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

 
Date: November 12th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


314/21:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 215 7

322/07:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 216 8

322/20:20:13 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 217 1

324/22:00:36 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 217 3

326/13:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 217 4

328/20:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 217 7

Coasting Arc #1 (Orbit 2758)
---------------------------------------

Vector Time (GMT): 2016/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3092465
82                 A    =         6790087
85  meter
 Y    =        5875558
36  meter          E    =           
0010607
 Z    =        1412762
69                 I    =           51
95833
 XDOT =      -4853
205060                 Wp   =           91
25838
 YDOT =       1145
976076  meter/sec      RA   =           52
65728  deg
 ZDOT =       5819
522908                 TA   =          284
06424
                                          MA   =          284
18212
                                          Ha   =            222
899  n
mi
                                          Hp   =            215
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10145885
22                 X    =         3019671
28
 Y    =       19276766
26  feet           Y    =         5909733
42  meter
 Z    =        4635048
19                 Z    =         1427608
30
 XDOT =     -15922
588779                 XDOT =       -4893
928123
 YDOT =       3759
764030  feet/sec       YDOT =        1091
476812  meter/sec
 ZDOT =      19092
922926                 ZDOT =        5795
847935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21116301
13                 X    =        -6436248
59
 Y    =       -5295095
51  feet           Y    =        -1613945
11  meter
 Z    =        4698953
74                 Z    =         1432241
10
 XDOT =       7496
164397                 XDOT =        2284
830908
 YDOT =     -12933
999721  feet/sec       YDOT =       -3942
283115  meter/sec
 ZDOT =      18989
004327                 ZDOT =        5787
848519


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   16314
56153551  
00016717  00000-0  10270-3 0  9003
2 25544  51
6431  53
0198 0007169 192
3487 167
7491 15
53568793 27595


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
56153551   =   yrday
fracday
Element set:     900
Inclination:       51
6431  deg
RA of node:        53
0198  deg
Eccentricity:     
0007169     
Arg of perigee:   192
3487  deg
Mean anomaly:     167
7491  deg
Mean motion:   15
53568793  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2759
Checksum:              332


Coasting Arc #2 (Orbit 2764)
---------------------------------------

Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5356296
95                 A    =         6787748
97  meter
 Y    =       -3077932
12  meter          E    =           
0014626
 Z    =        2790023
97                 I    =           51
94020
 XDOT =        566
116835                 Wp   =          127
43651
 YDOT =      -5661
398690  meter/sec      RA   =           50
59173  deg
 ZDOT =      -5148
998043                 TA   =           21
04629
                                          MA   =           20
98616
                                          Ha   =            222
797  n
mi
                                          Hp   =            215
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17573152
73                 X    =        -5335033
59
 Y    =      -10098202
50  feet           Y    =        -3137710
82  meter
 Z    =        9153621
94                 Z    =         2764055
78
 XDOT =       1857
338696                 XDOT =         654
393990
 YDOT =     -18574
142684  feet/sec       YDOT =       -5654
574630  meter/sec
 ZDOT =     -16893
038199                 ZDOT =       -5146
033279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19743943
54                 X    =        -6017953
99
 Y    =       -4798418
74  feet           Y    =        -1462558
03  meter
 Z    =        9040467
71                 Z    =         2755534
56
 XDOT =      -3623
971706                 XDOT =       -1104
586576
 YDOT =     -16950
575352  feet/sec       YDOT =       -5166
535367  meter/sec
 ZDOT =     -16878
969499                 ZDOT =       -5144
709903


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   16314
94748814  
00016717  00000-0  10270-3 0  9018
2 25544  51
6410  51
1000 0006644 194
4954 165
6009 15
53564963 27656


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
94748814   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:        51
1000  deg
Eccentricity:     
0006644     
Arg of perigee:   194
4954  deg
Mean anomaly:     165
6009  deg
Mean motion:   15
53564963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2765
Checksum:              308


Coasting Arc #3 (Orbit 2779)
---------------------------------------

Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5362433
42                 A    =         6790166
91  meter
 Y    =        3927135
71  meter          E    =           
0003341
 Z    =       -1389237
39                 I    =           51
92749
 XDOT =      -1871
711961                 Wp   =           78
12062
 YDOT =       4611
891593  meter/sec      RA   =           45
64007  deg
 ZDOT =       5824
741400                 TA   =          266
81598
                                          MA   =          266
85421
                                          Ha   =            222
534  n
mi
                                          Hp   =            215
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17593285
49                 X    =         5324869
08
 Y    =       12884303
51  feet           Y    =         3986891
94  meter
 Z    =       -4557865
45                 Z    =        -1363278
96
 XDOT =      -6140
787274                 XDOT =       -1951
438843
 YDOT =      15130
877930  feet/sec       YDOT =        4590
515360  meter/sec
 ZDOT =      19110
043963                 ZDOT =        5815
455036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20634814
87                 X    =         6289491
57
 Y    =        7123913
72  feet           Y    =         2171368
90  meter
 Z    =       -4444927
18                 Z    =        -1354813
80
 XDOT =      -1011
590854                 XDOT =        -308
332892
 YDOT =      14801
582309  feet/sec       YDOT =        4511
522288  meter/sec
 ZDOT =      19068
482138                 ZDOT =        5812
073356


