-0  10270-3 0  9021
2 25544  51
6400 127
5260 0001167 314
7381  45
3668 15
49377394 27657


Satellite: ISS
Catalog Number: 25544
Epoch time:      20141
09249398   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:       127
5260  deg
Eccentricity:     
0001167     
Arg of perigee:   314
7381  deg
Mean anomaly:      45
3668  deg
Mean motion:   15
49377394  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2765
Checksum:              312


Coasting Arc #4 (Orbit 2774)
---------------------------------------

Vector Time (GMT): 2020/141/17:30:57
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -389185
72                 A    =         6797625
75  meter
 Y    =        5745781
69  meter          E    =           
0004598
 Z    =       -3614745
23                 I    =           51
96795
 XDOT =      -5744
580792                 Wp   =           82
18492
 YDOT =       2407
607164  meter/sec      RA   =          123
27859  deg
 ZDOT =       4450
933857                 TA   =          235
36564
                                          MA   =          235
40900
                                          Ha   =            228
257  n
mi
                                          Hp   =            222
410

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1276856
02                 X    =         -435849
18
 Y    =       18850989
81  feet           Y    =         5741168
96  meter
 Z    =      -11859400
36                 Z    =        -3616748
58
 XDOT =     -18847
049842                 XDOT =       -5792
696860
 YDOT =       7898
973634  feet/sec       YDOT =        2343
097729  meter/sec
 ZDOT =      14602
801369                 ZDOT =        4422
911829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12872941
49                 X    =         3923672
57
 Y    =      -13822212
50  feet           Y    =        -4213010
37  meter
 Z    =      -11868840
47                 Z    =        -3617622
57
 XDOT =      18653
412299                 XDOT =        5685
560069
 YDOT =       4959
318791  feet/sec       YDOT =        1511
600368  meter/sec
 ZDOT =      14473
827891                 ZDOT =        4411
622741


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   20141
73748856  
00016717  00000-0  10270-3 0  9036
2 25544  51
6425 124
3384 0001592 330
6486  29
4574 15
49389407 27759


Satellite: ISS
Catalog Number: 25544
Epoch time:      20141
73748856   =   yrday
fracday
Element set:     903
Inclination:       51
6425  deg
RA of node:       124
3384  deg
Eccentricity:     
0001592     
Arg of perigee:   330
6486  deg
Mean anomaly:      29
4574  deg
Mean motion:   15
49389407  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2775
Checksum:              329


Coasting Arc #5 (Orbit 2790)
---------------------------------------

Vector Time (GMT): 2020/142/17:30:57
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          29140
47                 A    =         6798015
73  meter
 Y    =       -5820647
59  meter          E    =           
0011736
 Z    =        3503429
08                 I    =           51
98583
 XDOT =       5521
315890                 Wp   =           81
52836
 YDOT =      -2725
858895  meter/sec      RA   =          118
35276  deg
 ZDOT =      -4559
994304                 TA   =           57
58681
                                          MA   =           57
47333
                                          Ha   =            228
363  n
mi
                                          Hp   =            222
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          95605
21                 X    =           77208
57
 Y    =      -19096612
82  feet           Y    =        -5820053
34  meter
 Z    =       11494189
89                 Z    =         3503686
73
 XDOT =      18114
553444                 XDOT =        5573
537119
 YDOT =      -8943
106612  feet/sec       YDOT =       -2663
823115  meter/sec
 ZDOT =     -14960
611234                 ZDOT =       -4533
046914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11861227
89                 X    =        -3615302
26
 Y    =       14965565
19  feet           Y    =         4561504
27  meter
 Z    =       11495620
66                 Z    =         3503865
18
 XDOT =     -18743
851739                 XDOT =       -5713
126010
 YDOT =      -3422
187893  feet/sec       YDOT =       -1043
082870  meter/sec
 ZDOT =     -14836
548826                 ZDOT =       -4522
180082


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   20142
76948014  
00016717  00000-0  10270-3 0  9049
2 25544  51
6418 119
2314 0001568 337
8329  22
2753 15
49372146 27915


