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

 
Date: March 5th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17276 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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


There are no maneuvers



Coasting Arc #1 (Orbit 1174)
---------------------------------------

Vector Time (GMT): 2015/063/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4504613
91                 A    =         6776493
69  meter
 Y    =         160993
84  meter          E    =           
0013846
 Z    =        5050932
74                 I    =           51
29003
 XDOT =       1712
168335                 Wp   =           63
00949
 YDOT =       7276
526686  meter/sec      RA   =          245
95130  deg
 ZDOT =      -1749
018932                 TA   =           44
02085
                                          MA   =           43
91068
                                          Ha   =            222
948  n
mi
                                          Hp   =            210
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14778917
04                 X    =         4477943
76
 Y    =         528195
02  feet           Y    =          211218
96  meter
 Z    =       16571301
63                 Z    =         5072750
07
 XDOT =       5617
350180                 XDOT =        1639
169166
 YDOT =      23873
119048  feet/sec       YDOT =        7295
264864  meter/sec
 ZDOT =      -5738
251089                 ZDOT =       -1740
880022

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13733611
27                 X    =         4186004
72
 Y    =        5194411
10  feet           Y    =         1583256
50  meter
 Z    =       16664616
15                 Z    =         5079375
00
 XDOT =      -1898
893570                 XDOT =        -578
782760
 YDOT =      23425
510989  feet/sec       YDOT =        7140
095749  meter/sec
 ZDOT =      -5704
622418                 ZDOT =       -1738
768913


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   15063
54595058  
00016717  00000-0  10270-3 0  9003
2 25544  51
6406 246
6885 0008652  67
6435 292
5635 15
54765446 11758


Satellite: ISS
Catalog Number: 25544
Epoch time:      15063
54595058   =   yrday
fracday
Element set:     900
Inclination:       51
6406  deg
RA of node:       246
6885  deg
Eccentricity:     
0008652     
Arg of perigee:    67
6435  deg
Mean anomaly:     292
5635  deg
Mean motion:   15
54765446  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1175
Checksum:              335


Coasting Arc #2 (Orbit 1189)
---------------------------------------

Vector Time (GMT): 2015/064/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4952132
45                 A    =         6779790
40  meter
 Y    =       -2012304
87  meter          E    =           
0015787
 Z    =       -4184166
59                 I    =           51
31536
 XDOT =       -366
160059                 Wp   =           90
05959
 YDOT =      -6710
054276  meter/sec      RA   =          240
92651  deg
 ZDOT =       3672
487460                 TA   =          217
78937
                                          MA   =          217
90032
                                          Ha   =            223
017  n
mi
                                          Hp   =            210
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16247153
70                 X    =        -4908937
53
 Y    =       -6602050
09  feet           Y    =        -2067441
96  meter
 Z    =      -13727580
69                 Z    =        -4208117
50
 XDOT =      -1201
312530                 XDOT =        -308
938725
 YDOT =     -22014
613767  feet/sec       YDOT =       -6713
828423  meter/sec
 ZDOT =      12048
843372                 ZDOT =        3670
848743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13394037
17                 X    =        -4082502
53
 Y    =      -11195620
74  feet           Y    =        -3412425
20  meter
 Z    =      -13829728
31                 Z    =        -4215301
19
 XDOT =       4646
230276                 XDOT =        1416
170988
 YDOT =     -20386
550196  feet/sec       YDOT =       -6213
820500  meter/sec
 ZDOT =      12042
917751                 ZDOT =        3670
681331


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   15064
51006132  
00016717  00000-0  10270-3 0  9012
2 25544  51
6406 241
8762 0008730  71
5871 288
6231 15
54821439 11904


Satellite: ISS
Catalog Number: 25544
Epoch time:      15064
51006132   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:       241
8762  deg
Eccentricity:     
0008730     
Arg of perigee:    71
5871  deg
Mean anomaly:     288
6231  deg
Mean motion:   15
54821439  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1190
Checksum:              290


