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

 
Date: February 15th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


048/10:50:01 363 1 7 3 1 3 1
N/A -2 5 -0 4 222 1
000/00:11:58 727 0 9 0 2 213 5

Coasting Arc #1 (Orbit 2589)
---------------------------------------

Vector Time (GMT): 2016/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2349548
21                 A    =         6785261
83  meter
 Y    =        5892796
76  meter          E    =           
0020136
 Z    =        2379301
68                 I    =           51
37211
 XDOT =      -5501
339430                 Wp   =          109
20526
 YDOT =        -19
932918  meter/sec      RA   =          309
17744  deg
 ZDOT =      -5352
602195                 TA   =           44
08239
                                          MA   =           43
92204
                                          Ha   =            222
323  n
mi
                                          Hp   =            211
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7708491
52                 X    =        -2426825
80
 Y    =       19333322
71  feet           Y    =         5866090
60  meter
 Z    =        7806107
88                 Z    =         2367700
27
 XDOT =     -18049
013877                 XDOT =       -5474
707306
 YDOT =        -65
396713  feet/sec       YDOT =         -81
303930  meter/sec
 ZDOT =     -17561
030822                 ZDOT =       -5379
261351

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17623425
56                 X    =        -5371620
11
 Y    =       11109155
55  feet           Y    =         3386070
61  meter
 Z    =        7754680
08                 Z    =         2363626
49
 XDOT =     -13677
695765                 XDOT =       -4168
961669
 YDOT =      -9288
616985  feet/sec       YDOT =       -2831
170457  meter/sec
 ZDOT =     -17676
567874                 ZDOT =       -5387
817888


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   16046
53691242  
00016717  00000-0  10270-3 0  9006
2 25544  51
6424 309
6731 0006390 115
9329 244
2483 15
54713674 25907


Satellite: ISS
Catalog Number: 25544
Epoch time:      16046
53691242   =   yrday
fracday
Element set:     900
Inclination:       51
6424  deg
RA of node:       309
6731  deg
Eccentricity:     
0006390     
Arg of perigee:   115
9329  deg
Mean anomaly:     244
2483  deg
Mean motion:   15
54713674  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2590
Checksum:              307


Coasting Arc #2 (Orbit 2604)
---------------------------------------

Vector Time (GMT): 2016/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3412466
47                 A    =         6787357
46  meter
 Y    =       -5836281
95  meter          E    =           
0013649
 Z    =        -570404
76                 I    =           51
36073
 XDOT =       4395
585054                 Wp   =           67
37983
 YDOT =       1999
829946  meter/sec      RA   =          304
18213  deg
 ZDOT =       5954
160921                 TA   =          286
44124
                                          MA   =          286
59122
                                          Ha   =            222
163  n
mi
                                          Hp   =            211
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11195756
12                 X    =         3480246
34
 Y    =      -19147906
67  feet           Y    =        -5797742
54  meter
 Z    =       -1871406
70                 Z    =         -553663
19
 XDOT =      14421
210806                 XDOT =        4343
973405
 YDOT =       6561
121869  feet/sec       YDOT =        2048
695983  meter/sec
 ZDOT =      19534
648691                 ZDOT =        5975
387843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20151221
11                 X    =         6142092
20
 Y    =       -9283638
25  feet           Y    =        -2829652
94  meter
 Z    =       -1797719
81                 Z    =         -547945
00
 XDOT =       7286
918805                 XDOT =        2221
052852
 YDOT =      12095
522922  feet/sec       YDOT =        3686
715387  meter/sec
 ZDOT =      19626
259491                 ZDOT =        5982
083893


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   16047
50105928  
00016717  00000-0  10270-3 0  9016
2 25544  51
6430 304
8618 0006216 119
1602 241
0174 15
54761266 26051


Satellite: ISS
Catalog Number: 25544
Epoch time:      16047
50105928   =   yrday
fracday
Element set:     901
Inclination:       51
6430  deg
RA of node:       304
8618  deg
Eccentricity:     
0006216     
Arg of perigee:   119
1602  deg
Mean anomaly:     241
0174  deg
Mean motion:   15
54761266  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2605
Checksum:              281


