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

 
Date: July 18th 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) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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


198/02:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 213 1

198/21:41:46 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 213 1

200/04:45:26 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 213 1

201/00:22:53 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 213 0

201/08:38:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 213 0

202/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 213 0

Coasting Arc #1 (Orbit 938)
---------------------------------------

Vector Time (GMT): 2016/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894430
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4246688
14                 A    =         6776127
63  meter
 Y    =       -1432413
76  meter          E    =           
0005454
 Z    =        5078431
14                 I    =           51
25951
 XDOT =        546
680758                 Wp   =          112
37168
 YDOT =       7474
051883  meter/sec      RA   =          275
97576  deg
 ZDOT =       1647
509450                 TA   =          321
63018
                                          MA   =          321
66897
                                          Ha   =            220
058  n
mi
                                          Hp   =            213
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13932703
87                 X    =         4237721
44
 Y    =       -4699520
20  feet           Y    =        -1384975
09  meter
 Z    =       16661519
50                 Z    =         5099038
46
 XDOT =       1793
572042                 XDOT =         455
060551
 YDOT =      24521
167595  feet/sec       YDOT =        7479
652791  meter/sec
 ZDOT =       5405
214731                 ZDOT =        1649
943273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9710715
17                 X    =        -2959825
98
 Y    =      -10904082
89  feet           Y    =        -3323564
47  meter
 Z    =       16751565
49                 Z    =         5105877
16
 XDOT =      21106
008504                 XDOT =        6433
111392
 YDOT =     -10460
816257  feet/sec       YDOT =       -3188
456795  meter/sec
 ZDOT =       5414
389817                 ZDOT =        1650
306016


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   16197
55106782  
00016717  00000-0  10270-3 0  9005
2 25544  51
6440 276
5250 0001223  47
9145 312
2112 15
54856583  9390


Satellite: ISS
Catalog Number: 25544
Epoch time:      16197
55106782   =   yrday
fracday
Element set:     900
Inclination:       51
6440  deg
RA of node:       276
5250  deg
Eccentricity:     
0001223     
Arg of perigee:    47
9145  deg
Mean anomaly:     312
2112  deg
Mean motion:   15
54856583  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             939
Checksum:              299


Coasting Arc #2 (Orbit 947)
---------------------------------------

Vector Time (GMT): 2016/198/02:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894430
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2428940
87                 A    =         6782299
82  meter
 Y    =        5353266
73  meter          E    =           
0013539
 Z    =        3372379
77                 I    =           51
27856
 XDOT =      -3942
484350                 Wp   =           84
19827
 YDOT =       4701
294894  meter/sec      RA   =          272
97890  deg
 ZDOT =      -4605
883855                 TA   =           56
17387
                                          MA   =           56
04506
                                          Ha   =            220
219  n
mi
                                          Hp   =            213
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7968966
09                 X    =         2352517
31
 Y    =       17563211
06  feet           Y    =         5380001
11  meter
 Z    =       11064238
08                 Z    =         3383993
81
 XDOT =     -12934
659942                 XDOT =       -3972
389152
 YDOT =      15424
195846  feet/sec       YDOT =        4657
040679  meter/sec
 ZDOT =     -15111
167504                 ZDOT =       -4625
107475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3274620
43                 X    =         -998104
31
 Y    =       18977568
29  feet           Y    =         5784362
82  meter
 Z    =       11113817
09                 Z    =         3387491
45
 XDOT =     -17882
658282                 XDOT =       -5450
634244
 YDOT =       5846
560126  feet/sec       YDOT =        1782
031526  meter/sec
 ZDOT =     -15195
807635                 ZDOT =       -4631
682167


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   16198
12952446  
00016717  00000-0  10270-3 0  9016
2 25544  51
6441 273
6411 0001757  34
9230 325
2038 15
54871398  9483


Satellite: ISS
Catalog Number: 25544
Epoch time:      16198
12952446   =   yrday
fracday
Element set:     901
Inclination:       51
6441  deg
RA of node:       273
6411  deg
Eccentricity:     
0001757     
Arg of perigee:    34
9230  deg
Mean anomaly:     325
2038  deg
Mean motion:   15
54871398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             948
Checksum:              313


Coasting Arc #3 (Orbit 960)
---------------------------------------

Vector Time (GMT): 2016/198/21:41:46
000
Vector Time (MET): N/A
Weight (LBS)     : 894430
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1188314
72                 A    =         6786142
78  meter
 Y    =       -6470825
63  meter          E    =           
0015638
 Z    =        1632068
21                 I    =           51
28809
 XDOT =       4606
073686                 Wp   =           61
53824
 YDOT =       2290
380245  meter/sec      RA   =          268
93758  deg
 ZDOT =       5692
897406                 TA   =          316
43452
                                          MA   =          316
55791
                                          Ha   =            220
374  n
mi
                                          Hp   =            213
068