Satellite: ISS
Catalog Number: 25544
Epoch time:      20142
76948014   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:       119
2314  deg
Eccentricity:     
0001568     
Arg of perigee:   337
8329  deg
Mean anomaly:      22
2753  deg
Mean motion:   15
49372146  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2791
Checksum:              308


Coasting Arc #6 (Orbit 2794)
---------------------------------------

Vector Time (GMT): 2020/143/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4672155
16                 A    =         6793240
09  meter
 Y    =        -752057
04  meter          E    =           
0011494
 Z    =       -4884631
00                 I    =           51
97169
 XDOT =      -1445
645468                 Wp   =           66
79521
 YDOT =       7093
999559  meter/sec      RA   =          117
02696  deg
 ZDOT =      -2475
204670                 TA   =          178
95773
                                          MA   =          178
95534
                                          Ha   =            228
313  n
mi
                                          Hp   =            222
462

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15328593
05                 X    =         4703944
79
 Y    =       -2467378
73  feet           Y    =         -699631
35  meter
 Z    =      -16025692
27                 Z    =        -4861857
99
 XDOT =      -4742
931325                 XDOT =       -1512
841898
 YDOT =      23274
276769  feet/sec       YDOT =        7077
457893  meter/sec
 ZDOT =      -8120
750229                 ZDOT =       -2482
389550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5148303
10                 X    =        -1569202
78
 Y    =       14761304
86  feet           Y    =         4499245
72  meter
 Z    =      -15920910
44                 Z    =        -4852693
50
 XDOT =     -17190
341252                 XDOT =       -5239
616014
 YDOT =     -14789
350921  feet/sec       YDOT =       -4507
794161  meter/sec
 ZDOT =      -8154
103725                 ZDOT =       -2485
370815


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   20143
02747744  
00016717  00000-0  10270-3 0  9057
2 25544  51
6392 117
9498 0001155 332
9464  27
1626 15
49388500 27950


Satellite: ISS
Catalog Number: 25544
Epoch time:      20143
02747744   =   yrday
fracday
Element set:     905
Inclination:       51
6392  deg
RA of node:       117
9498  deg
Eccentricity:     
0001155     
Arg of perigee:   332
9464  deg
Mean anomaly:      27
1626  deg
Mean motion:   15
49388500  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2795
Checksum:              321


Coasting Arc #7 (Orbit 2810)
---------------------------------------

Vector Time (GMT): 2020/144/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4563290
23                 A    =         6792981
15  meter
 Y    =         997952
94  meter          E    =           
0005681
 Z    =        4928548
01                 I    =           51
98573
 XDOT =        957
208780                 Wp   =          115
99970
 YDOT =      -7231
989414  meter/sec      RA   =          112
09967  deg
 ZDOT =       2346
115526                 TA   =          311
10849
                                          MA   =          311
15752
                                          Ha   =            228
389  n
mi
                                          Hp   =            222
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14971424
63                 X    =        -4598050
93
 Y    =        3274123
82  feet           Y    =          946727
95  meter
 Z    =       16169776
92                 Z    =         4906296
67
 XDOT =       3140
448753                 XDOT =        1026
611619
 YDOT =     -23726
999390  feet/sec       YDOT =       -7220
897490  meter/sec
 ZDOT =       7697
229417                 ZDOT =        2350
932927

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4013394
31                 X    =         1223282
59
 Y    =      -14901589
55  feet           Y    =        -4542004
50  meter
 Z    =       16067371
37                 Z    =         4897334
79
 XDOT =      18574
765599                 XDOT =        5661
588555
 YDOT =      13342
412219  feet/sec       YDOT =        4066
767244  meter/sec
 ZDOT =       7719
722543                 ZDOT =        2352
971431


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   20144
05946705  
00016717  00000-0  10270-3 0  9060
2 25544  51
6397 112
8409 0001237 325
9375  34
1696 15
49401715 28113


