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

 
Date: August 17th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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


235/02:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 213 0

238/15:14:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 213 0

242/21:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 213 1

Coasting Arc #1 (Orbit 805)
---------------------------------------

Vector Time (GMT): 2018/229/13:50:05
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4147277
22                 A    =         6785299
75  meter
 Y    =       -4141928
15  meter          E    =           
0017620
 Z    =        3405260
76                 I    =           52
00428
 XDOT =       1937
932430                 Wp   =           83
60553
 YDOT =      -5784
085023  meter/sec      RA   =           71
95285  deg
 ZDOT =      -4652
661232                 TA   =           56
79276
                                          MA   =           56
62394
                                          Ha   =            223
429  n
mi
                                          Hp   =            213
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13606552
56                 X    =        -4117193
64
 Y    =      -13589003
10  feet           Y    =        -4188137
60  meter
 Z    =       11172115
36                 Z    =         3385188
01
 XDOT =       6358
046031                 XDOT =        2025
067649
 YDOT =     -18976
656900  feet/sec       YDOT =       -5761
926599  meter/sec
 ZDOT =     -15264
636588                 ZDOT =       -4643
035762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11799510
64                 X    =         3596490
84
 Y    =       15250068
41  feet           Y    =         4648220
85  meter
 Z    =       11082526
86                 Z    =         3377954
19
 XDOT =      -7757
619181                 XDOT =       -2364
522326
 YDOT =      17117
554401  feet/sec       YDOT =        5217
430581  meter/sec
 ZDOT =     -15220
651976                 ZDOT =       -4639
254722


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   18229
61570960  
00016717  00000-0  10270-3 0  9003
2 25544  51
6373  72
5716 0005431  68
0811 292
0919 15
53850627  8060


Satellite: ISS
Catalog Number: 25544
Epoch time:      18229
61570960   =   yrday
fracday
Element set:     900
Inclination:       51
6373  deg
RA of node:        72
5716  deg
Eccentricity:     
0005431     
Arg of perigee:    68
0811  deg
Mean anomaly:     292
0919  deg
Mean motion:   15
53850627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             806
Checksum:              307


Coasting Arc #2 (Orbit 820)
---------------------------------------

Vector Time (GMT): 2018/230/13:50:05
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3916488
36                 A    =         6788439
95  meter
 Y    =        5154837
97  meter          E    =           
0011804
 Z    =       -2036804
69                 I    =           52
00316
 XDOT =      -2880
771491                 Wp   =           55
41620
 YDOT =       4384
873945  meter/sec      RA   =           67
00141  deg
 ZDOT =       5587
580180                 TA   =          282
19835
                                          MA   =          282
33054
                                          Ha   =            223
508  n
mi
                                          Hp   =            213
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12849371
25                 X    =         3868448
11
 Y    =       16912198
07  feet           Y    =         5198366
23  meter
 Z    =       -6682430
08                 Z    =        -2017896
59
 XDOT =      -9451
350036                 XDOT =       -2956
731583
 YDOT =      14386
069374  feet/sec       YDOT =        4352
234473  meter/sec
 ZDOT =      18331
955972                 ZDOT =        5573
401978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10903170
79                 X    =        -3323286
46
 Y    =      -18258369
66  feet           Y    =        -5565151
07  meter
 Z    =       -6598216
52                 Z    =        -2011136
39
 XDOT =       9803
539684                 XDOT =        2988
118896
 YDOT =     -12420
498845  feet/sec       YDOT =       -3785
768048  meter/sec
 ZDOT =      18267
702529                 ZDOT =        5567
995731


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   18230
58041819  
00016717  00000-0  10270-3 0  9018
2 25544  51
6370  67
7646 0005624  74
0605 286
1167 15
53842621  8218


Satellite: ISS
Catalog Number: 25544
Epoch time:      18230
58041819   =   yrday
fracday
Element set:     901
Inclination:       51
6370  deg
RA of node:        67
7646  deg
Eccentricity:     
0005624     
Arg of perigee:    74
0605  deg
Mean anomaly:     286
1167  deg
Mean motion:   15
53842621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             821
Checksum:              300


