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

 
Date: October 17th 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) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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


290/03:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 213 6

294/08:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 3

299/12:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 212 8

303/19:34:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 212 6

Coasting Arc #1 (Orbit 61)
---------------------------------------

Vector Time (GMT): 2017/289/13:18:28
229
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1266431
86                 A    =         6779995
58  meter
 Y    =        4793709
87  meter          E    =           
0011724
 Z    =       -4633957
14                 I    =           51
79911
 XDOT =      -6979
333382                 Wp   =           85
06896
 YDOT =       1032
751320  meter/sec      RA   =          152
14716  deg
 ZDOT =       2983
239279                 TA   =          214
60092
                                          MA   =          214
67726
                                          Ha   =            222
093  n
mi
                                          Hp   =            213
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4154960
16                 X    =        -1297432
51
 Y    =       15727394
60  feet           Y    =         4779373
93  meter
 Z    =      -15203271
44                 Z    =        -4640184
96
 XDOT =     -22898
075400                 XDOT =       -7004
854453
 YDOT =       3388
291733  feet/sec       YDOT =         954
561275  meter/sec
 ZDOT =       9787
530442                 ZDOT =        2949
273336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8007274
77                 X    =        -2440617
35
 Y    =      -14129364
59  feet           Y    =        -4306630
33  meter
 Z    =      -15231503
68                 Z    =        -4642562
32
 XDOT =      13132
795955                 XDOT =        4002
876207
 YDOT =     -17804
591449  feet/sec       YDOT =       -5426
839474  meter/sec
 ZDOT =       9636
773308                 ZDOT =        2937
288504


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   17289
56535255  
00016717  00000-0  10270-3 0  9000
2 25544  51
6389 153
2478 0004983  22
1446 337
9921 15
54200052   623


Satellite: ISS
Catalog Number: 25544
Epoch time:      17289
56535255   =   yrday
fracday
Element set:     900
Inclination:       51
6389  deg
RA of node:       153
2478  deg
Eccentricity:     
0004983     
Arg of perigee:    22
1446  deg
Mean anomaly:     337
9921  deg
Mean motion:   15
54200052  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              62
Checksum:              307


Coasting Arc #2 (Orbit 70)
---------------------------------------

Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2201540
48                 A    =         6777229
84  meter
 Y    =        3574683
78  meter          E    =           
0017881
 Z    =       -5335271
33                 I    =           51
80522
 XDOT =      -6560
217659                 Wp   =           75
30385
 YDOT =       3946
030294  meter/sec      RA   =          149
31935  deg
 ZDOT =        -58
868207                 TA   =          194
11054
                                          MA   =          194
16056
                                          Ha   =            222
276  n
mi
                                          Hp   =            213
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7222901
85                 X    =         2187320
30
 Y    =       11727965
17  feet           Y    =         3599222
80  meter
 Z    =      -17504171
04                 Z    =        -5324611
72
 XDOT =     -21523
023814                 XDOT =       -6603
569695
 YDOT =      12946
293616  feet/sec       YDOT =        3872
427057  meter/sec
 ZDOT =       -193
137161                 ZDOT =         -90
841900

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13479410
82                 X    =         4108524
42
 Y    =       -3107672
88  feet           Y    =         -947218
69  meter
 Z    =      -17457357
63                 Z    =        -5321002
60
 XDOT =       4985
079014                 XDOT =        1519
452084
 YDOT =      23585
543572  feet/sec       YDOT =        7188
873681  meter/sec
 ZDOT =       -335
441604                 ZDOT =        -102
242601


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   17290
14404836  
00016717  00000-0  10270-3 0  9017
2 25544  51
6382 150
3634 0005055  28
3480 331
7947 15
54174604   718


Satellite: ISS
Catalog Number: 25544
Epoch time:      17290
14404836   =   yrday
fracday
Element set:     901
Inclination:       51
6382  deg
RA of node:       150
3634  deg
Eccentricity:     
0005055     
Arg of perigee:    28
3480  deg
Mean anomaly:     331
7947  deg
Mean motion:   15
54174604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              71
Checksum:              289


