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

 
Date: March 14th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 76 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 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


077/03:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 215 2

078/21:26:42 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 215 0

079/03:11:47 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 215 1

080/10:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 215 0

083/03:23:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 214 8

084/04:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 214 6

Coasting Arc #1 (Orbit 3024)
---------------------------------------

Vector Time (GMT): 2016/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4756709
42                 A    =         6784816
77  meter
 Y    =        3555240
71  meter          E    =           
0003065
 Z    =       -3282803
11                 I    =           51
71104
 XDOT =      -5344
345613                 Wp   =           70
73067
 YDOT =      -2779
818145  meter/sec      RA   =          169
09944  deg
 ZDOT =       4737
922949                 TA   =          251
21672
                                          MA   =          251
24998
                                          Ha   =            220
407  n
mi
                                          Hp   =            215
332

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15606002
04                 X    =        -4780165
06
 Y    =       11664175
54  feet           Y    =         3501916
55  meter
 Z    =      -10770351
39                 Z    =        -3305967
29
 XDOT =     -17533
942299                 XDOT =       -5335
878544
 YDOT =      -9120
138272  feet/sec       YDOT =       -2839
534354  meter/sec
 ZDOT =      15544
366629                 ZDOT =        4711
982346

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17059362
08                 X    =        -5199693
56
 Y    =        9294627
00  feet           Y    =         2833002
31  meter
 Z    =      -10871468
81                 Z    =        -3313623
69
 XDOT =     -15452
198010                 XDOT =       -4709
829954
 YDOT =     -10328
184872  feet/sec       YDOT =       -3148
030749  meter/sec
 ZDOT =      15432
179684                 ZDOT =        4703
728368


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   16074
50688678  
00016717  00000-0  10270-3 0  9003
2 25544  51
6428 170
2249 0001909 290
1223  69
9724 15
54079183 30251


Satellite: ISS
Catalog Number: 25544
Epoch time:      16074
50688678   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:       170
2249  deg
Eccentricity:     
0001909     
Arg of perigee:   290
1223  deg
Mean anomaly:      69
9724  deg
Mean motion:   15
54079183  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3025
Checksum:              318


Coasting Arc #2 (Orbit 3040)
---------------------------------------

Vector Time (GMT): 2016/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5769203
92                 A    =         6788015
33  meter
 Y    =       -3093511
79  meter          E    =           
0012203
 Z    =        1773413
53                 I    =           51
75230
 XDOT =       3686
220829                 Wp   =          114
88570
 YDOT =       3605
005731  meter/sec      RA   =          164
12956  deg
 ZDOT =      -5677
787982                 TA   =           45
66636
                                          MA   =           45
56640
                                          Ha   =            220
447  n
mi
                                          Hp   =            215
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18927834
39                 X    =         5794753
12
 Y    =      -10149316
90  feet           Y    =        -3028853
70  meter
 Z    =        5818285
86                 Z    =         1801501
09
 XDOT =      12093
900356                 XDOT =        3673
214917
 YDOT =      11827
446623  feet/sec       YDOT =        3646
154258  meter/sec
 ZDOT =     -18627
913326                 ZDOT =       -5659
913248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20030039
22                 X    =         6105155
95
 Y    =       -7656978
79  feet           Y    =        -2333847
13  meter
 Z    =        5940724
16                 Z    =         1810732
72
 XDOT =      10047
220759                 XDOT =        3062
392887
 YDOT =      11826
119660  feet/sec       YDOT =        3604
601272  meter/sec
 ZDOT =     -18550
863683                 ZDOT =       -5654
303250


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   16075
53573899  
00016717  00000-0  10270-3 0  9016
2 25544  51
6420 165
0969 0001749 292
9264  67
1704 15
54103050 30418


Satellite: ISS
Catalog Number: 25544
Epoch time:      16075
53573899   =   yrday
fracday
Element set:     901
Inclination:       51
6420  deg
RA of node:       165
0969  deg
Eccentricity:     
0001749     
Arg of perigee:   292
9264  deg
Mean anomaly:      67
1704  deg
Mean motion:   15
54103050  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3041
Checksum:              308


Coasting Arc #3 (Orbit 3055)
---------------------------------------

Vector Time (GMT): 2016/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6310809
99                 A    =         6789367
86  meter
 Y    =        2484644
25  meter          E    =           
0011591
 Z    =         -98867
47                 I    =           51
78807
 XDOT =      -1814
942806                 Wp   =           35
38343
 YDOT =      -4384
475964  meter/sec      RA   =          159
16737  deg
 ZDOT =       6025
074913                 TA   =          323
55364
                                          MA   =          323
63249
                                          Ha   =            220
459  n
mi
                                          Hp   =            215
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20704757
18                 X    =        -6337644
61
 Y    =        8151719
97  feet           Y    =         2413922
53  meter
 Z    =        -324368
34                 Z    =         -129588
97
 XDOT =      -5954
536765                 XDOT =       -1795
046612
 YDOT =     -14384
763661  feet/sec       YDOT =       -4404
660054  meter/sec
 ZDOT =      19767
306145                 ZDOT =        6016
307176

