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

 
Date: December 3rd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 25144 4947 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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


337/11:31:53 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 0

337/17:35:42 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 1

337/19:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 0

338/16:07:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 212 9

338/18:38:53 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 0

340/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 1

344/23:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 4

348/03:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 213 6

Coasting Arc #1 (Orbit 2436)
---------------------------------------

Vector Time (GMT): 2018/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3576063
07                 A    =         6781445
58  meter
 Y    =       -3766391
06  meter          E    =           
0013991
 Z    =       -4374471
65                 I    =           51
24933
 XDOT =       2594
072941                 Wp   =          105
57330
 YDOT =      -6368
088591  meter/sec      RA   =          269
01771  deg
 ZDOT =       3367
614620                 TA   =          198
73241
                                          MA   =          198
78395
                                          Ha   =            223
015  n
mi
                                          Hp   =            212
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11732490
40                 X    =        -3512431
45
 Y    =      -12356926
07  feet           Y    =        -3806025
13  meter
 Z    =      -14351941
10                 Z    =        -4391688
62
 XDOT =       8510
737994                 XDOT =        2648
731699
 YDOT =     -20892
679105  feet/sec       YDOT =       -6338
774382  meter/sec
 ZDOT =      11048
604397                 ZDOT =        3380
348308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15770650
70                 X    =         4806894
33
 Y    =       -6278293
06  feet           Y    =        -1913623
72  meter
 Z    =      -14428886
96                 Z    =        -4397924
75
 XDOT =      15869
117947                 XDOT =        4836
907150
 YDOT =      14376
810567  feet/sec       YDOT =        4382
051861  meter/sec
 ZDOT =      11106
627060                 ZDOT =        3385
299928


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   18334
50996722  
00016717  00000-0  10270-3 0  9006
2 25544  51
6386 269
8765 0005123  96
8692 263
3044 15
54026770 24370


Satellite: ISS
Catalog Number: 25544
Epoch time:      18334
50996722   =   yrday
fracday
Element set:     900
Inclination:       51
6386  deg
RA of node:       269
8765  deg
Eccentricity:     
0005123     
Arg of perigee:    96
8692  deg
Mean anomaly:     263
3044  deg
Mean motion:   15
54026770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2437
Checksum:              330


Coasting Arc #2 (Orbit 2452)
---------------------------------------

Vector Time (GMT): 2018/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3112993
51                 A    =         6785170
36  meter
 Y    =        5101619
05  meter          E    =           
0017862
 Z    =        3195366
60                 I    =           51
26458
 XDOT =      -3315
267547                 Wp   =           95
17813
 YDOT =       5020
205435  meter/sec      RA   =          264
00574  deg
 ZDOT =      -4763
842027                 TA   =           47
63215
                                          MA   =           47
48107
                                          Ha   =            222
909  n
mi
                                          Hp   =            212
924

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10213233
29                 X    =         3040192
86
 Y    =       16737595
30  feet           Y    =         5136023
55  meter
 Z    =       10483486
20                 Z    =         3210311
92
 XDOT =     -10876
862031                 XDOT =       -3348
018044
 YDOT =      16470
490271  feet/sec       YDOT =        4982
948837  meter/sec
 ZDOT =     -15629
402977                 ZDOT =       -4780
025987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19235942
38                 X    =        -5863115
24
 Y    =        3610434
55  feet           Y    =         1100460
45  meter
 Z    =       10550070
92                 Z    =         3215661
62
 XDOT =     -11367
002796                 XDOT =       -3464
662452
 YDOT =     -14472
469498  feet/sec       YDOT =       -4411
208703  meter/sec
 ZDOT =     -15702
763281                 ZDOT =       -4786
202248


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   18335
53885788  
00016717  00000-0  10270-3 0  9010
2 25544  51
6395 264
7478 0005093  99
7988 260
3740 15
54050427 24535


Satellite: ISS
Catalog Number: 25544
Epoch time:      18335
53885788   =   yrday
fracday
Element set:     901
Inclination:       51
6395  deg
RA of node:       264
7478  deg
Eccentricity:     
0005093     
Arg of perigee:    99
7988  deg
Mean anomaly:     260
3740  deg
Mean motion:   15
54050427  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2453
Checksum:              349