Coasting Arc #3 (Orbit 2619)
---------------------------------------

Vector Time (GMT): 2016/048/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1037977
98                 A    =         6781374
51  meter
 Y    =       -5158791
91  meter          E    =           
0012061
 Z    =       -4290251
37                 I    =           51
31844
 XDOT =       5489
414084                 Wp   =          117
35393
 YDOT =      -4022
376464  meter/sec      RA   =          299
37271  deg
 ZDOT =       3510
773900                 TA   =          188
60180
                                          MA   =          188
62249
                                          Ha   =            222
113  n
mi
                                          Hp   =            213
453

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3405439
58                 X    =         -959374
10
 Y    =      -16925170
31  feet           Y    =        -5169959
95  meter
 Z    =      -14075627
84                 Z    =        -4295102
39
 XDOT =      18009
888728                 XDOT =        5516
931765
 YDOT =     -13196
773175  feet/sec       YDOT =       -3960
836186  meter/sec
 ZDOT =      11518
287073                 ZDOT =        3537
506663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10830645
95                 X    =         3301180
89
 Y    =      -13423528
31  feet           Y    =        -4091491
43  meter
 Z    =      -14095662
59                 Z    =        -4296357
96
 XDOT =      20660
324248                 XDOT =        6297
266831
 YDOT =       4459
619130  feet/sec       YDOT =        1359
291911  meter/sec
 ZDOT =      11634
920242                 ZDOT =        3546
323690


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   16048
46519360  
00016717  00000-0  10270-3 0  9022
2 25544  51
6429 300
0492 0003871 133
5657 226
5818 15
54178661 26202


Satellite: ISS
Catalog Number: 25544
Epoch time:      16048
46519360   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:       300
0492  deg
Eccentricity:     
0003871     
Arg of perigee:   133
5657  deg
Mean anomaly:     226
5818  deg
Mean motion:   15
54178661  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2620
Checksum:              308


Coasting Arc #4 (Orbit 2635)
---------------------------------------

Vector Time (GMT): 2016/049/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -69894
84                 A    =         6785256
99  meter
 Y    =        6055885
76  meter          E    =           
0016246
 Z    =        3040722
82                 I    =           51
31621
 XDOT =      -5395
234728                 Wp   =          105
18683
 YDOT =       2406
159625  meter/sec      RA   =          294
36492  deg
 ZDOT =      -4898
372924                 TA   =           39
72711
                                          MA   =           39
60824
                                          Ha   =            222
065  n
mi
                                          Hp   =            213
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -229313
79                 X    =         -152378
29
 Y    =       19868391
60  feet           Y    =         6054643
10  meter
 Z    =        9976124
73                 Z    =         3040182
67
 XDOT =     -17700
901338                 XDOT =       -5397
946310
 YDOT =       7894
224493  feet/sec       YDOT =        2345
811140  meter/sec
 ZDOT =     -16070
777310                 ZDOT =       -4924
587795

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15186519
61                 X    =        -4628851
18
 Y    =       12815804
35  feet           Y    =         3906257
17  meter
 Z    =        9972633
32                 Z    =         3039658
64
 XDOT =     -16568
022989                 XDOT =       -5049
933407
 YDOT =      -6993
277249  feet/sec       YDOT =       -2131
550906  meter/sec
 ZDOT =     -16184
853313                 ZDOT =       -4933
143290


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   16049
49398858  
00016717  00000-0  10270-3 0  9034
2 25544  51
6426 294
9201 0003925 137
4808 222
6649 15
54181034 26363


Satellite: ISS
Catalog Number: 25544
Epoch time:      16049
49398858   =   yrday
fracday
Element set:     903
Inclination:       51
6426  deg
RA of node:       294
9201  deg
Eccentricity:     
0003925     
Arg of perigee:   137
4808  deg
Mean anomaly:     222
6649  deg
Mean motion:   15
54181034  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2636
Checksum:              331