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3898670
35                 X    =         1252656
99
 Y    =      -21229742
89  feet           Y    =        -6457177
53  meter
 Z    =        5354554
50                 Z    =         1637996
25
 XDOT =      15111
790307                 XDOT =        4552
466347
 YDOT =       7514
370882  feet/sec       YDOT =        2341
588060  meter/sec
 ZDOT =      18677
484928                 ZDOT =        5715
142418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20202012
87                 X    =         6157573
52
 Y    =        7582210
27  feet           Y    =         2311057
69  meter
 Z    =        5381601
17                 Z    =         1640312
04
 XDOT =      -9512
298372                 XDOT =       -2899
348544
 YDOT =      11939
910029  feet/sec       YDOT =        3639
284577  meter/sec
 ZDOT =      18773
967155                 ZDOT =        5722
305189


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   16198
96507258  
00016717  00000-0  10270-3 0  9026
2 25544  51
6420 269
4714 0001781  45
5800 314
5499 15
54833839  9612


Satellite: ISS
Catalog Number: 25544
Epoch time:      16198
96507258   =   yrday
fracday
Element set:     902
Inclination:       51
6420  deg
RA of node:       269
4714  deg
Eccentricity:     
0001781     
Arg of perigee:    45
5800  deg
Mean anomaly:     314
5499  deg
Mean motion:   15
54833839  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             961
Checksum:              332


Coasting Arc #4 (Orbit 975)
---------------------------------------

Vector Time (GMT): 2016/199/21:41:46
000
Vector Time (MET): N/A
Weight (LBS)     : 894430
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2121038
79                 A    =         6782394
97  meter
 Y    =        5502876
65  meter          E    =           
0006176
 Z    =       -3356085
71                 I    =           51
27818
 XDOT =      -4200
693682                 Wp   =           80
32392
 YDOT =      -4436
013338  meter/sec      RA   =          263
93229  deg
 ZDOT =      -4625
051370                 TA   =          139
01726
                                          MA   =          138
97083
                                          Ha   =            220
363  n
mi
                                          Hp   =            212
981

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6958788
67                 X    =        -2166113
48
 Y    =       18054057
26  feet           Y    =         5478906
14  meter
 Z    =      -11010779
89                 Z    =        -3366497
92
 XDOT =     -13781
803419                 XDOT =       -4128
310627
 YDOT =     -14553
849535  feet/sec       YDOT =       -4482
583053  meter/sec
 ZDOT =     -15174
053051                 ZDOT =       -4645
281742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16707627
51                 X    =        -5092484
86
 Y    =       -9705932
04  feet           Y    =        -2958368
09  meter
 Z    =      -11057172
49                 Z    =        -3370226
17
 XDOT =      15861
812687                 XDOT =        4834
680507
 YDOT =      -9941
596078  feet/sec       YDOT =       -3030
198485  meter/sec
 ZDOT =     -15261
368600                 ZDOT =       -4651
665149


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   16199
92916002  
00016717  00000-0  10270-3 0  9035
2 25544  51
6428 264
6611 0001774  47
3818 312
7484 15
54856904  9762


Satellite: ISS
Catalog Number: 25544
Epoch time:      16199
92916002   =   yrday
fracday
Element set:     903
Inclination:       51
6428  deg
RA of node:       264
6611  deg
Eccentricity:     
0001774     
Arg of perigee:    47
3818  deg
Mean anomaly:     312
7484  deg
Mean motion:   15
54856904  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             976
Checksum:              331


Coasting Arc #5 (Orbit 980)
---------------------------------------

Vector Time (GMT): 2016/200/04:45:26
000
Vector Time (MET): N/A
Weight (LBS)     : 894430
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3528066
21                 A    =         6777100
84  meter
 Y    =       -3117383
63  meter          E    =           
0007462
 Z    =        4869669
81                 I    =           51
25762
 XDOT =       2773
733902                 Wp   =          110
25481
 YDOT =       6768
556303  meter/sec      RA   =          262
44605  deg
 ZDOT =       2317
980667                 TA   =          316
92931
                                          MA   =          316
98768
                                          Ha   =            220
248  n
mi
                                          Hp   =            213
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11575020
36                 X    =         3539008
92
 Y    =      -10227636
57  feet           Y    =        -3077869
80  meter
 Z    =       15976606
99                 Z    =         4886834
28
 XDOT =       9100
176844                 XDOT =        2686
580449
 YDOT =      22206
549552  feet/sec       YDOT =        6799
086480  meter/sec
 ZDOT =       7604
923449                 ZDOT =        2331
243679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10152772
71                 X    =         3094565
12
 Y    =      -11536592
33  feet           Y    =        -3516353
34  meter
 Z    =       16051973
73                 Z    =         4892641
59
 XDOT =      10825
092321                 XDOT =        3299
488139
 YDOT =      20211
432079  feet/sec       YDOT =        6160
444498  meter/sec
 ZDOT =       7661
452709                 ZDOT =        2335
210786


