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

 
Date: December 3rd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 25144 4947 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


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

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

338/18:38:53 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 1

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

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

348/03:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 6

Coasting Arc #1 (Orbit 2487)
---------------------------------------

Vector Time (GMT): 2018/337/18:47:57
545
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3981248
75                 A    =         6785659
98  meter
 Y    =       -4596833
21  meter          E    =           
0009210
 Z    =       -3019215
91                 I    =           51
27801
 XDOT =       2451
087787                 Wp   =           92
84098
 YDOT =      -5341
428593  meter/sec      RA   =          252
56224  deg
 ZDOT =       4912
944681                 TA   =          232
41035
                                          MA   =          232
49401
                                          Ha   =            222
986  n
mi
                                          Hp   =            212
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13061839
72                 X    =        -3914883
78
 Y    =      -15081473
78  feet           Y    =        -4640983
08  meter
 Z    =       -9905564
01                 Z    =        -3038394
79
 XDOT =       8041
626598                 XDOT =        2486
770078
 YDOT =     -17524
372024  feet/sec       YDOT =       -5313
819552  meter/sec
 ZDOT =      16118
584913                 ZDOT =        4924
937822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11249244
51                 X    =        -3428769
73
 Y    =      -16425946
72  feet           Y    =        -5006628
56  meter
 Z    =       -9991270
15                 Z    =        -3045339
14
 XDOT =       8624
074623                 XDOT =        2628
617945
 YDOT =     -15718
766825  feet/sec       YDOT =       -4791
080128  meter/sec
 ZDOT =      16173
124645                 ZDOT =        4929
568392


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18337
78954911  
00016717  00000-0  10270-3 0  9003
2 25544  51
6369 253
5258 0005252 110
7148 249
4568 15
54038067 24887


Satellite: ISS
Catalog Number: 25544
Epoch time:      18337
78954911   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:       253
5258  deg
Eccentricity:     
0005252     
Arg of perigee:   110
7148  deg
Mean anomaly:     249
4568  deg
Mean motion:   15
54038067  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2488
Checksum:              334


Coasting Arc #2 (Orbit 2488)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4430218
96                 A    =         6782366
34  meter
 Y    =        3057714
47  meter          E    =           
0014989
 Z    =        4113382
43                 I    =           51
26674
 XDOT =      -1064
226931                 Wp   =           87
90187
 YDOT =       6608
873757  meter/sec      RA   =          252
41456  deg
 ZDOT =      -3754
144626                 TA   =           40
98791
                                          MA   =           40
87535
                                          Ha   =            222
925  n
mi
                                          Hp   =            213
001

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14534839
12                 X    =         4375716
51
 Y    =       10031871
64  feet           Y    =         3106951
32  meter
 Z    =       13495349
18                 Z    =         4134771
02
 XDOT =      -3491
558174                 XDOT =       -1119
814155
 YDOT =      21682
656684  feet/sec       YDOT =        6596
662208  meter/sec
 ZDOT =     -12316
747462                 ZDOT =       -3759
449048

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15139708
25                 X    =         4614583
08
 Y    =        8949515
24  feet           Y    =         2727812
25  meter
 Z    =       13591168
35                 Z    =         4142588
11
 XDOT =      -1161
823787                 XDOT =        -354
123890
 YDOT =      20769
027862  feet/sec       YDOT =        6330
399692  meter/sec
 ZDOT =     -12341
357967                 ZDOT =       -3761
645908


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18337
85385544  
00016717  00000-0  10270-3 0  9012
2 25544  51
6366 253
2048 0005281 111
8010 248
3705 15
54015814 24897


Satellite: ISS
Catalog Number: 25544
Epoch time:      18337
85385544   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       253
2048  deg
Eccentricity:     
0005281     
Arg of perigee:   111
8010  deg
Mean anomaly:     248
3705  deg
Mean motion:   15
54015814  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2489
Checksum:              303


Coasting Arc #3 (Orbit 2501)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3328826
66                 A    =         6778110
99  meter
 Y    =        2862836
03  meter          E    =           
0018437
 Z    =       -5180034
84                 I    =           51
26516
 XDOT =      -3715
779543                 Wp   =           88
11363
 YDOT =      -6574
714453  meter/sec      RA   =          248
15032  deg
 ZDOT =      -1249
044580                 TA   =          169
83050
                                          MA   =          169
79315
                                          Ha   =            222
846  n
mi
                                          Hp   =            212
936

