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

 
Date: May 27th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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


152/21:55:46 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 216 1

153/10:47:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 216 2

153/13:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 216 3

155/13:34:21 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 216 4

156/18:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 216 5

160/01:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 8
000/00:00:00 000 0 0 0 0 216 6

Coasting Arc #1 (Orbit 1837)
---------------------------------------

Vector Time (GMT): 2017/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915838
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5757854
75                 A    =         6784702
92  meter
 Y    =         606861
32  meter          E    =           
0011752
 Z    =        3532958
62                 I    =           51
84666
 XDOT =       2166
755967                 Wp   =          115
87435
 YDOT =      -5807
917461  meter/sec      RA   =          145
33826  deg
 ZDOT =       4512
259280                 TA   =          285
60926
                                          MA   =          285
73893
                                          Ha   =            221
624  n
mi
                                          Hp   =            215
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18890599
56                 X    =        -5781374
56
 Y    =        1991014
84  feet           Y    =          542341
16  meter
 Z    =       11591071
59                 Z    =         3504931
21
 XDOT =       7108
779420                 XDOT =        2209
621870
 YDOT =     -19054
847314  feet/sec       YDOT =       -5783
448198  meter/sec
 ZDOT =      14804
000263                 ZDOT =        4522
888304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6715306
62                 X    =        -2046825
46
 Y    =       17848719
06  feet           Y    =         5440289
57  meter
 Z    =       11467332
62                 Z    =         3495242
98
 XDOT =     -12591
937799                 XDOT =       -3838
022641
 YDOT =     -14314
894431  feet/sec       YDOT =       -4363
179823  meter/sec
 ZDOT =      14851
792403                 ZDOT =        4526
826324


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   17146
55696808  
00016717  00000-0  10270-3 0  9003
2 25544  51
6360 146
1378 0005009 199
1516 160
9449 15
53939675 18385


Satellite: ISS
Catalog Number: 25544
Epoch time:      17146
55696808   =   yrday
fracday
Element set:     900
Inclination:       51
6360  deg
RA of node:       146
1378  deg
Eccentricity:     
0005009     
Arg of perigee:   199
1516  deg
Mean anomaly:     160
9449  deg
Mean motion:   15
53939675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1838
Checksum:              342


Coasting Arc #2 (Orbit 1852)
---------------------------------------

Vector Time (GMT): 2017/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915838
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4955055
18                 A    =         6781094
76  meter
 Y    =         584068
58  meter          E    =           
0007658
 Z    =       -4598258
17                 I    =           51
86113
 XDOT =      -3550
007049                 Wp   =           98
87439
 YDOT =       6061
268765  meter/sec      RA   =          140
36620  deg
 ZDOT =      -3061
062658                 TA   =          140
62752
                                          MA   =          140
57183
                                          Ha   =            221
578  n
mi
                                          Hp   =            215
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16256742
72                 X    =         4970492
04
 Y    =        1916235
51  feet           Y    =          639566
28  meter
 Z    =      -15086148
85                 Z    =        -4574150
20
 XDOT =     -11647
004755                 XDOT =       -3602
652590
 YDOT =      19886
052380  feet/sec       YDOT =        6021
276230  meter/sec
 ZDOT =     -10042
856491                 ZDOT =       -3078
434760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8800522
52                 X    =         2682399
26
 Y    =      -13917608
68  feet           Y    =        -4242087
12  meter
 Z    =      -14979869
88                 Z    =        -4565864
34
 XDOT =      11904
682875                 XDOT =        3628
547340
 YDOT =      18401
044363  feet/sec       YDOT =        5608
638322  meter/sec
 ZDOT =     -10120
457254                 ZDOT =       -3084
715371


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   17147
52162262  
00016717  00000-0  10270-3 0  9014
2 25544  51
6365 141
3296 0004900 201
2244 158
8706 15
53923580 18535


Satellite: ISS
Catalog Number: 25544
Epoch time:      17147
52162262   =   yrday
fracday
Element set:     901
Inclination:       51
6365  deg
RA of node:       141
3296  deg
Eccentricity:     
0004900     
Arg of perigee:   201
2244  deg
Mean anomaly:     158
8706  deg
Mean motion:   15
53923580  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1853
Checksum:              293


Coasting Arc #3 (Orbit 1868)
---------------------------------------

Vector Time (GMT): 2017/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915838
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3934311
79                 A    =         6778560
25  meter
 Y    =       -1851215
70  meter          E    =           
0007004
 Z    =        5200389
88                 I    =           51
87763
 XDOT =       4590
547865                 Wp   =          168
12638
 YDOT =      -5996
346449  meter/sec      RA   =          135
38843  deg
 ZDOT =       1331
383230                 TA   =          269
08337
                                          MA   =          269
16362
                                          Ha   =            221
463  n
mi
                                          Hp   =            215
625