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   16315
91236307  
00016717  00000-0  10270-3 0  9026
2 25544  51
6413  46
2943 0006566 198
2712 161
8205 15
53570735 27804


Satellite: ISS
Catalog Number: 25544
Epoch time:      16315
91236307   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:        46
2943  deg
Eccentricity:     
0006566     
Arg of perigee:   198
2712  deg
Mean anomaly:     161
8205  deg
Mean motion:   15
53570735  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2780
Checksum:              304


Coasting Arc #4 (Orbit 2795)
---------------------------------------

Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5062098
79                 A    =         6790937
83  meter
 Y    =       -4509682
98  meter          E    =           
0015577
 Z    =        -151758
12                 I    =           51
90742
 XDOT =       3246
664739                 Wp   =          158
15448
 YDOT =      -3448
398253  meter/sec      RA   =           40
69152  deg
 ZDOT =      -6035
867107                 TA   =           23
47497
                                          MA   =           23
40394
                                          Ha   =            222
404  n
mi
                                          Hp   =            216
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16607935
65                 X    =        -5010556
94
 Y    =      -14795547
85  feet           Y    =        -4566002
59  meter
 Z    =        -497894
10                 Z    =         -176223
72
 XDOT =      10651
787202                 XDOT =        3314
304646
 YDOT =     -11313
642562  feet/sec       YDOT =       -3411
713939  meter/sec
 ZDOT =     -19802
713607                 ZDOT =       -6019
930804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20380877
00                 X    =        -6212091
31
 Y    =       -8901376
00  feet           Y    =        -2713139
40  meter
 Z    =        -604168
54                 Z    =         -184150
57
 XDOT =       6079
501709                 XDOT =        1853
032121
 YDOT =     -12619
506324  feet/sec       YDOT =       -3846
425528  meter/sec
 ZDOT =     -19732
248126                 ZDOT =       -6014
389229


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   16316
94155882  
00016717  00000-0  10270-3 0  9039
2 25544  51
6419  41
1683 0006523 202
1018 157
9854 15
53571885 27962


Satellite: ISS
Catalog Number: 25544
Epoch time:      16316
94155882   =   yrday
fracday
Element set:     903
Inclination:       51
6419  deg
RA of node:        41
1683  deg
Eccentricity:     
0006523     
Arg of perigee:   202
1018  deg
Mean anomaly:     157
9854  deg
Mean motion:   15
53571885  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2796
Checksum:              325


Coasting Arc #5 (Orbit 2811)
---------------------------------------

Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4478672
54                 A    =         6789689
22  meter
 Y    =        4823894
37  meter          E    =           
0009630
 Z    =        1655762
36                 I    =           51
87849
 XDOT =      -4561
193263                 Wp   =           88
45722
 YDOT =       2257
942478  meter/sec      RA   =           35
74109  deg
 ZDOT =       5730
795887                 TA   =          289
60700
                                          MA   =          289
71093
                                          Ha   =            222
229  n
mi
                                          Hp   =            216
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14693807
56                 X    =         4416354
45
 Y    =       15826425
11  feet           Y    =         4873629
50  meter
 Z    =        5432291
21                 Z    =         1677367
72
 XDOT =     -14964
544826                 XDOT =       -4613
941649
 YDOT =       7407
947762  feet/sec       YDOT =        2206
641380  meter/sec
 ZDOT =      18801
823775                 ZDOT =        5708
509962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19029384
46                 X    =         5800156
38
 Y    =       10160696
41  feet           Y    =         3096980
26  meter
 Z    =        5525963
78                 Z    =         1684313
76
 XDOT =     -11091
022428                 XDOT =       -3380
543636
 YDOT =      10549
580163  feet/sec       YDOT =        3215
512034  meter/sec
 ZDOT =      18703
781510                 ZDOT =        5700
912604


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   16317
97074930  
00016717  00000-0  10270-3 0  9048
2 25544  51
6419  36
0428 0006565 206
5273 153
5544 15
53591667 28126


