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

 
Date: November 6th 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


311/16:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 214 2

319/09:49:40 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 5

320/04:47:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 5

320/18:14:08 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 3

322/09:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 213 1

322/19:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 213 2

Coasting Arc #1 (Orbit 2048)
---------------------------------------

Vector Time (GMT): 2018/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3441945
89                 A    =         6786314
47  meter
 Y    =        5063483
05  meter          E    =           
0015397
 Z    =        2906805
56                 I    =           51
86639
 XDOT =      -5691
882115                 Wp   =           66
21554
 YDOT =        957
361706  meter/sec      RA   =           33
91052  deg
 ZDOT =       5057
030704                 TA   =          326
82687
                                          MA   =          326
92331
                                          Ha   =            222
183  n
mi
                                          Hp   =            214
466

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11292473
41                 X    =         3370948
74
 Y    =       16612477
21  feet           Y    =         5101576
45  meter
 Z    =        9536763
66                 Z    =         2923353
05
 XDOT =     -18674
153921                 XDOT =       -5726
729527
 YDOT =       3140
950478  feet/sec       YDOT =         893
516517  meter/sec
 ZDOT =      16591
308084                 ZDOT =        5029
296188

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19602369
12                 X    =        -5974802
11
 Y    =       -4222497
43  feet           Y    =        -1287017
22  meter
 Z    =        9610507
59                 Z    =         2929282
71
 XDOT =      11077
798457                 XDOT =        3376
512970
 YDOT =     -13837
665004  feet/sec       YDOT =       -4217
720293  meter/sec
 ZDOT =      16466
409670                 ZDOT =        5018
961667


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   18309
55834577  
00016717  00000-0  10270-3 0  9002
2 25544  51
6428  34
2302 0004382  13
7100 346
4171 15
53914070 20497


Satellite: ISS
Catalog Number: 25544
Epoch time:      18309
55834577   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:        34
2302  deg
Eccentricity:     
0004382     
Arg of perigee:    13
7100  deg
Mean anomaly:     346
4171  deg
Mean motion:   15
53914070  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2049
Checksum:              283


Coasting Arc #2 (Orbit 2063)
---------------------------------------

Vector Time (GMT): 2018/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2171901
08                 A    =         6782693
24  meter
 Y    =       -4922496
35  meter          E    =           
0010840
 Z    =       -4142052
18                 I    =           51
82493
 XDOT =       6644
745401                 Wp   =           51
15421
 YDOT =        263
254613  meter/sec      RA   =           28
94380  deg
 ZDOT =      -3797
116781                 TA   =          179
73979
                                          MA   =          179
73923
                                          Ha   =            222
292  n
mi
                                          Hp   =            214
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7125659
71                 X    =        -2096574
49
 Y    =      -16149922
40  feet           Y    =        -4946363
01  meter
 Z    =      -13589410
04                 Z    =        -4152419
68
 XDOT =      21800
345805                 XDOT =        6659
752642
 YDOT =        863
696236  feet/sec       YDOT =         337
644558  meter/sec
 ZDOT =     -12457
732220                 ZDOT =       -3764
801612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16369501
61                 X    =         4989424
09
 Y    =        6510257
57  feet           Y    =         1984326
51  meter
 Z    =      -13635360
23                 Z    =        -4156057
80
 XDOT =     -15667
090283                 XDOT =       -4775
329118
 YDOT =      13606
393346  feet/sec       YDOT =        4147
228692  meter/sec
 ZDOT =     -12312
406121                 ZDOT =       -3752
821386


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   18310
52301547  
00016717  00000-0  10270-3 0  9018
2 25544  51
6417  29
4241 0004372  16
8480 343
2817 15
53898322 20647


Satellite: ISS
Catalog Number: 25544
Epoch time:      18310
52301547   =   yrday
fracday
Element set:     901
Inclination:       51
6417  deg
RA of node:        29
4241  deg
Eccentricity:     
0004372     
Arg of perigee:    16
8480  deg
Mean anomaly:     343
2817  deg
Mean motion:   15
53898322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2064
Checksum:              289