Coasting Arc #3 (Orbit 1205)
---------------------------------------

Vector Time (GMT): 2015/065/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5054069
51                 A    =         6784034
36  meter
 Y    =        3619131
20  meter          E    =           
0021510
 Z    =        2697656
07                 I    =           51
34611
 XDOT =      -1212
520799                 Wp   =           90
96830
 YDOT =       5558
357087  meter/sec      RA   =          235
91591  deg
 ZDOT =      -5150
068709                 TA   =           58
38305
                                          MA   =           58
17333
                                          Ha   =            222
895  n
mi
                                          Hp   =            210
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16581592
87                 X    =         5000119
85
 Y    =       11873790
04  feet           Y    =         3675347
88  meter
 Z    =        8850577
66                 Z    =         2722075
85
 XDOT =      -3978
086610                 XDOT =       -1249
568740
 YDOT =      18236
079682  feet/sec       YDOT =        5544
589935  meter/sec
 ZDOT =     -16896
550881                 ZDOT =       -5156
049681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12421659
44                 X    =         3786121
80
 Y    =       16117954
62  feet           Y    =         4912752
57  meter
 Z    =        8954482
25                 Z    =         2729326
19
 XDOT =      -7766
316393                 XDOT =       -2367
173237
 YDOT =      15450
573876  feet/sec       YDOT =        4709
334917  meter/sec
 ZDOT =     -16923
030727                 ZDOT =       -5158
139766


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   15065
53842182  
00016717  00000-0  10270-3 0  9029
2 25544  51
6406 236
7433 0008596  74
3141 285
8960 15
54864009 12069


Satellite: ISS
Catalog Number: 25544
Epoch time:      15065
53842182   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:       236
7433  deg
Eccentricity:     
0008596     
Arg of perigee:    74
3141  deg
Mean anomaly:     285
8960  deg
Mean motion:   15
54864009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1206
Checksum:              312


Coasting Arc #4 (Orbit 1220)
---------------------------------------

Vector Time (GMT): 2015/066/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4769635
46                 A    =         6786733
07  meter
 Y    =       -4737726
10  meter          E    =           
0017606
 Z    =        -895617
34                 I    =           51
37474
 XDOT =       2854
048075                 Wp   =           57
82385
 YDOT =      -3972
018354  meter/sec      RA   =          230
91816  deg
 ZDOT =       5906
702258                 TA   =          292
44464
                                          MA   =          292
63101
                                          Ha   =            222
944  n
mi
                                          Hp   =            210
282

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15648410
29                 X    =        -4711952
06
 Y    =      -15543720
79  feet           Y    =        -4790740
89  meter
 Z    =       -2938377
09                 Z    =         -918646
25
 XDOT =       9363
674787                 XDOT =        2869
559695
 YDOT =     -13031
556281  feet/sec       YDOT =       -3940
014866  meter/sec
 ZDOT =      19378
944416                 ZDOT =        5920
604851

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10842216
41                 X    =        -3304707
56
 Y    =      -19192241
06  feet           Y    =        -5849795
07  meter
 Z    =       -3036163
22                 Z    =         -925422
55
 XDOT =      11021
157963                 XDOT =        3359
248947
 YDOT =      -9253
924159  feet/sec       YDOT =       -2820
596084  meter/sec
 ZDOT =      19439
061095                 ZDOT =        5925
025822


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   15066
50248945  
00016717  00000-0  10270-3 0  9035
2 25544  51
6415 231
9315 0008761  78
7438 281
4699 15
54895385 12215


Satellite: ISS
Catalog Number: 25544
Epoch time:      15066
50248945   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:       231
9315  deg
Eccentricity:     
0008761     
Arg of perigee:    78
7438  deg
Mean anomaly:     281
4699  deg
Mean motion:   15
54895385  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1221
Checksum:              334