Satellite: ISS
Catalog Number: 25544
Epoch time:      16317
97074930   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:        36
0428  deg
Eccentricity:     
0006565     
Arg of perigee:   206
5273  deg
Mean anomaly:     153
5544  deg
Mean motion:   15
53591667  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2812
Checksum:              318


Coasting Arc #6 (Orbit 2826)
---------------------------------------

Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3555518
02                 A    =         6786835
86  meter
 Y    =       -4906728
48  meter          E    =           
0006931
 Z    =       -3049206
11                 I    =           51
84377
 XDOT =       5752
816358                 Wp   =          170
67361
 YDOT =      -1098
530680  meter/sec      RA   =           30
78339  deg
 ZDOT =      -4948
555705                 TA   =           44
19184
                                          MA   =           44
13650
                                          Ha   =            221
991  n
mi
                                          Hp   =            216
331

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11665085
38                 X    =        -3485573
32
 Y    =      -16098190
54  feet           Y    =        -4946097
59  meter
 Z    =      -10003957
04                 Z    =        -3066308
52
 XDOT =      18874
069415                 XDOT =        5788
711491
 YDOT =      -3604
103281  feet/sec       YDOT =       -1033
998138  meter/sec
 ZDOT =     -16235
418980                 ZDOT =       -4920
521964

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16422432
34                 X    =        -5005557
38
 Y    =      -11137556
35  feet           Y    =        -3394727
18  meter
 Z    =      -10077880
08                 Z    =        -3071737
85
 XDOT =      15774
989693                 XDOT =        4808
216858
 YDOT =      -8705
217875  feet/sec       YDOT =       -2653
350408  meter/sec
 ZDOT =     -16112
435285                 ZDOT =       -4911
070275


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   16318
93560984  
00016717  00000-0  10270-3 0  9055
2 25544  51
6432  31
2371 0006419 210
4666 149
6114 15
53609569 28279


Satellite: ISS
Catalog Number: 25544
Epoch time:      16318
93560984   =   yrday
fracday
Element set:     905
Inclination:       51
6432  deg
RA of node:        31
2371  deg
Eccentricity:     
0006419     
Arg of perigee:   210
4666  deg
Mean anomaly:     149
6114  deg
Mean motion:   15
53609569  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2827
Checksum:              318


Coasting Arc #7 (Orbit 2842)
---------------------------------------

Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2385892
88                 A    =         6783445
80  meter
 Y    =        4793914
39  meter          E    =           
0010206
 Z    =        4164131
74                 I    =           51
80369
 XDOT =      -6681
776300                 Wp   =          140
78429
 YDOT =         51
152519  meter/sec      RA   =           25
81654  deg
 ZDOT =       3756
776900                 TA   =          270
57825
                                          MA   =          270
69520
                                          Ha   =            221
882  n
mi
                                          Hp   =            216
494

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7827732
54                 X    =         2311880
66
 Y    =       15728065
58  feet           Y    =         4820181
12  meter
 Z    =       13661849
54                 Z    =         4175542
48
 XDOT =     -21921
838256                 XDOT =       -6700
101002
 YDOT =        167
823224  feet/sec       YDOT =         -23
670141  meter/sec
 ZDOT =      12325
383529                 ZDOT =        3724
273093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12875735
71                 X    =         3924524
24
 Y    =       11896190
44  feet           Y    =         3625958
85  meter
 Z    =       13710859
19                 Z    =         4179069
88
 XDOT =     -19602
548545                 XDOT =       -5974
856796
 YDOT =       7127
166167  feet/sec       YDOT =        2172
360248  meter/sec
 ZDOT =      12183
036035                 ZDOT =        3713
389384


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   16319
96478918  
00016717  00000-0  10270-3 0  9065
2 25544  51
6427  26
1116 0006400 213
7720 146
3025 15
53608101 28434


Satellite: ISS
Catalog Number: 25544
Epoch time:      16319
96478918   =   yrday
fracday
Element set:     906
Inclination:       51
6427  deg
RA of node:        26
1116  deg
Eccentricity:     
0006400     
Arg of perigee:   213
7720  deg
Mean anomaly:     146
3025  deg
Mean motion:   15
53608101  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2843
Checksum:              293


