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

 
Date: May 30th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14262 1813 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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


146/12:07:22 200 0 0 0 0 0 0
N/A -0 0 -0 0 228 5
000/00:12:03 600 0 0 0 0 222 2

148/20:33:33 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 2

149/04:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 222 2

149/15:39:55 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 2

152/12:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 222 0

160/04:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 221 7

Coasting Arc #1 (Orbit 2848)
---------------------------------------

Vector Time (GMT): 2020/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2889874
51                 A    =         6794559
08  meter
 Y    =        4146263
08  meter          E    =           
0008863
 Z    =       -4549652
35                 I    =           52
01546
 XDOT =      -3558
870999                 Wp   =          100
43334
 YDOT =       5977
020061  meter/sec      RA   =           99
78665  deg
 ZDOT =       3190
246072                 TA   =          201
47895
                                          MA   =          201
51616
                                          Ha   =            228
508  n
mi
                                          Hp   =            222
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9481215
58                 X    =         2865394
76
 Y    =       13603225
32  feet           Y    =         4178443
61  meter
 Z    =      -14926680
95                 Z    =        -4535673
11
 XDOT =     -11676
085955                 XDOT =       -3640
939819
 YDOT =      19609
645868  feet/sec       YDOT =        5936
762816  meter/sec
 ZDOT =      10466
686589                 ZDOT =        3172
760012

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16485077
08                 X    =         5024651
49
 Y    =       -2256772
27  feet           Y    =         -687864
19  meter
 Z    =      -14862577
33                 Z    =        -4530113
57
 XDOT =      11850
386685                 XDOT =        3611
997862
 YDOT =      18245
111353  feet/sec       YDOT =        5561
109940  meter/sec
 ZDOT =      10385
912307                 ZDOT =        3165
626071


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   20146
51043290  
00016717  00000-0  10270-3 0  9004
2 25544  51
6406 100
7144 0001800 349
1600  10
9511 15
49370393 28497


Satellite: ISS
Catalog Number: 25544
Epoch time:      20146
51043290   =   yrday
fracday
Element set:     900
Inclination:       51
6406  deg
RA of node:       100
7144  deg
Eccentricity:     
0001800     
Arg of perigee:   349
1600  deg
Mean anomaly:      10
9511  deg
Mean motion:   15
49370393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2849
Checksum:              265


Coasting Arc #2 (Orbit 2848)
---------------------------------------

Vector Time (GMT): 2020/146/12:13:24
000
Vector Time (MET): N/A
Weight (LBS)     : 953907
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -701260
56                 A    =         6802998
96  meter
 Y    =        6735841
02  meter          E    =           
0011985
 Z    =        -577568
87                 I    =           52
04380
 XDOT =      -4756
359817                 Wp   =           34
69622
 YDOT =         13
772283  meter/sec      RA   =           99
75811  deg
 ZDOT =       6006
255110                 TA   =          319
11688
                                          MA   =          319
20671
                                          Ha   =            228
479  n
mi
                                          Hp   =            222
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2300723
61                 X    =         -773725
09
 Y    =       22099215
96  feet           Y    =         6727593
95  meter
 Z    =       -1894911
00                 Z    =         -581150
21
 XDOT =     -15604
855044                 XDOT =       -4785
335498
 YDOT =         45
184656  feet/sec       YDOT =         -39
579749  meter/sec
 ZDOT =      19705
561386                 ZDOT =        5983
080014

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19256206
59                 X    =         5869291
77
 Y    =       11081655
95  feet           Y    =         3377688
73  meter
 Z    =       -1911745
70                 Z    =         -582700
09
 XDOT =      -5553
452079                 XDOT =       -1692
692194
 YDOT =      12991
496985  feet/sec       YDOT =        3959
808281  meter/sec
 ZDOT =      19598
924930                 ZDOT =        5973
752319


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   20146
51043288  
00016717  00000-0  10270-3 0  9012
2 25544  51
6406 100
7145 0001739 350
4977   9
6140 15
49388265 28491


Satellite: ISS
Catalog Number: 25544
Epoch time:      20146
51043288   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:       100
7145  deg
Eccentricity:     
0001739     
Arg of perigee:   350
4977  deg
Mean anomaly:       9
6140  deg
Mean motion:   15
49388265  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2849
Checksum:              307