Coasting Arc #3 (Orbit 836)
---------------------------------------

Vector Time (GMT): 2018/231/13:50:05
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3462040
56                 A    =         6789960
25  meter
 Y    =       -5819273
21  meter          E    =           
0016572
 Z    =         424098
75                 I    =           51
99503
 XDOT =       3867
052993                 Wp   =          114
35981
 YDOT =      -2752
469328  meter/sec      RA   =           62
05578  deg
 ZDOT =      -6022
342701                 TA   =           61
09004
                                          MA   =           60
92391
                                          Ha   =            223
375  n
mi
                                          Hp   =            213
095

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11358400
80                 X    =        -3398770
57
 Y    =      -19092103
71  feet           Y    =        -5857634
38  meter
 Z    =        1391400
11                 Z    =          407435
15
 XDOT =      12687
181735                 XDOT =        3926
797577
 YDOT =      -9030
411182  feet/sec       YDOT =       -2708
891184  meter/sec
 ZDOT =     -19758
342194                 ZDOT =       -6003
412962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9487875
05                 X    =         2891904
31
 Y    =       20092348
29  feet           Y    =         6124147
76  meter
 Z    =        1317366
35                 Z    =          401533
26
 XDOT =     -12158
581721                 XDOT =       -3705
935709
 YDOT =       7071
711938  feet/sec       YDOT =        2155
457799  meter/sec
 ZDOT =     -19672
965635                 ZDOT =       -5996
319926


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   18231
60943648  
00016717  00000-0  10270-3 0  9024
2 25544  51
6372  62
6368 0005537  75
0301 285
1464 15
53888175  8372


Satellite: ISS
Catalog Number: 25544
Epoch time:      18231
60943648   =   yrday
fracday
Element set:     902
Inclination:       51
6372  deg
RA of node:        62
6368  deg
Eccentricity:     
0005537     
Arg of perigee:    75
0301  deg
Mean anomaly:     285
1464  deg
Mean motion:   15
53888175  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             837
Checksum:              320


Coasting Arc #4 (Orbit 852)
---------------------------------------

Vector Time (GMT): 2018/232/13:50:05
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2824233
57                 A    =         6789497
97  meter
 Y    =        6053251
98  meter          E    =           
0019005
 Z    =        1170884
73                 I    =           51
97808
 XDOT =      -4789
059936                 Wp   =           64
60299
 YDOT =       1081
437954  meter/sec      RA   =           57
11015  deg
 ZDOT =       5894
217260                 TA   =          308
05739
                                          MA   =          308
22873
                                          Ha   =            223
471  n
mi
                                          Hp   =            213
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9265858
18                 X    =         2750647
05
 Y    =       19859750
60  feet           Y    =         6084423
06  meter
 Z    =        3841485
34                 Z    =         1184425
07
 XDOT =     -15712
138896                 XDOT =       -4829
427636
 YDOT =       3548
024785  feet/sec       YDOT =        1027
657601  meter/sec
 ZDOT =      19337
983135                 ZDOT =        5870
855882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7651062
56                 X    =        -2332043
87
 Y    =      -20524686
35  feet           Y    =        -6255924
40  meter
 Z    =        3901451
43                 Z    =         1189162
40
 XDOT =      14573
473877                 XDOT =        4441
994838
 YDOT =      -1735
920510  feet/sec       YDOT =        -529
108572  meter/sec
 ZDOT =      19232
932428                 ZDOT =        5862
197804


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   18232
63845482  
00016717  00000-0  10270-3 0  9036
2 25544  51
6384  57
5090 0005634  81
9078 278
2713 15
53866302  8531


Satellite: ISS
Catalog Number: 25544
Epoch time:      18232
63845482   =   yrday
fracday
Element set:     903
Inclination:       51
6384  deg
RA of node:        57
5090  deg
Eccentricity:     
0005634     
Arg of perigee:    81
9078  deg
Mean anomaly:     278
2713  deg
Mean motion:   15
53866302  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             853
Checksum:              321


Coasting Arc #5 (Orbit 867)
---------------------------------------

Vector Time (GMT): 2018/233/13:50:05
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1911377
30                 A    =         6786940
76  meter
 Y    =       -5922514
29  meter          E    =           
0009968
 Z    =       -2713435
26                 I    =           51
95030
 XDOT =       5596
295203                 Wp   =          101
57565
 YDOT =        568
513521  meter/sec      RA   =           52
15990  deg
 ZDOT =      -5201
052638                 TA   =          108
92427
                                          MA   =          108
81620
                                          Ha   =            223
495  n
mi
                                          Hp   =            212
985