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   16200
25052113  
00016717  00000-0  10270-3 0  9049
2 25544  51
6392 263
0536 0001548  53
4597 306
6698 15
54833938  9819


Satellite: ISS
Catalog Number: 25544
Epoch time:      16200
25052113   =   yrday
fracday
Element set:     904
Inclination:       51
6392  deg
RA of node:       263
0536  deg
Eccentricity:     
0001548     
Arg of perigee:    53
4597  deg
Mean anomaly:     306
6698  deg
Mean motion:   15
54833938  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             981
Checksum:              312


Coasting Arc #6 (Orbit 992)
---------------------------------------

Vector Time (GMT): 2016/201/00:22:53
000
Vector Time (MET): N/A
Weight (LBS)     : 908864
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3410328
76                 A    =         6783671
42  meter
 Y    =       -5111568
09  meter          E    =           
0006221
 Z    =       -2874261
63                 I    =           51
28816
 XDOT =       3101
020998                 Wp   =           58
80227
 YDOT =      -4888
024523  meter/sec      RA   =          258
30787  deg
 ZDOT =       5024
700143                 TA   =          268
31035
                                          MA   =          268
38160
                                          Ha   =            220
302  n
mi
                                          Hp   =            213
041

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11188742
67                 X    =        -3338954
76
 Y    =      -16770236
50  feet           Y    =        -5149305
28  meter
 Z    =       -9429992
21                 Z    =        -2890655
08
 XDOT =      10173
953407                 XDOT =        3131
042210
 YDOT =     -16036
825862  feet/sec       YDOT =       -4853
179515  meter/sec
 ZDOT =      16485
236689                 ZDOT =        5039
836284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8292621
36                 X    =         2527590
99
 Y    =      -18339214
64  feet           Y    =        -5589792
62  meter
 Z    =       -9500483
43                 Z    =        -2895747
35
 XDOT =      17596
262292                 XDOT =        5363
340747
 YDOT =       -599
026868  feet/sec       YDOT =        -182
583389  meter/sec
 ZDOT =      16552
090399                 ZDOT =        5045
077154


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   16201
02178525  
00016717  00000-0  10270-3 0  9052
2 25544  51
6435 259
2097 0001702  43
1703 316
9583 15
54849885  9931


Satellite: ISS
Catalog Number: 25544
Epoch time:      16201
02178525   =   yrday
fracday
Element set:     905
Inclination:       51
6435  deg
RA of node:       259
2097  deg
Eccentricity:     
0001702     
Arg of perigee:    43
1703  deg
Mean anomaly:     316
9583  deg
Mean motion:   15
54849885  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             993
Checksum:              317


Coasting Arc #7 (Orbit 998)
---------------------------------------

Vector Time (GMT): 2016/201/08:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908864
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4201461
93                 A    =         6775152
10  meter
 Y    =        -624786
79  meter          E    =           
0003970
 Z    =        5275058
22                 I    =           51
26198
 XDOT =       1524
037827                 Wp   =           71
15546
 YDOT =       7513
279408  meter/sec      RA   =          256
59929  deg
 ZDOT =       -322
514389                 TA   =           21
94198
                                          MA   =           21
92498
                                          Ha   =            220
130  n
mi
                                          Hp   =            212
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13784323
93                 X    =         4182512
68
 Y    =       -2049825
42  feet           Y    =         -577909
73  meter
 Z    =       17306621
46                 Z    =         5295421
44
 XDOT =       5000
124103                 XDOT =        1441
475783
 YDOT =      24649
866824  feet/sec       YDOT =        7529
860617  meter/sec
 ZDOT =      -1058
118073                 ZDOT =        -315
310878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3638163
06                 X    =         1108912
10
 Y    =      -13337539
33  feet           Y    =        -4065281
99  meter
 Z    =       17395468
70                 Z    =         5302138
86
 XDOT =      23603
538321                 XDOT =        7194
358480
 YDOT =       5091
357269  feet/sec       YDOT =        1551
845696  meter/sec
 ZDOT =      -1028
105992                 ZDOT =        -313
366706


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   16201
40741631  
00016717  00000-0  10270-3 0  9069
2 25544  51
6432 257
2804 0001447  63
0516 297
0785 15
54892519  9992