Coasting Arc #8 (Orbit 2857)
---------------------------------------

Vector Time (GMT): 2016/320/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -966066
24                 A    =         6780377
93  meter
 Y    =       -4540035
15  meter          E    =           
0008193
 Z    =       -4948918
49                 I    =           51
76456
 XDOT =       7274
986256                 Wp   =          100
80636
 YDOT =        884
154972  meter/sec      RA   =           20
83893  deg
 ZDOT =      -2235
876372                 TA   =          147
41001
                                          MA   =          147
35941
                                          Ha   =            221
709  n
mi
                                          Hp   =            216
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3169508
68                 X    =         -891186
32
 Y    =      -14895128
46  feet           Y    =        -4550419
45  meter
 Z    =      -16236609
21                 Z    =        -4953429
84
 XDOT =      23868
065143                 XDOT =        7275
419894
 YDOT =       2900
770904  feet/sec       YDOT =         965
511278  meter/sec
 ZDOT =      -7335
552401                 ZDOT =       -2200
534370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8433003
74                 X    =        -2570379
54
 Y    =      -12656340
10  feet           Y    =        -3857652
46  meter
 Z    =      -16255448
90                 Z    =        -4954660
83
 XDOT =      22331
459309                 XDOT =        6806
628797
 YDOT =      -5676
091019  feet/sec       YDOT =       -1730
072543  meter/sec
 ZDOT =      -7180
967140                 ZDOT =       -2188
758784


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   16320
92964074  
00016717  00000-0  10270-3 0  9077
2 25544  51
6431  21
3060 0006340 217
7527 142
3182 15
53632349 28583


Satellite: ISS
Catalog Number: 25544
Epoch time:      16320
92964074   =   yrday
fracday
Element set:     907
Inclination:       51
6431  deg
RA of node:        21
3060  deg
Eccentricity:     
0006340     
Arg of perigee:   217
7527  deg
Mean anomaly:     142
3182  deg
Mean motion:   15
53632349  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2858
Checksum:              294


Coasting Arc #9 (Orbit 2873)
---------------------------------------

Vector Time (GMT): 2016/321/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -553255
77                 A    =         6778804
54  meter
 Y    =        4190737
20  meter          E    =           
0006063
 Z    =        5301421
25                 I    =           51
72890
 XDOT =      -7461
484400                 Wp   =          197
26108
 YDOT =      -1675
708118  meter/sec      RA   =           15
85380  deg
 ZDOT =        540
460645                 TA   =          247
55498
                                          MA   =          247
61920
                                          Ha   =            221
508  n
mi
                                          Hp   =            216
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1815143
60                 X    =         -625829
04
 Y    =       13749137
80  feet           Y    =         4184144
24  meter
 Z    =       17393114
34                 Z    =         5298557
58
 XDOT =     -24479
935695                 XDOT =       -7444
817019
 YDOT =      -5497
730046  feet/sec       YDOT =       -1759
054282  meter/sec
 ZDOT =       1773
164846                 ZDOT =         504
254336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3607114
83                 X    =         1099448
60
 Y    =       13408499
84  feet           Y    =         4086910
75  meter
 Z    =       17379724
32                 Z    =         5297339
97
 XDOT =     -23711
332531                 XDOT =       -7227
214156
 YDOT =       4262
101763  feet/sec       YDOT =        1299
088617  meter/sec
 ZDOT =       1614
957601                 ZDOT =         492
239077


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   16321
95880930  
00016717  00000-0  10270-3 0  9080
2 25544  51
6430  16
1801 0006512 222
8367 137
2279 15
53656483 28740


Satellite: ISS
Catalog Number: 25544
Epoch time:      16321
95880930   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:        16
1801  deg
Eccentricity:     
0006512     
Arg of perigee:   222
8367  deg
Mean anomaly:     137
2279  deg
Mean motion:   15
53656483  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2874
Checksum:              314


Coasting Arc #10 (Orbit 2879)
---------------------------------------

Vector Time (GMT): 2016/322/07:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4574517
27                 A    =         6782847
74  meter
 Y    =        2426477
73  meter          E    =           
0005247
 Z    =        4375570
95                 I    =           51
72907
 XDOT =      -5474
045053                 Wp   =          113
81757
 YDOT =      -4136
622545  meter/sec      RA   =           13
86534  deg
 ZDOT =      -3427
790625                 TA   =           10
88648
                                          MA   =           10
87512
                                          Ha   =            221
873  n
mi
                                          Hp   =            216
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15008258
76                 X    =        -4622565
76
 Y    =        7960884
93  feet           Y    =         2375053
50  meter
 Z    =       14355547
74                 Z    =         4353232
15
 XDOT =     -17959
465397                 XDOT =       -5410
730433
 YDOT =     -13571
596277  feet/sec       YDOT =       -4197
482784  meter/sec
 ZDOT =     -11246
032235                 ZDOT =       -3454
229054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16652126
76                 X    =         5075568
24
 Y    =       -3760748
92  feet           Y    =        -1146276
27  meter
 Z    =       14257233
69                 Z    =         4345604
83
 XDOT =      13466
494589                 XDOT =        4104
587551
 YDOT =      16543
089289  feet/sec       YDOT =        5042
333615  meter/sec
 ZDOT =     -11360
965123                 ZDOT =       -3462
822169


