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

 
Date: November 23rd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 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


331/13:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 9

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

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

337/18:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 1

338/16:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 0

341/20:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 1

Coasting Arc #1 (Orbit 2327)
---------------------------------------

Vector Time (GMT): 2018/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3587775
10                 A    =         6789565
65  meter
 Y    =       -5748414
81  meter          E    =           
0016206
 Z    =        -315333
53                 I    =           51
34291
 XDOT =       4210
102269                 Wp   =           53
19428
 YDOT =       2311
940611  meter/sec      RA   =          304
10297  deg
 ZDOT =       5978
530713                 TA   =          303
39300
                                          MA   =          303
54794
                                          Ha   =            223
063  n
mi
                                          Hp   =            212
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11770915
69                 X    =         3653320
59
 Y    =      -18859628
64  feet           Y    =        -5707927
30  meter
 Z    =       -1034558
82                 Z    =         -297746
18
 XDOT =      13812
671485                 XDOT =        4154
895293
 YDOT =       7585
106992  feet/sec       YDOT =        2358
711717  meter/sec
 ZDOT =      19614
602077                 ZDOT =        5998
848567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10964702
87                 X    =         3342041
44
 Y    =       19343581
73  feet           Y    =         5895923
71  meter
 Z    =        -954723
83                 Z    =         -290999
82
 XDOT =     -11780
559279                 XDOT =       -3590
714468
 YDOT =       7611
143422  feet/sec       YDOT =        2319
876515  meter/sec
 ZDOT =      19705
606211                 ZDOT =        6006
268773


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   18327
50056307  
00016717  00000-0  10270-3 0  9004
2 25544  51
6371 304
8129 0005302  76
4536 283
7207 15
54034357 23284


Satellite: ISS
Catalog Number: 25544
Epoch time:      18327
50056307   =   yrday
fracday
Element set:     900
Inclination:       51
6371  deg
RA of node:       304
8129  deg
Eccentricity:     
0005302     
Arg of perigee:    76
4536  deg
Mean anomaly:     283
7207  deg
Mean motion:   15
54034357  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2328
Checksum:              292


Coasting Arc #2 (Orbit 2343)
---------------------------------------

Vector Time (GMT): 2018/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4151563
20                 A    =         6788821
55  meter
 Y    =        5189508
46  meter          E    =           
0011827
 Z    =       -1377193
92                 I    =           51
32385
 XDOT =      -3077
050471                 Wp   =          118
23702
 YDOT =      -3983
922626  meter/sec      RA   =          299
11119  deg
 ZDOT =      -5779
809045                 TA   =           76
82828
                                          MA   =           76
69635
                                          Ha   =            223
067  n
mi
                                          Hp   =            212
923

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13620614
19                 X    =        -4202595
35
 Y    =       17025946
39  feet           Y    =         5142797
60  meter
 Z    =       -4518352
77                 Z    =        -1397484
65
 XDOT =     -10095
309945                 XDOT =       -3004
196552
 YDOT =     -13070
612290  feet/sec       YDOT =       -4017
924399  meter/sec
 ZDOT =     -18962
628099                 ZDOT =       -5794
580078

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8832165
60                 X    =        -2692044
07
 Y    =      -19913760
70  feet           Y    =        -6069714
26  meter
 Z    =       -4610257
96                 Z    =        -1405206
63
 XDOT =      14745
187370                 XDOT =        4494
333110
 YDOT =      -2166
861627  feet/sec       YDOT =        -660
459424  meter/sec
 ZDOT =     -19028
478343                 ZDOT =       -5799
880199


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   18328
52947589  
00016717  00000-0  10270-3 0  9019
2 25544  51
6384 299
6835 0005287  77
5390 282
6354 15
54013327 23448


Satellite: ISS
Catalog Number: 25544
Epoch time:      18328
52947589   =   yrday
fracday
Element set:     901
Inclination:       51
6384  deg
RA of node:       299
6835  deg
Eccentricity:     
0005287     
Arg of perigee:    77
5390  deg
Mean anomaly:     282
6354  deg
Mean motion:   15
54013327  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2344
Checksum:              341