Coasting Arc #5 (Orbit 2650)
---------------------------------------

Vector Time (GMT): 2016/050/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1029873
37                 A    =         6788083
25  meter
 Y    =       -6539870
63  meter          E    =           
0008253
 Z    =       -1494828
68                 I    =           51
31438
 XDOT =       5051
819133                 Wp   =           63
80418
 YDOT =       -510
162034  meter/sec      RA   =          289
36548  deg
 ZDOT =       5740
739837                 TA   =          279
80710
                                          MA   =          279
90028
                                          Ha   =            221
909  n
mi
                                          Hp   =            213
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3378849
64                 X    =         1110188
35
 Y    =      -21456268
46  feet           Y    =        -6527904
92  meter
 Z    =       -4904293
58                 Z    =        -1489630
48
 XDOT =      16574
209753                 XDOT =        5029
263028
 YDOT =      -1673
759955  feet/sec       YDOT =        -453
795025  meter/sec
 ZDOT =      18834
448285                 ZDOT =        5765
224992

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18228944
81                 X    =         5556182
38
 Y    =      -11820580
31  feet           Y    =        -3602912
88  meter
 Z    =       -4880535
72                 Z    =        -1487587
29
 XDOT =      11388
247132                 XDOT =        3471
137726
 YDOT =       9780
431677  feet/sec       YDOT =        2981
075575  meter/sec
 ZDOT =      18940
668386                 ZDOT =        5773
115724


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   16050
45846876  
00016717  00000-0  10270-3 0  9041
2 25544  51
6431 290
1111 0003777 141
8907 218
2514 15
54232148 26513


Satellite: ISS
Catalog Number: 25544
Epoch time:      16050
45846876   =   yrday
fracday
Element set:     904
Inclination:       51
6431  deg
RA of node:       290
1111  deg
Eccentricity:     
0003777     
Arg of perigee:   141
8907  deg
Mean anomaly:     218
2514  deg
Mean motion:   15
54232148  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2651
Checksum:              298


Coasting Arc #6 (Orbit 2666)
---------------------------------------

Vector Time (GMT): 2016/051/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1883141
87                 A    =         6789075
95  meter
 Y    =        6509617
28  meter          E    =           
0015336
 Z    =        -260280
26                 I    =           51
30750
 XDOT =      -4548
330320                 Wp   =          139
24225
 YDOT =      -1546
446119  meter/sec      RA   =          284
37154  deg
 ZDOT =      -5980
300756                 TA   =           43
57634
                                          MA   =           43
45530
                                          Ha   =            221
868  n
mi
                                          Hp   =            213
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6178286
97                 X    =        -1954529
76
 Y    =       21357012
09  feet           Y    =         6488159
57  meter
 Z    =        -853937
88                 Z    =         -269601
74
 XDOT =     -14922
343570                 XDOT =       -4501
650520
 YDOT =      -5073
642124  feet/sec       YDOT =       -1597
048008  meter/sec
 ZDOT =     -19620
409303                 ZDOT =       -6002
281373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19833087
15                 X    =        -6045124
96
 Y    =       10043358
83  feet           Y    =         3061215
77  meter
 Z    =        -895546
00                 Z    =         -272962
42
 XDOT =      -5641
051033                 XDOT =       -1719
392355
 YDOT =     -12838
753020  feet/sec       YDOT =       -3913
251921  meter/sec
 ZDOT =     -19715
393732                 ZDOT =       -6009
252010


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   16051
48723491  
00016717  00000-0  10270-3 0  9053
2 25544  51
6429 284
9816 0003834 147
3886 212
7504 15
54205371 26677


Satellite: ISS
Catalog Number: 25544
Epoch time:      16051
48723491   =   yrday
fracday
Element set:     905
Inclination:       51
6429  deg
RA of node:       284
9816  deg
Eccentricity:     
0003834     
Arg of perigee:   147
3886  deg
Mean anomaly:     212
7504  deg
Mean motion:   15
54205371  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2667
Checksum:              324