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10921347
32                 X    =        -3335429
97
 Y    =        9392506
67  feet           Y    =         2825574
19  meter
 Z    =      -16994864
97                 Z    =        -5196221
27
 XDOT =     -12190
877765                 XDOT =       -3635
915775
 YDOT =     -21570
585476  feet/sec       YDOT =       -6615
820256  meter/sec
 ZDOT =      -4097
915289                 ZDOT =       -1266
901314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14269415
44                 X    =        -4349317
82
 Y    =       -1178327
33  feet           Y    =         -359154
17  meter
 Z    =      -17067975
04                 Z    =        -5202318
79
 XDOT =       6860
867270                 XDOT =        2091
192344
 YDOT =     -22729
006760  feet/sec       YDOT =       -6927
801261  meter/sec
 ZDOT =      -4177
461854                 ZDOT =       -1273
290373


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18338
68982733  
00016717  00000-0  10270-3 0  9028
2 25544  51
6397 249
0414 0004903 110
4770 249
6909 15
54054624 25027


Satellite: ISS
Catalog Number: 25544
Epoch time:      18338
68982733   =   yrday
fracday
Element set:     902
Inclination:       51
6397  deg
RA of node:       249
0414  deg
Eccentricity:     
0004903     
Arg of perigee:   110
4770  deg
Mean anomaly:     249
6909  deg
Mean motion:   15
54054624  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2502
Checksum:              319


Coasting Arc #4 (Orbit 2503)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4674457
80                 A    =         6782239
43  meter
 Y    =        2630011
33  meter          E    =           
0014644
 Z    =        4138649
87                 I    =           51
27790
 XDOT =       -463
853166                 Wp   =           88
20230
 YDOT =       6696
971937  meter/sec      RA   =          247
58331  deg
 ZDOT =      -3719
980914                 TA   =           40
25999
                                          MA   =           40
15163
                                          Ha   =            222
834  n
mi
                                          Hp   =            213
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15336147
65                 X    =         4624597
13
 Y    =        8628646
10  feet           Y    =         2682005
30  meter
 Z    =       13578247
60                 Z    =         4161236
24
 XDOT =      -1521
827971                 XDOT =        -520
636082
 YDOT =      21971
692706  feet/sec       YDOT =        6691
467564  meter/sec
 ZDOT =     -12204
661790                 ZDOT =       -3722
371662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13963768
44                 X    =         4256156
62
 Y    =       10578463
73  feet           Y    =         3224315
74  meter
 Z    =       13679511
77                 Z    =         4169515
19
 XDOT =      -3575
031491                 XDOT =       -1089
669598
 YDOT =      20566
432731  feet/sec       YDOT =        6268
648696  meter/sec
 ZDOT =     -12216
173430                 ZDOT =       -3723
489662


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18338
81843956  
00016717  00000-0  10270-3 0  9037
2 25544  51
6375 248
3972 0005137 114
3353 245
8337 15
54026647 25043


Satellite: ISS
Catalog Number: 25544
Epoch time:      18338
81843956   =   yrday
fracday
Element set:     903
Inclination:       51
6375  deg
RA of node:       248
3972  deg
Eccentricity:     
0005137     
Arg of perigee:   114
3353  deg
Mean anomaly:     245
8337  deg
Mean motion:   15
54026647  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2504
Checksum:              324


Coasting Arc #5 (Orbit 2518)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4685059
67                 A    =         6785868
06  meter
 Y    =       -3953984
64  meter          E    =           
0009010
 Z    =       -2918083
82                 I    =           51
30437
 XDOT =       1609
174386                 Wp   =           94
52670
 YDOT =      -5581
994694  meter/sec      RA   =          242
57589  deg
 ZDOT =       4992
666948                 TA   =          232
06032
                                          MA   =          232
14178
                                          Ha   =            222
974  n
mi
                                          Hp   =            212
911

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15370930
68                 X    =        -4626322
15
 Y    =      -12972390
57  feet           Y    =        -4006047
56  meter
 Z    =       -9573765
82                 Z    =        -2940700
29
 XDOT =       5279
443522                 XDOT =        1647
222059
 YDOT =     -18313
630886  feet/sec       YDOT =       -5563
787487  meter/sec
 ZDOT =      16380
140907                 ZDOT =        5000
575818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13701845
48                 X    =        -4176322
50
 Y    =      -14658058
15  feet           Y    =        -4467776
12  meter
 Z    =       -9675028
74                 Z    =        -2948948
76
 XDOT =       6186
672336                 XDOT =        1885
697728
 YDOT =     -16591
510234  feet/sec       YDOT =       -5057
092319  meter/sec
 ZDOT =      16416
335161                 ZDOT =        5003
698957