Coasting Arc #3 (Orbit 2079)
---------------------------------------

Vector Time (GMT): 2018/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         668705
48                 A    =         6779419
34  meter
 Y    =        4568858
94  meter          E    =           
0006779
 Z    =        4957680
14                 I    =           51
78523
 XDOT =      -7232
235445                 Wp   =           83
21510
 YDOT =      -1324
237990  meter/sec      RA   =           23
96502  deg
 ZDOT =       2194
097546                 TA   =          345
43210
                                          MA   =          345
45163
                                          Ha   =            222
297  n
mi
                                          Hp   =            214
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2193915
62                 X    =          593483
05
 Y    =       14989694
69  feet           Y    =         4575916
34  meter
 Z    =       16265354
78                 Z    =         4960745
80
 XDOT =     -23727
806579                 XDOT =       -7227
548000
 YDOT =      -4344
612829  feet/sec       YDOT =       -1405
087634  meter/sec
 ZDOT =       7198
482763                 ZDOT =        2158
976258

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12194955
57                 X    =        -3717022
46
 Y    =       -8964345
55  feet           Y    =        -2732332
52  meter
 Z    =       16278499
51                 Z    =         4961686
65
 XDOT =      19045
531826                 XDOT =        5805
078101
 YDOT =     -13113
296925  feet/sec       YDOT =       -3996
932903  meter/sec
 ZDOT =       7040
694379                 ZDOT =        2146
003647


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   18311
55199063  
00016717  00000-0  10270-3 0  9021
2 25544  51
6421  24
2966 0004393  19
7944 340
3378 15
53938985 20807


Satellite: ISS
Catalog Number: 25544
Epoch time:      18311
55199063   =   yrday
fracday
Element set:     902
Inclination:       51
6421  deg
RA of node:        24
2966  deg
Eccentricity:     
0004393     
Arg of perigee:    19
7944  deg
Mean anomaly:     340
3378  deg
Mean motion:   15
53938985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2080
Checksum:              322


Coasting Arc #4 (Orbit 2082)
---------------------------------------

Vector Time (GMT): 2018/311/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4212869
74                 A    =         6780315
37  meter
 Y    =        2306794
06  meter          E    =           
0011680
 Z    =        4781831
82                 I    =           51
77917
 XDOT =      -5536
212207                 Wp   =           46
30042
 YDOT =      -4603
291238  meter/sec      RA   =           22
92754  deg
 ZDOT =      -2644
914254                 TA   =           69
79653
                                          MA   =           69
67097
                                          Ha   =            222
563  n
mi
                                          Hp   =            214
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13821751
10                 X    =        -4261580
12
 Y    =        7568221
97  feet           Y    =         2259410
50  meter
 Z    =       15688424
59                 Z    =         4761248
24
 XDOT =     -18163
425877                 XDOT =       -5471
477488
 YDOT =     -15102
661542  feet/sec       YDOT =       -4664
839076  meter/sec
 ZDOT =      -8677
540202                 ZDOT =       -2671
650750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13290767
55                 X    =        -4051025
95
 Y    =       -8636021
73  feet           Y    =        -2632259
42  meter
 Z    =       15595514
74                 Z    =         4753512
89
 XDOT =       4020
751755                 XDOT =        1225
525135
 YDOT =     -22145
387912  feet/sec       YDOT =       -6749
914236  meter/sec
 ZDOT =      -8797
148088                 ZDOT =       -2681
370737


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   18311
74492347  
00016717  00000-0  10270-3 0  9034
2 25544  51
6395  23
3365 0004768  21
9042 338
2314 15
53930325 20839


Satellite: ISS
Catalog Number: 25544
Epoch time:      18311
74492347   =   yrday
fracday
Element set:     903
Inclination:       51
6395  deg
RA of node:        23
3365  deg
Eccentricity:     
0004768     
Arg of perigee:    21
9042  deg
Mean anomaly:     338
2314  deg
Mean motion:   15
53930325  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2083
Checksum:              297


Coasting Arc #5 (Orbit 2097)
---------------------------------------

Vector Time (GMT): 2018/312/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5395899
42                 A    =         6783794
63  meter
 Y    =       -1444523
98  meter          E    =           
0008692
 Z    =       -3853904
70                 I    =           51
75992
 XDOT =       4256
121694                 Wp   =           69
75220
 YDOT =       4825
494488  meter/sec      RA   =           17
94919  deg
 ZDOT =       4160
891836                 TA   =          243
94228
                                          MA   =          244
03178
                                          Ha   =            222
691  n
mi
                                          Hp   =            214
133

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17703082
09                 X    =         5430372
22
 Y    =       -4739251
90  feet           Y    =        -1383990
48  meter
 Z    =      -12644044
29                 Z    =        -3827608
84
 XDOT =      13963
653853                 XDOT =        4181
633353
 YDOT =      15831
674829  feet/sec       YDOT =        4872
672845  meter/sec
 ZDOT =      13651
219936                 ZDOT =        4181
386331