Satellite: ISS
Catalog Number: 25544
Epoch time:      20144
05946705   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:       112
8409  deg
Eccentricity:     
0001237     
Arg of perigee:   325
9375  deg
Mean anomaly:      34
1696  deg
Mean motion:   15
49401715  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2811
Checksum:              307


Coasting Arc #8 (Orbit 2825)
---------------------------------------

Vector Time (GMT): 2020/145/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4457781
63                 A    =         6792800
79  meter
 Y    =       -1222740
89  meter          E    =           
0012227
 Z    =       -4988800
32                 I    =           51
99811
 XDOT =       -459
004442                 Wp   =           68
19240
 YDOT =       7312
686671  meter/sec      RA   =          107
17476  deg
 ZDOT =      -2202
381071                 TA   =          180
38066
                                          MA   =          180
38159
                                          Ha   =            228
336  n
mi
                                          Hp   =            222
441

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14625267
83                 X    =         4495356
44
 Y    =       -4011617
09  feet           Y    =        -1172679
94  meter
 Z    =      -16367455
11                 Z    =        -4967054
78
 XDOT =      -1505
920084                 XDOT =        -530
044906
 YDOT =      23991
754171  feet/sec       YDOT =        7307
156884  meter/sec
 ZDOT =      -7225
659681                 ZDOT =       -2204
782185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2942550
95                 X    =         -896889
53
 Y    =       14986652
54  feet           Y    =         4567931
69  meter
 Z    =      -16267352
49                 Z    =        -4958289
04
 XDOT =     -19761
284152                 XDOT =       -6023
239410
 YDOT =     -11735
843122  feet/sec       YDOT =       -3577
084984  meter/sec
 ZDOT =      -7237
063476                 ZDOT =       -2205
856948


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   20145
02695725  
00016717  00000-0  10270-3 0  9072
2 25544  51
6412 108
0531 0001249 337
3712  22
7382 15
49390188 28261


Satellite: ISS
Catalog Number: 25544
Epoch time:      20145
02695725   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       108
0531  deg
Eccentricity:     
0001249     
Arg of perigee:   337
3712  deg
Mean anomaly:      22
7382  deg
Mean motion:   15
49390188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2826
Checksum:              297


Coasting Arc #9 (Orbit 2839)
---------------------------------------

Vector Time (GMT): 2020/145/22:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3512496
34                 A    =         6792100
72  meter
 Y    =        2718840
52  meter          E    =           
0012953
 Z    =       -5149857
89                 I    =           52
00259
 XDOT =      -2884
798843                 Wp   =           97
12928
 YDOT =       6886
541519  meter/sec      RA   =          102
66490  deg
 ZDOT =       1670
153029                 TA   =          188
94109
                                          MA   =          188
96418
                                          Ha   =            228
450  n
mi
                                          Hp   =            222
332

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11523938
11                 X    =         3506847
72
 Y    =        8920080
45  feet           Y    =         2758089
02  meter
 Z    =      -16895859
21                 Z    =        -5132808
64
 XDOT =      -9464
563133                 XDOT =       -2969
704521
 YDOT =      22593
640154  feet/sec       YDOT =        6853
806632  meter/sec
 ZDOT =       5479
504687                 ZDOT =        1655
934574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14597916
07                 X    =        -4449444
82
 Y    =       -1381935
61  feet           Y    =         -421213
97  meter
 Z    =      -16817554
63                 Z    =        -5125990
65
 XDOT =      -4039
765446                 XDOT =       -1231
320508
 YDOT =     -23127
471793  feet/sec       YDOT =       -7049
253403  meter/sec
 ZDOT =       5413
731506                 ZDOT =        1650
105363


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   20145
92994631  
00016717  00000-0  10270-3 0  9080
2 25544  51
6399 103
5841 0001334 349
2665  10
8457 15
49386331 28405


Satellite: ISS
Catalog Number: 25544
Epoch time:      20145
92994631   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:       103
5841  deg
Eccentricity:     
0001334     
Arg of perigee:   349
2665  deg
Mean anomaly:      10
8457  deg
Mean motion:   15
49386331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2840
Checksum:              319