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12907847
08                 X    =        -3938579
70
 Y    =       -6073542
32  feet           Y    =        -1895236
38  meter
 Z    =       17061646
59                 Z    =         5181267
49
 XDOT =      15060
852577                 XDOT =        4650
792158
 YDOT =     -19673
052654  feet/sec       YDOT =       -5944
675163  meter/sec
 ZDOT =       4368
055215                 ZDOT =        1353
828369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10947393
86                 X    =        -3336765
65
 Y    =        9301476
08  feet           Y    =         2835089
91  meter
 Z    =       16977553
64                 Z    =         5174758
35
 XDOT =     -10934
953481                 XDOT =       -3332
973821
 YDOT =     -21067
375932  feet/sec       YDOT =       -6421
336184  meter/sec
 ZDOT =       4468
052497                 ZDOT =        1361
862401


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   17148
55058288  
00016717  00000-0  10270-3 0  9021
2 25544  51
6369 136
2017 0004829 206
2859 153
8049 15
53924932 18694


Satellite: ISS
Catalog Number: 25544
Epoch time:      17148
55058288   =   yrday
fracday
Element set:     902
Inclination:       51
6369  deg
RA of node:       136
2017  deg
Eccentricity:     
0004829     
Arg of perigee:   206
2859  deg
Mean anomaly:     153
8049  deg
Mean motion:   15
53924932  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1869
Checksum:              339


Coasting Arc #4 (Orbit 1883)
---------------------------------------

Vector Time (GMT): 2017/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915838
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2777702
97                 A    =         6778045
59  meter
 Y    =        3170979
34  meter          E    =           
0013345
 Z    =       -5318637
98                 I    =           51
89838
 XDOT =      -5268
590960                 Wp   =          113
07523
 YDOT =       5532
251310  meter/sec      RA   =          130
40803  deg
 ZDOT =        542
760100                 TA   =          162
11512
                                          MA   =          162
06811
                                          Ha   =            221
242  n
mi
                                          Hp   =            215
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9113198
73                 X    =         2767873
19
 Y    =       10403475
53  feet           Y    =         3201987
16  meter
 Z    =      -17449599
68                 Z    =        -5305168
23
 XDOT =     -17285
403413                 XDOT =       -5332
698939
 YDOT =      18150
430808  feet/sec       YDOT =        5472
975846  meter/sec
 ZDOT =       1780
708991                 ZDOT =         517
011804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13230201
69                 X    =         4032565
48
 Y    =       -4277626
32  feet           Y    =        -1303820
50  meter
 Z    =      -17390655
53                 Z    =        -5300671
80
 XDOT =       9372
816934                 XDOT =        2856
834601
 YDOT =      22161
495057  feet/sec       YDOT =        6754
823693  meter/sec
 ZDOT =       1666
186567                 ZDOT =         507
853666


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   17149
51523002  
00016717  00000-0  10270-3 0  9030
2 25544  51
6369 131
3945 0004791 210
0722 150
0156 15
53921794 18848


Satellite: ISS
Catalog Number: 25544
Epoch time:      17149
51523002   =   yrday
fracday
Element set:     903
Inclination:       51
6369  deg
RA of node:       131
3945  deg
Eccentricity:     
0004791     
Arg of perigee:   210
0722  deg
Mean anomaly:     150
0156  deg
Mean motion:   15
53921794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1884
Checksum:              292


Coasting Arc #5 (Orbit 1899)
---------------------------------------

Vector Time (GMT): 2017/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915838
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1598457
32                 A    =         6779664
28  meter
 Y    =       -4389435
09  meter          E    =           
0002980
 Z    =        4910705
50                 I    =           51
92452
 XDOT =       5599
210315                 Wp   =           99
28809
 YDOT =      -4680
363084  meter/sec      RA   =          125
43087  deg
 ZDOT =      -2360
226163                 TA   =           13
72719
                                          MA   =           13
71908
                                          Ha   =            221
127  n
mi
                                          Hp   =            215
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5244282
55                 X    =        -1573108
51
 Y    =      -14401033
76  feet           Y    =        -4407168
88  meter
 Z    =       16111238
52                 Z    =         4903001
82
 XDOT =      18370
112582                 XDOT =        5662
596040
 YDOT =     -15355
521928  feet/sec       YDOT =       -4617
394276  meter/sec
 ZDOT =      -7743
524156                 ZDOT =       -2332
873437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15348839
32                 X    =        -4678326
23
 Y    =        -614270
90  feet           Y    =         -187229
77  meter
 Z    =       16077937
75                 Z    =         4900555
43
 XDOT =      -7114
356982                 XDOT =       -2168
456008
 YDOT =     -21796
701782  feet/sec       YDOT =       -6643
634703  meter/sec
 ZDOT =      -7622
037084                 ZDOT =       -2323
196903


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   17150
54418471  
00016717  00000-0  10270-3 0  9049
2 25544  51
6370 126
2668 0004840 215
2593 144
8240 15
53946216 19003


Satellite: ISS
Catalog Number: 25544
Epoch time:      17150
54418471   =   yrday
fracday
Element set:     904
Inclination:       51
6370  deg
RA of node:       126
2668  deg
Eccentricity:     
0004840     
Arg of perigee:   215
2593  deg
Mean anomaly:     144
8240  deg
Mean motion:   15
53946216  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1900
Checksum:              296