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12871593
00                 X    =         3923261
55
 Y    =       13159169
82  feet           Y    =         4010914
96  meter
 Z    =      -12525566
80                 Z    =        -3817792
76
 XDOT =      -6008
559632                 XDOT =       -1831
408976
 YDOT =      18925
032782  feet/sec       YDOT =        5768
349992  meter/sec
 ZDOT =      13742
707442                 ZDOT =        4188
777228


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   18312
70958383  
00016717  00000-0  10270-3 0  9049
2 25544  51
6398  18
5300 0004956  26
7503 333
3904 15
53907452 20983


Satellite: ISS
Catalog Number: 25544
Epoch time:      18312
70958383   =   yrday
fracday
Element set:     904
Inclination:       51
6398  deg
RA of node:        18
5300  deg
Eccentricity:     
0004956     
Arg of perigee:    26
7503  deg
Mean anomaly:     333
3904  deg
Mean motion:   15
53907452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2098
Checksum:              316


Coasting Arc #6 (Orbit 2113)
---------------------------------------

Vector Time (GMT): 2018/313/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6270487
43                 A    =         6787242
73  meter
 Y    =         592348
92  meter          E    =           
0015638
 Z    =        2517328
09                 I    =           51
73868
 XDOT =      -2602
367103                 Wp   =           86
25630
 YDOT =      -4890
805957  meter/sec      RA   =           12
97688  deg
 ZDOT =      -5302
072626                 TA   =           65
53642
                                          MA   =           65
37339
                                          Ha   =            222
646  n
mi
                                          Hp   =            213
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20572465
31                 X    =        -6288873
37
 Y    =        1943401
98  feet           Y    =          522125
09  meter
 Z    =        8258950
42                 Z    =         2486822
80
 XDOT =      -8537
949813                 XDOT =       -2521
727982
 YDOT =     -16045
951301  feet/sec       YDOT =       -4919
456366  meter/sec
 ZDOT =     -17395
251396                 ZDOT =       -5314
518662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12123548
38                 X    =        -3695257
55
 Y    =      -16800937
40  feet           Y    =        -5120925
72  meter
 Z    =        8121667
28                 Z    =         2475484
19
 XDOT =       8345
907263                 XDOT =        2543
832534
 YDOT =     -14505
485801  feet/sec       YDOT =       -4421
272072  meter/sec
 ZDOT =     -17450
520884                 ZDOT =       -5318
918765


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   18313
73854925  
00016717  00000-0  10270-3 0  9051
2 25544  51
6385  13
4016 0005032  28
0949 332
0474 15
53953895 21141


Satellite: ISS
Catalog Number: 25544
Epoch time:      18313
73854925   =   yrday
fracday
Element set:     905
Inclination:       51
6385  deg
RA of node:        13
4016  deg
Eccentricity:     
0005032     
Arg of perigee:    28
0949  deg
Mean anomaly:     332
0474  deg
Mean motion:   15
53953895  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2114
Checksum:              306


Coasting Arc #7 (Orbit 2128)
---------------------------------------

Vector Time (GMT): 2018/314/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6709377
18                 A    =         6789451
67  meter
 Y    =         162243
89  meter          E    =           
0014806
 Z    =        -981067
32                 I    =           51
71331
 XDOT =        740
320908                 Wp   =           36
98804
 YDOT =       4822
010754  meter/sec      RA   =            8
01144  deg
 ZDOT =       5918
312116                 TA   =          312
39294
                                          MA   =          312
51815
                                          Ha   =            222
701  n
mi
                                          Hp   =            213
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22012392
32                 X    =         6711829
88
 Y    =         532296
23  feet           Y    =          237286
57  meter
 Z    =       -3218724
80                 Z    =         -948468
77
 XDOT =       2428
874370                 XDOT =         657
596111
 YDOT =      15820
245256  feet/sec       YDOT =        4829
826707  meter/sec
 ZDOT =      19417
034502                 ZDOT =        5921
707727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11030707
68                 X    =         3362159
70
 Y    =       19080733
13  feet           Y    =         5815807
46  meter
 Z    =       -3072141
86                 Z    =         -936388
84
 XDOT =     -10912
311486                 XDOT =       -3326
072541
 YDOT =       9405
061323  feet/sec       YDOT =        2866
662691  meter/sec
 ZDOT =      19431
604315                 ZDOT =        5922
752995


