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

 
Date: August 23rd 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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


239/04:51:15 873 0 7 1 0 1 0
N/A 0 7 -0 1 221 5
000/00:02:31 746 0 2 -0 0 215 2

242/05:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 215 6

246/10:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 215 8

Coasting Arc #1 (Orbit 3221)
---------------------------------------

Vector Time (GMT): 2017/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2447772
49                 A    =         6778547
11  meter
 Y    =        3807281
09  meter          E    =           
0009675
 Z    =        5043613
82                 I    =           51
95512
 XDOT =      -4760
497062                 Wp   =          145
52006
 YDOT =      -5682
583625  meter/sec      RA   =           62
04646  deg
 ZDOT =       1969
640796                 TA   =          285
39622
                                          MA   =          285
50308
                                          Ha   =            221
925  n
mi
                                          Hp   =            214
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8030749
62                 X    =        -2514663
63
 Y    =       12491079
68  feet           Y    =         3779534
82  meter
 Z    =       16547289
42                 Z    =         5031560
70
 XDOT =     -15618
428681                 XDOT =       -4706
166506
 YDOT =     -18643
647063  feet/sec       YDOT =       -5735
514808  meter/sec
 ZDOT =       6462
076104                 ZDOT =        1946
648531

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13162135
31                 X    =         4011818
84
 Y    =       -7004526
95  feet           Y    =        -2134979
82  meter
 Z    =       16493259
06                 Z    =         5027145
36
 XDOT =       4191
785765                 XDOT =        1277
656301
 YDOT =      22929
551181  feet/sec       YDOT =        6988
927200  meter/sec
 ZDOT =       6361
147931                 ZDOT =        1938
877889


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   17235
55160075  
00016717  00000-0  10270-3 0  9004
2 25544  51
6372  62
5046 0004823 172
2324 187
8904 15
54146595 32228


Satellite: ISS
Catalog Number: 25544
Epoch time:      17235
55160075   =   yrday
fracday
Element set:     900
Inclination:       51
6372  deg
RA of node:        62
5046  deg
Eccentricity:     
0004823     
Arg of perigee:   172
2324  deg
Mean anomaly:     187
8904  deg
Mean motion:   15
54146595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3222
Checksum:              296


Coasting Arc #2 (Orbit 3236)
---------------------------------------

Vector Time (GMT): 2017/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3500789
65                 A    =         6777171
75  meter
 Y    =       -2293089
17  meter          E    =           
0016046
 Z    =       -5343832
02                 I    =           51
93459
 XDOT =       4177
458954                 Wp   =          107
81393
 YDOT =       6417
502133  meter/sec      RA   =           57
06660  deg
 ZDOT =        -21
950872                 TA   =          162
00589
                                          MA   =          161
94903
                                          Ha   =            221
770  n
mi
                                          Hp   =            214
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11485530
35                 X    =         3552128
84
 Y    =       -7523258
44  feet           Y    =        -2253654
37  meter
 Z    =      -17532257
29                 Z    =        -5326701
56
 XDOT =      13705
573996                 XDOT =        4105
492893
 YDOT =      21054
797025  feet/sec       YDOT =        6463
814936  meter/sec
 ZDOT =        -72
017297                 ZDOT =          -1
833641

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13773069
18                 X    =        -4198031
49
 Y    =        1219881
73  feet           Y    =          371819
95  meter
 Z    =      -17455982
49                 Z    =        -5320583
46
 XDOT =      -2167
666257                 XDOT =        -660
704675
 YDOT =     -24016
839463  feet/sec       YDOT =       -7320
332668  meter/sec
 ZDOT =         16
039268                 ZDOT =           4
888769


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   17236
51609294  
00016717  00000-0  10270-3 0  9013
2 25544  51
6371  57
6951 0004978 175
6836 184
4360 15
54192823 32373


Satellite: ISS
Catalog Number: 25544
Epoch time:      17236
51609294   =   yrday
fracday
Element set:     901
Inclination:       51
6371  deg
RA of node:        57
6951  deg
Eccentricity:     
0004978     
Arg of perigee:   175
6836  deg
Mean anomaly:     184
4360  deg
Mean motion:   15
54192823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3237
Checksum:              330