Coasting Arc #6 (Orbit 1914)
---------------------------------------

Vector Time (GMT): 2017/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915838
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         470419
41                 A    =         6783002
01  meter
 Y    =        5434765
59  meter          E    =           
0006986
 Z    =       -4038903
20                 I    =           51
95459
 XDOT =      -5600
051660                 Wp   =          147
60213
 YDOT =       3422
816012  meter/sec      RA   =          120
46153  deg
 ZDOT =       3950
923403                 TA   =          163
32065
                                          MA   =          163
29767
                                          Ha   =            220
929  n
mi
                                          Hp   =            216
017

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1543370
76                 X    =          429230
49
 Y    =       17830595
77  feet           Y    =         5439796
17  meter
 Z    =      -13250994
74                 Z    =        -4036717
64
 XDOT =     -18372
872900                 XDOT =       -5657
101931
 YDOT =      11229
711327  feet/sec       YDOT =        3359
873131  meter/sec
 ZDOT =      12962
347124                 ZDOT =        3923
581791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17169773
95                 X    =         5233347
10
 Y    =        5073792
10  feet           Y    =         1546491
83  meter
 Z    =      -13242224
00                 Z    =        -4036229
88
 XDOT =       3985
707990                 XDOT =        1214
843795
 YDOT =      20048
761937  feet/sec       YDOT =        6110
862638  meter/sec
 ZDOT =      12841
095289                 ZDOT =        3913
965844


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   17151
50882605  
00016717  00000-0  10270-3 0  9051
2 25544  51
6379 121
4594 0004732 218
9063 141
1750 15
53932781 19153


Satellite: ISS
Catalog Number: 25544
Epoch time:      17151
50882605   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:       121
4594  deg
Eccentricity:     
0004732     
Arg of perigee:   218
9063  deg
Mean anomaly:     141
1750  deg
Mean motion:   15
53932781  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1915
Checksum:              308


Coasting Arc #7 (Orbit 1930)
---------------------------------------

Vector Time (GMT): 2017/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915838
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         551050
31                 A    =         6786585
62  meter
 Y    =       -6167621
00  meter          E    =           
0011587
 Z    =        2760532
19                 I    =           51
98233
 XDOT =       5358
336285                 Wp   =          120
62719
 YDOT =      -1840
926657  meter/sec      RA   =          115
50272  deg
 ZDOT =      -5172
318829                 TA   =           28
25216
                                          MA   =           28
18936
                                          Ha   =            220
769  n
mi
                                          Hp   =            216
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1807907
86                 X    =          606567
98
 Y    =      -20234977
04  feet           Y    =        -6161148
56  meter
 Z    =        9056864
13                 Z    =         2763343
45
 XDOT =      17579
843455                 XDOT =        5403
648403
 YDOT =      -6039
785619  feet/sec       YDOT =       -1780
752401  meter/sec
 ZDOT =     -16969
549963                 ZDOT =       -5146
179708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18309752
47                 X    =        -5580812
55
 Y    =       -8788208
88  feet           Y    =        -2678646
07  meter
 Z    =        9070279
13                 Z    =         2764621
08
 XDOT =        -38
956446                 XDOT =         -11
873925
 YDOT =     -17348
540670  feet/sec       YDOT =       -5287
835196  meter/sec
 ZDOT =     -16853
850670                 ZDOT =       -5137
053684


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   17152
53777331  
00016717  00000-0  10270-3 0  9065
2 25544  51
6378 116
3312 0004672 223
7280 136
3503 15
53957509 19316


Satellite: ISS
Catalog Number: 25544
Epoch time:      17152
53777331   =   yrday
fracday
Element set:     906
Inclination:       51
6378  deg
RA of node:       116
3312  deg
Eccentricity:     
0004672     
Arg of perigee:   223
7280  deg
Mean anomaly:     136
3503  deg
Mean motion:   15
53957509  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1931
Checksum:              305


Coasting Arc #8 (Orbit 1936)
---------------------------------------

Vector Time (GMT): 2017/152/21:55:46
000
Vector Time (MET): N/A
Weight (LBS)     : 915838
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1604232
45                 A    =         6781712
78  meter
 Y    =        4924157
09  meter          E    =           
0008471
 Z    =       -4386858
90                 I    =           51
97072
 XDOT =      -4975
174440                 Wp   =          143
65391
 YDOT =       4695
086162  meter/sec      RA   =          113
44563  deg
 ZDOT =       3447
524797                 TA   =          161
20574
                                          MA   =          161
17445
                                          Ha   =            220
831  n
mi
                                          Hp   =            216
111

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5263229
84                 X    =         1570359
28
 Y    =       16155371
04  feet           Y    =         4941907
59  meter
 Z    =      -14392581
68                 Z    =        -4379147
96
 XDOT =     -16322
750787                 XDOT =       -5044
052793
 YDOT =      15403
825991  feet/sec       YDOT =        4639
065046  meter/sec
 ZDOT =      11310
776892                 ZDOT =        3423
189875