Coasting Arc #3 (Orbit 86)
---------------------------------------

Vector Time (GMT): 2017/291/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -583154
87                 A    =         6778283
50  meter
 Y    =       -4472438
24  meter          E    =           
0010392
 Z    =        5055806
77                 I    =           51
83542
 XDOT =       6785
512170                 Wp   =           43
85191
 YDOT =      -3037
369049  meter/sec      RA   =          144
33167  deg
 ZDOT =      -1894
594420                 TA   =           64
50786
                                          MA   =           64
40040
                                          Ha   =            222
295  n
mi
                                          Hp   =            213
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1913237
77                 X    =         -557658
61
 Y    =      -14673353
80  feet           Y    =        -4478816
34  meter
 Z    =       16587292
55                 Z    =         5053036
37
 XDOT =      22262
179034                 XDOT =        6828
175704
 YDOT =      -9965
121553  feet/sec       YDOT =       -2961
250488  meter/sec
 ZDOT =      -6215
860958                 ZDOT =       -1861
527940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14575674
44                 X    =        -4442665
57
 Y    =       -2627877
02  feet           Y    =         -800976
92  meter
 Z    =       16575585
72                 Z    =         5052238
53
 XDOT =      -2749
205876                 XDOT =        -837
957951
 YDOT =     -23230
611945  feet/sec       YDOT =       -7080
690521  meter/sec
 ZDOT =      -6068
811965                 ZDOT =       -1849
773887


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   17291
17283596  
00016717  00000-0  10270-3 0  9020
2 25544  51
6369 145
2340 0005110  30
4224 329
7224 15
54198022   874


Satellite: ISS
Catalog Number: 25544
Epoch time:      17291
17283596   =   yrday
fracday
Element set:     902
Inclination:       51
6369  deg
RA of node:       145
2340  deg
Eccentricity:     
0005110     
Arg of perigee:    30
4224  deg
Mean anomaly:     329
7224  deg
Mean motion:   15
54198022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              87
Checksum:              288


Coasting Arc #4 (Orbit 101)
---------------------------------------

Vector Time (GMT): 2017/292/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -916021
98                 A    =         6781457
90  meter
 Y    =        5198803
89  meter          E    =           
0010763
 Z    =       -4265253
84                 I    =           51
87140
 XDOT =      -6496
089303                 Wp   =           82
71304
 YDOT =       1824
202733  meter/sec      RA   =          139
35290  deg
 ZDOT =       3627
759588                 TA   =          224
25719
                                          MA   =          224
34331
                                          Ha   =            222
391  n
mi
                                          Hp   =            213
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3005321
44                 X    =         -953369
34
 Y    =       17056443
22  feet           Y    =         5188351
03  meter
 Z    =      -13993614
95                 Z    =        -4269794
96
 XDOT =     -21312
628946                 XDOT =       -6533
627483
 YDOT =       5984
917102  feet/sec       YDOT =        1751
349530  meter/sec
 ZDOT =      11902
098385                 ZDOT =        3596
111540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15447184
96                 X    =         4708301
98
 Y    =        7794576
94  feet           Y    =         2375787
05  meter
 Z    =      -14014439
65                 Z    =        -4271601
21
 XDOT =          7
233330                 XDOT =           2
204719
 YDOT =      21078
526166  feet/sec       YDOT =        6424
734775  meter/sec
 ZDOT =      11761
484237                 ZDOT =        3584
900395


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   17292
13732254  
00016717  00000-0  10270-3 0  9038
2 25544  51
6364 140
4260 0005181  33
9995 326
1489 15
54177544  1026


Satellite: ISS
Catalog Number: 25544
Epoch time:      17292
13732254   =   yrday
fracday
Element set:     903
Inclination:       51
6364  deg
RA of node:       140
4260  deg
Eccentricity:     
0005181     
Arg of perigee:    33
9995  deg
Mean anomaly:     326
1489  deg
Mean motion:   15
54177544  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             102
Checksum:              298