Coasting Arc #3 (Orbit 3252)
---------------------------------------

Vector Time (GMT): 2017/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4448512
70                 A    =         6778479
21  meter
 Y    =         736177
21  meter          E    =           
0005098
 Z    =        5056651
50                 I    =           51
92079
 XDOT =      -3283
883769                 Wp   =          109
52864
 YDOT =      -6663
141507  meter/sec      RA   =           52
08630  deg
 ZDOT =      -1918
979217                 TA   =          358
99767
                                          MA   =          358
99870
                                          Ha   =            221
837  n
mi
                                          Hp   =            214
376

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14594857
95                 X    =        -4480976
77
 Y    =        2415279
55  feet           Y    =          686249
82  meter
 Z    =       16590063
96                 Z    =         5034963
24
 XDOT =     -10773
896880                 XDOT =       -3199
809295
 YDOT =     -21860
700482  feet/sec       YDOT =       -6699
394206  meter/sec
 ZDOT =      -6295
863574                 ZDOT =       -1934
726423

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14203888
10                 X    =         4329345
09
 Y    =        4502868
35  feet           Y    =         1372474
27  meter
 Z    =       16493859
94                 Z    =         5027328
51
 XDOT =         -1
186708                 XDOT =           -
361709
 YDOT =      23315
610900  feet/sec       YDOT =        7106
598202  meter/sec
 ZDOT =      -6364
505238                 ZDOT =       -1939
901196


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   17237
54488269  
00016717  00000-0  10270-3 0  9025
2 25544  51
6378  52
5655 0004946 179
8104 180
3052 15
54166291 32535


Satellite: ISS
Catalog Number: 25544
Epoch time:      17237
54488269   =   yrday
fracday
Element set:     902
Inclination:       51
6378  deg
RA of node:        52
5655  deg
Eccentricity:     
0004946     
Arg of perigee:   179
8104  deg
Mean anomaly:     180
3052  deg
Mean motion:   15
54166291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3253
Checksum:              324


Coasting Arc #4 (Orbit 3267)
---------------------------------------

Vector Time (GMT): 2017/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5241608
17                 A    =         6781605
25  meter
 Y    =         749850
72  meter          E    =           
0010690
 Z    =       -4248610
37                 I    =           51
91084
 XDOT =       2046
463265                 Wp   =          136
01295
 YDOT =       6411
700099  meter/sec      RA   =           47
11078  deg
 ZDOT =       3654
412933                 TA   =          171
31705
                                          MA   =          171
29854
                                          Ha   =            221
616  n
mi
                                          Hp   =            214
506

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17196877
20                 X    =         5253471
15
 Y    =        2460140
15  feet           Y    =          808531
96  meter
 Z    =      -13939010
41                 Z    =        -4223119
62
 XDOT =       6714
118324                 XDOT =        1956
862567
 YDOT =      21035
761479  feet/sec       YDOT =        6434
084336  meter/sec
 ZDOT =      11989
543743                 ZDOT =        3664
135858

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14470915
80                 X    =        -4410735
14
 Y    =       -9772879
87  feet           Y    =        -2978773
78  meter
 Z    =      -13826217
88                 Z    =        -4214231
21
 XDOT =       2521
666888                 XDOT =         768
604068
 YDOT =     -20764
786068  feet/sec       YDOT =       -6329
106794  meter/sec
 ZDOT =      12031
527141                 ZDOT =        3667
209472


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   17238
50936973  
00016717  00000-0  10270-3 0  9033
2 25544  51
6379  47
7564 0005024 181
3519 178
7621 15
54200603 32682


Satellite: ISS
Catalog Number: 25544
Epoch time:      17238
50936973   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:        47
7564  deg
Eccentricity:     
0005024     
Arg of perigee:   181
3519  deg
Mean anomaly:     178
7621  deg
Mean motion:   15
54200603  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3268
Checksum:              319


Coasting Arc #5 (Orbit 3278)
---------------------------------------

Vector Time (GMT): 2017/239/04:52:31
746
Vector Time (MET): N/A
Weight (LBS)     : 925114
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4003275
53                 A    =         6778414
27  meter
 Y    =       -1796411
52  meter          E    =           
0014151
 Z    =       -5178677
31                 I    =           51
88590
 XDOT =       4579
773593                 Wp   =          120
07366
 YDOT =       5959
160902  meter/sec      RA   =           43
63497  deg
 ZDOT =       1469
248874                 TA   =          164
06263
                                          MA   =          164
01806
                                          Ha   =            221
464  n
mi
                                          Hp   =            215
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13134106
06                 X    =         4048221
35
 Y    =       -5893738
57  feet           Y    =        -1751393
21  meter
 Z    =      -16990411
12                 Z    =        -5159121
41
 XDOT =      15025
503915                 XDOT =        4505
659430
 YDOT =      19551
052828  feet/sec       YDOT =        6009
960752  meter/sec
 ZDOT =       4820
370322                 ZDOT =        1491
315505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4508827
45                 X    =         1374290
61
 Y    =      -13778892
07  feet           Y    =        -4199806
30  meter
 Z    =      -16903478
19                 Z    =        -5152180
15
 XDOT =      23553
615488                 XDOT =        7179
142001
 YDOT =       1659
450402  feet/sec       YDOT =         505
800482  meter/sec
 ZDOT =       4917
100769                 ZDOT =        1498
732314