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21475904
06                 X    =        -6545855
56
 Y    =        5815354
74  feet           Y    =         1772520
13  meter
 Z    =        -458167
29                 Z    =         -139649
39
 XDOT =      -4031
669341                 XDOT =       -1228
852815
 YDOT =     -13400
619602  feet/sec       YDOT =       -4084
508855  meter/sec
 ZDOT =      19729
917693                 ZDOT =        6013
678913


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   16076
50027161  
00016717  00000-0  10270-3 0  9021
2 25544  51
6427 160
2888 0001936 302
5119  57
5846 15
54112176 30562


Satellite: ISS
Catalog Number: 25544
Epoch time:      16076
50027161   =   yrday
fracday
Element set:     902
Inclination:       51
6427  deg
RA of node:       160
2888  deg
Eccentricity:     
0001936     
Arg of perigee:   302
5119  deg
Mean anomaly:      57
5846  deg
Mean motion:   15
54112176  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3056
Checksum:              297


Coasting Arc #4 (Orbit 3066)
---------------------------------------

Vector Time (GMT): 2016/077/03:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2211787
17                 A    =         6781195
25  meter
 Y    =       -4726814
15  meter          E    =           
0008694
 Z    =        4326441
15                 I    =           51
77981
 XDOT =       6819
173226                 Wp   =           59
02017
 YDOT =        -30
454927  meter/sec      RA   =          155
83308  deg
 ZDOT =      -3509
820000                 TA   =           66
65214
                                          MA   =           66
56069
                                          Ha   =            220
352  n
mi
                                          Hp   =            215
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7256519
57                 X    =         2243463
40
 Y    =      -15507920
44  feet           Y    =        -4701902
94  meter
 Z    =       14194360
72                 Z    =         4337262
75
 XDOT =      22372
615571                 XDOT =        6836
055998
 YDOT =        -99
917739  feet/sec       YDOT =          45
895653  meter/sec
 ZDOT =     -11515
157480                 ZDOT =       -3476
653478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8317980
75                 X    =         2535320
53
 Y    =       14919998
41  feet           Y    =         4547615
51  meter
 Z    =       14242099
31                 Z    =         4340991
87
 XDOT =     -12042
923070                 XDOT =       -3670
682952
 YDOT =      17598
383687  feet/sec       YDOT =        5363
987348  meter/sec
 ZDOT =     -11371
112553                 ZDOT =       -3465
915106


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   16077
20758532  
00016717  00000-0  10270-3 0  9033
2 25544  51
6412 156
7633 0002285 311
0063  49
0892 15
54176111 30673


Satellite: ISS
Catalog Number: 25544
Epoch time:      16077
20758532   =   yrday
fracday
Element set:     903
Inclination:       51
6412  deg
RA of node:       156
7633  deg
Eccentricity:     
0002285     
Arg of perigee:   311
0063  deg
Mean anomaly:      49
0892  deg
Mean motion:   15
54176111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3067
Checksum:              290


Coasting Arc #5 (Orbit 3081)
---------------------------------------

Vector Time (GMT): 2016/078/03:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3612911
71                 A    =         6785019
55  meter
 Y    =        4822269
36  meter          E    =           
0003880
 Z    =       -3118737
68                 I    =           51
81959
 XDOT =      -5784
851971                 Wp   =           50
13826
 YDOT =      -1176
391644  meter/sec      RA   =          150
85836  deg
 ZDOT =       4888
968172                 TA   =          274
07553
                                          MA   =          274
11988
                                          Ha   =            220
472  n
mi
                                          Hp   =            215
077

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11853384
87                 X    =        -3651417
69
 Y    =       15821093
70  feet           Y    =         4781651
74  meter
 Z    =      -10232078
99                 Z    =        -3136382
14
 XDOT =     -18979
173133                 XDOT =       -5795
015553
 YDOT =      -3859
552637  feet/sec       YDOT =       -1241
137997  meter/sec
 ZDOT =      16039
921825                 ZDOT =        4860
842584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6173874
51                 X    =        -1881796
95
 Y    =      -18737747
52  feet           Y    =        -5711265
45  meter
 Z    =      -10309474
78                 Z    =        -3142327
91
 XDOT =      12756
317894                 XDOT =        3888
125694
 YDOT =     -12949
523647  feet/sec       YDOT =       -3947
014808  meter/sec
 ZDOT =      15917
944372                 ZDOT =        4851
789445


