[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: September 28th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


270/16:51:50 146 -1 0 1 5 1 5
N/A -0 9 -0 1 220 7
000/00:03:40 293 -0 5 -0 0 215 8

274/01:42:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 215 6

277/10:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 215 1

283/16:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 214 4

285/09:32:06 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 214 1

Coasting Arc #1 (Orbit 3765)
---------------------------------------

Vector Time (GMT): 2017/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2350450
21                 A    =         6788873
53  meter
 Y    =        6356133
57  meter          E    =           
0007266
 Z    =        -354077
06                 I    =           51
30942
 XDOT =      -4607
206511                 Wp   =          128
77093
 YDOT =       1376
006537  meter/sec      RA   =          247
30776  deg
 ZDOT =      -5970
175330                 TA   =           55
06205
                                          MA   =           54
99381
                                          Ha   =            220
686  n
mi
                                          Hp   =            215
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7711450
81                 X    =         2280919
49
 Y    =       20853456
59  feet           Y    =         6382029
11  meter
 Z    =       -1161670
16                 Z    =         -342828
53
 XDOT =     -15115
506926                 XDOT =       -4593
250473
 YDOT =       4514
457142  feet/sec       YDOT =        1324
563205  meter/sec
 ZDOT =     -19587
189403                 ZDOT =       -5992
522149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9717669
18                 X    =        -2961945
57
 Y    =      -20000280
38  feet           Y    =        -6096085
46  meter
 Z    =       -1112786
29                 Z    =         -339177
26
 XDOT =      13016
167379                 XDOT =        3967
327817
 YDOT =      -5245
605786  feet/sec       YDOT =       -1598
860643  meter/sec
 ZDOT =     -19686
280867                 ZDOT =       -6000
378408


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   17270
53152472  
00016717  00000-0  10270-3 0  9003
2 25544  51
6383 248
1268 0004361 331
9720  28
1198 15
54267279 37667


Satellite: ISS
Catalog Number: 25544
Epoch time:      17270
53152472   =   yrday
fracday
Element set:     900
Inclination:       51
6383  deg
RA of node:       248
1268  deg
Eccentricity:     
0004361     
Arg of perigee:   331
9720  deg
Mean anomaly:      28
1198  deg
Mean motion:   15
54267279  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3766
Checksum:              314


Coasting Arc #2 (Orbit 3768)
---------------------------------------

Vector Time (GMT): 2017/270/16:53:40
293
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2413826
91                 A    =         6779764
19  meter
 Y    =        4119967
43  meter          E    =           
0010532
 Z    =       -4822610
03                 I    =           51
28212
 XDOT =      -4614
613968                 Wp   =           49
49693
 YDOT =      -5594
307623  meter/sec      RA   =          246
30311  deg
 ZDOT =      -2466
356395                 TA   =          196
11333
                                          MA   =          196
14685
                                          Ha   =            220
667  n
mi
                                          Hp   =            215
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7919379
62                 X    =        -2436291
97
 Y    =       13516953
52  feet           Y    =         4092848
41  meter
 Z    =      -15822211
39                 Z    =        -4834390
64
 XDOT =     -15139
809607                 XDOT =       -4539
733491
 YDOT =     -18354
027635  feet/sec       YDOT =       -5645
492881  meter/sec
 ZDOT =      -8091
720457                 ZDOT =       -2488
590704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11815488
07                 X    =        -3601360
76
 Y    =      -10205286
63  feet           Y    =        -3110571
37  meter
 Z    =      -15874928
21                 Z    =        -4838678
12
 XDOT =      20108
184815                 XDOT =        6128
974732
 YDOT =     -10525
839174  feet/sec       YDOT =       -3208
275780  meter/sec
 ZDOT =      -8189
333712                 ZDOT =       -2496
108915


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   17270
72441677  
00016717  00000-0  10270-3 0  9013
2 25544  51
6414 247
1662 0004525 317
0297  43
0502 15
54010954 37699


Satellite: ISS
Catalog Number: 25544
Epoch time:      17270
72441677   =   yrday
fracday
Element set:     901
Inclination:       51
6414  deg
RA of node:       247
1662  deg
Eccentricity:     
0004525     
Arg of perigee:   317
0297  deg
Mean anomaly:      43
0502  deg
Mean motion:   15
54010954  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3769
Checksum:              296


Coasting Arc #3 (Orbit 3784)
---------------------------------------

Vector Time (GMT): 2017/271/16:53:40
293
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3342689
50                 A    =         6777807
49  meter
 Y    =       -2668709
32  meter          E    =           
0002114
 Z    =        5257669
92                 I    =           51
28907
 XDOT =       4119
606227                 Wp   =          353
76522
 YDOT =       6435
573488  meter/sec      RA   =          241
28200  deg
 ZDOT =        649
545755                 TA   =           90
01533
                                          MA   =           89
99111
                                          Ha   =            220
596  n
mi
                                          Hp   =            215
847