Coasting Arc #10 (Orbit 2848)
---------------------------------------

Vector Time (GMT): 2020/146/12:14:26
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -991795
00                 A    =         6803130
38  meter
 Y    =        6720520
84  meter          E    =           
0012732
 Z    =        -207256
36                 I    =           52
04404
 XDOT =      -4690
182340                 Wp   =           37
57957
 YDOT =       -512
295026  meter/sec      RA   =           99
75863  deg
 ZDOT =       6036
997331                 TA   =          320
20395
                                          MA   =          320
29727
                                          Ha   =            228
474  n
mi
                                          Hp   =            222
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3253920
61                 X    =        -1065865
41
 Y    =       22048952
89  feet           Y    =         6709015
76  meter
 Z    =        -679974
93                 Z    =         -212252
91
 XDOT =     -15387
737337                 XDOT =       -4713
429627
 YDOT =      -1680
757960  feet/sec       YDOT =        -564
874990  meter/sec
 ZDOT =      19806
421688                 ZDOT =        6014
157525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18872943
59                 X    =         5752473
21
 Y    =       11854283
15  feet           Y    =         3613185
50  meter
 Z    =        -703320
66                 Z    =         -214372
14
 XDOT =      -6924
561635                 XDOT =       -2110
606386
 YDOT =      12154
837399  feet/sec       YDOT =        3704
794439  meter/sec
 ZDOT =      19701
355795                 ZDOT =        6004
973246


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   20146
51043899  
00016717  00000-0  10270-3 0  9098
2 25544  51
6405 100
7148 0001726 349
7358  10
3756 15
49385963 28497


Satellite: ISS
Catalog Number: 25544
Epoch time:      20146
51043899   =   yrday
fracday
Element set:     909
Inclination:       51
6405  deg
RA of node:       100
7148  deg
Eccentricity:     
0001726     
Arg of perigee:   349
7358  deg
Mean anomaly:      10
3756  deg
Mean motion:   15
49385963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2849
Checksum:              329


Coasting Arc #11 (Orbit 2864)
---------------------------------------

Vector Time (GMT): 2020/147/12:14:26
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         529354
37                 A    =         6803176
68  meter
 Y    =       -6777678
65  meter          E    =           
0010838
 Z    =          56488
76                 I    =           52
04955
 XDOT =       4700
792380                 Wp   =          128
17414
 YDOT =        310
319970  meter/sec      RA   =           94
83718  deg
 ZDOT =      -6039
561387                 TA   =           51
22212
                                          MA   =           51
12534
                                          Ha   =            228
503  n
mi
                                          Hp   =            222
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1736726
92                 X    =          604830
65
 Y    =      -22236478
52  feet           Y    =        -6771337
03  meter
 Z    =         185330
58                 Z    =           59242
33
 XDOT =      15422
547177                 XDOT =        4726
309745
 YDOT =       1018
110139  feet/sec       YDOT =         363
031277  meter/sec
 ZDOT =     -19814
833946                 ZDOT =       -6016
664666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19832763
15                 X    =        -6045026
21
 Y    =      -10204592
01  feet           Y    =        -3110359
64  meter
 Z    =         198375
36                 Z    =           60464
81
 XDOT =       6213
420573                 XDOT =        1893
850591
 YDOT =     -12505
394535  feet/sec       YDOT =       -3811
644254  meter/sec
 ZDOT =     -19709
486711                 ZDOT =       -6007
451549


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   20147
54242661  
00016717  00000-0  10270-3 0  9102
2 25544  51
6414  95
6074 0001768 351
4397   8
6723 15
49375882 28657


Satellite: ISS
Catalog Number: 25544
Epoch time:      20147
54242661   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:        95
6074  deg
Eccentricity:     
0001768     
Arg of perigee:   351
4397  deg
Mean anomaly:       8
6723  deg
Mean motion:   15
49375882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2865
Checksum:              323