Coasting Arc #3 (Orbit 2467)
---------------------------------------

Vector Time (GMT): 2018/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2588606
58                 A    =         6788270
53  meter
 Y    =       -6029727
94  meter          E    =           
0010773
 Z    =       -1734895
61                 I    =           51
27901
 XDOT =       3970
432551                 Wp   =           63
84862
 YDOT =      -3321
367845  meter/sec      RA   =          259
00390  deg
 ZDOT =       5651
444244                 TA   =          277
02723
                                          MA   =          277
14974
                                          Ha   =            222
971  n
mi
                                          Hp   =            212
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8492803
73                 X    =        -2512560
76
 Y    =      -19782571
99  feet           Y    =        -6058250
28  meter
 Z    =       -5691914
72                 Z    =        -1747285
82
 XDOT =      13026
353514                 XDOT =        3979
825833
 YDOT =     -10896
876132  feet/sec       YDOT =       -3276
915374  meter/sec
 ZDOT =      18541
483741                 ZDOT =        5670
754184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21472839
52                 X    =         6544921
49
 Y    =       -1328867
30  feet           Y    =         -405038
75  meter
 Z    =       -5746915
47                 Z    =        -1751659
84
 XDOT =       5839
339242                 XDOT =        1779
830601
 YDOT =      14243
897323  feet/sec       YDOT =        4341
539904  meter/sec
 ZDOT =      18628
691690                 ZDOT =        5678
025227


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   18336
50343821  
00016717  00000-0  10270-3 0  9026
2 25544  51
6391 259
9401 0005134 102
7741 257
3986 15
54042974 24683


Satellite: ISS
Catalog Number: 25544
Epoch time:      18336
50343821   =   yrday
fracday
Element set:     902
Inclination:       51
6391  deg
RA of node:       259
9401  deg
Eccentricity:     
0005134     
Arg of perigee:   102
7741  deg
Mean anomaly:     257
3986  deg
Mean motion:   15
54042974  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2468
Checksum:              313


Coasting Arc #4 (Orbit 2483)
---------------------------------------

Vector Time (GMT): 2018/337/11:31:53
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3196607
21                 A    =         6778878
19  meter
 Y    =       -3320647
39  meter          E    =           
0010994
 Z    =        4963742
11                 I    =           51
25548
 XDOT =       3551
284847                 Wp   =          116
57472
 YDOT =       6488
102139  meter/sec      RA   =          254
12439  deg
 ZDOT =       2045
059035                 TA   =          313
40008
                                          MA   =          313
49156
                                          Ha   =            222
746  n
mi
                                          Hp   =            212
957

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10487556
48                 X    =         3209390
42
 Y    =      -10894512
45  feet           Y    =        -3284829
45  meter
 Z    =       16285243
15                 Z    =         4979301
27
 XDOT =      11651
197005                 XDOT =        3468
535159
 YDOT =      21286
424342  feet/sec       YDOT =        6527
352303  meter/sec
 ZDOT =       6709
511269                 ZDOT =        2062
109516

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5324180
11                 X    =         1622810
10
 Y    =       14072538
30  feet           Y    =         4289309
67  meter
 Z    =       16355584
94                 Z    =         4985182
29
 XDOT =     -23187
302168                 XDOT =       -7067
489701
 YDOT =        854
654954  feet/sec       YDOT =         260
498830  meter/sec
 ZDOT =       6785
425459                 ZDOT =        2068
197680


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   18337
53231864  
00016717  00000-0  10270-3 0  9034
2 25544  51
6394 254
8120 0005014 108
3861 251
7837 15
54089770 24846


Satellite: ISS
Catalog Number: 25544
Epoch time:      18337
53231864   =   yrday
fracday
Element set:     903
Inclination:       51
6394  deg
RA of node:       254
8120  deg
Eccentricity:     
0005014     
Arg of perigee:   108
3861  deg
Mean anomaly:     251
7837  deg
Mean motion:   15
54089770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2484
Checksum:              314


Coasting Arc #5 (Orbit 2487)
---------------------------------------

Vector Time (GMT): 2018/337/17:35:42
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1405040
65                 A    =         6783677
92  meter
 Y    =       -5504136
37  meter          E    =           
0016466
 Z    =        3696280
32                 I    =           51
27190
 XDOT =       4858
004451                 Wp   =           99
77546
 YDOT =       4123
171981  meter/sec      RA   =          252
86583  deg
 ZDOT =       4274
128082                 TA   =          304
57987
                                          MA   =          304
73511
                                          Ha   =            222
782  n
mi
                                          Hp   =            213
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4609713
41                 X    =         1448530
14
 Y    =      -18058190
20  feet           Y    =        -5488181
24  meter
 Z    =       12126903
93                 Z    =         3703211
00
 XDOT =      15938
334814                 XDOT =        4790
775130
 YDOT =      13527
467128  feet/sec       YDOT =        4177
121457  meter/sec
 ZDOT =      14022
729927                 ZDOT =        4297
563877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11598790
64                 X    =         3535311
39
 Y    =      -14561715
35  feet           Y    =        -4438410
84  meter
 Z    =       12158700
24                 Z    =         3705971
83
 XDOT =       7759
440524                 XDOT =        2365
077472
 YDOT =      18028
910943  feet/sec       YDOT =        5495
212055  meter/sec
 ZDOT =      14127
630408                 ZDOT =        4306
101748


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   18337
78953748  
00016717  00000-0  10270-3 0  9044
2 25544  51
6377 253
5281 0004852 110
1173 250
0502 15
54068185 24889