Coasting Arc #5 (Orbit 1236)
---------------------------------------

Vector Time (GMT): 2015/067/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3977863
40                 A    =         6786395
45  meter
 Y    =        5382626
78  meter          E    =           
0015771
 Z    =       -1109887
10                 I    =           51
39496
 XDOT =      -4469
734117                 Wp   =          112
80717
 YDOT =       2109
859012  meter/sec      RA   =          225
92642  deg
 ZDOT =      -5860
032868                 TA   =           79
27668
                                          MA   =           79
09916
                                          Ha   =            222
902  n
mi
                                          Hp   =            210
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13050732
94                 X    =         3922769
34
 Y    =       17659536
67  feet           Y    =         5426801
62  meter
 Z    =       -3641361
87                 Z    =        -1090698
15
 XDOT =     -14664
482012                 XDOT =       -4464
529154
 YDOT =       6922
109618  feet/sec       YDOT =        2059
903736  meter/sec
 ZDOT =     -19225
829621                 ZDOT =       -5881
733535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8161535
53                 X    =         2487636
03
 Y    =       20399887
83  feet           Y    =         6217885
81  meter
 Z    =       -3560097
84                 Z    =        -1085117
82
 XDOT =     -14335
254555                 XDOT =       -4369
385588
 YDOT =       2406
253421  feet/sec       YDOT =         733
426043  meter/sec
 ZDOT =     -19319
020339                 ZDOT =       -5888
437399


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   15067
53080217  
00016717  00000-0  10270-3 0  9046
2 25544  51
6415 226
7984 0008792  80
7360 279
4787 15
54964212 12378


Satellite: ISS
Catalog Number: 25544
Epoch time:      15067
53080217   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:       226
7984  deg
Eccentricity:     
0008792     
Arg of perigee:    80
7360  deg
Mean anomaly:     279
4787  deg
Mean motion:   15
54964212  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1237
Checksum:              328


Coasting Arc #6 (Orbit 1252)
---------------------------------------

Vector Time (GMT): 2015/068/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2758699
09                 A    =         6783307
47  meter
 Y    =       -5461649
90  meter          E    =           
0022012
 Z    =        2905716
80                 I    =           51
40804
 XDOT =       5810
645463                 Wp   =           83
41590
 YDOT =       -253
463075  meter/sec      RA   =          220
93075  deg
 ZDOT =       5010
045350                 TA   =          309
87083
                                          MA   =          310
06422
                                          Ha   =            222
867  n
mi
                                          Hp   =            210
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9050850
03                 X    =        -2711535
45
 Y    =      -17918798
89  feet           Y    =        -5492235
35  meter
 Z    =        9533191
59                 Z    =         2892430
94
 XDOT =      19063
797451                 XDOT =        5788
711019
 YDOT =       -831
571768  feet/sec       YDOT =        -188
606571  meter/sec
 ZDOT =      16437
156660                 ZDOT =        5038
219025

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4600510
72                 X    =        -1402235
67
 Y    =      -19567859
59  feet           Y    =        -5964283
60  meter
 Z    =        9477191
24                 Z    =         2888647
89
 XDOT =      17188
036929                 XDOT =        5238
913656
 YDOT =       4026
580553  feet/sec       YDOT =        1227
301753  meter/sec
 ZDOT =      16557
761304                 ZDOT =        5046
805645


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   15068
55909097  
00016717  00000-0  10270-3 0  9056
2 25544  51
6422 221
6659 0008725  85
9211 274
2939 15
54982764 12539


Satellite: ISS
Catalog Number: 25544
Epoch time:      15068
55909097   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       221
6659  deg
Eccentricity:     
0008725     
Arg of perigee:    85
9211  deg
Mean anomaly:     274
2939  deg
Mean motion:   15
54982764  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1253
Checksum:              339


Coasting Arc #7 (Orbit 1267)
---------------------------------------

Vector Time (GMT): 2015/069/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1091797
16                 A    =         6778740
44  meter
 Y    =        5087568
04  meter          E    =           
0017280
 Z    =       -4361314
19                 I    =           51
41836
 XDOT =      -6690
182144                 Wp   =           79
29458
 YDOT =      -1483
813738  meter/sec      RA   =          215
92427  deg
 ZDOT =      -3414
101395                 TA   =          155
96437
                                          MA   =          155
88362
                                          Ha   =            222
829  n
mi
                                          Hp   =            210
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3582011
67                 X    =         1056011
24
 Y    =       16691496
18  feet           Y    =         5099576
56  meter
 Z    =      -14308773
59                 Z    =        -4356098
04
 XDOT =     -21949
416482                 XDOT =       -6656
508145
 YDOT =      -4868
155308  feet/sec       YDOT =       -1558
439884  meter/sec
 ZDOT =     -11201
120063                 ZDOT =       -3446
518984