Coasting Arc #3 (Orbit 2864)
---------------------------------------

Vector Time (GMT): 2020/147/12:13:24
000
Vector Time (MET): N/A
Weight (LBS)     : 953907
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         240217
86                 A    =         6803092
67  meter
 Y    =       -6780518
15  meter          E    =           
0011549
 Z    =         426130
12                 I    =           52
04946
 XDOT =       4730
741475                 Wp   =          124
45933
 YDOT =       -217
667071  meter/sec      RA   =           94
83664  deg
 ZDOT =      -6020
727335                 TA   =           50
98127
                                          MA   =           50
87850
                                          Ha   =            228
508  n
mi
                                          Hp   =            222
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         788116
33                 X    =          313951
87
 Y    =      -22245794
47  feet           Y    =        -6777419
67  meter
 Z    =        1398064
69                 Z    =          427474
94
 XDOT =      15520
805365                 XDOT =        4762
069237
 YDOT =       -714
130811  feet/sec       YDOT =        -164
588367  meter/sec
 ZDOT =     -19753
042439                 ZDOT =       -5997
671111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20169169
59                 X    =        -6147562
89
 Y    =       -9417149
50  feet           Y    =        -2870347
17  meter
 Z    =        1404626
96                 Z    =          428130
30
 XDOT =       4777
859810                 XDOT =        1456
291670
 YDOT =     -13216
807430  feet/sec       YDOT =       -4028
482905  meter/sec
 ZDOT =     -19646
932111                 ZDOT =       -5988
384907


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   20147
54241826  
00016717  00000-0  10270-3 0  9025
2 25544  51
6415  95
6070 0001774 352
3114   7
8008 15
49379051 28657


Satellite: ISS
Catalog Number: 25544
Epoch time:      20147
54241826   =   yrday
fracday
Element set:     902
Inclination:       51
6415  deg
RA of node:        95
6070  deg
Eccentricity:     
0001774     
Arg of perigee:   352
3114  deg
Mean anomaly:       7
8008  deg
Mean motion:   15
49379051  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2865
Checksum:              296


Coasting Arc #4 (Orbit 2879)
---------------------------------------

Vector Time (GMT): 2020/148/12:13:24
000
Vector Time (MET): N/A
Weight (LBS)     : 953907
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         251524
14                 A    =         6803096
90  meter
 Y    =        6784787
01  meter          E    =           
0012691
 Z    =        -309656
41                 I    =           52
05143
 XDOT =      -4703
414238                 Wp   =           36
96813
 YDOT =        443
375401  meter/sec      RA   =           89
91521  deg
 ZDOT =       6032
082295                 TA   =          319
71962
                                          MA   =          319
81358
                                          Ha   =            228
529  n
mi
                                          Hp   =            222
181

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         825210
44                 X    =          177140
08
 Y    =       22259799
89  feet           Y    =         6787183
87  meter
 Z    =       -1015933
11                 Z    =         -308614
18
 XDOT =     -15431
149076                 XDOT =       -4737
323010
 YDOT =       1454
643705  feet/sec       YDOT =         390
587913  meter/sec
 ZDOT =      19790
296244                 ZDOT =        6009
152672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20945544
48                 X    =         6384201
96
 Y    =        7581079
66  feet           Y    =         2310713
08  meter
 Z    =       -1011524
16                 Z    =         -308312
57
 XDOT =      -3938
345258                 XDOT =       -1200
407635
 YDOT =      13447
015885  feet/sec       YDOT =        4098
650442  meter/sec
 ZDOT =      19684
747180                 ZDOT =        5999
910941


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   20148
50990252  
00016717  00000-0  10270-3 0  9037
2 25544  51
6417  90
8191 0001788 354
3512   5
7618 15
49390270 28806


Satellite: ISS
Catalog Number: 25544
Epoch time:      20148
50990252   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:        90
8191  deg
Eccentricity:     
0001788     
Arg of perigee:   354
3512  deg
Mean anomaly:       5
7618  deg
Mean motion:   15
49390270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2880
Checksum:              307


Coasting Arc #5 (Orbit 2885)
---------------------------------------

Vector Time (GMT): 2020/148/20:33:33
000
Vector Time (MET): N/A
Weight (LBS)     : 953907
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3083515
96                 A    =         6797274
51  meter
 Y    =       -4746944
28  meter          E    =           
0011636
 Z    =        3755767
29                 I    =           52
03018
 XDOT =       3184
651135                 Wp   =           76
55949
 YDOT =      -5483
136797  meter/sec      RA   =           88
17932  deg
 ZDOT =      -4301
754022                 TA   =           58
90773
                                          MA   =           58
79359
                                          Ha   =            228
524  n
mi
                                          Hp   =            222
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10116522
17                 X    =        -3048448
38
 Y    =      -15573964
18  feet           Y    =        -4781230
86  meter
 Z    =       12322071
15                 Z    =         3740873
23
 XDOT =      10448
330497                 XDOT =        3266
623933
 YDOT =     -17989
293953  feet/sec       YDOT =       -5447
064755  meter/sec
 ZDOT =     -14113
366215                 ZDOT =       -4286
086011