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14272848
20                 X    =        -4350364
13
 Y    =       -9270333
61  feet           Y    =        -2825597
68  meter
 Z    =      -14359342
89                 Z    =        -4376727
71
 XDOT =       2508
167244                 XDOT =         764
489376
 YDOT =     -21230
425396  feet/sec       YDOT =       -6471
033661  meter/sec
 ZDOT =      11202
572559                 ZDOT =        3414
544116


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   17152
92362774  
00016717  00000-0  10270-3 0  9070
2 25544  51
6367 114
4048 0004926 221
3045 138
7736 15
53959676 19371


Satellite: ISS
Catalog Number: 25544
Epoch time:      17152
92362774   =   yrday
fracday
Element set:     907
Inclination:       51
6367  deg
RA of node:       114
4048  deg
Eccentricity:     
0004926     
Arg of perigee:   221
3045  deg
Mean anomaly:     138
7736  deg
Mean motion:   15
53959676  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1937
Checksum:              335


Coasting Arc #9 (Orbit 1945)
---------------------------------------

Vector Time (GMT): 2017/153/10:47:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900606
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4573803
28                 A    =         6780298
84  meter
 Y    =        1562746
01  meter          E    =           
0007641
 Z    =        4755189
05                 I    =           51
97319
 XDOT =        422
056063                 Wp   =          153
95240
 YDOT =      -7146
134679  meter/sec      RA   =          110
83753  deg
 ZDOT =       2746
111572                 TA   =          268
95947
                                          MA   =          269
04701
                                          Ha   =            220
686  n
mi
                                          Hp   =            216
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15005916
28                 X    =        -4614036
86
 Y    =        5127119
45  feet           Y    =         1511373
39  meter
 Z    =       15601013
94                 Z    =         4732873
20
 XDOT =       1384
698369                 XDOT =         488
595323
 YDOT =     -23445
323751  feet/sec       YDOT =       -7141
043089  meter/sec
 ZDOT =       9009
552402                 ZDOT =        2748
322972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5263636
48                 X    =        -1604356
40
 Y    =       15060925
39  feet           Y    =         4590570
06  meter
 Z    =       15502231
15                 Z    =         4725080
05
 XDOT =     -16556
044605                 XDOT =       -5046
282396
 YDOT =     -15099
351537  feet/sec       YDOT =       -4602
282348  meter/sec
 ZDOT =       9020
489680                 ZDOT =        2749
445254


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   17153
50240790  
00016717  00000-0  10270-3 0  9089
2 25544  51
6371 111
5242 0004847 227
5420 132
5323 15
53978450 19462


Satellite: ISS
Catalog Number: 25544
Epoch time:      17153
50240790   =   yrday
fracday
Element set:     908
Inclination:       51
6371  deg
RA of node:       111
5242  deg
Eccentricity:     
0004847     
Arg of perigee:   227
5420  deg
Mean anomaly:     132
5323  deg
Mean motion:   15
53978450  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1946
Checksum:              295


Coasting Arc #10 (Orbit 1946)
---------------------------------------

Vector Time (GMT): 2017/153/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900606
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4299567
34                 A    =         6778289
10  meter
 Y    =         203656
36  meter          E    =           
0010533
 Z    =       -5245025
55                 I    =           51
96916
 XDOT =      -1761
058046                 Wp   =           95
42072
 YDOT =       7364
677590  meter/sec      RA   =          110
33346  deg
 ZDOT =      -1160
620341                 TA   =          163
50704
                                          MA   =          163
47274
                                          Ha   =            220
648  n
mi
                                          Hp   =            216
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14106192
06                 X    =         4322448
33
 Y    =         668163
91  feet           Y    =          251865
29  meter
 Z    =      -17208089
07                 Z    =        -5224083
89
 XDOT =      -5777
749494                 XDOT =       -1837
643165
 YDOT =      24162
328050  feet/sec       YDOT =        7344
556104  meter/sec
 ZDOT =      -3807
809517                 ZDOT =       -1169
360619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1203739
03                 X    =          366899
66
 Y    =      -14182895
15  feet           Y    =        -4322946
44  meter
 Z    =      -17115663
12                 Z    =        -5216854
12
 XDOT =      22892
971840                 XDOT =        6977
777817
 YDOT =       6574
403689  feet/sec       YDOT =        2003
878244  meter/sec
 ZDOT =      -3847
609696                 ZDOT =       -1172
751435


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   17153
56671801  
00016717  00000-0  10270-3 0  9097
2 25544  51
6387 111
2033 0004725 227
8497 132
2255 15
53963408 19475


Satellite: ISS
Catalog Number: 25544
Epoch time:      17153
56671801   =   yrday
fracday
Element set:     909
Inclination:       51
6387  deg
RA of node:       111
2033  deg
Eccentricity:     
0004725     
Arg of perigee:   227
8497  deg
Mean anomaly:     132
2255  deg
Mean motion:   15
53963408  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1947
Checksum:              316