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   17239
21665962  
00016717  00000-0  10270-3 0  9040
2 25544  51
6413  44
2346 0004625 195
4755 164
6257 15
54021809 32795


Satellite: ISS
Catalog Number: 25544
Epoch time:      17239
21665962   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:        44
2346  deg
Eccentricity:     
0004625     
Arg of perigee:   195
4755  deg
Mean anomaly:     164
6257  deg
Mean motion:   15
54021809  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3279
Checksum:              319


Coasting Arc #6 (Orbit 3294)
---------------------------------------

Vector Time (GMT): 2017/240/04:52:31
746
Vector Time (MET): N/A
Weight (LBS)     : 925114
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5036133
04                 A    =         6781119
94  meter
 Y    =         501412
61  meter          E    =           
0006962
 Z    =        4506783
49                 I    =           51
87078
 XDOT =      -3486
019803                 Wp   =           98
19686
 YDOT =      -6026
966528  meter/sec      RA   =           38
65819  deg
 ZDOT =      -3221
654930                 TA   =           24
08539
                                          MA   =           24
05285
                                          Ha   =            221
471  n
mi
                                          Hp   =            215
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16522746
19                 X    =        -5063257
36
 Y    =        1645054
48  feet           Y    =          444943
73  meter
 Z    =       14786035
07                 Z    =         4482253
67
 XDOT =     -11437
072845                 XDOT =       -3402
716394
 YDOT =     -19773
512232  feet/sec       YDOT =       -6065
483981  meter/sec
 ZDOT =     -10569
734022                 ZDOT =       -3238
386220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9690885
15                 X    =        -2953781
79
 Y    =       13601394
83  feet           Y    =         4145705
14  meter
 Z    =       14677294
80                 Z    =         4473639
45
 XDOT =     -21380
115304                 XDOT =       -6516
659145
 YDOT =      -3736
804258  feet/sec       YDOT =       -1138
977938  meter/sec
 ZDOT =     -10642
806113                 ZDOT =       -3243
927303


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   17240
24556185  
00016717  00000-0  10270-3 0  9052
2 25544  51
6414  39
1073 0004611 199
8285 160
2689 15
54028731 32957


Satellite: ISS
Catalog Number: 25544
Epoch time:      17240
24556185   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:        39
1073  deg
Eccentricity:     
0004611     
Arg of perigee:   199
8285  deg
Mean anomaly:     160
2689  deg
Mean motion:   15
54028731  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3295
Checksum:              313


Coasting Arc #7 (Orbit 3309)
---------------------------------------

Vector Time (GMT): 2017/241/04:52:31
746
Vector Time (MET): N/A
Weight (LBS)     : 925114
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5835792
09                 A    =         6784780
06  meter
 Y    =         681590
66  meter          E    =           
0004958
 Z    =       -3399678
21                 I    =           51
85821
 XDOT =       2035
967527                 Wp   =          143
13504
 YDOT =       5741
445055  meter/sec      RA   =           33
68676  deg
 ZDOT =       4645
612842                 TA   =          177
31204
                                          MA   =          177
30937
                                          Ha   =            221
182  n
mi
                                          Hp   =            215
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19146299
50                 X    =         5844250
56
 Y    =        2236189
82  feet           Y    =          746897
59  meter
 Z    =      -11153799
91                 Z    =        -3371309
31
 XDOT =       6679
683489                 XDOT =        1949
047800
 YDOT =      18836
761990  feet/sec       YDOT =        5763
726849  meter/sec
 ZDOT =      15241
511950                 ZDOT =        4655
291532

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14098725
65                 X    =         4297291
58
 Y    =      -13251109
06  feet           Y    =        -4038938
04  meter
 Z    =      -11028264
86                 Z    =        -3361415
13
 XDOT =      17676
339671                 XDOT =        5387
748332
 YDOT =       6086
406343  feet/sec       YDOT =        1855
136653  meter/sec
 ZDOT =      15283
384107                 ZDOT =        4658
375476