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6270922
89                 X    =        -1831827
79
 Y    =      -19430821
15  feet           Y    =        -5943443
81  meter
 Z    =       -8902346
64                 Z    =        -2722526
80
 XDOT =      18360
548567                 XDOT =        5614
785637
 YDOT =       1865
201841  feet/sec       YDOT =         631
198609  meter/sec
 ZDOT =     -17063
820990                 ZDOT =       -5173
823222

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5006533
45                 X    =         1525991
39
 Y    =       19776302
81  feet           Y    =         6027817
10  meter
 Z    =       -8942344
80                 Z    =        -2725626
69
 XDOT =     -16882
026870                 XDOT =       -5145
641790
 YDOT =      -3360
052068  feet/sec       YDOT =       -1024
143870  meter/sec
 ZDOT =     -16941
630483                 ZDOT =       -5163
808971


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   18233
60315712  
00016717  00000-0  10270-3 0  9043
2 25544  51
6379  52
7020 0005728  84
1883 275
9922 15
53865951  8689


Satellite: ISS
Catalog Number: 25544
Epoch time:      18233
60315712   =   yrday
fracday
Element set:     904
Inclination:       51
6379  deg
RA of node:        52
7020  deg
Eccentricity:     
0005728     
Arg of perigee:    84
1883  deg
Mean anomaly:     275
9922  deg
Mean motion:   15
53865951  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             868
Checksum:              326


Coasting Arc #6 (Orbit 883)
---------------------------------------

Vector Time (GMT): 2018/234/13:50:05
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         820039
97                 A    =         6783412
53  meter
 Y    =        5442975
01  meter          E    =           
0016499
 Z    =        3951636
63                 I    =           51
91780
 XDOT =      -6196
681680                 Wp   =           96
24965
 YDOT =      -2019
453458  meter/sec      RA   =           47
19997  deg
 ZDOT =       4051
292540                 TA   =          311
55860
                                          MA   =          311
69996
                                          Ha   =            223
432  n
mi
                                          Hp   =            213
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2690419
86                 X    =          739919
51
 Y    =       17857529
55  feet           Y    =         5451697
26  meter
 Z    =       12964687
11                 Z    =         3955425
47
 XDOT =     -20330
320473                 XDOT =       -6193
317778
 YDOT =      -6625
503471  feet/sec       YDOT =       -2088
730254  meter/sec
 ZDOT =      13291
642193                 ZDOT =        4021
199845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1811677
13                 X    =         -552199
19
 Y    =      -17956224
47  feet           Y    =        -5473057
22  meter
 Z    =       12980934
53                 Z    =         3956588
84
 XDOT =      18795
732271                 XDOT =        5728
939196
 YDOT =       7653
391450  feet/sec       YDOT =        2332
753714  meter/sec
 ZDOT =      13156
801065                 ZDOT =        4010
192965


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   18234
63217091  
00016717  00000-0  10270-3 0  9059
2 25544  51
6383  47
5744 0005563  89
4175 270
7615 15
53877890  8843


Satellite: ISS
Catalog Number: 25544
Epoch time:      18234
63217091   =   yrday
fracday
Element set:     905
Inclination:       51
6383  deg
RA of node:        47
5744  deg
Eccentricity:     
0005563     
Arg of perigee:    89
4175  deg
Mean anomaly:     270
7615  deg
Mean motion:   15
53877890  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             884
Checksum:              336