Satellite: ISS
Catalog Number: 25544
Epoch time:      18337
78953748   =   yrday
fracday
Element set:     904
Inclination:       51
6377  deg
RA of node:       253
5281  deg
Eccentricity:     
0004852     
Arg of perigee:   110
1173  deg
Mean anomaly:     250
0502  deg
Mean motion:   15
54068185  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2488
Checksum:              317


Coasting Arc #6 (Orbit 2488)
---------------------------------------

Vector Time (GMT): 2018/337/19:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4429235
88                 A    =         6782315
18  meter
 Y    =        3063526
17  meter          E    =           
0014932
 Z    =        4110031
08                 I    =           51
26668
 XDOT =      -1069
311443                 Wp   =           88
21142
 YDOT =       6605
409403  meter/sec      RA   =          252
41472  deg
 ZDOT =      -3758
853510                 TA   =           40
73560
                                          MA   =           40
62404
                                          Ha   =            222
872  n
mi
                                          Hp   =            212
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14531613
77                 X    =         4374684
78
 Y    =       10050938
88  feet           Y    =         3112751
75  meter
 Z    =       13484353
93                 Z    =         4131414
78
 XDOT =      -3508
239643                 XDOT =       -1124
836675
 YDOT =      21671
290692  feet/sec       YDOT =        6593
141342  meter/sec
 ZDOT =     -12332
196554                 ZDOT =       -3764
182480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15137959
24                 X    =         4614049
98
 Y    =        8968761
14  feet           Y    =         2733678
40  meter
 Z    =       13580150
43                 Z    =         4139229
85
 XDOT =      -1177
785499                 XDOT =        -358
989020
 YDOT =      20759
031245  feet/sec       YDOT =        6327
352724  meter/sec
 ZDOT =     -12356
917041                 ZDOT =       -3766
388314


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   18337
85384414  
00016717  00000-0  10270-3 0  9051
2 25544  51
6365 253
2048 0005246 112
8209 247
3488 15
54037416 24897


Satellite: ISS
Catalog Number: 25544
Epoch time:      18337
85384414   =   yrday
fracday
Element set:     905
Inclination:       51
6365  deg
RA of node:       253
2048  deg
Eccentricity:     
0005246     
Arg of perigee:   112
8209  deg
Mean anomaly:     247
3488  deg
Mean motion:   15
54037416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2489
Checksum:              322


Coasting Arc #7 (Orbit 2501)
---------------------------------------

Vector Time (GMT): 2018/338/16:07:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3336085
19                 A    =         6778033
48  meter
 Y    =        2849832
86  meter          E    =           
0018383
 Z    =       -5182378
18                 I    =           51
26502
 XDOT =      -3707
510174                 Wp   =           88
39190
 YDOT =      -6581
929714  meter/sec      RA   =          248
15023  deg
 ZDOT =      -1236
108034                 TA   =          169
67949
                                          MA   =          169
64169
                                          Ha   =            222
789  n
mi
                                          Hp   =            212
924

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10945161
38                 X    =        -3342531
17
 Y    =        9349845
34  feet           Y    =         2812490
73  meter
 Z    =      -17002553
10                 Z    =        -5198599
49
 XDOT =     -12163
747290                 XDOT =       -3627
629177
 YDOT =     -21594
257591  feet/sec       YDOT =       -6622
942947  meter/sec
 ZDOT =      -4055
472554                 ZDOT =       -1253
924556

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14255471
29                 X    =        -4345067
65
 Y    =       -1225127
40  feet           Y    =         -373418
83  meter
 Z    =      -17075818
53                 Z    =        -5204709
49
 XDOT =       6893
144182                 XDOT =        2101
030347
 YDOT =     -22727
334580  feet/sec       YDOT =       -6927
291580  meter/sec
 ZDOT =      -4134
837481                 ZDOT =       -1260
298464


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   18338
68980424  
00016717  00000-0  10270-3 0  9067
2 25544  51
6395 249
0414 0004862 111
5553 248
6118 15
54077491 25028


Satellite: ISS
Catalog Number: 25544
Epoch time:      18338
68980424   =   yrday
fracday
Element set:     906
Inclination:       51
6395  deg
RA of node:       249
0414  deg
Eccentricity:     
0004862     
Arg of perigee:   111
5553  deg
Mean anomaly:     248
6118  deg
Mean motion:   15
54077491  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2502
Checksum:              319


Coasting Arc #8 (Orbit 2503)
---------------------------------------

Vector Time (GMT): 2018/338/18:38:53
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4673444
04                 A    =         6782199
99  meter
 Y    =        2643883
55  meter          E    =           
0014602
 Z    =        4130879
61                 I    =           51
27790
 XDOT =       -476
344237                 Wp   =           88
55783
 YDOT =       6689
962089  meter/sec      RA   =          247
58329  deg
 ZDOT =      -3731
051628                 TA   =           40
03922
                                          MA   =           39
93167
                                          Ha   =            222
778  n
mi
                                          Hp   =            213
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15332821
64                 X    =         4623466
06
 Y    =        8674158
62  feet           Y    =         2695865
53  meter
 Z    =       13552754
63                 Z    =         4153460
77
 XDOT =      -1562
809178                 XDOT =        -532
994063
 YDOT =      21948
694519  feet/sec       YDOT =        6684
318778  meter/sec
 ZDOT =     -12240
983030                 ZDOT =       -3733
502732