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   16078
17209663  
00016717  00000-0  10270-3 0  9047
2 25544  51
6394 151
9546 0002062 315
4376  44
6611 15
54170069 30823


Satellite: ISS
Catalog Number: 25544
Epoch time:      16078
17209663   =   yrday
fracday
Element set:     904
Inclination:       51
6394  deg
RA of node:       151
9546  deg
Eccentricity:     
0002062     
Arg of perigee:   315
4376  deg
Mean anomaly:      44
6611  deg
Mean motion:   15
54170069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3082
Checksum:              304


Coasting Arc #6 (Orbit 3093)
---------------------------------------

Vector Time (GMT): 2016/078/21:26:42
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3249256
58                 A    =         6777496
85  meter
 Y    =       -2810773
10  meter          E    =           
0001855
 Z    =        5240318
77                 I    =           51
81704
 XDOT =       5889
440548                 Wp   =          104
97962
 YDOT =      -4793
841731  meter/sec      RA   =          147
27521  deg
 ZDOT =       1079
663644                 TA   =          334
69993
                                          MA   =          334
70901
                                          Ha   =            220
561  n
mi
                                          Hp   =            215
026

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10660290
62                 X    =        -3243039
23
 Y    =       -9221696
53  feet           Y    =        -2847073
06  meter
 Z    =       17192646
87                 Z    =         5224550
32
 XDOT =      19322
311508                 XDOT =        5937
364286
 YDOT =     -15727
827201  feet/sec       YDOT =       -4727
714006  meter/sec
 ZDOT =       3542
203555                 ZDOT =        1108
389690

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1759289
38                 X    =          536231
40
 Y    =       14068466
62  feet           Y    =         4288068
63  meter
 Z    =       17124594
51                 Z    =         5219576
41
 XDOT =     -23832
999328                 XDOT =       -7264
298195
 YDOT =      -1487
279410  feet/sec       YDOT =        -453
322764  meter/sec
 ZDOT =       3667
738326                 ZDOT =        1117
926642


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   16078
94369747  
00016717  00000-0  10270-3 0  9053
2 25544  51
6415 148
1109 0002180 319
5852  40
5138 15
54218754 30941


Satellite: ISS
Catalog Number: 25544
Epoch time:      16078
94369747   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       148
1109  deg
Eccentricity:     
0002180     
Arg of perigee:   319
5852  deg
Mean anomaly:      40
5138  deg
Mean motion:   15
54218754  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3094
Checksum:              318


Coasting Arc #7 (Orbit 3096)
---------------------------------------

Vector Time (GMT): 2016/079/03:11:47
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4581031
74                 A    =         6787871
69  meter
 Y    =        4702021
93  meter          E    =           
0008215
 Z    =       -1710003
16                 I    =           51
85674
 XDOT =      -4540
789296                 Wp   =           23
35293
 YDOT =      -2352
231554  meter/sec      RA   =          146
05730  deg
 ZDOT =       5713
356792                 TA   =          317
95307
                                          MA   =          318
01609
                                          Ha   =            220
458  n
mi
                                          Hp   =            215
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15029631
69                 X    =        -4624964
09
 Y    =       15426581
13  feet           Y    =         4650547
93  meter
 Z    =       -5610246
59                 Z    =        -1732363
68
 XDOT =     -14897
602676                 XDOT =       -4541
901267
 YDOT =      -7717
295126  feet/sec       YDOT =       -2403
015190  meter/sec
 ZDOT =      18744
608896                 ZDOT =        5691
296637

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          -5757
63                 X    =           -1754
92
 Y    =      -21511890
74  feet           Y    =        -6556824
30  meter
 Z    =       -5708119
19                 Z    =        -1739834
73
 XDOT =      14576
786386                 XDOT =        4443
004490
 YDOT =      -4938
089191  feet/sec       YDOT =       -1505
129585  meter/sec
 ZDOT =      18649
152239                 ZDOT =        5684
261602


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   16079
13659593  
00016717  00000-0  10270-3 0  9067
2 25544  51
6403 147
1476 0002196 318
1509  41
9475 15
54187173 30977


Satellite: ISS
Catalog Number: 25544
Epoch time:      16079
13659593   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       147
1476  deg
Eccentricity:     
0002196     
Arg of perigee:   318
1509  deg
Mean anomaly:      41
9475  deg
Mean motion:   15
54187173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3097
Checksum:              328