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10966829
07                 X    =         3346743
89
 Y    =       -8755608
01  feet           Y    =        -2631306
05  meter
 Z    =       17249573
21                 Z    =         5273917
83
 XDOT =      13515
768461                 XDOT =        4044
180552
 YDOT =      21114
086246  feet/sec       YDOT =        6481
220050  meter/sec
 ZDOT =       2131
055626                 ZDOT =         669
374030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6780445
24                 X    =         2066679
71
 Y    =       12184358
89  feet           Y    =         3713792
59  meter
 Z    =       17321857
53                 Z    =         5279702
18
 XDOT =     -22214
663649                 XDOT =       -6771
029480
 YDOT =       9218
790391  feet/sec       YDOT =        2809
887311  meter/sec
 ZDOT =       2217
921472                 ZDOT =         676
022465


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   17271
75333944  
00016717  00000-0  10270-3 0  9025
2 25544  51
6407 242
0382 0004521 319
5887  40
4930 15
54022078 37856


Satellite: ISS
Catalog Number: 25544
Epoch time:      17271
75333944   =   yrday
fracday
Element set:     902
Inclination:       51
6407  deg
RA of node:       242
0382  deg
Eccentricity:     
0004521     
Arg of perigee:   319
5887  deg
Mean anomaly:      40
4930  deg
Mean motion:   15
54022078  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3785
Checksum:              305


Coasting Arc #4 (Orbit 3799)
---------------------------------------

Vector Time (GMT): 2017/272/16:53:40
293
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4226183
28                 A    =         6778151
38  meter
 Y    =        1147007
67  meter          E    =           
0011227
 Z    =       -5183127
58                 I    =           51
30698
 XDOT =      -3344
512397                 Wp   =           83
10208
 YDOT =      -6781
083201  meter/sec      RA   =          236
26011  deg
 ZDOT =       1230
018938                 TA   =          198
74907
                                          MA   =          198
79045
                                          Ha   =            220
788  n
mi
                                          Hp   =            215
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13865430
71                 X    =        -4213518
08
 Y    =        3763148
52  feet           Y    =         1099818
03  meter
 Z    =      -17005011
74                 Z    =        -5203626
51
 XDOT =     -10972
809701                 XDOT =       -3274
410813
 YDOT =     -22247
648296  feet/sec       YDOT =       -6818
091765  meter/sec
 ZDOT =       4035
495202                 ZDOT =        1213
943015

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1611386
51                 X    =         -491150
61
 Y    =      -14167403
72  feet           Y    =        -4318224
66  meter
 Z    =      -17095905
51                 Z    =        -5210832
00
 XDOT =      22636
065968                 XDOT =        6899
472907
 YDOT =      -7345
251347  feet/sec       YDOT =       -2238
832610  meter/sec
 ZDOT =       3965
265561                 ZDOT =        1208
612943


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   17272
71795086  
00016717  00000-0  10270-3 0  9032
2 25544  51
6408 237
2310 0004612 322
7213  37
3619 15
54020117 38003


Satellite: ISS
Catalog Number: 25544
Epoch time:      17272
71795086   =   yrday
fracday
Element set:     903
Inclination:       51
6408  deg
RA of node:       237
2310  deg
Eccentricity:     
0004612     
Arg of perigee:   322
7213  deg
Mean anomaly:      37
3619  deg
Mean motion:   15
54020117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3800
Checksum:              279


Coasting Arc #5 (Orbit 3815)
---------------------------------------

Vector Time (GMT): 2017/273/16:53:40
293
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4988853
02                 A    =         6780521
09  meter
 Y    =         364397
63  meter          E    =           
0009004
 Z    =        4576891
03                 I    =           51
33482
 XDOT =       2277
693083                 Wp   =           34
33854
 YDOT =       6676
931422  meter/sec      RA   =          231
24280  deg
 ZDOT =      -3004
102422                 TA   =           85
82995
                                          MA   =           85
72705
                                          Ha   =            220
818  n
mi
                                          Hp   =            215
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16367628
03                 X    =         4962175
06
 Y    =        1195530
27  feet           Y    =          420037
62  meter
 Z    =       15016046
68                 Z    =         4601060
61
 XDOT =       7472
746334                 XDOT =        2217
453097
 YDOT =      21905
942987  feet/sec       YDOT =        6702
065057  meter/sec
 ZDOT =      -9855
979075                 ZDOT =       -2993
184942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3399850
27                 X    =        -1036274
36
 Y    =       15954508
47  feet           Y    =         4862934
18  meter
 Z    =       15122991
62                 Z    =         4609487
85
 XDOT =     -21563
716835                 XDOT =       -6572
620891
 YDOT =       4733
691741  feet/sec       YDOT =        1442
829243  meter/sec
 ZDOT =      -9808
550366                 ZDOT =       -2989
646151