Coasting Arc #5 (Orbit 117)
---------------------------------------

Vector Time (GMT): 2017/293/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2265317
90                 A    =         6785256
05  meter
 Y    =       -5653742
15  meter          E    =           
0016332
 Z    =        2979763
57                 I    =           51
90883
 XDOT =       5804
673128                 Wp   =           81
27165
 YDOT =       -324
460617  meter/sec      RA   =          134
38455  deg
 ZDOT =      -5002
765959                 TA   =           64
78473
                                          MA   =           64
61550
                                          Ha   =            222
344  n
mi
                                          Hp   =            213
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7432145
33                 X    =         2313896
59
 Y    =      -18549022
81  feet           Y    =        -5628137
91  meter
 Z    =        9776127
20                 Z    =         2990886
59
 XDOT =      19044
203177                 XDOT =        5832
171504
 YDOT =      -1064
503335  feet/sec       YDOT =        -259
395523  meter/sec
 ZDOT =     -16413
274143                 ZDOT =       -4974
501137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15778413
04                 X    =        -4809260
29
 Y    =      -12221406
35  feet           Y    =        -3725084
66  meter
 Z    =        9826220
19                 Z    =         2995031
91
 XDOT =       3394
400270                 XDOT =        1034
613202
 YDOT =     -17545
673477  feet/sec       YDOT =       -5347
921276  meter/sec
 ZDOT =     -16287
852927                 ZDOT =       -4964
537572


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   17293
16610355  
00016717  00000-0  10270-3 0  9040
2 25544  51
6366 135
2959 0005186  36
4778 323
6727 15
54222181  1189


Satellite: ISS
Catalog Number: 25544
Epoch time:      17293
16610355   =   yrday
fracday
Element set:     904
Inclination:       51
6366  deg
RA of node:       135
2959  deg
Eccentricity:     
0005186     
Arg of perigee:    36
4778  deg
Mean anomaly:     323
6727  deg
Mean motion:   15
54222181  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             118
Checksum:              313


Coasting Arc #6 (Orbit 132)
---------------------------------------

Vector Time (GMT): 2017/294/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3297075
32                 A    =         6788170
93  meter
 Y    =        5755838
05  meter          E    =           
0013705
 Z    =       -1416306
97                 I    =           51
94081
 XDOT =      -4808
536527                 Wp   =           39
38189
 YDOT =      -1331
486519  meter/sec      RA   =          129
42850  deg
 ZDOT =       5823
924463                 TA   =          305
23950
                                          MA   =          305
36769
                                          Ha   =            222
430  n
mi
                                          Hp   =            213
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10817176
23                 X    =        -3354313
68
 Y    =       18883983
11  feet           Y    =         5718647
75  meter
 Z    =       -4646676
41                 Z    =        -1432463
05
 XDOT =     -15776
038475                 XDOT =       -4821
580632
 YDOT =      -4368
394090  feet/sec       YDOT =       -1385
331334  meter/sec
 ZDOT =      19107
363725                 ZDOT =        5800
533885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15418931
85                 X    =         4699690
43
 Y    =       15336039
29  feet           Y    =         4674424
78  meter
 Z    =       -4719127
13                 Z    =        -1438389
95
 XDOT =      -7242
575964                 XDOT =       -2207
537154
 YDOT =      13088
634069  feet/sec       YDOT =        3989
415664  meter/sec
 ZDOT =      19003
779048                 ZDOT =        5792
351854


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   17294
13058244  
00016717  00000-0  10270-3 0  9052
2 25544  51
6367 130
4876 0005238  41
4387 318
7162 15
54223898  1336


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
13058244   =   yrday
fracday
Element set:     905
Inclination:       51
6367  deg
RA of node:       130
4876  deg
Eccentricity:     
0005238     
Arg of perigee:    41
4387  deg
Mean anomaly:     318
7162  deg
Mean motion:   15
54223898  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             133
Checksum:              312


Coasting Arc #7 (Orbit 136)
---------------------------------------

Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3330854
68                 A    =         6777051
85  meter
 Y    =        2539468
44  meter          E    =           
0018658
 Z    =       -5343460
17                 I    =           51
91223
 XDOT =      -4702
381488                 Wp   =           77
20109
 YDOT =       6040
409356  meter/sec      RA   =          128
23287  deg
 ZDOT =        -56
691535                 TA   =          192
23710
                                          MA   =          192
28248
                                          Ha   =            222
400  n
mi
                                          Hp   =            213
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10928000
90                 X    =         3328166
71
 Y    =        8331589
37  feet           Y    =         2576700
91  meter
 Z    =      -17531037
30                 Z    =        -5327286
19
 XDOT =     -15427
760789                 XDOT =       -4769
302078
 YDOT =      19817
615999  feet/sec       YDOT =        5987
449936  meter/sec
 ZDOT =       -185
995851                 ZDOT =         -79
697851

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8101335
84                 X    =        -2469287
16
 Y    =      -11211757
88  feet           Y    =        -3417343
80  meter
 Z    =      -17459630
49                 Z    =        -5321695
37
 XDOT =      19758
886592                 XDOT =        6022
508633
 YDOT =     -13807
647680  feet/sec       YDOT =       -4208
571013  meter/sec
 ZDOT =       -288
879464                 ZDOT =         -88
050461