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13954594
46                 X    =         4253360
39
 Y    =       10623151
70  feet           Y    =         3237936
64  meter
 Z    =       13653993
81                 Z    =         4161737
31
 XDOT =      -3609
094356                 XDOT =       -1100
051960
 YDOT =      20538
892730  feet/sec       YDOT =        6260
254504  meter/sec
 ZDOT =     -12252
765272                 ZDOT =       -3734
642855


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   18338
81841456  
00016717  00000-0  10270-3 0  9074
2 25544  51
6373 248
3971 0005099 115
3972 244
7709 15
54049638 25041


Satellite: ISS
Catalog Number: 25544
Epoch time:      18338
81841456   =   yrday
fracday
Element set:     907
Inclination:       51
6373  deg
RA of node:       248
3971  deg
Eccentricity:     
0005099     
Arg of perigee:   115
3972  deg
Mean anomaly:     244
7709  deg
Mean motion:   15
54049638  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2504
Checksum:              339


Coasting Arc #9 (Orbit 2518)
---------------------------------------

Vector Time (GMT): 2018/339/18:38:53
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4679491
34                 A    =         6785840
89  meter
 Y    =       -3972980
79  meter          E    =           
0008918
 Z    =       -2900981
51                 I    =           51
30441
 XDOT =       1629
501431                 Wp   =           94
57965
 YDOT =      -5564
826528  meter/sec      RA   =          242
57578  deg
 ZDOT =       5005
337613                 TA   =          232
22819
                                          MA   =          232
30900
                                          Ha   =            222
916  n
mi
                                          Hp   =            212
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15352661
87                 X    =        -4620624
89
 Y    =      -13034713
88  feet           Y    =        -4024980
72  meter
 Z    =       -9517655
86                 Z    =        -2923570
61
 XDOT =       5346
133305                 XDOT =        1667
294066
 YDOT =     -18257
304883  feet/sec       YDOT =       -5546
393437  meter/sec
 ZDOT =      16421
711329                 ZDOT =        5013
344608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13676856
21                 X    =        -4168705
77
 Y    =      -14717886
38  feet           Y    =        -4486011
77  meter
 Z    =       -9618793
59                 Z    =        -2931808
29
 XDOT =       6241
752556                 XDOT =        1902
486179
 YDOT =     -16529
693190  feet/sec       YDOT =       -5038
250484  meter/sec
 ZDOT =      16458
344928                 ZDOT =        5016
503534


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   18339
78298257  
00016717  00000-0  10270-3 0  9087
2 25544  51
6377 243
5890 0005354 118
3055 241
8638 15
54074519 25192


Satellite: ISS
Catalog Number: 25544
Epoch time:      18339
78298257   =   yrday
fracday
Element set:     908
Inclination:       51
6377  deg
RA of node:       243
5890  deg
Eccentricity:     
0005354     
Arg of perigee:   118
3055  deg
Mean anomaly:     241
8638  deg
Mean motion:   15
54074519  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2519
Checksum:              343


Coasting Arc #10 (Orbit 2529)
---------------------------------------

Vector Time (GMT): 2018/340/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3381812
68                 A    =         6789523
96  meter
 Y    =        5877613
77  meter          E    =           
0016791
 Z    =        -131898
60                 I    =           51
32973
 XDOT =      -4207
963079                 Wp   =          130
28859
 YDOT =       2298
352209  meter/sec      RA   =          239
19316  deg
 ZDOT =      -5986
889431                 TA   =           51
13870
                                          MA   =           50
98900
                                          Ha   =            222
856  n
mi
                                          Hp   =            213
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11095185
94                 X    =         3316476
91
 Y    =       19283509
74  feet           Y    =         5915066
25  meter
 Z    =        -432738
20                 Z    =         -115628
77
 XDOT =     -13805
653147                 XDOT =       -4204
269542
 YDOT =       7540
525619  feet/sec       YDOT =        2251
317098  meter/sec
 ZDOT =     -19642
025693                 ZDOT =       -6007
321379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22246873
43                 X    =        -6780847
02
 Y    =        -301700
81  feet           Y    =          -91958
41  meter
 Z    =        -360222
69                 Z    =         -109795
87
 XDOT =        476
315939                 XDOT =         145
181098
 YDOT =     -13984
746192  feet/sec       YDOT =       -4262
550639  meter/sec
 ZDOT =     -19734
172373                 ZDOT =       -6014
975739


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   18340
49033125  
00016717  00000-0  10270-3 0  9099
2 25544  51
6402 240
0678 0005071 117
5417 242
6251 15
54060306 25308