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   17273
74686146  
00016717  00000-0  10270-3 0  9043
2 25544  51
6413 232
1027 0004759 326
7128  33
3724 15
54058911 38162


Satellite: ISS
Catalog Number: 25544
Epoch time:      17273
74686146   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:       232
1027  deg
Eccentricity:     
0004759     
Arg of perigee:   326
7128  deg
Mean anomaly:      33
3724  deg
Mean motion:   15
54058911  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3816
Checksum:              309


Coasting Arc #6 (Orbit 3821)
---------------------------------------

Vector Time (GMT): 2017/274/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3502425
11                 A    =         6788979
64  meter
 Y    =       -5663233
20  meter          E    =           
0014185
 Z    =        1278958
90                 I    =           51
36945
 XDOT =       4738
208604                 Wp   =           42
07058
 YDOT =      -1610
982349  meter/sec      RA   =          229
43569  deg
 ZDOT =       5814
996419                 TA   =          331
90200
                                          MA   =          331
97848
                                          Ha   =            220
875  n
mi
                                          Hp   =            215
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11490896
04                 X    =        -3445049
60
 Y    =      -18580161
41  feet           Y    =        -5702078
78  meter
 Z    =        4196059
39                 Z    =         1262085
02
 XDOT =      15545
303818                 XDOT =        4727
624364
 YDOT =      -5285
375161  feet/sec       YDOT =       -1558
055109  meter/sec
 ZDOT =      19078
072242                 ZDOT =        5837
987702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20034729
29                 X    =        -6106585
49
 Y    =       -8745728
04  feet           Y    =        -2665697
91  meter
 Z    =        4122119
32                 Z    =         1256421
97
 XDOT =       9049
604144                 XDOT =        2758
319343
 YDOT =     -11647
996689  feet/sec       YDOT =       -3550
309391  meter/sec
 ZDOT =      19180
069635                 ZDOT =        5846
085225


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   17274
13270288  
00016717  00000-0  10270-3 0  9054
2 25544  51
6407 230
1745 0004167 326
3860  33
7028 15
54020231 38224


Satellite: ISS
Catalog Number: 25544
Epoch time:      17274
13270288   =   yrday
fracday
Element set:     905
Inclination:       51
6407  deg
RA of node:       230
1745  deg
Eccentricity:     
0004167     
Arg of perigee:   326
3860  deg
Mean anomaly:      33
7028  deg
Mean motion:   15
54020231  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3822
Checksum:              282


Coasting Arc #7 (Orbit 3836)
---------------------------------------

Vector Time (GMT): 2017/275/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2511352
18                 A    =         6786259
35  meter
 Y    =        5633501
55  meter          E    =           
0002296
 Z    =       -2833585
78                 I    =           51
38199
 XDOT =      -5753
140156                 Wp   =           57
56822
 YDOT =         20
001067  meter/sec      RA   =          224
44396  deg
 ZDOT =      -5060
931410                 TA   =          154
72816
                                          MA   =          154
71693
                                          Ha   =            220
944  n
mi
                                          Hp   =            215
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8239344
44                 X    =         2461934
45
 Y    =       18482616
63  feet           Y    =         5661308
58  meter
 Z    =       -9296541
28                 Z    =        -2821507
01
 XDOT =     -18875
131744                 XDOT =       -5728
352600
 YDOT =         65
620298  feet/sec       YDOT =         -44
196435  meter/sec
 ZDOT =     -16604
105677                 ZDOT =       -5088
818291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17508818
50                 X    =         5336687
88
 Y    =       10193766
14  feet           Y    =         3107059
92  meter
 Z    =       -9243808
78                 Z    =        -2817512
92
 XDOT =     -14476
408255                 XDOT =       -4412
409236
 YDOT =       9701
340444  feet/sec       YDOT =        2956
968567  meter/sec
 ZDOT =     -16727
572973                 ZDOT =       -5098
564242


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   17275
09729952  
00016717  00000-0  10270-3 0  9068
2 25544  51
6402 225
3673 0004146 328
5847  31
5058 15
54026902 38377


Satellite: ISS
Catalog Number: 25544
Epoch time:      17275
09729952   =   yrday
fracday
Element set:     906
Inclination:       51
6402  deg
RA of node:       225
3673  deg
Eccentricity:     
0004146     
Arg of perigee:   328
5847  deg
Mean anomaly:      31
5058  deg
Mean motion:   15
54026902  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3837
Checksum:              319