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   17294
38777577  
00016717  00000-0  10270-3 0  9067
2 25544  51
6402 129
2063 0005223  39
2652 320
8879 15
54235421  1372


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
38777577   =   yrday
fracday
Element set:     906
Inclination:       51
6402  deg
RA of node:       129
2063  deg
Eccentricity:     
0005223     
Arg of perigee:    39
2652  deg
Mean anomaly:     320
8879  deg
Mean motion:   15
54235421  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             137
Checksum:              313


Coasting Arc #8 (Orbit 152)
---------------------------------------

Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2138294
09                 A    =         6778118
81  meter
 Y    =       -3964891
88  meter          E    =           
0010641
 Z    =        5059640
10                 I    =           51
93532
 XDOT =       5240
445939                 Wp   =           49
33902
 YDOT =      -5270
345289  meter/sec      RA   =          123
25218  deg
 ZDOT =      -1905
925906                 TA   =           59
10453
                                          MA   =           58
99994
                                          Ha   =            222
419  n
mi
                                          Hp   =            213
089

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7015400
57                 X    =        -2118376
61
 Y    =      -13008175
47  feet           Y    =        -3988692
10  meter
 Z    =       16599869
11                 Z    =         5049301
25
 XDOT =      17193
064105                 XDOT =        5308
249168
 YDOT =     -17291
159086  feet/sec       YDOT =       -5211
364041  meter/sec
 ZDOT =      -6253
037750                 ZDOT =       -1880
303772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3229112
76                 X    =          984233
57
 Y    =       14474249
68  feet           Y    =         4411751
30  meter
 Z    =       16554547
88                 Z    =         5045826
19
 XDOT =     -20304
664135                 XDOT =       -6188
861628
 YDOT =      11586
018270  feet/sec       YDOT =        3531
418369  meter/sec
 ZDOT =      -6138
632145                 ZDOT =       -1871
055078


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   17295
41654796  
00016717  00000-0  10270-3 0  9070
2 25544  51
6399 124
0772 0005127  42
0142 318
1403 15
54262897  1534


Satellite: ISS
Catalog Number: 25544
Epoch time:      17295
41654796   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       124
0772  deg
Eccentricity:     
0005127     
Arg of perigee:    42
0142  deg
Mean anomaly:     318
1403  deg
Mean motion:   15
54262897  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             153
Checksum:              308


Coasting Arc #9 (Orbit 167)
---------------------------------------

Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         995163
71                 A    =         6781346
62  meter
 Y    =        5187667
18  meter          E    =           
0011343
 Z    =       -4261826
81                 I    =           51
96326
 XDOT =      -5403
286308                 Wp   =           86
15347
 YDOT =       4024
017888  meter/sec      RA   =          118
27868  deg
 ZDOT =       3645
577283                 TA   =          220
97835
                                          MA   =          221
06365
                                          Ha   =            222
446  n
mi
                                          Hp   =            213
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3264972
79                 X    =          957782
27
 Y    =       17019905
44  feet           Y    =         5198586
59  meter
 Z    =      -13982371
43                 Z    =        -4257083
50
 XDOT =     -17727
317283                 XDOT =       -5465
591253
 YDOT =      13202
158426  feet/sec       YDOT =        3963
246433  meter/sec
 ZDOT =      11960
555390                 ZDOT =        3619
177611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1207417
51                 X    =          368020
86
 Y    =      -17304539
59  feet           Y    =        -5274423
67  meter
 Z    =      -13962055
43                 Z    =        -4255634
49
 XDOT =      19375
167493                 XDOT =        5905
551052
 YDOT =      -8179
356554  feet/sec       YDOT =       -2493
067878  meter/sec
 ZDOT =      11842
852598                 ZDOT =        3609
701472


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   17296
38102078  
00016717  00000-0  10270-3 0  9089
2 25544  51
6402 119
2682 0005126  44
9476 315
2091 15
54236003  1682


Satellite: ISS
Catalog Number: 25544
Epoch time:      17296
38102078   =   yrday
fracday
Element set:     908
Inclination:       51
6402  deg
RA of node:       119
2682  deg
Eccentricity:     
0005126     
Arg of perigee:    44
9476  deg
Mean anomaly:     315
2091  deg
Mean motion:   15
54236003  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             168
Checksum:              295