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18339
78302215  
00016717  00000-0  10270-3 0  9043
2 25544  51
6379 243
5892 0005392 117
2838 242
8864 15
54050543 25198


Satellite: ISS
Catalog Number: 25544
Epoch time:      18339
78302215   =   yrday
fracday
Element set:     904
Inclination:       51
6379  deg
RA of node:       243
5892  deg
Eccentricity:     
0005392     
Arg of perigee:   117
2838  deg
Mean anomaly:     242
8864  deg
Mean motion:   15
54050543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2519
Checksum:              325


Coasting Arc #6 (Orbit 2529)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3399945
74                 A    =         6789598
02  meter
 Y    =        5867750
45  meter          E    =           
0016869
 Z    =        -106116
04                 I    =           51
32983
 XDOT =      -4189
192682                 Wp   =          129
80138
 YDOT =       2330
726605  meter/sec      RA   =          239
19323  deg
 ZDOT =      -5987
484950                 TA   =           51
34686
                                          MA   =           51
19601
                                          Ha   =            222
918  n
mi
                                          Hp   =            213
077

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11154677
64                 X    =         3334593
69
 Y    =       19251149
76  feet           Y    =         5905405
61  meter
 Z    =        -348149
73                 Z    =          -89758
16
 XDOT =     -13744
070478                 XDOT =       -4185
859666
 YDOT =       7646
740829  feet/sec       YDOT =        2283
899382  meter/sec
 ZDOT =     -19643
979495                 ZDOT =       -6007
826589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22249136
07                 X    =        -6781536
67
 Y    =        -234514
66  feet           Y    =          -71480
07  meter
 Z    =        -275237
14                 Z    =          -83892
28
 XDOT =        358
439345                 XDOT =         109
252313
 YDOT =     -13985
841820  feet/sec       YDOT =       -4262
884587  meter/sec
 ZDOT =     -19735
723634                 ZDOT =       -6015
448564


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18340
49038195  
00016717  00000-0  10270-3 0  9057
2 25544  51
6404 240
0680 0005115 116
4823 243
6855 15
54035580 25308


Satellite: ISS
Catalog Number: 25544
Epoch time:      18340
49038195   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:       240
0680  deg
Eccentricity:     
0005115     
Arg of perigee:   116
4823  deg
Mean anomaly:     243
6855  deg
Mean motion:   15
54035580  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2530
Checksum:              289


Coasting Arc #7 (Orbit 2545)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2619009
36                 A    =         6788326
35  meter
 Y    =       -6009728
69  meter          E    =           
0017326
 Z    =        1738975
70                 I    =           51
34315
 XDOT =       5147
720349                 Wp   =           78
63606
 YDOT =       -594
344353  meter/sec      RA   =          234
20197  deg
 ZDOT =       5654
201354                 TA   =          300
53173
                                          MA   =          300
70263
                                          Ha   =            222
860  n
mi
                                          Hp   =            213
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8592550
40                 X    =        -2560059
38
 Y    =      -19716957
63  feet           Y    =        -6038686
86  meter
 Z    =        5705300
86                 Z    =         1726395
77
 XDOT =      16888
846290                 XDOT =        5126
518403
 YDOT =      -1949
948664  feet/sec       YDOT =        -536
898178  meter/sec
 ZDOT =      18550
529375                 ZDOT =        5679
155955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21401919
53                 X    =         6523305
07
 Y    =        2276650
53  feet           Y    =          693923
08  meter
 Z    =        5649380
62                 Z    =         1721931
21
 XDOT =      -6450
992278                 XDOT =       -1966
262446
 YDOT =      13965
815871  feet/sec       YDOT =        4256
780678  meter/sec
 ZDOT =      18662
838663                 ZDOT =        5688
433224


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18341
51926661  
00016717  00000-0  10270-3 0  9066
2 25544  51
6400 234
9401 0005024 119
8094 240
3559 15
54042750 25462


Satellite: ISS
Catalog Number: 25544
Epoch time:      18341
51926661   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       234
9401  deg
Eccentricity:     
0005024     
Arg of perigee:   119
8094  deg
Mean anomaly:     240
3559  deg
Mean motion:   15
54042750  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2546
Checksum:              292