Coasting Arc #8 (Orbit 3852)
---------------------------------------

Vector Time (GMT): 2017/276/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1256234
76                 A    =         6782432
62  meter
 Y    =       -5258861
94  meter          E    =           
0008470
 Z    =        4086674
46                 I    =           51
39442
 XDOT =       6506
424274                 Wp   =           81
58663
 YDOT =       1412
002616  meter/sec      RA   =          219
44423  deg
 ZDOT =       3811
509444                 TA   =          328
91131
                                          MA   =          328
96141
                                          Ha   =            220
948  n
mi
                                          Hp   =            215
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4121505
13                 X    =        -1217186
58
 Y    =      -17253484
06  feet           Y    =        -5272691
17  meter
 Z    =       13407724
61                 Z    =         4080667
54
 XDOT =      21346
536332                 XDOT =        6471
636760
 YDOT =       4632
554515  feet/sec       YDOT =        1484
567867  meter/sec
 ZDOT =      12504
952244                 ZDOT =        3843
031142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13664196
33                 X    =        -4164847
04
 Y    =      -11342549
42  feet           Y    =        -3457209
06  meter
 Z    =       13381812
56                 Z    =         4078776
47
 XDOT =      19007
852124                 XDOT =        5793
593327
 YDOT =      -7959
256921  feet/sec       YDOT =       -2425
981509  meter/sec
 ZDOT =      12644
337154                 ZDOT =        3853
993965


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   17276
12619462  
00016717  00000-0  10270-3 0  9078
2 25544  51
6410 220
2389 0004142 331
6701  28
4226 15
54071413 38531


Satellite: ISS
Catalog Number: 25544
Epoch time:      17276
12619462   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       220
2389  deg
Eccentricity:     
0004142     
Arg of perigee:   331
6701  deg
Mean anomaly:      28
4226  deg
Mean motion:   15
54071413  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3853
Checksum:              283


Coasting Arc #9 (Orbit 3867)
---------------------------------------

Vector Time (GMT): 2017/277/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -208398
44                 A    =         6779243
69  meter
 Y    =        4643130
45  meter          E    =           
0012428
 Z    =       -4946381
86                 I    =           51
40971
 XDOT =      -6865
856920                 Wp   =           54
28213
 YDOT =      -2615
311092  meter/sec      RA   =          214
43679  deg
 ZDOT =      -2162
424127                 TA   =          194
52413
                                          MA   =          194
55988
                                          Ha   =            221
124  n
mi
                                          Hp   =            215
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -683721
93                 X    =         -236276
36
 Y    =       15233367
62  feet           Y    =         4640643
45  meter
 Z    =      -16228286
94                 Z    =        -4947462
55
 XDOT =     -22525
777295                 XDOT =       -6825
597436
 YDOT =      -8580
416970  feet/sec       YDOT =       -2691
864983  meter/sec
 ZDOT =      -7094
567346                 ZDOT =       -2195
678485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8831685
04                 X    =         2691897
60
 Y    =       12423750
53  feet           Y    =         3786759
16  meter
 Z    =      -16233669
44                 Z    =        -4948022
45
 XDOT =     -22142
017066                 XDOT =       -6748
886802
 YDOT =       6263
879431  feet/sec       YDOT =        1909
230451  meter/sec
 ZDOT =      -7241
483037                 ZDOT =       -2207
204030


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   17277
09077884  
00016717  00000-0  10270-3 0  9082
2 25544  51
6414 215
4317 0004291 335
1356  24
9589 15
54035589 38685


Satellite: ISS
Catalog Number: 25544
Epoch time:      17277
09077884   =   yrday
fracday
Element set:     908
Inclination:       51
6414  deg
RA of node:       215
4317  deg
Eccentricity:     
0004291     
Arg of perigee:   335
1356  deg
Mean anomaly:      24
9589  deg
Mean motion:   15
54035589  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3868
Checksum:              341


Coasting Arc #10 (Orbit 3873)
---------------------------------------

Vector Time (GMT): 2017/277/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         612910
87                 A    =         6780157
87  meter
 Y    =        4847861
32  meter          E    =           
0011847
 Z    =       -4711529
93                 I    =           51
42126
 XDOT =      -6915
223890                 Wp   =           47
88293
 YDOT =      -1804
428883  meter/sec      RA   =          212
51880  deg
 ZDOT =      -2752
898682                 TA   =          194
72554
                                          MA   =          194
76007
                                          Ha   =            221
334  n
mi
                                          Hp   =            215
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2010862
43                 X    =          581541
79
 Y    =       15905056
82  feet           Y    =         4854539
26  meter
 Z    =      -15457775
36                 Z    =        -4708629
43
 XDOT =     -22687
742422                 XDOT =       -6881
159955
 YDOT =      -5920
042268  feet/sec       YDOT =       -1881
569555  meter/sec
 ZDOT =      -9031
819823                 ZDOT =       -2786
408061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1125483
42                 X    =         -343047
35
 Y    =      -16003918
85  feet           Y    =        -4877994
47  meter
 Z    =      -15445552
36                 Z    =        -4707804
36
 XDOT =      21051
892858                 XDOT =        6416
616943
 YDOT =       7389
747137  feet/sec       YDOT =        2252
394927  meter/sec
 ZDOT =      -9179
974327                 ZDOT =       -2798
056175