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -97515
75                 X    =          -29722
80
 Y    =       17089266
82  feet           Y    =         5208808
53  meter
 Z    =      -14287242
71                 Z    =        -4354751
58
 XDOT =     -19019
896411                 XDOT =       -5797
264426
 YDOT =      -9565
787643  feet/sec       YDOT =       -2915
652074  meter/sec
 ZDOT =     -11339
625883                 ZDOT =       -3456
317969


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   15069
52308854  
00016717  00000-0  10270-3 0  9069
2 25544  51
6430 216
8545 0008788  88
3868 271
8292 15
55010769 12681


Satellite: ISS
Catalog Number: 25544
Epoch time:      15069
52308854   =   yrday
fracday
Element set:     906
Inclination:       51
6430  deg
RA of node:       216
8545  deg
Eccentricity:     
0008788     
Arg of perigee:    88
3868  deg
Mean anomaly:     271
8292  deg
Mean motion:   15
55010769  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1268
Checksum:              344


Coasting Arc #8 (Orbit 1283)
---------------------------------------

Vector Time (GMT): 2015/070/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         797980
52                 A    =         6775265
92  meter
 Y    =       -4312217
96  meter          E    =           
0012613
 Z    =        5154461
81                 I    =           51
43350
 XDOT =       6973
411817                 Wp   =          103
25946
 YDOT =       2915
907037  meter/sec      RA   =          210
90519  deg
 ZDOT =       1354
233291                 TA   =          333
67297
                                          MA   =          333
73702
                                          Ha   =            222
664  n
mi
                                          Hp   =            210
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2618046
32                 X    =          821103
02
 Y    =      -14147696
72  feet           Y    =        -4303164
53  meter
 Z    =       16910963
93                 Z    =         5158394
90
 XDOT =      22878
647694                 XDOT =        6933
708822
 YDOT =       9566
624136  feet/sec       YDOT =        2993
666445  meter/sec
 ZDOT =       4443
022608                 ZDOT =        1388
011965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5339243
41                 X    =         1627401
39
 Y    =      -13338352
86  feet           Y    =        -4065529
95  meter
 Z    =       16928467
52                 Z    =         5159796
90
 XDOT =      19449
975268                 XDOT =        5928
352462
 YDOT =      13630
920953  feet/sec       YDOT =        4154
704706  meter/sec
 ZDOT =       4587
145223                 ZDOT =        1398
161864


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   15070
55132657  
00016717  00000-0  10270-3 0  9071
2 25544  51
6429 211
7211 0008642  91
8197 268
3946 15
55063815 12841


Satellite: ISS
Catalog Number: 25544
Epoch time:      15070
55132657   =   yrday
fracday
Element set:     907
Inclination:       51
6429  deg
RA of node:       211
7211  deg
Eccentricity:     
0008642     
Arg of perigee:    91
8197  deg
Mean anomaly:     268
3946  deg
Mean motion:   15
55063815  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1284
Checksum:              316


Coasting Arc #9 (Orbit 1298)
---------------------------------------

Vector Time (GMT): 2015/071/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2773421
43                 A    =         6774802
84  meter
 Y    =        3299857
57  meter          E    =           
0023256
 Z    =       -5246958
53                 I    =           51
46045
 XDOT =      -6477
843735                 Wp   =           96
56294
 YDOT =      -3966
749290  meter/sec      RA   =          205
88307  deg
 ZDOT =        930
271741                 TA   =          182
37239
                                          MA   =          182
38344
                                          Ha   =            222
686  n
mi
                                          Hp   =            209
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9099151
69                 X    =        -2784627
39
 Y    =       10826304
35  feet           Y    =         3268780
15  meter
 Z    =      -17214430
86                 Z    =        -5260458
80
 XDOT =     -21252
768161                 XDOT =       -6437
524062
 YDOT =     -13014
269324  feet/sec       YDOT =       -4038
963228  meter/sec
 ZDOT =       3052
072641                 ZDOT =         898
902053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10853602
34                 X    =        -3308177
99
 Y    =        8955007
60  feet           Y    =         2729486
32  meter
 Z    =      -17272730
31                 Z    =        -5264728
20
 XDOT =     -17813
335849                 XDOT =       -5429
504767
 YDOT =     -15966
928635  feet/sec       YDOT =       -4866
719848  meter/sec
 ZDOT =       2918
407703                 ZDOT =         889
530668