Coasting Arc #11 (Orbit 1962)
---------------------------------------

Vector Time (GMT): 2017/154/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900606
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3784841
33                 A    =         6777933
76  meter
 Y    =       -1873068
02  meter          E    =           
0001858
 Z    =        5302409
19                 I    =           51
97931
 XDOT =       2557
340529                 Wp   =          216
93782
 YDOT =      -7193
280997  meter/sec      RA   =          105
35913  deg
 ZDOT =       -717
169850                 TA   =          239
87134
                                          MA   =          239
88976
                                          Ha   =            220
522  n
mi
                                          Hp   =            216
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12417458
42                 X    =        -3789371
60
 Y    =       -6145236
28  feet           Y    =        -1915418
34  meter
 Z    =       17396355
61                 Z    =         5284012
34
 XDOT =       8390
224834                 XDOT =        2641
071304
 YDOT =     -23600
003270  feet/sec       YDOT =       -7164
214870  meter/sec
 ZDOT =      -2352
919454                 ZDOT =        -704
544060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6400701
11                 X    =        -1950933
70
 Y    =       12401490
79  feet           Y    =         3779974
39  meter
 Z    =       17315439
43                 Z    =         5277745
94
 XDOT =     -22517
591469                 XDOT =       -6863
361880
 YDOT =      -8423
377223  feet/sec       YDOT =       -2567
445378  meter/sec
 ZDOT =      -2295
975984                 ZDOT =        -699
813480


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   17154
59565808  
00016717  00000-0  10270-3 0  9102
2 25544  51
6394 106
0760 0004789 233
4536 126
6176 15
53982864 19633


Satellite: ISS
Catalog Number: 25544
Epoch time:      17154
59565808   =   yrday
fracday
Element set:     910
Inclination:       51
6394  deg
RA of node:       106
0760  deg
Eccentricity:     
0004789     
Arg of perigee:   233
4536  deg
Mean anomaly:     126
6176  deg
Mean motion:   15
53982864  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1963
Checksum:              339


Coasting Arc #12 (Orbit 1977)
---------------------------------------

Vector Time (GMT): 2017/155/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900606
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3216964
32                 A    =         6779884
46  meter
 Y    =        3485419
14  meter          E    =           
0009441
 Z    =       -4853179
77                 I    =           51
99362
 XDOT =      -3200
015124                 Wp   =          130
65924
 YDOT =       6483
276131  meter/sec      RA   =          100
38573  deg
 ZDOT =       2532
193758                 TA   =          164
15900
                                          MA   =          164
12945
                                          Ha   =            220
296  n
mi
                                          Hp   =            216
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10554344
88                 X    =         3201324
98
 Y    =       11435102
17  feet           Y    =         3521306
31  meter
 Z    =      -15922505
81                 Z    =        -4837590
33
 XDOT =     -10498
737283                 XDOT =       -3284
575273
 YDOT =      21270
590980  feet/sec       YDOT =        6447
018411  meter/sec
 ZDOT =       8307
722304                 ZDOT =        2516
443978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11470003
61                 X    =         3496057
10
 Y    =      -10619014
11  feet           Y    =        -3236675
50  meter
 Z    =      -15854258
27                 Z    =        -4832377
92
 XDOT =      20460
829276                 XDOT =        6236
460763
 YDOT =       9788
908911  feet/sec       YDOT =        2983
659436  meter/sec
 ZDOT =       8237
086298                 ZDOT =        2510
663904


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   17155
56028628  
00016717  00000-0  10270-3 0  9115
2 25544  51
6396 101
2676 0004645 236
3230 123
7480 15
53977566 19787


Satellite: ISS
Catalog Number: 25544
Epoch time:      17155
56028628   =   yrday
fracday
Element set:     911
Inclination:       51
6396  deg
RA of node:       101
2676  deg
Eccentricity:     
0004645     
Arg of perigee:   236
3230  deg
Mean anomaly:     123
7480  deg
Mean motion:   15
53977566  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1978
Checksum:              326


Coasting Arc #13 (Orbit 1978)
---------------------------------------

Vector Time (GMT): 2017/155/13:34:21
000
Vector Time (MET): N/A
Weight (LBS)     : 923344
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3076852
59                 A    =         6786921
78  meter
 Y    =        5446303
12  meter          E    =           
0009412
 Z    =        2624221
58                 I    =           52
01726
 XDOT =      -3366
036505                 Wp   =           86
97518
 YDOT =      -4445
160146  meter/sec      RA   =          100
34329  deg
 ZDOT =       5263
118474                 TA   =          302
41861
                                          MA   =          302
50962
                                          Ha   =            220
325  n
mi
                                          Hp   =            216
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10094660
72                 X    =        -3150273
22
 Y    =       17868448
56  feet           Y    =         5411484
97  meter
 Z    =        8609650
85                 Z    =         2609097
08
 XDOT =     -11043
426853                 XDOT =       -3341
645310
 YDOT =     -14583
858748  feet/sec       YDOT =       -4482
665439  meter/sec
 ZDOT =      17267
449061                 ZDOT =        5246
826063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18819204
96                 X    =         5736093
67
 Y    =        8257258
95  feet           Y    =         2516812
53  meter
 Z    =        8541950
36                 Z    =         2603586
47
 XDOT =     -12754
314313                 XDOT =       -3887
515003
 YDOT =      11225
503170  feet/sec       YDOT =        3421
533366  meter/sec
 ZDOT =      17196
259350                 ZDOT =        5241
419850