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   17241
21015330  
00016717  00000-0  10270-3 0  9063
2 25544  51
6425  34
2989 0004564 203
4817 156
6128 15
54046859 33107


Satellite: ISS
Catalog Number: 25544
Epoch time:      17241
21015330   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:        34
2989  deg
Eccentricity:     
0004564     
Arg of perigee:   203
4817  deg
Mean anomaly:     156
6128  deg
Mean motion:   15
54046859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3310
Checksum:              294


Coasting Arc #8 (Orbit 3325)
---------------------------------------

Vector Time (GMT): 2017/242/04:52:31
746
Vector Time (MET): N/A
Weight (LBS)     : 925114
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6270469
74                 A    =         6788159
66  meter
 Y    =       -1704292
85  meter          E    =           
0014462
 Z    =        1933243
28                 I    =           51
84057
 XDOT =       -321
644063                 Wp   =          131
32188
 YDOT =      -5212
833620  meter/sec      RA   =           28
72525  deg
 ZDOT =      -5620
846160                 TA   =           27
41408
                                          MA   =           27
33785
                                          Ha   =            221
247  n
mi
                                          Hp   =            215
489

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20572407
28                 X    =        -6260336
56
 Y    =       -5591511
99  feet           Y    =        -1774356
78  meter
 Z    =        6342661
67                 Z    =         1902808
08
 XDOT =      -1055
262675                 XDOT =        -236
025661
 YDOT =     -17102
472507  feet/sec       YDOT =       -5215
951961  meter/sec
 ZDOT =     -18441
096324                 ZDOT =       -5622
200444

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17351405
25                 X    =        -5288708
32
 Y    =       12454147
75  feet           Y    =         3796024
23  meter
 Z    =        6208159
49                 Z    =         1892247
01
 XDOT =     -12944
870958                 XDOT =       -3945
596668
 YDOT =      -8810
118438  feet/sec       YDOT =       -2685
324100  meter/sec
 ZDOT =     -18446
183064                 ZDOT =       -5622
396598


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   17242
23905004  
00016717  00000-0  10270-3 0  9073
2 25544  51
6417  29
1717 0004618 206
2996 153
7922 15
54009666 33261


Satellite: ISS
Catalog Number: 25544
Epoch time:      17242
23905004   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:        29
1717  deg
Eccentricity:     
0004618     
Arg of perigee:   206
2996  deg
Mean anomaly:     153
7922  deg
Mean motion:   15
54009666  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3326
Checksum:              308


Coasting Arc #9 (Orbit 3325)
---------------------------------------

Vector Time (GMT): 2017/242/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925114
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5021056
35                 A    =         6781504
91  meter
 Y    =       -1208443
37  meter          E    =           
0009292
 Z    =       -4404560
50                 I    =           51
81815
 XDOT =       4275
061157                 Wp   =          139
08346
 YDOT =       5371
943605  meter/sec      RA   =           28
58889  deg
 ZDOT =       3396
784397                 TA   =          165
27392
                                          MA   =          165
24683
                                          Ha   =            221
033  n
mi
                                          Hp   =            215
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16473281
98                 X    =         5055591
42
 Y    =       -3964709
23  feet           Y    =        -1152101
57  meter
 Z    =      -14450657
81                 Z    =        -4380085
94
 XDOT =      14025
791198                 XDOT =        4198
173080
 YDOT =      17624
486892  feet/sec       YDOT =        5419
320474  meter/sec
 ZDOT =      11144
305765                 ZDOT =        3417
364280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4781405
59                 X    =         1457372
42
 Y    =      -16350942
12  feet           Y    =        -4983767
16  meter
 Z    =      -14342046
65                 Z    =        -4371455
82
 XDOT =      21034
195714                 XDOT =        6411
222854
 YDOT =      -3711
421313  feet/sec       YDOT =       -1131
241216  meter/sec
 ZDOT =      11234
516351                 ZDOT =        3424
280584


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   17242
23904851  
00016717  00000-0  10270-3 0  9083
2 25544  51
6420  29
1715 0004556 209
3482 150
7415 15
54038185 33260


Satellite: ISS
Catalog Number: 25544
Epoch time:      17242
23904851   =   yrday
fracday
Element set:     908
Inclination:       51
6420  deg
RA of node:        29
1715  deg
Eccentricity:     
0004556     
Arg of perigee:   209
3482  deg
Mean anomaly:     150
7415  deg
Mean motion:   15
54038185  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3326
Checksum:              297