Coasting Arc #8 (Orbit 2560)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1537350
69                 A    =         6785087
98  meter
 Y    =        5757160
76  meter          E    =           
0009327
 Z    =       -3248506
63                 I    =           51
35379
 XDOT =      -5929
358066                 Wp   =          111
71025
 YDOT =      -1078
823212  meter/sec      RA   =          229
20576  deg
 ZDOT =      -4732
352635                 TA   =          106
08579
                                          MA   =          105
98307
                                          Ha   =            222
779  n
mi
                                          Hp   =            213
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5043801
48                 X    =         1488637
92
 Y    =       18888322
70  feet           Y    =         5774080
52  meter
 Z    =      -10657830
17                 Z    =        -3241156
24
 XDOT =     -19453
274494                 XDOT =       -5893
866198
 YDOT =      -3539
446234  feet/sec       YDOT =       -1144
930367  meter/sec
 ZDOT =     -15526
091321                 ZDOT =       -4761
069601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19021207
14                 X    =        -5797663
94
 Y    =       -4592683
67  feet           Y    =        -1399849
98  meter
 Z    =      -10625391
63                 Z    =        -3238619
37
 XDOT =      12069
831524                 XDOT =        3678
884649
 YDOT =     -13879
112453  feet/sec       YDOT =       -4230
353476  meter/sec
 ZDOT =     -15655
157518                 ZDOT =       -4771
692011


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18342
48384185  
00016717  00000-0  10270-3 0  9073
2 25544  51
6410 230
1325 0004957 123
5604 236
6023 15
54057395 25611


Satellite: ISS
Catalog Number: 25544
Epoch time:      18342
48384185   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       230
1325  deg
Eccentricity:     
0004957     
Arg of perigee:   123
5604  deg
Mean anomaly:     236
6023  deg
Mean motion:   15
54057395  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2561
Checksum:              298


Coasting Arc #9 (Orbit 2576)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -280541
46                 A    =         6781405
01  meter
 Y    =       -5160248
95  meter          E    =           
0014379
 Z    =        4383293
64                 I    =           51
36294
 XDOT =       6427
403899                 Wp   =          115
36447
 YDOT =       2511
531734  meter/sec      RA   =          224
20108  deg
 ZDOT =       3353
401014                 TA   =          300
53963
                                          MA   =          300
68146
                                          Ha   =            222
802  n
mi
                                          Hp   =            213
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -920411
61                 X    =         -244109
10
 Y    =      -16929950
62  feet           Y    =        -5163183
01  meter
 Z    =       14380884
63                 Z    =         4382018
68
 XDOT =      21087
283133                 XDOT =        6382
552414
 YDOT =       8239
933509  feet/sec       YDOT =        2583
156221  meter/sec
 ZDOT =      11001
971830                 ZDOT =        3384
514664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15456127
99                 X    =         4711027
81
 Y    =        6980508
92  feet           Y    =         2127659
12  meter
 Z    =       14375702
80                 Z    =         4381714
21
 XDOT =     -16565
801605                 XDOT =       -5049
256329
 YDOT =      13635
253235  feet/sec       YDOT =        4156
025186  meter/sec
 ZDOT =      11141
687139                 ZDOT =        3395
986240


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18343
51272176  
00016717  00000-0  10270-3 0  9085
2 25544  51
6401 225
0042 0005053 125
9720 234
1902 15
54050590 25779


Satellite: ISS
Catalog Number: 25544
Epoch time:      18343
51272176   =   yrday
fracday
Element set:     908
Inclination:       51
6401  deg
RA of node:       225
0042  deg
Eccentricity:     
0005053     
Arg of perigee:   125
9720  deg
Mean anomaly:     234
1902  deg
Mean motion:   15
54050590  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2577
Checksum:              278


Coasting Arc #10 (Orbit 2591)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1169048
97                 A    =         6778392
83  meter
 Y    =        4314423
23  meter          E    =           
0016855
 Z    =       -5110188
14                 I    =           51
37770
 XDOT =      -6526
905649                 Wp   =           91
29861
 YDOT =      -3665
288054  meter/sec      RA   =          219
18880  deg
 ZDOT =      -1606
353156                 TA   =          163
15123
                                          MA   =          163
09518
                                          Ha   =            222
631  n
mi
                                          Hp   =            213
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3835462
51                 X    =        -1192384
54
 Y    =       14154931
87  feet           Y    =         4301220
26  meter
 Z    =      -16765709
13                 Z    =        -5115923
14
 XDOT =     -21413
732443                 XDOT =       -6477
631451
 YDOT =     -12025
223274  feet/sec       YDOT =       -3738
000743  meter/sec
 ZDOT =      -5270
187521                 ZDOT =       -1637
939427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10962037
31                 X    =        -3341228
97
 Y    =       -9696663
93  feet           Y    =        -2955543
16  meter
 Z    =      -16791971
84                 Z    =        -5118193
02
 XDOT =      19655
077491                 XDOT =        5990
867619
 YDOT =     -12876
229163  feet/sec       YDOT =       -3924
674649  meter/sec
 ZDOT =      -5411
931941                 ZDOT =       -1649
556856