Coasting Arc #8 (Orbit 3112)
---------------------------------------

Vector Time (GMT): 2016/080/03:11:47
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5292583
19                 A    =         6789039
20  meter
 Y    =       -4244788
26  meter          E    =           
0009883
 Z    =         -25258
30                 I    =           51
88750
 XDOT =       2947
774317                 Wp   =          132
07010
 YDOT =       3702
285013  meter/sec      RA   =          141
10216  deg
 ZDOT =      -6032
707040                 TA   =           48
20101
                                          MA   =           48
11662
                                          Ha   =            220
535  n
mi
                                          Hp   =            214
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17364118
08                 X    =         5339778
81
 Y    =      -13926470
68  feet           Y    =        -4185339
20  meter
 Z    =         -82868
44                 Z    =             566
67
 XDOT =       9671
175581                 XDOT =        2935
459323
 YDOT =      12146
604372  feet/sec       YDOT =        3735
179291  meter/sec
 ZDOT =     -19792
345932                 ZDOT =       -6018
418081

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2359149
98                 X    =         -719068
91
 Y    =       22133674
82  feet           Y    =         6746344
09  meter
 Z    =          29993
67                 Z    =            9142
07
 XDOT =     -13907
360551                 XDOT =       -4238
963496
 YDOT =      -1436
972535  feet/sec       YDOT =        -437
989229  meter/sec
 ZDOT =     -19730
855491                 ZDOT =       -6013
964754


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   16080
16538245  
00016717  00000-0  10270-3 0  9073
2 25544  51
6408 142
0185 0002302 325
9294  34
1711 15
54227814 31132


Satellite: ISS
Catalog Number: 25544
Epoch time:      16080
16538245   =   yrday
fracday
Element set:     907
Inclination:       51
6408  deg
RA of node:       142
0185  deg
Eccentricity:     
0002302     
Arg of perigee:   325
9294  deg
Mean anomaly:      34
1711  deg
Mean motion:   15
54227814  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3113
Checksum:              279


Coasting Arc #9 (Orbit 3117)
---------------------------------------

Vector Time (GMT): 2016/080/10:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4666838
38                 A    =         6779287
00  meter
 Y    =        -991388
42  meter          E    =           
0005680
 Z    =        4812643
76                 I    =           51
86520
 XDOT =       3959
571272                 Wp   =          112
51470
 YDOT =      -6037
216722  meter/sec      RA   =          139
62624  deg
 ZDOT =       2591
408867                 TA   =          312
02538
                                          MA   =          312
07372
                                          Ha   =            220
582  n
mi
                                          Hp   =            214
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15311149
54                 X    =        -4678783
08
 Y    =       -3252586
69  feet           Y    =        -1043642
21  meter
 Z    =       15789513
64                 Z    =         4789944
81
 XDOT =      12990
719395                 XDOT =        4014
198835
 YDOT =     -19807
141478  feet/sec       YDOT =       -5992
632353  meter/sec
 ZDOT =       8501
997596                 ZDOT =        2610
776805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12391127
53                 X    =        -3776815
67
 Y    =       -9724713
05  feet           Y    =        -2964092
54  meter
 Z    =       15691057
21                 Z    =         4782634
24
 XDOT =      19645
094906                 XDOT =        5987
824927
 YDOT =     -11151
823546  feet/sec       YDOT =       -3399
075817  meter/sec
 ZDOT =       8587
094876                 ZDOT =        2617
346518


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   16080
48687519  
00016717  00000-0  10270-3 0  9088
2 25544  51
6435 140
4150 0001926 318
4223  41
6783 15
54241672 31181


Satellite: ISS
Catalog Number: 25544
Epoch time:      16080
48687519   =   yrday
fracday
Element set:     908
Inclination:       51
6435  deg
RA of node:       140
4150  deg
Eccentricity:     
0001926     
Arg of perigee:   318
4223  deg
Mean anomaly:      41
6783  deg
Mean motion:   15
54241672  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3118
Checksum:              303


Coasting Arc #10 (Orbit 3132)
---------------------------------------

Vector Time (GMT): 2016/081/10:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3505636
19                 A    =         6777289
37  meter
 Y    =        2373318
39  meter          E    =           
0013718
 Z    =       -5304238
48                 I    =           51
88074
 XDOT =      -4963
064843                 Wp   =           77
47875
 YDOT =       5792
218184  meter/sec      RA   =          134
64465  deg
 ZDOT =       -687
092427                 TA   =          185
96503
                                          MA   =          185
98139
                                          Ha   =            220
557  n
mi
                                          Hp   =            215
054