Coasting Arc #10 (Orbit 3341)
---------------------------------------

Vector Time (GMT): 2017/243/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925114
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5954717
74                 A    =         6785220
14  meter
 Y    =         173832
38  meter          E    =           
0011352
 Z    =        3234050
30                 I    =           51
80182
 XDOT =      -2761
113420                 Wp   =          113
44473
 YDOT =      -5320
063090  meter/sec      RA   =           23
61618  deg
 ZDOT =      -4789
072284                 TA   =           29
17526
                                          MA   =           29
11189
                                          Ha   =            221
022  n
mi
                                          Hp   =            215
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19536475
53                 X    =        -5971928
36
 Y    =         570316
21  feet           Y    =          107146
55  meter
 Z    =       10610401
26                 Z    =         3205082
49
 XDOT =      -9058
771064                 XDOT =       -2678
155022
 YDOT =     -17454
275230  feet/sec       YDOT =       -5350
476057  meter/sec
 ZDOT =     -15712
179410                 ZDOT =       -4802
283164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8937381
38                 X    =        -2724113
85
 Y    =       17459354
82  feet           Y    =         5321611
35  meter
 Z    =       10482074
93                 Z    =         3194936
44
 XDOT =     -18337
917262                 XDOT =       -5589
397181
 YDOT =         98
300471  feet/sec       YDOT =          29
961984  meter/sec
 ZDOT =     -15769
754484                 ZDOT =       -4806
621167


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   17243
26794154  
00016717  00000-0  10270-3 0  9091
2 25544  51
6422  24
0437 0004480 212
8510 147
2364 15
54052188 33425


Satellite: ISS
Catalog Number: 25544
Epoch time:      17243
26794154   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:        24
0437  deg
Eccentricity:     
0004480     
Arg of perigee:   212
8510  deg
Mean anomaly:     147
2364  deg
Mean motion:   15
54052188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3342
Checksum:              290


Coasting Arc #11 (Orbit 3356)
---------------------------------------

Vector Time (GMT): 2017/244/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925114
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6514544
65                 A    =         6788290
69  meter
 Y    =         740882
99  meter          E    =           
0003139
 Z    =       -1754090
56                 I    =           51
78214
 XDOT =        954
984817                 Wp   =           37
56651
 YDOT =       5048
443825  meter/sec      RA   =           18
64943  deg
 ZDOT =       5686
851750                 TA   =          303
22846
                                          MA   =          303
25854
                                          Ha   =            220
739  n
mi
                                          Hp   =            215
760

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21373177
98                 X    =         6514296
17
 Y    =        2430718
46  feet           Y    =          813731
61  meter
 Z    =       -5754890
29                 Z    =        -1722445
81
 XDOT =       3133
152286                 XDOT =         870
837087
 YDOT =      16563
135910  feet/sec       YDOT =        5058
652817  meter/sec
 ZDOT =      18657
650099                 ZDOT =        5691
286175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12132476
11                 X    =         3697978
72
 Y    =      -17807753
84  feet           Y    =        -5427803
37  meter
 Z    =       -5614874
72                 Z    =        -1711413
82
 XDOT =      14759
249011                 XDOT =        4498
619098
 YDOT =       4175
011620  feet/sec       YDOT =        1272
543542  meter/sec
 ZDOT =      18676
399687                 ZDOT =        5692
566625


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   17244
23252360  
00016717  00000-0  10270-3 0  9109
2 25544  51
6425  19
2350 0004497 218
1845 141
8989 15
54057047 33574


Satellite: ISS
Catalog Number: 25544
Epoch time:      17244
23252360   =   yrday
fracday
Element set:     910
Inclination:       51
6425  deg
RA of node:        19
2350  deg
Eccentricity:     
0004497     
Arg of perigee:   218
1845  deg
Mean anomaly:     141
8989  deg
Mean motion:   15
54057047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3357
Checksum:              307