Satellite: ISS
Catalog Number: 25544
Epoch time:      16201
40741631   =   yrday
fracday
Element set:     906
Inclination:       51
6432  deg
RA of node:       257
2804  deg
Eccentricity:     
0001447     
Arg of perigee:    63
0516  deg
Mean anomaly:     297
0785  deg
Mean motion:   15
54892519  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             999
Checksum:              315


Coasting Arc #8 (Orbit 1013)
---------------------------------------

Vector Time (GMT): 2016/202/08:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908864
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4553253
10                 A    =         6777146
50  meter
 Y    =       -1425602
28  meter          E    =           
0012980
 Z    =       -4825191
86                 I    =           51
27628
 XDOT =       -335
522289                 Wp   =          103
55828
 YDOT =      -7245
789937  meter/sec      RA   =          251
56932  deg
 ZDOT =       2459
988851                 TA   =          190
73775
                                          MA   =          190
76549
                                          Ha   =            220
325  n
mi
                                          Hp   =            212
795

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14938494
41                 X    =        -4513535
00
 Y    =       -4677172
83  feet           Y    =        -1476297
29  meter
 Z    =      -15830681
96                 Z    =        -4847213
65
 XDOT =      -1100
794910                 XDOT =        -266
422433
 YDOT =     -23772
276697  feet/sec       YDOT =       -7249
155827  meter/sec
 ZDOT =       8070
829563                 ZDOT =        2458
526196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10060597
26                 X    =        -3066470
05
 Y    =       11865052
22  feet           Y    =         3616467
92  meter
 Z    =      -15926392
27                 Z    =        -4854364
36
 XDOT =     -21496
773506                 XDOT =       -6552
216565
 YDOT =      -7412
298294  feet/sec       YDOT =       -2259
268520  meter/sec
 ZDOT =       8065
765480                 ZDOT =        2458
445318


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   16202
37149344  
00016717  00000-0  10270-3 0  9070
2 25544  51
6425 252
4711 0001532  69
3790 290
7528 15
54887358 10145


Satellite: ISS
Catalog Number: 25544
Epoch time:      16202
37149344   =   yrday
fracday
Element set:     907
Inclination:       51
6425  deg
RA of node:       252
4711  deg
Eccentricity:     
0001532     
Arg of perigee:    69
3790  deg
Mean anomaly:     290
7528  deg
Mean motion:   15
54887358  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1014
Checksum:              309


Coasting Arc #9 (Orbit 1015)
---------------------------------------

Vector Time (GMT): 2016/202/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4526381
00                 A    =         6779369
07  meter
 Y    =        2735641
82  meter          E    =           
0011380
 Z    =        4234190
51                 I    =           51
28429
 XDOT =       -719
195701                 Wp   =           71
47749
 YDOT =       6748
393000  meter/sec      RA   =          251
07049  deg
 ZDOT =      -3579
722703                 TA   =           55
29828
                                          MA   =           55
19112
                                          Ha   =            220
158  n
mi
                                          Hp   =            212
971

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14850331
36                 X    =         4474886
49
 Y    =        8975202
82  feet           Y    =         2785970
54  meter
 Z    =       13891701
15                 Z    =         4256053
27
 XDOT =      -2359
565949                 XDOT =        -777
216077
 YDOT =      22140
396980  feet/sec       YDOT =        6740
026370  meter/sec
 ZDOT =     -11744
497056                 ZDOT =       -3583
356648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5481843
49                 X    =         1670865
89
 Y    =      -16382724
19  feet           Y    =        -4993454
33  meter
 Z    =       13986483
05                 Z    =         4263080
03
 XDOT =      20900
182620                 XDOT =        6370
375663
 YDOT =      -3079
731269  feet/sec       YDOT =        -938
702091  meter/sec
 ZDOT =     -11761
551744                 ZDOT =       -3584
920972


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   16202
50003520  
00016717  00000-0  10270-3 0  9081
2 25544  51
6419 251
8306 0001483  58
2448 301
8850 15
54898606 10165


Satellite: ISS
Catalog Number: 25544
Epoch time:      16202
50003520   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:       251
8306  deg
Eccentricity:     
0001483     
Arg of perigee:    58
2448  deg
Mean anomaly:     301
8850  deg
Mean motion:   15
54898606  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1016
Checksum:              290