Coasting Arc #10 (Orbit 183)
---------------------------------------

Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         105227
33                 A    =         6785208
86  meter
 Y    =       -6096664
09  meter          E    =           
0017092
 Z    =        2964022
39                 I    =           51
99148
 XDOT =       5293
492542                 Wp   =           83
95966
 YDOT =      -2363
616371  meter/sec      RA   =          113
31621  deg
 ZDOT =      -5023
081563                 TA   =           62
33937
                                          MA   =           62
16599
                                          Ha   =            222
485  n
mi
                                          Hp   =            212
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         345234
04                 X    =          158995
92
 Y    =      -20002178
76  feet           Y    =        -6095186
64  meter
 Z    =        9724482
90                 Z    =         2964664
34
 XDOT =      17367
101515                 XDOT =        5343
929965
 YDOT =      -7754
646885  feet/sec       YDOT =       -2304
139061  meter/sec
 ZDOT =     -16479
926388                 ZDOT =       -4997
244215

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5166863
05                 X    =        -1574859
86
 Y    =       19324530
58  feet           Y    =         5890116
92  meter
 Z    =        9728204
02                 Z    =         2965156
59
 XDOT =     -17432
311750                 XDOT =       -5313
368621
 YDOT =       3621
193346  feet/sec       YDOT =        1103
739732  meter/sec
 ZDOT =     -16364
936765                 ZDOT =       -4988
032726


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   17297
40978586  
00016717  00000-0  10270-3 0  9099
2 25544  51
6406 114
1383 0005296  47
6995 312
4606 15
54264255  1841


Satellite: ISS
Catalog Number: 25544
Epoch time:      17297
40978586   =   yrday
fracday
Element set:     909
Inclination:       51
6406  deg
RA of node:       114
1383  deg
Eccentricity:     
0005296     
Arg of perigee:    47
6995  deg
Mean anomaly:     312
4606  deg
Mean motion:   15
54264255  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             184
Checksum:              334


Coasting Arc #11 (Orbit 198)
---------------------------------------

Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1033081
48                 A    =         6788220
01  meter
 Y    =        6558371
51  meter          E    =           
0013734
 Z    =       -1390432
30                 I    =           52
01173
 XDOT =      -4952
400290                 Wp   =           42
94601
 YDOT =        448
287475  meter/sec      RA   =          108
36491  deg
 ZDOT =       5837
625953                 TA   =          301
97911
                                          MA   =          302
11253
                                          Ha   =            222
564  n
mi
                                          Hp   =            212
942

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3389374
94                 X    =        -1099587
97
 Y    =       21516966
89  feet           Y    =         6546446
99  meter
 Z    =       -4561785
75                 Z    =        -1395612
49
 XDOT =     -16248
032446                 XDOT =       -4985
402035
 YDOT =       1470
759433  feet/sec       YDOT =         392
721966  meter/sec
 ZDOT =      19152
316118                 ZDOT =        5813
488029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8176025
20                 X    =         2492052
48
 Y    =      -20184185
16  feet           Y    =        -6152139
64  meter
 Z    =       -4585727
53                 Z    =        -1397729
75
 XDOT =      14806
051341                 XDOT =        4512
884449
 YDOT =       1702
851558  feet/sec       YDOT =         519
029155  meter/sec
 ZDOT =      19045
131647                 ZDOT =        5804
956126


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   17298
37425135  
00016717  00000-0  10270-3 0  9105
2 25544  51
6392 109
3297 0005229  51
2925 308
8695 15
54223711  1990


Satellite: ISS
Catalog Number: 25544
Epoch time:      17298
37425135   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:       109
3297  deg
Eccentricity:     
0005229     
Arg of perigee:    51
2925  deg
Mean anomaly:     308
8695  deg
Mean motion:   15
54223711  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             199
Checksum:              319


Coasting Arc #12 (Orbit 214)
---------------------------------------

Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1864688
78                 A    =         6789006
54  meter
 Y    =       -6513098
09  meter          E    =           
0013063
 Z    =        -387040
81                 I    =           52
02434
 XDOT =       4450
097419                 Wp   =          115
15907
 YDOT =       1622
510258  meter/sec      RA   =          103
42034  deg
 ZDOT =      -6027
598934                 TA   =           68
99029
                                          MA   =           68
85060
                                          Ha   =            222
563  n
mi
                                          Hp   =            212
942