Coasting Arc #12 (Orbit 3372)
---------------------------------------

Vector Time (GMT): 2017/245/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925114
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6602409
45                 A    =         6789665
59  meter
 Y    =       -1546360
14  meter          E    =           
0013303
 Z    =          76011
41                 I    =           51
75435
 XDOT =       1012
973049                 Wp   =          153
76069
 YDOT =      -4640
337971  meter/sec      RA   =           13
68796  deg
 ZDOT =      -6024
067757                 TA   =           25
42156
                                          MA   =           25
35618
                                          Ha   =            220
743  n
mi
                                          Hp   =            215
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21661448
31                 X    =        -6584996
16
 Y    =       -5073360
03  feet           Y    =        -1620095
41  meter
 Z    =         249381
28                 Z    =           43981
65
 XDOT =       3323
402392                 XDOT =        1094
048919
 YDOT =     -15224
205943  feet/sec       YDOT =       -4628
557152  meter/sec
 ZDOT =     -19764
001827                 ZDOT =       -6018
949982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14297171
13                 X    =        -4357777
76
 Y    =       17046958
41  feet           Y    =         5195912
92  meter
 Z    =         107808
87                 Z    =           32860
14
 XDOT =     -10789
547912                 XDOT =       -3288
654203
 YDOT =      -8905
542515  feet/sec       YDOT =       -2714
409359  meter/sec
 ZDOT =     -19740
519873                 ZDOT =       -6016
910457


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   17245
26140950  
00016717  00000-0  10270-3 0  9115
2 25544  51
6417  14
1068 0004579 220
2239 139
8575 15
54013652 33737


Satellite: ISS
Catalog Number: 25544
Epoch time:      17245
26140950   =   yrday
fracday
Element set:     911
Inclination:       51
6417  deg
RA of node:        14
1068  deg
Eccentricity:     
0004579     
Arg of perigee:   220
2239  deg
Mean anomaly:     139
8575  deg
Mean motion:   15
54013652  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3373
Checksum:              296


Coasting Arc #13 (Orbit 3388)
---------------------------------------

Vector Time (GMT): 2017/246/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909883
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6211207
28                 A    =         6788353
06  meter
 Y    =        2220486
54  meter          E    =           
0009625
 Z    =        1587260
75                 I    =           51
71831
 XDOT =      -2951
843408                 Wp   =           70
93738
 YDOT =       4133
156615  meter/sec      RA   =            8
72394  deg
 ZDOT =       5743
617238                 TA   =          306
40262
                                          MA   =          306
49136
                                          Ha   =            220
449  n
mi
                                          Hp   =            215
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20377976
62                 X    =         6178205
54
 Y    =        7285060
81  feet           Y    =         2289760
05  meter
 Z    =        5207548
40                 Z    =         1617352
22
 XDOT =      -9684
525618                 XDOT =       -3025
741417
 YDOT =      13560
225114  feet/sec       YDOT =        4099
734232  meter/sec
 ZDOT =      18843
888577                 ZDOT =        5729
098550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15418566
82                 X    =         4699579
17
 Y    =      -15139365
90  feet           Y    =        -4614478
73  meter
 Z    =        5340412
00                 Z    =         1627757
58
 XDOT =       6832
208908                 XDOT =        2082
457275
 YDOT =      13611
090100  feet/sec       YDOT =        4148
660262  meter/sec
 ZDOT =      18778
868289                 ZDOT =        5723
799054


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   17246
29028935  
00016717  00000-0  10270-3 0  9128
2 25544  51
6413   8
9781 0004594 226
6711 133
4059 15
54078464 33894


Satellite: ISS
Catalog Number: 25544
Epoch time:      17246
29028935   =   yrday
fracday
Element set:     912
Inclination:       51
6413  deg
RA of node:         8
9781  deg
Eccentricity:     
0004594     
Arg of perigee:   226
6711  deg
Mean anomaly:     133
4059  deg
Mean motion:   15
54078464  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3389
Checksum:              326


Coasting Arc #14 (Orbit 3390)
---------------------------------------

Vector Time (GMT): 2017/246/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909883
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6680892
34                 A    =         6788956
47  meter
 Y    =         -40991
56  meter          E    =           
0004551
 Z    =       -1194112
93                 I    =           51
71237
 XDOT =       1074
944007                 Wp   =           35
15152
 YDOT =       4817
924471  meter/sec      RA   =            7
75947  deg
 ZDOT =       5863
523306                 TA   =          311
89511
                                          MA   =          311
93392
                                          Ha   =            220
689  n
mi
                                          Hp   =            215
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21918938
13                 X    =         6686654
53
 Y    =        -134486
73  feet           Y    =           33750
88  meter
 Z    =       -3917693
34                 Z    =        -1161645
63
 XDOT =       3526
719183                 XDOT =         992
507033
 YDOT =      15806
838817  feet/sec       YDOT =        4829
484651  meter/sec
 ZDOT =      19237
281189                 ZDOT =        5868
544470