Coasting Arc #7 (Orbit 2682)
---------------------------------------

Vector Time (GMT): 2016/052/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2568942
15                 A    =         6787326
02  meter
 Y    =       -5966196
83  meter          E    =           
0014918
 Z    =        1950263
18                 I    =           51
29465
 XDOT =       3934
545869                 Wp   =           81
40570
 YDOT =       3523
125305  meter/sec      RA   =          279
37508  deg
 ZDOT =       5560
807311                 TA   =          300
21651
                                          MA   =          300
36415
                                          Ha   =            221
700  n
mi
                                          Hp   =            213
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8428287
90                 X    =         2625993
41
 Y    =      -19574136
58  feet           Y    =        -5937150
04  meter
 Z    =        6398501
26                 Z    =         1962881
27
 XDOT =      12908
615055                 XDOT =        3867
845641
 YDOT =      11558
810056  feet/sec       YDOT =        3566
751580  meter/sec
 ZDOT =      18244
118475                 ZDOT =        5579
757551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19910947
17                 X    =         6068856
70
 Y    =       -7551165
23  feet           Y    =        -2301595
16  meter
 Z    =        6454282
65                 Z    =         1967265
35
 XDOT =          7
985611                 XDOT =           2
434014
 YDOT =      15780
196526  feet/sec       YDOT =        4809
803901  meter/sec
 ZDOT =      18325
612471                 ZDOT =        5585
646681


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   16052
51598493  
00016717  00000-0  10270-3 0  9061
2 25544  51
6424 279
8517 0003558 149
2057 210
9305 15
54254447 26832


Satellite: ISS
Catalog Number: 25544
Epoch time:      16052
51598493   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:       279
8517  deg
Eccentricity:     
0003558     
Arg of perigee:   149
2057  deg
Mean anomaly:     210
9305  deg
Mean motion:   15
54254447  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2683
Checksum:              327


Coasting Arc #8 (Orbit 2697)
---------------------------------------

Vector Time (GMT): 2016/053/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3166415
43                 A    =         6783753
82  meter
 Y    =        4894205
65  meter          E    =           
0007083
 Z    =       -3472539
00                 I    =           51
27816
 XDOT =      -3227
207850                 Wp   =          114
33528
 YDOT =      -5284
685139  meter/sec      RA   =          274
37094  deg
 ZDOT =      -4515
700817                 TA   =          106
65838
                                          MA   =          106
58061
                                          Ha   =            221
536  n
mi
                                          Hp   =            213
786

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10388502
08                 X    =        -3204040
61
 Y    =       16057105
16  feet           Y    =         4858585
93  meter
 Z    =      -11392844
49                 Z    =        -3488012
22
 XDOT =     -10587
952264                 XDOT =       -3145
938520
 YDOT =     -17338
205837  feet/sec       YDOT =       -5320
320017  meter/sec
 ZDOT =     -14815
291393                 ZDOT =       -4531
179442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18650827
59                 X    =        -5684772
25
 Y    =        4042938
68  feet           Y    =         1232287
71  meter
 Z    =      -11460793
35                 Z    =        -3493249
81
 XDOT =       5153
814501                 XDOT =        1570
882660
 YDOT =     -18315
938511  feet/sec       YDOT =       -5582
698058  meter/sec
 ZDOT =     -14881
430762                 ZDOT =       -4535
860096


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   16053
48042434  
00016717  00000-0  10270-3 0  9078
2 25544  51
6420 275
0425 0003523 156
6131 203
5182 15
54266186 26981


Satellite: ISS
Catalog Number: 25544
Epoch time:      16053
48042434   =   yrday
fracday
Element set:     907
Inclination:       51
6420  deg
RA of node:       275
0425  deg
Eccentricity:     
0003523     
Arg of perigee:   156
6131  deg
Mean anomaly:     203
5182  deg
Mean motion:   15
54266186  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2698
Checksum:              293