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6117745
35                 X    =         1939261
49
 Y    =      -21368432
06  feet           Y    =        -6491828
91  meter
 Z    =       -1269818
93                 Z    =         -377801
28
 XDOT =      14600
057148                 XDOT =        4460
903029
 YDOT =       5323
196385  feet/sec       YDOT =        1672
334576  meter/sec
 ZDOT =     -19775
587053                 ZDOT =       -6005
955104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10500545
23                 X    =        -3200566
19
 Y    =       19592857
49  feet           Y    =         5971902
96  meter
 Z    =       -1227852
59                 Z    =         -374249
47
 XDOT =     -11844
757464                 XDOT =       -3610
282075
 YDOT =      -7546
514294  feet/sec       YDOT =       -2300
177557  meter/sec
 ZDOT =     -19679
767780                 ZDOT =       -5998
393219


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   17299
40301147  
00016717  00000-0  10270-3 0  9117
2 25544  51
6399 104
2007 0005053  56
1053 304
0580 15
54217883  2154


Satellite: ISS
Catalog Number: 25544
Epoch time:      17299
40301147   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       104
2007  deg
Eccentricity:     
0005053     
Arg of perigee:    56
1053  deg
Mean anomaly:     304
0580  deg
Mean motion:   15
54217883  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             215
Checksum:              275


Coasting Arc #13 (Orbit 216)
---------------------------------------

Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2966539
65                 A    =         6787108
20  meter
 Y    =       -5740345
10  meter          E    =           
0009072
 Z    =       -2079525
81                 I    =           52
01726
 XDOT =       3581
762649                 Wp   =          104
90679
 YDOT =       3859
530150  meter/sec      RA   =          102
77581  deg
 ZDOT =      -5566
813779                 TA   =           97
96554
                                          MA   =           97
86257
                                          Ha   =            222
569  n
mi
                                          Hp   =            212
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9732741
63                 X    =         3040610
75
 Y    =      -18833153
22  feet           Y    =        -5706757
12  meter
 Z    =       -6822591
22                 Z    =        -2064934
96
 XDOT =      11751
189793                 XDOT =        3565
379521
 YDOT =      12662
500493  feet/sec       YDOT =        3899
492144  meter/sec
 ZDOT =     -18263
824733                 ZDOT =       -5549
454224

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2954230
72                 X    =          900449
52
 Y    =       21013741
24  feet           Y    =         6404988
33  meter
 Z    =       -6756986
80                 Z    =        -2059529
58
 XDOT =     -15480
448656                 XDOT =       -4718
440750
 YDOT =      -3647
887901  feet/sec       YDOT =       -1111
876232  meter/sec
 ZDOT =     -18187
349717                 ZDOT =       -5543
504194


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   17299
53160628  
00016717  00000-0  10270-3 0  9129
2 25544  51
6376 103
5550 0005216  59
5007 300
6661 15
54272002  2179


Satellite: ISS
Catalog Number: 25544
Epoch time:      17299
53160628   =   yrday
fracday
Element set:     912
Inclination:       51
6376  deg
RA of node:       103
5550  deg
Eccentricity:     
0005216     
Arg of perigee:    59
5007  deg
Mean anomaly:     300
6661  deg
Mean motion:   15
54272002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             217
Checksum:              282


Coasting Arc #14 (Orbit 232)
---------------------------------------

Vector Time (GMT): 2017/300/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3432693
13                 A    =         6783659
21  meter
 Y    =        4641999
26  meter          E    =           
0016876
 Z    =        3545719
60                 I    =           52
01198
 XDOT =      -2801
312540                 Wp   =           84
21461
 YDOT =      -5535
572253  meter/sec      RA   =           97
82167  deg
 ZDOT =       4518
332944                 TA   =          317
39217
                                          MA   =          317
52296
                                          Ha   =            222
653  n
mi
                                          Hp   =            212
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11262116
57                 X    =        -3501569
74
 Y    =       15229656
37  feet           Y    =         4603227
52  meter
 Z    =       11632938
31                 Z    =         3528876
94
 XDOT =      -9190
657941                 XDOT =       -2761
152315
 YDOT =     -18161
326288  feet/sec       YDOT =       -5566
673778  meter/sec
 ZDOT =      14823
926982                 ZDOT =        4504
822488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          80080
57                 X    =           24408
56
 Y    =      -18987390
63  feet           Y    =        -5787356
66  meter
 Z    =       11557488
51                 Z    =         3522722
50
 XDOT =      16871
398581                 XDOT =        5142
402288
 YDOT =       9092
013971  feet/sec       YDOT =        2771
245858  meter/sec
 ZDOT =      14764
789092                 ZDOT =        4500
307715