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   17155
62459499  
00016717  00000-0  10270-3 0  9127
2 25544  51
6397 100
9474 0004641 236
5206 123
5503 15
53969023 19795


Satellite: ISS
Catalog Number: 25544
Epoch time:      17155
62459499   =   yrday
fracday
Element set:     912
Inclination:       51
6397  deg
RA of node:       100
9474  deg
Eccentricity:     
0004641     
Arg of perigee:   236
5206  deg
Mean anomaly:     123
5503  deg
Mean motion:   15
53969023  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1979
Checksum:              326


Coasting Arc #14 (Orbit 1993)
---------------------------------------

Vector Time (GMT): 2017/156/13:34:21
000
Vector Time (MET): N/A
Weight (LBS)     : 923344
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3495260
65                 A    =         6783217
31  meter
 Y    =       -4274415
17  meter          E    =           
0002307
 Z    =       -3941717
34                 I    =           52
01090
 XDOT =       2643
545198                 Wp   =          101
18874
 YDOT =       5923
957505  meter/sec      RA   =           95
38864  deg
 ZDOT =      -4082
292941                 TA   =          126
30592
                                          MA   =          126
28461
                                          Ha   =            220
210  n
mi
                                          Hp   =            216
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11467390
58                 X    =         3561945
68
 Y    =      -14023671
82  feet           Y    =        -4234955
61  meter
 Z    =      -12932143
50                 Z    =        -3924576
62
 XDOT =       8673
048551                 XDOT =        2596
935505
 YDOT =      19435
556119  feet/sec       YDOT =        5953
259150  meter/sec
 ZDOT =     -13393
349544                 ZDOT =       -4069
563966

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15310025
40                 X    =        -4666495
74
 Y    =       -9784590
99  feet           Y    =        -2982343
33  meter
 Z    =      -12855724
61                 Z    =        -3918424
86
 XDOT =      17528
783098                 XDOT =        5342
773088
 YDOT =      -9913
398578  feet/sec       YDOT =       -3021
603886  meter/sec
 ZDOT =     -13338
155728                 ZDOT =       -4065
469866


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   17156
58921983  
00016717  00000-0  10270-3 0  9136
2 25544  51
6406  96
1403 0004633 240
6825 119
3865 15
53992189 19948


Satellite: ISS
Catalog Number: 25544
Epoch time:      17156
58921983   =   yrday
fracday
Element set:     913
Inclination:       51
6406  deg
RA of node:        96
1403  deg
Eccentricity:     
0004633     
Arg of perigee:   240
6825  deg
Mean anomaly:     119
3865  deg
Mean motion:   15
53992189  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1994
Checksum:              338


Coasting Arc #15 (Orbit 1997)
---------------------------------------

Vector Time (GMT): 2017/156/18:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923344
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1532447
34                 A    =         6789003
70  meter
 Y    =        6472525
31  meter          E    =           
0008869
 Z    =        1338033
28                 I    =           52
02805
 XDOT =      -4410
234654                 Wp   =           59
05647
 YDOT =      -2258
735517  meter/sec      RA   =           94
28692  deg
 ZDOT =       5851
060957                 TA   =          315
43118
                                          MA   =          315
50246
                                          Ha   =            220
122  n
mi
                                          Hp   =            216
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5027714
38                 X    =        -1611210
52
 Y    =       21235319
25  feet           Y    =         6454947
94  meter
 Z    =        4389872
97                 Z    =         1330398
29
 XDOT =     -14469
273800                 XDOT =       -4413
071054
 YDOT =      -7410
549597  feet/sec       YDOT =       -2308
070119  meter/sec
 ZDOT =      19196
394215                 ZDOT =        5829
630037

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6517015
93                 X    =         1986386
46
 Y    =      -20833860
35  feet           Y    =        -6350160
63  meter
 Z    =        4355048
39                 Z    =         1327418
75
 XDOT =      12526
077670                 XDOT =        3817
948474
 YDOT =       7928
041498  feet/sec       YDOT =        2416
467049  meter/sec
 ZDOT =      19102
148968                 ZDOT =        5822
335006


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   17156
84645078  
00016717  00000-0  10270-3 0  9144
2 25544  51
6378  94
8564 0004930 241
0910 118
9748 15
53983973 19989


Satellite: ISS
Catalog Number: 25544
Epoch time:      17156
84645078   =   yrday
fracday
Element set:     914
Inclination:       51
6378  deg
RA of node:        94
8564  deg
Eccentricity:     
0004930     
Arg of perigee:   241
0910  deg
Mean anomaly:     118
9748  deg
Mean motion:   15
53983973  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1998
Checksum:              357