Coasting Arc #12 (Orbit 2880)
---------------------------------------

Vector Time (GMT): 2020/148/12:14:26
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -36196
76                 A    =         6803141
50  meter
 Y    =        6795777
05  meter          E    =           
0013333
 Z    =          59228
85                 I    =           52
05140
 XDOT =      -4711
787836                 Wp   =           40
07610
 YDOT =        -84
238618  meter/sec      RA   =           89
91575  deg
 ZDOT =       6041
812687                 TA   =          320
55714
                                          MA   =          320
65413
                                          Ha   =            228
519  n
mi
                                          Hp   =            222
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -118755
77                 X    =         -112474
16
 Y    =       22295856
47  feet           Y    =         6794945
77  meter
 Z    =         194320
37                 Z    =           58868
85
 XDOT =     -15458
621508                 XDOT =       -4739
843313
 YDOT =       -276
373420  feet/sec       YDOT =        -137
087020  meter/sec
 ZDOT =      19822
220102                 ZDOT =        6018
856520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20659863
21                 X    =         6297126
31
 Y    =        8383922
80  feet           Y    =         2555419
67  meter
 Z    =         192275
51                 Z    =           58605
58
 XDOT =      -5429
785432                 XDOT =       -1654
998600
 YDOT =      12871
455402  feet/sec       YDOT =        3923
219606  meter/sec
 ZDOT =      19716
579009                 ZDOT =        6009
613282


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   20148
57441215  
00016717  00000-0  10270-3 0  9113
2 25544  51
6416  90
5001 0001774 353
5954   6
5173 15
49389278 28810


Satellite: ISS
Catalog Number: 25544
Epoch time:      20148
57441215   =   yrday
fracday
Element set:     911
Inclination:       51
6416  deg
RA of node:        90
5001  deg
Eccentricity:     
0001774     
Arg of perigee:   353
5954  deg
Mean anomaly:       6
5173  deg
Mean motion:   15
49389278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2881
Checksum:              307


Coasting Arc #13 (Orbit 2885)
---------------------------------------

Vector Time (GMT): 2020/148/20:33:31
100
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3092701
33                 A    =         6797247
29  meter
 Y    =       -4731071
64  meter          E    =           
0011592
 Z    =        3768210
69                 I    =           52
02986
 XDOT =       3173
351539                 Wp   =           76
32810
 YDOT =      -5500
535983  meter/sec      RA   =           88
18004  deg
 ZDOT =      -4287
854780                 TA   =           58
95176
                                          MA   =           58
83801
                                          Ha   =            228
524  n
mi
                                          Hp   =            222
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10146657
89                 X    =        -3057871
00
 Y    =      -15521888
57  feet           Y    =        -4765462
26  meter
 Z    =       12362895
96                 Z    =         3753271
44
 XDOT =      10411
258329                 XDOT =        3255
452224
 YDOT =     -18046
377896  feet/sec       YDOT =       -5464
589588  meter/sec
 ZDOT =     -14067
765025                 ZDOT =       -4272
241349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13534318
09                 X    =         4125260
15
 Y    =       12743408
12  feet           Y    =         3884190
79  meter
 Z    =       12294416
27                 Z    =         3747338
08
 XDOT =      -5132
174283                 XDOT =       -1564
286721
 YDOT =      18996
816471  feet/sec       YDOT =        5790
229660  meter/sec
 ZDOT =     -13995
591765                 ZDOT =       -4265
856370


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   20148
89690627  
00016717  00000-0  10270-3 0  9122
2 25544  51
6399  88
9003 0001547 349
7014  10
4104 15
49379997 28865


Satellite: ISS
Catalog Number: 25544
Epoch time:      20148
89690627   =   yrday
fracday
Element set:     912
Inclination:       51
6399  deg
RA of node:        88
9003  deg
Eccentricity:     
0001547     
Arg of perigee:   349
7014  deg
Mean anomaly:      10
4104  deg
Mean motion:   15
49379997  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2886
Checksum:              341