Coasting Arc #3 (Orbit 2359)
---------------------------------------

Vector Time (GMT): 2018/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4428559
91                 A    =         6785968
81  meter
 Y    =       -4246379
16  meter          E    =           
0018416
 Z    =        2879780
11                 I    =           51
29999
 XDOT =       1959
410952                 Wp   =           81
54690
 YDOT =       5463
971735  meter/sec      RA   =          294
11487  deg
 ZDOT =       5018
789796                 TA   =          311
43898
                                          MA   =          311
59704
                                          Ha   =            222
926  n
mi
                                          Hp   =            212
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14529396
03                 X    =         4461726
27
 Y    =      -13931690
16  feet           Y    =        -4196670
81  meter
 Z    =        9448097
46                 Z    =         2901372
96
 XDOT =       6428
513622                 XDOT =        1873
786617
 YDOT =      17926
416453  feet/sec       YDOT =        5485
403910  meter/sec
 ZDOT =      16465
845787                 ZDOT =        5028
100742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6013065
82                 X    =         1832782
46
 Y    =       19162047
59  feet           Y    =         5840592
10  meter
 Z    =        9545724
54                 Z    =         2909536
84
 XDOT =     -17466
197008                 XDOT =       -5323
696848
 YDOT =      -2782
452042  feet/sec       YDOT =        -848
091382  meter/sec
 ZDOT =      16506
963536                 ZDOT =        5031
322486


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   18329
55838319  
00016717  00000-0  10270-3 0  9024
2 25544  51
6389 294
5560 0005148  82
2292 277
9445 15
54050395 23604


Satellite: ISS
Catalog Number: 25544
Epoch time:      18329
55838319   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:       294
5560  deg
Eccentricity:     
0005148     
Arg of perigee:    82
2292  deg
Mean anomaly:     277
9445  deg
Mean motion:   15
54050395  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2360
Checksum:              332


Coasting Arc #4 (Orbit 2374)
---------------------------------------

Vector Time (GMT): 2018/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4523946
38                 A    =         6782278
59  meter
 Y    =        2913963
39  meter          E    =           
0012936
 Z    =       -4141339
15                 I    =           51
27441
 XDOT =       -865
787305                 Wp   =           75
54266
 YDOT =      -6632
340198  meter/sec      RA   =          289
10706  deg
 ZDOT =      -3727
572250                 TA   =          155
87945
                                          MA   =          155
81882
                                          Ha   =            223
072  n
mi
                                          Hp   =            212
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14842343
75                 X    =        -4536078
23
 Y    =        9560247
33  feet           Y    =         2863306
10  meter
 Z    =      -13587070
71                 Z    =        -4163344
31
 XDOT =      -2840
509530                 XDOT =        -773
451490
 YDOT =     -21759
646319  feet/sec       YDOT =       -6641
505335  meter/sec
 ZDOT =     -12229
567748                 ZDOT =       -3731
554463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2273422
59                 X    =         -692939
20
 Y    =      -17430340
87  feet           Y    =        -5312767
90  meter
 Z    =      -13686371
11                 Z    =        -4171605
92
 XDOT =      19555
947284                 XDOT =        5960
652732
 YDOT =       7048
412576  feet/sec       YDOT =        2148
356153  meter/sec
 ZDOT =     -12246
590764                 ZDOT =       -3732
760865


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   18330
52298436  
00016717  00000-0  10270-3 0  9034
2 25544  51
6385 289
7477 0005271  83
5518 276
6235 15
54021552 23757


Satellite: ISS
Catalog Number: 25544
Epoch time:      18330
52298436   =   yrday
fracday
Element set:     903
Inclination:       51
6385  deg
RA of node:       289
7477  deg
Eccentricity:     
0005271     
Arg of perigee:    83
5518  deg
Mean anomaly:     276
6235  deg
Mean motion:   15
54021552  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2375
Checksum:              325


Coasting Arc #5 (Orbit 2390)
---------------------------------------

Vector Time (GMT): 2018/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4428688
64                 A    =         6778995
85  meter
 Y    =       -1332856
73  meter          E    =           
0010632
 Z    =        4948493
85                 I    =           51
25448
 XDOT =       -122
708913                 Wp   =          107
13114
 YDOT =       7383
002342  meter/sec      RA   =          284
09052  deg
 ZDOT =       2091
589176                 TA   =          322
37893
                                          MA   =          322
45326
                                          Ha   =            222
800  n
mi
                                          Hp   =            212
929

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14529818
38                 X    =         4419226
53
 Y    =       -4372889
52  feet           Y    =        -1283385
45  meter
 Z    =       16235216
06                 Z    =         4969983
92
 XDOT =       -402
588296                 XDOT =        -215
418494
 YDOT =      24222
448628  feet/sec       YDOT =        7381
111546  meter/sec
 ZDOT =       6862
169212                 ZDOT =        2090
768652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2009477
33                 X    =         -612488
69
 Y    =       14934792
06  feet           Y    =         4552124
62  meter
 Z    =       16331993
52                 Z    =         4977991
62
 XDOT =     -20762
015351                 XDOT =       -6328
262279
 YDOT =     -10316
891569  feet/sec       YDOT =       -3144
588550  meter/sec
 ZDOT =       6857
521960                 ZDOT =        2090
172693