Coasting Arc #7 (Orbit 891)
---------------------------------------

Vector Time (GMT): 2018/235/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -857225
64                 A    =         6779748
06  meter
 Y    =        4575741
27  meter          E    =           
0011485
 Z    =        4920299
60                 I    =           51
89437
 XDOT =      -6320
718428                 Wp   =          105
22424
 YDOT =      -3684
522475  meter/sec      RA   =           44
62558  deg
 ZDOT =       2317
857216                 TA   =          322
16508
                                          MA   =          322
24575
                                          Ha   =            223
417  n
mi
                                          Hp   =            213
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2812420
07                 X    =         -932228
95
 Y    =       15012274
52  feet           Y    =         4565735
81  meter
 Z    =       16142715
22                 Z    =         4915953
40
 XDOT =     -20737
265183                 XDOT =       -6290
306051
 YDOT =     -12088
328331  feet/sec       YDOT =       -3755
035078  meter/sec
 ZDOT =       7604
518425                 ZDOT =        2287
227742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1744775
02                 X    =         -531807
43
 Y    =       15194879
48  feet           Y    =         4631399
27  meter
 Z    =       16122553
93                 Z    =         4914154
44
 XDOT =     -20555
283980                 XDOT =       -6265
250557
 YDOT =     -10309
618905  feet/sec       YDOT =       -3142
371842  meter/sec
 ZDOT =       7467
504467                 ZDOT =        2276
095361


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   18235
14667665  
00016717  00000-0  10270-3 0  9063
2 25544  51
6387  45
0150 0005472  86
1333 274
0445 15
53893201  8921


Satellite: ISS
Catalog Number: 25544
Epoch time:      18235
14667665   =   yrday
fracday
Element set:     906
Inclination:       51
6387  deg
RA of node:        45
0150  deg
Eccentricity:     
0005472     
Arg of perigee:    86
1333  deg
Mean anomaly:     274
0445  deg
Mean motion:   15
53893201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             892
Checksum:              308


Coasting Arc #8 (Orbit 906)
---------------------------------------

Vector Time (GMT): 2018/236/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2214351
72                 A    =         6778244
51  meter
 Y    =       -3591782
02  meter          E    =           
0020344
 Z    =       -5322350
72                 I    =           51
86483
 XDOT =       6131
339043                 Wp   =           86
44662
 YDOT =       4550
084702  meter/sec      RA   =           39
64527  deg
 ZDOT =       -520
176610                 TA   =          178
59878
                                          MA   =          178
59307
                                          Ha   =            223
480  n
mi
                                          Hp   =            213
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7264933
46                 X    =         2280204
14
 Y    =      -11784061
75  feet           Y    =        -3566651
48  meter
 Z    =      -17461780
57                 Z    =        -5311434
38
 XDOT =      20115
941741                 XDOT =        6082
529744
 YDOT =      14928
099415  feet/sec       YDOT =        4618
376663  meter/sec
 ZDOT =      -1706
616173                 ZDOT =        -490
511849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6230264
02                 X    =         1898984
47
 Y    =      -12431987
58  feet           Y    =        -3789269
81  meter
 Z    =      -17412255
62                 Z    =        -5307255
51
 XDOT =      20544
822705                 XDOT =        6262
061960
 YDOT =      12498
385498  feet/sec       YDOT =        3809
507900  meter/sec
 ZDOT =      -1574
063369                 ZDOT =        -479
774515


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   18236
11137547  
00016717  00000-0  10270-3 0  9073
2 25544  51
6390  40
2067 0005595  88
3100 271
8693 15
53851781  9075


Satellite: ISS
Catalog Number: 25544
Epoch time:      18236
11137547   =   yrday
fracday
Element set:     907
Inclination:       51
6390  deg
RA of node:        40
2067  deg
Eccentricity:     
0005595     
Arg of perigee:    88
3100  deg
Mean anomaly:     271
8693  deg
Mean motion:   15
53851781  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             907
Checksum:              312


Coasting Arc #9 (Orbit 922)
---------------------------------------

Vector Time (GMT): 2018/237/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3543815
81                 A    =         6778742
41  meter
 Y    =        2513425
59  meter          E    =           
0009553
 Z    =        5195919
08                 I    =           51
84023
 XDOT =      -5569
175571                 Wp   =           75
13490
 YDOT =      -5112
849784  meter/sec      RA   =           34
66378  deg
 ZDOT =      -1320
734718                 TA   =           27
53257
                                          MA   =           27
48200
                                          Ha   =            223
626  n
mi
                                          Hp   =            213
020

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11626692
30                 X    =        -3596896
81
 Y    =        8246146
93  feet           Y    =         2473499
55  meter
 Z    =       17046978
62                 Z    =         5178575
78
 XDOT =     -18271
573396                 XDOT =       -5505
173049
 YDOT =     -16774
441547  feet/sec       YDOT =       -5174
770341  meter/sec
 ZDOT =      -4333
119153                 ZDOT =       -1347
631726