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   16322
34474799  
00016717  00000-0  10270-3 0  9097
2 25544  51
6426  14
2527 0006776 219
9846 140
0808 15
53601903 28804


Satellite: ISS
Catalog Number: 25544
Epoch time:      16322
34474799   =   yrday
fracday
Element set:     909
Inclination:       51
6426  deg
RA of node:        14
2527  deg
Eccentricity:     
0006776     
Arg of perigee:   219
9846  deg
Mean anomaly:     140
0808  deg
Mean motion:   15
53601903  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2880
Checksum:              325


Coasting Arc #11 (Orbit 2887)
---------------------------------------

Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3322861
32                 A    =         6780645
34  meter
 Y    =       -3298718
45  meter          E    =           
0010508
 Z    =       -4913389
32                 I    =           51
70461
 XDOT =       6578
538727                 Wp   =          138
27664
 YDOT =       3165
082913  meter/sec      RA   =           11
16525  deg
 ZDOT =       2319
226648                 TA   =          154
44198
                                          MA   =          154
39000
                                          Ha   =            221
405  n
mi
                                          Hp   =            217
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10901775
99                 X    =         3383368
93
 Y    =      -10822567
08  feet           Y    =        -3261221
40  meter
 Z    =      -16120043
71                 Z    =        -4897100
68
 XDOT =      21583
132308                 XDOT =        6531
391068
 YDOT =      10384
130292  feet/sec       YDOT =        3238
384805  meter/sec
 ZDOT =       7609
011312                 ZDOT =        2351
069639

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10715785
73                 X    =         3266171
49
 Y    =      -11111465
37  feet           Y    =        -3386774
64  meter
 Z    =      -16048045
39                 Z    =        -4891444
23
 XDOT =      20990
335834                 XDOT =        6397
854362
 YDOT =       9030
029545  feet/sec       YDOT =        2752
353005  meter/sec
 ZDOT =       7747
806397                 ZDOT =        2361
531390


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   16322
85932908  
00016717  00000-0  10270-3 0  9106
2 25544  51
6423  11
6933 0006293 225
8448 134
2188 15
53634216 28888


Satellite: ISS
Catalog Number: 25544
Epoch time:      16322
85932908   =   yrday
fracday
Element set:     910
Inclination:       51
6423  deg
RA of node:        11
6933  deg
Eccentricity:     
0006293     
Arg of perigee:   225
8448  deg
Mean anomaly:     134
2188  deg
Mean motion:   15
53634216  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2888
Checksum:              318


Coasting Arc #12 (Orbit 2903)
---------------------------------------

Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4634083
24                 A    =         6783735
06  meter
 Y    =        2762230
68  meter          E    =           
0005840
 Z    =        4106670
76                 I    =           51
68276
 XDOT =      -5562
012801                 Wp   =          107
02577
 YDOT =      -3641
977387  meter/sec      RA   =            6
18282  deg
 ZDOT =      -3823
842562                 TA   =           22
44112
                                          MA   =           22
41558
                                          Ha   =            221
342  n
mi
                                          Hp   =            217
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15203685
18                 X    =        -4684575
43
 Y    =        9062436
61  feet           Y    =         2710126
76  meter
 Z    =       13473329
27                 Z    =         4084036
80
 XDOT =     -18248
073494                 XDOT =       -5502
299131
 YDOT =     -11948
744707  feet/sec       YDOT =       -3703
841505  meter/sec
 ZDOT =     -12545
415230                 ZDOT =       -3850
716816

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14880494
78                 X    =        -4535574
81
 Y    =        9722479
99  feet           Y    =         2963411
90  meter
 Z    =       13373655
45                 Z    =         4076290
18
 XDOT =     -17961
699594                 XDOT =       -5474
726036
 YDOT =     -10060
429210  feet/sec       YDOT =       -3066
418823  meter/sec
 ZDOT =     -12662
352736                 ZDOT =       -3859
485114


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   16323
88849050  
00016717  00000-0  10270-3 0  9116
2 25544  51
6420   6
5680 0006301 229
6913 130
3689 15
53628304 29049


Satellite: ISS
Catalog Number: 25544
Epoch time:      16323
88849050   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:         6
5680  deg
Eccentricity:     
0006301     
Arg of perigee:   229
6913  deg
Mean anomaly:     130
3689  deg
Mean motion:   15
53628304  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2904
Checksum:              299