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13518508
89                 X    =         4120441
51
 Y    =       12799223
14  feet           Y    =         3901203
21  meter
 Z    =       12253800
35                 Z    =         3734958
35
 XDOT =      -5174
880094                 XDOT =       -1577
303453
 YDOT =      18951
894138  feet/sec       YDOT =        5776
537333  meter/sec
 ZDOT =     -14040
942766                 ZDOT =       -4279
679355


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   20148
89689468  
00016717  00000-0  10270-3 0  9044
2 25544  51
6400  88
9000 0001552 350
3688   9
7432 15
49384063 28861


Satellite: ISS
Catalog Number: 25544
Epoch time:      20148
89689468   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:        88
9000  deg
Eccentricity:     
0001552     
Arg of perigee:   350
3688  deg
Mean anomaly:       9
7432  deg
Mean motion:   15
49384063  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2886
Checksum:              329


Coasting Arc #6 (Orbit 2890)
---------------------------------------

Vector Time (GMT): 2020/149/04:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 953907
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3424456
97                 A    =         6794135
53  meter
 Y    =       -3586466
27  meter          E    =           
0010891
 Z    =       -4655231
62                 I    =           52
02236
 XDOT =       2731
266477                 Wp   =           62
15332
 YDOT =       6490
755674  meter/sec      RA   =           86
54889  deg
 ZDOT =      -2991
826359                 TA   =          178
10843
                                          MA   =          178
10431
                                          Ha   =            228
556  n
mi
                                          Hp   =            222
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11235095
06                 X    =         3486919
79
 Y    =      -11766621
63  feet           Y    =        -3547821
61  meter
 Z    =      -15273069
62                 Z    =        -4638445
81
 XDOT =       8960
848023                 XDOT =        2673
014472
 YDOT =      21295
130164  feet/sec       YDOT =        6520
973378  meter/sec
 ZDOT =      -9815
703276                 ZDOT =       -2978
699479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16324519
36                 X    =         4975713
50
 Y    =        -742272
37  feet           Y    =         -226244
62  meter
 Z    =      -15195607
94                 Z    =        -4631621
30
 XDOT =      -8148
749160                 XDOT =       -2483
738744
 YDOT =      20475
963468  feet/sec       YDOT =        6241
073665  meter/sec
 ZDOT =      -9755
668588                 ZDOT =       -2973
527786


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   20149
21938957  
00016717  00000-0  10270-3 0  9052
2 25544  51
6431  87
3066 0001595 359
6128    
5021 15
49383675 28915


Satellite: ISS
Catalog Number: 25544
Epoch time:      20149
21938957   =   yrday
fracday
Element set:     905
Inclination:       51
6431  deg
RA of node:        87
3066  deg
Eccentricity:     
0001595     
Arg of perigee:   359
6128  deg
Mean anomaly:        
5021  deg
Mean motion:   15
49383675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2891
Checksum:              321


Coasting Arc #7 (Orbit 2897)
---------------------------------------

Vector Time (GMT): 2020/149/15:39:55
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3952090
34                 A    =         6791572
19  meter
 Y    =       -1734265
44  meter          E    =           
0014449
 Z    =       -5256571
32                 I    =           52
01410
 XDOT =       1662
795802                 Wp   =           73
23091
 YDOT =       7373
070355  meter/sec      RA   =           84
29978  deg
 ZDOT =      -1181
030567                 TA   =          185
46516
                                          MA   =          185
48094
                                          Ha   =            228
516  n
mi
                                          Hp   =            222
244

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12966175
67                 X    =         3996723
02
 Y    =       -5689847
24  feet           Y    =        -1689820
06  meter
 Z    =      -17245968
90                 Z    =        -5237265
51
 XDOT =       5455
366804                 XDOT =        1585
961111
 YDOT =      24189
863369  feet/sec       YDOT =        7391
235476  meter/sec
 ZDOT =      -3874
772201                 ZDOT =       -1173
138962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11575416
21                 X    =        -3528186
86
 Y    =       -8340630
30  feet           Y    =        -2542224
11  meter
 Z    =      -17157014
37                 Z    =        -5229457
98
 XDOT =      17387
365052                 XDOT =        5299
668868
 YDOT =     -16224
786995  feet/sec       YDOT =       -4945
315076  meter/sec
 ZDOT =      -3838
887915                 ZDOT =       -1170
093037


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   20149
67088053  
00016717  00000-0  10270-3 0  9066
2 25544  51
6442  85
0740 0001957 356
7746   3
3392 15
49414510 28989


Satellite: ISS
Catalog Number: 25544
Epoch time:      20149
67088053   =   yrday
fracday
Element set:     906
Inclination:       51
6442  deg
RA of node:        85
0740  deg
Eccentricity:     
0001957     
Arg of perigee:   356
7746  deg
Mean anomaly:       3
3392  deg
Mean motion:   15
49414510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2898
Checksum:              319