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   17277
47661093  
00016717  00000-0  10270-3 0  9096
2 25544  51
6393 213
5102 0004678 341
8085  18
2899 15
54058584 38741


Satellite: ISS
Catalog Number: 25544
Epoch time:      17277
47661093   =   yrday
fracday
Element set:     909
Inclination:       51
6393  deg
RA of node:       213
5102  deg
Eccentricity:     
0004678     
Arg of perigee:   341
8085  deg
Mean anomaly:      18
2899  deg
Mean motion:   15
54058584  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3874
Checksum:              341


Coasting Arc #11 (Orbit 3889)
---------------------------------------

Vector Time (GMT): 2017/278/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         987945
81                 A    =         6777767
32  meter
 Y    =       -4189195
36  meter          E    =           
0003165
 Z    =        5233850
26                 I    =           51
44185
 XDOT =       7064
892480                 Wp   =           33
23709
 YDOT =       2835
762516  meter/sec      RA   =          207
50928  deg
 ZDOT =        938
508354                 TA   =           47
77437
                                          MA   =           47
74751
                                          Ha   =            221
285  n
mi
                                          Hp   =            215
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3241292
03                 X    =         1009293
21
 Y    =      -13744079
26  feet           Y    =        -4178027
40  meter
 Z    =       17171424
75                 Z    =         5238701
89
 XDOT =      23178
781104                 XDOT =        7028
098265
 YDOT =       9303
682796  feet/sec       YDOT =        2914
561366  meter/sec
 ZDOT =       3079
095649                 ZDOT =         972
738174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3738562
16                 X    =        -1139513
75
 Y    =       13589415
17  feet           Y    =         4142053
74  meter
 Z    =       17193442
50                 Z    =         5240561
27
 XDOT =     -21728
993862                 XDOT =       -6622
997329
 YDOT =     -10055
212903  feet/sec       YDOT =       -3064
828893  meter/sec
 ZDOT =       3230
322976                 ZDOT =         984
602443


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   17278
50548821  
00016717  00000-0  10270-3 0  9106
2 25544  51
6393 208
3828 0004740 344
0397  16
0606 15
54093547 38907


Satellite: ISS
Catalog Number: 25544
Epoch time:      17278
50548821   =   yrday
fracday
Element set:     910
Inclination:       51
6393  deg
RA of node:       208
3828  deg
Eccentricity:     
0004740     
Arg of perigee:   344
0397  deg
Mean anomaly:      16
0606  deg
Mean motion:   15
54093547  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3890
Checksum:              317


Coasting Arc #12 (Orbit 3904)
---------------------------------------

Vector Time (GMT): 2017/279/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2610689
40                 A    =         6777790
06  meter
 Y    =        3433955
70  meter          E    =           
0013629
 Z    =       -5239068
63                 I    =           51
47166
 XDOT =      -6686
097329                 Wp   =           78
56636
 YDOT =      -3607
056580  meter/sec      RA   =          202
49723  deg
 ZDOT =        972
305432                 TA   =          200
74505
                                          MA   =          200
80042
                                          Ha   =            221
451  n
mi
                                          Hp   =            214
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8565253
92                 X    =        -2623445
44
 Y    =       11266258
86  feet           Y    =         3404689
21  meter
 Z    =      -17188545
36                 Z    =        -5251782
21
 XDOT =     -21936
014859                 XDOT =       -6649
988410
 YDOT =     -11834
175131  feet/sec       YDOT =       -3681
623066  meter/sec
 ZDOT =       3189
978450                 ZDOT =         939
913965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8758038
41                 X    =         2669450
11
 Y    =      -11028830
54  feet           Y    =        -3361587
55  meter
 Z    =      -17245286
75                 Z    =        -5256363
40
 XDOT =      20819
466302                 XDOT =        6345
773329
 YDOT =      11792
921950  feet/sec       YDOT =        3594
482610  meter/sec
 ZDOT =       3046
976310                 ZDOT =         928
718379


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   17279
47005459  
00016717  00000-0  10270-3 0  9119
2 25544  51
6397 203
5746 0004702 348
0132  12
0908 15
54076833 39053