Coasting Arc #16 (Orbit 2012)
---------------------------------------

Vector Time (GMT): 2017/157/18:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923344
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2183051
30                 A    =         6786233
72  meter
 Y    =       -5740583
97  meter          E    =           
0004113
 Z    =       -2880928
65                 I    =           52
02066
 XDOT =       4022
528938                 Wp   =          183
81990
 YDOT =       4083
207741  meter/sec      RA   =           89
33876  deg
 ZDOT =      -5091
728014                 TA   =           28
78026
                                          MA   =           28
75757
                                          Ha   =            220
012  n
mi
                                          Hp   =            216
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7162241
79                 X    =         2261076
09
 Y    =      -18833936
91  feet           Y    =        -5715735
05  meter
 Z    =       -9451865
65                 Z    =        -2870135
00
 XDOT =      13197
273419                 XDOT =        4001
303925
 YDOT =      13396
350856  feet/sec       YDOT =        4128
072237  meter/sec
 ZDOT =     -16705
144402                 ZDOT =       -5072
238676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8196966
10                 X    =        -2498435
27
 Y    =       18432096
61  feet           Y    =         5618103
05  meter
 Z    =       -9403202
25                 Z    =        -2866096
05
 XDOT =     -11244
791324                 XDOT =       -3427
412396
 YDOT =     -13473
325084  feet/sec       YDOT =       -4106
669485  meter/sec
 ZDOT =     -16619
792794                 ZDOT =       -5065
712844


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   17157
81107198  
00016717  00000-0  10270-3 0  9159
2 25544  51
6381  90
0483 0004837 245
6418 114
4230 15
53994713 20130


Satellite: ISS
Catalog Number: 25544
Epoch time:      17157
81107198   =   yrday
fracday
Element set:     915
Inclination:       51
6381  deg
RA of node:        90
0483  deg
Eccentricity:     
0004837     
Arg of perigee:   245
6418  deg
Mean anomaly:     114
4230  deg
Mean motion:   15
53994713  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2013
Checksum:              303


Coasting Arc #17 (Orbit 2028)
---------------------------------------

Vector Time (GMT): 2017/158/18:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923344
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2785278
72                 A    =         6782545
62  meter
 Y    =        4604995
12  meter          E    =           
0007040
 Z    =        4125978
36                 I    =           52
00706
 XDOT =      -3562
791699                 Wp   =          126
75575
 YDOT =      -5600
840577  meter/sec      RA   =           84
38146  deg
 ZDOT =       3837
376415                 TA   =          283
78065
                                          MA   =          283
85898
                                          Ha   =            219
864  n
mi
                                          Hp   =            216
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9138053
53                 X    =        -2856608
21
 Y    =       15108251
70  feet           Y    =         4573448
92  meter
 Z    =       13536674
40                 Z    =         4112275
46
 XDOT =     -11688
949144                 XDOT =       -3518
537169
 YDOT =     -18375
461210  feet/sec       YDOT =       -5640
435145  meter/sec
 ZDOT =      12589
817633                 ZDOT =        3820
176065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9749518
43                 X    =         2971653
22
 Y    =      -14777237
44  feet           Y    =        -4504101
97  meter
 Z    =       13475347
47                 Z    =         4107285
91
 XDOT =      10042
956506                 XDOT =        3061
093143
 YDOT =      18064
169694  feet/sec       YDOT =        5505
958923  meter/sec
 ZDOT =      12514
849623                 ZDOT =        3814
526165


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   17158
83999600  
00016717  00000-0  10270-3 0  9160
2 25544  51
6381  84
9195 0004941 248
9173 111
1451 15
54001951 20292


Satellite: ISS
Catalog Number: 25544
Epoch time:      17158
83999600   =   yrday
fracday
Element set:     916
Inclination:       51
6381  deg
RA of node:        84
9195  deg
Eccentricity:     
0004941     
Arg of perigee:   248
9173  deg
Mean anomaly:     111
1451  deg
Mean motion:   15
54001951  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2029
Checksum:              316


Coasting Arc #18 (Orbit 2043)
---------------------------------------

Vector Time (GMT): 2017/159/18:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923344
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3372174
45                 A    =         6779289
84  meter
 Y    =       -3140303
69  meter          E    =           
0007729
 Z    =       -4979571
35                 I    =           51
99167
 XDOT =       2998
165166                 Wp   =           76
36198
 YDOT =       6700
337583  meter/sec      RA   =           79
41532  deg
 ZDOT =      -2196
200754                 TA   =          172
31111
                                          MA   =          172
29926
                                          Ha   =            219
861  n
mi
                                          Hp   =            216
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11063564
46                 X    =         3431228
11
 Y    =      -10302833
64  feet           Y    =        -3102262
90  meter
 Z    =      -16337176
34                 Z    =        -4963047
17
 XDOT =       9836
499887                 XDOT =        2933
685589
 YDOT =      21982
734854  feet/sec       YDOT =        6733
504863  meter/sec
 ZDOT =      -7205
383051                 ZDOT =       -2181
792147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11351773
11                 X    =        -3460020
45
 Y    =       10103736
10  feet           Y    =         3079618
76  meter
 Z    =      -16263638
40                 Z    =        -4957156
99
 XDOT =      -8753
540216                 XDOT =       -2668
079058
 YDOT =     -21326
832334  feet/sec       YDOT =       -6500
418495  meter/sec
 ZDOT =      -7142
951926                 ZDOT =       -2177
171747