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   18331
55188679  
00016717  00000-0  10270-3 0  9046
2 25544  51
6390 284
6206 0005025  87
9790 272
1938 15
54059009 23911


Satellite: ISS
Catalog Number: 25544
Epoch time:      18331
55188679   =   yrday
fracday
Element set:     904
Inclination:       51
6390  deg
RA of node:       284
6206  deg
Eccentricity:     
0005025     
Arg of perigee:    87
9790  deg
Mean anomaly:     272
1938  deg
Mean motion:   15
54059009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2391
Checksum:              331


Coasting Arc #6 (Orbit 2391)
---------------------------------------

Vector Time (GMT): 2018/331/13:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1690353
45                 A    =         6789623
18  meter
 Y    =       -6568915
31  meter          E    =           
0016542
 Z    =          91120
88                 I    =           51
28935
 XDOT =       4622
481513                 Wp   =           58
19615
 YDOT =       1283
483813  meter/sec      RA   =          283
81372  deg
 ZDOT =       5983
157233                 TA   =          302
79022
                                          MA   =          302
94946
                                          Ha   =            223
036  n
mi
                                          Hp   =            212
924

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5545779
03                 X    =         1763240
65
 Y    =      -21551559
43  feet           Y    =        -6549605
08  meter
 Z    =         298953
00                 Z    =           99508
46
 XDOT =      15165
621761                 XDOT =        4578
722473
 YDOT =       4210
904897  feet/sec       YDOT =        1334
930349  meter/sec
 ZDOT =      19629
780947                 ZDOT =        6005
505640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20890914
84                 X    =         6367550
84
 Y    =        7666193
05  feet           Y    =         2336655
64  meter
 Z    =         337509
95                 Z    =          102873
03
 XDOT =      -5132
322076                 XDOT =       -1564
331769
 YDOT =      13015
822491  feet/sec       YDOT =        3967
222695  meter/sec
 ZDOT =      19730
077416                 ZDOT =        6013
727597


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   18331
61619459  
00016717  00000-0  10270-3 0  9059
2 25544  51
6392 284
3000 0005153  87
7950 272
3793 15
54026528 23922


Satellite: ISS
Catalog Number: 25544
Epoch time:      18331
61619459   =   yrday
fracday
Element set:     905
Inclination:       51
6392  deg
RA of node:       284
3000  deg
Eccentricity:     
0005153     
Arg of perigee:    87
7950  deg
Mean anomaly:     272
3793  deg
Mean motion:   15
54026528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2392
Checksum:              315


Coasting Arc #7 (Orbit 2406)
---------------------------------------

Vector Time (GMT): 2018/332/13:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2383798
57                 A    =         6788254
09  meter
 Y    =        6102515
07  meter          E    =           
0011362
 Z    =       -1771225
70                 I    =           51
27893
 XDOT =      -4074
739798                 Wp   =          120
47271
 YDOT =      -3218
476688  meter/sec      RA   =          278
81836  deg
 ZDOT =      -5637
599200                 TA   =           79
06978
                                          MA   =           78
94197
                                          Ha   =            223
026  n
mi
                                          Hp   =            212
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7820861
43                 X    =        -2443257
71
 Y    =       20021374
89  feet           Y    =         6075525
46  meter
 Z    =       -5811107
93                 Z    =        -1782949
35
 XDOT =     -13368
568890                 XDOT =       -4011
062454
 YDOT =     -10559
306720  feet/sec       YDOT =       -3263
686776  meter/sec
 ZDOT =     -18496
060369                 ZDOT =       -5657
238547

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19309358
98                 X    =        -5885492
62
 Y    =       -9409866
09  feet           Y    =        -2868127
18  meter
 Z    =       -5864586
73                 Z    =        -1787526
04
 XDOT =      10932
954074                 XDOT =        3332
364402
 YDOT =     -10918
932648  feet/sec       YDOT =       -3328
090671  meter/sec
 ZDOT =     -18583
940393                 ZDOT =       -5664
385032


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   18332
58078780  
00016717  00000-0  10270-3 0  9063
2 25544  51
6401 279
4919 0005180  89
9026 270
2720 15
54030541 24079


Satellite: ISS
Catalog Number: 25544
Epoch time:      18332
58078780   =   yrday
fracday
Element set:     906
Inclination:       51
6401  deg
RA of node:       279
4919  deg
Eccentricity:     
0005180     
Arg of perigee:    89
9026  deg
Mean anomaly:     270
2720  deg
Mean motion:   15
54030541  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2407
Checksum:              306