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11501431
07                 X    =         3504602
10
 Y    =        7786477
65  feet           Y    =         2412514
14  meter
 Z    =      -17402357
23                 Z    =        -5287212
01
 XDOT =     -16283
021137                 XDOT =       -5024
128431
 YDOT =      19003
340498  feet/sec       YDOT =        5736
376359  meter/sec
 ZDOT =      -2254
240245                 ZDOT =        -711
350756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7187303
38                 X    =         2190690
07
 Y    =       11992120
37  feet           Y    =         3655198
29  meter
 Z    =      -17328759
54                 Z    =        -5281805
91
 XDOT =     -21941
562358                 XDOT =       -6687
788207
 YDOT =       9732
664265  feet/sec       YDOT =        2966
516068  meter/sec
 ZDOT =      -2360
556652                 ZDOT =        -719
497667


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   16081
45134945  
00016717  00000-0  10270-3 0  9097
2 25544  51
6422 135
6076 0002007 324
5642  35
5377 15
54210528 31338


Satellite: ISS
Catalog Number: 25544
Epoch time:      16081
45134945   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:       135
6076  deg
Eccentricity:     
0002007     
Arg of perigee:   324
5642  deg
Mean anomaly:      35
5377  deg
Mean motion:   15
54210528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3133
Checksum:              289


Coasting Arc #11 (Orbit 3148)
---------------------------------------

Vector Time (GMT): 2016/082/10:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2212210
76                 A    =         6777444
86  meter
 Y    =       -3728848
62  meter          E    =           
0004680
 Z    =        5207908
72                 I    =           51
90385
 XDOT =       5563
700237                 Wp   =           30
36548
 YDOT =      -5117
976392  meter/sec      RA   =          129
66123  deg
 ZDOT =      -1296
670551                 TA   =           72
06484
                                          MA   =           72
01382
                                          Ha   =            220
557  n
mi
                                          Hp   =            214
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7257909
32                 X    =        -2195647
08
 Y    =      -12233755
30  feet           Y    =        -3753493
57  meter
 Z    =       17086314
70                 Z    =         5197203
25
 XDOT =      18253
609701                 XDOT =        5626
815851
 YDOT =     -16791
261129  feet/sec       YDOT =       -5055
406706  meter/sec
 ZDOT =      -4254
168473                 ZDOT =       -1269
489507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1695385
01                 X    =         -516753
35
 Y    =      -14178671
17  feet           Y    =        -4321658
97  meter
 Z    =       17040396
71                 Z    =         5193912
92
 XDOT =      22529
203524                 XDOT =        6866
901234
 YDOT =      -7681
327950  feet/sec       YDOT =       -2341
268759  meter/sec
 ZDOT =      -4135
248482                 ZDOT =       -1260
423737


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   16082
48011003  
00016717  00000-0  10270-3 0  9102
2 25544  51
6422 130
4787 0002016 327
5184  32
5845 15
54275918 31492


Satellite: ISS
Catalog Number: 25544
Epoch time:      16082
48011003   =   yrday
fracday
Element set:     910
Inclination:       51
6422  deg
RA of node:       130
4787  deg
Eccentricity:     
0002016     
Arg of perigee:   327
5184  deg
Mean anomaly:      32
5845  deg
Mean motion:   15
54275918  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3149
Checksum:              288


Coasting Arc #12 (Orbit 3159)
---------------------------------------

Vector Time (GMT): 2016/083/03:23:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2582466
70                 A    =         6777464
24  meter
 Y    =       -3430027
96  meter          E    =           
0004583
 Z    =        5242553
81                 I    =           51
91379
 XDOT =       5148
867350                 Wp   =           32
06710
 YDOT =      -5576
231337  meter/sec      RA   =          126
14973  deg
 ZDOT =      -1107
797327                 TA   =           68
53091
                                          MA   =           68
48204
                                          Ha   =            220
797  n
mi
                                          Hp   =            214
772

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8472659
76                 X    =        -2569385
34
 Y    =      -11253372
58  feet           Y    =        -3458832
82  meter
 Z    =       17199979
70                 Z    =         5230041
21
 XDOT =      16892
609417                 XDOT =        5216
220670
 YDOT =     -18294
722235  feet/sec       YDOT =       -5518
276864  meter/sec
 ZDOT =      -3634
505665                 ZDOT =       -1082
620987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14145482
76                 X    =         4311543
14
 Y    =         421975
52  feet           Y    =          128618
14  meter
 Z    =       17146163
24                 Z    =         5226150
56
 XDOT =       3583
740808                 XDOT =        1092
324198
 YDOT =      23630
674053  feet/sec       YDOT =        7202
629451  meter/sec
 ZDOT =      -3524
213510                 ZDOT =       -1074
180278


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   16083
18737993  
00016717  00000-0  10270-3 0  9114
2 25544  51
6385 126
9502 0001990 338
2547  21
8521 15
54220003 31607