Satellite: ISS
Catalog Number: 25544
Epoch time:      18340
49033125   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:       240
0678  deg
Eccentricity:     
0005071     
Arg of perigee:   117
5417  deg
Mean anomaly:     242
6251  deg
Mean motion:   15
54060306  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2530
Checksum:              271


Coasting Arc #11 (Orbit 2545)
---------------------------------------

Vector Time (GMT): 2018/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2589425
68                 A    =         6788203
08  meter
 Y    =       -6012990
26  meter          E    =           
0017258
 Z    =        1771377
53                 I    =           51
34289
 XDOT =       5166
804385                 Wp   =           79
10175
 YDOT =       -550
291915  meter/sec      RA   =          234
20170  deg
 ZDOT =       5641
272149                 TA   =          300
43788
                                          MA   =          300
60828
                                          Ha   =            222
795  n
mi
                                          Hp   =            213
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8495491
07                 X    =        -2530598
81
 Y    =      -19727658
34  feet           Y    =        -6041618
31  meter
 Z    =        5811606
06                 Z    =         1758941
01
 XDOT =      16951
457955                 XDOT =        5145
171218
 YDOT =      -1805
419667  feet/sec       YDOT =        -492
634738  meter/sec
 ZDOT =      18508
110724                 ZDOT =        5666
318412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21363451
86                 X    =         6511580
13
 Y    =        2365631
55  feet           Y    =          721044
50  meter
 Z    =        5756331
22                 Z    =         1754529
76
 XDOT =      -6601
200659                 XDOT =       -2012
045961
 YDOT =      13951
611937  feet/sec       YDOT =        4252
451318  meter/sec
 ZDOT =      18620
827442                 ZDOT =        5675
628204


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   18341
51919911  
00016717  00000-0  10270-3 0  9101
2 25544  51
6399 234
9398 0004979 120
8966 239
2677 15
54068606 25468


Satellite: ISS
Catalog Number: 25544
Epoch time:      18341
51919911   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       234
9398  deg
Eccentricity:     
0004979     
Arg of perigee:   120
8966  deg
Mean anomaly:     239
2677  deg
Mean motion:   15
54068606  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2546
Checksum:              353


Coasting Arc #12 (Orbit 2560)
---------------------------------------

Vector Time (GMT): 2018/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1494698
82                 A    =         6784914
55  meter
 Y    =        5749094
48  meter          E    =           
0009268
 Z    =       -3282322
42                 I    =           51
35338
 XDOT =      -5943
351823                 Wp   =          111
32514
 YDOT =      -1131
516807  meter/sec      RA   =          229
20514  deg
 ZDOT =      -4702
413236                 TA   =          106
93583
                                          MA   =          106
83421
                                          Ha   =            222
711  n
mi
                                          Hp   =            213
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4903867
52                 X    =         1446243
68
 Y    =       18861858
53  feet           Y    =         5765538
73  meter
 Z    =      -10768774
36                 Z    =        -3275178
59
 XDOT =     -19499
185770                 XDOT =       -5907
415112
 YDOT =      -3712
325482  feet/sec       YDOT =       -1197
777966  meter/sec
 ZDOT =     -15427
864948                 ZDOT =       -4731
197106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18931093
18                 X    =        -5770197
20
 Y    =       -4702020
23  feet           Y    =        -1433175
77  meter
 Z    =      -10737264
18                 Z    =        -3272718
12
 XDOT =      12235
834536                 XDOT =        3729
482367
 YDOT =     -13843
430189  feet/sec       YDOT =       -4219
477522  meter/sec
 ZDOT =     -15557
226373                 ZDOT =       -4741
842598


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   18342
48375798  
00016717  00000-0  10270-3 0  9118
2 25544  51
6409 230
1320 0004912 124
6383 235
5234 15
54084688 25618


Satellite: ISS
Catalog Number: 25544
Epoch time:      18342
48375798   =   yrday
fracday
Element set:     911
Inclination:       51
6409  deg
RA of node:       230
1320  deg
Eccentricity:     
0004912     
Arg of perigee:   124
6383  deg
Mean anomaly:     235
5234  deg
Mean motion:   15
54084688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2561
Checksum:              310