Coasting Arc #8 (Orbit 2422)
---------------------------------------

Vector Time (GMT): 2018/333/13:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2935838
17                 A    =         6785160
17  meter
 Y    =       -5190546
46  meter          E    =           
0017944
 Z    =        3220905
23                 I    =           51
26366
 XDOT =       3483
115441                 Wp   =           88
91369
 YDOT =       4926
173269  meter/sec      RA   =          273
81705  deg
 ZDOT =       4741
164272                 TA   =          308
62125
                                          MA   =          308
78177
                                          Ha   =            223
004  n
mi
                                          Hp   =            212
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9632014
98                 X    =         2978016
59
 Y    =      -17029351
90  feet           Y    =        -5157480
22  meter
 Z    =       10567274
38                 Z    =         3235268
73
 XDOT =      11427
544098                 XDOT =        3404
740555
 YDOT =      16161
985792  feet/sec       YDOT =        4964
685400  meter/sec
 ZDOT =      15555
000894                 ZDOT =        4757
894025

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16365885
43                 X    =         4988321
88
 Y    =       10655971
19  feet           Y    =         3247940
02  meter
 Z    =       10632492
58                 Z    =         3240783
74
 XDOT =     -16092
935979                 XDOT =       -4905
126886
 YDOT =       9047
474791  feet/sec       YDOT =        2757
670316  meter/sec
 ZDOT =      15629
600450                 ZDOT =        4763
902217


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   18333
60968431  
00016717  00000-0  10270-3 0  9079
2 25544  51
6392 274
3642 0005220  93
7146 266
4603 15
54030794 24231


Satellite: ISS
Catalog Number: 25544
Epoch time:      18333
60968431   =   yrday
fracday
Element set:     907
Inclination:       51
6392  deg
RA of node:       274
3642  deg
Eccentricity:     
0005220     
Arg of perigee:    93
7146  deg
Mean anomaly:     266
4603  deg
Mean motion:   15
54030794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2423
Checksum:              304


Coasting Arc #9 (Orbit 2437)
---------------------------------------

Vector Time (GMT): 2018/334/13:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3445245
89                 A    =         6781297
02  meter
 Y    =        3865415
38  meter          E    =           
0013879
 Z    =       -4392282
67                 I    =           51
25060
 XDOT =      -2811
067760                 Wp   =           79
31342
 YDOT =      -6291
504172  meter/sec      RA   =          268
80510  deg
 ZDOT =      -3338
355887                 TA   =          156
72888
                                          MA   =          156
66599
                                          Ha   =            222
990  n
mi
                                          Hp   =            212
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11303300
16                 X    =        -3466878
47
 Y    =       12681809
00  feet           Y    =         3826767
46  meter
 Z    =      -14410376
22                 Z    =        -4409070
97
 XDOT =      -9222
663253                 XDOT =       -2724
289406
 YDOT =     -20641
417888  feet/sec       YDOT =       -6322
454148  meter/sec
 ZDOT =     -10952
611177                 ZDOT =       -3351
800636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12124507
96                 X    =        -3695550
03
 Y    =      -11806547
92  feet           Y    =        -3598635
80  meter
 Z    =      -14486322
85                 Z    =        -4415431
21
 XDOT =      20199
203187                 XDOT =        6156
717131
 YDOT =      -7257
417644  feet/sec       YDOT =       -2212
060898  meter/sec
 ZDOT =     -11012
291518                 ZDOT =       -3356
546455


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18334
57427220  
00016717  00000-0  10270-3 0  9083
2 25544  51
6400 269
5564 0005190  96
8204 263
3539 15
54055035 24380


Satellite: ISS
Catalog Number: 25544
Epoch time:      18334
57427220   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:       269
5564  deg
Eccentricity:     
0005190     
Arg of perigee:    96
8204  deg
Mean anomaly:     263
3539  deg
Mean motion:   15
54055035  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2438
Checksum:              307


Coasting Arc #10 (Orbit 2453)
---------------------------------------

Vector Time (GMT): 2018/335/13:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3856501
46                 A    =         6778400
43  meter
 Y    =       -2274389
18  meter          E    =           
0009867
 Z    =        5082410
53                 I    =           51
24297
 XDOT =       2096
733324                 Wp   =          113
31180
 YDOT =       7201
189280  meter/sec      RA   =          263
78404  deg
 ZDOT =       1625
198914                 TA   =          320
89489
                                          MA   =          320
96617
                                          Ha   =            222
786  n
mi
                                          Hp   =            212
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12652563
83                 X    =         3856959
79
 Y    =       -7461906
77  feet           Y    =        -2231260
70  meter
 Z    =       16674575
23                 Z    =         5101145
30
 XDOT =       6879
046339                 XDOT =        2008
157344
 YDOT =      23625
949081  feet/sec       YDOT =        7224
141100  meter/sec
 ZDOT =       5332
017434                 ZDOT =        1635
169300