Coasting Arc #10 (Orbit 1030)
---------------------------------------

Vector Time (GMT): 2016/203/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4392591
10                 A    =         6783712
13  meter
 Y    =       -4336087
74  meter          E    =           
0006203
 Z    =       -2815574
45                 I    =           51
30889
 XDOT =       2057
968721                 Wp   =           63
16221
 YDOT =      -5368
751635  meter/sec      RA   =          246
05780  deg
 ZDOT =       5068
834833                 TA   =          264
71573
                                          MA   =          264
78651
                                          Ha   =            220
309  n
mi
                                          Hp   =            212
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14411388
12                 X    =        -4330100
85
 Y    =      -14226009
65  feet           Y    =        -4384859
03  meter
 Z    =       -9237449
00                 Z    =        -2836760
63
 XDOT =       6751
865881                 XDOT =        2093
228807
 YDOT =     -17614
014550  feet/sec       YDOT =       -5345
541247  meter/sec
 ZDOT =      16630
035541                 ZDOT =        5078
916998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10395712
50                 X    =        -3168613
17
 Y    =       17329068
43  feet           Y    =         5281900
06  meter
 Z    =       -9329012
33                 Z    =        -2843482
96
 XDOT =     -17424
942488                 XDOT =       -5311
122470
 YDOT =      -1496
316788  feet/sec       YDOT =        -456
077357  meter/sec
 ZDOT =      16674
931377                 ZDOT =        5082
519084


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   16203
46410845  
00016717  00000-0  10270-3 0  9090
2 25544  51
6408 247
0200 0001544  65
9817 294
1498 15
54879677 10312


Satellite: ISS
Catalog Number: 25544
Epoch time:      16203
46410845   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       247
0200  deg
Eccentricity:     
0001544     
Arg of perigee:    65
9817  deg
Mean anomaly:     294
1498  deg
Mean motion:   15
54879677  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1031
Checksum:              316


Coasting Arc #11 (Orbit 1046)
---------------------------------------

Vector Time (GMT): 2016/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3907459
57                 A    =         6786653
75  meter
 Y    =        5455033
81  meter          E    =           
0014500
 Z    =         974228
81                 I    =           51
33341
 XDOT =      -3434
298761                 Wp   =          118
27372
 YDOT =       3521
902725  meter/sec      RA   =          241
05746  deg
 ZDOT =      -5885
742048                 TA   =           51
12230
                                          MA   =           50
99304
                                          Ha   =            220
363  n
mi
                                          Hp   =            212
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12819749
24                 X    =         3841437
31
 Y    =       17897092
55  feet           Y    =         5498360
43  meter
 Z    =        3196288
74                 Z    =          993049
79
 XDOT =     -11267
384386                 XDOT =       -3444
836513
 YDOT =      11554
798966  feet/sec       YDOT =        3483
439471  meter/sec
 ZDOT =     -19310
177324                 ZDOT =       -5902
450092

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14041205
61                 X    =         4279759
47
 Y    =      -16940235
45  feet           Y    =        -5163383
76  meter
 Z    =        3277365
07                 Z    =          998940
87
 XDOT =      12777
469693                 XDOT =        3894
572762
 YDOT =       6803
478282  feet/sec       YDOT =        2073
700180  meter/sec
 ZDOT =     -19383
618289                 ZDOT =       -5908
126854


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   16204
49244659  
00016717  00000-0  10270-3 0  9104
2 25544  51
6414 241
8875 0001772  63
3148 296
8186 15
54904360 10479


Satellite: ISS
Catalog Number: 25544
Epoch time:      16204
49244659   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       241
8875  deg
Eccentricity:     
0001772     
Arg of perigee:    63
3148  deg
Mean anomaly:     296
8186  deg
Mean motion:   15
54904360  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1047
Checksum:              317


Coasting Arc #12 (Orbit 1062)
---------------------------------------

Vector Time (GMT): 2016/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3082580
64                 A    =         6786876
16  meter
 Y    =       -5960993
66  meter          E    =           
0015384
 Z    =         963254
84                 I    =           51
34901
 XDOT =       4692
115230                 Wp   =           56
72267
 YDOT =      -1464
912387  meter/sec      RA   =          236
06368  deg
 ZDOT =       5890
198083                 TA   =          313
75949
                                          MA   =          313
88671
                                          Ha   =            220
515  n
mi
                                          Hp   =            212
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10113453
55                 X    =        -3020373
20
 Y    =      -19557065
82  feet           Y    =        -5995117
34  meter
 Z    =        3160284
91                 Z    =          948431
61
 XDOT =      15394
078839                 XDOT =        4679
536008
 YDOT =      -4806
143001  feet/sec       YDOT =       -1412
512543  meter/sec
 ZDOT =      19324
796861                 ZDOT =        5912
960186

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16068696
03                 X    =        -4897738
55
 Y    =       15065045
78  feet           Y    =         4591825
95  meter
 Z    =        3096703
17                 Z    =          943875
13
 XDOT =      -7672
813622                 XDOT =       -2338
673592
 YDOT =     -12217
996967  feet/sec       YDOT =       -3724
045475  meter/sec
 ZDOT =      19424
267772                 ZDOT =        5920
516817


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   16205
52078322  
00016717  00000-0  10270-3 0  9112
2 25544  51
6405 236
7559 0001906  65
7580 294
3772 15
54844148 10635