Satellite: ISS
Catalog Number: 25544
Epoch time:      17279
47005459   =   yrday
fracday
Element set:     911
Inclination:       51
6397  deg
RA of node:       203
5746  deg
Eccentricity:     
0004702     
Arg of perigee:   348
0132  deg
Mean anomaly:      12
0908  deg
Mean motion:   15
54076833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3905
Checksum:              306


Coasting Arc #13 (Orbit 3920)
---------------------------------------

Vector Time (GMT): 2017/280/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4147780
76                 A    =         6780000
88  meter
 Y    =       -2601486
05  meter          E    =           
0010400
 Z    =        4688295
05                 I    =           51
51041
 XDOT =       5796
018732                 Wp   =           37
79160
 YDOT =       4165
163980  meter/sec      RA   =          197
49106  deg
 ZDOT =      -2805
229764                 TA   =           80
12860
                                          MA   =           80
01121
                                          Ha   =            221
459  n
mi
                                          Hp   =            214
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13608204
59                 X    =         4153789
03
 Y    =       -8535059
21  feet           Y    =        -2555068
63  meter
 Z    =       15381545
45                 Z    =         4708459
02
 XDOT =      19015
809489                 XDOT =        5762
638729
 YDOT =      13665
236154  feet/sec       YDOT =        4229
792075  meter/sec
 ZDOT =      -9203
509725                 ZDOT =       -2777
155385

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13593542
90                 X    =        -4143311
88
 Y    =        8395259
43  feet           Y    =         2558875
07  meter
 Z    =       15471186
73                 Z    =         4715617
72
 XDOT =     -18322
893361                 XDOT =       -5584
817896
 YDOT =     -12867
535781  feet/sec       YDOT =       -3922
024906  meter/sec
 ZDOT =      -9079
685681                 ZDOT =       -2767
488195


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   17280
49891442  
00016717  00000-0  10270-3 0  9129
2 25544  51
6402 198
4467 0004752 351
8456   8
2619 15
54092154 39216


Satellite: ISS
Catalog Number: 25544
Epoch time:      17280
49891442   =   yrday
fracday
Element set:     912
Inclination:       51
6402  deg
RA of node:       198
4467  deg
Eccentricity:     
0004752     
Arg of perigee:   351
8456  deg
Mean anomaly:       8
2619  deg
Mean motion:   15
54092154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3921
Checksum:              319


Coasting Arc #14 (Orbit 3935)
---------------------------------------

Vector Time (GMT): 2017/281/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5413717
83                 A    =         6783563
70  meter
 Y    =        1789754
36  meter          E    =           
0006425
 Z    =       -3676240
17                 I    =           51
55316
 XDOT =      -4429
167239                 Wp   =           55
56652
 YDOT =      -4508
077001  meter/sec      RA   =          192
49503  deg
 ZDOT =       4336
735509                 TA   =          260
65368
                                          MA   =          260
72634
                                          Ha   =            221
573  n
mi
                                          Hp   =            214
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17761541
42                 X    =        -5415471
17
 Y    =        5871897
51  feet           Y    =         1729204
35  meter
 Z    =      -12061155
41                 Z    =        -3702543
38
 XDOT =     -14531
388581                 XDOT =       -4399
493782
 YDOT =     -14790
278876  feet/sec       YDOT =       -4557
440679  meter/sec
 ZDOT =      14228
134871                 ZDOT =        4315
291935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17640631
94                 X    =         5376864
61
 Y    =       -5994151
64  feet           Y    =        -1827017
42  meter
 Z    =      -12177900
27                 Z    =        -3711824
00
 XDOT =      14290
170160                 XDOT =        4355
643865
 YDOT =      13400
321032  feet/sec       YDOT =        4084
417851  meter/sec
 ZDOT =      14133
714300                 ZDOT =        4307
956119


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   17281
46346180  
00016717  00000-0  10270-3 0  9132
2 25544  51
6395 193
6389 0004804 355
7974   4
3138 15
54101777 39364


Satellite: ISS
Catalog Number: 25544
Epoch time:      17281
46346180   =   yrday
fracday
Element set:     913
Inclination:       51
6395  deg
RA of node:       193
6389  deg
Eccentricity:     
0004804     
Arg of perigee:   355
7974  deg
Mean anomaly:       4
3138  deg
Mean motion:   15
54101777  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3936
Checksum:              330