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18344
47729406  
00016717  00000-0  10270-3 0  9095
2 25544  51
6400 220
1968 0004880 130
6423 229
5155 15
54081757 25925


Satellite: ISS
Catalog Number: 25544
Epoch time:      18344
47729406   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       220
1968  deg
Eccentricity:     
0004880     
Arg of perigee:   130
6423  deg
Mean anomaly:     229
5155  deg
Mean motion:   15
54081757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2592
Checksum:              314


Coasting Arc #11 (Orbit 2599)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4032968
39                 A    =         6787771
39  meter
 Y    =        5051376
41  meter          E    =           
0011769
 Z    =       -2060559
16                 I    =           51
42049
 XDOT =      -5015
254621                 Wp   =          138
31555
 YDOT =       1761
208050  meter/sec      RA   =          216
66472  deg
 ZDOT =      -5525
240022                 TA   =           64
54691
                                          MA   =           64
42519
                                          Ha   =            222
730  n
mi
                                          Hp   =            213
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13231523
58                 X    =         3986191
86
 Y    =       16572757
24  feet           Y    =         5096214
56  meter
 Z    =       -6760364
70                 Z    =        -2041081
41
 XDOT =     -16454
247445                 XDOT =       -5007
737494
 YDOT =       5778
241634  feet/sec       YDOT =        1705
166667  meter/sec
 ZDOT =     -18127
427894                 ZDOT =       -5549
583934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20574970
70                 X    =         6271251
07
 Y    =       -5250757
13  feet           Y    =        -1600430
77  meter
 Z    =       -6673242
09                 Z    =        -2034004
19
 XDOT =      -1863
932750                 XDOT =        -568
126702
 YDOT =      15760
772396  feet/sec       YDOT =        4803
883426  meter/sec
 ZDOT =     -18237
163376                 ZDOT =       -5558
687397


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18344
99173198  
00016717  00000-0  10270-3 0  9105
2 25544  51
6385 217
6301 0005137 135
9591 224
1972 15
54059547 26009


Satellite: ISS
Catalog Number: 25544
Epoch time:      18344
99173198   =   yrday
fracday
Element set:     910
Inclination:       51
6385  deg
RA of node:       217
6301  deg
Eccentricity:     
0005137     
Arg of perigee:   135
9591  deg
Mean anomaly:     224
1972  deg
Mean motion:   15
54059547  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2600
Checksum:              318


Coasting Arc #12 (Orbit 2615)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2902901
08                 A    =         6784414
07  meter
 Y    =       -5045894
92  meter          E    =           
0016172
 Z    =        3474799
29                 I    =           51
43707
 XDOT =       6179
894872                 Wp   =          104
64739
 YDOT =       -425
066934  meter/sec      RA   =          211
67196  deg
 ZDOT =       4523
842922                 TA   =          296
30933
                                          MA   =          296
47536
                                          Ha   =            222
657  n
mi
                                          Hp   =            213
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9523953
66                 X    =        -2863139
43
 Y    =      -16554773
36  feet           Y    =        -5078135
22  meter
 Z    =       11400260
15                 Z    =         3460794
07
 XDOT =      20275
245643                 XDOT =        6162
214387
 YDOT =      -1394
576556  feet/sec       YDOT =        -356
058389  meter/sec
 ZDOT =      14842
004336                 ZDOT =        4553
819670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19004836
49                 X    =        -5792674
16
 Y    =        2236926
59  feet           Y    =          681815
23  meter
 Z    =       11337746
47                 Z    =         3455745
12
 XDOT =       6895
994534                 XDOT =        2101
899134
 YDOT =     -17684
394154  feet/sec       YDOT =       -5390
203338  meter/sec
 ZDOT =      14976
966546                 ZDOT =        4564
979403


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18346
02060527  
00016717  00000-0  10270-3 0  9113
2 25544  51
6389 212
5013 0005071 138
8052 221
3484 15
54077997 26161