Coasting Arc #14 (Orbit 2890)
---------------------------------------

Vector Time (GMT): 2020/149/04:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3421591
65                 A    =         6794158
93  meter
 Y    =       -3593350
74  meter          E    =           
0010854
 Z    =       -4652025
02                 I    =           52
02221
 XDOT =       2735
830496                 Wp   =           62
11116
 YDOT =       6485
950150  meter/sec      RA   =           86
54954  deg
 ZDOT =      -2998
111916                 TA   =          178
08181
                                          MA   =          178
07765
                                          Ha   =            228
555  n
mi
                                          Hp   =            222
248

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11225694
39                 X    =         3484116
08
 Y    =      -11789208
46  feet           Y    =        -3554737
78  meter
 Z    =      -15262549
26                 Z    =        -4635252
98
 XDOT =       8975
821836                 XDOT =        2677
662419
 YDOT =      21279
364009  feet/sec       YDOT =        6516
219362  meter/sec
 ZDOT =      -9836
325183                 ZDOT =       -2984
962663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16333179
72                 X    =         4978353
18
 Y    =        -765182
12  feet           Y    =         -233227
51  meter
 Z    =      -15185150
55                 Z    =        -4628433
89
 XDOT =      -8128
603851                 XDOT =       -2477
598454
 YDOT =      20474
282974  feet/sec       YDOT =        6240
561450  meter/sec
 ZDOT =      -9776
187245                 ZDOT =       -2979
781872


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   20149
21940193  
00016717  00000-0  10270-3 0  9136
2 25544  51
6430  87
3069 0001588 358
9628   1
1518 15
49379898 28916


Satellite: ISS
Catalog Number: 25544
Epoch time:      20149
21940193   =   yrday
fracday
Element set:     913
Inclination:       51
6430  deg
RA of node:        87
3069  deg
Eccentricity:     
0001588     
Arg of perigee:   358
9628  deg
Mean anomaly:       1
1518  deg
Mean motion:   15
49379898  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2891
Checksum:              336


Coasting Arc #15 (Orbit 2897)
---------------------------------------

Vector Time (GMT): 2020/149/15:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1377828
11                 A    =         6802872
85  meter
 Y    =       -6591516
56  meter          E    =           
0012486
 Z    =         927676
08                 I    =           52
05121
 XDOT =       4485
582340                 Wp   =          118
53064
 YDOT =      -1782
536798  meter/sec      RA   =           84
36074  deg
 ZDOT =      -5948
643438                 TA   =           51
50334
                                          MA   =           51
39143
                                          Ha   =            228
614  n
mi
                                          Hp   =            222
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4520433
43                 X    =        -1308523
52
 Y    =      -21625710
50  feet           Y    =        -6606537
04  meter
 Z    =        3043556
70                 Z    =          921150
55
 XDOT =      14716
477493                 XDOT =        4534
076834
 YDOT =      -5848
217841  feet/sec       YDOT =       -1732
103838  meter/sec
 ZDOT =     -19516
546714                 ZDOT =       -5926
736765

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17684554
09                 X    =        -5390252
09
 Y    =       13249218
23  feet           Y    =         4038361
72  meter
 Z    =        3013913
27                 Z    =          918640
76
 XDOT =     -10606
996518                 XDOT =       -3233
012539
 YDOT =      -9699
871829  feet/sec       YDOT =       -2956
520934  meter/sec
 ZDOT =     -19415
619201                 ZDOT =       -5917
880733


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   20149
67089564  
00016717  00000-0  10270-3 0  9143
2 25544  51
6442  85
0747 0001744 359
2656    
8491 15
49359435 28984


Satellite: ISS
Catalog Number: 25544
Epoch time:      20149
67089564   =   yrday
fracday
Element set:     914
Inclination:       51
6442  deg
RA of node:        85
0747  deg
Eccentricity:     
0001744     
Arg of perigee:   359
2656  deg
Mean anomaly:        
8491  deg
Mean motion:   15
49359435  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2898
Checksum:              341