Satellite: ISS
Catalog Number: 25544
Epoch time:      16205
52078322   =   yrday
fracday
Element set:     911
Inclination:       51
6405  deg
RA of node:       236
7559  deg
Eccentricity:     
0001906     
Arg of perigee:    65
7580  deg
Mean anomaly:     294
3772  deg
Mean motion:   15
54844148  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1063
Checksum:              311


Coasting Arc #13 (Orbit 1077)
---------------------------------------

Vector Time (GMT): 2016/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1866752
95                 A    =         6783760
03  meter
 Y    =        5886319
36  meter          E    =           
0006142
 Z    =       -2810672
60                 I    =           51
35877
 XDOT =      -5709
268433                 Wp   =          107
65603
 YDOT =       -608
297247  meter/sec      RA   =          231
06573  deg
 ZDOT =      -5076
851682                 TA   =          104
37476
                                          MA   =          104
30658
                                          Ha   =            220
447  n
mi
                                          Hp   =            212
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6124517
54                 X    =         1814444
73
 Y    =       19312071
38  feet           Y    =         5906902
22  meter
 Z    =       -9221366
81                 Z    =        -2801731
45
 XDOT =     -18731
195646                 XDOT =       -5677
381188
 YDOT =      -1995
725876  feet/sec       YDOT =        -671
963705  meter/sec
 ZDOT =     -16656
337539                 ZDOT =       -5104
508027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16710169
64                 X    =         5093259
71
 Y    =      -11486290
79  feet           Y    =        -3501021
43  meter
 Z    =       -9183396
79                 Z    =        -2799099
34
 XDOT =       2616
238263                 XDOT =         797
429422
 YDOT =      17190
289953  feet/sec       YDOT =        5239
600378  meter/sec
 ZDOT =     -16776
792814                 ZDOT =       -5113
566450


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   16206
48484194  
00016717  00000-0  10270-3 0  9127
2 25544  51
6414 231
9443 0001849  73
5854 286
5502 15
54900142 10788


Satellite: ISS
Catalog Number: 25544
Epoch time:      16206
48484194   =   yrday
fracday
Element set:     912
Inclination:       51
6414  deg
RA of node:       231
9443  deg
Eccentricity:     
0001849     
Arg of perigee:    73
5854  deg
Mean anomaly:     286
5502  deg
Mean motion:   15
54900142  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1078
Checksum:              309


Coasting Arc #14 (Orbit 1093)
---------------------------------------

Vector Time (GMT): 2016/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -374064
65                 A    =         6779451
68  meter
 Y    =       -5270665
46  meter          E    =           
0011744
 Z    =        4239022
06                 I    =           51
36522
 XDOT =       6331
161148                 Wp   =          101
56104
 YDOT =       2441
540732  meter/sec      RA   =          226
05725  deg
 ZDOT =       3583
666876                 TA   =          311
67321
                                          MA   =          311
77367
                                          Ha   =            220
469  n
mi
                                          Hp   =            212
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1227246
24                 X    =         -335690
06
 Y    =      -17292209
51  feet           Y    =        -5274634
01  meter
 Z    =       13907552
70                 Z    =         4237298
08
 XDOT =      20771
526076                 XDOT =        6285
980963
 YDOT =       8010
304238  feet/sec       YDOT =        2512
087323  meter/sec
 ZDOT =      11757
437256                 ZDOT =        3614
312040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16068199
23                 X    =        -4897587
12
 Y    =        6521027
73  feet           Y    =         1987609
25  meter
 Z    =       13900929
33                 Z    =         4237003
26
 XDOT =       1802
832735                 XDOT =         549
503418
 YDOT =     -20980
262582  feet/sec       YDOT =       -6394
784035  meter/sec
 ZDOT =      11890
621675                 ZDOT =        3624
261486


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   16207
51316751  
00016717  00000-0  10270-3 0  9136
2 25544  51
6413 226
8123 0001942  75
0972 285
0396 15
54901997 10949


Satellite: ISS
Catalog Number: 25544
Epoch time:      16207
51316751   =   yrday
fracday
Element set:     913
Inclination:       51
6413  deg
RA of node:       226
8123  deg
Eccentricity:     
0001942     
Arg of perigee:    75
0972  deg
Mean anomaly:     285
0396  deg
Mean motion:   15
54901997  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1094
Checksum:              309