Coasting Arc #15 (Orbit 3951)
---------------------------------------

Vector Time (GMT): 2017/282/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6326911
93                 A    =         6787131
52  meter
 Y    =        -963990
31  meter          E    =           
0013103
 Z    =        2249167
20                 I    =           51
59765
 XDOT =       2660
576409                 Wp   =           87
98105
 YDOT =       4701
290354  meter/sec      RA   =          187
51163  deg
 ZDOT =      -5441
364249                 TA   =           66
98951
                                          MA   =           66
85136
                                          Ha   =            221
659  n
mi
                                          Hp   =            214
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20757585
06                 X    =         6326295
69
 Y    =       -3162697
87  feet           Y    =         -893241
76  meter
 Z    =        7379157
47                 Z    =         2279900
65
 XDOT =       8728
925228                 XDOT =        2634
239681
 YDOT =      15424
180952  feet/sec       YDOT =        4730
895117  meter/sec
 ZDOT =     -17852
244912                 ZDOT =       -5428
503976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20626217
96                 X    =        -6286871
24
 Y    =        3661862
59  feet           Y    =         1116135
72  meter
 Z    =        7515441
13                 Z    =         2290706
46
 XDOT =      -8949
145282                 XDOT =       -2727
699482
 YDOT =     -13700
236736  feet/sec       YDOT =       -4175
832157  meter/sec
 ZDOT =     -17795
865496                 ZDOT =       -5424
179803


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   17282
49230423  
00016717  00000-0  10270-3 0  9149
2 25544  51
6398 188
5106 0004774 358
9744   1
1398 15
54120155 39525


Satellite: ISS
Catalog Number: 25544
Epoch time:      17282
49230423   =   yrday
fracday
Element set:     914
Inclination:       51
6398  deg
RA of node:       188
5106  deg
Eccentricity:     
0004774     
Arg of perigee:   358
9744  deg
Mean anomaly:       1
1398  deg
Mean motion:   15
54120155  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3952
Checksum:              318


Coasting Arc #16 (Orbit 3966)
---------------------------------------

Vector Time (GMT): 2017/283/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6750182
26                 A    =         6789152
65  meter
 Y    =         190084
12  meter          E    =           
0014732
 Z    =        -617480
84                 I    =           51
63684
 XDOT =       -674
105509                 Wp   =           29
08412
 YDOT =      -4764
048631  meter/sec      RA   =          182
53761  deg
 ZDOT =       5975
070336                 TA   =          324
24682
                                          MA   =          324
34538
                                          Ha   =            221
714  n
mi
                                          Hp   =            214
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22146267
25                 X    =        -6748806
66
 Y    =         623635
55  feet           Y    =          114606
63  meter
 Z    =       -2025855
77                 Z    =         -650268
46
 XDOT =      -2211
632249                 XDOT =        -649
807093
 YDOT =     -15630
080809  feet/sec       YDOT =       -4771
450781  meter/sec
 ZDOT =      19603
249133                 ZDOT =        5971
854929

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22087756
93                 X    =         6732348
31
 Y    =       -1538574
01  feet           Y    =         -468957
36  meter
 Z    =       -2171163
19                 Z    =         -661770
54
 XDOT =       2872
572240                 XDOT =         875
560019
 YDOT =      13907
600345  feet/sec       YDOT =        4239
036585  meter/sec
 ZDOT =      19589
607904                 ZDOT =        5970
912489


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   17283
45683454  
00016717  00000-0  10270-3 0  9153
2 25544  51
6397 183
7023 0004840   1
8107 358
3062 15
54125617 39679


Satellite: ISS
Catalog Number: 25544
Epoch time:      17283
45683454   =   yrday
fracday
Element set:     915
Inclination:       51
6397  deg
RA of node:       183
7023  deg
Eccentricity:     
0004840     
Arg of perigee:     1
8107  deg
Mean anomaly:     358
3062  deg
Mean motion:   15
54125617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3967
Checksum:              316


Coasting Arc #17 (Orbit 3970)
---------------------------------------

Vector Time (GMT): 2017/283/16:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1013799
75                 A    =         6777674
30  meter
 Y    =        4184113
82  meter          E    =           
0015854
 Z    =       -5248152
29                 I    =           51
60376
 XDOT =      -7570
352342                 Wp   =           65
64624
 YDOT =        599
063951  meter/sec      RA   =          181
34968  deg
 ZDOT =       -980
728885                 TA   =          194
92462
                                          MA   =          194
97146
                                          Ha   =            221
717  n
mi
                                          Hp   =            214
382

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3326114
66                 X    =          992429
96
 Y    =       13727407
56  feet           Y    =         4195331
09  meter
 Z    =      -17218347
40                 Z    =        -5243279
57
 XDOT =     -24837
113983                 XDOT =       -7571
724596
 YDOT =       1965
432910  feet/sec       YDOT =         514
399387  meter/sec
 ZDOT =      -3217
614453                 ZDOT =       -1017
507375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13770778
49                 X    =        -4197333
28
 Y    =        3255023
13  feet           Y    =          992131
05  meter
 Z    =      -17197288
41                 Z    =        -5241733
51
 XDOT =      -1395
536542                 XDOT =        -425
359538
 YDOT =     -23835
363306  feet/sec       YDOT =       -7265
018736  meter/sec
 ZDOT =      -3380
663625                 ZDOT =       -1030
426273