Coasting Arc #9 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2016/054/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3634496
76                 A    =         6779873
13  meter
 Y    =       -3428215
36  meter          E    =           
0011260
 Z    =        4578503
93                 I    =           51
26358
 XDOT =       2469
507984                 Wp   =          126
27795
 YDOT =       6620
758872  meter/sec      RA   =          269
35507  deg
 ZDOT =       2985
343809                 TA   =          293
73482
                                          MA   =          293
85289
                                          Ha   =            221
444  n
mi
                                          Hp   =            213
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11924201
96                 X    =         3650321
85
 Y    =      -11247425
72  feet           Y    =        -3387482
94  meter
 Z    =       15021338
36                 Z    =         4596197
91
 XDOT =       8102
060316                 XDOT =        2380
788267
 YDOT =      21721
649844  feet/sec       YDOT =        6647
878866  meter/sec
 ZDOT =       9794
435068                 ZDOT =        2997
123487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16319982
63                 X    =         4974330
71
 Y    =         144874
72  feet           Y    =           44157
82  meter
 Z    =       15098641
06                 Z    =         4602065
80
 XDOT =      -9320
550236                 XDOT =       -2840
903712
 YDOT =      20009
553424  feet/sec       YDOT =        6098
911883  meter/sec
 ZDOT =       9844
317941                 ZDOT =        3000
548108


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   16054
50914675  
00016717  00000-0  10270-3 0  9088
2 25544  51
6417 269
9121 0003464 156
6901 203
4409 15
54288275 27144


Satellite: ISS
Catalog Number: 25544
Epoch time:      16054
50914675   =   yrday
fracday
Element set:     908
Inclination:       51
6417  deg
RA of node:       269
9121  deg
Eccentricity:     
0003464     
Arg of perigee:   156
6901  deg
Mean anomaly:     203
4409  deg
Mean motion:   15
54288275  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2714
Checksum:              316


Coasting Arc #10 (Orbit 2728)
---------------------------------------

Vector Time (GMT): 2016/055/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4032934
45                 A    =         6777131
02  meter
 Y    =        1647846
20  meter          E    =           
0015109
 Z    =       -5204215
23                 I    =           51
25526
 XDOT =      -1617
986605                 Wp   =           94
19468
 YDOT =      -7404
590390  meter/sec      RA   =          264
32860  deg
 ZDOT =      -1094
572574                 TA   =          165
26759
                                          MA   =          165
22351
                                          Ha   =            221
292  n
mi
                                          Hp   =            213
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13231412
23                 X    =        -4025781
94
 Y    =        5406319
57  feet           Y    =         1602786
54  meter
 Z    =      -17074196
96                 Z    =        -5223788
72
 XDOT =      -5308
355003                 XDOT =       -1529
749520
 YDOT =     -24293
275558  feet/sec       YDOT =       -7422
190576  meter/sec
 ZDOT =      -3591
117370                 ZDOT =       -1102
216889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13275522
04                 X    =        -4046379
12
 Y    =       -5014455
89  feet           Y    =        -1528406
16  meter
 Z    =      -17159327
19                 Z    =        -5230162
93
 XDOT =      12366
874682                 XDOT =        3769
423403
 YDOT =     -20385
967525  feet/sec       YDOT =       -6213
642902  meter/sec
 ZDOT =      -3622
953828                 ZDOT =       -1104
276327


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   16055
47355820  
00016717  00000-0  10270-3 0  9097
2 25544  51
6407 265
1016 0003341 163
0404 197
0861 15
54344285 27298


Satellite: ISS
Catalog Number: 25544
Epoch time:      16055
47355820   =   yrday
fracday
Element set:     909
Inclination:       51
6407  deg
RA of node:       265
1016  deg
Eccentricity:     
0003341     
Arg of perigee:   163
0404  deg
Mean anomaly:     197
0861  deg
Mean motion:   15
54344285  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2729
Checksum:              299