Coasting Arc #13 (Orbit 2576)
---------------------------------------

Vector Time (GMT): 2018/343/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -224609
11                 A    =         6781214
62  meter
 Y    =       -5138132
77  meter          E    =           
0014203
 Z    =        4412260
90                 I    =           51
36248
 XDOT =       6430
208097                 Wp   =          116
19382
 YDOT =       2568
791226  meter/sec      RA   =          224
19995  deg
 ZDOT =       3304
281197                 TA   =          300
27544
                                          MA   =          300
41592
                                          Ha   =            222
731  n
mi
                                          Hp   =            213
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -736906
53                 X    =         -188568
92
 Y    =      -16857390
98  feet           Y    =        -5140443
55  meter
 Z    =       14475921
58                 Z    =         4411256
70
 XDOT =      21096
483259                 XDOT =        6384
954712
 YDOT =       8427
792735  feet/sec       YDOT =        2640
444830  meter/sec
 ZDOT =      10840
817577                 ZDOT =        3335
407501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15306781
67                 X    =         4665507
05
 Y    =        7108579
70  feet           Y    =         2166695
09  meter
 Z    =       14471955
53                 Z    =         4411052
04
 XDOT =     -16727
501115                 XDOT =       -5098
542340
 YDOT =      13567
798988  feet/sec       YDOT =        4135
465132  meter/sec
 ZDOT =      10980
583667                 ZDOT =        3346
881902


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   18343
51261984  
00016717  00000-0  10270-3 0  9125
2 25544  51
6399 225
0036 0005007 127
0710 233
0901 15
54078260 25770


Satellite: ISS
Catalog Number: 25544
Epoch time:      18343
51261984   =   yrday
fracday
Element set:     912
Inclination:       51
6399  deg
RA of node:       225
0036  deg
Eccentricity:     
0005007     
Arg of perigee:   127
0710  deg
Mean anomaly:     233
0901  deg
Mean motion:   15
54078260  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2577
Checksum:              289


Coasting Arc #14 (Orbit 2591)
---------------------------------------

Vector Time (GMT): 2018/344/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1235919
49                 A    =         6778238
26  meter
 Y    =        4276422
69  meter          E    =           
0016893
 Z    =       -5126214
03                 I    =           51
37736
 XDOT =      -6511
370135                 Wp   =           91
73549
 YDOT =      -3721
300621  meter/sec      RA   =          219
18712  deg
 ZDOT =      -1539
437072                 TA   =          163
37842
                                          MA   =          163
32298
                                          Ha   =            222
558  n
mi
                                          Hp   =            213
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4054853
96                 X    =        -1258747
30
 Y    =       14030258
18  feet           Y    =         4262474
77  meter
 Z    =      -16818287
51                 Z    =        -5132272
64
 XDOT =     -21362
762910                 XDOT =       -6461
795787
 YDOT =     -12208
991538  feet/sec       YDOT =       -3793
837910  meter/sec
 ZDOT =      -5050
646563                 ZDOT =       -1570
947154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10752101
91                 X    =        -3277240
66
 Y    =       -9836121
64  feet           Y    =        -2998049
88  meter
 Z    =      -16846002
37                 Z    =        -5134661
52
 XDOT =      19786
700661                 XDOT =        6030
986361
 YDOT =     -12764
611624  feet/sec       YDOT =       -3890
653623  meter/sec
 ZDOT =      -5192
042231                 ZDOT =       -1582
534472


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   18344
47717469  
00016717  00000-0  10270-3 0  9136
2 25544  51
6399 220
1960 0004835 131
7950 228
3616 15
54110270 25923


Satellite: ISS
Catalog Number: 25544
Epoch time:      18344
47717469   =   yrday
fracday
Element set:     913
Inclination:       51
6399  deg
RA of node:       220
1960  deg
Eccentricity:     
0004835     
Arg of perigee:   131
7950  deg
Mean anomaly:     228
3616  deg
Mean motion:   15
54110270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2592
Checksum:              313


Coasting Arc #15 (Orbit 2599)
---------------------------------------

Vector Time (GMT): 2018/344/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3977165
78                 A    =         6787580
51  meter
 Y    =        5070315
55  meter          E    =           
0011547
 Z    =       -2121455
02                 I    =           51
42003
 XDOT =      -5071
927627                 Wp   =          138
38595
 YDOT =       1689
753227  meter/sec      RA   =          216
66388  deg
 ZDOT =      -5495
665364                 TA   =           65
19271
                                          MA   =           65
07264
                                          Ha   =            222
657  n
mi
                                          Hp   =            213
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13048444
15                 X    =         3930477
41
 Y    =       16634893
55  feet           Y    =         5114530
18  meter
 Z    =       -6960154
27                 Z    =        -2102248
12
 XDOT =     -16640
182502                 XDOT =       -5063
750918
 YDOT =       5543
809801  feet/sec       YDOT =        1633
081771  meter/sec
 ZDOT =     -18030
398177                 ZDOT =       -5520
282981

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20556523
20                 X    =         6265628
27
 Y    =       -5059578
25  feet           Y    =        -1542159
45  meter
 Z    =       -6874252
51                 Z    =        -2095272
17
 XDOT =      -2140
532134                 XDOT =        -652
434194
 YDOT =      15835
278361  feet/sec       YDOT =        4826
592845  meter/sec
 ZDOT =     -18141
357872                 ZDOT =       -5529
485879


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   18344
99160308  
00016717  00000-0  10270-3 0  9148
2 25544  51
6384 217
6293 0005097 137
0906 223
0645 15
54088267 26002