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14745453
48                 X    =        -4494414
22
 Y    =      -16252244
21  feet           Y    =        -4953684
03  meter
 Z    =       -3773912
63                 Z    =        -1150288
57
 XDOT =       8318
256977                 XDOT =        2535
404727
 YDOT =     -12007
410443  feet/sec       YDOT =       -3659
858703  meter/sec
 ZDOT =      19258
669046                 ZDOT =        5870
042325


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   17246
41890150  
00016717  00000-0  10270-3 0  9139
2 25544  51
6397   8
3321 0004778 220
4391 139
6407 15
54062043 33913


Satellite: ISS
Catalog Number: 25544
Epoch time:      17246
41890150   =   yrday
fracday
Element set:     913
Inclination:       51
6397  deg
RA of node:         8
3321  deg
Eccentricity:     
0004778     
Arg of perigee:   220
4391  deg
Mean anomaly:     139
6407  deg
Mean motion:   15
54062043  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3391
Checksum:              296


Coasting Arc #15 (Orbit 3406)
---------------------------------------

Vector Time (GMT): 2017/247/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909883
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6723130
57                 A    =         6789316
82  meter
 Y    =        -730804
41  meter          E    =           
0012072
 Z    =        -509055
70                 I    =           51
68142
 XDOT =        959
882183                 Wp   =          160
85237
 YDOT =      -4693
275447  meter/sec      RA   =            2
79332  deg
 ZDOT =      -5990
891685                 TA   =           24
63759
                                          MA   =           24
57997
                                          Ha   =            220
424  n
mi
                                          Hp   =            215
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22057514
99                 X    =        -6711986
13
 Y    =       -2397652
27  feet           Y    =         -805924
77  meter
 Z    =       -1670130
26                 Z    =         -541687
05
 XDOT =       3149
219760                 XDOT =        1041
392745
 YDOT =     -15397
885326  feet/sec       YDOT =       -4682
086117  meter/sec
 ZDOT =     -19655
156447                 ZDOT =       -5986
030585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13235439
17                 X    =         4034161
86
 Y    =       17793335
95  feet           Y    =         5423408
80  meter
 Z    =       -1814492
99                 Z    =         -553057
46
 XDOT =     -12221
647849                 XDOT =       -3725
158264
 YDOT =       7104
725399  feet/sec       YDOT =        2165
520302  meter/sec
 ZDOT =     -19632
809412                 ZDOT =       -5984
080309


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   17247
44777745  
00016717  00000-0  10270-3 0  9148
2 25544  51
6397   3
2031 0004623 225
8639 134
2134 15
54088693 34073


Satellite: ISS
Catalog Number: 25544
Epoch time:      17247
44777745   =   yrday
fracday
Element set:     914
Inclination:       51
6397  deg
RA of node:         3
2031  deg
Eccentricity:     
0004623     
Arg of perigee:   225
8639  deg
Mean anomaly:     134
2134  deg
Mean motion:   15
54088693  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3407
Checksum:              315


Coasting Arc #16 (Orbit 3422)
---------------------------------------

Vector Time (GMT): 2017/248/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909883
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6270980
94                 A    =         6787391
96  meter
 Y    =        1455822
50  meter          E    =           
0009687
 Z    =        2139214
60                 I    =           51
64340
 XDOT =      -2921
442813                 Wp   =           81
34400
 YDOT =       4468
901448  meter/sec      RA   =          357
82393  deg
 ZDOT =       5502
884516                 TA   =          302
36762
                                          MA   =          302
46134
                                          Ha   =            220
368  n
mi
                                          Hp   =            215
914

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20574084
44                 X    =         6243844
33
 Y    =        4776320
55  feet           Y    =         1525797
37  meter
 Z    =        7018420
59                 Z    =         2169610
68
 XDOT =      -9584
786132                 XDOT =       -2997
928143
 YDOT =      14661
750158  feet/sec       YDOT =        4435
804768  meter/sec
 ZDOT =      18054
083059                 ZDOT =        5488
507008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10771760
49                 X    =        -3283232
60
 Y    =      -18115511
66  feet           Y    =        -5521607
96  meter
 Z    =        7152749
77                 Z    =         2180158
13
 XDOT =      15976
163694                 XDOT =        4869
534694
 YDOT =      -2371
345923  feet/sec       YDOT =        -722
786237  meter/sec
 ZDOT =      17989
645381                 ZDOT =        5483
243912