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
02060527   =   yrday
fracday
Element set:     911
Inclination:       51
6389  deg
RA of node:       212
5013  deg
Eccentricity:     
0005071     
Arg of perigee:   138
8052  deg
Mean anomaly:     221
3484  deg
Mean motion:   15
54077997  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2616
Checksum:              298


Coasting Arc #13 (Orbit 2630)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1434508
50                 A    =         6780706
79  meter
 Y    =        4802300
56  meter          E    =           
0012561
 Z    =       -4577615
60                 I    =           51
45263
 XDOT =      -6985
408314                 Wp   =           92
93221
 YDOT =       -800
891701  meter/sec      RA   =          206
67172  deg
 ZDOT =      -3037
104492                 TA   =          146
64186
                                          MA   =          146
56265
                                          Ha   =            222
635  n
mi
                                          Hp   =            213
498

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4706392
73                 X    =         1402936
80
 Y    =       15755579
28  feet           Y    =         4818166
13  meter
 Z    =      -15018423
89                 Z    =        -4570723
52
 XDOT =     -22918
006279                 XDOT =       -6961
180738
 YDOT =      -2627
597444  feet/sec       YDOT =        -878
871649  meter/sec
 ZDOT =      -9964
253583                 ZDOT =       -3070
978326

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16397004
38                 X    =         4997806
93
 Y    =        1562991
40  feet           Y    =          476399
78  meter
 Z    =      -14987887
52                 Z    =        -4568308
12
 XDOT =     -11027
848064                 XDOT =       -3361
288090
 YDOT =      18927
402053  feet/sec       YDOT =        5769
072146  meter/sec
 ZDOT =     -10116
651347                 ZDOT =       -3083
555330


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18346
98517487  
00016717  00000-0  10270-3 0  9121
2 25544  51
6382 207
6937 0005116 141
2995 218
8525 15
54056371 26315


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
98517487   =   yrday
fracday
Element set:     912
Inclination:       51
6382  deg
RA of node:       207
6937  deg
Eccentricity:     
0005116     
Arg of perigee:   141
2995  deg
Mean anomaly:     218
8525  deg
Mean motion:   15
54056371  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2631
Checksum:              330


Coasting Arc #14 (Orbit 2646)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         189616
29                 A    =         6778067
04  meter
 Y    =       -4362320
23  meter          E    =           
0009169
 Z    =        5179984
24                 I    =           51
47411
 XDOT =       7342
023195                 Wp   =          136
20123
 YDOT =       1831
851940  meter/sec      RA   =          201
66469  deg
 ZDOT =       1266
098909                 TA   =          301
57672
                                          MA   =          301
66620
                                          Ha   =            222
516  n
mi
                                          Hp   =            213
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         622100
69                 X    =          213221
31
 Y    =      -14312074
26  feet           Y    =        -4360068
23  meter
 Z    =       16994698
96                 Z    =         5180962
33
 XDOT =      24088
002607                 XDOT =        7314
843214
 YDOT =       6010
012925  feet/sec       YDOT =        1913
803477  meter/sec
 ZDOT =       4153
867811                 ZDOT =        1301
697960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13135978
73                 X    =        -4003846
32
 Y    =       -5701229
55  feet           Y    =        -1737734
77  meter
 Z    =       16999538
70                 Z    =         5181459
40
 XDOT =      13968
085398                 XDOT =        4257
472429
 YDOT =     -19243
647240  feet/sec       YDOT =       -5865
463679  meter/sec
 ZDOT =       4313
950431                 ZDOT =        1314
892091


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18348
01404561  
00016717  00000-0  10270-3 0  9136
2 25544  51
6381 202
5653 0005031 145
3550 214
7931 15
54078589 26479


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
01404561   =   yrday
fracday
Element set:     913
Inclination:       51
6381  deg
RA of node:       202
5653  deg
Eccentricity:     
0005031     
Arg of perigee:   145
3550  deg
Mean anomaly:     214
7931  deg
Mean motion:   15
54078589  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2647
Checksum:              299