Coasting Arc #8 (Orbit 2913)
---------------------------------------

Vector Time (GMT): 2020/150/15:39:55
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3833331
39                 A    =         6791512
11  meter
 Y    =        1899084
64  meter          E    =           
0003154
 Z    =        5272106
00                 I    =           52
00853
 XDOT =      -2183
876654                 Wp   =           90
85231
 YDOT =      -7272
857605  meter/sec      RA   =           79
37532  deg
 ZDOT =       1031
315979                 TA   =          349
31227
                                          MA   =          349
31897
                                          Ha   =            228
761  n
mi
                                          Hp   =            222
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12576546
55                 X    =        -3879891
42
 Y    =        6230592
64  feet           Y    =         1855956
64  meter
 Z    =       17296935
71                 Z    =         5253372
37
 XDOT =      -7164
949653                 XDOT =       -2107
396620
 YDOT =     -23861
081382  feet/sec       YDOT =       -7296
851764  meter/sec
 ZDOT =       3383
582607                 ZDOT =        1020
892477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11972657
45                 X    =         3649265
99
 Y    =        7524927
84  feet           Y    =         2293598
01  meter
 Z    =       17210599
27                 Z    =         5245790
66
 XDOT =     -15974
229044                 XDOT =       -4868
945013
 YDOT =      17781
672720  feet/sec       YDOT =        5419
853845  meter/sec
 ZDOT =       3336
050235                 ZDOT =        1016
828112


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   20150
70286133  
00016717  00000-0  10270-3 0  9072
2 25544  51
6435  79
9662 0001894   2
3710 357
7449 15
49392457 29144


Satellite: ISS
Catalog Number: 25544
Epoch time:      20150
70286133   =   yrday
fracday
Element set:     907
Inclination:       51
6435  deg
RA of node:        79
9662  deg
Eccentricity:     
0001894     
Arg of perigee:     2
3710  deg
Mean anomaly:     357
7449  deg
Mean motion:   15
49392457  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2914
Checksum:              320


Coasting Arc #9 (Orbit 2928)
---------------------------------------

Vector Time (GMT): 2020/151/15:39:55
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3725093
87                 A    =         6791367
59  meter
 Y    =       -2065957
70  meter          E    =           
0014870
 Z    =       -5302329
77                 I    =           52
00036
 XDOT =       2689
744462                 Wp   =           75
69881
 YDOT =       7107
262304  meter/sec      RA   =           74
45019  deg
 ZDOT =       -878
060369                 TA   =          185
91686
                                          MA   =          185
93444
                                          Ha   =            228
581  n
mi
                                          Hp   =            222
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12221436
60                 X    =         3773674
85
 Y    =       -6778076
44  feet           Y    =        -2024028
87  meter
 Z    =      -17396095
05                 Z    =        -5284116
94
 XDOT =       8824
620939                 XDOT =        2614
334151
 YDOT =      23317
789711  feet/sec       YDOT =        7136
919385  meter/sec
 ZDOT =      -2880
775488                 ZDOT =        -865
177081

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12369678
90                 X    =        -3770278
13
 Y    =       -6723894
36  feet           Y    =        -2049443
00  meter
 Z    =      -17312141
52                 Z    =        -5276740
74
 XDOT =      14357
603851                 XDOT =        4376
197654
 YDOT =     -19134
660074  feet/sec       YDOT =       -5832
244391  meter/sec
 ZDOT =      -2821
923849                 ZDOT =        -860
122389


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   20151
67034205  
00016717  00000-0  10270-3 0  9081
2 25544  51
6430  75
1776 0001969   1
9303 358
1854 15
49413342 29297


Satellite: ISS
Catalog Number: 25544
Epoch time:      20151
67034205   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:        75
1776  deg
Eccentricity:     
0001969     
Arg of perigee:     1
9303  deg
Mean anomaly:     358
1854  deg
Mean motion:   15
49413342  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2929
Checksum:              302


Coasting Arc #10 (Orbit 2942)
---------------------------------------

Vector Time (GMT): 2020/152/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3942327
12                 A    =         6791047
42  meter
 Y    =        1391871
96  meter          E    =           
0003231
 Z    =        5349372
14                 I    =           51
99118
 XDOT =      -2583
917138                 Wp   =           51
65637
 YDOT =      -7214
389109  meter/sec      RA   =           70
14733  deg
 ZDOT =        -25
172616                 TA   =           38
59405
                                          MA   =           38
57096
                                          Ha   =            228
716  n
mi
                                          Hp   =            221
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12934144
10                 X    =        -3983582
72
 Y    =        4566509
06  feet           Y    =         1347554
88  meter
 Z    =       17550433
52                 Z    =         5330121
72
 XDOT =      -8477
418432                 XDOT =       -2502
929379
 YDOT =     -23669
255606  feet/sec       YDOT =       -7242
831477  meter/sec
 ZDOT =        -82
587323                 ZDOT =         -37
528286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1650666
96                 X    =          503123
29
 Y    =       13730460
88  feet           Y    =         4185044
48  meter
 Z    =       17461745
26                 Z    =         5322339
96
 XDOT =     -23937
793464                 XDOT =       -7296
239448
 YDOT =       3062
766006  feet/sec       YDOT =         933
531079  meter/sec
 ZDOT =       -138
991037                 ZDOT =         -42
364468