Satellite: ISS
Catalog Number: 25544
Epoch time:      16083
18737993   =   yrday
fracday
Element set:     911
Inclination:       51
6385  deg
RA of node:       126
9502  deg
Eccentricity:     
0001990     
Arg of perigee:   338
2547  deg
Mean anomaly:      21
8521  deg
Mean motion:   15
54220003  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3160
Checksum:              295


Coasting Arc #13 (Orbit 3174)
---------------------------------------

Vector Time (GMT): 2016/084/03:23:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1383007
11                 A    =         6779793
24  meter
 Y    =        4745901
61  meter          E    =           
0009474
 Z    =       -4648834
80                 I    =           51
94088
 XDOT =      -5442
289538                 Wp   =          100
49036
 YDOT =       4496
556222  meter/sec      RA   =          121
17120  deg
 ZDOT =       2974
846869                 TA   =          199
04215
                                          MA   =          199
07759
                                          Ha   =            220
740  n
mi
                                          Hp   =            214
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4537424
90                 X    =         1352416
53
 Y    =       15570543
34  feet           Y    =         4761195
53  meter
 Z    =      -15252082
66                 Z    =        -4642191
55
 XDOT =     -17855
280636                 XDOT =       -5506
617207
 YDOT =      14752
481043  feet/sec       YDOT =        4435
337719  meter/sec
 ZDOT =       9759
996291                 ZDOT =        2948
252604

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15116295
33                 X    =        -4607446
82
 Y    =       -5948436
08  feet           Y    =        -1813083
32  meter
 Z    =      -15223987
45                 Z    =        -4640271
38
 XDOT =      -1004
085932                 XDOT =        -306
045392
 YDOT =     -22100
675669  feet/sec       YDOT =       -6736
285944  meter/sec
 ZDOT =       9643
704468                 ZDOT =        2939
401122


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   16084
15182610  
00016717  00000-0  10270-3 0  9123
2 25544  51
6391 122
1409 0001893 345
8721  14
2379 15
54272361 31755


Satellite: ISS
Catalog Number: 25544
Epoch time:      16084
15182610   =   yrday
fracday
Element set:     912
Inclination:       51
6391  deg
RA of node:       122
1409  deg
Eccentricity:     
0001893     
Arg of perigee:   345
8721  deg
Mean anomaly:      14
2379  deg
Mean motion:   15
54272361  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3175
Checksum:              292


Coasting Arc #14 (Orbit 3175)
---------------------------------------

Vector Time (GMT): 2016/084/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2159635
48                 A    =         6787644
05  meter
 Y    =       -6197368
77  meter          E    =           
0012746
 Z    =        1711211
37                 I    =           51
96755
 XDOT =       5104
529415                 Wp   =          109
37392
 YDOT =        190
847592  meter/sec      RA   =          120
98033  deg
 ZDOT =      -5720
513456                 TA   =           51
94369
                                          MA   =           51
82875
                                          Ha   =            220
682  n
mi
                                          Hp   =            214
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7085418
25                 X    =         2220463
15
 Y    =      -20332574
70  feet           Y    =        -6172877
91  meter
 Z    =        5614210
52                 Z    =         1721851
08
 XDOT =      16747
143751                 XDOT =        5129
803759
 YDOT =        626
140393  feet/sec       YDOT =         248
070239  meter/sec
 ZDOT =     -18768
088767                 ZDOT =       -5695
655547

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15765799
54                 X    =         4805415
70
 Y    =       14646625
34  feet           Y    =         4464291
40  meter
 Z    =        5661451
79                 Z    =         1725610
50
 XDOT =      -6302
389955                 XDOT =       -1920
968458
 YDOT =      14035
107846  feet/sec       YDOT =        4277
900871  meter/sec
 ZDOT =     -18660
104020                 ZDOT =       -5687
599705


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   16084
21612197  
00016717  00000-0  10270-3 0  9139
2 25544  51
6389 121
8197 0001878 342
7111  17
3978 15
54274614 31767


Satellite: ISS
Catalog Number: 25544
Epoch time:      16084
21612197   =   yrday
fracday
Element set:     913
Inclination:       51
6389  deg
RA of node:       121
8197  deg
Eccentricity:     
0001878     
Arg of perigee:   342
7111  deg
Mean anomaly:      17
3978  deg
Mean motion:   15
54274614  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3176
Checksum:              320