Coasting Arc #11 (Orbit 2744)
---------------------------------------

Vector Time (GMT): 2016/056/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4308719
59                 A    =         6776946
86  meter
 Y    =         236894
79  meter          E    =           
0003967
 Z    =        5222110
07                 I    =           51
25921
 XDOT =        688
183356                 Wp   =          112
51727
 YDOT =       7586
533969  meter/sec      RA   =          259
29928  deg
 ZDOT =       -912
906422                 TA   =          346
25223
                                          MA   =          346
26303
                                          Ha   =            221
073  n
mi
                                          Hp   =            213
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14136219
12                 X    =         4280383
93
 Y    =         777213
86  feet           Y    =          284920
04  meter
 Z    =       17132907
04                 Z    =         5242971
59
 XDOT =       2257
819410                 XDOT =         607
732151
 YDOT =      24890
203309  feet/sec       YDOT =        7593
779736  meter/sec
 ZDOT =      -2995
099809                 ZDOT =        -909
759901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9885802
52                 X    =         3013192
61
 Y    =        9980099
69  feet           Y    =         3041934
39  meter
 Z    =       17223291
63                 Z    =         5249659
29
 XDOT =     -14267
520896                 XDOT =       -4348
740369
 YDOT =      19274
995104  feet/sec       YDOT =        5875
018508  meter/sec
 ZDOT =      -2982
775033                 ZDOT =        -909
149830


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   16056
50225061  
00016717  00000-0  10270-3 0  9107
2 25544  51
6409 259
9715 0003354 167
6618 192
4618 15
54358621 27454


Satellite: ISS
Catalog Number: 25544
Epoch time:      16056
50225061   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:       259
9715  deg
Eccentricity:     
0003354     
Arg of perigee:   167
6618  deg
Mean anomaly:     192
4618  deg
Mean motion:   15
54358621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2745
Checksum:              315


Coasting Arc #12 (Orbit 2759)
---------------------------------------

Vector Time (GMT): 2016/057/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4471619
19                 A    =         6779272
17  meter
 Y    =       -2077151
87  meter          E    =           
0012578
 Z    =       -4665178
60                 I    =           51
27296
 XDOT =        352
530975                 Wp   =          122
93260
 YDOT =      -7109
010074  meter/sec      RA   =          254
27174  deg
 ZDOT =       2826
205006                 TA   =          175
30532
                                          MA   =          175
29352
                                          Ha   =            221
098  n
mi
                                          Hp   =            213
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14670666
64                 X    =        -4425398
44
 Y    =       -6814802
73  feet           Y    =        -2126898
68  meter
 Z    =      -15305704
05                 Z    =        -4686787
82
 XDOT =       1156
597688                 XDOT =         418
271148
 YDOT =     -23323
523866  feet/sec       YDOT =       -7104
699881  meter/sec
 ZDOT =       9272
326136                 ZDOT =        2828
078129

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6498018
17                 X    =        -1980595
94
 Y    =      -14716678
18  feet           Y    =        -4485643
51  meter
 Z    =      -15399016
71                 Z    =        -4693620
29
 XDOT =      15087
725178                 XDOT =        4598
738634
 YDOT =     -16377
777643  feet/sec       YDOT =       -4991
946626  meter/sec
 ZDOT =       9281
663746                 ZDOT =        2829
051110


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   16057
46663586  
00016717  00000-0  10270-3 0  9112
2 25544  51
6398 255
1602 0003291 171
9916 188
1290 15
54381890 27602


Satellite: ISS
Catalog Number: 25544
Epoch time:      16057
46663586   =   yrday
fracday
Element set:     911
Inclination:       51
6398  deg
RA of node:       255
1602  deg
Eccentricity:     
0003291     
Arg of perigee:   171
9916  deg
Mean anomaly:     188
1290  deg
Mean motion:   15
54381890  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2760
Checksum:              328