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   17300
56036093  
00016717  00000-0  10270-3 0  9134
2 25544  51
6377  98
4252 0005105  65
2201 294
9482 15
54266748  2332


Satellite: ISS
Catalog Number: 25544
Epoch time:      17300
56036093   =   yrday
fracday
Element set:     913
Inclination:       51
6377  deg
RA of node:        98
4252  deg
Eccentricity:     
0005105     
Arg of perigee:    65
2201  deg
Mean anomaly:     294
9482  deg
Mean motion:   15
54266748  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             233
Checksum:              300


Coasting Arc #15 (Orbit 247)
---------------------------------------

Vector Time (GMT): 2017/301/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3807994
28                 A    =         6779822
28  meter
 Y    =       -3132534
97  meter          E    =           
0015645
 Z    =       -4668467
84                 I    =           52
00289
 XDOT =       1968
427380                 Wp   =           69
65172
 YDOT =       6784
909726  meter/sec      RA   =           92
85868  deg
 ZDOT =      -2949
751593                 TA   =          171
09184
                                          MA   =          171
06405
                                          Ha   =            222
647  n
mi
                                          Hp   =            212
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12493419
57                 X    =         3865417
59
 Y    =      -10277345
72  feet           Y    =        -3089630
47  meter
 Z    =      -15316495
54                 Z    =        -4649829
91
 XDOT =       6458
095080                 XDOT =        1906
739081
 YDOT =      22260
202512  feet/sec       YDOT =        6806
577000  meter/sec
 ZDOT =      -9677
662706                 ZDOT =       -2940
339506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3759061
66                 X    =        -1145762
00
 Y    =       15815202
34  feet           Y    =         4820473
67  meter
 Z    =      -15233293
59                 Z    =        -4643107
89
 XDOT =     -17549
558011                 XDOT =       -5349
105282
 YDOT =     -13445
038814  feet/sec       YDOT =       -4098
047830  meter/sec
 ZDOT =      -9636
912066                 ZDOT =       -2937
330798


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   17301
52481586  
00016717  00000-0  10270-3 0  9143
2 25544  51
6380  93
6175 0005250  68
5391 291
6321 15
54263786  2485


Satellite: ISS
Catalog Number: 25544
Epoch time:      17301
52481586   =   yrday
fracday
Element set:     914
Inclination:       51
6380  deg
RA of node:        93
6175  deg
Eccentricity:     
0005250     
Arg of perigee:    68
5391  deg
Mean anomaly:     291
6321  deg
Mean motion:   15
54263786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             248
Checksum:              312


Coasting Arc #16 (Orbit 263)
---------------------------------------

Vector Time (GMT): 2017/302/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4054706
64                 A    =         6777333
80  meter
 Y    =        1363666
18  meter          E    =           
0008007
 Z    =        5249803
72                 I    =           51
99537
 XDOT =      -1123
806047                 Wp   =           92
90692
 YDOT =      -7514
747529  meter/sec      RA   =           87
88462  deg
 ZDOT =       1082
209732                 TA   =          346
77406
                                          MA   =          346
79504
                                          Ha   =            222
769  n
mi
                                          Hp   =            212
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13302843
31                 X    =        -4095155
53
 Y    =        4473970
40  feet           Y    =         1318097
78  meter
 Z    =       17223765
50                 Z    =         5230008
60
 XDOT =      -3687
027712                 XDOT =       -1044
947534
 YDOT =     -24654
683495  feet/sec       YDOT =       -7526
873717  meter/sec
 ZDOT =       3550
556865                 ZDOT =        1076
942458

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7734904
34                 X    =         2357598
84
 Y    =      -11839744
33  feet           Y    =        -3608754
07  meter
 Z    =       17135689
62                 Z    =         5222958
19
 XDOT =      17356
853991                 XDOT =        5290
369096
 YDOT =      16454
436486  feet/sec       YDOT =        5015
312241  meter/sec
 ZDOT =       3528
326183                 ZDOT =        1075
433820


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   17302
55356368  
00016717  00000-0  10270-3 0  9157
2 25544  51
6381  88
4871 0005114  71
4541 288
7167 15
54262993  2642