Coasting Arc #15 (Orbit 2649)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4416428
65                 A    =         6780328
69  meter
 Y    =       -2259708
36  meter          E    =           
0010313
 Z    =        4612709
63                 I    =           51
48595
 XDOT =       5423
143606                 Wp   =           92
73996
 YDOT =       4555
235867  meter/sec      RA   =          200
63187  deg
 ZDOT =      -2955
593277                 TA   =           26
77190
                                          MA   =           26
71871
                                          Ha   =            222
366  n
mi
                                          Hp   =            213
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14489595
29                 X    =         4418963
04
 Y    =       -7413741
35  feet           Y    =        -2210306
96  meter
 Z    =       15133561
78                 Z    =         4634169
06
 XDOT =      17792
465900                 XDOT =        5386
159308
 YDOT =      14944
999563  feet/sec       YDOT =        4615
674657  meter/sec
 ZDOT =      -9696
828335                 ZDOT =       -2929
339066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15840803
79                 X    =        -4828277
00
 Y    =       -3322723
74  feet           Y    =        -1012766
20  meter
 Z    =       15230399
44                 Z    =         4642225
75
 XDOT =      -4673
711423                 XDOT =       -1424
547242
 YDOT =     -21704
377080  feet/sec       YDOT =       -6615
494134  meter/sec
 ZDOT =      -9579
084051                 ZDOT =       -2919
704819


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18348
20695937  
00016717  00000-0  10270-3 0  9147
2 25544  51
6360 201
6041 0004871 144
0598 216
0883 15
54073591 26509


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
20695937   =   yrday
fracday
Element set:     914
Inclination:       51
6360  deg
RA of node:       201
6041  deg
Eccentricity:     
0004871     
Arg of perigee:   144
0598  deg
Mean anomaly:     216
0883  deg
Mean motion:   15
54073591  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2650
Checksum:              310


Coasting Arc #16 (Orbit 2664)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5609846
33                 A    =         6784037
51  meter
 Y    =        1375373
60  meter          E    =           
0009303
 Z    =       -3569747
64                 I    =           51
53057
 XDOT =      -3998
993944                 Wp   =          120
92513
 YDOT =      -4786
164419  meter/sec      RA   =          195
63518  deg
 ZDOT =       4444
304918                 TA   =          196
89332
                                          MA   =          196
92432
                                          Ha   =            222
464  n
mi
                                          Hp   =            213
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18405007
63                 X    =        -5607469
26
 Y    =        4512380
58  feet           Y    =         1312653
91  meter
 Z    =      -11711770
48                 Z    =        -3596992
46
 XDOT =     -13120
058870                 XDOT =       -3966
764581
 YDOT =     -15702
639171  feet/sec       YDOT =       -4830
704023  meter/sec
 ZDOT =      14581
052882                 ZDOT =        4424
957178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17203150
41                 X    =         5243520
25
 Y    =        7763104
18  feet           Y    =         2366194
16  meter
 Z    =      -11834579
89                 Z    =        -3607179
95
 XDOT =       1272
327750                 XDOT =         387
805498
 YDOT =      19257
212700  feet/sec       YDOT =        5869
598431  meter/sec
 ZDOT =      14494
408823                 ZDOT =        4417
895809


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18349
17152376  
00016717  00000-0  10270-3 0  9150
2 25544  51
6370 196
7962 0004820 145
9783 214
1679 15
54053927 26655


Satellite: ISS
Catalog Number: 25544
Epoch time:      18349
17152376   =   yrday
fracday
Element set:     915
Inclination:       51
6370  deg
RA of node:       196
7962  deg
Eccentricity:     
0004820     
Arg of perigee:   145
9783  deg
Mean anomaly:     214
1679  deg
Mean motion:   15
54053927  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2665
Checksum:              339


Coasting Arc #17 (Orbit 2680)
---------------------------------------

Vector Time (GMT): 2018/350/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6414653
78                 A    =         6787481
51  meter
 Y    =        -511570
58  meter          E    =           
0017761
 Z    =        2128156
94                 I    =           51
57430
 XDOT =       2222
886862                 Wp   =          119
75865
 YDOT =       4862
253922  meter/sec      RA   =          190
65061  deg
 ZDOT =      -5505
535939                 TA   =           36
61341
                                          MA   =           36
49215
                                          Ha   =            222
281  n
mi
                                          Hp   =            213
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21045452
04                 X    =         6409560
07
 Y    =       -1678381
16  feet           Y    =         -439866
06  meter
 Z    =        6982142
19                 Z    =         2159304
78
 XDOT =       7292
935899                 XDOT =        2195
093616
 YDOT =      15952
276647  feet/sec       YDOT =        4886
956695  meter/sec
 ZDOT =     -18062
781952                 ZDOT =       -5494
805134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17753791
07                 X    =        -5411355
52
 Y    =      -11338070
18  feet           Y    =        -3455843
79  meter
 Z    =        7122456
87                 Z    =         2170924
85
 XDOT =       2891
840922                 XDOT =         881
433113
 YDOT =     -15897
234050  feet/sec       YDOT =       -4845
476939  meter/sec
 ZDOT =     -18014
934744                 ZDOT =       -5490
952110