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   17248
47664852  
00016717  00000-0  10270-3 0  9157
2 25544  51
6405 358
0753 0004761 228
0289 132
0459 15
54102511 34234


Satellite: ISS
Catalog Number: 25544
Epoch time:      17248
47664852   =   yrday
fracday
Element set:     915
Inclination:       51
6405  deg
RA of node:       358
0753  deg
Eccentricity:     
0004761     
Arg of perigee:   228
0289  deg
Mean anomaly:     132
0459  deg
Mean motion:   15
54102511  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3423
Checksum:              305


Coasting Arc #17 (Orbit 3437)
---------------------------------------

Vector Time (GMT): 2017/249/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909883
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5336834
35                 A    =         6783963
75  meter
 Y    =       -2184169
66  meter          E    =           
0002652
 Z    =       -3572856
66                 I    =           51
59902
 XDOT =       4670
946353                 Wp   =          142
74394
 YDOT =      -4140
804714  meter/sec      RA   =          352
84471  deg
 ZDOT =      -4449
494062                 TA   =           79
48288
                                          MA   =           79
45300
                                          Ha   =            220
185  n
mi
                                          Hp   =            216
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17509299
04                 X    =        -5294658
70
 Y    =       -7165910
97  feet           Y    =        -2243614
36  meter
 Z    =      -11721970
66                 Z    =        -3598678
44
 XDOT =      15324
627141                 XDOT =        4738
516055
 YDOT =     -13585
317304  feet/sec       YDOT =       -4088
193699  meter/sec
 ZDOT =     -14598
077631                 ZDOT =       -4426
639672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7204490
55                 X    =         2195928
72
 Y    =       17416570
81  feet           Y    =         5308570
78  meter
 Z    =      -11835911
71                 Z    =        -3607585
89
 XDOT =     -19236
538436                 XDOT =       -5863
296915
 YDOT =      -1885
565064  feet/sec       YDOT =        -574
720231  meter/sec
 ZDOT =     -14496
176870                 ZDOT =       -4418
434710


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   17249
44121329  
00016717  00000-0  10270-3 0  9163
2 25544  51
6404 353
2680 0004712 232
7098 127
3626 15
54075690 34381


Satellite: ISS
Catalog Number: 25544
Epoch time:      17249
44121329   =   yrday
fracday
Element set:     916
Inclination:       51
6404  deg
RA of node:       353
2680  deg
Eccentricity:     
0004712     
Arg of perigee:   232
7098  deg
Mean anomaly:     127
3626  deg
Mean motion:   15
54075690  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3438
Checksum:              308


Coasting Arc #18 (Orbit 3453)
---------------------------------------

Vector Time (GMT): 2017/250/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909883
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4033115
09                 A    =         6780205
90  meter
 Y    =        2886131
42  meter          E    =           
0006986
 Z    =        4623295
89                 I    =           51
55580
 XDOT =      -6035
672342                 Wp   =          150
07611
 YDOT =       3695
147632  meter/sec      RA   =          347
85256  deg
 ZDOT =       2950
613983                 TA   =          270
45519
                                          MA   =          270
53525
                                          Ha   =            219
970  n
mi
                                          Hp   =            216
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13232004
90                 X    =         3978084
25
 Y    =        9468935
12  feet           Y    =         2930925
32  meter
 Z    =       15168293
61                 Z    =         4642753
42
 XDOT =     -19802
074613                 XDOT =       -6090
876453
 YDOT =      12123
187768  feet/sec       YDOT =        3627
344315  meter/sec
 ZDOT =       9680
492070                 ZDOT =        2921
160175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2814482
79                 X    =         -857854
35
 Y    =      -15944280
69  feet           Y    =        -4859816
76  meter
 Z    =       15253931
19                 Z    =         4649398
23
 XDOT =      21531
926135                 XDOT =        6562
931086
 YDOT =       5359
701858  feet/sec       YDOT =        1633
637126  meter/sec
 ZDOT =       9549
466345                 ZDOT =        2910
677342


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   17250
47007496  
00016717  00000-0  10270-3 0  9177
2 25544  51
6417 348
1395 0004734 237
5431 122
5264 15
54113424 34540


Satellite: ISS
Catalog Number: 25544
Epoch time:      17250
47007496   =   yrday
fracday
Element set:     917
Inclination:       51
6417  deg
RA of node:       348
1395  deg
Eccentricity:     
0004734     
Arg of perigee:   237
5431  deg
Mean anomaly:     122
5264  deg
Mean motion:   15
54113424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3454
Checksum:              301
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