Coasting Arc #13 (Orbit 2918)
---------------------------------------

Vector Time (GMT): 2016/324/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5692823
48                 A    =         6787117
16  meter
 Y    =       -2219012
29  meter          E    =           
0002100
 Z    =       -2956727
36                 I    =           51
66268
 XDOT =       4172
524736                 Wp   =          206
74526
 YDOT =       4040
919877  meter/sec      RA   =            1
20471  deg
 ZDOT =       4997
785362                 TA   =          119
52064
                                          MA   =          119
49969
                                          Ha   =            221
044  n
mi
                                          Hp   =            217
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18677242
39                 X    =         5731576
56
 Y    =       -7280224
05  feet           Y    =        -2155134
55  meter
 Z    =       -9700549
08                 Z    =        -2928978
76
 XDOT =      13689
385617                 XDOT =        4102
750743
 YDOT =      13257
611145  feet/sec       YDOT =        4087
189586  meter/sec
 ZDOT =      16396
933603                 ZDOT =        5017
885240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18262129
15                 X    =         5566296
96
 Y    =       -8407549
07  feet           Y    =        -2562620
96  meter
 Z    =       -9578593
62                 Z    =        -2919555
33
 XDOT =      13751
102352                 XDOT =        4191
335997
 YDOT =      11076
634680  feet/sec       YDOT =        3376
158250  meter/sec
 ZDOT =      16484
123783                 ZDOT =        5024
360929


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   16324
85332567  
00016717  00000-0  10270-3 0  9125
2 25544  51
6426   1
7614 0006365 233
6946 126
3619 15
53647171 29197


Satellite: ISS
Catalog Number: 25544
Epoch time:      16324
85332567   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:         1
7614  deg
Eccentricity:     
0006365     
Arg of perigee:   233
6946  deg
Mean anomaly:     126
3619  deg
Mean motion:   15
53647171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2919
Checksum:              316


Coasting Arc #14 (Orbit 2919)
---------------------------------------

Vector Time (GMT): 2016/324/22:00:36
000
Vector Time (MET): N/A
Weight (LBS)     : 909067
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6777399
98                 A    =         6790673
68  meter
 Y    =        -161055
21  meter          E    =           
0005359
 Z    =        -335186
95                 I    =           51
67373
 XDOT =        407
505531                 Wp   =           28
62011
 YDOT =       4750
800519  meter/sec      RA   =             
87864  deg
 ZDOT =       6001
277912                 TA   =          327
77085
                                          MA   =          327
80359
                                          Ha   =            221
003  n
mi
                                          Hp   =            217
310

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22235564
26                 X    =         6780325
44
 Y    =        -528396
36  feet           Y    =          -85249
41  meter
 Z    =       -1099694
73                 Z    =         -302256
68
 XDOT =       1336
960402                 XDOT =         325
198725
 YDOT =      15586
615877  feet/sec       YDOT =        4754
897160  meter/sec
 ZDOT =      19689
231996                 ZDOT =        6003
057696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19265227
85                 X    =         5872041
45
 Y    =      -11128653
28  feet           Y    =        -3392013
52  meter
 Z    =        -955469
02                 Z    =         -291226
96
 XDOT =       7724
154480                 XDOT =        2354
322285
 YDOT =      11694
910930  feet/sec       YDOT =        3564
608851  meter/sec
 ZDOT =      19696
058786                 ZDOT =        6003
358718


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   16324
91764714  
00016717  00000-0  10270-3 0  9136
2 25544  51
6438   1
4416 0006438 234
7466 125
3085 15
53652230 29207


Satellite: ISS
Catalog Number: 25544
Epoch time:      16324
91764714   =   yrday
fracday
Element set:     913
Inclination:       51
6438  deg
RA of node:         1
4416  deg
Eccentricity:     
0006438     
Arg of perigee:   234
7466  deg
Mean anomaly:     125
3085  deg
Mean motion:   15
53652230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2920
Checksum:              297


Coasting Arc #15 (Orbit 2935)
---------------------------------------

Vector Time (GMT): 2016/325/22:00:36
000
Vector Time (MET): N/A
Weight (LBS)     : 909067
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6653478
02                 A    =         6790145
18  meter
 Y    =        -495440
66  meter          E    =           
0010564
 Z    =       -1223637
95                 I    =           51
63996
 XDOT =       1427
875754                 Wp   =          179
49046
 YDOT =      -4746
248771  meter/sec      RA   =          355
91236  deg
 ZDOT =      -5853
005840                 TA   =           13
80991
                                          MA   =           13
78104
                                          Ha   =            220
876  n
mi
                                          Hp   =            217
499