Satellite: ISS
Catalog Number: 25544
Epoch time:      18344
99160308   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:       217
6293  deg
Eccentricity:     
0005097     
Arg of perigee:   137
0906  deg
Mean anomaly:     223
0645  deg
Mean motion:   15
54088267  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2600
Checksum:              314


Coasting Arc #16 (Orbit 2615)
---------------------------------------

Vector Time (GMT): 2018/345/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2824070
66                 A    =         6784155
16  meter
 Y    =       -5050727
88  meter          E    =           
0016006
 Z    =        3531949
00                 I    =           51
43640
 XDOT =       6226
417749                 Wp   =          105
73086
 YDOT =       -343
100477  meter/sec      RA   =          211
67054  deg
 ZDOT =       4466
715923                 TA   =          296
05065
                                          MA   =          296
21534
                                          Ha   =            222
579  n
mi
                                          Hp   =            213
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9265323
70                 X    =        -2784538
43
 Y    =      -16570629
52  feet           Y    =        -5082087
93  meter
 Z    =       11587759
18                 Z    =         3518326
15
 XDOT =      20427
879754                 XDOT =        6208
094726
 YDOT =      -1125
657733  feet/sec       YDOT =        -273
575267  meter/sec
 ZDOT =      14654
579801                 ZDOT =        4496
917111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18917173
54                 X    =        -5765954
49
 Y    =        1994423
87  feet           Y    =          607900
40  meter
 Z    =       11526966
96                 Z    =         3513419
53
 XDOT =       7186
210964                 XDOT =        2190
357102
 YDOT =     -17725
233313  feet/sec       YDOT =       -5402
651114  meter/sec
 ZDOT =      14790
543711                 ZDOT =        4508
157723


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   18346
02045685  
00016717  00000-0  10270-3 0  9155
2 25544  51
6388 212
5003 0005027 139
9652 220
1872 15
54108250 26163


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
02045685   =   yrday
fracday
Element set:     915
Inclination:       51
6388  deg
RA of node:       212
5003  deg
Eccentricity:     
0005027     
Arg of perigee:   139
9652  deg
Mean anomaly:     220
1872  deg
Mean motion:   15
54108250  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2616
Checksum:              292


Coasting Arc #17 (Orbit 2630)
---------------------------------------

Vector Time (GMT): 2018/346/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1333886
99                 A    =         6780449
70  meter
 Y    =        4790021
55  meter          E    =           
0012711
 Z    =       -4620579
13                 I    =           51
45197
 XDOT =      -7010
877616                 Wp   =           92
79612
 YDOT =       -888
572854  meter/sec      RA   =          206
66956  deg
 ZDOT =      -2952
734385                 TA   =          147
70864
                                          MA   =          147
63076
                                          Ha   =            222
555  n
mi
                                          Hp   =            213
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4376269
66                 X    =         1302668
77
 Y    =       15715293
79  feet           Y    =         4804763
87  meter
 Z    =      -15159380
33                 Z    =        -4614174
97
 XDOT =     -23001
566980                 XDOT =       -6986
077496
 YDOT =      -2915
265270  feet/sec       YDOT =        -966
834424  meter/sec
 ZDOT =      -9687
448770                 ZDOT =       -2986
730557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16234253
12                 X    =         4948200
35
 Y    =        1851942
17  feet           Y    =          564471
97  meter
 Z    =      -15131039
06                 Z    =        -4611940
70
 XDOT =     -11305
259629                 XDOT =       -3445
843135
 YDOT =      18908
558448  feet/sec       YDOT =        5763
328615  meter/sec
 ZDOT =      -9840
388331                 ZDOT =       -2999
350363


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   18346
98500767  
00016717  00000-0  10270-3 0  9168
2 25544  51
6381 207
6926 0005071 142
4532 217
6975 15
54086543 26312


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
98500767   =   yrday
fracday
Element set:     916
Inclination:       51
6381  deg
RA of node:       207
6926  deg
Eccentricity:     
0005071     
Arg of perigee:   142
4532  deg
Mean anomaly:     217
6975  deg
Mean motion:   15
54086543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2631
Checksum:              324


Coasting Arc #18 (Orbit 2646)
---------------------------------------

Vector Time (GMT): 2018/347/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         307863
09                 A    =         6777884
41  meter
 Y    =       -4332068
03  meter          E    =           
0008869
 Z    =        5199512
01                 I    =           51
47373
 XDOT =       7336
897940                 Wp   =          136
84377
 YDOT =       1921
297943  meter/sec      RA   =          201
66186  deg
 ZDOT =       1158
830246                 TA   =          301
98133
                                          MA   =          302
06750
                                          Ha   =            222
431  n
mi
                                          Hp   =            213
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1010049
50                 X    =          331026
18
 Y    =      -14212821
62  feet           Y    =        -4328496
18  meter
 Z    =       17058766
43                 Z    =         5201063
42
 XDOT =      24071
187466                 XDOT =        7309
239183
 YDOT =       6303
470940  feet/sec       YDOT =        2003
189497  meter/sec
 ZDOT =       3801
936503                 ZDOT =        1194
403244