Coasting Arc #15 (Orbit 3190)
---------------------------------------

Vector Time (GMT): 2016/085/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2989829
79                 A    =         6788855
86  meter
 Y    =        6087283
08  meter          E    =           
0013145
 Z    =          19101
54                 I    =           51
98821
 XDOT =      -4229
491425                 Wp   =           39
26345
 YDOT =      -2103
391361  meter/sec      RA   =          116
03229  deg
 ZDOT =       6043
275168                 TA   =          320
94138
                                          MA   =          321
03622
                                          Ha   =            220
723  n
mi
                                          Hp   =            214
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9809152
86                 X    =        -3057769
88
 Y    =       19971401
17  feet           Y    =         6053468
94  meter
 Z    =          62669
10                 Z    =            4411
70
 XDOT =     -13876
284204                 XDOT =       -4235
012198
 YDOT =      -6900
890292  feet/sec       YDOT =       -2150
718304  meter/sec
 ZDOT =      19827
018267                 ZDOT =        6022
716177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14613929
02                 X    =        -4454325
57
 Y    =      -16778359
44  feet           Y    =        -5114043
96  meter
 Z    =          -2167
61                 Z    =            -660
69
 XDOT =      10560
483389                 XDOT =        3218
835337
 YDOT =      -9173
103324  feet/sec       YDOT =       -2795
961893  meter/sec
 ZDOT =      19738
025120                 ZDOT =        6016
150057


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   16085
18055971  
00016717  00000-0  10270-3 0  9148
2 25544  51
6397 117
0114 0001767 348
0499  12
0611 15
54291452 31919


Satellite: ISS
Catalog Number: 25544
Epoch time:      16085
18055971   =   yrday
fracday
Element set:     914
Inclination:       51
6397  deg
RA of node:       117
0114  deg
Eccentricity:     
0001767     
Arg of perigee:   348
0499  deg
Mean anomaly:      12
0611  deg
Mean motion:   15
54291452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3191
Checksum:              301


Coasting Arc #16 (Orbit 3206)
---------------------------------------

Vector Time (GMT): 2016/086/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905478
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3603012
23                 A    =         6787460
03  meter
 Y    =       -5465964
71  meter          E    =           
0005901
 Z    =       -1785922
51                 I    =           51
99700
 XDOT =       3231
812157                 Wp   =          132
92285
 YDOT =       3985
654174  meter/sec      RA   =          111
08430  deg
 ZDOT =      -5694
169646                 TA   =           66
58872
                                          MA   =           66
52668
                                          Ha   =            220
729  n
mi
                                          Hp   =            214
491

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11820906
26                 X    =         3672541
52
 Y    =      -17932955
09  feet           Y    =        -5425284
92  meter
 Z    =       -5859325
84                 Z    =        -1768250
23
 XDOT =      10603
058258                 XDOT =        3214
663402
 YDOT =      13076
293223  feet/sec       YDOT =        4021
697774  meter/sec
 ZDOT =     -18681
658944                 ZDOT =       -5678
512411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12247271
54                 X    =         3732968
36
 Y    =       17670134
52  feet           Y    =         5385857
00  meter
 Z    =       -5781616
39                 Z    =        -1762236
68
 XDOT =     -14833
205540                 XDOT =       -4521
161049
 YDOT =       4207
594707  feet/sec       YDOT =        1282
474867  meter/sec
 ZDOT =     -18614
281858                 ZDOT =       -5673
633110


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   16086
20928279  
00016717  00000-0  10270-3 0  9153
2 25544  51
6397 111
8814 0001886 350
8231   9
2887 15
54317162 32073


Satellite: ISS
Catalog Number: 25544
Epoch time:      16086
20928279   =   yrday
fracday
Element set:     915
Inclination:       51
6397  deg
RA of node:       111
8814  deg
Eccentricity:     
0001886     
Arg of perigee:   350
8231  deg
Mean anomaly:       9
2887  deg
Mean motion:   15
54317162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3207
Checksum:              320


Coasting Arc #17 (Orbit 3222)
---------------------------------------

Vector Time (GMT): 2016/087/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918408
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3970993
70                 A    =         6784058
87  meter
 Y    =        4368914
74  meter          E    =           
0012603
 Z    =        3328704
18                 I    =           51
99794
 XDOT =      -2216
338439                 Wp   =           80
00222
 YDOT =      -5624
190388  meter/sec      RA   =          106
13051  deg
 ZDOT =       4724
722458                 TA   =          318
55312
                                          MA   =          318
64865
                                          Ha   =            220
779  n
mi
                                          Hp   =            214
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13028194
56                 X    =        -4035722
40
 Y    =       14333709
77  feet           Y    =         4324146
94  meter
 Z    =       10920945
48                 Z    =         3309256
17
 XDOT =      -7271
451573                 XDOT =       -2176
233476
 YDOT =     -18452
068201  feet/sec       YDOT =       -5648
750129  meter/sec
 ZDOT =      15501
057932                 ZDOT =        4714
054065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8744932
89                 X    =        -2665455
55
 Y    =      -17336958
79  feet           Y    =        -5284305
04  meter
 Z    =       10835688
63                 Z    =         3302717
89
 XDOT =      18601
501095                 XDOT =        5669
737534
 YDOT =        303
984761  feet/sec       YDOT =          92
654555  meter/sec
 ZDOT =      15455
644752                 ZDOT =        4710
880520