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   20152
57332332  
00016717  00000-0  10270-3 0  9094
2 25544  51
6434  70
7082 0001915   3
9610 356
1555 15
49434558 29430


Satellite: ISS
Catalog Number: 25544
Epoch time:      20152
57332332   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:        70
7082  deg
Eccentricity:     
0001915     
Arg of perigee:     3
9610  deg
Mean anomaly:     356
1555  deg
Mean motion:   15
49434558  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2943
Checksum:              298


Coasting Arc #11 (Orbit 2957)
---------------------------------------

Vector Time (GMT): 2020/153/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3885946
87                 A    =         6791126
99  meter
 Y    =       -1572988
27  meter          E    =           
0015324
 Z    =       -5355806
04                 I    =           51
97990
 XDOT =       3077
685885                 Wp   =           83
84458
 YDOT =       7000
873640  meter/sec      RA   =           65
22082  deg
 ZDOT =        178
933036                 TA   =          187
84489
                                          MA   =          187
86889
                                          Ha   =            228
711  n
mi
                                          Hp   =            222
038

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12749169
53                 X    =         3929263
33
 Y    =       -5160722
67  feet           Y    =        -1529290
13  meter
 Z    =      -17571542
11                 Z    =        -5336824
42
 XDOT =      10097
394637                 XDOT =        2998
302135
 YDOT =      22968
745538  feet/sec       YDOT =        7034
846636  meter/sec
 ZDOT =        587
050644                 ZDOT =         193
691209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2505678
05                 X    =         -763730
67
 Y    =      -13636790
95  feet           Y    =        -4156493
88  meter
 Z    =      -17484078
02                 Z    =        -5329146
98
 XDOT =      23520
373777                 XDOT =        7169
009927
 YDOT =      -5152
285385  feet/sec       YDOT =       -1570
416585  meter/sec
 ZDOT =        654
508009                 ZDOT =         199
494041


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   20153
54080201  
00016717  00000-0  10270-3 0  9109
2 25544  51
6446  65
9195 0002034  12
2919 347
8281 15
49415880 29588


Satellite: ISS
Catalog Number: 25544
Epoch time:      20153
54080201   =   yrday
fracday
Element set:     910
Inclination:       51
6446  deg
RA of node:        65
9195  deg
Eccentricity:     
0002034     
Arg of perigee:    12
2919  deg
Mean anomaly:     347
8281  deg
Mean motion:   15
49415880  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2958
Checksum:              301


Coasting Arc #12 (Orbit 2973)
---------------------------------------

Vector Time (GMT): 2020/154/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3817524
40                 A    =         6791078
99  meter
 Y    =        1736794
88  meter          E    =           
0003967
 Z    =        5338849
60                 I    =           51
96452
 XDOT =      -3561
240704                 Wp   =           47
38391
 YDOT =      -6777
156614  meter/sec      RA   =           60
29411  deg
 ZDOT =       -338
984404                 TA   =           45
85191
                                          MA   =           45
81929
                                          Ha   =            228
816  n
mi
                                          Hp   =            221
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12524686
34                 X    =        -3862595
40
 Y    =        5698145
94  feet           Y    =         1693852
01  meter
 Z    =       17515910
77                 Z    =         5320196
06
 XDOT =     -11683
860576                 XDOT =       -3483
545234
 YDOT =     -22234
765795  feet/sec       YDOT =       -6816
546483  meter/sec
 ZDOT =      -1112
153556                 ZDOT =        -356
095762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3309189
57                 X    =         1008640
98
 Y    =       13468113
97  feet           Y    =         4105081
14  meter
 Z    =       17429943
65                 Z    =         5312646
82
 XDOT =     -23002
860688                 XDOT =       -7011
271938
 YDOT =       7204
381325  feet/sec       YDOT =        2195
895428  meter/sec
 ZDOT =      -1190
436204                 ZDOT =        -362
844955


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   20154
57277630  
00016717  00000-0  10270-3 0  9118
2 25544  51
6443  60
8122 0001995  12
6931 347
4269 15
49438452 29742