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10742960
32                 X    =        -3274454
31
 Y    =        9509399
45  feet           Y    =         2898464
95  meter
 Z    =       16968751
25                 Z    =         5172075
38
 XDOT =     -19311
634679                 XDOT =       -5886
186250
 YDOT =     -13844
486069  feet/sec       YDOT =       -4219
799354  meter/sec
 ZDOT =      -4453
157071                 ZDOT =       -1357
322275


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   18237
14038509  
00016717  00000-0  10270-3 0  9086
2 25544  51
6389  35
0798 0005661  91
2999 268
8802 15
53857577  9234


Satellite: ISS
Catalog Number: 25544
Epoch time:      18237
14038509   =   yrday
fracday
Element set:     908
Inclination:       51
6389  deg
RA of node:        35
0798  deg
Eccentricity:     
0005661     
Arg of perigee:    91
2999  deg
Mean anomaly:     268
8802  deg
Mean motion:   15
53857577  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             923
Checksum:              354


Coasting Arc #10 (Orbit 937)
---------------------------------------

Vector Time (GMT): 2018/238/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4761626
10                 A    =         6781237
59  meter
 Y    =       -1463706
39  meter          E    =           
0015466
 Z    =       -4615912
21                 I    =           51
82093
 XDOT =       4571
014569                 Wp   =          104
40314
 YDOT =       5343
916928  meter/sec      RA   =           29
68362  deg
 ZDOT =       3025
491406                 TA   =          195
75544
                                          MA   =          195
80361
                                          Ha   =            223
463  n
mi
                                          Hp   =            213
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15622132
88                 X    =         4800061
04
 Y    =       -4802186
31  feet           Y    =        -1410243
91  meter
 Z    =      -15144068
93                 Z    =        -4592688
88
 XDOT =      14996
766959                 XDOT =        4496
221708
 YDOT =      17532
535852  feet/sec       YDOT =        5394
615132  meter/sec
 ZDOT =       9926
152907                 ZDOT =        3047
513495

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14971486
75                 X    =         4563309
16
 Y    =       -6791170
16  feet           Y    =        -2069948
67  meter
 Z    =      -15039595
91                 Z    =        -4584068
83
 XDOT =      16572
123749                 XDOT =        5051
183319
 YDOT =      14369
221737  feet/sec       YDOT =        4379
738785  meter/sec
 ZDOT =      10024
262849                 ZDOT =        3055
395316


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   18238
10507997  
00016717  00000-0  10270-3 0  9096
2 25544  51
6391  30
2726 0005552  95
2165 264
9622 15
53856992  9386


Satellite: ISS
Catalog Number: 25544
Epoch time:      18238
10507997   =   yrday
fracday
Element set:     909
Inclination:       51
6391  deg
RA of node:        30
2726  deg
Eccentricity:     
0005552     
Arg of perigee:    95
2165  deg
Mean anomaly:     264
9622  deg
Mean motion:   15
53856992  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             938
Checksum:              336


Coasting Arc #11 (Orbit 946)
---------------------------------------

Vector Time (GMT): 2018/238/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1521818
57                 A    =         6778020
31  meter
 Y    =        3916480
08  meter          E    =           
0008061
 Z    =        5311851
24                 I    =           51
79767
 XDOT =      -6957
996766                 Wp   =          102
76078
 YDOT =      -3216
210715  meter/sec      RA   =           27
01846  deg
 ZDOT =        375
694732                 TA   =          343
65469
                                          MA   =          343
68067
                                          Ha   =            223
401  n
mi
                                          Hp   =            213
034

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4992843
07                 X    =        -1591302
37
 Y    =       12849344
10  feet           Y    =         3899073
85  meter
 Z    =       17427333
47                 Z    =         5304289
91
 XDOT =     -22828
073379                 XDOT =       -6923
339975
 YDOT =     -10551
872424  feet/sec       YDOT =       -3293
826054  meter/sec
 ZDOT =       1232
594264                 ZDOT =         341
980130