Coasting Arc #13 (Orbit 2775)
---------------------------------------

Vector Time (GMT): 2016/058/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4438650
84                 A    =         6783000
79  meter
 Y    =        3690423
47  meter          E    =           
0012387
 Z    =        3549109
87                 I    =           51
29613
 XDOT =      -1498
590097                 Wp   =          101
72082
 YDOT =       6079
133529  meter/sec      RA   =          249
25584  deg
 ZDOT =      -4436
302992                 TA   =           36
12303
                                          MA   =           36
03941
                                          Ha   =            220
763  n
mi
                                          Hp   =            214
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14562502
76                 X    =         4379813
82
 Y    =       12107688
55  feet           Y    =         3739730
89  meter
 Z    =       11644061
26                 Z    =         3570528
17
 XDOT =      -4916
634177                 XDOT =       -1544
907624
 YDOT =      19944
663808  feet/sec       YDOT =        6062
115755  meter/sec
 ZDOT =     -14554
799844                 ZDOT =       -4443
695983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3274814
06                 X    =          998163
33
 Y    =       18595217
70  feet           Y    =         5667822
36  meter
 Z    =       11736278
92                 Z    =         3577217
82
 XDOT =     -15184
061703                 XDOT =       -4628
102007
 YDOT =      11903
097692  feet/sec       YDOT =        3628
064176  meter/sec
 ZDOT =     -14587
878955                 ZDOT =       -4446
385506


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   16058
49529734  
00016717  00000-0  10270-3 0  9123
2 25544  51
6404 250
0299 0003121 178
1484 181
9681 15
54436249 27768


Satellite: ISS
Catalog Number: 25544
Epoch time:      16058
49529734   =   yrday
fracday
Element set:     912
Inclination:       51
6404  deg
RA of node:       250
0299  deg
Eccentricity:     
0003121     
Arg of perigee:   178
1484  deg
Mean anomaly:     181
9681  deg
Mean motion:   15
54436249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2776
Checksum:              325


Coasting Arc #14 (Orbit 2790)
---------------------------------------

Vector Time (GMT): 2016/059/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4192936
85                 A    =         6786676
37  meter
 Y    =       -4930557
57  meter          E    =           
0004554
 Z    =       -2041679
77                 I    =           51
31907
 XDOT =       2699
974351                 Wp   =           68
17542
 YDOT =      -4577
645598  meter/sec      RA   =          244
25060  deg
 ZDOT =       5521
535758                 TA   =          269
15788
                                          MA   =          269
21006
                                          Ha   =            220
870  n
mi
                                          Hp   =            214
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13756354
50                 X    =        -4127572
97
 Y    =      -16176369
99  feet           Y    =        -4977080
55  meter
 Z    =       -6698424
43                 Z    =        -2061888
52
 XDOT =       8858
183567                 XDOT =        2724
140985
 YDOT =     -15018
522303  feet/sec       YDOT =       -4547
316915  meter/sec
 ZDOT =      18115
274796                 ZDOT =        5534
710707

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -425784
18                 X    =         -129779
02
 Y    =      -21202851
15  feet           Y    =        -6462629
03  meter
 Z    =       -6785199
76                 Z    =        -2068128
89
 XDOT =      14712
535192                 XDOT =        4484
380726
 YDOT =      -6099
082509  feet/sec       YDOT =       -1859
000349  meter/sec
 ZDOT =      18173
158822                 ZDOT =        5539
178809


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   16059
45965555  
00016717  00000-0  10270-3 0  9136
2 25544  51
6390 245
2189 0003237 180
9307 179
1841 15
54415497 27915


Satellite: ISS
Catalog Number: 25544
Epoch time:      16059
45965555   =   yrday
fracday
Element set:     913
Inclination:       51
6390  deg
RA of node:       245
2189  deg
Eccentricity:     
0003237     
Arg of perigee:   180
9307  deg
Mean anomaly:     179
1841  deg
Mean motion:   15
54415497  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2791
Checksum:              335