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   15071
51527711  
00016717  00000-0  10270-3 0  9088
2 25544  51
6435 206
9103 0008788  95
0205 265
1952 15
55098231 12999


Satellite: ISS
Catalog Number: 25544
Epoch time:      15071
51527711   =   yrday
fracday
Element set:     908
Inclination:       51
6435  deg
RA of node:       206
9103  deg
Eccentricity:     
0008788     
Arg of perigee:    95
0205  deg
Mean anomaly:     265
1952  deg
Mean motion:   15
55098231  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1299
Checksum:              311


Coasting Arc #10 (Orbit 1314)
---------------------------------------

Vector Time (GMT): 2015/072/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4556386
14                 A    =         6777670
70  meter
 Y    =       -2122412
89  meter          E    =           
0016763
 Z    =        4533250
15                 I    =           51
49897
 XDOT =       5265
138611                 Wp   =           83
03043
 YDOT =       4648
900039  meter/sec      RA   =          200
86464  deg
 ZDOT =      -3103
601507                 TA   =           38
12302
                                          MA   =           38
00455
                                          Ha   =            222
591  n
mi
                                          Hp   =            209
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14948773
42                 X    =         4557760
09
 Y    =       -6963296
87  feet           Y    =        -2071452
28  meter
 Z    =       14872867
94                 Z    =         4555387
63
 XDOT =      17274
076807                 XDOT =        5227
838261
 YDOT =      15252
296717  feet/sec       YDOT =        4707
569397  meter/sec
 ZDOT =     -10182
419642                 ZDOT =       -3078
115652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15820909
37                 X    =         4822213
18
 Y    =       -4337546
72  feet           Y    =        -1322084
24  meter
 Z    =       14967967
33                 Z    =         4562236
44
 XDOT =      14179
283517                 XDOT =        4321
845616
 YDOT =      16821
302081  feet/sec       YDOT =        5127
132874  meter/sec
 ZDOT =     -10074
031095                 ZDOT =       -3070
564678


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   15072
54346597  
00016717  00000-0  10270-3 0  9094
2 25544  51
6434 201
7762 0008818  98
5587 261
6565 15
55090233 13151


Satellite: ISS
Catalog Number: 25544
Epoch time:      15072
54346597   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:       201
7762  deg
Eccentricity:     
0008818     
Arg of perigee:    98
5587  deg
Mean anomaly:     261
6565  deg
Mean motion:   15
55090233  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1315
Checksum:              329


Coasting Arc #11 (Orbit 1329)
---------------------------------------

Vector Time (GMT): 2015/073/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5917266
22                 A    =         6781972
13  meter
 Y    =         949939
10  meter          E    =           
0013031
 Z    =       -3187083
94                 I    =           51
54431
 XDOT =      -3369
283222                 Wp   =           94
28224
 YDOT =      -4923
632484  meter/sec      RA   =          195
86217  deg
 ZDOT =       4804
039226                 TA   =          228
87720
                                          MA   =          228
98976
                                          Ha   =            222
518  n
mi
                                          Hp   =            209
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19413603
07                 X    =        -5911967
33
 Y    =        3116598
11  feet           Y    =          883797
70  meter
 Z    =      -10456312
15                 Z    =        -3215815
87
 XDOT =     -11054
078811                 XDOT =       -3337
311636
 YDOT =     -16153
649883  feet/sec       YDOT =       -4961
130797  meter/sec
 ZDOT =      15761
283550                 ZDOT =        4787
750141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19595806
83                 X    =        -5972801
92
 Y    =         121052
26  feet           Y    =           36896
73  meter
 Z    =      -10579476
98                 Z    =        -3224624
58
 XDOT =      -8544
287132                 XDOT =       -2604
298718
 YDOT =     -16238
737865  feet/sec       YDOT =       -4949
567301  meter/sec
 ZDOT =      15692
297603                 ZDOT =        4783
012309


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   15073
50736664  
00016717  00000-0  10270-3 0  9101
2 25544  51
6440 196
9642 0008624 100
7010 259
5114 15
55141930 13306