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   18314
70320243  
00016717  00000-0  10270-3 0  9061
2 25544  51
6381   8
5951 0004896  34
5161 325
6309 15
53957995 21291


Satellite: ISS
Catalog Number: 25544
Epoch time:      18314
70320243   =   yrday
fracday
Element set:     906
Inclination:       51
6381  deg
RA of node:         8
5951  deg
Eccentricity:     
0004896     
Arg of perigee:    34
5161  deg
Mean anomaly:     325
6309  deg
Mean motion:   15
53957995  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2129
Checksum:              316


Coasting Arc #8 (Orbit 2144)
---------------------------------------

Vector Time (GMT): 2018/315/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6690536
42                 A    =         6789605
50  meter
 Y    =        -908385
16  meter          E    =           
0010422
 Z    =        -698044
22                 I    =           51
68192
 XDOT =       1245
756262                 Wp   =          111
34602
 YDOT =      -4651
898697  meter/sec      RA   =            3
04551  deg
 ZDOT =      -5961
942560                 TA   =           76
18551
                                          MA   =           76
06956
                                          Ha   =            222
730  n
mi
                                          Hp   =            213
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21950578
80                 X    =        -6676490
55
 Y    =       -2980266
27  feet           Y    =         -983124
81  meter
 Z    =       -2290171
32                 Z    =         -730511
10
 XDOT =       4087
126845                 XDOT =        1326
643047
 YDOT =     -15262
134832  feet/sec       YDOT =       -4637
515197  meter/sec
 ZDOT =     -19560
179002                 ZDOT =       -5955
694775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9237313
83                 X    =        -2815533
26
 Y    =      -20116970
07  feet           Y    =        -6131652
48  meter
 Z    =       -2436047
96                 Z    =         -742507
42
 XDOT =      13680
124137                 XDOT =        4169
701837
 YDOT =      -3944
667270  feet/sec       YDOT =       -1202
334584  meter/sec
 ZDOT =     -19531
402463                 ZDOT =       -5953
171471


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   18315
73215996  
00016717  00000-0  10270-3 0  9074
2 25544  51
6392   3
4660 0005082  35
9434 324
2059 15
53951233 21454


Satellite: ISS
Catalog Number: 25544
Epoch time:      18315
73215996   =   yrday
fracday
Element set:     907
Inclination:       51
6392  deg
RA of node:         3
4660  deg
Eccentricity:     
0005082     
Arg of perigee:    35
9434  deg
Mean anomaly:     324
2059  deg
Mean motion:   15
53951233  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2145
Checksum:              302


Coasting Arc #9 (Orbit 2160)
---------------------------------------

Vector Time (GMT): 2018/316/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6188363
17                 A    =         6787488
34  meter
 Y    =        1585531
98  meter          E    =           
0018127
 Z    =        2264797
44                 I    =           51
64172
 XDOT =      -3131
600518                 Wp   =           63
61059
 YDOT =       4413
707653  meter/sec      RA   =          358
07631  deg
 ZDOT =       5441
077443                 TA   =          321
61159
                                          MA   =          321
74045
                                          Ha   =            222
613  n
mi
                                          Hp   =            213
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20303028
78                 X    =         6159172
00
 Y    =        5201876
56  feet           Y    =         1654571
21  meter
 Z    =        7430437
80                 Z    =         2294788
04
 XDOT =     -10274
279916                 XDOT =       -3207
153402
 YDOT =      14480
668154  feet/sec       YDOT =        4378
265194  meter/sec
 ZDOT =      17851
303948                 ZDOT =        5425
681685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6801236
84                 X    =         2073016
99
 Y    =       19773637
31  feet           Y    =         6027004
65  meter
 Z    =        7565074
22                 Z    =         2305834
62
 XDOT =     -16369
278247                 XDOT =       -4989
356010
 YDOT =      -1204
422058  feet/sec       YDOT =        -367
107843  meter/sec
 ZDOT =      17781
424264                 ZDOT =        5419
778116


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   18316
76111145  
00016717  00000-0  10270-3 0  9080
2 25544  51
6388 358
3388 0004892  39
7186 320
4324 15
53987749 21614


Satellite: ISS
Catalog Number: 25544
Epoch time:      18316
76111145   =   yrday
fracday
Element set:     908
Inclination:       51
6388  deg
RA of node:       358
3388  deg
Eccentricity:     
0004892     
Arg of perigee:    39
7186  deg
Mean anomaly:     320
4324  deg
Mean motion:   15
53987749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2161
Checksum:              338