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   17283
71403971  
00016717  00000-0  10270-3 0  9167
2 25544  51
6371 182
4174 0004684   2
5995 357
5182 15
54141890 39713


Satellite: ISS
Catalog Number: 25544
Epoch time:      17283
71403971   =   yrday
fracday
Element set:     916
Inclination:       51
6371  deg
RA of node:       182
4174  deg
Eccentricity:     
0004684     
Arg of perigee:     2
5995  deg
Mean anomaly:     357
5182  deg
Mean motion:   15
54141890  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3971
Checksum:              324


Coasting Arc #18 (Orbit 3986)
---------------------------------------

Vector Time (GMT): 2017/284/16:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         831109
53                 A    =         6777657
04  meter
 Y    =       -4211499
00  meter          E    =           
0007295
 Z    =        5242762
98                 I    =           51
63594
 XDOT =       7603
799445                 Wp   =           28
99759
 YDOT =        284
266355  meter/sec      RA   =          176
34811  deg
 ZDOT =       -970
234566                 TA   =           70
32507
                                          MA   =           70
24637
                                          Ha   =            221
784  n
mi
                                          Hp   =            214
301

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2726737
29                 X    =          852674
71
 Y    =      -13817253
92  feet           Y    =        -4202084
16  meter
 Z    =       17200665
95                 Z    =         5246852
87
 XDOT =      24946
848574                 XDOT =        7604
768565
 YDOT =        932
632397  feet/sec       YDOT =         369
302606  meter/sec
 ZDOT =      -3183
184273                 ZDOT =        -933
294776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13825713
57                 X    =         4214077
50
 Y    =        2561026
72  feet           Y    =          780600
94  meter
 Z    =       17219329
19                 Z    =         5248451
54
 XDOT =       -650
254382                 XDOT =        -198
197536
 YDOT =      23962
389960  feet/sec       YDOT =        7303
736460  meter/sec
 ZDOT =      -3019
507624                 ZDOT =        -920
345924


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   17284
74286229  
00016717  00000-0  10270-3 0  9177
2 25544  51
6367 177
2882 0004654   6
5964 353
5249 15
54119219 39870


Satellite: ISS
Catalog Number: 25544
Epoch time:      17284
74286229   =   yrday
fracday
Element set:     917
Inclination:       51
6367  deg
RA of node:       177
2882  deg
Eccentricity:     
0004654     
Arg of perigee:     6
5964  deg
Mean anomaly:     353
5249  deg
Mean motion:   15
54119219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3987
Checksum:              351


Coasting Arc #19 (Orbit 3997)
---------------------------------------

Vector Time (GMT): 2017/285/09:32:06
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3361562
99                 A    =         6779476
72  meter
 Y    =       -3403079
81  meter          E    =           
0007345
 Z    =        4797474
19                 I    =           51
66766
 XDOT =       6620
941980                 Wp   =           81
70820
 YDOT =      -2888
482605  meter/sec      RA   =          172
88553  deg
 ZDOT =       2587
966455                 TA   =          342
81418
                                          MA   =          342
83904
                                          Ha   =            221
871  n
mi
                                          Hp   =            214
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11028749
98                 X    =        -3346563
07
 Y    =      -11164960
01  feet           Y    =        -3440587
01  meter
 Z    =       15739744
70                 Z    =         4781181
15
 XDOT =      21722
250590                 XDOT =        6640
178455
 YDOT =      -9476
648968  feet/sec       YDOT =       -2814
335038  meter/sec
 ZDOT =       8490
703592                 ZDOT =        2620
176179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7456678
35                 X    =         2272795
56
 Y    =       13890360
79  feet           Y    =         4233781
97  meter
 Z    =       15667962
43                 Z    =         4775594
95
 XDOT =     -22461
866188                 XDOT =       -6846
376814
 YDOT =       2310
589181  feet/sec       YDOT =         704
267583  meter/sec
 ZDOT =       8633
837198                 ZDOT =        2631
593578


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   17285
45017287  
00016717  00000-0  10270-3 0  9183
2 25544  51
6391 173
7652 0004747   8
4308 351
6924 15
54183593 39986


Satellite: ISS
Catalog Number: 25544
Epoch time:      17285
45017287   =   yrday
fracday
Element set:     918
Inclination:       51
6391  deg
RA of node:       173
7652  deg
Eccentricity:     
0004747     
Arg of perigee:     8
4308  deg
Mean anomaly:     351
6924  deg
Mean motion:   15
54183593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3998
Checksum:              343
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