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7066739
49                 X    =         2153942
20
 Y    =       12767279
88  feet           Y    =         3891466
91  meter
 Z    =       16759076
36                 Z    =         5108166
48
 XDOT =     -22896
879115                 XDOT =       -6978
968754
 YDOT =       5589
428156  feet/sec       YDOT =        1703
657702  meter/sec
 ZDOT =       5375
985735                 ZDOT =        1638
600452


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18335
60316124  
00016717  00000-0  10270-3 0  9099
2 25544  51
6401 264
4281 0005050 101
7244 258
4476 15
54071669 24540


Satellite: ISS
Catalog Number: 25544
Epoch time:      18335
60316124   =   yrday
fracday
Element set:     909
Inclination:       51
6401  deg
RA of node:       264
4281  deg
Eccentricity:     
0005050     
Arg of perigee:   101
7244  deg
Mean anomaly:     258
4476  deg
Mean motion:   15
54071669  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2454
Checksum:              293


Coasting Arc #11 (Orbit 2468)
---------------------------------------

Vector Time (GMT): 2018/336/13:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930150
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4225300
14                 A    =         6777581
91  meter
 Y    =         525777
33  meter          E    =           
0019924
 Z    =       -5290470
37                 I    =           51
24556
 XDOT =      -1277
867132                 Wp   =           95
04198
 YDOT =      -7541
349907  meter/sec      RA   =          258
75733  deg
 ZDOT =        270
274768                 TA   =          177
55830
                                          MA   =          177
54856
                                          Ha   =            222
969  n
mi
                                          Hp   =            212
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13862533
28                 X    =        -4205166
85
 Y    =        1724991
23  feet           Y    =          478639
83  meter
 Z    =      -17357186
25                 Z    =        -5310946
77
 XDOT =      -4192
477466                 XDOT =       -1194
755543
 YDOT =     -24741
961638  feet/sec       YDOT =       -7555
175209  meter/sec
 ZDOT =        886
728241                 ZDOT =         264
268864

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1532112
51                 X    =         -466987
89
 Y    =      -13769223
01  feet           Y    =        -4196859
17  meter
 Z    =      -17449311
38                 Z    =        -5318550
11
 XDOT =      23793
890752                 XDOT =        7252
377901
 YDOT =      -3741
643342  feet/sec       YDOT =       -1140
452891  meter/sec
 ZDOT =        860
608147                 ZDOT =         262
313363


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18336
56774335  
00016717  00000-0  10270-3 0  9109
2 25544  51
6409 259
6200 0005161 103
4109 256
7619 15
54060677 24690


Satellite: ISS
Catalog Number: 25544
Epoch time:      18336
56774335   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:       259
6200  deg
Eccentricity:     
0005161     
Arg of perigee:   103
4109  deg
Mean anomaly:     256
7619  deg
Mean motion:   15
54060677  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2469
Checksum:              313


Coasting Arc #12 (Orbit 2483)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3195784
16                 A    =         6778897
18  meter
 Y    =       -3322209
44  meter          E    =           
0010987
 Z    =        4963271
76                 I    =           51
25553
 XDOT =       3552
207773                 Wp   =          116
67055
 YDOT =       6487
080822  meter/sec      RA   =          254
12489  deg
 ZDOT =       2046
595948                 TA   =          313
28848
                                          MA   =          313
38007
                                          Ha   =            222
749  n
mi
                                          Hp   =            212
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10484856
18                 X    =         3208587
18
 Y    =      -10899637
26  feet           Y    =        -3286400
59  meter
 Z    =       16283700
01                 Z    =         4978826
97
 XDOT =      11654
224976                 XDOT =        3469
461971
 YDOT =      21283
073563  feet/sec       YDOT =        6526
341328  meter/sec
 ZDOT =       6714
553636                 ZDOT =        2063
650922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5329964
45                 X    =         1624573
16
 Y    =       14072333
08  feet           Y    =         4289247
12  meter
 Z    =       16354024
23                 Z    =         4984706
58
 XDOT =     -23185
593914                 XDOT =       -7066
969025
 YDOT =        858
383037  feet/sec       YDOT =         261
635150  meter/sec
 ZDOT =       6790
488143                 ZDOT =        2069
740786


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
53232159  
00016717  00000-0  10270-3 0  9111
2 25544  51
6393 254
8123 0005000 108
5830 251
5866 15
54083994 24843