Coasting Arc #15 (Orbit 2806)
---------------------------------------

Vector Time (GMT): 2016/060/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3639785
41                 A    =         6788320
82  meter
 Y    =        5714565
13  meter          E    =           
0014694
 Z    =         258689
43                 I    =           51
33998
 XDOT =      -3919
035611                 Wp   =          141
57840
 YDOT =       2774
795420  meter/sec      RA   =          239
25606  deg
 ZDOT =      -5983
376221                 TA   =           35
62098
                                          MA   =           35
52300
                                          Ha   =            220
690  n
mi
                                          Hp   =            214
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11941553
17                 X    =         3574356
61
 Y    =       18748573
27  feet           Y    =         5754901
82  meter
 Z    =         848718
59                 Z    =          276210
95
 XDOT =     -12857
728382                 XDOT =       -3920
708303
 YDOT =       9103
659514  feet/sec       YDOT =        2730
960166  meter/sec
 ZDOT =     -19630
499412                 ZDOT =       -6002
418156

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2195739
48                 X    =         -669261
39
 Y    =       22116859
52  feet           Y    =         6741218
78  meter
 Z    =         923725
20                 Z    =          281551
44
 XDOT =     -14021
519596                 XDOT =       -4273
759173
 YDOT =       -547
054300  feet/sec       YDOT =        -166
742151  meter/sec
 ZDOT =     -19713
515029                 ZDOT =       -6008
679381


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   16060
48828719  
00016717  00000-0  10270-3 0  9142
2 25544  51
6393 240
0885 0003071 184
3779 175
7348 15
54465039 28070


Satellite: ISS
Catalog Number: 25544
Epoch time:      16060
48828719   =   yrday
fracday
Element set:     914
Inclination:       51
6393  deg
RA of node:       240
0885  deg
Eccentricity:     
0003071     
Arg of perigee:   184
3779  deg
Mean anomaly:     175
7348  deg
Mean motion:   15
54465039  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2807
Checksum:              336


Coasting Arc #16 (Orbit 2821)
---------------------------------------

Vector Time (GMT): 2016/061/10:56:00
727
Vector Time (MET): N/A
Weight (LBS)     : 922145
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2800127
74                 A    =         6787372
61  meter
 Y    =       -5985586
82  meter          E    =           
0012281
 Z    =        1529699
29                 I    =           51
35281
 XDOT =       5018
301241                 Wp   =           74
51988
 YDOT =       -873
677075  meter/sec      RA   =          234
26199  deg
 ZDOT =       5732
129880                 TA   =          302
26377
                                          MA   =          302
38271
                                          Ha   =            220
669  n
mi
                                          Hp   =            214
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9186770
81                 X    =        -2740417
89
 Y    =      -19637752
04  feet           Y    =        -6016565
70  meter
 Z    =        5018698
46                 Z    =         1516242
67
 XDOT =      16464
242916                 XDOT =        4999
853915
 YDOT =      -2866
394602  feet/sec       YDOT =        -817
661692  meter/sec
 ZDOT =      18806
200395                 ZDOT =        5756
462640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4517003
44                 X    =         1376782
65
 Y    =      -21218084
50  feet           Y    =        -6467272
15  meter
 Z    =        4961347
35                 Z    =         1512218
67
 XDOT =      13207
016644                 XDOT =        4025
498673
 YDOT =       7261
041557  feet/sec       YDOT =        2213
165467  meter/sec
 ZDOT =      18911
843094                 ZDOT =        5764
329775


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   16061
51690334  
00016717  00000-0  10270-3 0  9158
2 25544  51
6381 234
9565 0003230 188
0786 172
0315 15
54468864 28220


Satellite: ISS
Catalog Number: 25544
Epoch time:      16061
51690334   =   yrday
fracday
Element set:     915
Inclination:       51
6381  deg
RA of node:       234
9565  deg
Eccentricity:     
0003230     
Arg of perigee:   188
0786  deg
Mean anomaly:     172
0315  deg
Mean motion:   15
54468864  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2822
Checksum:              312
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