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12902025
03                 X    =        -3932537
23
 Y    =       -6025704
57  feet           Y    =        -1836634
75  meter
 Z    =       17066184
25                 Z    =         5201772
96
 XDOT =      14212
292744                 XDOT =        4331
906828
 YDOT =     -19140
050907  feet/sec       YDOT =       -5833
887516  meter/sec
 ZDOT =       3961
892896                 ZDOT =        1207
584955


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   18348
01385775  
00016717  00000-0  10270-3 0  9175
2 25544  51
6380 202
5641 0004987 146
5280 213
6189 15
54110367 26471


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
01385775   =   yrday
fracday
Element set:     917
Inclination:       51
6380  deg
RA of node:       202
5641  deg
Eccentricity:     
0004987     
Arg of perigee:   146
5280  deg
Mean anomaly:     213
6189  deg
Mean motion:   15
54110367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2647
Checksum:              320


Coasting Arc #19 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2018/348/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4504867
82                 A    =         6780427
29  meter
 Y    =       -2184416
39  meter          E    =           
0010506
 Z    =        4563227
74                 I    =           51
48651
 XDOT =       5329
203758                 Wp   =           93
04754
 YDOT =       4601
963388  meter/sec      RA   =          200
62935  deg
 ZDOT =      -3052
560909                 TA   =           27
53373
                                          MA   =           27
47812
                                          Ha   =            222
281  n
mi
                                          Hp   =            213
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14779750
06                 X    =         4506794
06
 Y    =       -7166720
44  feet           Y    =        -2134029
40  meter
 Z    =       14971219
62                 Z    =         4585115
30
 XDOT =      17484
264297                 XDOT =        5292
174937
 YDOT =      15098
305080  feet/sec       YDOT =        4661
351437  meter/sec
 ZDOT =     -10014
963612                 ZDOT =       -3026
763129

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15911009
55                 X    =        -4849675
71
 Y    =       -3698090
19  feet           Y    =        -1127177
89  meter
 Z    =       15069977
26                 Z    =         4593329
07
 XDOT =      -4366
889478                 XDOT =       -1331
027913
 YDOT =     -21625
160066  feet/sec       YDOT =       -6591
348788  meter/sec
 ZDOT =      -9899
278873                 ZDOT =       -3017
300201


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   18348
20676757  
00016717  00000-0  10270-3 0  9180
2 25544  51
6359 201
6029 0004821 145
2178 214
9290 15
54105744 26500


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
20676757   =   yrday
fracday
Element set:     918
Inclination:       51
6359  deg
RA of node:       201
6029  deg
Eccentricity:     
0004821     
Arg of perigee:   145
2178  deg
Mean anomaly:     214
9290  deg
Mean motion:   15
54105744  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2650
Checksum:              314


Coasting Arc #20 (Orbit 2664)
---------------------------------------

Vector Time (GMT): 2018/349/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5681599
60                 A    =         6784187
20  meter
 Y    =        1287708
83  meter          E    =           
0008887
 Z    =       -3487684
28                 I    =           51
53130
 XDOT =      -3867
875988                 Wp   =          120
30870
 YDOT =      -4817
111653  meter/sec      RA   =          195
63300  deg
 ZDOT =       4526
644790                 TA   =          198
69152
                                          MA   =          198
72418
                                          Ha   =            222
379  n
mi
                                          Hp   =            213
550

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18640418
64                 X    =        -5678635
53
 Y    =        4224766
51  feet           Y    =         1224190
03  meter
 Z    =      -11442533
72                 Z    =        -3515276
23
 XDOT =     -12689
881852                 XDOT =       -3835
710273
 YDOT =     -15804
172091  feet/sec       YDOT =       -4860
185366  meter/sec
 ZDOT =      14851
196819                 ZDOT =        4507
933819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17212242
66                 X    =         5246291
56
 Y    =        8135786
49  feet           Y    =         2479787
72  meter
 Z    =      -11566897
50                 Z    =        -3525590
36
 XDOT =        899
827399                 XDOT =         274
267391
 YDOT =      19071
994243  feet/sec       YDOT =        5813
143845  meter/sec
 ZDOT =      14767
422949                 ZDOT =        4501
110515


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   18349
17131199  
00016717  00000-0  10270-3 0  9194
2 25544  51
6368 196
7948 0004769 147
0956 213
0495 15
54086837 26653


Satellite: ISS
Catalog Number: 25544
Epoch time:      18349
17131199   =   yrday
fracday
Element set:     919
Inclination:       51
6368  deg
RA of node:       196
7948  deg
Eccentricity:     
0004769     
Arg of perigee:   147
0956  deg
Mean anomaly:     213
0495  deg
Mean motion:   15
54086837  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2665
Checksum:              361
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