Coasting Arc #16 (Orbit 2912)
---------------------------------------

Vector Time (GMT): 2020/150/15:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1854469
06                 A    =         6802819
94  meter
 Y    =        6488331
43  meter          E    =           
0011780
 Z    =        -812555
18                 I    =           52
04654
 XDOT =      -4367
241755                 Wp   =           33
62003
 YDOT =       1989
747970  meter/sec      RA   =           79
43829  deg
 ZDOT =       5971
912882                 TA   =          317
65959
                                          MA   =          317
75045
                                          Ha   =            228
585  n
mi
                                          Hp   =            222
095

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6084216
07                 X    =         1785723
70
 Y    =       21287176
60  feet           Y    =         6508685
14  meter
 Z    =       -2665863
47                 Z    =         -803713
12
 XDOT =     -14328
220982                 XDOT =       -4418
175180
 YDOT =       6528
044521  feet/sec       YDOT =        1940
624864  meter/sec
 ZDOT =      19592
890033                 ZDOT =        5950
575117

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16466126
64                 X    =         5018875
40
 Y    =      -14806805
84  feet           Y    =        -4513114
42  meter
 Z    =       -2625561
85                 Z    =         -800271
25
 XDOT =      11122
165992                 XDOT =        3390
036194
 YDOT =       8941
775905  feet/sec       YDOT =        2725
453296  meter/sec
 ZDOT =      19494
562527                 ZDOT =        5941
942658


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   20150
63837857  
00016717  00000-0  10270-3 0  9158
2 25544  51
6437  80
2860 0001909 359
5261    
5887 15
49405956 29133


Satellite: ISS
Catalog Number: 25544
Epoch time:      20150
63837857   =   yrday
fracday
Element set:     915
Inclination:       51
6437  deg
RA of node:        80
2860  deg
Eccentricity:     
0001909     
Arg of perigee:   359
5261  deg
Mean anomaly:        
5887  deg
Mean motion:   15
49405956  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2913
Checksum:              325


Coasting Arc #17 (Orbit 2928)
---------------------------------------

Vector Time (GMT): 2020/151/15:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2297035
61                 A    =         6803060
25  meter
 Y    =       -6363972
86  meter          E    =           
0012228
 Z    =         659775
11                 I    =           52
03944
 XDOT =       4252
205639                 Wp   =          120
96612
 YDOT =      -2163
993609  meter/sec      RA   =           74
51653  deg
 ZDOT =      -5992
972538                 TA   =           51
96290
                                          MA   =           51
85260
                                          Ha   =            228
680  n
mi
                                          Hp   =            222
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7536206
07                 X    =        -2228905
86
 Y    =      -20879176
07  feet           Y    =        -6389279
08  meter
 Z    =        2164616
49                 Z    =          648781
83
 XDOT =      13950
805902                 XDOT =        4305
198448
 YDOT =      -7099
716564  feet/sec       YDOT =       -2116
145507  meter/sec
 ZDOT =     -19661
983394                 ZDOT =       -5972
188502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15188774
65                 X    =        -4629538
51
 Y    =       16194144
76  feet           Y    =         4935975
32  meter
 Z    =        2114417
08                 Z    =          644474
33
 XDOT =     -11532
390899                 XDOT =       -3515
072746
 YDOT =      -8228
429001  feet/sec       YDOT =       -2508
025159  meter/sec
 ZDOT =     -19566
189638                 ZDOT =       -5963
774602


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   20151
67036241  
00016717  00000-0  10270-3 0  9162
2 25544  51
6436  75
1787 0001774   4
8848 355
2319 15
49356882 29294


Satellite: ISS
Catalog Number: 25544
Epoch time:      20151
67036241   =   yrday
fracday
Element set:     916
Inclination:       51
6436  deg
RA of node:        75
1787  deg
Eccentricity:     
0001774     
Arg of perigee:     4
8848  deg
Mean anomaly:     355
2319  deg
Mean motion:   15
49356882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2929
Checksum:              330