Coasting Arc #10 (Orbit 2175)
---------------------------------------

Vector Time (GMT): 2018/317/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5251299
47                 A    =         6784072
56  meter
 Y    =       -2280166
42  meter          E    =           
0010157
 Z    =       -3652027
28                 I    =           51
59695
 XDOT =       4799
460652                 Wp   =           61
29761
 YDOT =      -4067
388941  meter/sec      RA   =          353
09593  deg
 ZDOT =      -4366
173588                 TA   =          162
03811
                                          MA   =          162
00220
                                          Ha   =            222
817  n
mi
                                          Hp   =            213
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17228672
80                 X    =        -5207671
85
 Y    =       -7480860
96  feet           Y    =        -2338645
99  meter
 Z    =      -11981716
80                 Z    =        -3677430
78
 XDOT =      15746
261982                 XDOT =        4865
795491
 YDOT =     -13344
451906  feet/sec       YDOT =       -4013
346936  meter/sec
 ZDOT =     -14324
716495                 ZDOT =       -4342
698211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3506279
08                 X    =        -1068713
86
 Y    =      -18378084
30  feet           Y    =        -5601640
09  meter
 Z    =      -12095619
43                 Z    =        -3686744
80
 XDOT =      18618
576748                 XDOT =        5674
942193
 YDOT =       5796
298446  feet/sec       YDOT =        1766
711766  meter/sec
 ZDOT =     -14218
558931                 ZDOT =       -4333
816762


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   18317
72575365  
00016717  00000-0  10270-3 0  9096
2 25544  51
6388 353
5307 0005100  42
0878 318
0666 15
53958120 21769


Satellite: ISS
Catalog Number: 25544
Epoch time:      18317
72575365   =   yrday
fracday
Element set:     909
Inclination:       51
6388  deg
RA of node:       353
5307  deg
Eccentricity:     
0005100     
Arg of perigee:    42
0878  deg
Mean anomaly:     318
0666  deg
Mean motion:   15
53958120  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2176
Checksum:              319


Coasting Arc #11 (Orbit 2191)
---------------------------------------

Vector Time (GMT): 2018/318/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3953331
41                 A    =         6780407
84  meter
 Y    =        2939596
81  meter          E    =           
0010651
 Z    =        4649515
71                 I    =           51
55333
 XDOT =      -6109
884769                 Wp   =           89
91986
 YDOT =       3633
474098  meter/sec      RA   =          348
10500  deg
 ZDOT =       2892
102403                 TA   =          331
28882
                                          MA   =          331
34741
                                          Ha   =            222
612  n
mi
                                          Hp   =            213
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12970247
41                 X    =         3897581
02
 Y    =        9644346
48  feet           Y    =         2983493
81  meter
 Z    =       15254316
62                 Z    =         4668584
56
 XDOT =     -20045
553705                 XDOT =       -6164
109677
 YDOT =      11920
846778  feet/sec       YDOT =        3564
845826  meter/sec
 ZDOT =       9488
524943                 ZDOT =        2862
290751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -419593
22                 X    =         -127892
01
 Y    =       16076518
52  feet           Y    =         4900122
84  meter
 Z    =       15339635
14                 Z    =         4675520
79
 XDOT =     -20186
705994                 XDOT =       -6152
907987
 YDOT =      -9469
860027  feet/sec       YDOT =       -2886
413336  meter/sec
 ZDOT =       9353
946366                 ZDOT =        2851
082852


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   18318
75469763  
00016717  00000-0  10270-3 0  9106
2 25544  51
6398 348
4034 0004879  44
7534 315
4012 15
54001204 21927


Satellite: ISS
Catalog Number: 25544
Epoch time:      18318
75469763   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:       348
4034  deg
Eccentricity:     
0004879     
Arg of perigee:    44
7534  deg
Mean anomaly:     315
4012  deg
Mean motion:   15
54001204  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2192
Checksum:              307


Coasting Arc #12 (Orbit 2202)
---------------------------------------

Vector Time (GMT): 2018/319/09:49:40
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3759286
94                 A    =         6779808
43  meter
 Y    =        2929969
93  meter          E    =           
0009776
 Z    =        4813361
88                 I    =           51
52974
 XDOT =      -6182
474714                 Wp   =           91
71178
 YDOT =       3784
173237  meter/sec      RA   =          344
56837  deg
 ZDOT =       2520
378919                 TA   =          333
46201
                                          MA   =          333
51203
                                          Ha   =            222
670  n
mi
                                          Hp   =            213
489