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21828996
12                 X    =        -6641499
42
 Y    =       -1625461
49  feet           Y    =         -569777
33  meter
 Z    =       -4014560
20                 Z    =        -1255930
04
 XDOT =       4684
631739                 XDOT =        1509
274998
 YDOT =     -15571
682319  feet/sec       YDOT =       -4729
826110  meter/sec
 ZDOT =     -19202
775064                 ZDOT =       -5845
871866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19754101
07                 X    =        -6021050
01
 Y    =        9368472
50  feet           Y    =         2855510
42  meter
 Z    =       -4155851
77                 Z    =        -1266703
62
 XDOT =      -2838
224640                 XDOT =        -865
090870
 YDOT =     -14473
606757  feet/sec       YDOT =       -4411
555340  meter/sec
 ZDOT =     -19170
575207                 ZDOT =       -5843
191323


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   16325
94680042  
00016717  00000-0  10270-3 0  9142
2 25544  51
6444 356
3157 0006499 237
8600 122
1922 15
53614239 29368


Satellite: ISS
Catalog Number: 25544
Epoch time:      16325
94680042   =   yrday
fracday
Element set:     914
Inclination:       51
6444  deg
RA of node:       356
3157  deg
Eccentricity:     
0006499     
Arg of perigee:   237
8600  deg
Mean anomaly:     122
1922  deg
Mean motion:   15
53614239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2936
Checksum:              314


Coasting Arc #16 (Orbit 2945)
---------------------------------------

Vector Time (GMT): 2016/326/13:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6425298
09                 A    =         6790119
97  meter
 Y    =        1796294
05  meter          E    =           
0012266
 Z    =        1219583
51                 I    =           51
61680
 XDOT =      -2336
780443                 Wp   =          148
24915
 YDOT =      -4374
172953  meter/sec      RA   =          352
70644  deg
 ZDOT =      -5851
995584                 TA   =           18
48913
                                          MA   =           18
44459
                                          Ha   =            220
821  n
mi
                                          Hp   =            217
385

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21080374
30                 X    =        -6450831
42
 Y    =        5893353
19  feet           Y    =         1724299
28  meter
 Z    =        4001258
22                 Z    =         1188308
74
 XDOT =      -7666
602502                 XDOT =       -2259
266936
 YDOT =     -14350
961133  feet/sec       YDOT =       -4399
870976  meter/sec
 ZDOT =     -19199
460577                 ZDOT =       -5863
158917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2183652
80                 X    =         -665577
37
 Y    =      -21804250
12  feet           Y    =        -6645935
44  meter
 Z    =        3863961
29                 Z    =         1177735
40
 XDOT =      13844
228690                 XDOT =        4219
720905
 YDOT =      -4807
318002  feet/sec       YDOT =       -1465
270527  meter/sec
 ZDOT =     -19247
451365                 ZDOT =       -5866
623176


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   16326
59001795  
00016717  00000-0  10270-3 0  9157
2 25544  51
6416 353
1103 0006133 238
6444 121
4109 15
53655336 29466


Satellite: ISS
Catalog Number: 25544
Epoch time:      16326
59001795   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       353
1103  deg
Eccentricity:     
0006133     
Arg of perigee:   238
6444  deg
Mean anomaly:     121
4109  deg
Mean motion:   15
53655336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2946
Checksum:              297


Coasting Arc #17 (Orbit 2961)
---------------------------------------

Vector Time (GMT): 2016/327/13:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6674442
52                 A    =         6790520
48  meter
 Y    =       -1184829
27  meter          E    =           
0006698
 Z    =         327754
93                 I    =           51
58601
 XDOT =        545
331884                 Wp   =           36
63925
 YDOT =       4746
413581  meter/sec      RA   =          347
73655  deg
 ZDOT =       5994
969983                 TA   =          326
89442
                                          MA   =          326
93633
                                          Ha   =            220
607  n
mi
                                          Hp   =            217
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21897777
30                 X    =         6685603
42
 Y    =       -3887235
15  feet           Y    =        -1110128
77  meter
 Z    =        1075311
44                 Z    =          360205
15
 XDOT =       1789
146600                 XDOT =         463
094459
 YDOT =      15572
223035  feet/sec       YDOT =        4752
052053  meter/sec
 ZDOT =      19668
536689                 ZDOT =        5997
419332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         454623
09                 X    =          138569
12
 Y    =       22228141
13  feet           Y    =         6775137
42  meter
 Z    =        1217621
67                 Z    =          371131
08
 XDOT =     -14022
703850                 XDOT =       -4274
120133
 YDOT =       -800
356474  feet/sec       YDOT =        -243
948653  meter/sec
 ZDOT =      19678
300616                 ZDOT =        5997
946028