Coasting Arc #18 (Orbit 2942)
---------------------------------------

Vector Time (GMT): 2020/152/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2709960
65                 A    =         6792946
98  meter
 Y    =        3816312
92  meter          E    =           
0006222
 Z    =        4918429
80                 I    =           51
99711
 XDOT =      -4133
928537                 Wp   =          105
16029
 YDOT =      -6000
763171  meter/sec      RA   =           70
18674  deg
 ZDOT =       2374
321680                 TA   =          321
66615
                                          MA   =          321
71036
                                          Ha   =            228
738  n
mi
                                          Hp   =            222
001

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8890947
02                 X    =        -2776325
38
 Y    =       12520711
69  feet           Y    =         3785636
69  meter
 Z    =       16136580
71                 Z    =         4905105
00
 XDOT =     -13562
757668                 XDOT =       -4078
052112
 YDOT =     -19687
543211  feet/sec       YDOT =       -6046
679500  meter/sec
 ZDOT =       7789
769290                 ZDOT =        2354
375759

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9985684
35                 X    =         3043636
59
 Y    =       11751024
61  feet           Y    =         3581712
30  meter
 Z    =       16075009
35                 Z    =         4899662
85
 XDOT =     -21529
614158                 XDOT =       -6562
226395
 YDOT =       7745
772947  feet/sec       YDOT =        2360
911594  meter/sec
 ZDOT =       7698
353905                 ZDOT =        2346
458270


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   20152
57334520  
00016717  00000-0  10270-3 0  9174
2 25544  51
6432  70
7083 0001861   6
7131 353
4044 15
49408990 29432


Satellite: ISS
Catalog Number: 25544
Epoch time:      20152
57334520   =   yrday
fracday
Element set:     917
Inclination:       51
6432  deg
RA of node:        70
7083  deg
Eccentricity:     
0001861     
Arg of perigee:     6
7131  deg
Mean anomaly:     353
4044  deg
Mean motion:   15
49408990  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2943
Checksum:              290


Coasting Arc #19 (Orbit 2957)
---------------------------------------

Vector Time (GMT): 2020/153/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2484856
74                 A    =         6792705
39  meter
 Y    =       -3909936
17  meter          E    =           
0013429
 Z    =       -4980224
13                 I    =           51
98512
 XDOT =       4554
918496                 Wp   =           65
98604
 YDOT =       5729
402385  meter/sec      RA   =           65
26089  deg
 ZDOT =      -2224
882065                 TA   =          182
34785
                                          MA   =          182
35416
                                          Ha   =            228
706  n
mi
                                          Hp   =            221
986

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8152417
13                 X    =         2552585
40
 Y    =      -12827874
57  feet           Y    =        -3881769
56  meter
 Z    =      -16339318
00                 Z    =        -4967989
44
 XDOT =      14943
958319                 XDOT =        4501
319372
 YDOT =      18797
251919  feet/sec       YDOT =        5780
039248  meter/sec
 ZDOT =      -7299
481839                 ZDOT =       -2202
885514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10650878
90                 X    =        -3246387
89
 Y    =      -10927964
12  feet           Y    =        -3330843
46  meter
 Z    =      -16282750
47                 Z    =        -4962982
34
 XDOT =      20881
675234                 XDOT =        6364
734611
 YDOT =      -9623
375458  feet/sec       YDOT =       -2933
204839  meter/sec
 ZDOT =      -7198
626523                 ZDOT =       -2194
141364


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   20153
54082593  
00016717  00000-0  10270-3 0  9183
2 25544  51
6445  65
9199 0002054  12
2599 347
8601 15
49417110 29581


Satellite: ISS
Catalog Number: 25544
Epoch time:      20153
54082593   =   yrday
fracday
Element set:     918
Inclination:       51
6445  deg
RA of node:        65
9199  deg
Eccentricity:     
0002054     
Arg of perigee:    12
2599  deg
Mean anomaly:     347
8601  deg
Mean motion:   15
49417110  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2958
Checksum:              318
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