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12333618
58                 X    =         3702862
74
 Y    =        9612762
23  feet           Y    =         2971693
26  meter
 Z    =       15791869
67                 Z    =         4831486
45
 XDOT =     -20283
709691                 XDOT =       -6236
573723
 YDOT =      12415
266527  feet/sec       YDOT =        3714
733953  meter/sec
 ZDOT =       8268
959707                 ZDOT =        2490
214936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14859141
51                 X    =        -4529066
33
 Y    =       -4600229
66  feet           Y    =        -1402150
00  meter
 Z    =       15872942
18                 Z    =         4838072
78
 XDOT =      14211
496691                 XDOT =        4331
664191
 YDOT =     -17789
384339  feet/sec       YDOT =       -5422
204346  meter/sec
 ZDOT =       8132
782558                 ZDOT =        2478
872124


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   18319
46209470  
00016717  00000-0  10270-3 0  9113
2 25544  51
6413 344
8766 0004820  48
8972 311
2596 15
53980971 22034


Satellite: ISS
Catalog Number: 25544
Epoch time:      18319
46209470   =   yrday
fracday
Element set:     911
Inclination:       51
6413  deg
RA of node:       344
8766  deg
Eccentricity:     
0004820     
Arg of perigee:    48
8972  deg
Mean anomaly:     311
2596  deg
Mean motion:   15
53980971  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2203
Checksum:              321


Coasting Arc #13 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2018/320/04:47:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5906650
72                 A    =         6789198
97  meter
 Y    =        3106434
96  meter          E    =           
0016156
 Z    =        1217506
99                 I    =           51
53437
 XDOT =      -3210
046833                 Wp   =          105
78297
 YDOT =      -3790
224096  meter/sec      RA   =          340
59268  deg
 ZDOT =      -5842
360368                 TA   =           60
96617
                                          MA   =           60
80440
                                          Ha   =            222
841  n
mi
                                          Hp   =            213
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19378775
32                 X    =        -5946862
83
 Y    =       10191715
73  feet           Y    =         3040157
82  meter
 Z    =        3994445
51                 Z    =         1188716
55
 XDOT =     -10531
649716                 XDOT =       -3139
045444
 YDOT =     -12435
118425  feet/sec       YDOT =       -3825
723971  meter/sec
 ZDOT =     -19167
848977                 ZDOT =       -5857
781478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19665766
58                 X    =         5994125
65
 Y    =        9679177
00  feet           Y    =         2950213
15  meter
 Z    =        3864551
05                 Z    =         1177915
16
 XDOT =      -3217
132303                 XDOT =        -980
581926
 YDOT =      14298
602710  feet/sec       YDOT =        4358
214106  meter/sec
 ZDOT =     -19236
640797                 ZDOT =       -5863
328115


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   18320
23380042  
00016717  00000-0  10270-3 0  9126
2 25544  51
6400 341
0276 0004784  54
8617 305
2984 15
53971765 22155


Satellite: ISS
Catalog Number: 25544
Epoch time:      18320
23380042   =   yrday
fracday
Element set:     912
Inclination:       51
6400  deg
RA of node:       341
0276  deg
Eccentricity:     
0004784     
Arg of perigee:    54
8617  deg
Mean anomaly:     305
2984  deg
Mean motion:   15
53971765  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              295


Coasting Arc #14 (Orbit 2223)
---------------------------------------

Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4154175
19                 A    =         6779892
70  meter
 Y    =        2411528
10  meter          E    =           
0010345
 Z    =        4776009
24                 I    =           51
48668
 XDOT =      -5624
695400                 Wp   =           92
18964
 YDOT =       4527
234975  meter/sec      RA   =          337
83039  deg
 ZDOT =       2601
185675                 TA   =          332
11413
                                          MA   =          332
16954
                                          Ha   =            222
726  n
mi
                                          Hp   =            213
342

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13629183
68                 X    =         4103700
41
 Y    =        7911837
59  feet           Y    =         2457700
70  meter
 Z    =       15669321
65                 Z    =         4796066
48
 XDOT =     -18453
725066                 XDOT =       -5687
537524
 YDOT =      14853
133120  feet/sec       YDOT =        4463
984323  meter/sec
 ZDOT =       8534
073738                 ZDOT =        2573
709902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7377836
24                 X    =         2248764
49
 Y    =       13823748
67  feet           Y    =         4213478
59  meter
 Z    =       15759155
05                 Z    =         4803390
46
 XDOT =     -22539
652465                 XDOT =       -6870
086071
 YDOT =       2422
683463  feet/sec       YDOT =         738
433920  meter/sec
 ZDOT =       8409
893288                 ZDOT =        2563
335474