Satellite: ISS
Catalog Number: 25544
Epoch time:      20154
57277630   =   yrday
fracday
Element set:     911
Inclination:       51
6443  deg
RA of node:        60
8122  deg
Eccentricity:     
0001995     
Arg of perigee:    12
6931  deg
Mean anomaly:     347
4269  deg
Mean motion:   15
49438452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2974
Checksum:              314


Coasting Arc #13 (Orbit 2988)
---------------------------------------

Vector Time (GMT): 2020/155/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3752880
36                 A    =         6791189
45  meter
 Y    =       -1918724
59  meter          E    =           
0015220
 Z    =       -5337941
63                 I    =           51
94747
 XDOT =       4016
024688                 Wp   =           86
26773
 YDOT =       6492
048964  meter/sec      RA   =           55
36645  deg
 ZDOT =        492
099615                 TA   =          188
40545
                                          MA   =          188
43097
                                          Ha   =            228
735  n
mi
                                          Hp   =            221
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12312599
60                 X    =         3799986
21
 Y    =       -6295028
17  feet           Y    =        -1876493
10  meter
 Z    =      -17512931
84                 Z    =        -5319597
19
 XDOT =      13175
934017                 XDOT =        3940
739817
 YDOT =      21299
373240  feet/sec       YDOT =        6536
538000  meter/sec
 ZDOT =       1614
500048                 ZDOT =         511
426182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4164024
01                 X    =        -1269194
52
 Y    =      -13298234
84  feet           Y    =        -4053301
98  meter
 Z    =      -17428371
24                 Z    =        -5312167
56
 XDOT =      22206
027415                 XDOT =        6768
397156
 YDOT =      -9175
786450  feet/sec       YDOT =       -2796
779710  meter/sec
 ZDOT =       1702
977018                 ZDOT =         519
067395


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   20155
54025356  
00016717  00000-0  10270-3 0  9123
2 25544  51
6448  56
0244 0002017  15
3179 344
8032 15
49420344 29895


Satellite: ISS
Catalog Number: 25544
Epoch time:      20155
54025356   =   yrday
fracday
Element set:     912
Inclination:       51
6448  deg
RA of node:        56
0244  deg
Eccentricity:     
0002017     
Arg of perigee:    15
3179  deg
Mean anomaly:     344
8032  deg
Mean motion:   15
49420344  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2989
Checksum:              292


Coasting Arc #14 (Orbit 3004)
---------------------------------------

Vector Time (GMT): 2020/156/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3679011
95                 A    =         6791177
98  meter
 Y    =        2080987
82  meter          E    =           
0004608
 Z    =        5313011
36                 I    =           51
92842
 XDOT =      -4456
970395                 Wp   =           44
58426
 YDOT =      -6199
559359  meter/sec      RA   =           50
43717  deg
 ZDOT =       -654
476607                 TA   =           51
66437
                                          MA   =           51
62297
                                          Ha   =            228
833  n
mi
                                          Hp   =            221
825

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12070249
18                 X    =        -3727816
65
 Y    =        6827387
87  feet           Y    =         2039572
75  meter
 Z    =       17431139
63                 Z    =         5295021
72
 XDOT =     -14622
606284                 XDOT =       -4384
134714
 YDOT =     -20339
761677  feet/sec       YDOT =       -6248
993018  meter/sec
 ZDOT =      -2147
232961                 ZDOT =        -675
951216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4954534
95                 X    =         1510142
25
 Y    =       13062981
02  feet           Y    =         3981596
61  meter
 Z    =       17348195
29                 Z    =         5287729
92
 XDOT =     -21320
609679                 XDOT =       -6498
521830
 YDOT =      11084
232419  feet/sec       YDOT =        3378
474041  meter/sec
 ZDOT =      -2245
597850                 ZDOT =        -684
458225


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   20156
57222510  
00016717  00000-0  10270-3 0  9139
2 25544  51
6456  50
9169 0001990  15
7573 344
3639 15
49442796 30057


Satellite: ISS
Catalog Number: 25544
Epoch time:      20156
57222510   =   yrday
fracday
Element set:     913
Inclination:       51
6456  deg
RA of node:        50
9169  deg
Eccentricity:     
0001990     
Arg of perigee:    15
7573  deg
Mean anomaly:     344
3639  deg
Mean motion:   15
49442796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3005
Checksum:              310