Satellite: ISS
Catalog Number: 25544
Epoch time:      17302
55356368   =   yrday
fracday
Element set:     915
Inclination:       51
6381  deg
RA of node:        88
4871  deg
Eccentricity:     
0005114     
Arg of perigee:    71
4541  deg
Mean anomaly:     288
7167  deg
Mean motion:   15
54262993  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             264
Checksum:              323


Coasting Arc #17 (Orbit 278)
---------------------------------------

Vector Time (GMT): 2017/303/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4228073
97                 A    =         6777201
13  meter
 Y    =         507053
80  meter          E    =           
0019393
 Z    =       -5289002
78                 I    =           51
99390
 XDOT =        226
834074                 Wp   =           91
24225
 YDOT =       7596
436654  meter/sec      RA   =           82
90826  deg
 ZDOT =        912
072182                 TA   =          187
44127
                                          MA   =          187
47009
                                          Ha   =            222
649  n
mi
                                          Hp   =            212
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13871633
75                 X    =         4247781
53
 Y    =        1663562
34  feet           Y    =          554444
87  meter
 Z    =      -17352371
33                 Z    =        -5268415
93
 XDOT =        744
206281                 XDOT =         137
441358
 YDOT =      24922
692436  feet/sec       YDOT =        7598
473501  meter/sec
 ZDOT =       2992
362801                 ZDOT =         912
956479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11864455
39                 X    =        -3616286
00
 Y    =        7588459
75  feet           Y    =         2312962
53  meter
 Z    =      -17261066
89                 Z    =        -5261173
19
 XDOT =     -15819
491258                 XDOT =       -4821
780935
 YDOT =     -17939
290975  feet/sec       YDOT =       -5467
895889  meter/sec
 ZDOT =       2995
112759                 ZDOT =         912
910369


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   17303
51801042  
00016717  00000-0  10270-3 0  9169
2 25544  51
6392  83
6791 0005227  75
3028 284
8704 15
54278015  2792


Satellite: ISS
Catalog Number: 25544
Epoch time:      17303
51801042   =   yrday
fracday
Element set:     916
Inclination:       51
6392  deg
RA of node:        83
6791  deg
Eccentricity:     
0005227     
Arg of perigee:    75
3028  deg
Mean anomaly:     284
8704  deg
Mean motion:   15
54278015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             279
Checksum:              305


Coasting Arc #18 (Orbit 283)
---------------------------------------

Vector Time (GMT): 2017/303/19:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2302074
07                 A    =         6782545
16  meter
 Y    =       -5069461
03  meter          E    =           
0011741
 Z    =       -3885846
75                 I    =           52
01247
 XDOT =       4037
521500                 Wp   =           74
04014
 YDOT =       5010
522985  meter/sec      RA   =           81
39583  deg
 ZDOT =      -4152
035083                 TA   =          152
52565
                                          MA   =          152
46353
                                          Ha   =            222
705  n
mi
                                          Hp   =            212
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7552736
46                 X    =         2377466
91
 Y    =      -16632089
98  feet           Y    =        -5043296
38  meter
 Z    =      -12748841
05                 Z    =        -3874480
33
 XDOT =      13246
461615                 XDOT =        4001
361316
 YDOT =      16438
723704  feet/sec       YDOT =        5055
470843  meter/sec
 ZDOT =     -13622
162347                 ZDOT =       -4132
509885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14538959
25                 X    =         4431474
78
 Y    =      -11117230
95  feet           Y    =        -3388531
99  meter
 Z    =      -12697599
51                 Z    =        -3870228
33
 XDOT =       3269
894136                 XDOT =         996
663733
 YDOT =      19709
539801  feet/sec       YDOT =        6007
467731  meter/sec
 ZDOT =     -13536
269791                 ZDOT =       -4125
855032


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   17303
83949074  
00016717  00000-0  10270-3 0  9173
2 25544  51
6411  82
0792 0005403  73
3460 286
8285 15
54280992  2841


Satellite: ISS
Catalog Number: 25544
Epoch time:      17303
83949074   =   yrday
fracday
Element set:     917
Inclination:       51
6411  deg
RA of node:        82
0792  deg
Eccentricity:     
0005403     
Arg of perigee:    73
3460  deg
Mean anomaly:     286
8285  deg
Mean motion:   15
54280992  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             284
Checksum:              318
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list