Satellite: ISS
Catalog Number: 25544
Epoch time:      18337
53232159   =   yrday
fracday
Element set:     911
Inclination:       51
6393  deg
RA of node:       254
8123  deg
Eccentricity:     
0005000     
Arg of perigee:   108
5830  deg
Mean anomaly:     251
5866  deg
Mean motion:   15
54083994  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2484
Checksum:              308


Coasting Arc #13 (Orbit 2487)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1403505
67                 A    =         6783700
87  meter
 Y    =       -5505495
59  meter          E    =           
0016453
 Z    =        3694905
21                 I    =           51
27196
 XDOT =       4858
536971                 Wp   =           99
80453
 YDOT =       4120
897385  meter/sec      RA   =          252
86634  deg
 ZDOT =       4275
666064                 TA   =          304
52962
                                          MA   =          304
68483
                                          Ha   =            222
786  n
mi
                                          Hp   =            213
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4604677
39                 X    =         1447017
15
 Y    =      -18062649
56  feet           Y    =        -5489557
50  meter
 Z    =       12122392
41                 Z    =         3701828
49
 XDOT =      15940
081926                 XDOT =        4791
325575
 YDOT =      13520
004543  feet/sec       YDOT =        4174
852916  meter/sec
 ZDOT =      14027
775800                 ZDOT =        4299
104489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11596080
51                 X    =         3534485
34
 Y    =      -14567847
45  feet           Y    =        -4440279
90  meter
 Z    =       12154155
60                 Z    =         3704586
63
 XDOT =       7763
642687                 XDOT =        2366
358291
 YDOT =      18023
025457  feet/sec       YDOT =        5493
418159  meter/sec
 ZDOT =      14132
688368                 ZDOT =        4307
643414


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
78954147  
00016717  00000-0  10270-3 0  9127
2 25544  51
6376 253
5283 0004838 110
3160 249
8513 15
54061826 24885


Satellite: ISS
Catalog Number: 25544
Epoch time:      18337
78954147   =   yrday
fracday
Element set:     912
Inclination:       51
6376  deg
RA of node:       253
5283  deg
Eccentricity:     
0004838     
Arg of perigee:   110
3160  deg
Mean anomaly:     249
8513  deg
Mean motion:   15
54061826  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2488
Checksum:              326


Coasting Arc #14 (Orbit 2487)
---------------------------------------

Vector Time (GMT): 2018/337/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4172310
40                 A    =         6784322
49  meter
 Y    =        4062736
03  meter          E    =           
0016821
 Z    =        3464421
61                 I    =           51
27459
 XDOT =      -1964
170856                 Wp   =           94
72020
 YDOT =       5884
526835  meter/sec      RA   =          252
72961  deg
 ZDOT =      -4517
663871                 TA   =           44
33423
                                          MA   =           44
19964
                                          Ha   =            222
712  n
mi
                                          Hp   =            213
054

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13688682
40                 X    =         4109741
04
 Y    =       13329186
44  feet           Y    =         4109043
69  meter
 Z    =       11366212
64                 Z    =         3484537
81
 XDOT =      -6444
130105                 XDOT =       -2007
882511
 YDOT =      19306
190402  feet/sec       YDOT =        5862
317920  meter/sec
 ZDOT =     -14821
731861                 ZDOT =       -4527
311177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8718793
73                 X    =         2657488
33
 Y    =       16940374
08  feet           Y    =         5163426
02  meter
 Z    =       11456194
34                 Z    =         3491848
03
 XDOT =     -10869
783568                 XDOT =       -3313
110032
 YDOT =      15686
427269  feet/sec       YDOT =        4781
223031  meter/sec
 ZDOT =     -14865
786594                 ZDOT =       -4531
091754


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
78954098  
00016717  00000-0  10270-3 0  9133
2 25544  51
6378 253
5272 0004828 110
2475 249
9197 15
54070673 24881


Satellite: ISS
Catalog Number: 25544
Epoch time:      18337
78954098   =   yrday
fracday
Element set:     913
Inclination:       51
6378  deg
RA of node:       253
5272  deg
Eccentricity:     
0004828     
Arg of perigee:   110
2475  deg
Mean anomaly:     249
9197  deg
Mean motion:   15
54070673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2488
Checksum:              348