Satellite: ISS
Catalog Number: 25544
Epoch time:      15073
50736664   =   yrday
fracday
Element set:     910
Inclination:       51
6440  deg
RA of node:       196
9642  deg
Eccentricity:     
0008624     
Arg of perigee:   100
7010  deg
Mean anomaly:     259
5114  deg
Mean motion:   15
55141930  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1330
Checksum:              281


Coasting Arc #12 (Orbit 1345)
---------------------------------------

Vector Time (GMT): 2015/074/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6646669
93                 A    =         6785492
90  meter
 Y    =         229388
74  meter          E    =           
0022306
 Z    =        1297352
63                 I    =           51
58718
 XDOT =        982
389227                 Wp   =          114
67616
 YDOT =       4895
423240  meter/sec      RA   =          190
87503  deg
 ZDOT =      -5829
036861                 TA   =           51
18028
                                          MA   =           50
98134
                                          Ha   =            222
450  n
mi
                                          Hp   =            209
859

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21806659
88                 X    =         6637308
87
 Y    =         752587
74  feet           Y    =          303663
93  meter
 Z    =        4256406
26                 Z    =         1329617
76
 XDOT =       3223
061770                 XDOT =         955
889419
 YDOT =      16061
099870  feet/sec       YDOT =        4906
260223  meter/sec
 ZDOT =     -19124
136682                 ZDOT =       -5824
329495

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21474957
97                 X    =         6545567
19
 Y    =        3705136
18  feet           Y    =         1129325
51  meter
 Z    =        4394535
68                 Z    =         1339454
47
 XDOT =       1401
445190                 XDOT =         427
160494
 YDOT =      14798
899774  feet/sec       YDOT =        4510
704651  meter/sec
 ZDOT =     -19104
728713                 ZDOT =       -5823
121312


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   15074
53550331  
00016717  00000-0  10270-3 0  9111
2 25544  51
6441 191
8302 0008679 104
8657 255
3458 15
55189143 13466


Satellite: ISS
Catalog Number: 25544
Epoch time:      15074
53550331   =   yrday
fracday
Element set:     911
Inclination:       51
6441  deg
RA of node:       191
8302  deg
Eccentricity:     
0008679     
Arg of perigee:   104
8657  deg
Mean anomaly:     255
3458  deg
Mean motion:   15
55189143  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1346
Checksum:              311


Coasting Arc #13 (Orbit 1361)
---------------------------------------

Vector Time (GMT): 2015/075/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6619215
38                 A    =         6785914
91  meter
 Y    =       -1271351
33  meter          E    =           
0019595
 Z    =         738053
69                 I    =           51
62107
 XDOT =       1557
346728                 Wp   =           74
01425
 YDOT =      -4579
076610  meter/sec      RA   =          185
89726  deg
 ZDOT =       5953
158725                 TA   =          293
96720
                                          MA   =          294
17226
                                          Ha   =            222
390  n
mi
                                          Hp   =            209
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21716585
90                 X    =        -6608092
02
 Y    =       -4171100
16  feet           Y    =        -1345309
44  meter
 Z    =        2421436
00                 Z    =          705926
39
 XDOT =       5109
405276                 XDOT =        1579
517447
 YDOT =     -15023
217223  feet/sec       YDOT =       -4561
536729  meter/sec
 ZDOT =      19531
360645                 ZDOT =        5960
778266

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21082049
23                 X    =        -6425808
61
 Y    =       -6723236
02  feet           Y    =        -2049242
34  meter
 Z    =        2284037
97                 Z    =          696174
77
 XDOT =       6244
542237                 XDOT =        1903
336474
 YDOT =     -12785
464577  feet/sec       YDOT =       -3897
009603  meter/sec
 ZDOT =      19564
690538                 ZDOT =        5963
317676


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   15075
56361318  
00016717  00000-0  10270-3 0  9121
2 25544  51
6450 186
6968 0008672 107
0869 253
1235 15
55233997 13623


Satellite: ISS
Catalog Number: 25544
Epoch time:      15075
56361318   =   yrday
fracday
Element set:     912
Inclination:       51
6450  deg
RA of node:       186
6968  deg
Eccentricity:     
0008672     
Arg of perigee:   107
0869  deg
Mean anomaly:     253
1235  deg
Mean motion:   15
55233997  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1362
Checksum:              328