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   17159
80461051  
00016717  00000-0  10270-3 0  9173
2 25544  51
6377  80
1122 0004701 250
1709 109
8937 15
54002244 20445


Satellite: ISS
Catalog Number: 25544
Epoch time:      17159
80461051   =   yrday
fracday
Element set:     917
Inclination:       51
6377  deg
RA of node:        80
1122  deg
Eccentricity:     
0004701     
Arg of perigee:   250
1709  deg
Mean anomaly:     109
8937  deg
Mean motion:   15
54002244  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2044
Checksum:              282


Coasting Arc #19 (Orbit 2048)
---------------------------------------

Vector Time (GMT): 2017/160/01:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923344
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3518509
29                 A    =         6778609
33  meter
 Y    =        2706084
80  meter          E    =           
0004622
 Z    =        5124766
31                 I    =           51
99162
 XDOT =      -2834
072264                 Wp   =          186
46771
 YDOT =      -6917
433595  meter/sec      RA   =           77
97410  deg
 ZDOT =       1702
577101                 TA   =          247
13780
                                          MA   =          247
18661
                                          Ha   =            219
804  n
mi
                                          Hp   =            216
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11543665
65                 X    =        -3573401
80
 Y    =        8878230
98  feet           Y    =         2666430
83  meter
 Z    =       16813537
75                 Z    =         5107541
34
 XDOT =      -9298
137350                 XDOT =       -2764
779445
 YDOT =     -22694
992110  feet/sec       YDOT =       -6948
738903  meter/sec
 ZDOT =       5585
882876                 ZDOT =        1688
977264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11397591
53                 X    =        -3473985
90
 Y    =       -9205577
80  feet           Y    =        -2805860
11  meter
 Z    =       16736979
97                 Z    =         5101431
49
 XDOT =      19150
215507                 XDOT =        5836
985687
 YDOT =     -13635
384516  feet/sec       YDOT =       -4156
065201  meter/sec
 ZDOT =       5527
066452                 ZDOT =        1684
649855


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   17160
12614616  
00016717  00000-0  10270-3 0  9188
2 25544  51
6415  78
5113 0005020 251
0422 109
0187 15
54019416 20499


Satellite: ISS
Catalog Number: 25544
Epoch time:      17160
12614616   =   yrday
fracday
Element set:     918
Inclination:       51
6415  deg
RA of node:        78
5113  deg
Eccentricity:     
0005020     
Arg of perigee:   251
0422  deg
Mean anomaly:     109
0187  deg
Mean motion:   15
54019416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2049
Checksum:              271


Coasting Arc #20 (Orbit 2063)
---------------------------------------

Vector Time (GMT): 2017/161/01:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923344
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4054689
62                 A    =         6777770
90  meter
 Y    =       -1024012
36  meter          E    =           
0010141
 Z    =       -5342426
53                 I    =           51
98036
 XDOT =       2102
288319                 Wp   =           99
08916
 YDOT =       7364
701735  meter/sec      RA   =           72
99995  deg
 ZDOT =        182
657335                 TA   =          172
65257
                                          MA   =          172
63770
                                          Ha   =            219
629  n
mi
                                          Hp   =            216
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13302787
47                 X    =         4091790
13
 Y    =       -3359620
59  feet           Y    =         -978461
86  meter
 Z    =      -17527646
09                 Z    =        -5322639
98
 XDOT =       6897
271388                 XDOT =        2018
890779
 YDOT =      24162
407266  feet/sec       YDOT =        7387
744616  meter/sec
 ZDOT =        599
269472                 ZDOT =         192
668187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6666692
50                 X    =         2032007
87
 Y    =       12118938
48  feet           Y    =         3693852
45  meter
 Z    =      -17440072
36                 Z    =        -5315734
05
 XDOT =     -20727
170912                 XDOT =       -6317
641694
 YDOT =      12332
209205  feet/sec       YDOT =        3758
857366  meter/sec
 ZDOT =        642
140600                 ZDOT =         195
724455


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   17161
09075509  
00016717  00000-0  10270-3 0  9198
2 25544  51
6411  73
7041 0004996 255
7990 104
2608 15
53989585 20648


Satellite: ISS
Catalog Number: 25544
Epoch time:      17161
09075509   =   yrday
fracday
Element set:     919
Inclination:       51
6411  deg
RA of node:        73
7041  deg
Eccentricity:     
0004996     
Arg of perigee:   255
7990  deg
Mean anomaly:     104
2608  deg
Mean motion:   15
53989585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2064
Checksum:              330
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