Coasting Arc #15 (Orbit 3019)
---------------------------------------

Vector Time (GMT): 2020/157/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3605128
07                 A    =         6791315
14  meter
 Y    =       -2264003
83  meter          E    =           
0015131
 Z    =       -5304440
68                 I    =           51
90597
 XDOT =       4860
536062                 Wp   =           88
27934
 YDOT =       5851
447704  meter/sec      RA   =           45
50628  deg
 ZDOT =        808
391358                 TA   =          189
42330
                                          MA   =          189
45172
                                          Ha   =            228
808  n
mi
                                          Hp   =            221
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11827847
99                 X    =         3655943
08
 Y    =       -7427834
07  feet           Y    =        -2223403
60  meter
 Z    =      -17403020
60                 Z    =        -5286805
20
 XDOT =      15946
640624                 XDOT =        4790
815448
 YDOT =      19197
663071  feet/sec       YDOT =        5905
411694  meter/sec
 ZDOT =       2652
202618                 ZDOT =         831
833936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5805483
09                 X    =        -1769511
24
 Y    =      -12813717
94  feet           Y    =        -3905621
23  meter
 Z    =      -17321686
74                 Z    =        -5279650
12
 XDOT =      20178
737011                 XDOT =        6150
479041
 YDOT =     -12861
988900  feet/sec       YDOT =       -3920
334217  meter/sec
 ZDOT =       2759
635004                 ZDOT =         841
136749


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   20157
53969837  
00016717  00000-0  10270-3 0  9147
2 25544  51
6453  46
1285 0002133  20
6040 339
5196 15
49426741 30207


Satellite: ISS
Catalog Number: 25544
Epoch time:      20157
53969837   =   yrday
fracday
Element set:     914
Inclination:       51
6453  deg
RA of node:        46
1285  deg
Eccentricity:     
0002133     
Arg of perigee:    20
6040  deg
Mean anomaly:     339
5196  deg
Mean motion:   15
49426741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3020
Checksum:              298


Coasting Arc #16 (Orbit 3035)
---------------------------------------

Vector Time (GMT): 2020/158/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3524345
89                 A    =         6791375
54  meter
 Y    =        2426894
50  meter          E    =           
0005472
 Z    =        5270911
24                 I    =           51
88111
 XDOT =      -5248
194455                 Wp   =           44
97962
 YDOT =      -5499
066676  meter/sec      RA   =           40
57412  deg
 ZDOT =       -972
825434                 TA   =           54
33134
                                          MA   =           54
28041
                                          Ha   =            228
933  n
mi
                                          Hp   =            221
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11562814
60                 X    =        -3576825
40
 Y    =        7962252
28  feet           Y    =         2387188
25  meter
 Z    =       17293015
87                 Z    =         5253664
28
 XDOT =     -17218
485745                 XDOT =       -5181
586749
 YDOT =     -18041
557336  feet/sec       YDOT =       -5557
383097  meter/sec
 ZDOT =      -3191
684495                 ZDOT =        -998
158578

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6586160
78                 X    =         2007461
81
 Y    =       12508561
02  feet           Y    =         3812609
40  meter
 Z    =       17213451
95                 Z    =         5246660
16
 XDOT =     -18964
656344                 XDOT =       -5780
427254
 YDOT =      14557
420570  feet/sec       YDOT =        4437
101790  meter/sec
 ZDOT =      -3307
833379                 ZDOT =       -1008
227614


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   20158
57166748  
00016717  00000-0  10270-3 0  9153
2 25544  51
6445  41
0211 0002083  23
3917 336
7327 15
49437661 30363


Satellite: ISS
Catalog Number: 25544
Epoch time:      20158
57166748   =   yrday
fracday
Element set:     915
Inclination:       51
6445  deg
RA of node:        41
0211  deg
Eccentricity:     
0002083     
Arg of perigee:    23
3917  deg
Mean anomaly:     336
7327  deg
Mean motion:   15
49437661  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3036
Checksum:              300


Coasting Arc #17 (Orbit 3050)
---------------------------------------

Vector Time (GMT): 2020/159/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3437294
31                 A    =         6791528
11  meter
 Y    =       -2613757
43  meter          E    =           
0014880
 Z    =       -5254844
43                 I    =           51
85456
 XDOT =       5592
244878                 Wp   =           90
72103
 YDOT =       5097
019119  meter/sec      RA   =           35
63977  deg
 ZDOT =       1125
312688                 TA   =          190
04471
                                          MA   =          190
07448
                                          Ha   =            228
854  n
mi
                                          Hp   =            221
822

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11277212
31                 X    =         3491791
67
 Y    =       -8575319
64  feet           Y    =        -2575013
36  meter
 Z    =      -17240303
25                 Z    =        -5238015
58
 XDOT =      18347
260099                 XDOT =        5529
366749
 YDOT =      16722
503672  feet/sec       YDOT =        5159
203776  meter/sec
 ZDOT =       3691
970762                 ZDOT =        1152
325946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7438121
30                 X    =        -2267139
37
 Y    =      -12167895
01  feet           Y    =        -3708774
40  meter
 Z    =      -17162644
41                 Z    =        -5231174
02
 XDOT =      17523
468607                 XDOT =        5341
153231
 YDOT =     -16082
209945  feet/sec       YDOT =       -4901
857591  meter/sec
 ZDOT =       3815
875793                 ZDOT =        1163
078942