Coasting Arc #15 (Orbit 2501)
---------------------------------------

Vector Time (GMT): 2018/338/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2859119
50                 A    =         6778934
71  meter
 Y    =        3615591
67  meter          E    =           
0016805
 Z    =       -4985619
28                 I    =           51
26796
 XDOT =      -4183
034398                 Wp   =           84
95144
 YDOT =      -6085
654328  meter/sec      RA   =          248
16384  deg
 ZDOT =      -2018
932445                 TA   =          165
31400
                                          MA   =          165
26512
                                          Ha   =            222
792  n
mi
                                          Hp   =            212
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9380313
32                 X    =        -2875119
63
 Y    =       11862177
41  feet           Y    =         3583529
87  meter
 Z    =      -16357018
65                 Z    =        -4999546
77
 XDOT =     -13723
866136                 XDOT =       -4104
864935
 YDOT =     -19966
057505  feet/sec       YDOT =       -6131
994722  meter/sec
 ZDOT =      -6623
794110                 ZDOT =       -2039
063064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14977957
94                 X    =        -4565281
58
 Y    =        1515288
87  feet           Y    =          461860
05  meter
 Z    =      -16420056
81                 Z    =        -5004833
32
 XDOT =       5057
693529                 XDOT =        1541
584988
 YDOT =     -22599
880234  feet/sec       YDOT =       -6888
443495  meter/sec
 ZDOT =      -6713
621099                 ZDOT =       -2046
311711


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
68981263  
00016717  00000-0  10270-3 0  9148
2 25544  51
6395 249
0418 0004821 111
8162 248
3504 15
54062626 25026


Satellite: ISS
Catalog Number: 25544
Epoch time:      18338
68981263   =   yrday
fracday
Element set:     914
Inclination:       51
6395  deg
RA of node:       249
0418  deg
Eccentricity:     
0004821     
Arg of perigee:   111
8162  deg
Mean anomaly:     248
3504  deg
Mean motion:   15
54062626  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2502
Checksum:              308


Coasting Arc #16 (Orbit 2517)
---------------------------------------

Vector Time (GMT): 2018/339/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3700656
79                 A    =         6777601
41  meter
 Y    =       -2067494
42  meter          E    =           
0007341
 Z    =        5282386
77                 I    =           51
27667
 XDOT =       3574
045495                 Wp   =          109
71308
 YDOT =       6789
365619  meter/sec      RA   =          243
14018  deg
 ZDOT =        150
857582                 TA   =          338
82791
                                          MA   =          338
85828
                                          Ha   =            222
735  n
mi
                                          Hp   =            213
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12141262
44                 X    =         3697841
56
 Y    =       -6783118
17  feet           Y    =        -2026127
29  meter
 Z    =       17330665
25                 Z    =         5300356
57
 XDOT =      11725
871048                 XDOT =        3497
126479
 YDOT =      22274
821586  feet/sec       YDOT =        6828
902986  meter/sec
 ZDOT =        494
939574                 ZDOT =         168
033109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13284129
52                 X    =         4049002
68
 Y    =        3759948
94  feet           Y    =         1146032
44  meter
 Z    =       17411708
43                 Z    =         5307088
73
 XDOT =      -7281
800683                 XDOT =       -2219
492848
 YDOT =      23041
498376  feet/sec       YDOT =        7023
048705  meter/sec
 ZDOT =        571
413698                 ZDOT =         174
166895


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
71869176  
00016717  00000-0  10270-3 0  9152
2 25544  51
6394 243
9134 0004961 115
1917 244
9751 15
54042935 25187


Satellite: ISS
Catalog Number: 25544
Epoch time:      18339
71869176   =   yrday
fracday
Element set:     915
Inclination:       51
6394  deg
RA of node:       243
9134  deg
Eccentricity:     
0004961     
Arg of perigee:   115
1917  deg
Mean anomaly:     244
9751  deg
Mean motion:   15
54042935  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2518
Checksum:              333


Coasting Arc #17 (Orbit 2532)
---------------------------------------

Vector Time (GMT): 2018/340/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4494057
15                 A    =         6778519
68  meter
 Y    =         466452
46  meter          E    =           
0018122
 Z    =       -5069602
42                 I    =           51
29407
 XDOT =      -2684
291876                 Wp   =          107
70577
 YDOT =      -6954
111315  meter/sec      RA   =          238
11622  deg
 ZDOT =       1739
450729                 TA   =          179
22576
                                          MA   =          179
22295
                                          Ha   =            222
786  n
mi
                                          Hp   =            212
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14744282
00                 X    =        -4474313
32
 Y    =        1530355
84  feet           Y    =          416307
72  meter
 Z    =      -16632553
86                 Z    =        -5091385
32
 XDOT =      -8806
731875                 XDOT =       -2614
779017
 YDOT =     -22815
325838  feet/sec       YDOT =       -6983
740444  meter/sec
 ZDOT =       5706
859348                 ZDOT =        1726
579277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11550449
07                 X    =        -3520576
88
 Y    =       -9113325
46  feet           Y    =        -2777741
60  meter
 Z    =      -16730574
22                 Z    =        -5099479
02
 XDOT =       8915
773467                 XDOT =        2717
527753
 YDOT =     -21673
579507  feet/sec       YDOT =       -6606
107034  meter/sec
 ZDOT =       5649
744587                 ZDOT =        1722
042150