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   18320
81257648  
00016717  00000-0  10270-3 0  9136
2 25544  51
6403 338
1482 0005015  52
1111 308
0495 15
54000681 22241


Satellite: ISS
Catalog Number: 25544
Epoch time:      18320
81257648   =   yrday
fracday
Element set:     913
Inclination:       51
6403  deg
RA of node:       338
1482  deg
Eccentricity:     
0005015     
Arg of perigee:    52
1111  deg
Mean anomaly:     308
0495  deg
Mean motion:   15
54000681  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2224
Checksum:              271


Coasting Arc #15 (Orbit 2238)
---------------------------------------

Vector Time (GMT): 2018/321/18:14:08
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2718119
32                 A    =         6777952
37  meter
 Y    =       -3319561
11  meter          E    =           
0019240
 Z    =       -5263926
79                 I    =           51
45036
 XDOT =       6459
965329                 Wp   =           76
27021
 YDOT =      -4027
744384  meter/sec      RA   =          332
82231  deg
 ZDOT =       -793
697963                 TA   =          186
09858
                                          MA   =          186
12204
                                          Ha   =            222
934  n
mi
                                          Hp   =            213
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8917714
32                 X    =        -2655227
27
 Y    =      -10890948
53  feet           Y    =        -3349605
36  meter
 Z    =      -17270101
01                 Z    =        -5276977
92
 XDOT =      21194
111972                 XDOT =        6508
379998
 YDOT =     -13214
384461  feet/sec       YDOT =       -3955
233859  meter/sec
 ZDOT =      -2603
995943                 ZDOT =        -762
199611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2033551
07                 X    =         -619826
37
 Y    =      -13856020
90  feet           Y    =        -4223315
17  meter
 Z    =      -17328304
37                 Z    =        -5281667
17
 XDOT =      23973
488730                 XDOT =        7307
119365
 YDOT =       -431
411315  feet/sec       YDOT =        -131
494169  meter/sec
 ZDOT =      -2461
815468                 ZDOT =        -750
361355


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   18321
77720320  
00016717  00000-0  10270-3 0  9145
2 25544  51
6410 333
3405 0005148  55
1355 305
0281 15
53989743 22391


Satellite: ISS
Catalog Number: 25544
Epoch time:      18321
77720320   =   yrday
fracday
Element set:     914
Inclination:       51
6410  deg
RA of node:       333
3405  deg
Eccentricity:     
0005148     
Arg of perigee:    55
1355  deg
Mean anomaly:     305
0281  deg
Mean motion:   15
53989743  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2239
Checksum:              290


Coasting Arc #16 (Orbit 2248)
---------------------------------------

Vector Time (GMT): 2018/322/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917504
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4615360
76                 A    =         6780307
23  meter
 Y    =       -1641781
11  meter          E    =           
0015943
 Z    =       -4703377
92                 I    =           51
43939
 XDOT =       4730
165210                 Wp   =           67
10432
 YDOT =      -5338
623161  meter/sec      RA   =          329
64038  deg
 ZDOT =      -2779
590458                 TA   =          175
23495
                                          MA   =          175
21975
                                          Ha   =            222
967  n
mi
                                          Hp   =            213
111

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15142259
73                 X    =        -4573811
96
 Y    =       -5386420
95  feet           Y    =        -1693160
98  meter
 Z    =      -15431029
92                 Z    =        -4725697
21
 XDOT =      15518
914730                 XDOT =        4803
013649
 YDOT =     -17515
167851  feet/sec       YDOT =       -5285
319854  meter/sec
 ZDOT =      -9119
391267                 ZDOT =       -2756
435598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15974326
28                 X    =         4868974
65
 Y    =        -151577
50  feet           Y    =          -46200
82  meter
 Z    =      -15531135
46                 Z    =        -4733890
09
 XDOT =      -8563
748599                 XDOT =       -2610
230573
 YDOT =      20661
047840  feet/sec       YDOT =        6297
487382  meter/sec
 ZDOT =      -9014
543319                 ZDOT =       -2747
632804