Coasting Arc #15 (Orbit 1108)
---------------------------------------

Vector Time (GMT): 2016/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1334015
98                 A    =         6775995
22  meter
 Y    =        4256243
71  meter          E    =           
0015366
 Z    =       -5114672
24                 I    =           51
37773
 XDOT =      -6399
229091                 Wp   =           78
08836
 YDOT =      -3899
731031  meter/sec      RA   =          221
03769  deg
 ZDOT =      -1577
076325                 TA   =          176
63356
                                          MA   =          176
62320
                                          Ha   =            220
457  n
mi
                                          Hp   =            212
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4376692
84                 X    =        -1356666
54
 Y    =       13964054
17  feet           Y    =         4241199
34  meter
 Z    =      -16780420
74                 Z    =        -5121207
41
 XDOT =     -20994
846100                 XDOT =       -6347
485015
 YDOT =     -12794
393147  feet/sec       YDOT =       -3971
002125  meter/sec
 ZDOT =      -5174
134924                 ZDOT =       -1608
036357

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14593728
52                 X    =         4448168
45
 Y    =        -438456
20  feet           Y    =         -133641
45  meter
 Z    =      -16809628
59                 Z    =        -5123574
80
 XDOT =      -5423
191280                 XDOT =       -1652
988702
 YDOT =      22894
246147  feet/sec       YDOT =        6978
166226  meter/sec
 ZDOT =      -5308
461134                 ZDOT =       -1618
018954


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   16208
47721946  
00016717  00000-0  10270-3 0  9149
2 25544  51
6423 222
0015 0001845  77
6088 282
5271 15
54894366 11098


Satellite: ISS
Catalog Number: 25544
Epoch time:      16208
47721946   =   yrday
fracday
Element set:     914
Inclination:       51
6423  deg
RA of node:       222
0015  deg
Eccentricity:     
0001845     
Arg of perigee:    77
6088  deg
Mean anomaly:     282
5271  deg
Mean motion:   15
54894366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1109
Checksum:              311


Coasting Arc #16 (Orbit 1124)
---------------------------------------

Vector Time (GMT): 2016/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3054319
74                 A    =         6775173
26  meter
 Y    =       -2973493
32  meter          E    =           
0004842
 Z    =        5262303
04                 I    =           51
39861
 XDOT =       5872
149615                 Wp   =           72
12556
 YDOT =       4898
456032  meter/sec      RA   =          216
01266  deg
 ZDOT =       -638
440368                 TA   =           23
99702
                                          MA   =           23
97446
                                          Ha   =            220
373  n
mi
                                          Hp   =            212
711

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10020734
07                 X    =         3061781
26
 Y    =       -9755555
50  feet           Y    =        -2939296
37  meter
 Z    =       17264773
75                 Z    =         5277158
07
 XDOT =      19265
582728                 XDOT =        5820
038663
 YDOT =      16071
049974  feet/sec       YDOT =        4963
830987  meter/sec
 ZDOT =      -2094
620630                 ZDOT =        -610
041480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12523805
76                 X    =        -3817256
00
 Y    =       -6040056
15  feet           Y    =        -1841009
12  meter
 Z    =       17330043
22                 Z    =         5282197
17
 XDOT =       8189
223898                 XDOT =        2496
075444
 YDOT =     -22655
166516  feet/sec       YDOT =       -6905
294754  meter/sec
 ZDOT =      -1971
611848                 ZDOT =        -600
947291


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   16209
50553774  
00016717  00000-0  10270-3 0  9157
2 25544  51
6407 216
8697 0001985  80
7558 279
3820 15
54915367 11256


Satellite: ISS
Catalog Number: 25544
Epoch time:      16209
50553774   =   yrday
fracday
Element set:     915
Inclination:       51
6407  deg
RA of node:       216
8697  deg
Eccentricity:     
0001985     
Arg of perigee:    80
7558  deg
Mean anomaly:     279
3820  deg
Mean motion:   15
54915367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1125
Checksum:              337


Coasting Arc #17 (Orbit 1139)
---------------------------------------

Vector Time (GMT): 2016/210/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4617139
23                 A    =         6777588
78  meter
 Y    =        1604547
32  meter          E    =           
0012620
 Z    =       -4707072
09                 I    =           51
43462
 XDOT =      -4688
760897                 Wp   =          105
23715
 YDOT =      -5388
429658  meter/sec      RA   =          210
99238  deg
 ZDOT =       2765
329004                 TA   =          192
24720
                                          MA   =          192
27790
                                          Ha   =            220
436  n
mi
                                          Hp   =            212
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15148094
58                 X    =        -4611873
76
 Y    =        5264262
86  feet           Y    =         1552945
11  meter
 Z    =      -15443149
91                 Z    =        -4729487
96
 XDOT =     -15383
073808                 XDOT =       -4641
590320
 YDOT =     -17678
574994  feet/sec       YDOT =       -5440
598930  meter/sec
 ZDOT =       9072
601719                 ZDOT =        2742
666588