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   20159
53913921  
00016717  00000-0  10270-3 0  9164
2 25544  51
6439  36
2325 0002106  25
7314 334
3941 15
49426941 30513


Satellite: ISS
Catalog Number: 25544
Epoch time:      20159
53913921   =   yrday
fracday
Element set:     916
Inclination:       51
6439  deg
RA of node:        36
2325  deg
Eccentricity:     
0002106     
Arg of perigee:    25
7314  deg
Mean anomaly:     334
3941  deg
Mean motion:   15
49426941  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3051
Checksum:              291


Coasting Arc #18 (Orbit 3061)
---------------------------------------

Vector Time (GMT): 2020/160/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2842517
57                 A    =         6791281
17  meter
 Y    =        3137908
83  meter          E    =           
0004951
 Z    =        5306871
95                 I    =           51
83185
 XDOT =      -6171
099180                 Wp   =           51
01506
 YDOT =      -4498
843242  meter/sec      RA   =           32
30485  deg
 ZDOT =       -641
856605                 TA   =           45
12019
                                          MA   =           45
08000
                                          Ha   =            229
058  n
mi
                                          Hp   =            221
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9325845
04                 X    =        -2903172
98
 Y    =       10294976
46  feet           Y    =         3105781
56  meter
 Z    =       17410997
20                 Z    =         5292917
47
 XDOT =     -20246
388385                 XDOT =       -6117
215371
 YDOT =     -14759
984389  feet/sec       YDOT =       -4567
551452  meter/sec
 ZDOT =      -2105
828757                 ZDOT =        -671
703309

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13422958
21                 X    =        -4091317
66
 Y    =        3875966
42  feet           Y    =         1181394
56  meter
 Z    =       17346522
04                 Z    =         5287219
92
 XDOT =      -9310
304367                 XDOT =       -2837
780771
 YDOT =     -22154
558397  feet/sec       YDOT =       -6752
709399  meter/sec
 ZDOT =      -2242
818002                 ZDOT =        -683
610927


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   20160
24861767  
00016717  00000-0  10270-3 0  9175
2 25544  51
6409  32
7196 0002088  33
6699 326
4584 15
49407739 30621


Satellite: ISS
Catalog Number: 25544
Epoch time:      20160
24861767   =   yrday
fracday
Element set:     917
Inclination:       51
6409  deg
RA of node:        32
7196  deg
Eccentricity:     
0002088     
Arg of perigee:    33
6699  deg
Mean anomaly:     326
4584  deg
Mean motion:   15
49407739  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3062
Checksum:              330


Coasting Arc #19 (Orbit 3076)
---------------------------------------

Vector Time (GMT): 2020/161/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980162
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2718185
57                 A    =         6791403
09  meter
 Y    =       -3287201
38  meter          E    =           
0015683
 Z    =       -5298311
04                 I    =           51
80358
 XDOT =       6443
644369                 Wp   =           89
07041
 YDOT =       4043
601805  meter/sec      RA   =           27
36740  deg
 ZDOT =        799
320456                 TA   =          188
55721
                                          MA   =          188
58398
                                          Ha   =            229
023  n
mi
                                          Hp   =            221
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8917931
66                 X    =         2780477
97
 Y    =      -10784781
43  feet           Y    =        -3256455
41  meter
 Z    =      -17382910
24                 Z    =        -5284956
57
 XDOT =      21140
565514                 XDOT =        6394
066098
 YDOT =      13266
410123  feet/sec       YDOT =        4115
381865  meter/sec
 ZDOT =       2622
442442                 ZDOT =         830
501260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13249941
89                 X    =         4038582
29
 Y    =       -4735212
94  feet           Y    =        -1443292
90  meter
 Z    =      -17321183
05                 Z    =        -5279496
59
 XDOT =      11167
812292                 XDOT =        3403
949187
 YDOT =      21160
662797  feet/sec       YDOT =        6449
770021  meter/sec
 ZDOT =       2765
603024                 ZDOT =         842
955802


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   20161
21608553  
00016717  00000-0  10270-3 0  9186
2 25544  51
6415  27
9310 0002203  36
5304 323
5996 15
49397635 30770


Satellite: ISS
Catalog Number: 25544
Epoch time:      20161
21608553   =   yrday
fracday
Element set:     918
Inclination:       51
6415  deg
RA of node:        27
9310  deg
Eccentricity:     
0002203     
Arg of perigee:    36
5304  deg
Mean anomaly:     323
5996  deg
Mean motion:   15
49397635  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3077
Checksum:              300
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