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   18322
42028382  
00016717  00000-0  10270-3 0  9158
2 25544  51
6409 330
1342 0005055  60
1772 299
9882 15
53974762 22494


Satellite: ISS
Catalog Number: 25544
Epoch time:      18322
42028382   =   yrday
fracday
Element set:     915
Inclination:       51
6409  deg
RA of node:       330
1342  deg
Eccentricity:     
0005055     
Arg of perigee:    60
1772  deg
Mean anomaly:     299
9882  deg
Mean motion:   15
53974762  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2249
Checksum:              316


Coasting Arc #17 (Orbit 2255)
---------------------------------------

Vector Time (GMT): 2018/322/19:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6123894
50                 A    =         6788844
39  meter
 Y    =       -2523988
54  meter          E    =           
0019063
 Z    =        1445714
20                 I    =           51
45726
 XDOT =        690
326007                 Wp   =           60
17821
 YDOT =       5008
394391  meter/sec      RA   =          327
58716  deg
 ZDOT =       5771
826694                 TA   =          315
64335
                                          MA   =          315
79592
                                          Ha   =            222
961  n
mi
                                          Hp   =            213
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20091517
39                 X    =         6144640
65
 Y    =       -8280802
30  feet           Y    =        -2455390
89  meter
 Z    =        4743156
81                 Z    =         1475512
91
 XDOT =       2264
849103                 XDOT =         606
232416
 YDOT =      16431
740129  feet/sec       YDOT =        5015
643920  meter/sec
 ZDOT =      18936
439284                 ZDOT =        5774
975851

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21331901
63                 X    =         6501963
62
 Y    =       -3987299
08  feet           Y    =        -1215328
76  meter
 Z    =        4877469
98                 Z    =         1486652
85
 XDOT =      -1570
230904                 XDOT =        -478
606380
 YDOT =      14966
709447  feet/sec       YDOT =        4561
853039  meter/sec
 ZDOT =      18949
890649                 ZDOT =        5775
926670


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   18322
87044054  
00016717  00000-0  10270-3 0  9162
2 25544  51
6420 327
8922 0005192  58
0045 302
1612 15
53975255 22569


Satellite: ISS
Catalog Number: 25544
Epoch time:      18322
87044054   =   yrday
fracday
Element set:     916
Inclination:       51
6420  deg
RA of node:       327
8922  deg
Eccentricity:     
0005192     
Arg of perigee:    58
0045  deg
Mean anomaly:     302
1612  deg
Mean motion:   15
53975255  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2256
Checksum:              295


Coasting Arc #18 (Orbit 2270)
---------------------------------------

Vector Time (GMT): 2018/323/19:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5907342
75                 A    =         6785917
67  meter
 Y    =        1524070
67  meter          E    =           
0008719
 Z    =       -2980076
83                 I    =           51
41958
 XDOT =       1011
166065                 Wp   =           84
08150
 YDOT =      -5751
172416  meter/sec      RA   =          322
59935  deg
 ZDOT =      -4957
327108                 TA   =          130
07512
                                          MA   =          129
99864
                                          Ha   =            222
951  n
mi
                                          Hp   =            213
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19381045
78                 X    =        -5909470
33
 Y    =        5000231
85  feet           Y    =         1457998
77  meter
 Z    =       -9777154
96                 Z    =        -3008778
46
 XDOT =       3317
473967                 XDOT =        1099
482747
 YDOT =     -18868
675907  feet/sec       YDOT =       -5739
371029  meter/sec
 ZDOT =     -16264
196548                 ZDOT =       -4952
200613

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19911469
66                 X    =        -6069015
95
 Y    =        1271580
35  feet           Y    =          387577
69  meter
 Z    =       -9906385
44                 Z    =        -3019466
28
 XDOT =       7011
599969                 XDOT =        2137
135670
 YDOT =     -16434
813347  feet/sec       YDOT =       -5009
331108  meter/sec
 ZDOT =     -16240
347971                 ZDOT =       -4950
058062


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   18323
83505785  
00016717  00000-0  10270-3 0  9173
2 25544  51
6414 323
0853 0005011  61
9895 298
1764 15
53972715 22716


Satellite: ISS
Catalog Number: 25544
Epoch time:      18323
83505785   =   yrday
fracday
Element set:     917
Inclination:       51
6414  deg
RA of node:       323
0853  deg
Eccentricity:     
0005011     
Arg of perigee:    61
9895  deg
Mean anomaly:     298
1764  deg
Mean motion:   15
53972715  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2271
Checksum:              323
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