Coasting Arc #14 (Orbit 1376)
---------------------------------------

Vector Time (GMT): 2015/076/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5779265
78                 A    =         6782889
09  meter
 Y    =        2261009
73  meter          E    =           
0013420
 Z    =       -2739760
10                 I    =           51
64311
 XDOT =      -4003
841926                 Wp   =          115
91630
 YDOT =       4016
817456  meter/sec      RA   =          180
91775  deg
 ZDOT =      -5156
188078                 TA   =           95
08391
                                          MA   =           94
93071
                                          Ha   =            222
328  n
mi
                                          Hp   =            209
901

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18960845
73                 X    =         5766861
66
 Y    =        7418010
92  feet           Y    =         2325567
55  meter
 Z    =       -8988714
23                 Z    =        -2711716
34
 XDOT =     -13135
964325                 XDOT =       -4023
414856
 YDOT =      13178
534960  feet/sec       YDOT =        3971
933785  meter/sec
 ZDOT =     -16916
627554                 ZDOT =       -5175
685757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18164429
56                 X    =         5536518
13
 Y    =        9313052
35  feet           Y    =         2838618
36  meter
 Z    =       -8868939
89                 Z    =        -2703252
88
 XDOT =     -13621
985574                 XDOT =       -4151
981203
 YDOT =      10459
001943  feet/sec       YDOT =        3187
903792  meter/sec
 ZDOT =     -17000
748759                 ZDOT =       -5181
828222


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   15076
52744211  
00016717  00000-0  10270-3 0  9136
2 25544  51
6452 181
8841 0008622 110
8137 249
3941 15
55275622 13775


Satellite: ISS
Catalog Number: 25544
Epoch time:      15076
52744211   =   yrday
fracday
Element set:     913
Inclination:       51
6452  deg
RA of node:       181
8841  deg
Eccentricity:     
0008622     
Arg of perigee:   110
8137  deg
Mean anomaly:     249
3941  deg
Mean motion:   15
55275622  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1377
Checksum:              305


Coasting Arc #15 (Orbit 1392)
---------------------------------------

Vector Time (GMT): 2015/077/12:01:00
251
Vector Time (MET): N/A
Weight (LBS)     : 905416
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4261459
62                 A    =         6778155
27  meter
 Y    =       -3079616
56  meter          E    =           
0018574
 Z    =        4266799
98                 I    =           51
66009
 XDOT =       5957
640457                 Wp   =          110
21451
 YDOT =      -3260
939009  meter/sec      RA   =          175
92665  deg
 ZDOT =       3577
654163                 TA   =          303
24072
                                          MA   =          303
41860
                                          Ha   =            222
237  n
mi
                                          Hp   =            209
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13981166
74                 X    =        -4247432
17
 Y    =      -10103728
88  feet           Y    =        -3127191
93  meter
 Z    =       13998687
60                 Z    =         4246133
41
 XDOT =      19546
064492                 XDOT =        5976
283565
 YDOT =     -10698
618795  feet/sec       YDOT =       -3194
212014  meter/sec
 ZDOT =      11737
710508                 ZDOT =        3606
640640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13164733
83                 X    =        -4012610
87
 Y    =      -11256372
68  feet           Y    =        -3430942
39  meter
 Z    =       13910624
45                 Z    =         4239958
33
 XDOT =      19485
469303                 XDOT =        5939
171044
 YDOT =      -8052
304753  feet/sec       YDOT =       -2454
342489  meter/sec
 ZDOT =      11862
369933                 ZDOT =        3615
650356


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   15077
55549991  
00016717  00000-0  10270-3 0  9149
2 25544  51
6458 176
7503 0008590 114
0292 246
1761 15
55342746 13936


Satellite: ISS
Catalog Number: 25544
Epoch time:      15077
55549991   =   yrday
fracday
Element set:     914
Inclination:       51
6458  deg
RA of node:       176
7503  deg
Eccentricity:     
0008590     
Arg of perigee:   114
0292  deg
Mean anomaly:     246
1761  deg
Mean motion:   15
55342746  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1393
Checksum:              329
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