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -214714
52                 X    =          -65444
99
 Y    =      -13827128
43  feet           Y    =        -4214508
74  meter
 Z    =       17392828
83                 Z    =         5301334
23
 XDOT =      24128
392445                 XDOT =        7354
334017
 YDOT =        995
129728  feet/sec       YDOT =         303
315541  meter/sec
 ZDOT =       1081
691923                 ZDOT =         329
699698


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   18238
68389378  
00016717  00000-0  10270-3 0  9102
2 25544  51
6416  27
3850 0005500 102
5327 257
6442 15
53907541  9470


Satellite: ISS
Catalog Number: 25544
Epoch time:      18238
68389378   =   yrday
fracday
Element set:     910
Inclination:       51
6416  deg
RA of node:        27
3850  deg
Eccentricity:     
0005500     
Arg of perigee:   102
5327  deg
Mean anomaly:     257
6442  deg
Mean motion:   15
53907541  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             947
Checksum:              316


Coasting Arc #12 (Orbit 961)
---------------------------------------

Vector Time (GMT): 2018/239/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3057810
22                 A    =         6778800
88  meter
 Y    =       -3160979
70  meter          E    =           
0019304
 Z    =       -5175672
61                 I    =           51
77017
 XDOT =       6450
744816                 Wp   =          101
74845
 YDOT =       3851
147106  meter/sec      RA   =           22
03239  deg
 ZDOT =       1459
866521                 TA   =          182
30042
                                          MA   =          182
30931
                                          Ha   =            223
398  n
mi
                                          Hp   =            213
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10032185
77                 X    =         3118070
25
 Y    =      -10370668
32  feet           Y    =        -3126448
59  meter
 Z    =      -16980553
17                 Z    =        -5160672
45
 XDOT =      21163
860945                 XDOT =        6400
109631
 YDOT =      12634
997068  feet/sec       YDOT =        3923
000790  meter/sec
 ZDOT =       4789
588324                 ZDOT =        1491
078296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5154664
52                 X    =        -1571141
74
 Y    =       13561803
57  feet           Y    =         4133637
73  meter
 Z    =      -16912764
89                 Z    =        -5155010
74
 XDOT =     -23431
318158                 XDOT =       -7141
865775
 YDOT =      -2762
053928  feet/sec       YDOT =        -841
874037  meter/sec
 ZDOT =       4929
152060                 ZDOT =        1502
405548


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   18239
64858586  
00016717  00000-0  10270-3 0  9112
2 25544  51
6418  22
5789 0005611 104
1611 256
0165 15
53890675  9628


Satellite: ISS
Catalog Number: 25544
Epoch time:      18239
64858586   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:        22
5789  deg
Eccentricity:     
0005611     
Arg of perigee:   104
1611  deg
Mean anomaly:     256
0165  deg
Mean motion:   15
53890675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             962
Checksum:              324


Coasting Arc #13 (Orbit 977)
---------------------------------------

Vector Time (GMT): 2018/240/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4456627
42                 A    =         6781450
72  meter
 Y    =        2362332
82  meter          E    =           
0013760
 Z    =        4521930
73                 I    =           51
74782
 XDOT =      -5507
805175                 Wp   =           82
56942
 YDOT =      -4303
192054  meter/sec      RA   =           17
04782  deg
 ZDOT =      -3170
212390                 TA   =           39
21593
                                          MA   =           39
11632
                                          Ha   =            223
503  n
mi
                                          Hp   =            213
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14621481
04                 X    =        -4504677
38
 Y    =        7750435
78  feet           Y    =         2312227
43  meter
 Z    =       14835730
74                 Z    =         4500165
31
 XDOT =     -18070
226951                 XDOT =       -5443
877281
 YDOT =     -14118
084168  feet/sec       YDOT =       -4364
426963  meter/sec
 ZDOT =     -10400
959286                 ZDOT =       -3196
811494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10170644
64                 X    =         3100012
48
 Y    =      -13164885
31  feet           Y    =        -4012657
04  meter
 Z    =       14737694
92                 Z    =         4492049
41
 XDOT =      21278
731392                 XDOT =        6485
757328
 YDOT =       4625
588814  feet/sec       YDOT =        1409
879471  meter/sec
 ZDOT =     -10519
740386                 ZDOT =       -3206
416870