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   18350
20039097  
00016717  00000-0  10270-3 0  9161
2 25544  51
6368 191
6673 0004729 149
8742 210
2684 15
54077958 26812


Satellite: ISS
Catalog Number: 25544
Epoch time:      18350
20039097   =   yrday
fracday
Element set:     916
Inclination:       51
6368  deg
RA of node:       191
6673  deg
Eccentricity:     
0004729     
Arg of perigee:   149
8742  deg
Mean anomaly:     210
2684  deg
Mean motion:   15
54077958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2681
Checksum:              337


Coasting Arc #18 (Orbit 2695)
---------------------------------------

Vector Time (GMT): 2018/351/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6763130
03                 A    =         6789308
53  meter
 Y    =        -270083
59  meter          E    =           
0010053
 Z    =        -505135
29                 I    =           51
61318
 XDOT =       -248
179485                 Wp   =           67
87530
 YDOT =      -4786
333050  meter/sec      RA   =          185
67636  deg
 ZDOT =       5981
092174                 TA   =          286
67642
                                          MA   =          286
78674
                                          Ha   =            222
274  n
mi
                                          Hp   =            213
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22188746
82                 X    =        -6757153
54
 Y    =        -886101
01  feet           Y    =         -345680
17  meter
 Z    =       -1657268
00                 Z    =         -537973
90
 XDOT =       -814
237154                 XDOT =        -223
692063
 YDOT =     -15703
192421  feet/sec       YDOT =       -4788
971792  meter/sec
 ZDOT =      19623
005820                 ZDOT =        5979
945798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17385651
72                 X    =         5299146
64
 Y    =       13796839
79  feet           Y    =         4205276
77  meter
 Z    =       -1805138
10                 Z    =         -550206
09
 XDOT =      -7492
396918                 XDOT =       -2283
682581
 YDOT =      11969
037899  feet/sec       YDOT =        3648
162752  meter/sec
 ZDOT =      19618
309384                 ZDOT =        5979
660700


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   18351
16495290  
00016717  00000-0  10270-3 0  9179
2 25544  51
6366 186
8598 0004826 154
2972 205
8421 15
54089394 26967


Satellite: ISS
Catalog Number: 25544
Epoch time:      18351
16495290   =   yrday
fracday
Element set:     917
Inclination:       51
6366  deg
RA of node:       186
8598  deg
Eccentricity:     
0004826     
Arg of perigee:   154
2972  deg
Mean anomaly:     205
8421  deg
Mean motion:   15
54089394  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2696
Checksum:              350


Coasting Arc #19 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2018/352/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965840
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6590837
88                 A    =         6788873
06  meter
 Y    =        1042092
36  meter          E    =           
0013767
 Z    =       -1214285
47                 I    =           51
64615
 XDOT =      -1800
741908                 Wp   =          147
83656
 YDOT =       4612
843032  meter/sec      RA   =          180
70568  deg
 ZDOT =      -5857
186425                 TA   =           45
36089
                                          MA   =           45
24873
                                          Ha   =            222
215  n
mi
                                          Hp   =            213
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21623483
84                 X    =         6584593
47
 Y    =        3418938
20  feet           Y    =         1115760
86  meter
 Z    =       -3983876
21                 Z    =        -1182284
31
 XDOT =      -5907
945891                 XDOT =       -1823
738832
 YDOT =      15133
999448  feet/sec       YDOT =        4592
577704  meter/sec
 ZDOT =     -19216
490897                 ZDOT =       -5865
989412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15730699
38                 X    =        -4794717
17
 Y    =      -15262248
39  feet           Y    =        -4651933
31  meter
 Z    =       -3839835
00                 Z    =        -1170381
71
 XDOT =      12326
570465                 XDOT =        3757
138678
 YDOT =      -7896
044632  feet/sec       YDOT =       -2406
714404  meter/sec
 ZDOT =     -19256
592314                 ZDOT =       -5869
409337


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   18352
19381628  
00016717  00000-0  10270-3 0  9183
2 25544  51
6381 181
7307 0004626 158
2758 201
8591 15
54085355 27126


Satellite: ISS
Catalog Number: 25544
Epoch time:      18352
19381628   =   yrday
fracday
Element set:     918
Inclination:       51
6381  deg
RA of node:       181
7307  deg
Eccentricity:     
0004626     
Arg of perigee:   158
2758  deg
Mean anomaly:     201
8591  deg
Mean motion:   15
54085355  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              323
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list