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   16327
61916337  
00016717  00000-0  10270-3 0  9169
2 25544  51
6409 347
9844 0006357 241
9595 118
0915 15
53698461 29624


Satellite: ISS
Catalog Number: 25544
Epoch time:      16327
61916337   =   yrday
fracday
Element set:     916
Inclination:       51
6409  deg
RA of node:       347
9844  deg
Eccentricity:     
0006357     
Arg of perigee:   241
9595  deg
Mean anomaly:     118
0915  deg
Mean motion:   15
53698461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2962
Checksum:              347


Coasting Arc #18 (Orbit 2976)
---------------------------------------

Vector Time (GMT): 2016/328/13:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6506671
04                 A    =         6789162
40  meter
 Y    =         472097
30  meter          E    =           
0007955
 Z    =       -1860495
06                 I    =           51
54941
 XDOT =       1239
928595                 Wp   =          188
24116
 YDOT =      -5061
566706  meter/sec      RA   =          342
76217  deg
 ZDOT =      -5625
459283                 TA   =           12
25799
                                          MA   =           12
23865
                                          Ha   =            220
303  n
mi
                                          Hp   =            217
541

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21347345
94                 X    =        -6502428
96
 Y    =        1548875
66  feet           Y    =          399359
04  meter
 Z    =       -6103986
42                 Z    =        -1892092
95
 XDOT =       4068
007202                 XDOT =        1323
762590
 YDOT =     -16606
189979  feet/sec       YDOT =       -5047
232277  meter/sec
 ZDOT =     -18456
231245                 ZDOT =       -5619
232291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1399392
20                 X    =          426534
74
 Y    =      -21317618
16  feet           Y    =        -6497610
01  meter
 Z    =       -6242411
59                 Z    =        -1902687
05
 XDOT =      14318
853738                 XDOT =        4364
386619
 YDOT =       6331
759646  feet/sec       YDOT =        1929
920340  meter/sec
 ZDOT =     -18427
949644                 ZDOT =       -5616
839051


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   16328
58398768  
00016717  00000-0  10270-3 0  9179
2 25544  51
6404 343
1779 0006146 247
0059 113
0446 15
53657894 29777


Satellite: ISS
Catalog Number: 25544
Epoch time:      16328
58398768   =   yrday
fracday
Element set:     917
Inclination:       51
6404  deg
RA of node:       343
1779  deg
Eccentricity:     
0006146     
Arg of perigee:   247
0059  deg
Mean anomaly:     113
0446  deg
Mean motion:   15
53657894  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2977
Checksum:              350


Coasting Arc #19 (Orbit 2980)
---------------------------------------

Vector Time (GMT): 2016/328/20:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4480772
27                 A    =         6786747
82  meter
 Y    =       -4078073
52  meter          E    =           
0001823
 Z    =       -3057496
36                 I    =           51
53628
 XDOT =       5426
818507                 Wp   =          247
44272
 YDOT =       2281
126346  meter/sec      RA   =          341
32770  deg
 ZDOT =       4907
440261                 TA   =           77
43068
                                          MA   =           77
41029
                                          Ha   =            220
219  n
mi
                                          Hp   =            217
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14700696
42                 X    =         4540893
51
 Y    =      -13379506
31  feet           Y    =        -4027630
37  meter
 Z    =      -10031156
03                 Z    =        -3035583
54
 XDOT =      17804
522662                 XDOT =        5377
068473
 YDOT =       7484
010323  feet/sec       YDOT =        2341
534531  meter/sec
 ZDOT =      16100
525791                 ZDOT =        4933
681903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14047729
97                 X    =         4281748
09
 Y    =      -14132042
58  feet           Y    =        -4307446
58  meter
 Z    =       -9934405
40                 Z    =        -3028006
77
 XDOT =      17035
429379                 XDOT =        5192
398875
 YDOT =       5528
121026  feet/sec       YDOT =        1684
971289  meter/sec
 ZDOT =      16214
945012                 ZDOT =        4942
315240


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   16328
84127326  
00016717  00000-0  10270-3 0  9189
2 25544  51
6440 341
8972 0006341 250
0136 110
0334 15
53679988 29810


Satellite: ISS
Catalog Number: 25544
Epoch time:      16328
84127326   =   yrday
fracday
Element set:     918
Inclination:       51
6440  deg
RA of node:       341
8972  deg
Eccentricity:     
0006341     
Arg of perigee:   250
0136  deg
Mean anomaly:     110
0334  deg
Mean motion:   15
53679988  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2981
Checksum:              313
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