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   18240
67758830  
00016717  00000-0  10270-3 0  9129
2 25544  51
6417  17
4514 0005591 107
5090 252
6674 15
53888968  9787


Satellite: ISS
Catalog Number: 25544
Epoch time:      18240
67758830   =   yrday
fracday
Element set:     912
Inclination:       51
6417  deg
RA of node:        17
4514  deg
Eccentricity:     
0005591     
Arg of perigee:   107
5090  deg
Mean anomaly:     252
6674  deg
Mean motion:   15
53888968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             978
Checksum:              340


Coasting Arc #14 (Orbit 992)
---------------------------------------

Vector Time (GMT): 2018/241/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5605674
00                 A    =         6785035
12  meter
 Y    =       -1608017
76  meter          E    =           
0010249
 Z    =       -3478807
81                 I    =           51
72748
 XDOT =       4131
439433                 Wp   =          101
61008
 YDOT =       4561
196304  meter/sec      RA   =           12
07040  deg
 ZDOT =       4558
345047                 TA   =          217
65555
                                          MA   =          217
72734
                                          Ha   =            223
351  n
mi
                                          Hp   =            213
250

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18391318
91                 X    =         5640136
79
 Y    =       -5275648
82  feet           Y    =        -1545138
83  meter
 Z    =      -11413411
46                 Z    =        -3451493
73
 XDOT =      13554
591316                 XDOT =        4057
985923
 YDOT =      14964
554804  feet/sec       YDOT =        4606
986603  meter/sec
 ZDOT =      14955
200285                 ZDOT =        4578
235225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14390502
13                 X    =        -4386225
05
 Y    =       12719084
30  feet           Y    =         3876776
89  meter
 Z    =      -11290588
38                 Z    =        -3441371
34
 XDOT =     -17663
090292                 XDOT =       -5383
709921
 YDOT =      -6657
549216  feet/sec       YDOT =       -2029
221001  meter/sec
 ZDOT =      15043
820713                 ZDOT =        4585
356553


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   18241
64227616  
00016717  00000-0  10270-3 0  9131
2 25544  51
6414  12
6453 0005492 111
8828 248
2909 15
53880377  9935


Satellite: ISS
Catalog Number: 25544
Epoch time:      18241
64227616   =   yrday
fracday
Element set:     913
Inclination:       51
6414  deg
RA of node:        12
6453  deg
Eccentricity:     
0005492     
Arg of perigee:   111
8828  deg
Mean anomaly:     248
2909  deg
Mean motion:   15
53880377  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             993
Checksum:              320


Coasting Arc #15 (Orbit 1008)
---------------------------------------

Vector Time (GMT): 2018/242/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6401708
99                 A    =         6788307
16  meter
 Y    =         844897
34  meter          E    =           
0019492
 Z    =        2063888
91                 I    =           51
70615
 XDOT =      -2422
171723                 Wp   =          111
56031
 YDOT =      -4715
685227  meter/sec      RA   =            7
09929  deg
 ZDOT =      -5547
492111                 TA   =           45
61492
                                          MA   =           45
45546
                                          Ha   =            223
384  n
mi
                                          Hp   =            213
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21002982
24                 X    =        -6420706
33
 Y    =        2771972
90  feet           Y    =          773202
94  meter
 Z    =        6771289
09                 Z    =         2032745
51
 XDOT =      -7946
757623                 XDOT =       -2342
312882
 YDOT =     -15471
408225  feet/sec       YDOT =       -4742
325553  meter/sec
 ZDOT =     -18200
433435                 ZDOT =       -5559
063811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17596708
01                 X    =         5363476
60
 Y    =      -11876019
53  feet           Y    =        -3619810
75  meter
 Z    =        6631401
03                 Z    =         2021251
03
 XDOT =      13043
410376                 XDOT =        3975
631483
 YDOT =       9069
362016  feet/sec       YDOT =        2764
341543  meter/sec
 ZDOT =     -18251
689848                 ZDOT =       -5563
115066


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   18242
67127385  
00016717  00000-0  10270-3 0  9148
2 25544  51
6416   7
5178 0005559 113
7755 246
3981 15
53886047 10096