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
68326350  
00016717  00000-0  10270-3 0  9163
2 25544  51
6375 239
1049 0004947 119
6672 240
4974 15
54068288 25333


Satellite: ISS
Catalog Number: 25544
Epoch time:      18340
68326350   =   yrday
fracday
Element set:     916
Inclination:       51
6375  deg
RA of node:       239
1049  deg
Eccentricity:     
0004947     
Arg of perigee:   119
6672  deg
Mean anomaly:     240
4974  deg
Mean motion:   15
54068288  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2533
Checksum:              330


Coasting Arc #18 (Orbit 2548)
---------------------------------------

Vector Time (GMT): 2018/341/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5115528
25                 A    =         6781444
92  meter
 Y    =        1065068
53  meter          E    =           
0013039
 Z    =        4311494
71                 I    =           51
32312
 XDOT =       1540
040874                 Wp   =           88
56488
 YDOT =       6672
034440  meter/sec      RA   =          233
09974  deg
 ZDOT =      -3466
015204                 TA   =           36
82413
                                          MA   =           36
73465
                                          Ha   =            222
517  n
mi
                                          Hp   =            213
236

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16783229
16                 X    =         5082294
93
 Y    =        3494319
34  feet           Y    =         1122087
59  meter
 Z    =       14145323
86                 Z    =         4336263
89
 XDOT =       5052
627540                 XDOT =        1482
154137
 YDOT =      21889
876771  feet/sec       YDOT =        6688
932997  meter/sec
 ZDOT =     -11371
440957                 ZDOT =       -3458
673926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9759649
76                 X    =         2974741
25
 Y    =       13981247
19  feet           Y    =         4261484
14  meter
 Z    =       14256619
49                 Z    =         4345417
62
 XDOT =     -10244
306728                 XDOT =       -3122
464691
 YDOT =      18744
805526  feet/sec       YDOT =        5713
416724  meter/sec
 ZDOT =     -11339
153965                 ZDOT =       -3456
174129


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
71213802  
00016717  00000-0  10270-3 0  9176
2 25544  51
6382 233
9764 0004741 124
2794 235
8808 15
54080396 25491


Satellite: ISS
Catalog Number: 25544
Epoch time:      18341
71213802   =   yrday
fracday
Element set:     917
Inclination:       51
6382  deg
RA of node:       233
9764  deg
Eccentricity:     
0004741     
Arg of perigee:   124
2794  deg
Mean anomaly:     235
8808  deg
Mean motion:   15
54080396  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2549
Checksum:              321


Coasting Arc #19 (Orbit 2551)
---------------------------------------

Vector Time (GMT): 2018/341/20:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945381
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2982740
63                 A    =         6788453
98  meter
 Y    =       -5889668
64  meter          E    =           
0016808
 Z    =        1557446
60                 I    =           51
35131
 XDOT =       5005
217499                 Wp   =           79
25283
 YDOT =      -1008
617427  meter/sec      RA   =          232
26656  deg
 ZDOT =       5721
927299                 TA   =          297
84441
                                          MA   =          298
01461
                                          Ha   =            222
817  n
mi
                                          Hp   =            213
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9785894
47                 X    =        -2924224
37
 Y    =      -19323059
86  feet           Y    =        -5922696
73  meter
 Z    =        5109732
93                 Z    =         1543098
72
 XDOT =      16421
317253                 XDOT =        4988
329719
 YDOT =      -3309
112292  feet/sec       YDOT =        -952
740729  meter/sec
 ZDOT =      18772
727359                 ZDOT =        5746
200054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15685061
15                 X    =        -4780806
64
 Y    =      -14959013
62  feet           Y    =        -4559507
35  meter
 Z    =        5045841
02                 Z    =         1537972
34
 XDOT =      13178
433450                 XDOT =        4016
786516
 YDOT =      -7393
360582  feet/sec       YDOT =       -2253
496305  meter/sec
 ZDOT =      18882
020428                 ZDOT =        5755
239826


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
90505330  
00016717  00000-0  10270-3 0  9188
2 25544  51
6396 233
0122 0005302 127
9948 232
1684 15
54086059 25528


Satellite: ISS
Catalog Number: 25544
Epoch time:      18341
90505330   =   yrday
fracday
Element set:     918
Inclination:       51
6396  deg
RA of node:       233
0122  deg
Eccentricity:     
0005302     
Arg of perigee:   127
9948  deg
Mean anomaly:     232
1684  deg
Mean motion:   15
54086059  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2552
Checksum:              300
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