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10240049
70                 X    =         3121167
15
 Y    =       12218084
09  feet           Y    =         3724072
03  meter
 Z    =      -15541168
41                 Z    =        -4736948
13
 XDOT =     -10191
055472                 XDOT =       -3106
233708
 YDOT =      19944
522058  feet/sec       YDOT =        6079
090323  meter/sec
 ZDOT =       8974
672091                 ZDOT =        2735
480053


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   16210
46958135  
00016717  00000-0  10270-3 0  9165
2 25544  51
6421 212
0590 0001832  79
1153 281
0206 15
54899015 11402


Satellite: ISS
Catalog Number: 25544
Epoch time:      16210
46958135   =   yrday
fracday
Element set:     916
Inclination:       51
6421  deg
RA of node:       212
0590  deg
Eccentricity:     
0001832     
Arg of perigee:    79
1153  deg
Mean anomaly:     281
0206  deg
Mean motion:   15
54899015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1140
Checksum:              281


Coasting Arc #18 (Orbit 1155)
---------------------------------------

Vector Time (GMT): 2016/211/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5813819
73                 A    =         6781714
68  meter
 Y    =        -241028
89  meter          E    =           
0014182
 Z    =        3471576
38                 I    =           51
47519
 XDOT =       2942
128369                 Wp   =           87
54888
 YDOT =       5448
121016  meter/sec      RA   =          205
98462  deg
 ZDOT =      -4532
281795                 TA   =           51
53891
                                          MA   =           51
41174
                                          Ha   =            220
334  n
mi
                                          Hp   =            212
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19074211
71                 X    =         5799219
62
 Y    =        -790777
21  feet           Y    =         -176096
76  meter
 Z    =       11389686
27                 Z    =         3499782
70
 XDOT =       9652
652128                 XDOT =        2903
003095
 YDOT =      17874
412782  feet/sec       YDOT =        5480
803421  meter/sec
 ZDOT =     -14869
690930                 ZDOT =       -4518
084451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7751640
25                 X    =        -2362699
95
 Y    =      -17365039
62  feet           Y    =        -5292864
08  meter
 Z    =       11512745
39                 Z    =         3509084
80
 XDOT =      11742
328639                 XDOT =        3579
061769
 YDOT =     -15095
372108  feet/sec       YDOT =       -4601
069418  meter/sec
 ZDOT =     -14808
673715                 ZDOT =       -4513
683748


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   16211
49788975  
00016717  00000-0  10270-3 0  9173
2 25544  51
6403 206
9268 0001993  80
6643 279
4735 15
54949448 11566


Satellite: ISS
Catalog Number: 25544
Epoch time:      16211
49788975   =   yrday
fracday
Element set:     917
Inclination:       51
6403  deg
RA of node:       206
9268  deg
Eccentricity:     
0001993     
Arg of perigee:    80
6643  deg
Mean anomaly:     279
4735  deg
Mean motion:   15
54949448  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1156
Checksum:              353


Coasting Arc #19 (Orbit 1170)
---------------------------------------

Vector Time (GMT): 2016/212/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929830
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6472751
04                 A    =         6785486
76  meter
 Y    =        -962802
56  meter          E    =           
0008679
 Z    =       -1786250
07                 I    =           51
51671
 XDOT =       -792
364651                 Wp   =           49
38210
 YDOT =      -5117
755493  meter/sec      RA   =          200
99304  deg
 ZDOT =       5653
354653                 TA   =          290
96043
                                          MA   =          291
05328
                                          Ha   =            220
380  n
mi
                                          Hp   =            212
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21236059
85                 X    =        -6452826
96
 Y    =       -3158801
04  feet           Y    =        -1035073
64  meter
 Z    =       -5860400
49                 Z    =        -1817644
33
 XDOT =      -2599
621558                 XDOT =        -762
538908
 YDOT =     -16790
536393  feet/sec       YDOT =       -5126
449903  meter/sec
 ZDOT =      18547
751486                 ZDOT =        5649
577653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5251664
40                 X    =         1600707
31
 Y    =       20778506
94  feet           Y    =         6333288
91  meter
 Z    =       -5997184
89                 Z    =        -1827941
96
 XDOT =     -12929
780456                 XDOT =       -3940
997083
 YDOT =       8594
931849  feet/sec       YDOT =        2619
735228  meter/sec
 ZDOT =      18532
120389                 ZDOT =        5648
590294


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   16212
46192636  
00016717  00000-0  10270-3 0  9185
2 25544  51
6397 202
1163 0001996  89
4208 270
7173 15
54961094 11715


Satellite: ISS
Catalog Number: 25544
Epoch time:      16212
46192636   =   yrday
fracday
Element set:     918
Inclination:       51
6397  deg
RA of node:       202
1163  deg
Eccentricity:     
0001996     
Arg of perigee:    89
4208  deg
Mean anomaly:     270
7173  deg
Mean motion:   15
54961094  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1171
Checksum:              314
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