Satellite: ISS
Catalog Number: 25544
Epoch time:      18242
67127385   =   yrday
fracday
Element set:     914
Inclination:       51
6416  deg
RA of node:         7
5178  deg
Eccentricity:     
0005559     
Arg of perigee:   113
7755  deg
Mean anomaly:     246
3981  deg
Mean motion:   15
53886047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1009
Checksum:              328


Coasting Arc #16 (Orbit 1012)
---------------------------------------

Vector Time (GMT): 2018/242/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -491179
20                 A    =         6778301
56  meter
 Y    =       -4245128
33  meter          E    =           
0019738
 Z    =       -5278485
85                 I    =           51
66086
 XDOT =       7609
581432                 Wp   =           91
05609
 YDOT =        122
665364  meter/sec      RA   =            5
75029  deg
 ZDOT =       -809
722467                 TA   =          171
20926
                                          MA   =          171
17464
                                          Ha   =            223
394  n
mi
                                          Hp   =            213
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1611480
31                 X    =         -418032
43
 Y    =      -13927586
39  feet           Y    =        -4250212
45  meter
 Z    =      -17317866
96                 Z    =        -5280693
84
 XDOT =      24965
818345                 XDOT =        7611
577393
 YDOT =        402
445421  feet/sec       YDOT =         207
772074  meter/sec
 ZDOT =      -2656
569772                 ZDOT =        -772
752986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10363095
89                 X    =         3158671
63
 Y    =       -9426482
00  feet           Y    =        -2873191
71  meter
 Z    =      -17327167
34                 Z    =        -5281320
61
 XDOT =      13728
261151                 XDOT =        4184
373999
 YDOT =      19652
567741  feet/sec       YDOT =        5990
102647  meter/sec
 ZDOT =      -2490
677930                 ZDOT =        -759
158633


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   18242
92852333  
00016717  00000-0  10270-3 0  9155
2 25544  51
6389   6
2368 0005611 111
1609 249
0144 15
53871018 10139


Satellite: ISS
Catalog Number: 25544
Epoch time:      18242
92852333   =   yrday
fracday
Element set:     915
Inclination:       51
6389  deg
RA of node:         6
2368  deg
Eccentricity:     
0005611     
Arg of perigee:   111
1609  deg
Mean anomaly:     249
0144  deg
Mean motion:   15
53871018  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1013
Checksum:              288


Coasting Arc #17 (Orbit 1028)
---------------------------------------

Vector Time (GMT): 2018/243/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1221410
36                 A    =         6778458
01  meter
 Y    =        4125861
54  meter          E    =           
0008168
 Z    =        5230562
30                 I    =           51
62769
 XDOT =      -7548
504886                 Wp   =           91
06529
 YDOT =       -919
707466  meter/sec      RA   =             
75407  deg
 ZDOT =      -1035
969921                 TA   =            8
85645
                                          MA   =            8
84205
                                          Ha   =            223
358  n
mi
                                          Hp   =            213
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4007251
84                 X    =        -1292863
45
 Y    =       13536291
13  feet           Y    =         4111803
69  meter
 Z    =       17160637
48                 Z    =         5224455
30
 XDOT =     -24765
435977                 XDOT =       -7532
627242
 YDOT =      -3017
412946  feet/sec       YDOT =       -1004
031366  meter/sec
 ZDOT =      -3398
851447                 ZDOT =       -1072
599350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13279500
67                 X    =        -4047591
80
 Y    =        4889194
05  feet           Y    =         1490226
35  meter
 Z    =       17132640
40                 Z    =         5222028
79
 XDOT =     -12177
960673                 XDOT =       -3711
842413
 YDOT =     -20576
360821  feet/sec       YDOT =       -6271
674778  meter/sec
 ZDOT =      -3563
088544                 ZDOT =       -1086
029388


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   18243
95751821  
00016717  00000-0  10270-3 0  9160
2 25544  51
6381   1
1096 0005495 114
7648 245
4077 15
53879292 10299


Satellite: ISS
Catalog Number: 25544
Epoch time:      18243
95751821   =   yrday
fracday
Element set:     916
Inclination:       51
6381  deg
RA of node:         1
1096  deg
Eccentricity:     
0005495     
Arg of perigee:   114
7648  deg
Mean anomaly:     245
4077  deg
Mean motion:   15
53879292  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1029
Checksum:              323
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