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   16087
23799420  
00016717  00000-0  10270-3 0  9162
2 25544  51
6411 106
7518 0001823 353
2612   6
8516 15
54349423 32230


Satellite: ISS
Catalog Number: 25544
Epoch time:      16087
23799420   =   yrday
fracday
Element set:     916
Inclination:       51
6411  deg
RA of node:       106
7518  deg
Eccentricity:     
0001823     
Arg of perigee:   353
2612  deg
Mean anomaly:       6
8516  deg
Mean motion:   15
54349423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3223
Checksum:              296


Coasting Arc #18 (Orbit 3237)
---------------------------------------

Vector Time (GMT): 2016/088/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918408
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4171847
90                 A    =         6780174
49  meter
 Y    =       -2852909
96  meter          E    =           
0010340
 Z    =       -4530167
70                 I    =           51
99240
 XDOT =       1202
505516                 Wp   =           59
79685
 YDOT =       6850
867219  meter/sec      RA   =          101
16729  deg
 ZDOT =      -3207
391187                 TA   =          178
10142
                                          MA   =          178
09749
                                          Ha   =            220
793  n
mi
                                          Hp   =            214
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13687165
04                 X    =         4225445
58
 Y    =       -9359940
83  feet           Y    =        -2805958
41  meter
 Z    =      -14862754
92                 Z    =        -4509771
24
 XDOT =       3945
228071                 XDOT =        1141
388297
 YDOT =      22476
598486  feet/sec       YDOT =        6863
972354  meter/sec
 ZDOT =     -10522
936965                 ZDOT =       -3201
698873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4131187
44                 X    =         1259185
93
 Y    =       16140689
36  feet           Y    =         4919682
12  meter
 Z    =      -14773621
77                 Z    =        -4502999
91
 XDOT =     -21327
293039                 XDOT =       -6500
558918
 YDOT =      -4150
225893  feet/sec       YDOT =       -1264
988852  meter/sec
 ZDOT =     -10499
371346                 ZDOT =       -3200
208386


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   16088
20240437  
00016717  00000-0  10270-3 0  9170
2 25544  51
6408 101
9436 0001872 358
6642   1
4505 15
54325465 32383


Satellite: ISS
Catalog Number: 25544
Epoch time:      16088
20240437   =   yrday
fracday
Element set:     917
Inclination:       51
6408  deg
RA of node:       101
9436  deg
Eccentricity:     
0001872     
Arg of perigee:   358
6642  deg
Mean anomaly:       1
4505  deg
Mean motion:   15
54325465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3238
Checksum:              297


Coasting Arc #19 (Orbit 3253)
---------------------------------------

Vector Time (GMT): 2016/089/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918408
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4206477
28                 A    =         6777205
25  meter
 Y    =        1057478
91  meter          E    =           
0003583
 Z    =        5204558
10                 I    =           51
98913
 XDOT =       -235
781141                 Wp   =           99
81103
 YDOT =      -7549
649156  meter/sec      RA   =           96
19350  deg
 ZDOT =       1342
019470                 TA   =          337
35302
                                          MA   =          337
36882
                                          Ha   =            220
864  n
mi
                                          Hp   =            214
255

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13800778
48                 X    =        -4243271
32
 Y    =        3469418
99  feet           Y    =         1010234
07  meter
 Z    =       17075321
86                 Z    =         5184034
47
 XDOT =       -773
560174                 XDOT =        -157
860562
 YDOT =     -24769
190143  feet/sec       YDOT =       -7551
850006  meter/sec
 ZDOT =       4402
951017                 ZDOT =        1341
064097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1207718
18                 X    =          368112
50
 Y    =      -14285808
84  feet           Y    =        -4354314
53  meter
 Z    =       16985936
95                 Z    =         5177313
58
 XDOT =      22658
625122                 XDOT =        6906
348937
 YDOT =       7152
718807  feet/sec       YDOT =        2180
148693  meter/sec
 ZDOT =       4400
109345                 ZDOT =        1341
153328


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   16089
23109627  
00016717  00000-0  10270-3 0  9180
2 25544  51
6416  96
8138 0001869 359
2725    
8424 15
54381022 32540


Satellite: ISS
Catalog Number: 25544
Epoch time:      16089
23109627   =   yrday
fracday
Element set:     918
Inclination:       51
6416  deg
RA of node:        96
8138  deg
Eccentricity:     
0001869     
Arg of perigee:   359
2725  deg
Mean anomaly:        
8424  deg
Mean motion:   15
54381022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3254
Checksum:              314
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